Diamond Aircraft DV 20 E 2022 Airplane Maintenance Manual Download

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AIRCRAFT

DV 20 E AMM

Time Limits and

Maintenance Checks

Interval

Inspection Items, Center Fuselage, Internal

100

200 1000 Initials

Doc # 4.02.25

Rev. 2

05-28-50

Page 9

15 Mar 2022

21.

With the wings removed perform a visual inspection and a tap

test of the spar bridge.

Examine the condition of the laminates and the bond to

the fuselage.

Look especially around:

The LH and RH A-bolt bushing.

The B-bolt bushing.

The MLG brackets.

The LH and RH top aft outer corners (behind the

back-rest).

The seat fastener through the side of the spar bridge (if

applicable).

Do a visual inspection of the inside spar bridge.

Refer to Chapter 51-10.

22.

Install the B-Bulkhead cover plate (connect antenna).

23.

Install the bottom center fuselage panels.

Summary of Contents for DV 20 E 2022

Page 1: ...AIRCRAFT DV 20 E AIRPLANE MAINTENANCE MANUAL Copyright by DIAMOND AIRCRAFT INDUSTRIES Wiener Neustadt Austria...

Page 2: ...f translation reprinting radio transmission reproduction by photo mechanical or similar means and storing in data processing facilities in whole or part are reserved Diamond Aircraft Industries GmbH N...

Page 3: ...5 28 50 Maintenance Checklist Airframe 05 28 70 6000 Hour Inspection 05 28 90 Maintenance Report 05 28 91 Engine Ground Test Record 05 28 92 Check Flight Report 05 50 Unscheduled Maintenance Checks 06...

Page 4: ...trols Flaps 28 00 Fuel 28 10 Fuel Storage 28 20 Fuel Distribution 28 40 Fuel Indicating 31 00 Indicating Systems 31 10 Instrument and Control Panels 31 20 Independent Instruments 31 50 Warning Systems...

Page 5: ...r Fin 55 40 Rudder and Trim Tab 56 00 Windows 56 10 Repair of the Canopy Glass 56 11 Replacement of the Rear Window 57 00 Wings 57 10 Wing Structure 57 50 Flaps 57 60 Ailerons 61 00 Propeller 61 10 Pr...

Page 6: ...AIRCRAFT Table of Contents DV 20 E AMM Page iv 15 Mar 2022 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 7: ...u put in this Airplane Maintenance Manual AMM Put the affected pages of the revision into the AMM as soon as you get them Remove and destroy the pages which are superseded Complete the table below whe...

Page 8: ...re incorporated into the DV 20 E AMM by Revision 2 Temporary Revision Number Description of Temporary Revision AMM TR M M 20 446 Weighing Report Improvement AMM TR M M 20 450 Wiring Improvement AMM TR...

Page 9: ...10 15 Mar 2022 LOEP 11 15 Mar 2022 LOEP 12 15 Mar 2022 Chapter Section Page Revision Date 01 00 Title 1 15 Mar 2022 01 00 Title 2 15 Mar 2022 01 00 TOC 1 15 Mar 2022 01 00 TOC 2 15 Mar 2022 01 00 1 1...

Page 10: ...05 28 50 6 15 Mar 2022 05 28 50 7 15 Mar 2022 05 28 50 8 15 Mar 2022 05 28 50 9 15 Mar 2022 05 28 50 10 15 Mar 2022 05 28 50 11 15 Mar 2022 05 28 50 12 15 Mar 2022 05 28 50 13 15 Mar 2022 05 28 50 14...

Page 11: ...22 12 00 TOC 2 15 Mar 2022 12 00 1 15 Mar 2022 12 00 2 15 Mar 2022 12 10 1 15 Mar 2022 12 10 2 15 Mar 2022 12 10 3 15 Mar 2022 12 10 4 15 Mar 2022 12 10 5 15 Mar 2022 12 10 6 15 Mar 2022 12 10 7 15 Ma...

Page 12: ...00 5 15 Mar 2022 24 00 6 15 Mar 2022 24 30 1 15 Mar 2022 24 30 2 15 Mar 2022 24 31 1 15 Mar 2022 24 31 2 15 Mar 2022 24 31 101 15 Mar 2022 24 31 102 15 Mar 2022 24 31 201 15 Mar 2022 24 31 202 15 Mar...

Page 13: ...r 2022 27 10 207 15 Mar 2022 27 10 208 15 Mar 2022 27 10 209 15 Mar 2022 27 10 210 15 Mar 2022 27 20 1 15 Mar 2022 27 20 2 15 Mar 2022 27 20 3 15 Mar 2022 27 20 4 15 Mar 2022 27 20 5 15 Mar 2022 27 20...

Page 14: ...2022 28 20 201 15 Mar 2022 28 20 202 15 Mar 2022 28 20 203 15 Mar 2022 28 20 204 15 Mar 2022 28 20 205 15 Mar 2022 28 20 206 15 Mar 2022 28 40 1 15 Mar 2022 28 40 2 15 Mar 2022 28 40 101 15 Mar 2022...

Page 15: ...2 32 20 102 15 Mar 2022 32 20 201 15 Mar 2022 32 20 202 15 Mar 2022 32 20 203 15 Mar 2022 32 20 204 15 Mar 2022 32 20 205 15 Mar 2022 32 20 206 15 Mar 2022 32 20 207 15 Mar 2022 32 20 208 15 Mar 2022...

Page 16: ...r 2022 34 20 201 15 Mar 2022 34 20 202 15 Mar 2022 34 20 203 15 Mar 2022 34 20 204 15 Mar 2022 34 30 1 15 Mar 2022 34 30 2 15 Mar 2022 34 30 101 15 Mar 2022 34 30 102 15 Mar 2022 34 50 1 15 Mar 2022 3...

Page 17: ...2022 52 10 203 15 Mar 2022 52 10 204 15 Mar 2022 52 10 205 15 Mar 2022 52 10 206 15 Mar 2022 52 40 1 15 Mar 2022 52 40 2 15 Mar 2022 53 00 Title 1 15 Mar 2022 53 00 Title 2 15 Mar 2022 53 00 TOC 1 15...

Page 18: ...57 50 202 15 Mar 2022 57 50 203 15 Mar 2022 57 50 204 15 Mar 2022 57 60 1 15 Mar 2022 57 60 2 15 Mar 2022 57 60 201 15 Mar 2022 57 60 202 15 Mar 2022 61 00 Title 1 15 Mar 2022 61 00 Title 2 15 Mar 202...

Page 19: ...022 77 00 1 15 Mar 2022 77 00 2 15 Mar 2022 77 00 3 15 Mar 2022 77 00 4 15 Mar 2022 78 00 Title 1 15 Mar 2022 78 00 Title 2 15 Mar 2022 78 00 TOC 1 15 Mar 2022 78 00 TOC 2 15 Mar 2022 Chapter Section...

Page 20: ...AIRCRAFT List of Effective Pages DV 20 E AMM Page 12 15 Mar 2022 LOEP Doc 4 02 25 Rev 2 Intentionally left blank...

Page 21: ...AIRCRAFT DV 20 E AMM Introduction Doc 4 02 25 Rev 2 01 TITLE Page 1 15 Mar 2022 CHAPTER 01 INTRODUCTION...

Page 22: ...AIRCRAFT Introduction DV 20 E AMM Page 2 15 Mar 2022 01 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 23: ...01 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 01 INTRODUCTION 1 General 1 2 Revision Service 1 3 Warning Cautions and Notes 1 4 Manual Configuration 2 5 Page Numbering System 6 6 Figures 6...

Page 24: ...AIRCRAFT Introduction DV 20 E AMM Page 2 15 Mar 2022 01 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 25: ...enance data is referenced in Chapter 05 00 2 Revision Service The manufacturer provides a revision service for the Airplane Maintenance Manual The revision shows design changes to the airplane or chan...

Page 26: ...uirement of the ATA iSpec2200 There are only 3 sources of words available to use in Simplified English SE Approved words from the SE Guide These words have defined meanings and selected parts of speec...

Page 27: ...Chapter 57 Section 50 contains the data for the trailing edge flaps installation The third pair of numbers shows a unit A unit could be the flap itself Only complex systems use unit numbers For simpl...

Page 28: ...ns of the airplane and general procedures such as towing parking and weighing Chapter 11 tells you about the placards and markings which are important for the safe operation of the airplane Chapter 12...

Page 29: ...r maintenance of the engine on the airplane Refer to the engine manufacturer s manual for other data C Chapter Configuration The first page of each chapter shows the number of the chapter and the titl...

Page 30: ...99 Trouble Shooting Pages 101 to 199 Maintenance Procedures Pages 201 to 299 6 Figures Figures are given numbers in sequence The first figure in a chapter or section is Figure 1 7 Record of Revisions...

Page 31: ...AIRCRAFT DV 20 E AMM Manual Organization Doc 4 02 25 Rev 2 02 TITLE Page 1 15 Mar 2022 CHAPTER 02 ORGANIZATION AND HANDLING OF THE MANUAL...

Page 32: ...AIRCRAFT Manual Organization DV 20 E AMM Page 2 15 Mar 2022 02 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 33: ...S CHAPTER 02 ORGANIZATION AND HANDLING OF THE MANUAL 1 General 1 2 Applicability 1 3 Revisions 1 4 Temporary Revisions 1 5 Service Bulletins 2 6 Service Information 2 7 Concession Reports and Non Conf...

Page 34: ...AIRCRAFT Manual Organization DV 20 E AMM Page 2 15 Mar 2022 02 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 35: ...to the Airplane Maintenance Manual to show design changes maintenance procedure changes or other changes Each group of changes is called a Revision A manual revision contains these items The changed p...

Page 36: ...t do the work given in a Mandatory Service Bulletin C Recommended Service Bulletins Recommended Service Bulletins give data about A minor problem and its correction A better technical design If you do...

Page 37: ...ies these Concession and Non Conformance Reports are contained in the airplane log Before you do maintenance check the airplane log for such Concession and Non Conformance Reports 8 Abbreviations Wher...

Page 38: ...utside Air Temperature PFD Primary Flight Display P N Part Number SB Service Bulletin S N Serial Number TBO Time Between Overhaul TSMOH Time Since Major Overhaul UHF Ultra High Frequency TTSN Total Ti...

Page 39: ...m 1 852 nm km 1 609 sm in x 25 4 mm ft x 0 3048 m nm x 1 852 km sm x 1 609 km Velocity Kilometers per hour km h Meters per second m s Miles per hour mph Knots kts Feet per minute fpm km h 1 852 kts km...

Page 40: ...gal US quart US qt Imperial gallon Imp gal Cubic inch in3 l 3 7854 US gal l 0 9464 US qts l 4 5461 Imp gal l 61 024 in3 US gal x 3 7854 l US qt x 0 9464 l Imp gal x 4 5461 l in3 x 61 024 l Torque New...

Page 41: ...rque values Nm lbf ft Use Figure 2 for conversion of Nm lbf in Figure 1 Nm lbf ft Find the Nm value on the horizontal axis Move vertically to the solid black diagonal line Then move horizontally to th...

Page 42: ...bf in 75 80 85 90 Figure 2 Nm lbf in Find the Nm value on the horizontal axis Move vertically to the solid black diagonal line Then move horizontally to the vertical axis Read the value in lbf in Exam...

Page 43: ...DV 20 E AMM Airworthiness Limitations Doc 4 02 25 Rev 2 04 TITLE Page 1 15 Mar 2022 CHAPTER 04 AIRWORTHINESS LIMITATIONS...

Page 44: ...AIRCRAFT Airworthiness Limitations DV 20 E AMM Page 2 15 Mar 2022 04 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 45: ...DV 20 E AMM Airworthiness Limitations Doc 4 02 25 Rev 2 04 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 04 AIRWORTHINESS LIMITATIONS 1 Airworthiness Limitations 3...

Page 46: ...AIRCRAFT Airworthiness Limitations DV 20 E AMM Page 2 15 Mar 2022 04 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 47: ...LIMITATIONS SECTION IS APPROVED BY EUROPEAN AVIATION SAFETY AGENCY EASA IN ACCORDANCE WITH THE APPLICABLE CERTIFICATION PROCEDURES AND THE TYPE CERTIFICATION BASIS IT SPECIFIES THE AIRWORTHINESS LIMI...

Page 48: ...AIRCRAFT Airworthiness Limitations DV 20 E AMM Page 2 15 Mar 2022 04 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 49: ...f the DV 20 E airplane white This will help to keep the temperature of the composite structure below the structural temperature limit for the flight 54 C 129 F Paint colors markings and placards are s...

Page 50: ...AIRCRAFT Airworthiness Limitations DV 20 E AMM Page 4 15 Mar 2022 04 00 00 Doc 4 02 25 Rev 2...

Page 51: ...AIRCRAFT DV 20 E AMM Time Limits and Maintenance Checks Doc 4 02 25 Rev 2 05 TITLE Page 1 15 Mar 2022 CHAPTER 05 TIME LIMITS AND MAINTENANCE CHECKS...

Page 52: ...AIRCRAFT Time Limits and Maintenance Checks DV 20 E AMM Page 2 15 Mar 2022 05 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 53: ...ion 05 10 Time Limits 1 General 1 2 Regulatory Authorities 1 3 Scheduled Maintenance Time Limits 1 4 Component Time Limits 3 5 Component Time Tracking 4 Section 05 20 Scheduled Maintenance Checks 1 Ge...

Page 54: ...2 Preparation 2 3 Engine Ground Test 3 4 Maintenance Checklist Engine 4 Section 05 28 50 Maintenance Checklist Airframe 1 Front Fuselage 1 2 Cockpit 4 3 Center Fuselage Internal 7 4 Rear Fuselage 10 5...

Page 55: ...5 CONTENTS Page 3 15 Mar 2022 Section 05 28 92 Check Flight Report 1 Check Flight Report 1 Section 05 50 Unscheduled Maintenance Checks 1 General 1 2 Hard Landing Check 1 3 Propeller Strike 5 4 Engine...

Page 56: ...AIRCRAFT Time Limits and Maintenance Checks DV 20 E AMM Page 4 15 Mar 2022 05 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 57: ...ed You must make sure that all Airworthiness Directives Service Bulletins and any other requirements of the Airworthiness Authority are completed as required The airplane manufacturer can change the t...

Page 58: ...28 00 DV 20 E Maintenance Checklist for the engine Maintenance checks schedule for 100 200 and 1000 hour checks on the engine and propeller 2 Section 05 28 50 DV 20 E Maintenance Checklist for the ai...

Page 59: ...intenance Manual 912 iS MML 912i 898742 Cleveland Parker Cleveland Parker Maintenance Manual AWBCMM0001 13 Cleveland Parker Cleveland Parker Product Catalog AWBPC0001 15 Cleveland Parker Cleveland Par...

Page 60: ...e Is correctly attached Has no loose parts Shows no signs of leaks Is not cracked or damaged Is not worn S Make sure that The surface protection is not damaged All locking devices are installed correc...

Page 61: ...nce Log Replace To remove an item and install a serviceable item in the same location Set To put equipment into a given adjustment condition or mode For example set the altimeter scale to 1013 mbar 10...

Page 62: ...AIRCRAFT Time Limits and Maintenance Checks DV 20 E AMM Page 6 15 Mar 2022 05 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 63: ...must make sure that you meet the requirements of the Regulatory Authority of the country where the airplane is registered 3 Scheduled Maintenance Time Limits Refer to Sections 05 20 through 05 28 The...

Page 64: ...the 100 hour inspection was done at 110 hours the next inspection must be done at 200 10 hours not 210 10 hours If an inspection is done earlier than allowed by the specified tolerance all subsequent...

Page 65: ...days VFR 34 Magnetic compass Compensate 2 30 days NVFR 34 Transponder System check 2 30 days NVFR B Airplane Life Limited Components Replace the following components at the times indicated Component...

Page 66: ...omponent Time Tracking To make sure that component overhaul replacement is done at the correct time you must record the data that follows in the Airplane Maintenance Log for each component requiring o...

Page 67: ...ance of airplanes do the items marked X in the Maintenance Checklist Note The interval columns 100 200 and 1000 are used for maintenance items which must be done at intervals of 100 200 or 1000 flight...

Page 68: ...in landing gear and the brake system 3 Center Fuselage Internal All items inside the fuselage shell below the baggage compartment floor from the aft face of the spar bridge and seatback to the B bulkh...

Page 69: ...aintenance Checks Doc 4 02 25 Rev 2 05 20 00 Page 3 15 Mar 2022 C Section 05 28 70 6000 Hour Inspection All 6000 hour inspection items listed in the tables must be performed within 6000 hours of fligh...

Page 70: ...AIRCRAFT Time Limits and Maintenance Checks DV 20 E AMM Page 4 15 Mar 2022 05 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 71: ...rplane log book for problems before doing the pre flight check WARNING DO ALL THE STEPS OF THE PRE FLIGHT CHECK CAREFULLY ACCIDENTS CAN OCCUR IF THE PRE FLIGHT CHECK IS NOT DONE CORRECTLY The schedule...

Page 72: ...AIRCRAFT Time Limits and Maintenance Checks DV 20 E AMM Page 2 15 Mar 2022 05 21 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 73: ...nce personnel Record the completion of the 25 hour engine check in the engine log book and in the airplane log book Enter the applicable data in the blocks below Registration ____________________ Date...

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Page 75: ...E Engine 1 General Enter the applicable data in the blocks below Registration _________________ Date _________________ Airplane S N _________________ Engine S N _________________ Airplane Operating Ho...

Page 76: ...ou start the applicable check Interval Inspection Items 100 200 1000 Initials 1 Before you do the inspection S Read the applicable Airworthiness Directives S Read the applicable Service Bulletins X X...

Page 77: ...rking brake to ON X X X 2 Put the chocks against the airplane main wheels X X X 3 Do an engine ground run Refer to Section 71 00 and the engine maintenance manual X X X 4 Check engine instruments X X...

Page 78: ...L FUEL BURNS AND CAN CAUSE INJURY TO PEOPLE AND DAMAGE TO EQUIPMENT 1 Remove the top and bottom cowlings Examine the cowlings Make sure that the fasteners are serviceable Look for cracks and areas tha...

Page 79: ...em S Exhaust S Push pull cables S Cylinder air duct and fins X X X 7 Check air filter in accordance with the engine maintenance manual X X X 8 Check oil tank breather for blockage X X X NOTE Extended...

Page 80: ...Doc 4 02 25 Rev 2 12 Clean gascolator S Check for fuel leakage X X X 13 Clean the fuel separator X 14 Do a check of the airplane battery Look specially for S Charge and capacity S Corrosion pitting b...

Page 81: ...the structure and leaks or breaks in the plexiglass seal Make sure that the canopy locking mechanism will release Refer to Chapter 52 10 X X X 3 Do the canopy latch force test Refer to Chapter 52 10 X...

Page 82: ...t mounting hardware for security and damage X X X 15 Check for abnormal tire wear and correct tire pressure Refer to Chapter 12 10 and Chapter 32 10 X X X 16 Examine the nose wheel assembly Look espec...

Page 83: ...he NLG fork pivot as per Chapter 12 00 and install the NLG fork as per Chapter 32 00 X X X 24 Visually examine the NLG strut condition Look especially for distortion corrosion and condition of the pai...

Page 84: ...he safety hammer installation S Check attachments for looseness S Check release mechanism for interference or improper function X X 4 Examine the cable ties and electrical connectors Pull lightly to m...

Page 85: ...structure Look especially for correct attachment function wear damage and corrosion Refer to Chapter 27 20 X X X 15 Examine the brake pipes hoses and components Look especially for leakage X X X 16 Ex...

Page 86: ...the drain trap block along the floor of the cockpit to the fuel shut off valve Make sure that there are no signs of fuel leaks X X X 22 Examine the instrument panel Make sure that S Wiring is correctl...

Page 87: ...4 Examine the ELT Refer to Chapter 25 60 X X X 5 Remove the center fuselage panels on the bottom of the airplane for access X X X 6 Remove the baggage compartment floor for access Refer to Chapter 25...

Page 88: ...JURY TO PEOPLE AND DAMAGE TO EQUIPMENT 14 Remove and clean the gascolator filter bowl Install the gascolator filter bowl Refer to Chapter 28 20 X X X 15 Examine the fuel tank strap Look especially for...

Page 89: ...ine the condition of the laminates and the bond to the fuselage S Look especially around S The LH and RH A bolt bushing S The B bolt bushing S The MLG brackets S The LH and RH top aft outer corners be...

Page 90: ...de of the window including surrounding structure and seal Look especially for damage dents cracks holes scratches and delamination X X X 2 Visually inspect the condition of the paint for chips scratch...

Page 91: ...attachment X X X 5 Remove the rudder S Visually examine the hinge pin for cracks corrosion and fit in the composite S If sleeve installed over the hinge pin Replace the sleeve if it is damaged or wor...

Page 92: ...n holes in the elevator for blockage X X 18 Examine the elevator hinges and control horn Check the laminate around the hinges and the control horn fasteners for cracks corrosion or delamination Look e...

Page 93: ...l push rod for corrosion in the following areas S Under the trim spring mounts by removing the roll pin S Upper and lower trim spring mounts S Under the chaffing protection sleeve of the center bushin...

Page 94: ...in of radial play S Grease the A bolts S Examine the B bolts and bushings for security in surrounding composite tightness of fit of pin bolt cracks corrosion wear and distortion S Replace the B bolts...

Page 95: ...of wear as follows S Take a measurement of the push rod diameter at the edge of the paint S Take a measurement of the push rod diameter at the middle of the wear mark S Compare the two measurements If...

Page 96: ...s Refer to Chapter 57 10 X X X 14 Remove the aileron push rods and examine them for damage Look especially for rub marks and excessive wear The maximum wear permitted is 0 25 mm 0 010 in Measure the a...

Page 97: ...t at the top of the control stick Maximum play allowed S 10 mm 0 375 in Refer to Chapter 27 10 X X X 4 Do a system test for the correct range of movement of the aileron control system Refer to Chapter...

Page 98: ...S CAN CAUSE INJURY OR DEATH WARNING SET THE PARKING BRAKE TO ON IF YOU DO NOT DO THIS THE AIRPLANE CAN MOVE THIS CAN CAUSE INJURY OR DEATH 11 Set the parking brake to ON X X X 12 Put the chocks agains...

Page 99: ...dge of the fire shield on the front face of the firewall Check for cracks damage and disbond from the fire shield 2 Front Fuselage Inspection Items Front Fuselage Initials 1 Do a visual inspection and...

Page 100: ...seat attachments Look especially for cracks delamination and damage around the fastener holes 2 Visually examine the cockpit floor Look especially for cracks or delamination around the aft rudder peda...

Page 101: ...e skin around the lower tail fin 5 Perform a visual inspection and a tap test of the horizontal stabilizer S Inspect for disbonding between internal composite components including leading trailing edg...

Page 102: ...e core or a disbond between the skin and core 2 Perform a visual inspection and tap test of the leading edge Examine for disbonds and cracks above or below the overlap seam 3 Perform a visual inspecti...

Page 103: ...roots in front and behind the spar to inspect the joints with the main spar and spar stump Examine the condition of the laminate Look especially for damage cracks and delamination 11 Visually examine...

Page 104: ...and Maintenance Checks DV 20 E AMM Inspection Items Wings Initials Page 6 15 Mar 2022 05 28 70 Doc 4 02 25 Rev 2 15 Visually examine the main pin bushing in the spar bridge Replace the main pin bushi...

Page 105: ...f the Maintenance Report after all of the applicable maintenance tasks in the Maintenance Checklist have been initialed DV 20 E Airplane Serial Number Registration Number Check __________ 100 hr 200 h...

Page 106: ...AIRCRAFT Time Limits and Maintenance Checks DV 20 E AMM Page 2 15 Mar 2022 05 28 90 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 107: ...ET TO OFF THE ENGINE MASTER SWITCH IS SET TO OFF THE THROTTLE LEVER IS SET TO IDLE WARNING DO NOT GET OIL ON YOU OIL CAN CAUSE SKIN DISEASE WARNING DO NOT GET FUEL ON YOU FUEL CAN CAUSE SKIN DISEASE D...

Page 108: ...AIRCRAFT Time Limits and Maintenance Checks DV 20 E AMM Page 2 15 Mar 2022 05 28 91 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 109: ...DV 20 E Page 1 of 2 Registration Pilot Airdrome Date Take Off Landing Functional Check Flight Behavior Findings N A NO YES Fuel quantity indicator ACL Navigation lights Warning and Caution lights Alti...

Page 110: ...Findings N A NO YES AIRCRAFT Page 2 15 Mar 2022 05 28 92 Doc 4 02 25 Rev 2 Backup altimeter Backup artificial horizon Compass Behavior during climb Coolant temperature Cabin heat cabin air Behavior du...

Page 111: ...a hard landing Or when ground handling applies unusual loads A Equipment Item Quantity Part No Slide sheets 4 Commercial B Procedure Detail Steps Work Items Key Items CAUTION IF YOU THINK THE AIRPLANE...

Page 112: ...mm 0 12 in examine the strut for corrosion and cracks particularly in the area of the maximum gap If the gap is more than 3 mm 0 12 in replace the strut as per Chapter 32 10 5 Check toe in and camber...

Page 113: ...efer to Chapter 32 20 13 Examine the control surfaces Look specially for S Correct attachment of the hinges S Correct attachment of the mass balance to the structure 14 Examine the leading edge of the...

Page 114: ...022 05 50 00 Doc 4 02 25 Rev 2 Spar Bridge Inner Mount Outer Mount Main Gear Strut Axle Attachment Brake Disk Wheel and Tire Attachment to Engine Mount Shock Absorber Assembly Nose Leg Journal Assembl...

Page 115: ...e the propeller Refer to Chapter 61 2 Remove engine Refer to Chapter 71 00 3 Do an inspection of the engine mount Refer to Section 71 20 4 Do an inspection of the propeller Refer to the Propeller Owne...

Page 116: ...Look specially for signs of fire damage Replace damaged cables 5 Examine the fuel lines Look specially for signs of fire damage to the fire protection sleeves Replace damaged fuel lines 6 Examine the...

Page 117: ...NS USE SAFETY MASKS AND GLOVES AS RECOMMENDED 9 Clean the engine Make sure you clean all the fire extinguisher particles from the engine Refer to the manufacturer of the fire extinguisher 10 Connect t...

Page 118: ...ve the flap bellcrank inside fuselage Refer to Section 27 50 3 Inspect the flap bellcrank for any visual signs of damage Look in particular around the weld joints of the bellcrank arms 4 Inspect the f...

Page 119: ...AIRCRAFT DV 20 E AMM Dimensions and Areas Doc 4 02 25 Rev 2 06 TITLE Page 1 15 Mar 2022 CHAPTER 06 DIMENSIONS AND AREAS...

Page 120: ...AIRCRAFT Dimensions and Areas DV 20 E AMM Page 2 15 Mar 2022 06 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 121: ...Dimensions and Areas Doc 4 02 25 Rev 2 06 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 06 DIMENSIONS AND AREAS 1 General 1 2 Dimensions 3 3 Adjustment Reports 4 4 Weight and Static Moments o...

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Page 123: ...ar 2022 CHAPTER 06 DIMENSIONS AND AREAS 1 General The DV 20 E uses the System Internationale SI for dimensions and areas Imperial dimensions are also given in brackets For example Wing span 10 87 m 35...

Page 124: ...AIRCRAFT Dimensions and Areas DV 20 E AMM Page 2 15 Mar 2022 06 00 00 Doc 4 02 25 Rev 2 Figure 1 DV 20 E Overall Dimensions Approximate Values...

Page 125: ...il Wortmann FX63 137 20 HOAC Wing area 11 6 m 125 ft Dihedral nominal 4 Aspect ratio 10 Sweep back 1 Horizontal Tail Surfaces Span 2 66 m 8 ft 9 in Angle of incidence 4 Landing Gear typical static nor...

Page 126: ...nce to show any deviations 4 Weight and Static Moments of Control Surfaces WARNING IF YOU REPAINT OR DO REPAIRS TO THE CONTROL SURFACES YOU MUST MAKE SURE THAT THE WEIGHT AND STATIC MOMENTS OF THE CON...

Page 127: ...AIRCRAFT DV 20 E AMM Dimensions and Areas Doc 4 02 25 Rev 2 06 00 00 Page 5 15 Mar 2022 Figure 2 Control Surface Deflections...

Page 128: ...AIRCRAFT Dimensions and Areas DV 20 E AMM Page 6 15 Mar 2022 06 00 00 Doc 4 02 25 Rev 2 1 Control Surface Adjustment Reports Figure 3 Control Surface Weigh Balance Report...

Page 129: ...AIRCRAFT DV 20 E AMM Dimensions and Areas Doc 4 02 25 Rev 2 06 00 00 Page 7 15 Mar 2022 Figure 4 Control Surface Adjustment Report...

Page 130: ...ff 50 mm RUDDER CABLE TENSION 13 25 7 33 kg CANOPY UNLATCHING FORCE 4 5 9 0 kg 10 20 lbs No outside handles 6 8 11 3 kg 15 25 lbs With outside handles HORIZONTAL STABILIZER INCIDENCE 4 0 5 MAIN LANDIN...

Page 131: ...AIRCRAFT DV 20 AMM Lifting and Shoring General Doc 4 02 25 Rev 2 07 TITLE Page 1 15 Mar 2022 CHAPTER 07 LIFTING AND SHORING GENERAL...

Page 132: ...AIRCRAFT Lifting and Shoring General DV 20 AMM Page 2 15 Mar 2022 07 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 133: ...AIRCRAFT DV 20 AMM Lifting and Shoring General Doc 4 02 25 Rev 2 07 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 07 LIFTING AND SHORING GENERAL 1 General 1 2 Lifting the Airplane on Jacks 1...

Page 134: ...AIRCRAFT Lifting and Shoring General DV 20 AMM Page 2 15 Mar 2022 07 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 135: ...aces 2 Lifting the Airplane on Jacks The DV 20 E airplane has two jacking points They are located under the fuselage at the root ribs To support the rear fuselage a trestle with a former is positioned...

Page 136: ...AIRCRAFT Lifting and Shoring General DV 20 AMM Page 2 15 Mar 2022 07 00 00 Doc 4 02 25 Rev 2 Figure 1 Lifting the Airplane on Jacks...

Page 137: ...hold down strap in position on the rear fuselage 5 Put the 2 jacks into position under the main jacking points Extend the jacks to engage with the jacking plates Refer to Figure 1 6 Put the jack into...

Page 138: ...down strap 2 Remove the trestle from under the rear fuselage 3 Retract the jacks until the airplane wheels are on the ground Retract the jacks together to keep the airplane level at all times 4 Apply...

Page 139: ...AIRCRAFT DV 20 E AMM Weighing and Levelling Doc 4 02 25 Rev 2 08 TITLE Page 1 15 Mar 2022 CHAPTER 08 WEIGHING AND LEVELLING...

Page 140: ...AIRCRAFT Weighing and Levelling DV 20 E AMM Page 2 15 Mar 2022 08 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 141: ...ing Doc 4 02 25 Rev 2 08 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 08 WEIGHING AND LEVELLING 1 General 1 Section 08 10 Weighing 1 General 1 2 Weighing 4 Section 08 20 Levelling 1 General 1...

Page 142: ...AIRCRAFT Weighing and Levelling DV 20 E AMM Page 2 15 Mar 2022 08 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 143: ...t also tells you how to level the airplane Use the procedures in Section 08 10 to weigh the airplane and to calculate the airplane moment Use the procedures in Section 08 20 to level the airplane Note...

Page 144: ...AIRCRAFT Weighing and Levelling DV 20 E AMM Page 2 15 Mar 2022 08 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 145: ...calculate the new weight of the airplane You must also calculate its center of gravity Only an approved person can weigh the airplane The national Airworthiness Authority of the country where the airp...

Page 146: ...AIRCRAFT Weighing and Levelling DV 20 E AMM Page 2 15 Mar 2022 08 10 00 Doc 4 02 25 Rev 2 Figure 1 Level the Airplane Laterally...

Page 147: ...Arm Reference Plane to center line of nose wheel G1 G1LH G1RH Net weight main wheel scales LH and RH G2 Net weight Nose wheel scale G G1LH G1RH G2 Empty Weight XCG Arm Empty Weight center of gravity c...

Page 148: ...ve the airplane a small distance back and forward to allow the landing gear to spread This will prevent side loads on the scales causing errors Before you weigh the airplane do these items Make sure t...

Page 149: ...e canopy 4 Move the airplane onto the scales The scales under the main wheels must be of the same type CAUTION DO NOT ALLOW THE AIRPLANE TO RUN OFF THE SCALES THIS WILL CAUSE DAMAGE TO THE WHEEL FAIRI...

Page 150: ...om the right main wheel scale Enter the value on the weighing form under MAIN G1RH Gross 11 Read the value from the nose wheel scale Enter the value on the weighing form under NOSE G2 Gross 12 Use the...

Page 151: ...the calibration records for the weighing scales If necessary correct the Gross and Tare values of MAIN G1LH MAIN G1RH and NOSE G2 22 Subtract each Tare value from the related Gross value Record the r...

Page 152: ..._____ Weight and Balance Calculations Weighing at the wheels Weight Condition Including brake fluid engine oil MAX level coolant and unusable fuel 2 4 US gal 9 liters Support Gross Tare Net Lever Arm...

Page 153: ...with jacks Make the airplane level with jacks unless you are weighing the airplane If you weigh the airplane change the airplane tire pressures or use blocks to make the airplane level see Section 08...

Page 154: ...AIRCRAFT Weighing and Levelling DV 20 E AMM Page 2 15 Mar 2022 08 20 00 Doc 4 02 25 Rev 2 Figure 1 Level the Airplane Laterally Figure 2 Level the Airplane Longitudinally...

Page 155: ...Make the airplane level laterally S Put a spirit level on the back rest of the seat S Adjust the main jacks to bring the sprit level horizontal Refer to Figure 1 If necessary use two packing blocks of...

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Page 157: ...AIRCRAFT DV 20 E AMM Placards and Markings Doc 4 02 25 Rev 2 11 TITLE Page 1 15 Mar 2022 CHAPTER 11 PLACARDS AND MARKINGS...

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Page 159: ...25 Rev 2 11 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 11 PLACARDS AND MARKINGS 1 General 1 2 Replace Plastic Foil Placards 1 Section 11 20 Exterior Placards and Markings 1 General 1 Secti...

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Page 161: ...ation and operating limitations of systems and equipment This chapter shows you the location of the exterior placards and markings and the location of the interior placards Self adhesive plastic foil...

Page 162: ...ly pull the placard off Do not over heat the composite structure WARNING DO NOT GET SOLVENT ON YOUR SKIN DO NOT BREATHE SOLVENT VAPOR SOLVENT CAN CAUSE DISEASE OR ILLNESS 2 Clean the surface where the...

Page 163: ...s 1 General Figure 1 and 2 show the exterior placards and markings for the DV 20 E airplane Figure 1 Exterior Placards Sheet 1 of 2 DO NOT PUSH ON SPINNER STEP BELOW STEP BELOW COOLANT Dispatcher Vess...

Page 164: ...NS GROUND HERE TIE DOWN 2 3 bar 33 psi 230 kPa 1 8 bar 26 psi 180 kPa Super EN 228 AVGAS 100 LL or see AFM 93 l 24 5 US gal usable 84 l 22 2 US gal EMERGENCY LOCATOR TRANSMITTER INSTALLED HERE ELT EMP...

Page 165: ...e prohibited See Flight Manual for other limitations S T A R T C A N O P Y E M U V O L T A G E Usable 84 l 22 2 US gal ENGINE MASTER LANE A FAIL LANE A AUTO LANE B LANE SELECTOR SWITCH ON OFF E NGINE...

Page 166: ...AIRCRAFT Placards and Markings DV 20 E AMM Page 2 15 Mar 2022 11 30 00 Doc 4 02 25 Rev 2 Figure 2 Interior Placards and Markings if O M 20 245 b is installed...

Page 167: ...ds and Markings Sheet 2 of 2 FORWARD OFF FULL HIGH ON IDLE LOW A L T E R N A T E A I R T H R O T T L E P R O P E L L E R R P M TO LIFT CANOPY OPEN BOTH SIDES CLOSE OPEN FUEL PULL OFF TO LIFT CANOPY OP...

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Page 169: ...AIRCRAFT DV 20 E AMM Servicing General Doc 4 02 25 Rev 2 12 TITLE Page 1 15 Mar 2022 CHAPTER 12 SERVICING GENERAL...

Page 170: ...AIRCRAFT Servicing General DV 20 E AMM Page 2 15 Mar 2022 12 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 171: ...neral 1 2 Fuel System 1 3 Refueling Defueling 3 4 Fuel Contamination Test 4 5 Engine Oil System 4 6 Brake System 5 7 Tires 6 8 Cooling System 7 Section 12 20 Scheduled Servicing 1 General 1 2 Lubricat...

Page 172: ...AIRCRAFT Servicing General DV 20 E AMM Page 2 15 Mar 2022 12 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 173: ...hment procedures for various systems Section 12 20 Lubrication data Section 12 30 Cleaning and snow and ice removal The procedures for preventive and corrective maintenance of systems are given in the...

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Page 175: ...elow the tank The drain pipe comes through the fuselage bottom skin WARNING DO NOT ALLOW FIRE SPARKS OR HEAT NEAR FUEL FUEL BURNS VIOLENTLY AND CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE AIRPLANE W...

Page 176: ...CRAFT Servicing General DV 20 E AMM Page 2 15 Mar 2022 12 10 00 Doc 4 02 25 Rev 2 Engine Oil Coolant Brake Fluid on Co Pilot s Brake Pedals Tire Air Tire Air Fuel Drain Fuel Figure 1 Replenishing Poin...

Page 177: ...nstall the fuel filler cap Make sure that the filler cap is locked 9 Remove the ground cable from the airplane 10 Remove the ground cable from the refueling vehicle B Defueling Detail Items Work Steps...

Page 178: ...the glass container stand for 1 minute 5 Examine the fuel S It must be clear or dyed S Look specifically for small drops of water in the bottom of the glass container S Look for small particles of so...

Page 179: ...IN YOUR MOUTH BRAKE FLUID IS TOXIC AND CAN CAUSE INTERNAL INJURY CAUTION REMOVED SPILLED BRAKE FLUID IMMEDIATELY BRAKE FLUID CAN CAUSE DAMAGE TO PAINT AND OTHER MATERIALS A Fill the Brake System Reser...

Page 180: ...ressure Detail Steps Work Items Key Items References 1 Examine the tires Look specially for S Cuts and friction damage S Correct alignment of the slippage markers Move the airplane as necessary so tha...

Page 181: ...4 Open the pressure cap on top of the engine 5 Fill the dispatcher vessel up completely The level in the equalizing reservoir must not exceed the maximum marking 6 Close the pressure cap 7 Let the en...

Page 182: ...AIRCRAFT Servicing General DV 20 E AMM Page 8 15 Mar 2022 12 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 183: ...or Teflon bushes These bearings MUST NOT be lubricated Table 1 shows the bearings which MUST NOT be lubricated Table 1 Items Which MUST NOT Be Lubricated Rudder pedal sled DO NOT LUBRICATE Flap rod en...

Page 184: ...ake cabin heat defrost and alternate air control cables 200 1 Brake pedal pivot see Note 4 100 2 Rudder cable S tubes 200 3 Flap actuator universal pivot block 1000 4 Stick support pivot pins 1000 5 F...

Page 185: ...0 24 Nose landing gear strut axle stud end 100 Notes NS Item is not shown in the Figures 1 Lubricate at the time shown or at every disassembly assembly 2 Lubricate more frequently in severe climates o...

Page 186: ...th MIL G 81322 For main wheel bearings and felt seals lubrication only Mobil Aviation Grease SHC 100 Exxon Mobil Oil Corp TYPE 2 MIL L 7870 Royco 363 Royal Lubricants Co Inc Brayco 363 Bray Oil Co War...

Page 187: ...AIRCRAFT DV 20 E AMM Servicing General Doc 4 02 25 Rev 2 12 20 00 Page 5 15 Mar 2022 Figure 1 Lubrication Points Sheet 1 2 2 1 7 3 5 4 12 10 11 11 9 24 8 6...

Page 188: ...AIRCRAFT Servicing General DV 20 E AMM Page 6 15 Mar 2022 12 20 00 Doc 4 02 25 Rev 2 Figure 2 Lubrication Points Sheet 2 15 21 20 23 22 19 18 17 13 16 16A 16 17 14...

Page 189: ...ed on dirt and dead insects are very difficult to remove CAUTION DO NOT USE CLEANING OR POLISHING AGENTS WHICH CONTAIN SILICON IF THE AIRPLANE NEEDS REPAIR AT SOME TIME SILICON CAN PREVENT REPAIR MATE...

Page 190: ...al components and cables Use polythene bags to seal intakes and other areas that you want to keep dry After washing you can dry the engine using compressed air 8 bar 116 PSI 6 Snow and Ice Removal Rem...

Page 191: ...AIRCRAFT DV 20 E AMM Standard Practices Doc 4 02 25 Rev 2 20 TITLE Page 1 15 Mar 2022 CHAPTER 20 STANDARD PRACTICES...

Page 192: ...AIRCRAFT Standard Practices DV 20 E AMM Page 2 15 Mar 2022 20 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 193: ...CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 20 STANDARD PRACTICES 1 General 1 Section 20 10 Standard Practices Airframe 1 General 1 2 Bolt and Nut Types Used in the Airplane 2 3 Standard Tor...

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Page 195: ...1 15 Mar 2022 CHAPTER 20 STANDARD PRACTICES 1 General This Chapter gives you the standard practices for the DV 20 E airplane Use industry standard practice where no specific practice is given This Cha...

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Page 197: ...This Section tells you the procedures used to tighten the fasteners Note Use the standard torque values listed on the subsequent pages of this section where no specific values are given Note Composit...

Page 198: ...nimum strength for the bolts is DIN specification 8 8 Letters and numbers on the head of the bolt identify the bolt type The surface treatment also identifies the bolt A DIN Bolt Bolt Head Identificat...

Page 199: ...rque Nm Torque lbf ft 10 32 1 6 1 2 1 4 28 6 2 4 6 5 16 24 13 6 10 3 8 24 20 7 15 3 7 16 20 37 7 27 8 1 2 20 54 2 40 9 16 18 90 4 66 7 5 8 18 124 3 91 7 B AN Coarse Thread Series Bolt Size Torque Nm T...

Page 200: ...back plates to the caliper Refer to Cleveland Parker Maintenance Manual latest revision or placard on brake cylinder assy Main landing gear bolt inner 0 16 0 02 in Height of spring washers 4 0 5 mm M...

Page 201: ...AIRCRAFT DV 20 E AMM Heating and Ventilation Doc 4 02 25 Rev 2 21 TITLE Page 1 15 Mar 2022 CHAPTER 21 HEATING AND VENTILATION...

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Page 203: ...neral 1 2 Description and Operation 1 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove Install the Heat Control Valve 201 3 Test Adjust the Heat Control Valve 203 4 Remove I...

Page 204: ...AIRCRAFT Heating and Ventilation DV 20 E AMM Page 2 15 Mar 2022 21 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 205: ...exchanger A shroud around the exhaust muffler makes the heat exchanger The shroud has an air inlet connection at the front on the right It also has a warm air outlet connection at the back on the lef...

Page 206: ...ugh a large flexible hose to the heat control valve The CABIN HEAT control lever moves the flap in the heat control valve In the OFF position fully forward no hot air can flow into the cockpit Move th...

Page 207: ...trument Panel Cover HEAT OFF HEAT MAX DEFROST FLOOR Floor Hot Air FLOOR HEAT DEFROST Selector Firewall Exhaust Gases Exhaust Muffler Shroud Air Intake Coolant Radiator Cockpit Lever Cockpit Lever DEFR...

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Page 209: ...olumn 1 do the repair given in column 3 Trouble Possible Cause Repair Burning smell in the cockpit Exhaust heat exchanger cracked Replace or repair the heat exchanger Heating system supplies warm air...

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Page 211: ...ences 1 Remove the engine cowlings Refer to Chapter 71 10 WARNING IF THE ENGINE HAS BEEN RUNNING TAKE CARE WHEN YOU TOUCH THE HEAT CONTROL VALVE THE HEAT CONTROL VALVE GETS HOT 2 Release the worm driv...

Page 212: ...rward about 3 mm 0 1 in 4 Put the bowden cable in position on the heat control valve Adjust the nuts on the outer sheath adjuster to a mid position Make sure that the inner cable is through the end fi...

Page 213: ...OL VALVE GETS HOT 3 Make sure that S The flap fully closes the opening to the distribution box Look or feel inside the heat control valve 4 If necessary adjust the outer sheath of the cable that goes...

Page 214: ...AKE SURE THAT THE ENGINE MASTER SWITCH IS IN THE OFF POSITION THE ELECTRIC MASTER SWITCH IS IN THE OFF POSITION THE BATTERY BACKUP SWITCH IS IN THE OFF POSITION THE THROTTLE IS SET TO IDLE WARNING IF...

Page 215: ...he HEAT DEFROST FLOOR control from the lever at the control quadrant S Loosen the swivel attachment 8 Disconnect the outer sheath of the HEAT DEFROST FLOOR control bowden cable from the tab at the con...

Page 216: ...t air distribution hoses at the rear of the distribution box 14 Remove the distribution box B Install the Distribution Box Detail Steps Work Items Key Items References 1 Install the HEAT DEFROST FLOOR...

Page 217: ...ROST FLOOR control bowden cable to the tab at the control quadrant S Install the two nuts 9 Install the cable wire end of the HEAT DEFROST FLOOR control to the lever at the control quadrant S Tighten...

Page 218: ...center console 15 Install the face plate to the center console cover 16 Install the control knobs from the following levers at the center console S PARKING BRAKE S HEAT control ON OFF S HEAT distribut...

Page 219: ...Refer to Paragraph 2A NOTE Only do steps 3 through 7 if you must adjust the distribution valve range of movement 3 Disconnect the airplane battery Refer to Chapter 24 31 4 Install the control knobs fr...

Page 220: ...cable that goes through the tab in the control quadrant to give the correct bounce 12 Install the heat control valve Refer to Paragraph 2B NOTE Only do steps 14 through 21 if you had to do steps 3 thr...

Page 221: ...lamps which attach the inlet and outlet hoses to the heat exchanger 3 Disconnect the inlet and outlet hoses from the heat exchanger 4 Release the screws which hold the shroud to the muffler 5 Remove t...

Page 222: ...1 Remove the heat exchanger shroud Refer to Paragraph 6A 2 Examine the inside of the shroud Look especially for soot marks and cracks If you find soot marks the exhaust muffler is cracked You must re...

Page 223: ...AIRCRAFT DV 20 E AMM Communications Doc 4 02 25 Rev 2 23 TITLE Page 1 15 Mar 2022 CHAPTER 23 COMMUNICATIONS...

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Page 225: ...ication 1 General 1 2 Description 2 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove Install the Garmin GTN 650 201 3 Remove Install the GTR 225A VHF COM Transceiver 204 4 A...

Page 226: ...AIRCRAFT Communications DV 20 E AMM Page 2 15 Mar 2022 23 CONTENTS Doc 4 02 25 Rev 2 Section 23 60 Static Discharging 1 General 1 2 Description 1...

Page 227: ...ks for shop data 2 Description A Speech Communication The basic speech communication system has the following components Garmin GTN 650 COM NAV GPS Garmin GTR 225A COM COM antennas B Audio Integrating...

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Page 229: ...the COM 2 The audio panel with speaker amplifier operates the cabin speaker Figure 1 shows the antenna locations The 1 VHF COM antenna is a dipole It is installed in the leading edge of the vertical...

Page 230: ...ion Hints Transponder Panel Control Optional 2 Description A GTN 650 The GTN 650 is a VHF communications transceiver and a GPS receiver Refer to Chapter 34 50 for GPS functions It also includes VOR Lo...

Page 231: ...n the Default Navigation page from any other page Direct To Key provides access to the direct to function which allows you to enter a waypoint and establishes a direct course to the selected destinati...

Page 232: ...ey Press to Return to Com Display Press to View Recent or User Frequencies Press to Select Intercom Function Function Selection Clear Data Key Enter Key Large and Small Knobs Frequency Adjust B Garmin...

Page 233: ...e radio Replace the defective mic Radio check reports readability poor strength poor Co ax connector faulty Examine the co ax and connections for condition and security Received audio is poor Faulty r...

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Page 235: ...Work Items Key Items References 1 Open the COM1 and GPS NAV1 circuit breakers 2 Put a 3 32 allen wrench into the access hole for the locking screw Engage the screw 3 Turn the screw counter clockwise u...

Page 236: ...the unit into the rack Engage the locking screw so that the latch front lobe touches the rack 3 Turn the locking screw clockwise so that the rear lobe engages the mounting rack CAUTION DO NOT OVER TIG...

Page 237: ...ach control function Refer to Chapter 23 50 2 Make sure that the database date is valid Once the database has been acknowledged the instrument panel self test page will appear Refer to the units Pilot...

Page 238: ...the locking screw in the front panel Engage the screw Refer to Figure 4 3 Turn the screw counter clockwise until the unit disengages from the mounting rack CAUTION DO NOT PULL ON THE KNOBS DO NOT PRY...

Page 239: ...ting rack 5 Close the COM2 circuit breaker 6 Do an operational test Refer to Paragraph C C Operational Test of the GTR 225A VHF COM Transceiver Detail Steps Work Items Key Items References 1 Do a test...

Page 240: ...AIRCRAFT Communications DV 20 E AMM Page 206 15 Mar 2022 23 10 00 Doc 4 02 25 Rev 2 Figure 4 GTR 225A VHF COM Transceiver Removal Installation...

Page 241: ...340 is a panel mounted TSO d audio panel that provides control of the airplane audio system The GMA 340 provides flexibility in switching up to three microphone and audio receiver communication input...

Page 242: ...ivity Indicator LEDs 4 Marker Beacon Receiver Sensitivity Selection Button 5 Unit On Off Pilot Intercom System ICS Volume 6 Pilot ICS Voice Activated VOX Intercom Squelch Level 7 Copilot ICS Volume Co...

Page 243: ...Refer to Chapter 92 for the wiring diagrams Replace the audio panel No voice modulation when transmitting from pilot s side on head set Co pilot s side OK Faulty head set Open mic audio line Faulty a...

Page 244: ...the audio panel switched OFF Faulty head set Open audio line Replace head set Do a test of the head set audio wiring Refer to Chapter 92 for the wiring diagrams No audio on co pilot s or passenger hea...

Page 245: ...il Steps Work Items Key Items References 1 Open the ICS circuit breaker 2 Put a 3 32 allen wrench into the access hole for the locking screw Engage the screw 3 Turn the screw counter clockwise until t...

Page 246: ...AGE THE LOCKING MECHANISM 4 Continue to turn the screw until the unit is fully installed in the mounting rack 5 Close the ICS circuit breaker 6 Do a functional test C Adjustment Test of the GMA 340 Au...

Page 247: ...e key and audio over the headphones and speaker Make sure that the communications are loud and clear and PTT operation is correct 4 Do the Intercom System ICS check as follows S Set the intercom to th...

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Page 249: ...rewall The other end of the loop connects to the right side of the firewall in the same way The copper tape goes along each side of the fuselage The side tapes are connected by a piece of copper tape...

Page 250: ...d Connection KEY To Rear Fuselage B Bulkhead To Landing Gear To Wing Aileron Bellcrank External Lights Forward Ground Stud at Firewall To Control Sticks To Flap Actuator To Wing Pitot Tube Aileron Bel...

Page 251: ...AIRCRAFT DV 20 E AMM Electrical Power Doc 4 02 25 Rev 2 24 TITLE Page 1 15 Mar 2022 CHAPTER 24 ELECTRICAL POWER...

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Page 253: ...tion 24 30 DC Generation 1 General 1 2 Description and Operation 1 Section 24 31 Battery System 1 General 1 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Safety Precautions 201...

Page 254: ...ge 2 15 Mar 2022 24 CONTENTS Doc 4 02 25 Rev 2 Maintenance Practices 1 General 201 2 Electrical Safety 201 3 Remove Install the Avionics Master Relay 202 4 Remove Install a Circuit Breaker 203 5 Remov...

Page 255: ...isted in Section 6 5 of the Airplane Flight Manual is called Additional Equipment The installation of Additional Equipment is a modification which must be handled in accordance with nation regulations...

Page 256: ...e coil of the relay is tied to the battery The ELECTRIC MASTER switch provides the coil ground when set to the ON position 2 Bus Structure All buses are flat metal strips connecting rows of circuit br...

Page 257: ...ttery Backup switch is located at the bottom center of the instrument panel The switch has a guard to prevent inadvertent operation The normal position of the Battery Backup Switch is OFF During emerg...

Page 258: ...AIRCRAFT Electrical Power DV 20 E AMM Page 4 15 Mar 2022 24 00 00 Doc 4 02 25 Rev 2 Figure 1 Electrical Schematic Simplified...

Page 259: ...AIRCRAFT DV 20 E AMM Electrical Power Doc 4 02 25 Rev 2 24 00 00 Page 5 15 Mar 2022 Figure 2 External Alternator Electric Schematic Simplified if O M 20 245 b is installed...

Page 260: ...DC GDC 74A 0 41 Cooling fan 0 32 Relays 0 80 Flap control system only during operation 5 00 Powerplant instrument EMU 912iS evo 0 60 Annunciation lights 0 50 Position lights 1 00 Strobe lights 2 00 Ta...

Page 261: ...nd charges the battery Note When doing prolonged maintenance on the airplane with external power connected to the electrical system pull the ALT CONTROL and ALT circuit breakers to prevent damage to t...

Page 262: ...electrical system of the BRP Rotax 912 iS also includes two separate regulators The alternator regulators are on the fuse box in the engine compartment One controls the output of alternator A and the...

Page 263: ...battery voltage the generator charges the battery The ammeter shows the current flowing to or from the battery Additional a low voltage monitor is implemented into the system When both generators are...

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Page 265: ...battery voltage low Battery capacity low Alternator output low Do a capacity test If necessary replace the battery Trouble Shoot the alternator refer to Section 24 31 Main battery will not connect to...

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Page 267: ...S APPROVED BY THE AIRPLANE MANUFACTURER 2 Safety Precautions Obey the maintenance instructions of the battery manufacturer Always disconnect the battery when you do work on the electrical system Disco...

Page 268: ...compound DC4 to the battery terminal and the cable lug 4 Connect the negative cable to the negative battery terminal Apply Dow Corning compound DC4 to the battery terminal and the cable lug 5 Install...

Page 269: ...ve battery terminal Apply Dow Corning compound DC4 to the battery terminal and the cable lug 3 Install the top engine cowling 5 Remove Install the Battery Relay A Remove the Battery Relay Detail Steps...

Page 270: ...2 Connect the electrical cables to the relay Refer to Chapter 92 for the wiring diagrams 3 Connect the cables to the main battery S Connect the positive cable to the positive battery terminal S Connec...

Page 271: ...stem has these components Main bus Avionic bus Battery relay Engine Master relay Avionics Master relay Start Power relay Switches Circuit breakers Fuses Figure 1 shows the electrical system bus struct...

Page 272: ...AIRCRAFT Electrical Power DV 20 E AMM Page 2 15 Mar 2022 24 60 00 Doc 4 02 25 Rev 2 Figure 1 Electrical System Bus Structure Diagram...

Page 273: ...AIRCRAFT DV 20 E AMM Electrical Power Doc 4 02 25 Rev 2 24 60 00 Page 3 15 Mar 2022 Figure 2 Addition to Electrical Bus Structure Diagram if O M 20 245 b is installed...

Page 274: ...AIRCRAFT Electrical Power DV 20 E AMM Page 4 15 Mar 2022 24 60 00 Doc 4 02 25 Rev 2 Figure 3 Electrical Switches and Circuit Breakers...

Page 275: ...AIRCRAFT DV 20 E AMM Electrical Power Doc 4 02 25 Rev 2 24 60 00 Page 5 15 Mar 2022 Figure 4 Electrical Switches and Circuit Breakers if O M 20 245 b is installed...

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Page 277: ...bution system If you have the trouble detailed in the Trouble column read across to the Possible Cause column Then do the repair given in the Repair column Trouble Possible Cause Repair There is 14 VD...

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Page 279: ...ance circuits for example if you connect the positive battery terminal and the negative battery terminal with a wrench by accident Always follow the usual safety practices for working on electrical eq...

Page 280: ...he relay clear of the airplane B Install the Avionics Master Relay Detail Steps Work Items Key Items References 1 Put the relay in position on the instrument panel floor 2 Install the bolt washer and...

Page 281: ...connect the wires from the circuit breaker 6 Shift back the copper bus bar together with the remaining circuit breakers 7 Remove the circuit breaker from the instrument panel B Install a Circuit Break...

Page 282: ...o the system The system must stop operating Make sure there is no electrical power supplied to the system 5 Remove Install an Instrument Panel Switch This procedure applies to the following switches P...

Page 283: ...Key Items References 1 Hold the spring clips on the switch compressed and put the switch in position in the instrument panel From the front of the instrument panel Make sure that the clips have expan...

Page 284: ...Switch Detail Steps Work Items Key Items References 1 Disconnect the main battery for maintenance Refer to Section 24 31 2 Remove the instrument panel cover Refer to Section 25 10 3 Remove the nut an...

Page 285: ...ve the switch into position in the instrument panel Hold the switch in position 4 Install the washer and nut that attach the switch to the instrument panel 5 Install the instrument panel cover Refer t...

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Page 287: ...AIRCRAFT DV 20 E AMM Equipment Furnishings Doc 4 02 25 Rev 2 25 TITLE Page 1 15 Mar 2022 CHAPTER 25 EQUIPMENT FURNISHINGS...

Page 288: ...AIRCRAFT Equipment Furnishings DV 20 E AMM Page 2 15 Mar 2022 25 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 289: ...2 Remove Install a Pilot s Seat 201 3 Remove Install a Safety Belt 203 4 Remove Install the Instrument Panel Cover 205 5 Remove Install the Baggage Compartment Floor Panel 206 6 Cleaning 207 Section...

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Page 291: ...r 2022 CHAPTER 25 EQUIPMENT FURNISHINGS 1 General This chapter describes about the equipment and furnishing in the flight compartment Chapter 25 10 includes the cabin trim panels pilot s seats and saf...

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Page 293: ...adjust each of the four straps to give the correct fit Shoulder straps with inertia reels are optional Replace frayed or damaged straps C Fabric Wall Panels Fabric wall panels bond to the inside of t...

Page 294: ...el The baggage compartment floor has three pieces You can remove the center piece by itself The outer pieces make stowage boxes The pieces are made of GFRP or CFRP G Baggage Net A net attaches to the...

Page 295: ...he five screws from the seat shell 4 Lift the seat a little S Release the quick release fastener for the outer strap S Move the inner strap through the hole in the seat shell Take care not to loose th...

Page 296: ...AIRCRAFT Equipment Furnishings DV 20 E AMM Page 202 15 Mar 2022 25 10 00 Doc 4 02 25 Rev 2 Figure 2 Safety Belt Installation...

Page 297: ...release 4 Loosen the mounting bolt for the lap strap without a central lock Pull the strap from the mounting or release the quick release B Install a Safety Harness Detail Steps Work Items Key Items R...

Page 298: ...AIRCRAFT Equipment Furnishings DV 20 E AMM Page 204 15 Mar 2022 25 10 00 Doc 4 02 25 Rev 2 Figure 3 Baggage Compartment Floor Panel Installation...

Page 299: ...rost hoses 3 Loosen the hose clamps on the defrost hoses Remove the hoses from the cover 4 Lift the cover clear of the airplane B Install the Instrument Panel Cover Detail Steps Work Items Key Items R...

Page 300: ...the gripper clips for the dip stick 6 Lift the center panel clear 7 If necessary remove the screws from the outer edges of the outer panels Only remove the outer panels if necessary 8 Lift the outer p...

Page 301: ...tall the screws along the aft edge of the center panel 8 Install inertia reel covers if fitted 9 Tighten all of the screws 6 Cleaning A Seats The seat cushions are a fire resistant material Clean the...

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Page 303: ...position The ME 406 ELT has an antenna installed through a side bracket hole in accordance with the Artex ME 406 Manual 2 Signal Transmission The ME 406 ELT transmits signals automatically after a cra...

Page 304: ...wn period of time After 1 hour of accumulated use testing On or before the battery pack expiry date 3 Operation A ELT The ELT has a switch with the following two positions ON ARM The ON position is fo...

Page 305: ...AIRCRAFT DV 20 E AMM Equipment Furnishings Doc 4 02 25 Rev 2 25 60 00 Page 3 15 Mar 2022 Figure 1 ARTEX Model ME 406 ELT Installation...

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Page 307: ...eneral This table explains how to troubleshoot the ELT system If you find the trouble in column 1 do the repair given in column 3 Trouble Possible Cause Repair ELT does not operate on test ELT batteri...

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Page 309: ...ry to maintain the ELT equipment in a serviceable condition 2 Remove Install the ELT A Remove the ELT Detail Steps Work Items Key Items References 1 Disconnect all the cables from ELT At the ELT 2 Rel...

Page 310: ...AIRCRAFT Equipment Furnishings DV 20 E AMM Page 202 15 Mar 2022 25 60 00 Doc 4 02 25 Rev 2 Figure 2 Removal Installation of ME 406 ELT Artex Antenna Artex Buzzer Artex ELT Strap...

Page 311: ...ane which it was originally registered with then the ELT must be registered and the product label re marked to indicate the new programming and or new country of registry 1 Put the ELT into position t...

Page 312: ...l tower or other monitoring facility tell them before you do the test Detail Steps Work Items Key Items References 1 Set the AVIONICS MASTER switch to ON 2 Set the radio to receive on 121 5 MHz 3 Set...

Page 313: ...s follows S Remove the eight screws from the battery side cover S Carefully move the battery pack a short distance clear of the ELT S Disconnect the wiring harness S Move the battery pack clear of the...

Page 314: ...ttery pack replacement date in the airplane log book 12 Do a functional test of the ELT Refer to Paragraph 3 5 ELT Periodic Inspection The ELT installation must be inspected at least once every 12 mon...

Page 315: ...AIRCRAFT DV 20 E AMM Fire Protection Doc 4 02 25 Rev 2 26 TITLE Page 1 15 Mar 2022 CHAPTER 26 FIRE PROTECTION...

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Page 317: ...AIRCRAFT DV 20 E AMM Fire Protection Doc 4 02 25 Rev 2 26 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 26 FIRE PROTECTION 1 General 1 2 Description 1...

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Page 319: ...the mounting bracket for the fire extinguisher to the baggage compartment floor The extinguisher uses a dry powder which is non toxic The powder does not leave a residue The only on airplane maintenan...

Page 320: ...AIRCRAFT Fire Protection DV 20 E AMM Page 2 15 Mar 2022 26 00 00 Doc 4 02 25 Rev 2 Figure 1 Fire Extinguisher Installation...

Page 321: ...AIRCRAFT DV 20 E AMM Flight Controls Doc 4 02 25 Rev 2 27 TITLE Page 1 15 Mar 2022 CHAPTER 27 FLIGHT CONTROLS...

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Page 323: ...e Control Stick 202 Section 27 10 Flight Controls Aileron and Tabs 1 General 1 2 Description 1 3 Operation 2 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Aileron Control System...

Page 324: ...ontrol Cables 205 Section 27 30 Flight Controls Elevator 1 General 1 2 Description 1 3 Operation 3 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Elevator Control System Test for...

Page 325: ...TS Page 3 15 Mar 2022 Section 27 50 Flight Controls Flaps 1 General 1 2 Description 1 3 Operation 5 4 Fail Safe Operation 5 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove...

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Page 327: ...he cockpit floor The pilot can adjust the position of the rudder pedals with a T grip selector on the rudder pedal assembly The pilot moves each primary control through a system of control rods and be...

Page 328: ...AIRCRAFT Flight Controls DV 20 E AMM Page 2 15 Mar 2022 27 00 00 Doc 4 02 25 Rev 2 Figure 1 Standard Control Rod...

Page 329: ...LLATION PROCEDURE IS NOT DONE CORRECTLY THIS CAN CAUSE DEATH OR INJURY TO PERSONNEL WARNING WHEN YOU DO WORK ON THE AIRPLANE CONTROLS MAKE SURE THAT THE AREA AROUND THE CONTROLS CONTROL SURFACES ARE C...

Page 330: ...cables to the control stick S Disconnect the electrical cables from the control stick S Disconnect the ground cable from the control stick connection Refer to Section 27 10 Figure 1 4 Disconnect the a...

Page 331: ...is at right angles to the control stick with the control sticks centered Torque to 4 5 Nm 3 3 lbf ft Shear nut 4 Connect the ground cable to the control stick Make sure that the cable does not limit...

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Page 333: ...a control rod under the center console The control rod connects to the rear control bellcrank The rear control bellcrank connects to the two long control rods in the wing Each long control rod has 2 p...

Page 334: ...to the rear The control rod below the center console moves the rear bellcrank so that the long control rods in the wing move to the left The aileron bellcrank in the left wing moves the short control...

Page 335: ...AIRCRAFT DV 20 E AMM Flight Controls Doc 4 02 25 Rev 2 27 10 00 Page 3 15 Mar 2022 Figure 1 Aileron Controls in the Fuselage...

Page 336: ...AIRCRAFT Flight Controls DV 20 E AMM Page 4 15 Mar 2022 27 10 00 Doc 4 02 25 Rev 2 Figure 2 Aileron Controls in the Wing...

Page 337: ...ntrol system If you have the trouble detailed in the Trouble column read across to the Possible Cause column Then do the repair given in the Repair column Trouble Possible Cause Repair Airplane moves...

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Page 339: ...ilerons WARNING WHEN YOU DO WORK ON THE AIRPLANE CONTROLS MAKE SURE THAT THE AREA AROUND THE CONTROLS CONTROL SURFACES ARE CLEAR OF PERSONNEL EQUIPMENT IF YOU DO NOT DO THIS INJURY TO PERSONNEL AND DA...

Page 340: ...of each aileron and the trailing edge of the flap S Record these measurements The left aileron must align with the right aileron 5 Remove the control stick lock WARNING WHEN YOU DO WORK ON THE AIRPLAN...

Page 341: ...against the stop 10 Measure the angle between the trailing edge of the right aileron and the trailing edge of the flap S Record these measurements The left aileron must be between 15 and 17 degrees up...

Page 342: ...HIS CAN CAUSE DEATH OR INJURY TO PERSONS A Equipment Item Quantity Part Number Control Stick Lock 1 20 1000 01 00 Quick grips 2 Commercial B Aileron Adjustment Procedure Detail Steps Work Items Key It...

Page 343: ...l the bolts that hold the aileron control rods to the control sticks Use a piece of safety lock wire to make sure that the aileron control rods that you have adjusted are still safe Torque to 6 5 Nm 4...

Page 344: ...8 If necessary adjust the length of the aileron control rods S Release the bolt that holds the aileron control rod to the bellcrank at the forward control bulkhead S Adjust the length of the control...

Page 345: ...aileron down The measurement must be between 15 and 17 degrees with the aileron up and 12 and 14 degrees with the aileron down 12 If necessary adjust the length of the aileron control rod at the ailer...

Page 346: ...the length of the control rod S Install the bolt that holds the aileron control rod to the bellcrank Use a piece of safety lock wire to make sure that the aileron control rods that you have adjusted a...

Page 347: ...ment Refer to Paragraph 2 23 Do an inspection of all the controls that you have adjusted S If necessary for your airworthiness authority do a second inspection of the controls 24 Install the following...

Page 348: ...Between the bellcrank at the aft control bulkhead and the bellcrank in the left right wing Wing left right Refer to Section 57 10 Between the bellcrank in the left right wing and the left right ailer...

Page 349: ...e fuselage behind the seats The yoke attaches to the bottom of the B bulkhead A rudder lower mounting bracket at the rear of the fuselage The rudder attaches to the mounting bracket Cable assemblies S...

Page 350: ...AIRCRAFT Flight Controls DV 20 E AMM Page 2 15 Mar 2022 27 20 00 Doc 4 02 25 Rev 2 Figure 1 Rudder Control System...

Page 351: ...t fuselage cable moves aft with the right side of the yoke The right side of the yoke pulls the right cockpit cables aft And the cables pull the S shaped tubes on the right rudder pedals aft If you mo...

Page 352: ...AIRCRAFT Flight Controls DV 20 E AMM Page 4 15 Mar 2022 27 20 00 Doc 4 02 25 Rev 2 Figure 2 Rudder Pedal Assembly...

Page 353: ...AIRCRAFT DV 20 E AMM Flight Controls Doc 4 02 25 Rev 2 27 20 00 Page 5 15 Mar 2022 Figure 3 Thimble Installation...

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Page 355: ...the trouble detailed in the Trouble column read across to the Possible Cause column and then do the repair given in the Repair column Trouble Possible Cause Repair Airplane moves about its yaw axis Ru...

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Page 357: ...THE AIRPLANE CONTROLS MAKE SURE THAT THE AREA AROUND THE CONTROLS CONTROL SURFACES ARE CLEAR OF PERSONNEL EQUIPMENT IF YOU DO NOT DO THIS INJURY TO PERSONNEL AND DAMAGE TO CONTROL SURFACES CAN OCCUR W...

Page 358: ...position The left pedal must align with the right pedal 4 Set the rudder pedals to fully left S The rudder must hit the stops at the rudder mounting bracket The rudder position must be between 26 28 d...

Page 359: ...pedals fully forward 3 Set the rudder pedals central S Make sure the rudder is in the neutral position The left pedal must align with the right pedal 4 If necessary adjust the length of the cables be...

Page 360: ...osition 7 Set the rudder pedals to fully right S The rudder must hit the stops at the rudder lower mounting bracket The rudder position must be between 26 28 degrees to the right when measured from th...

Page 361: ...oke Detail Steps Work Items Key Items References 1 Remove the following items for access S Pilots seats S Baggage compartment floor S Fuel tank Refer to Section 25 10 Refer to Section 25 10 Refer to S...

Page 362: ...e S tube on the rudder pedal assembly Refer to Figure 1 4 Install the cable to the yoke S Install the bolt that attaches the cable to the yoke S Tighten the bolt Torque to 6 5 Nm 4 6 lbf ft 5 Install...

Page 363: ...he proof test Refer to Figure 3 8 Install the cable to the bracket at the firewall S Install the clevis pin that attaches the cable to the firewall bracket S Install the cotter pin 9 Do a check of the...

Page 364: ...Remove the bolt that attaches the turnbuckle to the rudder yoke S Remove the bolt that attaches the cable to the rudder lower mounting bracket S Cut the eye end from the old cable at the lower bracket...

Page 365: ...igns with the right pedal Refer to Paragraph 3 4 Clamp the cable end by the oval sleeve to prevent thimble from shifting on the cable Use the vise grip pliers with protective sleeves on the jaws to pr...

Page 366: ...stall the rudder Refer to Section 55 40 9 Adjust both the rudder cables to give the correct tension Refer to Paragraph 3 10 Do a check of the rudder range of movement Refer to Paragraph 2 11 Do an ins...

Page 367: ...a short control rod The short control rod attaches to a long control rod behind the aft control bulkhead The aft control bulkhead has an UHMW bush for the short control rod The long control rod has tw...

Page 368: ...AIRCRAFT Flight Controls DV 20 E AMM Page 2 15 Mar 2022 27 30 00 Doc 4 02 25 Rev 2 Figure 1 Elevator Controls...

Page 369: ...ontrol rod aft The short control rod pushes the long control rod aft The long control rod pushes the bellcrank rearward The bellcrank pushes the vertical control rod up The vertical control rod moves...

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Page 371: ...the trouble detailed in the Trouble column read across to the Possible Cause column Then do the repair given in the Repair column Trouble Possible Cause Repair Control vibration in the air Too much ba...

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Page 373: ...N THE AIRPLANE CONTROLS MAKE SURE THAT THE AREA AROUND THE CONTROLS CONTROL SURFACES ARE CLEAR OF PERSONNEL EQUIPMENT IF YOU DO NOT DO THIS INJURY TO PERSONNEL AND DAMAGE TO CONTROL SURFACES CAN OCCUR...

Page 374: ...e elevator The elevator must align with the horizontal stabilizer WARNING WHEN YOU DO WORK ON THE AIRPLANE CONTROLS MAKE SURE THAT THE AREA AROUND THE CONTROLS CONTROL SURFACES ARE CLEAR OF PERSONNEL...

Page 375: ...ty Part Number Protractor 1 Commercial B Elevator Control Adjustment Procedure Detail Steps Work Items Key Items References 1 Remove the following items for access S Pilots seats S Center fuselage acc...

Page 376: ...tube assembly and the bellcrank Use a piece of safety lock wire to make sure the elevator control rods that you have adjusted are still safe Torque to 6 5 Nm 4 6 lbf ft 5 Do a check of the elevator co...

Page 377: ...direction and at the same time will cause the trim motor to operate in that direction 2 Description Figure 1 shows the elevator trim control system The trim control system has the following parts The...

Page 378: ...sher and Bolt Lock Wire Fork Lock Wire Hole DETAIL OF FORK ATTACHMENT TO ACTUATOR Washer Nut Bolt Bottom Mounting Bracket DETAIL OF BOTTOM MOUNTING Washer Washer Electrical Connector Trim Actuator Top...

Page 379: ...the bottom spring This gives an upwards force on the rod The vertical control rod will move upwards until the 2 springs are equally compressed The elevator moves down The actuator will continue to mo...

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Page 381: ...fective Open circuit in the electrical control system Trim switch defective Set the trim circuit breaker Do a test for correct trim system operation If the circuit breaker opens S Do a short circuit t...

Page 382: ...tor trim position indicator out of adjustment Elevator trim position indicator defective Trim electric actuator defective Trim electric actuator disconnected Spring mount assembly defective Adjust ele...

Page 383: ...40 WARNING WHEN YOU DO WORK ON THE AIRPLANE CONTROLS MAKE SURE THAT THE AREA AROUND THE CONTROLS CONTROL SURFACES ARE CLEAR OF PERSONNEL EQUIPMENT IF YOU DO NOT DO THIS INJURY TO PERSONNEL AND DAMAGE...

Page 384: ...Key Items References 1 Put the fork assembly in the correct position Refer to Figure 1 2 Carefully put the elevator trim actuator in the upper mounting bracket S Make sure you align the actuator rod...

Page 385: ...e 1 Torque to 6 5 Nm 4 6 lbf ft 6 Connect the airplane battery Refer to Section 24 31 7 Do an operational check of the elevator trim control system 8 Do a test for correct full and free movement of th...

Page 386: ...y two to get the midpoint of travel 8 Using the elevator trim switch set the trim actuator to the midpoint of travel 9 Use a small screwdriver to adjust the potentiometer on top of the trim position i...

Page 387: ...aft face of the T panel holds the front of the actuator The electric actuator has an electric motor The motor has a reduction gear which turns a spindle The spindle operates a control rod The control...

Page 388: ...AIRCRAFT Flight Controls DV 20 E AMM Page 2 15 Mar 2022 27 50 00 Doc 4 02 25 Rev 2 Figure 1 Flap Control System in the Fuselage...

Page 389: ...hey control 4 power transistors Two of the power transistors can connect the power supply to the flap motor The other two can connect the motor to ground The flap position indicator has three bulbs Th...

Page 390: ...AIRCRAFT Flight Controls DV 20 E AMM Page 4 15 Mar 2022 27 50 00 Doc 4 02 25 Rev 2 Figure 2 Flap Controls in the Aft Control Bulkhead and Wing...

Page 391: ...t and right wing The two short control rods move the flaps When the flaps come to the set position The cam on the flap control rod operates the related position and indication micro switches The logic...

Page 392: ...Looking Forward Flaps CRUISE T O LDG T O CRUISE Cruise Indication and T O Position Moving Down Micro Switch S2 S4 S1 S3 S5 Attaching Screws T O Indication Micro Switch LDG Indication and T O Position...

Page 393: ...ch Short to ground in a wire between a closed micro switch and the control unit Do an insulation test between each wire and ground Repair or replace defective wires Replace the electrical control unit...

Page 394: ...the LDG setting Short to ground in the wires to the electrical control unit from micro switch 4 Do an insulation test between each wire and ground Repair or replace defective wires Flaps move slowly...

Page 395: ...test of the wiring Repair or replace the defective wire No CRUISE indication when the flaps are in the CRUISE position Flaps will not move from CRUISE to T O Flaps move from CRUISE to LDG correctly M...

Page 396: ...perate correctly Long side of cam making contact Rotate switch tray T O light stays on when the flaps are not in the T O position The other indications operate correctly Micro switch 3 defective Repla...

Page 397: ...Items Key Items References 1 If possible set the flaps to the LDG position 2 Disconnect the airplane battery Refer to Section 24 31 3 Remove the pilot s seat Refer to Section 25 10 4 Disconnect the s...

Page 398: ...stall the bolt which attaches the actuator control rod to the bellcrank At the aft control bulkhead Hold the flaps 4 Connect the control harness plug for the switch board 5 Connect the supply wires to...

Page 399: ...clamps which hold the switch board to the actuator body 6 Set the ELECTRIC MASTER switch to ON 7 Set the flap selector switch to LDG 8 Close the FLAP circuit breaker 9 Set the flap selector switch to...

Page 400: ...to ON 22 Set the flap selector switch to T O 23 Do the items 18 to 22 again until the flaps stop correctly 24 Test the flap pre load S Make sure that both flaps contact the bumpers together S Pull do...

Page 401: ...teps 28 to 32 again until the flaps stop correctly 34 When the flaps stop measure the angle on the angle level The angle must be 14 to 16 degrees 35 If necessary adjust the angle with micro switch 5 S...

Page 402: ...44 Do the items 39 to 43 again until the flaps stop correctly 45 When the flaps stop measure the angle on the angle level The angle must be 14 to 16 degrees 46 If necessary adjust the angle with micro...

Page 403: ...G 55 When the flap stops at LDG S Set the flap selector switch to T O 56 When the flaps stop at T O S Make sure that the T O light on the flap position indicator is on 57 If necessary adjust the angle...

Page 404: ...e the angle level 64 Install the cover on the switch board of the flap actuator 65 Do an inspection of the control connections which you disconnected If necessary for your airworthiness authority do a...

Page 405: ...AIRCRAFT DV 20 E AMM Fuel Doc 4 02 25 Rev 2 28 TITLE Page 1 15 Mar 2022 CHAPTER 28 FUEL...

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Page 407: ...ce Practices 1 General 201 2 Remove Install the Fuel Tank 201 3 Remove Install the Fuel Filler Neck 205 4 Flush the Fuel System Procedure 208 5 Replace the Fuel Cap O Rings 210 Section 28 20 Fuel Dist...

Page 408: ...4 02 25 Rev 2 Section 28 40 Fuel Indicating 1 General 1 2 Description 1 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove Install the Fuel Quantity Sensor 201 3 Calibrate the...

Page 409: ...off valve is located below the fuel tank A gascolator The gascolator is located below the fuel tank It has a 62 micron filter screen A fuel line filter is located in the engine compartment An electric...

Page 410: ...AIRCRAFT Fuel DV 20 E AMM Page 2 15 Mar 2022 28 00 00 Doc 4 02 25 Rev 2 Flexible fuel hoses An Air Fuel Separator with integrated orifice...

Page 411: ...AIRCRAFT DV 20 E AMM Fuel Doc 4 02 25 Rev 2 28 00 00 Page 3 15 Mar 2022 Figure 1 Fuel System Schematic...

Page 412: ...line Fuel shut off valve Fuel line filter Fuel returns from the engine to the fuel tank through the following components Fuel return line Maintenance drain tap in the return pipe Check valve With the...

Page 413: ...par bridge and the B bulkhead Pads on the spar bridge and B bulkhead positions the fuel tank A steel band holds the tank in position The baggage compartment floor panel covers the fuel tank The top of...

Page 414: ...ve Hose with Worm Drive Clamps Fuel Supply Connection Finger Filter Fuel Return Connection Fuel Tank Cushion Mount x 2 Fuel Supply Connection Bonding Wire Vent Pipe Refuelling Ground Rubber Hose Worm...

Page 415: ...tion Replace or repair the fuel tank Tighten the connection Fuel tank filler cap leaking Defective filler cap seal Replace the seal Fuel tank connection leaking Defective drain valve seal Damaged thre...

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Page 417: ...ENT WARNING DO NOT GET FUEL ON YOUR SKIN FUEL CAN CAUSE SKIN DISEASE 2 Remove Install the Fuel Tank A Remove the Fuel Tank Detail Steps Work Items Key Items References 1 Disconnect the airplane batter...

Page 418: ...ferences Page 202 15 Mar 2022 28 10 00 Doc 4 02 25 Rev 2 11 Remove the tank from the airplane S Lift the back of the tank upwards and forwards S Turn the tank upside down as you remove it over the sea...

Page 419: ...the tank S Tighten the nuts at each end equally S Pull upwards on the middle of the strap with a spring balance Refer to Figure 2 The movement of the strap must be 0 15 0 23 in at 11 lb load 5 1 mm at...

Page 420: ...CRAFT Fuel DV 20 E AMM Detail Steps Work Items Key Items References Page 204 15 Mar 2022 28 10 00 Doc 4 02 25 Rev 2 11 Install the baggage compartment floor 12 Connect the battery Refer to Chapter 24...

Page 421: ...eck 2 Remove the necessary floor covering from the baggage compartment 3 Inside the baggage compartment pry the fuel filler neck and spacer free from the fuselage Make sure that the fuel cap surround...

Page 422: ...AIRCRAFT Fuel DV 20 E AMM Page 206 15 Mar 2022 28 10 00 Doc 4 02 25 Rev 2 Figure 3 Fuel Filler Neck Removal Installation...

Page 423: ...o washers and locknut 4 Align and install the fuel filler neck assembly and spacer with low adhesion fuel compatible sealant inner fuselage mating surfaces and between the fuel filler spacer and fille...

Page 424: ...fuel 3 Put a fire extinguisher in position next to the airplane 4 Disconnect the fuel feed hose from the fuel fine filter in the engine compartment NOTE Make sure to note the orientation of inline fu...

Page 425: ...4 02 25 Rev 2 28 10 00 Page 209 15 Mar 2022 9 Set the EMERGENCY FUEL PUMP switch to ON S Do a leak check of the fuel feed hose connection S Set the EMERGENCY FUEL PUMP switch to OFF S Set the ELECTRIC...

Page 426: ...BURNS VIOLENTLY THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT WARNING DO NOT GET FUEL ON YOUR SKIN FUEL CAN CAUSE SKIN DISEASE Detail Steps Work Items Key Items References 1 Remove the fue...

Page 427: ...fuel system For example when you clean the fuel filter B Gascolator The gascolator is located below the fuel tank on the left It attaches to the B bulkhead The gascolator is a sediment trap It also ha...

Page 428: ...4 02 25 Rev 2 Figure 1 Fuel Distribution System Fuel Supply Connection Fuel Return Connection Air Fuel Separator Maintenance Drain Taps Fuel Supply Hoses Maintenance Shut Off Valve Gascolator Shut Off...

Page 429: ...tion when you operate the airplane CLOSED The valve stops all fuel flow to the engine G Check Valve A check valve is located beside the fuel tank on the left It is in the fuel return pipe The check va...

Page 430: ...2 Fuel Shut Off Valve Instrument Panel Latch Spring Fuel Shut Off Handle Center Console Side Plate Lever Elbow Shut Off Valve Shut Off Valve Shaft Seal Cover Elbow Fuel Return Hose Fuel Shut Off Brac...

Page 431: ...ell of fuel in the airplane Fuel hose connection loose Electrical fuel pump leaking Gascolator leaking Fuel shut off valve leaking Tighten the connection Replace the fuel pump Repair or replace the ga...

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Page 433: ...nit A Remove the Electric Fuel Pump Unit Detail Steps Work Items Key Items References 1 Disconnect the airplane battery Refer to Chapter 24 31 2 Remove the fuel tank access panels from the bottom of t...

Page 434: ...the electrical connector for the fuel pump unit 6 Install the fuel tank Refer to Chapter 28 10 7 Open the maintenance shut off valve 8 Connect the battery Refer to Chapter 24 31 9 Do a functional tes...

Page 435: ...t Use clean fuel 6 Clean the inside of the gascolator bowl 7 Install the filter and the gascolator bowl Align the arrow on the bowl with the mark on the housing rotate retaining ring counter clockwise...

Page 436: ...SE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT WARNING DO NOT GET FUEL ON YOUR SKIN FUEL CAN CAUSE SKIN DISEASE 5 Drain the fuel lines S Open the maintenance taps at the bottom of the fuselage Use a cor...

Page 437: ...cap from the hose Connect the fuel hose to the fuel valve at the engine side Apply Loctite 545 to the threads of the connector from the third thread aft 6 Tighten the valve stem packing nut to give a...

Page 438: ...Do the fuel shut off valve functional test Refer to Chapter 28 20 4 Functional Test of the Fuel Shut Off Valve Detail Steps Work Items Key Items References 1 Do an engine run up test S Set the engine...

Page 439: ...top of the fuel tank It has a tube which goes close to the bottom of the fuel tank Five screws attach the sensor to the top of the fuel tank A cork gasket makes a fuel tight seal between the tank and...

Page 440: ...AMM Page 2 15 Mar 2022 28 40 00 Doc 4 02 25 Rev 2 Figure 1 Location and Installation of the Fuel Indication Components Fuel Quantity Indicator Attaching Screws Instrument Panel Attaching Screws Fuel Q...

Page 441: ...use Repair Fuel quantity indication incorrect Fuel quantity senor and gauge need calibration and adjustment Fuel quantity sensor defective Fuel quantity gauge defective High resistance connection in t...

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Page 443: ...Work Items Key Items References 1 Disconnect the airplane battery Refer to Chapter 24 31 2 Drain the fuel tank Refer to Chapter 12 10 3 Remove the baggage compartment floor Refer to Chapter 25 10 4 R...

Page 444: ...e a new gasket 3 Put the gasket in position on the sensor The holes for the screws are not equally spaced There is only one correct position 4 Put the sensor in position in the fuel tank The holes for...

Page 445: ...and power off jump the yellow lead of the fuel probe to ground Switch the ELECTRIC MASTER ON and count 10 seconds Then remove the jumper The fuel quantity indicator will fluctuate between empty and f...

Page 446: ...g screws 5 Remove the fuel quantity gauge B Install the Fuel Quantity Gauge Detail Steps Work Items Key Items References 1 Put the fuel quantity gauge in position in the instrument panel 2 Install the...

Page 447: ...AIRCRAFT DV 20 E AMM Indicating Systems Doc 4 02 25 Rev 2 31 TITLE Page 1 15 Mar 2022 CHAPTER 31 INDICATING SYSTEMS...

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Page 449: ...s 1 General 1 2 Description 1 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove Install the Control Panel 201 Section 31 20 Independent Instruments 1 General 1 2 Description...

Page 450: ...202 Section 31 60 Garmin G500 Integrated Display System 1 General 1 2 Description and Operation 1 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove Install the GDU 620 Displa...

Page 451: ...a forward part and an aft part Independent instruments The airplane has an hour meter controlled with the ENGINE MASTER switch Warning Lights Red The airplane has warning lights for canopy unlocked st...

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Page 453: ...MM Chapter for data about the controls For example refer to Chapter 76 00 for data on the engine controls 2 Description A Instrument Panel Figure 1 shows the instrument panel The airplane has an alumi...

Page 454: ...Caution Lights 18 Transponder 4 Backup artificial horizon 19 Battery Backup switch 5 Backup airspeed indicator 20 Fuel Pump Test button 6 Audio panel 21 Emergency Fuel Pump switch 7 Backup altitude i...

Page 455: ...attaches to the center console below the instrument panel It has two control levers for the cabin heat system and one for the parking brake The left lever sets the cabin heat ON or OFF The middle leve...

Page 456: ...RK BRAKE ON ON FLOOR ON OFF ALTERNATE AIR POWER F U L L P R O P E L L E R R P A I D L E ALTERNATE AIR POWER FORWARD Center Console Cover View Looking Down Friction Adjuster FORWARD Heating Distributio...

Page 457: ...do the repair given in column 3 Refer to the related AMM Chapter for other data on an instrument or switch Trouble Possible Cause Repair Indication incorrect Sensor defective Indicator defective High...

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Page 459: ...TER SWITCH IS IN THE OFF POSITION THE BATTERY BACKUP SWITCH IS IN THE OFF POSITION THE THROTTLE IS SET TO IDLE 2 Remove Install the Control Panel A Remove the Control Panel Detail Steps Work Items Key...

Page 460: ...over into position over the heating control levers 2 Move the aft cover forward and down into position around the control levers Make sure that the wires for the trim switch do not catch 3 Install the...

Page 461: ...which is in the instrument panel Refer to Figure 1 in Section 31 10 2 Description and Operation A Hour Meter Hobbs Meter The engine operated hour meter is at the top right of the instrument panel It...

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Page 463: ...e in column 1 do the repair given in column 3 Trouble Possible Cause Repair Hour meter does not operate Hour meter defective High resistance or open connection in the electrical wiring of the hour met...

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Page 465: ...Chapter 24 31 2 Remove the instrument panel cover Refer to Chapter 25 10 3 Release the two faston connectors from the hour meter 4 Remove the two screws and the nuts that attach the hour meter 5 Remov...

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Page 467: ...t of the unit to operate the test switch The ELECTRIC MASTER switch must be ON The main bus provides power to the VOLTAGE and CANOPY warnings through circuit breakers The VOLTAGE and CANOPY warnings o...

Page 468: ...AIRCRAFT Indicating Systems DV 20 E AMM Page 2 15 Mar 2022 31 50 00 Doc 4 02 25 Rev 2 Figure 1 Warning and Cautions Locations...

Page 469: ...AIRCRAFT DV 20 E AMM Indicating Systems Doc 4 02 25 Rev 2 31 50 00 Page 3 15 Mar 2022 Figure 2 Warning and Cautions Location if O M 20 245 b is installed...

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Page 471: ...he trouble in column 1 do the repair given in column 3 Trouble Possible Cause Repair Warning indication incorrect Warning lamp bulb failed Sensor defective High resistance or open connection in the el...

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Page 473: ...the ELECTRIC MASTER ENGINE MASTER and BATTERY BACKUP switches OFF 2 Pull the lens from the front of the annunciator unit 3 Carefully pull the PULL tab to remove the bulb 4 Carefully push the PULL tab...

Page 474: ...ugh the instrument panel into the cockpit B Install an Annunciator Unit Detail Steps Work Items Key Items References 1 Put the annunciator unit in position in the instrument panel Make sure that the s...

Page 475: ...more detailed data about this integrated display system refer to the G500 Cockpit Reference Guide 2 Description and Operation The G500 system consists of Garmin Display Unit GDU 620 PFD MFD Garmin Da...

Page 476: ...light Display PFD and the right side is the Multi Function Display MFD The PFD shows primary flight information The MFD shows navigation and flight plan information and terrain An external configurati...

Page 477: ...Barometric Pressure Indicator The barometric pressure indicator is located immediately below the altitude indicator The indicator shows the barometric pressure that has been set in either inches of me...

Page 478: ...agnetic heading This unit receives power directly from the GRS 77 and communicates with the GRS 77 using an RS 485 digital interface E Databases The GDU 620 utilizes the following databases Basemap Da...

Page 479: ...erting and one higher resolution Terrain database for SVT this higher resolution database can also be used for terrain alerting so only one Terrain database is required for any given installation The...

Page 480: ...AIRCRAFT Indicating Systems DV 20 E AMM Page 6 15 Mar 2022 31 60 00 Doc 4 02 25 Rev 2 Figure 1 Garmin G500 Integrated Display System...

Page 481: ...he GDC OAT probe type shows up as UNKNOWN The RS 232 connection to the GDC 74A is not working Make sure that the GDC 74A RS 232 connection to the GDU is properly wired and that the GDC ADC 74A circuit...

Page 482: ...ng received from an ARINC 429 device no data is being received on the 429 input port as shown on the GDU 620 PORT MONITORING page On the transmitting LRU the ARINC 429 transmitter speed is not set cor...

Page 483: ...how to maintain the components GDU 620 Display GDC 74A Air Data Computer ADC GRS 77 Attitude Heading and Reference Unit AHRS GMU 44 Magnetometer GTP 59 Temperature Probe For more data about maintainin...

Page 484: ...nel to gain access to the three rear connectors S Disconnect the three rear connectors S Remove the GDU 620 display B Install the GDU 620 Display Detail Steps Work Items Key Items References 1 Open th...

Page 485: ...ration settings are stored in the configuration module and will be retained when the GDU 620 display is replaced with a new unit User settings such as map orientation preferences are stored internally...

Page 486: ...tems DV 20 E AMM Page 204 15 Mar 2022 31 60 00 Doc 4 02 25 Rev 2 Figure 2 GDC 74A Air Data Computer ADC Installation Connector Kit Remote Mounting Rack 4 Minimum Fasteners Required Hardware Not Suppli...

Page 487: ...Loosen each thumbscrew on the holddown clamp and remove the clamp S Carefully remove the unit from the mount B Install the GDC 74A Air Data Computer ADC Detail Steps Work Items Key Items References 1...

Page 488: ...ed for proper operation Refer to Chapter 34 10 4 Remove Install the GRS77 Attitude Heading and Reference Unit AHRS A Remove the GRS77 Attitude Heading and Reference Unit AHRS Detail Steps Work Items K...

Page 489: ...AIRCRAFT DV 20 E AMM Indicating Systems Doc 4 02 25 Rev 2 31 60 00 Page 207 15 Mar 2022 Figure 3 GRS 77 Attitude Heading and Reference System AHRS Installation...

Page 490: ...he aft baggage compartment 3 Close the AHRS circuit breaker 4 Connect the airplane battery Refer to Chapter 24 31 5 Energize the G500 system with GDU 620 in normal mode 6 Verify that the GDU 620 displ...

Page 491: ...0 E AMM Indicating Systems Doc 4 02 25 Rev 2 31 60 00 Page 209 15 Mar 2022 Aircraft Mounting Rack Pan Head Brass Screws Flat Head Brass Screws GMU 44 Magnetometer Figure 4 GMU 44 Magnetometer Assembly...

Page 492: ...to the mounting plate S Carefully lift the GMU 44 from the plate S Disconnect the wiring harness 5 Remove the GMU 44 magnetometer B Install the GMU 44 Magnetometer Detail Steps Work Items Key Items Re...

Page 493: ...e ground power cart 7 Verify that no unexpected alerts are present If alerts are present troubleshoot the system 6 Remove Install the Temperature Probe GTP 59 A Remove the Temperature Probe GTP 59 Det...

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Page 495: ...AIRCRAFT DV 20 E AMM Landing Gear Doc 4 02 25 Rev 2 32 TITLE Page 1 15 Mar 2022 CHAPTER 32 LANDING GEAR...

Page 496: ...AIRCRAFT Landing Gear DV 20 E AMM Page 2 15 Mar 2022 32 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 497: ...ear 1 General 1 2 Description and Operation 1 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove Install the Main Landing Gear 201 3 Remove Install the Hardware at the Inner a...

Page 498: ...sembly 213 7 Adjust the Nose Landing Steering Friction 213 8 Nose Wheel Balancing 214 Section 32 40 Wheels and Brakes 1 General 1 2 Description and Operation 1 Trouble Shooting 1 General 101 Maintenan...

Page 499: ...An elastomer spring pack elastomer pack attaches the strut to the engine mount A pivot at the bottom of the strut has a trailing fork for the wheel It also holds the GFRP fairing Nose and main gear h...

Page 500: ...AIRCRAFT Landing Gear DV 20 E AMM Page 2 15 Mar 2022 32 00 00 Doc 4 02 25 Rev 2 Figure 1 Location of Landing Gear Components...

Page 501: ...e Spring washers separate the top face of the spring from the block A castle nut pre loads the spring washers The outer mount is an H shaped bracket The top arms of the H go fore and aft of the spar b...

Page 502: ...AIRCRAFT Landing Gear DV 20 E AMM Page 2 15 Mar 2022 32 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 503: ...and MLG tires WARNING YOU MUST DO A HARD LANDING CHECK AFTER A HARD LANDING HARD LANDINGS CAN CAUSE DAMAGE TO THE STRUCTURE AS WELL AS THE LANDING GEAR Trouble Possible Cause Repair Strut bent Hard la...

Page 504: ...AIRCRAFT Landing Gear DV 20 E AMM Page 102 15 Mar 2022 32 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 505: ...s Refer to Chapter 07 10 2 Remove the wheel fairing S Remove the outer bolt S Remove the two screws on the inner side If installed 3 Remove the back plate from the brake caliper Refer to Chapter 32 40...

Page 506: ...1 10 for GFRP inspection procedures 2 Install the retaining bar Install the bolts the washers and the nuts to hold the retaining bar to the outer mount attachment bracket Leave the hardware loose 3 Ap...

Page 507: ...washers and the inner mount on the high side 8 Tighten the nuts on the outer mount Torque to 15 20 Nm 132 177 lbf in Make sure that there is no gap between the retaining bar and the outer mount 9 Tig...

Page 508: ...04 15 Mar 2022 32 10 00 Doc 4 02 25 Rev 2 16 Install the wheel fairing Install the outer bolt S Install the two screws on the inner side Airplane with wheel fairing option only 17 Lower the airplane w...

Page 509: ...Mount Outer Mount Main Gear Strut Axle Belleville Washers Plain Washer Bonding Tape Convex Washer Concave Washer Plain Washer Nut Brass Strip Brass Strip UHMW Insert Retaining Bar Plain Washer Nut Pla...

Page 510: ...AIRCRAFT Landing Gear DV 20 E AMM Page 206 15 Mar 2022 32 10 00 Doc 4 02 25 Rev 2 Figure 2 Main Landing Gear...

Page 511: ...Remove the hardware from the inner mount of the main landing gear strut as follows Note The inner mount is not removed Note The bolts for the forward side and rear side are different in length The wa...

Page 512: ...in length The washers are installed on the bolt side and the nut side S Remove the nuts bolts and washers at the forward side of the outer mount S Remove the nuts the bolts and the washers at the rea...

Page 513: ...rear side are the same in length The washers are installed on the bolt side and the nut side S Install the bolts the washers and the nuts at the rear side of the outer mount and spar bridge S Torque...

Page 514: ...l the bolts the washers and the nuts at the rear side of the inner mount and spar bridge S Torque the bolts to 5 6 7 9 Nm 50 70 lbf in S Install the bolts the washers and the nuts at the forward side...

Page 515: ...AIRCRAFT DV 20 E AMM Landing Gear Doc 4 02 25 Rev 2 32 10 00 Page 211 15 Mar 2022 Figure 3 Measure Toe In and Camber...

Page 516: ...asure the toe in Refer to Figure 3 4 Measure the camber Refer to Figure 3 WARNING USE ONLY THE SHIMS LISTED FOR THE PURPOSE IN THE AIRPLANE ILLUSTRATED PARTS CATALOG OTHER SHIMS COULD CAUSE LANDING GE...

Page 517: ...olds the bottom of the shock absorber assembly The upper end of the shock absorber assembly attaches to the engine mount The forward bottom end of the nose gear strut has a near vertical pivot for the...

Page 518: ...AMM Page 2 15 Mar 2022 32 20 00 Doc 4 02 25 Rev 2 Figure 1 Nose Landing Gear Pivot Stop Pivot Nut Shock Absorber Assembly Attachment to Engine Mount Bearing Stainless Steel Bush in Fuselage Fairing A...

Page 519: ...across to the Possible Cause column Then do the repair given in the Repair column WARNING YOU MUST DO A HARD LANDING CHECK AFTER A HARD LANDING HARD LANDINGS CAN CAUSE DAMAGE TO THE STRUCTURE AS WELL...

Page 520: ...AIRCRAFT Landing Gear DV 20 E AMM Page 102 15 Mar 2022 32 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 521: ...07 10 2 Remove the engine cowling Refer to Chapter 71 10 3 Disconnect the shock absorber assembly from the nose landing gear strut as follows S Remove the rivets Discard the rivets S Remove the two cl...

Page 522: ...sembly Shock Absorber Assembly Bearing Stainless Steel Bush in Fuselage Eye End Center Tube Rubber Damper Washer Adjusting Nut Bearing Spacers x5 Rubber Dampers x5 Stud Spring Pin Engine Mounting Fram...

Page 523: ...om the journal to engage the bearings in the fuselage S Drill a 2 mm 0 015 mm hole in the large pivot through the pilot hole in the strut journal one side only S Slide the large pivot inwards and remo...

Page 524: ...put the nose gear strut in position in the airplane from below 4 Slide out the large pivot of the unit to engage the bearings in the fuselage Refer to Figure 2 5 Install the lock bolt in the journal b...

Page 525: ...AIRCRAFT DV 20 E AMM Landing Gear Doc 4 02 25 Rev 2 32 20 00 Page 205 15 Mar 2022 Figure 3 Lock Bolt Hole Centerline Position...

Page 526: ...Remove the NLG Fork Assembly Detail Steps Work Items Key Items References 1 Jack the airplane Refer to Chapter 07 10 2 Remove fairing if installed 3 Remove the cotter pin castellated nut washers and...

Page 527: ...AIRCRAFT DV 20 E AMM Landing Gear Doc 4 02 25 Rev 2 32 20 00 Page 207 15 Mar 2022 Figure 5 NLG Fork Installation...

Page 528: ...NLG strut S Install the thrust washer the stop plate and the lower spacer S Install the spring disc the washers and the Castellated nut S Tightened the nut to achieve break out S force S Install the...

Page 529: ...AIRCRAFT DV 20 E AMM Landing Gear Doc 4 02 25 Rev 2 32 20 00 Page 209 15 Mar 2022 Figure 6 Adjust the Nose Wheel Steering Friction...

Page 530: ...PORT THE NOSE LANDING GEAR PRIOR TO REMOVAL OF THE UNIT FAILURE TO SUPPORT THE ASSEMBLY WILL DAMAGE THE EQUIPMENT AND MAY CAUSE HARM OR INJURY TO PERSONNEL 3 Disconnect the shock absorber assembly fro...

Page 531: ...ion protection on strut pins and clip retainers S Install the shock absorber assembly using the strut pins S Install the clip retainers and secure with rivets Refer to Figure 2 Use Mastinox 6856K Clea...

Page 532: ...CAUSE INJURY TO PERSONNEL 2 Disassemble the shock absorber assembly S Remove the adjusting nut from the shock absorber assembly S Remove the washer and the rubber damper S Remove the shock absorber r...

Page 533: ...Procedure Detail Steps Work Items Key Items References 1 Jack the airplane Refer to Chapter 07 10 2 Remove the nose wheel fairing 3 Inspect condition of belleville springs washers spacer and stop pla...

Page 534: ...sion protection to the stud nut and washers only Use CRC SP 400 or CRC Corrosion shell Do not contaminate tire or fiberglass 7 Install the nose wheel fairing 8 Remove the trestle from the front fusela...

Page 535: ...diagram The DV 20 E airplane has two separate brake systems The pilots and co pilots left rudder pedals operate the left system It supplies pressure to the left brake caliper The right rudder pedals o...

Page 536: ...ion from the co pilots master cylinder is cut off by the initial movement Note Any hydraulic pressure from the co pilot s master cylinder pushes on the back of the piston in the pilot s master cylinde...

Page 537: ...Page 3 15 Mar 2022 3 Parking Brake Operation To apply the parking brake Press on both pedals Pull the parking brake knob fully aft Release your foot pressure on the pedals If necessary pump the brake...

Page 538: ...Inner Tube NOSE WHEEL MAIN WHEEL Inner Tube Snap Ring Seals Seals Bearing Bearing Hub Brake Disc Bolt Washer Washer Self Locking Nut Hub Nut Nut Washer Washer Hub Hub Axle Nut Cotter Pin Bolt Bolt Fla...

Page 539: ...AIRCRAFT DV 20 E AMM Landing Gear Doc 4 02 25 Rev 2 32 40 00 Page 5 15 Mar 2022 Figure 2 Brake System Schematic...

Page 540: ...AIRCRAFT Landing Gear DV 20 E AMM Page 6 15 Mar 2022 32 40 00 Doc 4 02 25 Rev 2 Figure 3 Brake Master Cylinder and Reservoir Installation...

Page 541: ...AIRCRAFT DV 20 E AMM Landing Gear Doc 4 02 25 Rev 2 32 40 00 Page 7 15 Mar 2022 Figure 4 Wheel Brake Assembly...

Page 542: ...AIRCRAFT Landing Gear DV 20 E AMM Page 8 15 Mar 2022 32 40 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 543: ...arings Brake disk distorted Brakes applied too hard Hard landing Replace the brake disk Brakes do not hold static engine run up with the usual pedal force Too much light braking Brake lining glaze wor...

Page 544: ...AIRCRAFT Landing Gear DV 20 E AMM Page 102 15 Mar 2022 32 40 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 545: ...antity Part Number Airplane jacks 2 Commercial Tail former 1 B Remove the Main Wheel Detail Steps Work Items Key Items References 1 Remove the wheel fairing S Remove the outer bolt S Remove the two sc...

Page 546: ...g of the wheel bearing grease to the axle bearings installation areas Use grease TYPE 1 Refer to Chapter 12 20 4 Install the slotted ring or seal axle inner with wheel bearing grease between the slott...

Page 547: ...Measure the end play in the hub assembly Wheel must rotate freely without perceptible play 11 Install a new cotter pin Bend the ends of the cotter pin against the axle nut Check security of the wheel...

Page 548: ...ng screws S Remove the fairing 2 Use weights to hold the rear fuselage down with the nose wheel clear of the ground Use a strap around the rear fuselage 3 Put a padded trestle under the front fuselage...

Page 549: ...wheel in position in the fork 3 Install the axle shims between the wheel axle spacers and the fork assembly Select the shims thickness as required to fill the gap 4 Divide shim installation evenly fr...

Page 550: ...Work Items Key Items References Page 206 15 Mar 2022 32 40 00 Doc 4 02 25 Rev 2 9 Install the wheel fairing if applicable S Put the two halves in position S Install the LH and RH mounting screws S Ins...

Page 551: ...ILT BRAKE FLUID IMMEDIATELY BRAKE FLUID CAN DAMAGE PAINT AND OTHER MATERIAL 1 Disconnect the brake pipe s from the brake master cylinder Catch the brake fluid Refer to Figure 3 Put the caps on the con...

Page 552: ...on on the bottom pivot pin Refer to Figure 3 2 Attach the master cylinder to the bottom pivot pin S Install the washer S Install the cotter pin 3 Install the top pivot pin as follows S Install the piv...

Page 553: ...TERIAL 2 Disconnect the brake pipe or hose from the caliper Catch the brake fluid Put the caps on the connections 3 Remove the pressure plate and the caliper from the torque plate B Install a Brake Ca...

Page 554: ...AIRCRAFT Landing Gear DV 20 E AMM Page 210 15 Mar 2022 32 40 00 Doc 4 02 25 Rev 2 Figure 5 Parking Brake Valve Installation...

Page 555: ...Loosen the bolt in the end fitting S Pull the center wire from the end fitting Refer to Figure 5 WARNING DO NOT GET BRAKE FLUID ON YOU BRAKE FLUID CAN CAUSE DISEASE CAUTION CLEAN UP SPILT BRAKE FLUID...

Page 556: ...t the four brake pipes to the parking brake valve 4 Put center wire of the bowden cable through the end fitting on the parking brake lever Tighten the bolt With the brake lever in the center console s...

Page 557: ...IMMEDIATELY BRAKE FLUID CAN DAMAGE PAINT AND OTHER MATERIAL 3 Connect the transparent overflow pipe to the reservoir Put the free end of the pipe in a container 4 Clean the area around the bleed nippl...

Page 558: ...f the brake system 8 Condition of the Brake Linings The brake linings are a non asbestos organic material You must condition new brake linings Conditioning gives a thin layer of glaze at the friction...

Page 559: ...ES WITH EACH OTHER IF USING OTHER APPROVED GREASE COMPLETE REMOVAL OF CONTAINED GREASE AND BEARING CLEANING IS REQUIRED REPLACEMENT OF PREVIOUSLY LUBRICATED FELT GREASE SEALS IS ALSO REQUIRED 2 Inspec...

Page 560: ...aragraph 2 B CAUTION DO NOT USE HIGH PRESSURE SPRAY WASH EQUIPMENT THE USE OF HIGH PRESSURE SPRAY WASH MAY INJECT SOAP SOLUTION AND WATER INTO BEARINGS AND OTHER INTERNAL CAVITIES RESULTING IN CORROSI...

Page 561: ...AIRCRAFT DV 20 E AMM Lights Doc 4 02 25 Rev 2 33 TITLE Page 1 15 Mar 2022 CHAPTER 33 LIGHTS...

Page 562: ...AIRCRAFT Lights DV 20 E AMM Page 2 15 Mar 2022 33 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 563: ...neral 101 Maintenance Practices 1 General 201 2 Remove Install the General Instrument Light Map Light Module 201 Section 33 40 Exterior Lights 1 General 1 2 Description 1 Trouble Shooting 1 General 10...

Page 564: ...AIRCRAFT Lights DV 20 E AMM Page 2 15 Mar 2022 33 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 565: ...ng for the standby instruments Some avionics equipment has internal lighting Refer to the related chapter and the manufacturers handbooks for the equipment in your airplane The controls for the interi...

Page 566: ...ocated inboard in the housing Taxi light The taxi light has a optic lens and a 35 Watt bulb If O M 20 271 is installed the DV 20 E has a LED taxi light It is located outboard in the housing The switch...

Page 567: ...has internal lighting Refer to the related AMM Chapter and the manufacturers handbooks for the equipment in your airplane A General Instrument Panel Lighting Two lights give general lighting to the in...

Page 568: ...AIRCRAFT Lights DV 20 E AMM Page 2 15 Mar 2022 33 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 569: ...dule Defective wiring Set the circuit breaker Replace the switch potentiometer Check wiring and repair replace lighting control module Do a continuity test of the wiring Repair replace defective wirin...

Page 570: ...AIRCRAFT Lights DV 20 E AMM Page 102 15 Mar 2022 33 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 571: ...wiring harness S Remove the light B Install a Instrument Light Map Light Module Detail Steps Work Items Key Items References 1 Put the light in position and connect the wiring harness 2 Install the sc...

Page 572: ...AIRCRAFT Lights DV 20 E AMM Page 202 15 Mar 2022 33 20 00 Doc 4 02 25 Rev 2 Figure 1 General Instrument Light Map Light Adjustment...

Page 573: ...he anti collision light is designed with 24 white LEDs If one of the LEDs fails the unit must be replaced The position lights and the anti collision lights are controlled by separate switches and are...

Page 574: ...Mar 2022 33 40 00 Doc 4 02 25 Rev 2 Figure 1 Wing Tip Light Unit In Line Connector LH SHOWN LED Position and Anti Collision Light Assy Base Plate Rear Position Light Anti Collision Light Screw Clear L...

Page 575: ...ing Refer to Chapter 92 for wiring diagrams One position light does not operate Defective light unit Defective wiring Replace the light unit Do a continuity test of the wiring Repair replace defective...

Page 576: ...ircuit breaker not set or defective Defective landing or taxiing light switch Defective wiring in forward cockpit area Loose connector next to the light Replace the light unit Set replace the circuit...

Page 577: ...ERATES ANTI COLLISION LIGHTS CAN CAUSE EYE DAMAGE 2 Remove Install the Taxi Light A Remove the Taxi Light Detail Steps Work Items Key Items References 1 Set the ELECTRIC MASTER switch to OFF 2 Open th...

Page 578: ...AIRCRAFT Lights DV 20 E AMM Page 202 15 Mar 2022 33 40 00 Doc 4 02 25 Rev 2 Figure 2 Landing and Taxi Light Installation Sheet 1...

Page 579: ...ts Doc 4 02 25 Rev 2 33 40 00 Page 203 15 Mar 2022 Figure 3 Landing and Taxi Light Installation LED Lights if O M 20 271 is installed LED Taxi Light LED Landing Light Landing Light Mounting Bracket Ta...

Page 580: ...nstalled behind the light Do not tighten the lock nuts at this time 4 Install the taxi light assembly to the wing with the attaching screws Refer to Figure 4 for the alignment dimensions of the four s...

Page 581: ...AIRCRAFT DV 20 E AMM Lights Doc 4 02 25 Rev 2 33 40 00 Page 205 15 Mar 2022 Figure 4 Landing and Taxi Light Installation Sheet 2...

Page 582: ...3 Remove the taxi landing light cover from the wing S Examine the white vinyl tape on the cover for damage If necessary replace the tape 4 Loosen the lock nuts and remove the screws that attach the l...

Page 583: ...nstalled behind the light Do not tighten the lock nuts at this time 4 Install the landing light assembly to the wing with the attaching screws Refer to Figure 4 for the alignment dimensions of the fou...

Page 584: ...nsions S When the alignment is complete tighten the lock nuts of the four attaching screws behind the light If O M 20 271 is installed S Loosen the four lock nuts S Adjust LED light to the correct ali...

Page 585: ...t from the wing tip S Disconnect the two electrical connections from the rear of the light unit S Remove the light unit B Install the Light Unit in the Wing Tip Detail Steps Work Items Key Items Refer...

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Page 587: ...AIRCRAFT DV 20 E AMM Navigation Doc 4 02 25 Rev 2 34 TITLE Page 1 15 Mar 2022 CHAPTER 34 NAVIGATION...

Page 588: ...AIRCRAFT Navigation DV 20 E AMM Page 2 15 Mar 2022 34 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 589: ...intenance Practices 1 General 201 2 Remove Install a Pitot Static Instrument 201 3 Remove Install the Pitot Probe 202 4 Pitot and Static Leak Tests 203 Section 34 20 Attitude and Direction 1 General 1...

Page 590: ...and Taxiing Aids 1 General 1 2 Description and Operation 1 Trouble Shooting 1 General 101 Section 34 50 Dependent Position Determining 1 General 1 Trouble Shooting 1 General 101 Maintenance Practices...

Page 591: ...he transponder and Global Positioning Systems GPS This chapter describes only the on airplane data about the systems and components Refer to the manufacturers handbooks for shop data Many different in...

Page 592: ...irection system has the following components Magnetic compass Backup artificial horizon C Landing and Taxiing Aids The audio control panel has a marker beacon receiver D Dependent Position Determining...

Page 593: ...struments A pitot static probe mounted below the left wing senses pitot and static pressure The probe has an internal heater element Flexible hoses connect the pitot static probe to the air data instr...

Page 594: ...10 00 Doc 4 02 25 Rev 2 Figure 1 Flight Environment Data Component Locations Temperature Sensor for the OAT Indicator Water Traps below Left Seat In Line Connectors at Wing Root Flight Instruments Pit...

Page 595: ...Airspeed indicator reads low Faulty indicator Blocked or kinked pitot hose Water in the system Replace the indicator Clear the hose Drain the water Pitot heat does not operate PITOT circuit breaker i...

Page 596: ...AIRCRAFT Navigation DV 20 E AMM Page 102 15 Mar 2022 34 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 597: ...pitot static hoses from the rear of the indicator 3 Remove the mounting screws Hold the instrument 4 Remove the instrument from the panel B Install a Pitot Static Instrument Detail Steps Work Items Ke...

Page 598: ...onnections Put the caps on the hoses 4 Disconnect the bonding cable and electrical connector 5 Remove the pitot static probe B Install the Pitot Probe Detail Steps Work Items Key Items References 1 Ho...

Page 599: ...UTIONS YOU CAN DAMAGE THE AIR DATA INSTRUMENTS A Test Precautions S The pressure in the pitot system must be equal to or greater than the pressure in the static system S Reversal of the pitot and stat...

Page 600: ...Apply a partial vacuum to the static port until you get a pressure altitude of 1000 ft above the ambient pressure altitude Note the altitude 4 Let the pressure stabilize 5 Monitor the system pressure...

Page 601: ...k tester to the pitot static probe 3 Apply a pressure to the pitot port equal to 150 knots 4 Let the pressure stabilize 5 Monitor the system pressure The leak rate must not be more than 10 knots min 6...

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Page 603: ...on the right hand side There is also an artificial horizon installed in the instrument panel arranged centrally Refer to the manufacturer s manuals for data about these instruments 2 Description and O...

Page 604: ...s behind the symbolic airplane Precession error is corrected by the internal erection system or by pulling the PULL TO CAGE knob A warning flag drops into view to indicate that the gyro motor is not r...

Page 605: ...he power supply wiring connector Do a test for correct ground connection Repair the ground wiring connector Replace the instrument Magnetic compass leaking fluid Defective compass housing Replace the...

Page 606: ...AIRCRAFT Navigation DV 20 E AMM Page 102 15 Mar 2022 34 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 607: ...only the correct shock proof container for shipping Mark the container VERY FRAGILE HANDLE LIKE RAW EGGS 2 Remove Install the Magnetic Compass A Remove the Magnetic Compass Detail Steps Work Items Key...

Page 608: ...THE COMPASS CAUTION DO NOT WEAR OR CARRY METALIC MATERIAL WATCHES BRACELETS ETC WHEN YOU ADJUST THE COMPENSATING MAGNETS OR OPERATE THE LAND COMPASS METALIC MATERIAL CAN CAUSE ERRORS NOTE If possible...

Page 609: ...the E W compensator so that the compass indicates a heading of 90 degrees 6 Align the airplane to magnetic south Adjust the N S compensator so that the compass indicates a heading of 180 degrees 7 Ali...

Page 610: ...zon Indicator Detail Steps Work Items Key Items References 1 Place the Artificial Horizon Indicator in position in the instrument panel 2 Install the three mounting screws 3 Plug in connector 3490 01...

Page 611: ...to the manufacturers manuals for data about the equipment installed Refer to Chapter 23 50 for maintenance practices to remove install the GMA 340 audio panel 2 Description and Operation The GMA 340 i...

Page 612: ...AIRCRAFT Navigation DV 20 E AMM Page 2 15 Mar 2022 34 30 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 613: ...le Cause Repair Test operates correctly but the marker does not operate Faulty marker receiver Poor co ax connections Faulty antenna Replace the GMA 340 Examine the co ax connectors for condition and...

Page 614: ...AIRCRAFT Navigation DV 20 E AMM Page 102 15 Mar 2022 34 30 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 615: ...34 50 Dependent Position Determining 1 General This chapter describes about the equipment that shows dependent position determining The DV 20 E airplane has the following position determining systems...

Page 616: ...dbased radar on a frequency of 1090 MHz The GTX 328 330 is equipped with IDENT capability that activates the Special Position Identification SPI pulse for 18 seconds The GTX 328 330 replies to ATCRBS...

Page 617: ...Mode S interrogations ON Selects Mode A and Mode S In this mode the transponder replies to Mode A and Mode C interrogations as indicated by the Reply Symbol but the replies do not include altitude inf...

Page 618: ...onal by default but can be disabled in configuration mode FUNC Changes the page shown on the right side of the display Display data includes Pressure Altitude Flight Time Count Up and Count Down timer...

Page 619: ...Function Hints Transponder Panel Control Optional B GTN 650 The GTN 650 is a VHF communications transceiver and a GPS receiver Refer to Chapter 23 10 for COM functions It also includes VOR Localizer a...

Page 620: ...Navigation page from any other page Direct To Key provides access to the direct to function which allows you to enter a waypoint and establishes a direct course to the selected destination Large and...

Page 621: ...ble Possible Cause Repair ATC reports no reply Transponder reply lamp flashes Low output power Examine the antenna connections Replace the transponder ATC reports no reply Transponder reply lamp does...

Page 622: ...AIRCRAFT Navigation DV 20 E AMM Page 102 15 Mar 2022 34 50 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 623: ...Transponder Detail Steps Work Items Key Items References 1 Open the related circuit breaker 2 Put a 3 32 allen wrench into the access hole for the locking screw in the front panel Engage the screw 3 T...

Page 624: ...nism is in a vertical position This can be accomplished by using a 3 32 inch allen wrench through the face plate 2 Insert the transponder slowly until the front lobe of the unit touches the mounting r...

Page 625: ...AIRCRAFT DV 20 E AMM Standard Practices and Structures Doc 4 02 25 Rev 2 51 TITLE Page 1 15 Mar 2022 CHAPTER 51 STANDARD PRACTICES AND STRUCTURES...

Page 626: ...AIRCRAFT Standard Practices and Structures DV 20 E AMM Page 2 15 Mar 2022 51 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 627: ...wich Structure 2 5 Bonded Components 2 6 Repair Limitations 2 7 Identification of Primary Structure 3 Section 51 10 Investigation 1 General 1 2 Damage Classification 1 3 Types of Damage 2 4 Inspection...

Page 628: ...ices 1 General 201 2 Resin 201 3 Glass and Carbon Cloth 202 4 Core Material 202 5 Laminating 203 6 Bonding Paste Thickened Resin 207 7 Curing 207 8 Exterior Paint Finish 208 9 Repair of Fire Retardant...

Page 629: ...rotects the airplane against moisture and ultraviolet rays 2 Types of Structure The DV 20 E is constructed from two main types of composite structure A Glass Fiber Reinforced Plastic GFRP GFRP is very...

Page 630: ...GFRP make the skins and rigid plastic foam makes the core The skins must bond to the core of a sandwich structure completely If the skins do not bond to the core the component can fail 5 Bonded Compo...

Page 631: ...ary structure of the DV 20 E consists of the following components A Wing Spar Ribs Web at hinge line Skin Wing fuselage connection Ailerons Wing flaps B Fuselage Skin Bulkheads and stiffeners Rudder f...

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Page 633: ...ed into the classes described below In doubtful cases i e if you are not sure about the classification of a damage you must contact the airplane manufacturer A Class 1 Major structural damage that req...

Page 634: ...jor cracks do not occur with normal flight loads or normal landing loads You must repair major cracks 4 Inspection Techniques A Examine Visually Use this method to find all types of damage to composit...

Page 635: ...damage for secondary damage which can remain undetected 5 Further Inspection If you find paint damage when you examine a composite structure then do this further inspection Find a way to see the insi...

Page 636: ...AIRCRAFT Standard Practices and Structures DV 20 E AMM Page 4 15 Mar 2022 51 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 637: ...plane after a large repair and calculate the center of gravity Refer to Section 08 10 for data about weighing the airplane 3 Control Surface Balancing When you repair a control surface it becomes heav...

Page 638: ...esins hardeners and solvents used for composite repairs are poisonous You must not take food into the work area Use a mask to protect your face and use eye protection WARNING DO NOT GET RESINS HARDENE...

Page 639: ...nding dust as it occurs The working area must not be affected by air draughts The temperature of the workshop should be maintained between 18 C 65 F and 27 C 77 F and must not fall below 15 C 59 F The...

Page 640: ...AIRCRAFT Standard Practices and Structures DV 20 E AMM Page 4 15 Mar 2022 51 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 641: ...a composite structure is stressed Failure of the structure can cause an accident 2 Resin You must use the correct quantity of mixed resin for the repair Weigh all the cut cloth patches that you will...

Page 642: ...ns of the layer Make sure that the fibers in each layer of cloth point in the direction given in the lay up drawing This gives the correct strength to the laminate Only use sharp shears or scissors to...

Page 643: ...ure once the laminate is hardened and fully cured You can make the laminate in place directly on the repair or you can make the laminate on a work table and then apply the wet laminate to the repair W...

Page 644: ...IN YOUR EYES THESE CHEMICALS CAN CAUSE DISEASE 4 Apply a thin coat of resin to the repair 5 Apply the first layer of cloth to the repair and trim to the correct size Make sure that the fibers in the c...

Page 645: ...to S Trace onto the plastic sheet the extreme outline of the repair S Trace onto the plastic sheet the contour lines of each layer of cloth in the structure The outer layer of the structure must be t...

Page 646: ...11 Do steps 9 and 10 as necessary until all the layers of cloth are in place 12 Apply a thin coat of resin to the area of the repair on the structure where you will attach the laminate patch 13 Put th...

Page 647: ...t curing The following procedure gives a typical curing process Detail Steps Work Items Key Items References 1 Maintain the temperature of the repair at 20 C to 25 C 68 F to 77 F for at least 24 hours...

Page 648: ...GREASE OR DUST ON THE REPAIR AREA GREASE AND DUST PREVENT A GOOD BOND 1 Make sure that the area to be repaired is clean and free from any contaminants If necessary use acetone and re sand the area 2 A...

Page 649: ...SKIN DISEASE WARNING DO NOT BREATHE ACETONE FUMES ACETONE FUMES CAN CAUSE DISEASE 1 Sand the repair area with 150 grit sanding paper 2 Make sure that the area to be repaired is clean and free from an...

Page 650: ...Interglas 92110 glass 2 2 twill 163 0 17 7 8 4551 60 Interglas 92125 glass 2 2 twill 280 0 30 12 8 4554 60 Interglas 92140 glass 2 2 twill 390 0 43 18 8 4520 6 Interglas 92145 glass uni directional 22...

Page 651: ...ged loose laminate until the edges of the laminates bond together and to any core material Refer to Figure 1 Use a sharp knife or grinding disk 4 Scarf the edges of the repair area with a grinding dis...

Page 652: ...AMM Page 212 15 Mar 2022 51 20 00 Doc 4 02 25 Rev 2 Scarf the Edges of the Repair Area Repair the Laminate Contour the Laminate New Laminate New Laminate Laminate Foam Core Remove Damaged Loose Lamin...

Page 653: ...LS CAN CAUSE DISEASE 7 Repair the laminate Use one of the 2 methods given in Paragraph 5 8 Pre cure the repair Refer to Paragraph 7 9 Post cure the repair Refer to Paragraph 7 10 When the repair is fu...

Page 654: ...Remove Damaged Loose Laminate Remove Damaged Foam Core and Scarf Laminate min 20 mm 0 8 in min 20 mm 0 8 in Scarf Scarf Foam Insert Foam Insert Laminate Laminate Insert the Laminate and Foam Core into...

Page 655: ...damaged foam core Remove sufficient foam core to give a minimum of a 20 mm 0 8 in edge around the outside of the damaged area Refer to Figure 1 5 Scarf the edges of the external laminate repair area w...

Page 656: ...am core Make sure that the fibers in the cloth point in the correct direction Refer to Paragraph 6 Use one of the 2 methods given in Paragraph 5 10 Apply a thin coat of resin to the area to be repaire...

Page 657: ...Mar 2022 20 When the repair is fully post cured remove any peel ply and sand smooth the surface of the repair 21 Contour the repair so that the final surface level of the repair is slightly lower than...

Page 658: ...Items Key Items References WARNING OBEY THE SAFETY PRECAUTIONS THAT FOLLOW WHEN YOU DO WORK WITH COMPOSITE MATERIALS DO THE WORK IN AN AREA THAT HAS A GOOD FLOW OF CLEAN AIR USE APPROVED EYE MOUTH AND...

Page 659: ...at will not be painted Use masking tape to hold the cover s in place Make sure that you do not damage the laminate Only remove the transparent top coat and the fire resistant paint WARNING OBEY THE SA...

Page 660: ...010 in 250 microns Make sure that the painting is done in a dust free area 6 Let the fire resistant paint dry in a dust free area for a minimum of 24 hours 7 Before the transparent top coat is applie...

Page 661: ...uctures Detail Steps Work Items Key Items References Doc 4 02 25 Rev 2 51 20 00 Page 221 15 Mar 2022 13 Visually inspect the completed paint repair s Make sure that there are no defects such as bubble...

Page 662: ...AIRCRAFT Standard Practices and Structures DV 20 E AMM Page 222 15 Mar 2022 51 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 663: ...airplane Note If the approved material for the repair work is not available please contact Diamond Aircraft Industries for information about alternative materials 2 Approved Materials A Resin System R...

Page 664: ...3063 8 4554 60 2 2 twill 390 92140 1989 8 4520 6 UD 220 92145 8 4525 60 UD 425 92146 All cloth types consist of alkali free E glass with I 550 or PT 55 finish and comply with LN 9169 German aviation s...

Page 665: ...2 twill 200 98141 CCC 452 UD tape 380 Sigratex KDU 1034 The cloth complies with LN 9169 German aviation standard Supplier for Interglas fabric Rudolf Usner GmbH see above Supplier for Cramer fabric C...

Page 666: ...al Type PVC rigid foam Divinycell H 60 Thickness 3 mm 6 mm 8 mm Supplier Conti Tech Kautschuk und KunststoffvertriebsgesmbH Industriestr 31 A 2353 Guntramsdorf Austria Phone 43 2236 49101 0 Fax 43 223...

Page 667: ...rkt Allhau Nr 463 A 7411 Markt Allhau Austria Phone 43 3356 20444 Fax 43 3356 20445 E Mail chemie polychem at G Exterior Paint 1 Putty a Putty Sikkens Polysoft Manufacturer Akzo Nobel Supplier Akzo No...

Page 668: ...Coating Paint a Durodur Coating paint Durodur 3067 R916g color RAL 9016 white or DB 147 white Manufacturer Morton International GmbH Strullendorf Germany Supplier Lorenz Industrielacke see above or b...

Page 669: ...above or b Putty ICI P551 1052 Manufacturer ICI Paints Berkshire Great Britain Supplier ICI Autocolor see above 2 Coating Paint Glare shield Nuvovern DS 10 1 Nuvovern ACR Instr panel cover Nuvovern DS...

Page 670: ...aulds Aerospace 4232 0303 Hardener Courtaulds Aerospace N 39 1327 4 1 Supplier PRO DeSoto Deutschland GmbH Aerospace Coatings Lauenburger Landstr 11 D 21039 B rnsen Germany Phone 49 40 742193 10 Fax 4...

Page 671: ...8B900D Hardener 9008B or b Fire retardant paint Desothane HS Matt Clear Coat CA8720M0900C Hardener CA8000B Manufacturer PPG Aerospace Supplier PRC Desoto International Hein Sass Weg 29 D 21129 Hamburg...

Page 672: ...AIRCRAFT Standard Practices and Structures DV 20 E AMM Page 10 15 Mar 2022 51 30 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 673: ...the control surface Any report of control vibration or flutter in flight You can use any convenient method to weigh a control surface If you use anything to connect the control surface to the weighin...

Page 674: ...n and the bottom mounting bracket The center line of the rudder must be horizontal Use any suitable method to support the rudder horizontally at the pivot axis The rudder must be able to rotate freely...

Page 675: ...60 00 Page 3 15 Mar 2022 B Elevator Use any suitable method to support the elevator horizontally at the pivot axis The elevator must be able to rotate freely around the pivot axis The balance includes...

Page 676: ...2022 51 60 00 Doc 4 02 25 Rev 2 C Aileron Use any suitable method to support the aileron horizontally at the pivot axis The aileron must be able to rotate freely around the pivot axis The balance inc...

Page 677: ...Page 5 15 Mar 2022 D Flap Use any suitable method to support the wing flap horizontally at the pivot axis The wing flap must be able to rotate freely around the pivot axis The balance includes the ho...

Page 678: ...AIRCRAFT Standard Practices and Structures DV 20 E AMM Page 6 15 Mar 2022 51 60 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 679: ...AIRCRAFT DV 20 E AMM Doors Doc 4 02 25 Rev 2 52 TITLE Page 1 15 Mar 2022 CHAPTER 52 DOORS...

Page 680: ...AIRCRAFT Doors DV 20 E AMM Page 2 15 Mar 2022 52 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 681: ...1 General 1 2 Description 1 3 Operation 5 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove Install the Canopy 201 3 Canopy Latch Force Test 202 4 Adjust the Canopy Latch Fo...

Page 682: ...AIRCRAFT Doors DV 20 E AMM Page 2 15 Mar 2022 52 CONTENTS Doc 4 02 25 Rev 1 Intentionally left blank...

Page 683: ...M Doors Doc 4 02 25 Rev 2 52 00 00 Page 1 15 Mar 2022 CHAPTER 52 DOORS 1 General The DV 20 E airplane has two types of doors The canopy which gives access to the cockpit Access panels which give acces...

Page 684: ...AIRCRAFT Doors DV 20 E AMM Page 2 15 Mar 2022 52 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 685: ...opy has a warning light system The red warning light comes on when the canopy is not correctly locked The warning light is on the instrument panel 2 Description A Canopy Structure Figure 1 shows the c...

Page 686: ...AIRCRAFT Doors DV 20 E AMM Page 2 15 Mar 2022 52 10 00 Doc 4 02 25 Rev 2 Figure 1 Canopy...

Page 687: ...ball bearing that turns on a stainless steel shaft makes the strike bearing The strike bearing attaches to an aluminum block The aluminum block attaches to the underside of the fuselage at the canopy...

Page 688: ...AIRCRAFT Doors DV 20 E AMM Page 4 15 Mar 2022 52 10 00 Doc 4 02 25 Rev 2 Figure 2 Canopy Latch Installation...

Page 689: ...A Canopy Closed These actions lock the canopy closed Move the canopy fully down Move both grips to the CLOSED position Both internal grips fully forward The hook goes to the rear It fully engages the...

Page 690: ...AIRCRAFT Doors DV 20 E AMM Page 6 15 Mar 2022 52 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 691: ...ven in the Repair column Trouble Possible Cause Repair Canopy is hard to move Canopy frame damaged Replace the canopy Canopy unlock lock grips hard to move Latch mechanism out of adjustment Adjust the...

Page 692: ...AIRCRAFT Doors DV 20 E AMM Page 102 15 Mar 2022 52 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 693: ...the canopy Hold the canopy 3 Remove the rod end bearings from the stabilizing rods at the canopy frame 4 Lift the canopy clear of the airplane B Install the Canopy Detail Steps Work Items Key Items Re...

Page 694: ...to ON 3 Make sure the canopy warning light goes off S Set the ELECTRIC MASTER switch to OFF 4 Put a strap around the canopy grip at the top Attach the spring scale to the strap S Pull the spring scale...

Page 695: ...sition Do not trap the cable for the canopy lock micro switch 4 Do a latch force test Refer to Paragraph 3 5 Adjust the Canopy Warning Light Micro Switch Detail Steps Work Items Key Items References 1...

Page 696: ...fer to Figure 3 2 Remove the clear and tinted sliding window air scoop as follows S Remove the screw the washer and the nut from the sliding window air scoop hinge S Remove the hinge S Remove the clea...

Page 697: ...ock using two screws Refer to Figure 3 2 Install the sliding window with the guide rails 3 Secure the guide rails with eight nylon screws 4 If the sliding window installed does not include the clear t...

Page 698: ...AIRCRAFT Doors DV 20 E AMM Page 206 15 Mar 2022 52 10 00 Doc 4 02 25 Rev 2 Figure 3 Sliding Window Assembly...

Page 699: ...of access panels The panels give access for maintenance Most panels are GFRP moldings Self tapping screws or camlock quick release fasteners hold the panels Refer to Chapter 71 10 for data about the...

Page 700: ...AIRCRAFT Doors DV 20 E AMM Page 2 15 Mar 2022 52 40 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 701: ...AIRCRAFT DV 20 E AMM Fuselage Doc 4 02 25 Rev 2 53 TITLE Page 1 15 Mar 2022 CHAPTER 53 FUSELAGE...

Page 702: ...AIRCRAFT Fuselage DV 20 E AMM Page 2 15 Mar 2022 53 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 703: ...AIRCRAFT DV 20 E AMM Fuselage Doc 4 02 25 Rev 2 53 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 53 FUSELAGE 1 General 1 Section 53 10 Fuselage Structure 1 General 1 2 Description 1...

Page 704: ...AIRCRAFT Fuselage DV 20 E AMM Page 2 15 Mar 2022 53 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 705: ...half shell also makes the vertical stabilizer The fuselage shells have many layers of glass cloth Some areas have more glass cloth than other areas This gives more strength and stiffness where it is n...

Page 706: ...AIRCRAFT Fuselage DV 20 E AMM Page 2 15 Mar 2022 53 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 707: ...FRP inserts The inserts give strength and stiffness for attaching other components such as brackets for controls Bonding paste thickened resin bonds each component to other components Most components...

Page 708: ...AIRCRAFT Fuselage DV 20 E AMM Page 2 15 Mar 2022 53 10 00 Doc 4 02 25 Rev 2 Figure 1 Fuselage Shells and Front Fuselage Structure...

Page 709: ...landing gear D Floor The floor is a rigid GFRP molding It bonds to the inner bottom skin of the fuselage shell behind the firewall It goes over the T panel The center part of the floor makes the cent...

Page 710: ...AIRCRAFT Fuselage DV 20 E AMM Page 4 15 Mar 2022 53 10 00 Doc 4 02 25 Rev 2 Figure 2 Front Fuselage Structure...

Page 711: ...at back A rigid GFRP insert bonds inside the top of the seat back The insert has strong points for the pilot s safety belts The seat back bonds to the top face of the spar bridge It also bonds to the...

Page 712: ...AIRCRAFT Fuselage DV 20 E AMM Page 6 15 Mar 2022 53 10 00 Doc 4 02 25 Rev 2 Figure 3 Rear Fuselage Structure...

Page 713: ...ilizer It has holes for the elevator control pushrod and the rudder control cables It has a cut out on the right side for a cable conduit P Ring Bulkhead 4 The ring bulkhead 4 is a rigid GFRP molding...

Page 714: ...AIRCRAFT Fuselage DV 20 E AMM Page 8 15 Mar 2022 53 10 00 Doc 4 02 25 Rev 2 Figure 4 Vertical Stabilizer Structure...

Page 715: ...to the fuselage shell It also bonds to the upper and vertical stabilizer lower ribs The spar has mounting points for these components The elevator bellcrank The elevator trim actuator The rudder top b...

Page 716: ...AIRCRAFT Fuselage DV 20 E AMM Page 10 15 Mar 2022 53 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 717: ...AIRCRAFT DV 20 E AMM Stabilizers Doc 4 02 25 Rev 2 55 TITLE Page 1 15 Mar 2022 CHAPTER 55 STABILIZERS...

Page 718: ...AIRCRAFT Stabilizers DV 20 E AMM Page 2 15 Mar 2022 55 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 719: ...neral 1 Section 55 10 Horizontal Stabilizer 1 General 1 2 Description 1 Maintenance Practices 1 General 201 2 Remove Install the Horizontal Stabilizer 201 Section 55 20 Elevator 1 General 1 2 Descript...

Page 720: ...ONTENTS Doc 4 02 25 Rev 2 Maintenance Practices 1 General 201 2 Remove Install the Lower Fin 201 Section 55 40 Rudder 1 General 1 2 Description 1 Maintenance Practices 1 General 201 2 Remove Install t...

Page 721: ...ent bracket Center ribs fore and aft give strength to the center area A trailing edge web holds the hinges for the elevator The elevator has top and bottom shells Each shell has GFRP skins with a rigi...

Page 722: ...AIRCRAFT Stabilizers DV 20 E AMM Page 2 15 Mar 2022 55 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 723: ...achment bolts from below The mount plate goes down through the large cut out in the bottom shell Four more holes in the bottom part of the mount plate attach to the vertical stabilizer top rib Fore an...

Page 724: ...AIRCRAFT Stabilizers DV 20 E AMM Page 2 15 Mar 2022 55 10 00 Doc 4 02 25 Rev 2 Figure 1 Horizontal Stabilizer Structure...

Page 725: ...ll the horizontal stabilizer Detail Steps Work Items Key Items References 1 Remove the horizontal stabilizer fairing S Remove the four screws 2 Remove the bolt that connects the elevator vertical cont...

Page 726: ...l the two bolts that connect the lower mounting bracket to the upper mounting bracket Torque to 6 24 Nm 4 6 lbf ft 4 Install the bolt which connects the elevator vertical control rod to the elevator h...

Page 727: ...r The top edge of the leading edge spar has a flange which goes forward The shells bond together at this flange and at the trailing edge The hinges attach to the bottom shell Each hinge is a small met...

Page 728: ...AIRCRAFT Stabilizers DV 20 E AMM Page 2 15 Mar 2022 55 20 00 Doc 4 02 25 Rev 2 Figure 1 Elevator Structure...

Page 729: ...se 2 persons to remove install the elevator Or use control clamps to hold the elevator in position while you remove install the attaching bolts Detail Steps Work Items Key Items References 1 Remove th...

Page 730: ...side and one center bolt through the control horn Refer to Chapter 20 for standard torque values 3 Install the bolt which connects the elevator vertical control rod to the elevator horn Make sure tha...

Page 731: ...ps give directional stability It makes a tail bumper It also has a tie down point 2 Description Figure 1 shows the lower fin The lower fin is a rigid GFRP molding Five screws attach the lower fin to t...

Page 732: ...AIRCRAFT Stabilizers DV 20 E AMM Page 2 15 Mar 2022 55 30 00 Doc 4 02 25 Rev 2 Figure 1 Lower Fin...

Page 733: ...alls and epoxy Refer to Chapter 51 2 Remove Install the Lower Fin A Remove the Lower Fin Detail Steps Work Items Key Items References 1 Remove the adhesive tape that seals the joint between the lower...

Page 734: ...AIRCRAFT Stabilizers DV 20 E AMM Page 202 15 Mar 2022 55 30 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 735: ...e The shells bond together all around with bonding paste The rudder has two pivots The top pivot pin bonds to the top face of the shells near the leading edge The top pivot has a bushing This bushing...

Page 736: ...AIRCRAFT Stabilizers DV 20 E AMM Page 2 15 Mar 2022 55 40 00 Doc 4 02 25 Rev 2 Figure 1 Rudder Assembly...

Page 737: ...old the rudder in position while you remove install the attaching bolts Detail Steps Work Items Key Items References 1 Remove the two nuts and the washers that attach the rudder to the lower mounting...

Page 738: ...AIRCRAFT Stabilizers DV 20 E AMM Page 202 15 Mar 2022 55 40 00 Doc 4 02 25 Rev 2 Figure 2 Rudder Installation...

Page 739: ...a test for correct full and free movement of the rudder control If necessary adjust the rudder control Refer to Chapter 27 30 3 Remove Install the Top Pivot Bushing A Remove the Top Pivot Bushing Det...

Page 740: ...p Pivot Bushing Detail Steps Work Items Key Items References 1 Clean the surface of the pivot pin 2 Apply 680 Loctite to the pivot pin 3 Install the pivot bushing over the pivot pin 4 Clean all 680 Lo...

Page 741: ...AIRCRAFT DV 20 E AMM Windows Doc 4 02 25 Rev 2 56 TITLE Page 1 15 Mar 2022 CHAPTER 56 WINDOWS...

Page 742: ...AIRCRAFT Windows DV 20 E AMM Page 2 15 Mar 2022 56 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 743: ...3 Removal and Installation 1 Section 56 10 Repair of the Canopy Glass 1 Damage Limits 1 2 Tools and Equipment 1 3 Materials 1 4 Fillers 1 5 Temporary Repair to the Canopy Glass 2 6 Permanent Repair t...

Page 744: ...AIRCRAFT Windows DV 20 E AMM Page 2 15 Mar 2022 56 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 745: ...d one large acrylic glass bubble The canopy glass has two small emergency windows The canopy has a hinge at the back and a stabilizing rod on each side The support arms have counterbalance springs to...

Page 746: ...AIRCRAFT Windows DV 20 E AMM Page 2 15 Mar 2022 56 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 747: ...ed grinder Drill UV light cold 3 Materials The following materials are required for the repair of the cockpit glass Item Quantity Part Number Filler ACRYFIX 192 A R Commercial Masking Tape A R Commerc...

Page 748: ...Detail Steps Work Items Key Items References 1 If necessary remove the canopy for the repair Put the canopy on a firm working surface with the crack horizontal Refer to Chapter 52 10 2 If the canopy...

Page 749: ...to Step 3 of Figure 3 9 On the inner surface countersink the filler of the temporary stop drill holes to a depth of approx 1 mm 0 04 in Refer to Step 3 of Figure 4 10 Apply filler to the groove and s...

Page 750: ...Windows DV 20 E AMM Page 4 15 Mar 2022 56 10 00 Doc 4 02 25 Rev 2 Dimensions x 50 mm 2 in y 100 mm 4 in No cracks are permitted in the shaded area The maximum crack length is 150 mm 6 in Figure 2 Crac...

Page 751: ...AIRCRAFT DV 20 E AMM Windows Doc 4 02 25 Rev 2 56 10 00 Page 5 15 Mar 2022 Figure 3 Crack Repairs...

Page 752: ...AIRCRAFT Windows DV 20 E AMM Page 6 15 Mar 2022 56 10 00 Doc 4 02 25 Rev 2 Figure 4 Store Drill Hole Repair...

Page 753: ...ndustries 2 Tools and Equipment The following tools and equipment are required for the replacement of the rear window High speed grinder Blade Drill Jigsaw Chisel 3 Materials The following materials a...

Page 754: ...and away any remaining adhesive from the bonding flange on the fuselage Use extreme care not to damage the surrounding composite or the bonding flange CAUTION KEEP BONDING SURFACES CLEAN FROM OIL DIRT...

Page 755: ...s bead Make sure that the bead cover most of the bonding flange 16 Install the window on the fuselage immediately Pot lifetime for adhesive Terostat MS 9380 is 10 minutes 17 Move the window to align t...

Page 756: ...t Remove the excess black sealant with plastic scraper or spatula 26 Allow the caulk to cure overnight 27 Remove masking or flash tape 28 Mask off fuselage and window in preparation for paint applicat...

Page 757: ...AIRCRAFT DV 20 E AMM Wings Doc 4 02 25 Rev 2 57 TITLE Page 1 15 Mar 2022 CHAPTER 57 WINGS...

Page 758: ...AIRCRAFT Wings DV 20 E AMM Page 2 15 Mar 2022 57 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 759: ...tructure 1 General 1 2 Description 1 Maintenance Practices 1 General 201 2 Remove Install the Wings 201 3 Install a Wing Spar Bushing to a New Replacement Wing 208 4 Bolt Play 209 Section 57 50 Flaps...

Page 760: ...AIRCRAFT Wings DV 20 E AMM Page 2 15 Mar 2022 57 CONTENTS Doc 4 02 25 Rev 2 Maintenance Practices 1 General 201 2 Remove Install the Aileron 201...

Page 761: ...iling edge There is an aileron on the outboard trailing edge The wings are monocoque structure Each wing has top and bottom shells The shells have GFRP skins and a rigid foam core Each wing has an I s...

Page 762: ...AIRCRAFT Wings DV 20 E AMM Page 2 15 Mar 2022 57 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 763: ...to each other The wing has the following main parts A Wing Shells Each wing has top and bottom shells Each shell has GFRP skins with a rigid foam core The skins have many layers of glass cloth Some ar...

Page 764: ...AIRCRAFT Wings DV 20 E AMM Page 2 15 Mar 2022 57 10 00 Doc 4 02 25 Rev 2 Figure 1 Wing Structure Shells Spar Root Rib and Webs...

Page 765: ...AIRCRAFT DV 20 E AMM Wings Doc 4 02 25 Rev 2 57 10 00 Page 3 15 Mar 2022 Figure 2 Wing Structure Ribs...

Page 766: ...h parts of the root rib to the spar The forward root rib has a bearing housing for the A bolt The A bolt is a small distance in front of the spar The A bolt transmits lift loads into the fuselage stru...

Page 767: ...ng It has a guide bearing for the aileron control rod It bonds to the aft face of the spar the top and bottom shells and the aft inner web I Aileron Control Rib The aileron control rib is located half...

Page 768: ...AIRCRAFT Wings DV 20 E AMM Page 6 15 Mar 2022 57 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 769: ...ntenance practices describe how to Remove and install the wings The procedure is simple You need no special tools Remove Install the wing using 3 persons Install a wing spar bushing to a new replaceme...

Page 770: ...AIRCRAFT Wings DV 20 E AMM Page 202 15 Mar 2022 57 10 00 Doc 4 02 25 Rev 2 Figure 3 Wing Attachment Bolts...

Page 771: ...AIRCRAFT DV 20 E AMM Wings Doc 4 02 25 Rev 2 57 10 00 Page 203 15 Mar 2022 Figure 4 Wing Connections...

Page 772: ...he trestles under the wings To touch the wing under the spar 5 Remove the nut and spacer from the B bolt 6 Release the locking device for the main bolts Pull it up against the spring Then turn it 180...

Page 773: ...the static hose forward of the spar Left wing only The hose is 8 mm 5 16 in diameter Purple Color CAUTION DO NOT LIFT ON THE FLAP ONLY LIFT ON THE WING STRUCTURE OTHERWISE YOU MAY DAMAGE THE FLAP 15 M...

Page 774: ...e wing with a trestle To touch the wing under the spar 4 Connect the static hose forward of the spar Left wing only The hose is 8 mm 5 16 in diameter Purple Color 5 Connect the Pitot hose forward of t...

Page 775: ...dard torque values 17 Connect the aileron control rods at the bellcrank on the bulkhead aft control Refer to Chapter 27 10 Through the panels below the fuselage Refer to Chapter 20 for standard torque...

Page 776: ...on composite surfaces Wipe dry Do not touch clean bonding surfaces with bare hands 6 Mix resin Refer to Chapter 51 00 7 Prepare thickened resin paste 8 Wet surfaces to be bonded with a thin coat of mi...

Page 777: ...nd for safety 20 Re install the wing Refer to paragraph 2 C 4 Bolt Play A Radial Play The wing connection bolt values given in the table below must not be exceeded A bolt in spherical bearing 0 08 mm...

Page 778: ...AIRCRAFT Wings DV 20 E AMM Page 210 15 Mar 2022 57 10 00 Doc 4 02 25 Rev 2 Figure 5 Installation of Spar Bushing to a New Replacement Wing Sweep and Dihedral Tolerances...

Page 779: ...outer GFRP skins The skins bond to a rigid plastic foam core Carbon cloth gives extra strength and stiffness in the outer skin B Bottom Shell The bottom shell has inner and outer GFRP skins The skins...

Page 780: ...AIRCRAFT Wings DV 20 E AMM Page 2 15 Mar 2022 57 50 00 Doc 4 02 25 Rev 2 Figure 1 Flap Structure...

Page 781: ...Detail Steps Work Items Key Items References CAUTION MAKE SURE THAT THE AREA UNDER THE FLAPS IS CLEAR BEFORE YOU MOVE THE FLAPS 1 Lower the flaps S Set the ELECTRIC MASTER switch to ON S Set the flap...

Page 782: ...AIRCRAFT Wings DV 20 E AMM Page 202 15 Mar 2022 57 50 00 Doc 4 02 25 Rev 2 Figure 2 Flap Connections...

Page 783: ...hat there is a gap of 3 5 mm 0 12 0 20 in between the flap and the aileron 3 Install the bolt which attaches the control rod to the flap horn 4 Install the bushing Ream the bushing to 9 525 0 010 and...

Page 784: ...AIRCRAFT Wings DV 20 E AMM Page 204 15 Mar 2022 57 50 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 785: ...the outer skin B Bottom Shell The bottom shell has inner and outer GFRP skins The skins bond to a rigid plastic foam core Carbon cloth gives extra strength and stiffness in the outer skin C End Ribs T...

Page 786: ...AIRCRAFT Wings DV 20 E AMM Page 2 15 Mar 2022 57 60 00 Doc 4 02 25 Rev 2 Figure 1 Aileron Structure...

Page 787: ...ems References 1 Put the aileron in position on the airplane Hold the aileron 2 Install the pivot bolts in the hinges and the aileron horn Hold the aileron Make sure that there is a gap of 3 5 mm 0 12...

Page 788: ...AIRCRAFT Wings DV 20 E AMM Page 202 15 Mar 2022 57 60 00 Doc 4 02 25 Rev 2 Figure 2 Aileron Installation...

Page 789: ...AIRCRAFT DV 20 E AMM Propeller Doc 4 02 25 Rev 2 61 TITLE Page 1 15 Mar 2022 CHAPTER 61 PROPELLER...

Page 790: ...AIRCRAFT Propeller DV 20 E AMM Page 2 15 Mar 2022 61 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 791: ...25 Rev 2 61 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 61 PROPELLER 1 General 1 Section 61 10 Propeller Assembly 1 General 1 2 Propeller Control 1 Trouble Shooting 1 General 101 Maintenanc...

Page 792: ...AIRCRAFT Propeller DV 20 E AMM Page 2 15 Mar 2022 61 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 793: ...e Equipment which is certified for installation in the DV 20 E is listed in Section 6 5 of the Airplane Flight Manual Such equipment may be installed in accordance with the Airplane Maintenance Manual...

Page 794: ...AIRCRAFT Propeller DV 20 E AMM Page 2 15 Mar 2022 61 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 795: ...minimizing vibration Low Pitch 14 5 0 2 High Pitch 30 1 2 Propeller Control The propeller pitch control system consists of the mt propeller P 850 12 governor The pitch is set by the pilot via the prop...

Page 796: ...AIRCRAFT Propeller DV 20 E AMM Page 2 15 Mar 2022 61 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 797: ...peller manufacturer to inspect blade retention system Engine vibration Propeller out of balance Spinner out of balance Propeller mounting loose Spinner attaching screws loose Blade tracking not correc...

Page 798: ...00 RPM with a drop of about 1000 RPM Contact repair station to clean oil lines in engine cylinder propeller and governor Check governor designation 5 periods of surging with low amplitude are acceptab...

Page 799: ...nor speeder spring or plunger stuck in governor Defective propeller speed control bowden cable Dirt in fuel system Contact repair station to replace governor Repair or replace Clean Pitch change extre...

Page 800: ...AIRCRAFT Propeller DV 20 E AMM Trouble Possible Cause Repair Page 104 15 Mar 2022 61 10 00 Doc 4 02 25 Rev 2 Oil leakage may either be visible from outside or not Defective seals Replace...

Page 801: ...lean 2 Check O rings NOTE Do not install additional O Rings Check position of O Ring installed in propeller flange 3 Install spinner backplate Install propeller considering position relative to spinne...

Page 802: ...AIRCRAFT Propeller DV 20 E AMM Page 202 15 Mar 2022 61 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 803: ...AIRCRAFT DV 20 E AMM Power Plant Doc 4 02 25 Rev 2 71 TITLE Page 1 15 Mar 2022 CHAPTER 71 POWER PLANT...

Page 804: ...AIRCRAFT Power Plant DV 20 E AMM Page 2 15 Mar 2022 71 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 805: ...ouble Shooting 1 General 101 Maintenance Practices 1 Remove Install the Engine 201 Section 71 10 Cowling 1 General 1 Maintenance Practices 1 Remove Install the Cowlings 201 Section 71 20 Engine Mount...

Page 806: ...AIRCRAFT Power Plant DV 20 E AMM Page 2 15 Mar 2022 71 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 807: ...20 E Airplane Flight Manual for engine start stop procedures Refer to these Chapters for data about other engine systems Chapter 76 Engine controls Chapter 77 Engine indicating Chapter 78 Exhaust syst...

Page 808: ...erator 1 when the engine is running For engine start the ECU receives its electrical power from the battery The engine has a redundancy concept for generator failure After failure of Generator 1 the E...

Page 809: ...S CAN CAUSE INJURY TO PERSONNEL If you have the trouble detailed in the Trouble column read across to the Possible Cause column Then do the repair given in the Repair column Trouble Possible Cause Rep...

Page 810: ...ne overhaul might be required Engine idles unsteadily after warm up black exhaust gas Intake manifold leaky Tighten all connectors replace defective parts Engine runs irregularly or misfires occasiona...

Page 811: ...r gas mixture leakage Check for free air passage clean Check oil level replenish if necessary Change oil use approved oil Replace Usual reason worn or seized piston rings overhaul required If there ar...

Page 812: ...il pressure indicator Defective crankshaft bearings Check oil level replenish if required Check oil return line for clogging Replace See engine runs too hot Check for foreign matter check spring Bleed...

Page 813: ...ve cylinder heads remove combustion residue check oil consumption Engine hard to start at low temperatures Starting RPM too low Low battery change High oil pressure Too low oil pressure after cold sta...

Page 814: ...AIRCRAFT Power Plant DV 20 E AMM Page 106 15 Mar 2022 71 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 815: ...IF THE ENGINE IS TURNED THE PROPELLER CAN CAUSE INJURY OR DEATH 2 Remove upper and lower cowling 3 Disconnect nose wheel elastomer package assembly from engine mount 4 Disconnect ignition wires 5 Rem...

Page 816: ...AIRCRAFT Power Plant DV 20 E AMM Page 202 15 Mar 2022 71 00 00 Doc 4 02 25 Rev 2 B Install Engine For installation of the engine reverse the engine removal sequence...

Page 817: ...cowling consists of two halves with two inspection covers located on the upper half allowing access to the oil dipstick and the coolant equalizing reservoir The covers are attached to the cowling by...

Page 818: ...AIRCRAFT Power Plant DV 20 E AMM Page 2 15 Mar 2022 71 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 819: ...E THAT THE ENGINE IS SAFE BEFORE YOU DO ANY WORK ON THE PROPELLER IF THE ENGINE IS TURNED THE PROPELLER CAN CAUSE INJURY OR DEATH 1 Loosen fasteners on upper engine cowling 2 Remove upper cowling 3 Lo...

Page 820: ...AIRCRAFT Power Plant DV 20 E AMM Page 202 15 Mar 2022 71 10 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 821: ...shock mounts are located between the engine and the engine ring mount to reduce the vibration transmission from the engine to the airframe 2 Description The engine mount is electrically grounded to t...

Page 822: ...AIRCRAFT Power Plant DV 20 E AMM Page 2 15 Mar 2022 71 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 823: ...unt Detail Steps Work Items Key Items References 1 Remove bolts holding the engine mount 2 Remove engine mount from firewall B Install the Engine Mount For installation of the engine mount reverse the...

Page 824: ...AIRCRAFT Power Plant DV 20 E AMM Page 202 15 Mar 2022 71 20 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 825: ...m air guide made of GFRP is installed on the engine to ensure optimal engine cooling 2 Description The air guide is designed to follow the contours of the engine block and cylinders The exact fitting...

Page 826: ...AIRCRAFT Power Plant DV 20 E AMM Page 2 15 Mar 2022 71 60 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 827: ...AIRCRAFT DV 20 E AMM Liquid Cooling System Doc 4 02 25 Rev 2 75 TITLE Page 1 15 Mar 2022 CHAPTER 75 LIQUID COOLING SYSTEM...

Page 828: ...AIRCRAFT Liquid Cooling System DV 20 E AMM Page 2 15 Mar 2022 75 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 829: ...2 75 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 75 LIQUID COOLING SYSTEM 1 General 1 Maintenance Practices 1 General 201 2 Remove and Install the Coolant Tank 201 3 Remove and Install the...

Page 830: ...AIRCRAFT Liquid Cooling System DV 20 E AMM Page 2 15 Mar 2022 75 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 831: ...on top of the engine and an equalizing reservoir overflow bottle An inspection hole in the right hand side of the upper cowling provides access to the overflow bottle A dipstick is used for checking i...

Page 832: ...AIRCRAFT Liquid Cooling System DV 20 E AMM Page 2 15 Mar 2022 75 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 833: ...se the sequence 3 Remove and Install the Radiator Detail Steps Work Items Key Items References NOTE Disconnecting the hoses to the radiator will cause coolant to leak out An appropriate container shou...

Page 834: ...AIRCRAFT Liquid Cooling System DV 20 E AMM Page 202 15 Mar 2022 75 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 835: ...AIRCRAFT DV 20 E AMM Engine Controls Doc 4 02 25 Rev 2 76 TITLE Page 1 15 Mar 2022 CHAPTER 76 ENGINE CONTROLS...

Page 836: ...AIRCRAFT Engine Controls DV 20 E AMM Page 2 15 Mar 2022 76 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 837: ...ral 101 Maintenance Practices 1 Remove and Install an Throttle Control Bowden Cable 201 2 Adjustment of Throttle Control Bowden Cable 202 3 Remove and Install an Alternate Air Bowden Cable 202 4 Adjus...

Page 838: ...AIRCRAFT Engine Controls DV 20 E AMM Page 2 15 Mar 2022 76 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 839: ...e valve is controlled by the throttle lever which is located in the center console The bowden cable is attached to the throttle lever by a clamp The bowden cables are attached on the other end to the...

Page 840: ...switch over to the other lane G Alternate Air lever In the event of power loss because of icing or blocking of the air filter there is the possibility of drawing air from the engine compartment The A...

Page 841: ...Crankshaft RPM twice Manifold pressure twice Manifold air temperature twice Ambient air pressure Ambient air temperature ECU voltage In accordance with the received signals and a comparison with the...

Page 842: ...AIRCRAFT Engine Controls DV 20 E AMM Page 4 15 Mar 2022 76 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 843: ...do the repair given in the Repair column For all other engine control trouble refer to the engine manufacturer Trouble Possible Cause Repair Engine is not controllable Broken bowden cable Loose bowde...

Page 844: ...AIRCRAFT Engine Controls DV 20 E AMM Page 102 15 Mar 2022 76 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 845: ...Items References 1 Remove engine cowlings 2 Remove throttle quadrant 3 Disconnect bowden cable clamps on the throttle valve 4 Disconnect bowden cable clamps on shift lever below instrument panel 5 Di...

Page 846: ...s Key Items References 1 Remove engine cowlings 2 Remove throttle quadrant cover 3 Disconnect bowden cable from flap actuating lever on alternate air valve 4 Disconnect bowden cable from alternate air...

Page 847: ...ble from propeller governor 3 Remove the throttle quadrant cover 4 Disconnect bowden cable from propeller speed control lever 5 Remove bowden cables by pulling rearward For Installation reverse the se...

Page 848: ...25 Rev 2 7 Remove and Install the Throttle Quadrant Friction Control Detail Steps Work Items Key Items References 1 Remove rotary knob on RH side of center console 2 Remove washer springs and replace...

Page 849: ...AIRCRAFT DV 20 E AMM Engine Indicating Doc 4 02 25 Rev 2 77 TITLE Page 1 15 Mar 2022 CHAPTER 77 ENGINE INDICATING...

Page 850: ...AIRCRAFT Engine Indicating DV 20 E AMM Page 2 15 Mar 2022 77 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 851: ...AIRCRAFT DV 20 E AMM Engine Indicating Doc 4 02 25 Rev 2 77 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 77 ENGINE INDICATING 1 General 1 2 Engine Instruments 1...

Page 852: ...AIRCRAFT Engine Indicating DV 20 E AMM Page 2 15 Mar 2022 77 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 853: ...s During that time is the ECU already functional After successful completion of the internal test procedure the lights are extinguished In case of an fault detected by ECU internal mechanisms the LANE...

Page 854: ...ncluding color coded bars and drag indicators The drag indicators are reset by pressing the ZERO button The brightness of the display can be adjusted by rotating the MCR button A SDHC Card slot is ava...

Page 855: ...nHG OIL Oil pressure bar Oil temperature C EGT Exhaust gas temperature C CT Coolant temperature C FUEL Fuel pressure bar Fuel consumption rate l h ECV ECU voltage V MAT Manifold air temperature C MODE...

Page 856: ...AIRCRAFT Engine Indicating DV 20 E AMM Page 4 15 Mar 2022 77 00 00 Doc 4 02 25 Rev 2 Figure 2 EMU Display INFO Page RET Return to main page 88 Page down 99 Page Up ZERO Reset drag indicators...

Page 857: ...AIRCRAFT DV 20 E AMM Exhaust Doc 4 02 25 Rev 2 78 TITLE Page 1 15 Mar 2022 CHAPTER 78 EXHAUST...

Page 858: ...AIRCRAFT Exhaust DV 20 E AMM Page 2 15 Mar 2022 78 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 859: ...age 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 78 EXHAUST 1 General 1 2 Description 1 Trouble Shooting 1 General 101 Maintenance Practices 1 General 201 2 Remove Install the Exhaust System 201 3 Inspecti...

Page 860: ...AIRCRAFT Exhaust DV 20 E AMM Page 2 15 Mar 2022 78 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 861: ...o springs each The end pipe runs to the exterior of the airplane through the lower engine cowling on the left hand side A jacket around the muffler serves as a heat exchanger for cabin heat Figure 1 E...

Page 862: ...AIRCRAFT Exhaust DV 20 E AMM Page 2 15 Mar 2022 78 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 863: ...read across to the Possible Cause column Then do the repair given in the Repair column Trouble Possible Cause Repair Excessive engine noise Defective muffler or exhaust pipe Replace Cracks in muffler...

Page 864: ...AIRCRAFT Exhaust DV 20 E AMM Page 102 15 Mar 2022 78 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 865: ...Items Key Items References WARNING DO NOT STAND WITHIN THE DANGER AREA OF THE PROPELLER IF THE ENGINE STARTS THE PROPELLER CAN CAUSE DEATH OR INJURY TO PERSONS WARNING YOU MUST MAKE SURE THAT THE ENGI...

Page 866: ...is suspicion of leakage the cabin should be checked for contamination using a gas detector apparatus The maximum permissible level of carbon monoxide contamination is 50 PPM parts per million In the e...

Page 867: ...AIRCRAFT DV 20 E AMM Oil Cooling Doc 4 02 25 Rev 2 79 TITLE Page 1 15 Mar 2022 CHAPTER 79 OIL COOLING...

Page 868: ...AIRCRAFT Oil Cooling DV 20 E AMM Page 2 15 Mar 2022 79 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 869: ...25 Rev 2 79 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 79 OIL COOLING 1 General 1 2 Description 1 SECTION 79 21 OIL RADIATOR 1 General 1 Trouble Shooting 1 General 101 Maintenance Practices...

Page 870: ...AIRCRAFT Oil Cooling DV 20 E AMM Page 2 15 Mar 2022 79 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 871: ...regulator 2 Description The Rotax 912 iSc3 Sport has a dry sump lubrication system The camshaft driven oil pump has an integrated oil pressure regulator and oil pressure sensor The oil pump transport...

Page 872: ...AIRCRAFT Oil Cooling DV 20 E AMM Page 2 15 Mar 2022 79 00 00 Doc 4 02 25 Rev 2 1 Pressure regulator 4 Oil cooler 2 Oil pump 5 Oil filter 3 Oil tank 6 Venting tube Figure 1 Oil System...

Page 873: ...cated on the lower right hand side of the engine and is attached to the engine mount The oil radiator has two threaded connection sleeves to which the oil lines are attached The sleeves are also used...

Page 874: ...AIRCRAFT Oil Cooling DV 20 E AMM Page 2 15 Mar 2022 79 21 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 875: ...If you have the trouble detailed in the Trouble column read across to the Possible Cause column Then do the repair given in the Repair column Trouble Possible Cause Repair Excessive oil temperature Da...

Page 876: ...AIRCRAFT Oil Cooling DV 20 E AMM Page 102 15 Mar 2022 79 21 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 877: ...References 1 Disconnect hose lines from radiator ports 2 Straighten locking plates on hose connectors 3 Remove mounting nuts 4 Remove oil radiator Figure 2 Oil Radiator For Installation reverse the s...

Page 878: ...AIRCRAFT Oil Cooling DV 20 E AMM Page 202 15 Mar 2022 79 21 00 Doc 4 02 25 Rev 2 Intentionally left blank...

Page 879: ...AIRCRAFT DV 20 E AMM Wiring Diagrams Doc 4 02 25 Rev 2 92 TITLE Page 1 15 Mar 2022 CHAPTER 92 WIRING DIAGRAMS...

Page 880: ...AIRCRAFT Wiring Diagrams DV 20 E AMM Page 2 15 Mar 2022 92 TITLE Doc 4 02 25 Rev 2 Intentionally left blank...

Page 881: ...AIRCRAFT DV 20 E AMM Wiring Diagrams Doc 4 02 25 Rev 2 92 CONTENTS Page 1 15 Mar 2022 TABLE OF CONTENTS CHAPTER 92 WIRING DIAGRAMS 1 General 1...

Page 882: ...AIRCRAFT Wiring Diagrams DV 20 E AMM Page 2 15 Mar 2022 92 CONTENTS Doc 4 02 25 Rev 2 Intentionally left blank...

Page 883: ...1 Schematic External Power Connector Wiring D21 9224 40 01 1 Schematic Accessory Power Plug D21 9224 60 01 1 Schematic USB Charging Ports D21 9224 60 02 1 Schematic Flaps Wiring D21 9227 50 00 1 Schem...

Page 884: ...AIRCRAFT Wiring Diagrams DV 20 E AMM Page 2 15 Mar 2022 92 00 00 Doc 4 02 25 Rev 2 Intentionally left blank...

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Page 888: ...A 1 2 3 4 5 6 7 8 Confidential PROJECT TITLE DWG ORIG CODE SCALE SH OF DWG NO REV NAME SIGN DATE DRAWN CHECKED RELEASE D IDENTIFICATION MARKINGS CLASSIFICATION INTERCHANGEABLE PART THIS DRAWING WAS P...

Page 889: ...USTRIES Confidential F E D C B A 1 2 3 4 5 6 7 8 Confidential PROJECT TITLE DWG ORIG CODE SCALE SH OF DWG NO REV NAME SIGN DATE DRAWN CHECKED RELEASE D IDENTIFICATION MARKINGS CLASSIFICATION INTERCHAN...

Page 890: ...USTRIES Confidential F E D C B A 1 2 3 4 5 6 7 8 Confidential PROJECT TITLE DWG ORIG CODE SCALE SH OF DWG NO REV NAME SIGN DATE DRAWN CHECKED RELEASE D IDENTIFICATION MARKINGS CLASSIFICATION INTERCHAN...

Page 891: ...0 02 27303B24WH P2400 02 11 3 TRIM ACTUATOR BL FLAP TRIM GS IP 12 GS IP 02 1 5 6 27312A22 27310A22 J2400 01 22 P2400 01 16 27303B24BL 27303B24WH 27303B24BL WH 5 J2730 01 27301A18BL 27301A18WH 18 27306...

Page 892: ...CALE SH OF DWG NO REV NAME SIGN DATE DRAWN CHECKED RELEASE D IDENTIFICATION MARKINGS CLASSIFICATION INTERCHANGEABLE PART THIS DRAWING WAS PRODUCED USING SOFTWARE FILENAME DIMENSIONS FIRST ANGLE PROJEC...

Page 893: ...SIFICATION INTERCHANGEABLE PART THIS DRAWING WAS PRODUCED USING SOFTWARE FILENAME DIMENSIONS FIRST ANGLE PROJECTION FORMAT FINISH IN MICRO METER IF NOT OTHERWISE SPECIFIED GEOMETRIC DIMENSIONING AND T...

Page 894: ...ential F E D C B A 1 2 3 4 5 6 7 8 Confidential PROJECT TITLE DWG ORIG CODE SCALE SH OF DWG NO REV NAME SIGN DATE DRAWN CHECKED RELEASE D IDENTIFICATION MARKINGS CLASSIFICATION INTERCHANGEABLE PART TH...

Page 895: ...IED GEOMETRIC DIMENSI O NING AND TOLERANCING ACC TO DIMENSI O NS IN ISO 2768 mK mm NTS REV ZONE SH DESCRIPTION DATE REVISION V M 20 002 NEW DRAWI N G DOES NOT SUPER SEDE ANOTHER DRAWING ALL 01 20 10 1...

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Page 901: ...SO 2768 mK mm NTS REV ZONE SH DESCRIPTION DATE REVISION V M 20 002 NEW DRAWI N G DOES NOT SUPER SEDE ANOTHER DRAWING ALL 01 15 09 15 33734A22 3K 33737A22N V IN V OUT V ADJ 2 3 4 5 6 33711A22 33713A22...

Page 902: ...16 09 2015 PITOT STATIC PORT R H WING 33404A18OR 33404A18WH 33404A18BL 33405C18 CONDUIT AILERON BELLCRANK 33418A16BL J3340 02 33416B14N 33402A18OR 33402A18BL 33402A18WH 33416C14N 5 7 P3340 02 10 9 8...

Page 903: ...ential F E D C B A 1 2 3 4 5 6 7 8 Confidential PROJECT TITLE DWG ORIG CODE SCALE SH OF DWG NO REV NAME SIGN DATE DRAWN CHECKED RELEASE D IDENTIFICATION MARKINGS CLASSIFICATION INTERCHANGEABLE PART TH...

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