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Section 913

GARMIN GTX 327 Transponder

Page Date: 19. February 2014

913 - 3

Pilot´s Operating Handbook US
EXTRA 330LX

913.1

GENERAL

The GARMIN GTX 327 is a panel-mounted TSO.d transponder with the addition of timing functions.
The transponder is a radio transmitter and receiver that operates on radar frequencies, receiving
ground radar interrogations at 1030 MHz and transmitting a coded response of pulses to ground-
based radar on a frequency of 1090 MHz.

N O T E

The GTX 327 owner accepts all responsibility for obtaining the proper license before using
the transponder.

The coverage you can expect from the GTX 327 is limited to „line of sight“. Low altitude or aircraft
antenna shielding by the aircraft itself may result in reduced range. Range can be improved by
climbing to a higher altitude. It may be possible to minimize antenna shielding by locating the
antenna where dead spots are only noticed during abnormal flight attitudes.

CAUTION

The GTX 327 should be turned off before starting or shutting down aircraft engine.

The GTX 327 Transponder is powered on by pressing the

STBY

,

ALT

or

ON

keys, or by the

AVIONIC

switch. After power on a start-up page will be displayed while the unit performs a self test.

913.1.1

MODE SELECTION KEYS

OFF

Powers off the GTX 327.

STBY

Powers on the transponder in standby mode. At power on the last active identification code will be
selected. When in standby mode, the transponder will not reply to any interrogations.

ON

Powers on the transponder in Mode A. At power on the last active identification code will be
selected. In this mode the transponder replies to interrogations, as indicated by the Reply Symbol.
Replies do not include altitude information.

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Summary of Contents for 330lx

Page 1: ...deral Republic of Germany TITLE PAGE W A R N I N G This is an Information Manual and may be used for general purposes only This Information Manual is not kept current It must not be used as a substitute for the official FAA approved Airplane Flight Manual AFM Pilot s Operating Handbook POH required for operation of an U S registered airplane ...

Page 2: ...Left blank intentionally ...

Page 3: ...i Pilot s Operating Handbook US EXTRA330LX LOG OF REVISIONS Dates of issue for original and revised pages Original 19 February2014 Date and sign of approval ApprovedbyCSVProjectN 0010009466 DateofApproval 07 March 2014 SECTION 0 ...

Page 4: ...ii Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Page Date All 19 February2014 LOGOFEFFECTIVEPAGES Page Date ...

Page 5: ...Page Date 19 February 2014 iii Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 6: ...ght Manual includ ing revisions and any relevant supplements Pages of this Airplane Flight Manual must not be exchanged and no alterations of or additions to the approved contents may be made without the EXTRA Flugzeugproduktions undVertriebs GmbH FAAapproval The editor has the copyright of this Flight Manual and is responsible for edition of revisions amendmentsandsupplements Amendments which aff...

Page 7: ...y or loss of life if not carefully followed CAUTION Operating procedures techniques etc which could result in damage to equipment if not carefully followed N O T E An operating procedures technique etc which is considered essential to emphasize Shall Will Should and May The words Shall or will is used to express a mandatory requirement The word should is used to express nonmandatory provisions The...

Page 8: ...30LX MAINTABLEOFCONTENTS Section Page 1 GENERAL 1 1 2 LIMITATIONS 2 1 3 EMERGENCYPROCEDURES 3 1 4 NORMALPROCEDURES 4 1 5 PERFORMANCE 5 1 6 WEIGHT BALANCE EQUIPMENTLIST 6 1 7 AIRPLANE SYSTEMSDESCRIPTIONS 7 1 8 AIRPLANEHANDLING SERVICE MAINTENANCE 8 1 9 SUPPLEMENTS 9 1 ...

Page 9: ...N OF CLASS 1 3 1 2 MANUFACTURER 1 3 1 3 TECHNICALDATA 1 3 1 3 1 3 View Drawing 1 3 1 3 2 Main Data 1 4 1 3 3 Wing 1 4 1 3 4 Horizontal Tail 1 4 1 3 5 Elevator 1 4 1 3 6 Vertical Tail 1 4 1 3 7 Rudder 1 4 1 4 ENGINE 1 5 1 5 PROPELLER 1 5 1 5 1 Exhaust System 1 5 1 6 FUEL 1 5 1 7 OIL 1 5 1 8 LOADING 1 6 1 9 TERMINOLOGY 1 6 1 10 SECONDARYTERMINOLOGY 1 7 1 11 CONVERSION TABLE 1 7 ...

Page 10: ...1 2 Page Date 19 February 2014 Section 1 General Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 11: ...s empennageandlandinggeararemanufacturedfromcompositematerial Theaircraftisatwo seaterwiththerearcockpitequippedwithacompletesetofairplanecontrols and instruments 1 1 SPECIFICATIONOFCLASS The aircraft is certified in the acrobatic category 1 2 MANUFACTURER EXTRAFlugzeugproduktions undVertriebs GmbH FlugplatzDinslaken 46569Hünxe FederalRepublicofGermany 1 3 TECHNICALDATA 1 3 1 3 VIEWDRAWING ...

Page 12: ... 4 61 ft Aileron area without horn balance 2 x 0 839 m 2 x 9 03 ft Aileron area with horn balance 2 x 0 876 m 2 x 9 43 ft Aileron deflection up down 30 tolerance 2 1 3 4 HORIZONTALTAIL Span 3 20 m 10 50 ft Area 2 56 m 27 56 ft Airfoil WortmannFX71 L 150 30 1 3 5 ELEVATOR Area 0 768 m 8 27 ft Elevator deflection up 25 toler 2 down 25 toler 2 Trim tab deflection up 35 down 27 tolerance 2 1 3 6 VERTI...

Page 13: ... of Germany Complete 6 in 1 System with integrated Silencer 1 6 FUEL Fuel type AVGAS 100 100 LL for alternate fuel grades see later issues of Textron Lycoming S I No 1070 Minimum 100 130 octane Maximum 115 145 octane Total fuel capacity 189 L 49 9US gal Wingtanks 2 x 60 L 120 L 31 7US gal Center tank 60 L 15 9US gal Acro tank 9 L 2 3 US gal Usable fuel capacity in the system 187 L 49 4US gal Usabl...

Page 14: ...cII 81 16 kg m 16 63lbs ft Acrobatic I 76 49 kg m 15 67lbs ft Power loading MTOW AcrobaticIII 4 04 kg kW 6 65lbs hp AcrobaticII 3 70 kg kW 6 09lbs hp Acrobatic I 3 49 kg kW 5 74lbs hp 1 9 TERMINOLOGY Air Speeds CAS Calibrated Air Speed CAS is the same as TAS True Air Speed in standard atmospheric condition at sea level KCAS Calibrated speed in knots GS Groundspeed IAS Indicatedairspeed KIAS Indica...

Page 15: ...L Litres US gal US liquid gallon 3 79 litres US qt US liquid quart 0 946 litres hp Horsepower english h Hour kts Knots nm h 1 852 kilometer per hour km h Kilometerperhour lbs English pound 0 4536 kg hPa hekto Pascal inHg Inches of mercury MP Manifoldpressure PA Pressure altitude ft nm Nautical miles 1 852 km rpm Revolutionsperminute CG Centerofgravity Arm Arm is the horizontal distance from refere...

Page 16: ...1 8 Page Date 19 February 2014 Section 1 General Pilot s Operating Handbook US EXTRA330LX 1 11 CONVERSIONTABLE ...

Page 17: ...E 2 5 2 7 1 Reserved 2 5 2 7 2 Acrobatic Flight 2 5 2 8 ACROBATICMANEUVERS 2 6 2 8 1 Reserved 2 6 2 8 2 Acrobatic Flight 2 6 2 9 LOAD FACTOR 2 7 2 9 1 Reserved 2 7 2 9 2 Acrobatic Flight 2 7 2 10 FLIGHT CREW LIMITS 2 8 2 11 KINDS OF OPERATION LIMITS 2 8 2 11 1 Structural Temperature Colour Limitation 2 8 2 12 MAXIMUM OPERATING ALTITUDE 2 8 2 13 TIRE PRESSURE 2 8 2 14 MARKINGS AND PLACARDS 2 8 2 14...

Page 18: ...2 2 Page Date 19 February 2014 Section 2 Limitations Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 19: ...he pilot so that necessary inspection or maintenance procedures according to the MAINTENANCE MANUAL EXTRA 330LX can be performed 2 2 AIRSPEED IAS NeverExceedSpeed VNE 219 knots 406km h Max Structural Cruising Speed Acro Cat I II III VNO 154 knots 285km h Maneuver Speed Acro Cat I II III VA 154 knots 285km h Max Aileron Control Inputs Acro Cat I II III up to 185 knots 343km h 2 3 CROSS WINDCOMPONEN...

Page 20: ... CAUTION It is normal for the oil pressure to flicker from 69 to 207 kPa 10 to 30 psig when going from upright to inverted flight During knife edge flights and zero g flights oil pressure may drop and the oil system may not scavenge resulting in engine failure or damage if flight is prolonged Knife edge and zero g flight should not exceed 10 seconds WARNING If oil pressure drops to 0 kPa psig the ...

Page 21: ...S Max allowed empty weight Acrobatic category III 742 kg 1636 lbs Acrobatic category II 662 kg 1460 lbs Acrobatic category I 686 kg 1513 lbs Max allowed T O weight Acrobatic category III 950 kg 2095 lbs Acrobatic category II 870 kg 1918 lbs Acrobatic category I 820 kg 1808 lbs Max allowed landing weight 950 kg 2095 lbs 2 7 WEIGHTANDC G ENVELOPE Vertical reference fire wall Horizontal reference upp...

Page 22: ...ger the pilot should ensure that the co pilot passenger has been properly briefed on the physiological effects of high g maneuvers This briefing should include accepted muscles straining and breathing techniques to counter the physiological effects of high g maneuvers During the flight the pilot should ensure the co pilot passenger is doing OK Check weight and C G CAUTION Particular caution must b...

Page 23: ...throttle 1 4 Loop climb 100 185 190 352 Loop 100 185 190 352 Stall turn 100 185 190 352 Aileron roll 80 148 185 343 fulldeflection Snap roll 80 148 140 259 tail slide 100 185 190 352 Spin VS Inverted spin VS Knife edge 150 278 10 s Inverted Flight VS 190 352 4 min 2 9 LOADFACTOR 2 9 1 RESERVED 2 9 2 ACROBATICFLIGHT Category I MTOW 820 kg 1808 lbs 10 g 10 g for 1 seat occupied Category II MTOW 870 ...

Page 24: ...LIMITATION Structure is qualified up to 72 C 161 6 F Structure temperatures composite above 72 C 161 6 F are not permitted Not to exceed this temperature limit color specification for composite structure has to be complied with To check the temperature inside the cockpit potential green house effect a reversible temperature indicator STRUCTURAL OVERHEAT INDICATOR is applied on the upper side of th...

Page 25: ...ument panel on the trim LED indicator F U E L AVGAS 100 100LL OIL TRIM DOWN UP This airplane is certified for VFR day operation Operation under known icing conditions prohibited V 154 KTS ACRO A The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the acrobatic category Other operating limitations which must ...

Page 26: ...s On the right side of both instrument panels NO SMOKING CENTER TANK INDICATION SHOWS ZERO IN LEVEL FLIGHT BELOW 9 L 2 4 US GAL UNUSABLE FUEL 2 L 0 5 US GAL THE REMAINING FUEL IN LEVEL FLIGHT CANNOT BE USED SAFELY WHEN INDICATOR READS ZERO ACROBATIC 10 G 1 Pilot MTOW 820 kg 1808 lbs 8 G 2 Persons on board MTOW 870 kg 1918 lbs 6 G 2 Persons on board MTOW 950 kg 2095 lbs USE OF HEADSET IS REQUIRED U...

Page 27: ...Near Mag Dir Indicator LOW RPM PROP HIGH RPM CLOSE THROTTLE OPEN VENT OPEN CALLSIGN For For Steer Steer N 030 060 E 120 150 S 210 240 W 300 330 LEAN MIXTURE RICH CANOPY LOCK LOCK UNLOCK WARNING SOLO FLYING FROM REAR SEAT ONLY CAUTION Particular caution must be exercised when performing maneuvers at speeds above V 154 KIAS 285 km h Large or abrupt rudder and elevator control inputs above this speed...

Page 28: ...f the separate hatch upper cowling On the outside of the wheel fairings On the centreline of bottom fuselage cover In rear cockpit on the aileron control rods In rear cockpit on the LH side of the panel cover On the FOD protection cover behind the pilot seat In both cockpits on the RH side WING TANK DRAIN CENTER TANK DRAIN GASCOLATOR DRAIN USE STRAIGHT MINERAL OIL FOR A MINIMUM OF 50 HOURS TORQUE ...

Page 29: ...max KIAS Segment Horizontal Line V V Aileron roll 80 45 climbing 80 V Snap roll 80 13 90 up V Tail slide 100 1 1 9 8 0 5 45 diving V V Spin 90 diving V V Inverted spin 1 4 Loop climb 100 190 Inverted flight 190 Less than 4 min Loop 100 190 Knifeedge 150 Stall turn 100 190 Less than 10 s S NE NE NE S NE VS VS VS S NE VA Approved acrobatic maneuvers and recommended entry airspeeds ...

Page 30: ...55 psig greenarc 55 psig 95 psig yellow arc 95 psig 115 psig red line 115 psig OILTEMPERATUREINDICATOR yellow arc 140 F greenarc 140 F 210 F yellow arc 210 F 245 F red line 245 F CYLINDERHEADTEMPERATUREINDICATOR yellow arc 150 F greenarc 150 F 435 F yellow arc 435 F 465 F red line 465 F RPMINDICATOR greenarc 700 rpm 2600 rpm red line 2600 rpm G METER greenarc 5 g 8 g yellow arc 8 g 10 g red line 1...

Page 31: ...owing systems and items of equipment must be installed and operable for the particular kind of operation indicated ACROBATIC 1 seat 2 seats COMMUNICATION 1 Transceiver VHF 1 1 ELECTRICALPOWER 1 Battery 1 1 2 Alternator 1 1 3 Ammeter 1 1 4 Voltmeter 0 0 FLIGHTCONTROLSYSTEM 1 Elevator trim control electric 1 1 2 Stall warning 0 0 FUEL 1 Boost pump 1 1 2 Fuel quantity indicator wing tank 1 1 3 Fuel q...

Page 32: ...dset rear 1 1 6 Headset front 0 1 N O T E The zeros 0 used in the above list mean that either the equipment or system or both were not required for type certification for that kind of operation Either equipment or systems in addition to those listed above may be required by the national operating regulations The asterisks used in the above list mean that according to FAR Part 91 General Operating ...

Page 33: ...re immediately after Take off 3 4 3 2 3 Engine Failure during Flight Restart Process 3 4 3 2 4 Loss of Oil Pressure 3 5 3 2 5 High Oil Temperature 3 5 3 2 6 Alternator Failure 3 5 3 3 FORCED LANDINGS 3 6 3 3 1 Emergency Landing without Engine Power 3 6 3 3 2 Precautionary Landing with Engine Power 3 6 3 4 FIRES 3 6 3 4 1 During Start on Ground 3 6 3 4 2 If Engine Fails to Start 3 7 3 4 3 Engine Fi...

Page 34: ...3 2 Page Date 19 February 2014 Section 3 Emergency Procedures Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 35: ...e first transmission Thereafter the ground station should be kept informed of the progress of the flight and of any changes or developments in the emergency Three basic rules apply to most emergencies and should be observed by eachaircrewmember 1 Maintain aircraft control 2 Analyze the situation and take proper action 3 Land as soon as possible as soon as practical The meaning of as soon as possib...

Page 36: ...aximum demonstrated cross wind component 15 Knots 27 km h 3 2 OPERATIONALCHECKLIST 3 2 1 ENGINE FAILURE DURING TAKE OFF ROLL 1 Throttle IDLE 2 Brakes APPLY 3 Mixture IDLE CUT OFF 4 Ignition switch OFF 5 Battery switch OFF 6 Alternator switch OFF 3 2 2 ENGINEFAILUREIMMEDIATELYAFTERTAKE OFF Stall speed 64 KIAS 119 km h 1 Airspeed 90 KIAS 167 km h 2 Mixture IDLE CUT OFF 3 Fuel shutoff valve OFF Pull ...

Page 37: ...ing decrease in RPM 3 2 5 HIGHOILTEMPERATURE 1 Throttle REDUCE 2 Mixture ENRICH ifpractical 3 Airspeed INCREASE if practical 4 Land ASAP BE PREPARED FOR POWER OFF LANDING 3 2 6 ALTERNATORFAILURE An alternator failure is indicated by the red light of the low voltage monitor If red light illuminates 1 Digital voltage indication CROSSCHECK If indication is above 13 V alternator is in function 2 Fligh...

Page 38: ... km h 3 Selected field FLY OVER noting terrain and obstructions then reaching a safe altitude and airspeed 4 Battery switch OFF 5 Alternator switch OFF 6 Touchdown SLIGHTLYTAILLOW 7 Ignition switch OFF 8 Mixture IDLECUTOFF 9 Fuelshutoffvalve OFF Pull Turn 10 Brakes APPLY HEAVILY 3 4 FIRES 3 4 1 DURING START ON GROUND 1 Cranking CONTINUE to get a start which would suck the flames and accumulated fu...

Page 39: ...5 1 INADVERTENT ICING ENCOUNTER 1 Turn back or change altitude to obtain an outside temperature that is less conductive to icing 2 Plan a landing at the nearest airfield With extremely rapid ice build up select a suitable off airport landing field 3 6 UNINTENTIONAL SPIN Refer to section 4 Normal Procedures acrobatic maneuver spin recovery 3 7 MANUALBAIL OUT When in an emergency situation that requ...

Page 40: ...Canopyhandle PULL TO OPEN N O T E If canopy fails to open break the canopy 7 Aircraft EVACUATE ASAP 3 9 ELEVATOR CONTROL FAILURE In case of elevator control failure the aircraft can be flown with the elevator trim In this case trim nose up to the desired speed and control horizontal flight or descend with engine power For landing trim nose up and establish a shallow descend by adjusting throttle T...

Page 41: ...S 4 4 4 3 STARTING PROCEDURES 4 6 4 3 1 Cold Engines 4 6 4 3 2 Hot Engines 4 6 4 4 TAXIING THE AIRCRAFT 4 6 4 5 TAKE OFFPROCEDURE 4 7 4 5 1 BeforeTake Off 4 7 4 5 2 Take Off 4 7 4 6 CLIMB 4 8 4 7 CRUISE 4 8 4 8 LANDINGPROCEDURES 4 8 4 8 1 Descent 4 8 4 8 2 Approach 4 8 4 8 3 Before Landing 4 8 4 8 4 Normal Landing 4 9 4 9 GO AROUND 4 9 4 10 SHUTDOWN 4 9 4 11 LEAVING THEAIRCRAFT 4 9 4 12 ACROBATIC ...

Page 42: ...4 2 Page Date 19 February 2014 Section 4 Normal Procedures Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 43: ...5 181 335 181 335 Landing Approach 84 156 89 165 93 172 onFinal 76 141 78 144 82 152 Go AroundSpeed 93 172 98 181 102 189 RecommendedAirspeed For Flight In Rough Air max VA 154 285 154 285 154 285 Max Demonstrated Cross WindComponent 15 kts 27 15 kts 27 15 kts 27 4 0 2 CHECKLISTANDPROCEDURES This handbook contains the checklist and procedures to operate the aircraft The pilot should be familiar wi...

Page 44: ...ry switch ON 5 Fuel quantity indicators CHECK 6 Battery switch OFF 7 Fuel selector ACRO CENTER TANK N O T E Although safe operation does not require the use of the tanks in a specific sequence it is recommended to set fuel selector to ACRO CENTER TANK position 2 Empennage 1 All round inspection canopy surfaces stabilizer elevator trim rudder and tailwheel CHECK 2 Horizontal stabilizer attachment b...

Page 45: ...LE WATER CHECKCLOSED 6 Exhaust silencer CHECK FOR DAMAGE AND SECUREATTACHMENT 5 Left wing 1 Left landing gear wheel and brakes CHECK 2 Fuel quantity CHECK 3 Fuel tank filler cap CHECK 4 Wing fuel tank drain DRAIN FOR AT LEAST 4 SECONDS TO CLEAR SUMP OF POSSIBLE WATER CHECKCLOSED 5 Pitotcover REMOVE 6 Trailingedge CHECK 7 Aileron freedom of movement and security CHECK 6 Before starting engine 1 Pre...

Page 46: ... fires release the ignition switch back to BOTH 8 Move mixture control slowly and smoothly to FULL RICH 9 Checktheoilpressuregauge Ifminimumoilpressureisnotindicatedwithin30seconds shut off the engine and determine cause of trouble 4 3 2 HOTENGINES Because of the fact that the fuel percolates and the system must be cleared of vapor it is recommended to use the same procedure as outlined for cold e...

Page 47: ...rwise the difference is more than permissible N O T E During the short circuit grounding of a single magneto the respective red LED must illuminate The maximum allowed RPM drop at 1800 min 1 is 175 min 1 The maximum difference between the magnetos shall not to be more than 50 RPM identify with the illuminated yellow LED AlternatorOutput CHECK Propellercontrol MOVE through its complete range to che...

Page 48: ...rottle REDUCE 2 Mixture FULLRICH 3 RPMControl SET to 2400 RPM 4 Trim ADJUST 5 Fuel selector ACRO CENTER TANK N O T E Although safe operation does not require the use of the tanks in a specific sequence it is recommended to set fuel selector to ACRO CENTER TANK position 4 8 2 APPROACH 1 Boost pump ON 2 Mixture SET to RICH 3 Airspeed REDUCEtoapproachspeed 4 Propeller SET to low pitch HIGH RPM N O T ...

Page 49: ...ng 4 Throttle CLOSE IDLE 5 Braking Minimumrequired 4 9 GO AROUND Decide early in the approach if it is necessary to go around and then start go around before too low altitude and airspeed are reached Proceed as follows 1 RPM control HIGH RPM Full forward 2 Throttle OPEN Take offpower 3 Airspeed Minimum 102 KIAS 189 km h rotatetogo aroundaltitude 4 10 SHUTDOWN 1 Boost pump OFF 2 Landinglight OFF 3 ...

Page 50: ...ilot or passenger This fact must be considered when pulling or pushing high g s 4 12 2 MANEUVERS CAUTION Particular caution must be exercised when performing maneuvers at speeds above VA 154 KIAS 285 km h Large or abrupt rudder and elevator control inputs above this speed as well as full aileron control inputs above 185 KIAS 343 km h may impose unacceptably high loads which exceed the structural c...

Page 51: ...or aileron rolls with max deflection Snap rolls should not be performed at speeds above 140 KIAS 259 km h Segment 1 4 loop climbing The minimum recommended speed is 100 KIAS 185 km h If the maneuver is to be followed by a vertical line a higher entry speed is required depending on the expected length of the line A complete loop can be performed at speeds above 100 KIAS 185 km h N O T E Since the m...

Page 52: ...n still be improved by feeding in in spin ailerons N O T E If ever disorientation should occur during spins normal or inverted one method always works to stop the spin Power idle Kick rudder to the heavier side this will always be against spin direction Take hands off the stick The spin will end after 1 2 turn The plane will be in a steep dive in a side slip Recovery to normal flight can be perfor...

Page 53: ...been made by the Federal Aviation Administration that the noise levels of thisaircraftareorshouldbeacceptableorunacceptableforoperationat into oroutofanyairport The above noise levels were established at 950 kg 1980 lbs takeoff weight This aircraft model is in compliance with FAR 36 noise standards applicable to this type ...

Page 54: ...4 14 Page Date 19 February 2014 Section 4 Normal Procedures Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 55: ...1 GENERAL 5 3 5 1 1 Performance Charts 5 3 5 1 2 Definitions of Terms 5 3 5 1 3 Sample Problem 5 3 5 2 ISA CONVERSION 5 5 5 3 AIRSPEED CALIBRATION 5 6 5 4 STALL SPEED 5 7 5 5 TAKE OFFPERFORMANCE 5 8 5 6 RATE OF CLIMB PERFORMANCE 5 9 5 7 TIME TO CLIMB FUEL TO CLIMB 5 10 5 8 RANGE 5 11 5 9 ENDURANCE 5 12 5 10 CRUISE PERFORMANCE 5 13 5 11 LANDINGPERFORMANCE 5 14 ...

Page 56: ...5 2 Page Date 19 February 2014 Section 5 Performance Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 57: ...timate the fuel required for the particular flight 5 1 1 Performance Charts Performance data are presented in tabular or graphical form to illustrate the effect of different variables Sufficiently detailed information are provided in the tables so that conservative values can be selected and used to determine the particular performance figure with reasonableaccuracy All speeds in this chapter are ...

Page 58: ...4 Liters 1 2 US Gal CRUISE Cruise Altitude and Power Setting should be determined for most economical fuel consumption and several other considerations In an altitude of 8000 ft 2438 m and a Power Setting of 65 a Fuel Consumption of 52 L H 13 7 US Gal H and 3 25 NM L 12 3 NM US Gal can be obtained by Fig 5 9 RANGEANDENDURANCE Fig 5 8 presents Range and Endurance values for a T O Weight of 950 kg 2...

Page 59: ...Page Date 19 February 2014 5 5 Section 5 Performance Pilot s Operating Handbook US EXTRA330LX 5 2 ISACONVERSION ISA Conversion of pressure altitude and outside air temperature ...

Page 60: ...d airspeed assumes zero instrument error 50 60 70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 50 60 70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 KCAS KIAS 90 110 130 150 170 190 210 230 250 270 290 310 330 350 370 390 410 90 110 130 150 170 190 210 230 250 270 290 310 330 350 370 390 410 CAS km h IAS km h ...

Page 61: ...ORWARDC G STALL SPEEDS ANGLE OF BANK WEIGHT CATEGORY 0 30 45 60 1 g 1 15 g 1 41 g 2 g kg lbs KIAS km h KIAS km h KIAS km h KIAS km h 950 ACROIII 64 69 76 91 2095 119 128 141 169 870 ACROII 61 66 73 87 1918 113 122 135 161 820 ACROI 59 64 71 84 1808 109 119 131 156 Max altitude loss during stall recovery is approximately 100 ft 30 m ...

Page 62: ...ft m ft m ft m ft m ft lbs km h 950 68 SL 96 315 207 679 115 377 248 813 133 436 285 935 2095 126 2000 610 115 377 248 814 138 453 298 978 160 525 342 1122 4000 1219 138 453 298 978 166 545 357 1171 192 630 410 1345 6000 1829 166 545 358 1175 199 653 429 1407 230 755 492 1614 870 65 SL 78 256 167 548 93 305 200 656 107 351 230 755 1918 120 2000 610 94 308 200 656 112 367 240 787 128 420 276 906 40...

Page 63: ...RFORMANCE 36 F 18 F 18 F 36 F 20 C 2 0 C 4 F 10 C 1 0 C 1 4 F 10 C 1 0 C 5 0 F 20 C 2 0 C 6 8 F 3 0 C 8 6 F 0 C 3 2 F 193 187 181 176 170 V Y Weight KIAS km h EXAMPLE Weight 850 KG 1874 LBS PA 2000 ft ISA 8000 ft ISA ROC 2320 ft min 1520 ft min Power Max power full rich 2600 rpm 2095 1985 1874 1764 1654 lbs MTOW ...

Page 64: ...B FUEL TO CLIMB EXAMPLE WEIGHT 850 KG 1874 LBS ALT 2000 ft ISA 8000 ft ISA TIME TO CLIMB 3 1 min FUEL TO CLIMB 4 4 ltr 1 16 US Gal WEIGHT KG LBS 2095 lbs 1654 lbs 1874 lbs 2029 lbs 1544 1654 1764 1874 1985 2095 LTR US GAL 0 53 1 59 2 64 3 70 4 76 5 81 FUEL TO CLIMB CONDITIONS MAX CONT POWER CLIMB AT VY SPEED ISA ...

Page 65: ...Page Date 19 February 2014 5 11 Section 5 Performance Pilot s Operating Handbook US EXTRA330LX 5 8 RANGE ...

Page 66: ...5 12 Page Date 19 February 2014 Section 5 Performance Pilot s Operating Handbook US EXTRA330LX 5 9 ENDURANCE ...

Page 67: ... 259 3 57 544 1007 Economy 2000 19 0 43 135 36 5 9 6 142 6 264 131 243 4 18 591 1095 Economy 6000 2600 23 4 79 248 77 6 20 5 180 5 334 158 293 1 97 351 650 Power 1829 2500 22 2 71 225 69 8 18 4 174 3 323 153 283 2 19 377 698 Power 2200 22 2 62 195 50 5 13 3 165 6 307 146 270 3 00 493 913 Economy 2000 21 5 52 165 42 6 11 3 156 1 289 139 257 3 55 551 1020 Economy 2000 18 5 43 135 36 5 9 6 145 4 269 ...

Page 68: ...527 1729 177 581 548 1798 185 607 586 1923 2095 172 2000 610 181 594 558 1831 188 617 580 1903 197 646 602 1975 4000 1219 192 630 592 1942 199 653 615 2018 208 682 639 2096 6000 1829 203 666 627 2057 211 692 652 2139 220 722 678 2224 870 89 SL 158 518 488 1601 164 538 507 1663 171 561 527 1729 1918 165 2000 610 165 541 518 1699 175 574 537 1762 181 594 558 1831 4000 1219 177 581 548 1798 185 607 5...

Page 69: ... Contents Paragraph Page SECTION 6 WEIGHTAND BALANCEAND EQUIPMENT LIST 6 1 GENERAL 6 3 6 2 AIRCRAFT WEIGHING PROCEDURE 6 3 6 2 1 Owners Weight and Balance Record 6 4 6 3 CENTER OF GRAVITYCALCULATION SAMPLE PROBLEM 6 5 6 3 1 Sample 6 7 6 3 2 Weight and Balance Record Sheet 6 7 6 4 LOADING WEIGHTS AND MOMENTS 6 8 6 5 WEIGHTS AND MOMENTS LIMITS 6 9 6 6 EQUIPMENT LIST 6 10 ...

Page 70: ...6 2 Page Date 19 February 2014 Section 6 Weight and Balance and Equipment List Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 71: ... pilot to ensure that the aircraft is loaded properly 6 2 AIRCRAFTWEIGHINGPROCEDURE The aircraft weight is determined by weighing all three wheel loads simultaneously by three scales with the aircraft levelled Upperfuselagereferencelinehorizontal Datum line for weight arms x is the fire wall X1 distance fire wall main wheel X2 distance fire wall tail wheel XN distance fire wall item N XG distance ...

Page 72: ...item Wo Xo Airplane weight CG position Wn Xn Weight distance from fire wall of item to add New Weight of airplane and new CG W Wo Wn XG Wo x Xo Wn x Xn CG position W 6 2 1 Owners Weight and Balance Record Enter below all weight change data from aircraft log book EXTRA330LX SERIALNUMBER Date Descriptionof Weightchange Runningempty modification Added Removed weight Wt kg Arm cm Moment kg cm Wt kg Mo...

Page 73: ...n 51 LTR 120LTR 13 4 US GAL 31 7 US GAL kg lbs kg lbs kg lbs kg lbs 1 90 198 5 2 90 198 5 37 81 5 3 90 198 5 37 81 5 86 4 190 5 4 90 198 5 60 132 3 5 90 198 5 37 81 5 60 132 3 6 90 198 5 37 81 5 60 132 3 86 4 190 5 7 90 198 5 90 198 5 8 90 198 5 37 81 5 90 198 5 PILOT ACRO TANK COPILOT WING TANK RearSeat Fuel Front Seat Fuel Position 51 LTR 101LTR 13 4 US GAL 26 7 US GAL kg lbs kg lbs kg lbs kg lb...

Page 74: ...6 6 Page Date 19 February 2014 Section 6 Weight and Balance and Equipment List Pilot s Operating Handbook US EXTRA330LX 6 3 CENTER OF GRAVITY CALCULATION SAMPLE PROBLEM ...

Page 75: ... Aircraft Empty Weight 660 0 kg 1455 lbs 950 0 kg 2094 4lbs To find C G follow line Pilot Rear Seat from Empty Weight to 90 kg 198 5 lbs Point 1 Continue on line Copilot Front Seat to 90 kg Point 7 Now follow line Fuel via Point 8 51 L 13 5 US gal Acro Fuel to Point 9 101 L 26 6 US gal Fuel in Wing Tank FIND Weight 950 kg 2094 4lbs C G 75 4 cm 29 6inch 6 3 2 Weight and Balance Record Sheet WEIGHT ...

Page 76: ...8330 7180 90 198 18630 16137 8820 7603 TOTAL FUEL CAPACITY 189 L 49 9 US gal FUEL ACRO CENTER TANK WINGTANK L kg kg x cm L kg kg x cm USgal lb lb x in USgal lb lb x in 9 2 4 6 5 14 3 182 157 10 2 6 7 2 15 9 360 313 20 5 3 14 4 31 8 420 365 20 5 3 14 4 31 8 721 629 25 6 6 18 0 39 7 529 459 40 10 6 28 8 63 5 1442 1257 30 7 9 21 6 47 6 638 553 60 15 9 43 2 95 3 2164 1886 35 9 2 25 2 55 6 746 648 80 2...

Page 77: ... 2014 6 9 Section 6 Weight and Balance and Equipment List Pilot s Operating Handbook US EXTRA330LX 6 5 WEIGHTS AND MOMENTS LIMITS EXAMPLE At 790 KG 1741 LBS and 640000 kgcm the C G location is 80 0 cm 31 4 aft of ref datum ...

Page 78: ...nal S 50 FA3008 0 09 0 25 R 1 Volt Ammeter Electronics International VA 1A 50 FA3007 PG 0 22 1 62 R 1 External Power Socket Cole Hersee 11041 06 31731 1 46 1 07 O Piper Type 1 Batt Charger Plug 12V Extra EA 93102 18 02636 0 02 0 17 O 1 12VDC Power Outlet Sutars 1218 31494 0 03 1 62 O Socket Cockpit 25 1 Safety Belt Assy Hooker 1011230 3x FK0002 or FK0019 3 30 2 12 R Rear Seat 1113012 1 1x seat bel...

Page 79: ...FB0001 0 55 1 11 R Cylinders rear 1 Tail Wheel 6 Assy Special Products 32477 VB 1 28 5 23 R Soft Aviation Inc 1 Tail Wheel 5 Steerable Extra EA 53201 7 53201 007 VB 0 90 5 23 A L R Wheel fairing CRP Extra EA 53102 301 0 33 2 50 R 1 Brake Fluid Reservoir ACS A 315 02889 0 20 0 04 R Lights 33 1 Strobe Nav Light RH Whelen 01 0790340 00 32989 0 30 1 35 R 14V green 1 Strobe Nav Light LH Whelen 01 07903...

Page 80: ... Instr UI7030C 27 01485 0 54 1 62 O Indicator fpm reserved 1 Vertical Speed Ind fpm Mikrotechna Praha LUN 1144 B0B1 34161 0 40 1 61 A reserved 1 Attitude Gyro RC Allen RCA2600 2 0 tilt 33027 0 24 1 63 O electronic 2 1 4 1 Attitude Gyro RC Allen RCA2600 2 0 tilt 33881 0 13 1 61 A electronic 2 1 4 102 0202 01 1 Attitude Gyro RC Allen RCA2600 3 0 tilt 33217 0 45 1 63 A electronic 3 1 8 1 Attitude Gyr...

Page 81: ...talClock Astrotech LC 2 FI0004 0 14 1 60 O Optional Aerobatics Equipment 1 Aresti Card Holder Extra EA 83504 4 EA 83504 0 09 1 66 O 004 PG 1 Aresti Card Holder Aspen Extra EA 86504 4 EA 86504 0 09 1 66 A 004 PG 1 1 Sighting device Extra EA 8E801 30 0 55 1 60 O 45 90 1 Smoke System Extra 86112 9 20 0 30 O Optional Electronic Accelerometer 1 El accelerometer with TL Electronik TL 3424_EXT 32582 0 30...

Page 82: ...5 32269 0 11 0 14 O 1 ELT Artex ME406 32173 PG 1 42 2 60 O Including ELT Antenna Artex or 110 773 33524 0 08 3 00 O Rami AV 200 33965 0 08 3 00 A 1 Intercom Northern Airborne NAT AA83 001 31659 PG 0 28 1 55 O 1 PanelDock AirGizmos GPSMAP696 33665 0 25 1 60 O 1 PanelDock AirGizmos GPSMAP796 34175 0 27 1 60 O 1 Remote Audio Panel Garmin GMA 35 33902 PG 1 00 1 53 O Cowling 54 1 Cowling CRP Extra EA 8...

Page 83: ...RPM Vernier Control ACS Products Co A 750 30 1200 00113 0 71 0 82 R 1 Mixture Vernier Control ACS Products Co A 750 20 1080 00112 0 65 0 94 R 1 Throttle Control Teleflex CC330 10 33052 0 56 0 60 R Engine Instruments Conventional engine gauges 1 RPMIndicatordigital Horizon P100 230 33624 0 68 1 60 R max 2600 RPM 635 00 reserved 1 Oil Press Oil Temp UMA D2 OP130U 33428 0 09 1 62 R Ind 2 1 4 OT300U 0...

Page 84: ...1 Fuel Flow Transducer Flowscan 201 B or FXT 201 0 09 0 02 O Shadin 680501 or 680600 FI4015 0 09 0 02 A Exhaust 78 1 Exhaust System 6 in 1 Gomolzig EA300 606000 33891 8 48 0 39 R incl silencer with 1 2 inlet outlet cooling Gomolzig EA300 606009 32153 shroud 1 Exhaust System 6 in 1 Gomolzig EA300 606000 33891 8 48 0 39 A incl silencer with 1 3 inlet outlet cooling Gomolzig EA300 606024 03248 shroud...

Page 85: ...7 5 3 Lateral Flight Control System 7 5 7 5 4 Directional Flight Control System 7 5 7 5 5 Secondary Control 7 5 7 6 INSTRUMENTATION 7 5 7 6 1 Instrument Panel Rear Cockpit 7 6 7 6 2 Instrument Panel Front Cockpit 7 8 7 7 LANDING GEAR 7 8 7 8 SEATS SEAT BELTS 7 8 7 9 CANOPY 7 8 7 10 POWER PLANT 7 9 7 10 1 Engine 7 9 7 10 2 Oil System 7 9 7 10 3 Engine Installation 7 10 7 10 4 Propeller 7 10 7 10 5 ...

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Page 87: ...eat indicator immediately and flying is prohibited When the structure cools down below this temperature limit the word RISK disappears and you may go on with the preflight checklist a Below72 C 161 6 F b At 72 C 161 6 F or above The standard aircraft is designed to operate within a range of ambient air temperature from 20 C to 44 C 4 F to 111 F at sea level It is possible to start the engine using...

Page 88: ...ore the ailerons are equipped with spades to decrease pilot s forces The aileron control push pull rods are connected to the aileron at the second bearing point in span wise direction To prevent flutter the ailerons are mass balanced at the leading edge of the shielded horn 7 4 EMPENNAGE The EXTRA 330LX possesses a cruziform empennage with stabilizers and moveable control surfaces The rudder is ba...

Page 89: ...o the ailerons The ailerons are statically as well as dynamically balanced dynamically with spades The ailerons are supported by lubricated sealed bearings 7 5 4 DIRECTIONALFLIGHTCONTROLSYSTEM The dual rudder pedals with brake pedals are electric adjustable and operate the rudder through a cable system Springs keep the cables under tension when they are not operated 7 5 5 SECONDARYCONTROL The elev...

Page 90: ...e 19 February 2014 Section 7 Description and Operation of Aircraft and Systems Pilot s Operating Handbook US EXTRA330LX 7 6 1 INSTRUMENTPANEL REARCOCKPIT Figure 1 Instrument Panel Figure 2 Switches Circuit Breaker ...

Page 91: ...17 Fuel quantity center tank 18 Fuel quantity wing tank 19 Circuitbreaker 20 Switches Position Item Fig 2 1 Alternator warning light incl press to test feature 2 Battery switch red cap 3 Alternator switch red cap 4 Boost pump switch 5 Strobe light switch 6 NAV light switch 7 Reserved 8 Trim circuit breaker 9 12 V circuit breaker 10 Starter circuit breaker 11 Alternator circuit breaker 12 Boost pum...

Page 92: ...left and two right lap belts and a negative g strap All belts are adjustable As each lap belt features a single point release they are redundant for safety during aerobatic maneuvers If one release is opened unintentionally the second one guarantees full safety For safe operation the releases are arranged in a way that one has to be closed to the right side the other one to the left During acrobat...

Page 93: ...re included in the power plant installation Fuel Injector Magnetos Start System Alternator Starter Fuel pump Shielded ignition system Propellergovernordrive The engine is operated with the following manual controls Throttle control dual RPM control Fuel mixture control The starter magneto switch is located on the right side of the instrument panel in front of the rear seat Thepropellergovernormoni...

Page 94: ...talled This propeller has a diameter of 1 90 m 74 8 in 7 10 5 THROTTLE Dual control cub type mounted on the left side of the cockpit 7 10 6 MIXTURE Vernier control located at the left side of the rear cockpit red knob 7 10 7 RPM CONTROL Vernier control on the left side of the rear cockpit Preselection of RPM possible due to constant speed governor blue knob 7 10 8 FUELSELECTORVALVE Dual control A ...

Page 95: ...Page Date 19 February 2014 7 11 Section 7 Description and Operation of Aircraft and Systems Pilot s Operating Handbook US EXTRA330LX Figure 3 Fuel System ...

Page 96: ...ormal float type transducers and electrically operated fuel indicators are used 7 12 ELECTRICALSYSTEM The electrical system refer to Figure 4 is supplied by a 12 V alternator with integrated rectifier transistor voltage regulator The alternator is mounted on and belt driven by the engine The field current is controlled by the voltage regulator to nominal 14 5 V under all load conditions The ALTERN...

Page 97: ...Page Date 19 February 2014 7 13 Section 7 Description and Operation of Aircraft and Systems Pilot s Operating Handbook US EXTRA330LX Figure 4 Electrical System ...

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Page 99: ... s Operating Handbook US EXTRA330LX TABLEOFCONTENTS Paragraph Page SECTION 8 HANDLING SERVICING MAINTENANCE 8 1 INTRODUCTION 8 3 8 2 AIRPLANE INSPECTION PERIODS 8 3 8 3 PILOT CONDUCTED PREVENTIVE MAINTENANCE 8 3 8 4 ALTERATIONS OR REPAIR 8 3 8 5 SERVICING 8 4 8 6 GROUNDHANDLING 8 4 ...

Page 100: ...8 2 Page Date 19 February 2014 Section 8 Handling Servicing and Maintenance Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 101: ...ust pass a complete inspection after every 100 flights hours with a minor check after 50 hours The Airworthiness Authority may require other inspections by the issuance of airworthiness directives applicable to the aircraft engine propeller and components The owner is responsible for compliance with all applicable airworthiness directives and periodical inspections 8 3 PILOTCONDUCTEDPREVENTIVEMAIN...

Page 102: ...g can be used as third point to tie down the airplane If the aircraft is parked in the open it must be protected against the effects of weather the degree of protection depending on severity of the weather conditions and the expected duration of the parking period When the airplane is parked in good weather conditions for less than a half day park the aircraft headed into the wind and place wheel ...

Page 103: ...rometerTL 3424_EXT 6 p 905 External Power 4 p 906 Digital RPM Indicator 6 p 907 Smoke System 8 p 908 Single Seat Canopy 4 p 909 ARTEXME 406ELT 8 p 910 NATAA83 001Intercom 8 p 911 BECKERATC4401Transponder 8 p 912 BECKERBXP6401Transponder 12 p 913 GARMIN GTX 327 Transponder 6 p 914 GARMIN GTX 328 Transponder 8 p 915 GARMIN GTX 330 Transponder 8 p 916 GARMIN GNC 420W GNS 430W 8 p 917 ASPENEFD1000 500...

Page 104: ...9 2 Page Date 19 February 2014 Section 9 Supplements Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 105: ...he editor has the copyright of these Supplements and is responsible for edition of revisions The log of effective pages is found on the preceding pages of this Pilot s Operating Handbook Each Supplement section e g steerable tailwheel covers only a single system device or piece of equipment and is a self contained miniature Pilot s Operating Handbook The owner is responsible for incorporating pres...

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Page 107: ...Table of Contents Paragraph Page SECTION 901 STEERABLE TAILWHEEL 901 1 GENERAL 901 3 901 2 LIMITATION 901 3 901 3 EMERGENCYPROCEDURES 901 3 901 4 NORMALPROCEDURES 901 3 901 5 PERFORMANCE 901 3 901 6 WEIGHT AND BALANCE 901 3 901 7 DESCRIPTION OF THE SYSTEM 901 3 901 8 HANDLING SERVICINGAND MAINTENANCE 901 4 ...

Page 108: ...901 2 Page Date 19 Februar 2014 Section 901 Steerable Tail Wheel Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 109: ... be checked during the preflight check 901 5 PERFORMANCE Changes in flight performance due to installation of the steerable tailwheel are not notice able The given basic performance data under section 5 are still valid 901 6 WEIGHT AND BALANCE A change of the running empty weight and resulting C G position after installation of the steerable tailwheel is neglectable because of minor differences in...

Page 110: ...rating Handbook US EXTRA330LX 901 8 HANDLING SERVICINGANDMAINTENANCE During 50 hour inspection the bearing steel sleeve has to be lubricated on the point of lubri cating Additionally all parts of the tailwheel have to be inspected visually for deformations cracks and corrosion ...

Page 111: ...able of Contents Paragraph Page SECTION 902 ELECTRIC PEDAL ADJUSTMENT 902 1 GENERAL 902 3 902 2 LIMITATIONS 902 3 902 3 EMERGENCYPROCEDURES 902 3 902 4 NORMALPROCEDURES 902 3 902 5 PERFORMANCE 902 3 902 6 WEIGHT AND BALANCE 902 3 902 7 DESCRIPTION OF THE SYSTEM 902 4 902 8 HANDLING SERVICINGAND MAINTENANCE 902 4 ...

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Page 113: ...justment of the pedal position during takeoff and landing is not allowed It is recommended not to adjust the pedals when radio transmissions are made or when the magnetic direction indicator is used 902 3 EMERGENCYPROCEDURES Pedal Run away Pedal switch USE in reverse direction of run away if no effect PEDALS Circuit Breaker PULL 902 4 NORMALPROCEDURES Onground Rudderpedals ADJUST position using th...

Page 114: ...t the steel frame The connection to the front seat pedals is realized by a further cable which is fixed to the control cable by two Nicopress oval sleeves The stepless pedal adjustment is realized by electromechanical actuators which are controlled separately by switches on the rear instrument panel refer to Figure 1 below The total travel of the system is limited to 160 mm 6 3 by a front and a re...

Page 115: ... Table of Contents Paragraph Page SECTION 903 CABIN HEATING SYSTEM 903 1 GENERAL 903 3 903 2 LIMITATIONS 903 3 903 3 EMERGENCYPROCEDURES 903 3 903 4 NORMALPROCEDURES 903 3 903 5 PERFORMANCE 903 3 903 6 WEIGHT CENTER OF GRAVITY 903 3 903 7 SYSTEM DESCRIPTION 903 4 903 8 HANDLING SERVICINGAND MAINTENANCE 903 4 ...

Page 116: ...Section 903 Cabin Heating System 903 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA 330LX Left blank intentionally ...

Page 117: ...system is controlled by two handles in the rear cockpit 903 2 LIMITATIONS The operation limitations are not affected due to the installation of the cabin heat system The following operation placards have to be attached to the aircraft next to the main handle next to the distribution handle 903 3 EMERGENCYPROCEDURES Engine fire Heater OFF 903 4 NORMALPROCEDURES Notaffected 903 5 PERFORMANCE Notaffe...

Page 118: ...ctor box 4 is placed on the engine side of the firewall Using the main handle 9 the warm air can there be guided into the cockpit or dumped overboard A further selector box 5 is located ontheaftsideofthefirewall Usingthedistributionhandle 8 theratioofwarmairsupplybetween frontandrearcanbecontrolledthere Therearselectorboxincorporatesthewarmairdispensers for the front occupant as well as the flange...

Page 119: ...rating Handbook US EXTRA330LX Table of Contents Paragraph Page SECTION 904 ACCELEROMETERTL 3424_EXT 904 1 GENERAL 904 3 904 2 LIMITATIONS 904 3 904 3 EMERGENCYPROCEDURES 904 3 904 4 NORMALPROCEDURES 904 3 904 5 PERFORMANCE 904 3 904 6 WEIGHT AND BALANCE 904 4 904 7 DESCRIPTION 904 4 ...

Page 120: ...Section 904 Accelerometer TL 3424_EXT 904 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 121: ...ntaccelerationvalues 2 displaying the minimum and maximum acceleration 3 recording of all acceleration and speed values into the long term memory 4 recording of any exceedance of limits 5 warning the pilot before reaching load limits by a sound to hear on the head set 6 indicating to the pilot when he has exceeded a load or speed limit by a sound on the head set and theG VLIMITSWARNINGLIGHTand 7 t...

Page 122: ... female The TL 3424_EXT is complete weight acceleration management The instrument incorporates a high precision sensor for measuring acceleration in the vertical axis The instrument also incorporates a sensor connected to the Pitot static system for measuring the indicated airspeed It is possible to download the measured values from the instrument via the serial cable RS 232c into a PC Pressing th...

Page 123: ... the exceeded acceleration The USER BUTTON is programmed in the main set up to display the minimum and maximum accelerationoverview MEMORY ThefollowingmemorytypesareincludedintheTL 3424_EXT 1 A long term memory storing the last recorded 30 minutes 20 000 lines entries every 0 1 seconds 2 A Scheck Report storing all cases of limit exceedance and the values in the immediate vicinity of this event 16...

Page 124: ...CONTROLLINGTHEINSTRUMENTVIANAV MENU There are black labels on the display Each is affiliated to the left and the right button The left label is for the Left button The right label is for the Right button Before pressing a button read the information on the label Its functions are different in every menu To store a value into the memory press both buttons simultaneously Release buttons when the set...

Page 125: ...ble of Contents Paragraph Page SECTION 905 EXTERNAL POWER 905 1 GENERAL 905 3 905 2 LIMITATIONS 905 3 905 3 EMERGENCY PROCEDURES 905 3 905 4 NORMAL PROCEDURES 905 3 905 5 PERFORMANCE 905 4 905 6 WEIGHT AND BALANCE 905 4 905 7 DESCRIPTION OF THE SYSTEM 905 4 905 8 HANDLING SERVICING AND MAINTENANCE 905 4 ...

Page 126: ...Section 905 External Power 905 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 127: ...EDURES Not affected 905 4 NORMAL PROCEDURES The following starting procedures are recommended however the starting conditions may necessitate some variation from these procedures 1 Perform Pre flight inspection 2 Set propeller governor control to High RPM position 3 Open throttle approximately 1 4 travel 4 Battery switch OFF 5 Alternator switch OFF CAUTION Risk of damage of electrical system due t...

Page 128: ... the external power plug from the board receptacle 905 5 PERFORMANCE Not affected 905 6 WEIGHT AND BALANCE Refer to the Equipment List in Section 6 of this Handbook 905 7 DESCRIPTION OF THE SYSTEM The external power receptacle with its spring loaded door is attached left under the seat and reachable from outside It is directly connected to the aircraft electrical system and does not feature an inv...

Page 129: ... Contents Paragraph Page SECTION 906 DIGITAL RPM INDICATOR 906 1 GENERAL 906 3 906 2 LIMITATIONS 906 3 906 3 EMERGENCYPROCEDURES 906 3 906 4 NORMALPROCEDURES 906 3 906 5 PERFORMANCE 906 3 906 6 WEIGHT AND BALANCE 906 4 906 7 DESCRIPTION AND OPERATION OF THE SYSTEM 906 4 906 8 HANDLING SERVICINGAND MAINTENANCE 906 6 ...

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Page 131: ...imitations are not affected by the installation of the P 1000 Digital RPM indicator The face of the indicator is placarded with the unchanged engine RPM operating range Additionally the operating RPM ranges are indicated by a large green yellow and a red LED These LEDs are located on the upper right corner of the indicator face ModelP100 230 635 00 max 2600RPM 906 3 EMERGENCYPROCEDURES Notaffected...

Page 132: ... of the engine rpm appears on the display The default display is insured via the use of internal timers that will restore the display to the current rpm even in the event that one of the panel buttons becomes stuck or defective Internally two independent tachometers watch the pulses received from each magneto Each tachometer is accurate to less than 1 rpm and can be individually enabled disabled v...

Page 133: ...indicator This small yellow indicator is illuminated when there is a difference of more than 50 rpm between the right and left tachometers This indicator also may flicker during extreme rpm excursions of the engine OPERATIONBUTTONS There are three panel buttons Each button has two modes of operation PRESS AND HOLD operation mode press and hold for more than 2 3 of a second Thisoperationmodeisplaca...

Page 134: ...y However a mechanism exists to mask either tachometer from the display leaving the remaining tachometer to determine magneto ignition problems Quickly pressing and releasing the left button L causes the tachometer to mask the left tachometer Quickly pressing and releasing the right button R causes the tachometer to mask the right tachometer Dimmer DIM Quickly pressing and releasing the middle but...

Page 135: ...Table of Contents Paragraph Page SECTION 907 SMOKE SYSTEM 907 1 GENERAL 907 3 907 2 LIMITATIONS 907 3 907 3 EMERGENCYPROCEDURES 907 3 907 4 NORMALPROCEDURES 907 4 907 5 PERFORMANCE 907 5 907 6 WEIGHT AND BALANCE 907 5 907 7 DESCRIPTION OF THE SYSTEM 907 5 907 8 HANDLING SERVICINGAND MAINTENANCE 907 7 ...

Page 136: ...Section 907 Smoke System 907 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 137: ...nditions have to be considered For the prevention of a fire alarm inform the flight control before you activate the smoke system 4 Recommended Manifold pressure min 20 Hg 5 The activation of the smoke system on ground is only allowable for a brief system test 6 Wearing a parachute is strongly recommended Operating Markings Placards 907 3 EMERGENCYPROCEDURES FAILUREOFTHESMOKE SYSTEM 1 Switch SMOKE ...

Page 138: ...4 NORMALPROCEDURES The smoke system includes features for refilling the smoke tanks and smoke generation A REFILL A separate refill hose is delivered with the smoke system which has to be used for filling the smoke oil tanks from the paraffin oil supply cansister or barrel 1 Refill hose CONNECT hose nipple to quick connector at the fuselage bottom IMMERSE the other end into the paraffin oil in the...

Page 139: ... to operate the smoke system only in forward flight because during reverse maneuvers for example tail slide smoke might enter the cockpit via the air vents 907 5 PERFORMANCE Notaffected 907 6 WEIGHTANDBALANCE Specific Weight of the paraffin oil 0 85 kg Litre N O T E The smoke system does not feature a capacity dipstick In the case of unknown filling the smoke oil tanks should be drained and refill...

Page 140: ...interconnected floptube smoke oil tank Filledtanksaredetectedbyafloatswitchplacedinthemainsmokeoiltankwhichshutsthepump off Thesamepump normalpolarity injectsthesmokeoilfromthefloptubesmokeoiltankthrough anoverpressure checkvalveandtheinjectornozzleintothehotexhaustgastogeneratesmoke The system consists of Main smoke oil tank with float switch Floptube smoke oil tank Refill Injection pump in the p...

Page 141: ...ines fittings tanks Check the smoke oil tanks for proper attachment Cleantheoverpressure checkvalve ifrequired removeoilresidue Clean the injector nozzle if required remove carbon debris Clean the filter element After each flight with activated Smoke System Clean the aircraft belly fairing and the rudder cables from smoke oil contamination N O T E The rudder cables might suffer from increased wear...

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Page 143: ...Contents Paragraph Page SECTION 908 SINGLE SEAT CANOPY 908 1 GENERAL 908 3 908 2 LIMITATIONS 908 3 908 3 EMERGENCYPROCEDURES 908 3 908 4 NORMALPROCEDURES 908 3 908 5 PERFORMANCE 908 3 908 6 WEIGHT AND BALANCE AND EQUIPMENT LIST 908 3 908 7 DESCRIPTION OF THE SYSTEM 908 3 908 8 HANDLING SERVICEAND MAINTENANCE 908 3 ...

Page 144: ...Section 908 Single Seat Canopy 908 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 145: ...area and ensure seat belts and shoulder harness of front seat are completely removed or fastened and secured so that nothing can obstruct the freemovementofcontrols 908 5 PERFORMANCE Notaffected 908 6 WEIGHTANDBALANCEANDEQUIPMENTLIST Refer to the equipment list in section 6 908 7 DESCRIPTIONOFTHESYSTEM The single seat canopy has been designed to easily replace the standard canopy This can be achie...

Page 146: ...Section 908 Single Seat Canopy 908 4 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 147: ...ELT 909 1 GENERAL 909 3 909 2 LIMITATIONS 909 3 909 3 EMERGENCYPROCEDURES 909 4 909 4 NORMALPROCEDURES 909 4 909 5 PERFORMANCE 909 4 909 6 WEIGHT CENTER OF GRAVITY 909 4 909 7 SYSTEM DESCRIPTION 909 5 909 7 1 Switch Operation 909 5 909 7 2 Self Test Mode 909 5 909 8 HANDLING SERVICINGAND MAINTENANCE 909 6 909 8 1 Transmitter Test 909 6 909 8 2 Self Test 909 6 ...

Page 148: ...Section 909 ARTEXME 406ELT 909 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA 330LX Left blank intentionally ...

Page 149: ...conandowner When the ELT is activated the buzzer beeps and the panel LED pulses periodically The time between pulses lengthen after a predetermined transmitter on time N O T E In October 2000 the International Cospas Sarsat Program announced at its 25th Council SessionheldinLondon UKthatitplanstoterminatesatelliteprocessingofdistresssignals from 121 5 and 243 MHz emergency beacons on February 1 20...

Page 150: ...ference Attempt contact with rescue aircraft with the radio transceiver set to a frequency of 121 5 MHz If no contact is established switch the remote switch to the ON position immediately If the function of the remote switch is in doubt proceed as follows Remove quick pins from the backrest adjustment and swivel the backrest forward to get access to the ELT unit Use the unit master switch at the ...

Page 151: ... of the ELT Care should be taken when transporting or shipping the ELT not to move the switch or allow packing material to become lodged such as to toggle the switch 909 7 2 SELFTESTMODE Upon turn off from ON back to ARM state the ELT automatically enters a self test mode that transmits a 406 MHz test coded transmission that monitors certain system functions before returningtothe ARM mode Thetrans...

Page 152: ...N Do not allow test duration to exceed 5 seconds A false alarm may be generated Any time the ELT is activated it is transmitting a 121 5 MHz distress signal After approximately 50 seconds a live 406 MHz distress signal is transmitted and is considered valid by the satellite system Whenever the ELT is switched from ON to ARM a 406 MHz signal is transmitted however it is specially coded as a self te...

Page 153: ...For this error code the ELT must be sent back for repairorreplacement 5Flashes Indicates that ELT has not been programmed or is incorrectly programmed Does notindicateerroneousorcorruptedprogrammeddata 6Flashes Indicates that the G switch loop between pins 5 and 12 at the D sub connector is not installed ELT will not activate during a crash Check that the harness D sub jumper is installed by verif...

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Page 155: ...TION 910 NATAA83 001 INTERCOM 910 1 GENERAL 910 3 910 1 1 Installation Adjustments 910 3 910 2 LIMITATIONS 910 3 910 3 EMERGENCYPROCEDURES 910 4 910 4 NORMALPROCEDURES 910 4 910 5 PERFORMANCE 910 4 910 6 WEIGHT AND BALANCE 910 4 910 7 SYSTEM DESCRIPTION 910 4 910 7 1 Controls and Indicators 910 4 910 7 2 Operation 910 6 910 7 3 Functions 910 7 ...

Page 156: ...910 2 Page Date 19 February 2014 Section 910 NAT AA83 001 Intercom Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 157: ...ance during VOX operation ApanelannunciatorallowseasyvisualsettingoftheVOXthreshold andalsoindicates transmit operation The AA83 001 provides full boom mic transmit and ICS functions for the pilot and copilot Pilot priority on transmit and pilot isolation fail safe direct connection to the aircraft radio system are standard features CAUTION Ensure headsets are of good quality and are installed cor...

Page 158: ...ating Handbook US EXTRA330LX 910 3 EMERGENCYPROCEDURES Not applicable 910 4 NORMAL PROCEDURES Not applicable 910 5 PERFORMANCE Not applicable 910 6 WEIGHT AND BALANCE Refer to the Equipment List in Section 6 of this Handbook 910 7 SYSTEM DESCRIPTION 910 7 1 CONTROLS AND INDICATORS ...

Page 159: ...er rear knob is the COPILOT VOX control that controls VOX for the copilot and passengers For full information on VOX operation see section 910 7 2 below ANNUNCIATOR The panel annunciator is a bi colour LED that shows intercom status IftheLEDisilluminatedgreen itindicatestransmitactivity andifitisred itindicatesVOXactivity For transmit with sidetone or mic activity it will illuminate amber The gree...

Page 160: ...he NORM mode default permits everyone on the system to talk to each other listen to music and hear all radio communications Radio transmit functions may be initiated by either the pilot or the copilot The pilot has priority In NORM mode external tie line users are included in the ICS communications PIL ISO PILOT ISOLATION OPERATION In normal operation the pilot and copilot hear the same signals fr...

Page 161: ...cations without requiring adjustment of the ICS Audio level All users are permitted to talk to each other listen to music and hear all radio communications There is provision for an external ICS tie line load to maintain the ICS audio at the same level as in NORM mode 910 7 3 FUNCTIONS RADIO FUNCTIONS TherearetwoPTTinputs oneeachforthepilotandcopilotonthecontrolstick Activationofeither PTT input c...

Page 162: ...ctivated Fail safemoderoutes the pilot s phones mic audio and mic PTT directly to the COM radio Duringtransmitmode thepilotmicisdirectlyconnectedtothetransceivermic Micbiasisprovided bythetransceiver nottheAA83 001 ThepilotTXkeylineisdirectlyconnectedtothetransceiver The sidetone audio is directly connected from the audio source to the pilot phones Duringreceivemode receiveaudioisdirectlyconnected...

Page 163: ...4 911 1 2 Switching on the unit pre flight check 911 4 911 1 3 Squawk selection 911 5 911 1 4 Flight operation in Mode A transponder reply code only 911 7 911 1 5 Flight operation in Mode A C reply code and altitude code 911 7 911 1 6 Squawk Ident 911 7 911 1 7 Test 911 7 911 1 8 Configuration Mode 911 8 911 2 LIMITATIONS 911 8 911 3 EMERGENCYPROCEDURES 911 8 911 3 1 Important Codes 911 8 911 4 NO...

Page 164: ...911 2 Page Date 19 February 2014 Section 911 BECKER ATC 4401 Transponder Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 165: ...ar Beacon System ATCRBS Its functionality includes replying to ATCRBS Mode A and Mode C interrogations It operates on radar frequencies receiving ground radar interrogations at 1030 MHz and transmitting a coded response of pulses to ground based radar on a frequency of 1090 MHz The ATC4401isequippedwithIDENTcapabilitythatactivatestheSpecialPositionIdentification SPI pulse N O T E The ATC 4401 owne...

Page 166: ... h t C A e d o M d n a A e d o M n I 8 1 x o r p p a r o f e d o c y l p e r A e d o M e h t o t l a n o i t i d d a e s l u p m i n o i t a c i f i t n e d i C L e h t f o e n i l m o t t o b e h t n i s r a e p p a t d I e m i t s i h t g n i r u D s d n o c e s y a l p s i d E y a l p s i d C L e n i l 2 e n i l p o t n o i t a c i d n i e d o C e l b i s s o p e r a 7 7 7 7 o t 0 0 0 0 m o r f...

Page 167: ...e right or the left The cursor appears only in the code display and is indicated by the flashing digit If no cursor is visible the first digit flashes after a clockwise rotation and thelastdigitafteracounter clockwiserotation WhenthecodeisbeingchangedintheON or ALT position the transponder temporarily switches to the standby mode The active time of the cursor and the rate of flashing can be change...

Page 168: ...theconfigurationmode Ifthesame button is again pressed within 3 seconds the previous code appears 2 Activation of the VFR codes a Press the VFR push button 1 or 2 F G The selected code is then displayed After 3 seconds the displayed code becomes activate and overwrites the previously set reply code b Pressing button F or G again within 3 seconds reactivates the previously set reply code N O T E Wh...

Page 169: ...e 2 Set mode switch A from SBY to ON The transponder immediality replies with the set code A triangle on the left next to the code signals the tranponder replies 911 1 5 FLIGHTOPERATIONINMODEA C REPLYCODEANDALTITUDECODE 1 Select squawk as described above 2 ATC requests the transmission alpha charlie or charlie switch the transponder to ALT using mode switch A 3 The transponder replies using the co...

Page 170: ...evaluation are tested on correct function in the SBY ON and ALT modes 4 In case of a failure appears the report e g E10 in the top line of the display Switch OFF the transponder at such E fault indications 911 1 8 CONFIGURATIONMODE The configuration Mode is used to set the unit on the ground and must not be called up in flight Refer to BECKER s Pilot s Guide for further information 911 2 LIMITATIO...

Page 171: ...he Unit pre flight check 912 4 912 1 3 Display 912 5 912 1 4 Squawk Selection 912 5 912 1 5 Squawk Ident 912 6 912 1 6 Selftests of the Unit BITs 912 6 912 1 7 Selection Mode 912 7 912 1 8 Flight Operation in Mode A C S reply code and altitude code 912 9 912 1 9 VFR CodeActivation 912 10 912 1 10 Configuration Mode 912 10 912 2 LIMITATIONS 912 10 912 3 EMERGENCYPROCEDURES 912 10 912 3 1 Important ...

Page 172: ...912 2 Page Date 19 February 2014 Section 912 BECKER BXP 6401 Transponder Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 173: ...ir Traffic Radar BeaconSystem ATCRBS ItsfunctionalityincludesreplyingtoATCRBSModeA CandModeS interrogations Itoperatesonradarfrequencies receivinggroundradarinterrogationsat1030MHzandtransmitting acodedresponseofpulsestoground basedradaronafrequencyof1090MHz TheBXP6401is equipped with IDENT capability that activates the Special Position Identification SPI pulse NOTE The BXP 6401 owner accepts all ...

Page 174: ...d o m y r a t o r s g n i t t e s e g n a h c o t h c t i w s y r a t o R n r u t r e p s p e t s 6 1 C n o t t u B n o t t u b h s u P B f o e d o m m o r f r o s g n i t t e s r o f t i g i d o t t i g i d m o r f p m u j o t h s u P t x e n e h t o t u n e m e n o y e k r e t n e n a s a d e s u y l l a r e n e g D T D I n o t t u b h s u P o t n o i t i d d a n i I P S r e i f i t n e d I l a ...

Page 175: ...CTION 1 Thetransponderremainsswitchedinthestandbymodeuntilrequestedbythegroundstation ATC to transmit a code e g squawk alpha 6426 2 Using the rotary switch B and the button C set the 4 digit code requested by ATC as follows a Usingswitch C movethecursortotheparticulardigit Digits0to7canthenbesetusingtherotary switch B N O T E S Whilst settings are taking place the transmission branch of the trans...

Page 176: ...LCdisplayduring this time 912 1 6 SELFTESTS OF THE UNIT BITS Thefollowingdifferenttestsareintegratedinthetransponderorcanbetriggeredatthetransponder 1 The IBIT Initiated Built in Test can be activated in any mode excluding the configuration mode withthepushof F and G atthesametime Theactionstartswiththeleadingedgeofthesecond pushed button The IBIT works as follows in all modes Theteststartswithall...

Page 177: ...ay starts immediately after finalisation of the PBIT Negativeresultsareindicatedonthedisplaywith FAILURE Thetranspondermaybenotswitched into ON or ALT mode if any failure was found The PBIT takes not longer than 1 second If the test was successful the XPDR switches immediately into the normal operating mode 912 1 7 SELECTIONMODE PressSELbutton G androtateencoder B forselection Inselectionmodeaddit...

Page 178: ...aracters with spaces 8 StorethechangeswithSTObutton F Forleavingthesettingprocedurewithoutstoring pushthe SEL button G N O T E Aircraft Identifier Flight Number consists of max 7 characters on the left hand side oriented No dashes or spaces shall be included If the FN con sists of less than 7 characters the remaining characters on the right side shall be filled with spaces SWITCHINGBACKTODEFAULTAI...

Page 179: ...for inversion 10 sec is introduced if no action happens Nothing stored as long as F is not pressed N O T E It is possible to leave the setting procedure with SEL button G at any time and normal mode is available then Indication SEL on the display changes back to mode indication If STO button F was not used no change has been stored 912 1 8 FLIGHTOPERATIONINMODEA C S REPLYCODEANDALTITUDECODE 1 When...

Page 180: ...wninthecodedisplayandthetransponder then switches back to the previously active code 912 1 10 CONFIGURATIONMODE The configuration mode is available from SBY mode only To get into configuration mode press button SEL G turn rotary encoder B until CFG appears in the bottom row of the display Refer to BECKER s Pilot s Guide for available options 912 2 LIMITATIONS Notapplicable 912 3 EMERGENCYPROCEDURE...

Page 181: ...ents Paragraph Page SECTION 913 GARMIN GTX 327 TRANSPONDER 913 1 GENERAL 913 3 913 1 1 Mode Selection Keys 913 3 913 1 2 Code Selection 913 4 913 1 3 Keys for other GTX 327 Functions 913 4 913 2 LIMITATIONS 913 6 913 3 EMERGENCYPROCEDURES 913 6 913 3 1 Important Codes 913 6 913 4 NORMALPROCEDURES 913 6 913 5 PERFORMANCE 913 6 ...

Page 182: ...Section 913 GARMIN GTX 327Transponder 913 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 183: ...range Range can be improved by climbing to a higher altitude It may be possible to minimize antenna shielding by locating the antenna where dead spots are only noticed during abnormal flight attitudes CAUTION The GTX 327 should be turned off before starting or shutting down aircraft engine TheGTX327TransponderispoweredonbypressingtheSTBY ALTorONkeys orbytheAVIONIC switch After power on a start up ...

Page 184: ...bers8and 9 are not used for code entry only for entering a Count Down time and in Configuration Mode IMPORTANTCODES 1200 The VFR code for any altitude in the US Refer to ICAO standards elsewhere 7500 Hijack code Aircraft is subject to unlawful interference 7600 Loss of communications 7700 Emergency 7777 Military interceptor operations Never squawk this code 0000 Military use Not enterable Care sho...

Page 185: ... the Count Down timer FUNC Changes the page shown on the right side of the display Displayed data includes Pressure Altitude Flight Time Count Up timer Count Down timer and may include Contrast and Display Brightness depending on configuration refer to the screen description below SCREEN DESCRIPTION PRESSURE ALT Displays the altitude data supplied to GTX 327 in feet hundreds of feets i e flight le...

Page 186: ...3 3 EMERGENCYPROCEDURES 913 3 1 IMPORTANTCODES 7600 Loss of communications 7500 Hijacking 7700 Emergency All secondary surveillance radar sites are ready to receive this code at all times See the Airman s Information Manual AIM for a detailed explanation of identification codes 913 4 NORMALPROCEDURES Notapplicable 913 5 PERFORMANCE Notapplicable ...

Page 187: ...ERAL 914 3 914 1 1 Mode Selection Keys 914 4 914 1 2 Code Selection 914 4 914 1 3 Keys for other GTX 328 Functions 914 5 914 1 4 Function Display 914 5 914 1 5 Configuration Mode 914 6 914 1 6 Altitude trend indicator 914 6 914 1 7 FailureAnnunciation 914 6 914 2 LIMITATIONS 914 7 914 3 EMERGENCYPROCEDURES 914 7 914 3 1 Important Codes 914 7 914 4 NORMALPROCEDURES 914 7 914 5 PERFORMANCE 914 7 ...

Page 188: ...Section 914 GARMIN GTX 328 Transponder 914 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 189: ...baro corrected altitude under non standard conditions The unit also features flight timers The Traffic Information Service TIS is not available in this installation N O T E TheGTX328owneracceptsallresponsibilityforobtainingtheproperlicensebeforeusing the transponder The coverage you can expect from the GTX 328 is limited to line of sight Low altitude or aircraft antenna shielding by the aircraft i...

Page 190: ...he transponder also respondstointerrogationsfromTCASequippedaircraft 914 1 2 CODESELECTION Codeselectionisdonewitheightkeys 0 7 providing4 096activeidentificationcodes Pushing one of these keys begins the code selection sequence Digits that are not yet entered appear as dashes The new code is activated when the fourth digit is entered Pressing the CLR Key moves the cursor back to the previous digi...

Page 191: ... and Display if manual control and backlighting is selected in the installation configuration START STOP Starts and stops the Count Up Count Down and Flight timers CRSR Initiates starting time entry for the Count Down timer and cancels transponder code entry CLR Resets the Count Up Count Down and Flight timers Cancels the previous keypress during code selection and Count Down entry Returns cursor ...

Page 192: ...ring installation configuration Contrast is controlled by the 8 and 9 keys DISPLAY Thispageisonlydisplayedifmanualbacklightingmodeisselectedduringinstallationconfiguration Backlighting is controlled by the 8 and 9 keys 914 1 5 CONFIGURATIONMODE The configurartion mode is not active TheGTX328 soptionsarenormallysetattimeofinstallation TorequestanychangesoftheGTX 328 parameters contact an authorized...

Page 193: ...14 3 EMERGENCYPROCEDURES 914 3 1 IMPORTANTCODES 7600 Loss of communications 7500 Hijacking 7700 Emergency All secondary surveillance radar sites are ready to receive this code at all times See the Airman s Information Manual AIM for a detailed explanation of identification codes 914 4 NORMALPROCEDURES Notapplicable 914 5 PERFORMANCE Notapplicable ...

Page 194: ...Section 914 GARMIN GTX 328 Transponder 914 8 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 195: ...ERAL 915 3 915 1 1 Mode Selection Keys 915 4 915 1 2 Code Selection 915 4 915 1 3 Keys for other GTX 330 Functions 915 5 915 1 4 Function Display 915 5 915 1 5 Configuration Mode 915 6 915 1 6 Altitude trend indicator 915 6 915 1 7 FailureAnnunciation 915 6 915 2 LIMITATIONS 915 7 915 3 EMERGENCYPROCEDURES 915 7 915 3 1 Important Codes 915 7 915 4 NORMALPROCEDURES 915 7 915 5 PERFORMANCE 915 7 ...

Page 196: ...Section 915 GARMIN GTX 330 Transponder 915 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 197: ...not agree with the aircraft s baro corrected altitude under non standard conditions The unit also features flight timers The Traffic Information Service TIS is not available in this installation N O T E TheGTX330owneracceptsallresponsibilityforobtainingtheproperlicensebeforeusing the transponder The coverage you can expect from the GTX 330 is limited to line of sight Low altitude or aircraft anten...

Page 198: ...SELECTION Code selection is done with eight keys 0 7 that provide 4 096 active identification codes Pushingoneofthesekeysbeginsthecodeselectionsequence Thenewcodewillnotbeactivated until the fourth digit is entered Pressing the CLR key will move the cursor back to the previous digit Pressing the CLR key when the cursor is on the first key of the code or pressing the CRSR key during code entry will...

Page 199: ... the display Displayed data includes Pressure Altitude Flight Time Count Up timer Count Down timers In the Configuration Mode steps through function pages START STOP Starts and stops the Count Up Count Down and flight timers In the Configuration Mode steps through functions in reverse CRSR InitiatesstartingtimeentryfortheCountDowntimerandcancelstranspondercodeentry Returns cursortolastcodedigitwit...

Page 200: ...t active CONTRAST This page is only displayed if manual contrast mode is selected in Configuration Mode Contrast is controlled by the 8 and 9 keys DISPLAY This page is only displayed if manual backlighting mode is selected on Configuration Mode Backlighting is controlled by the 8 and 9 keys 915 1 5 CONFIGURATION MODE The configuration is normally set at time of installation including the unique Mo...

Page 201: ... 3 EMERGENCYPROCEDURES 915 3 1 IMPORTANTCODES 7600 Loss of communications 7500 Hijacking 7700 Emergency All secondary surveillance radar sites are ready to receive this code at all times See the Airman s Information Manual AIM for a detailed explanation of identification codes 915 4 NORMAL PROCEDURES Not applicable 915 5 PERFORMANCE Not applicable ...

Page 202: ...Section 915 GARMIN GTX 330 Transponder 915 8 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 203: ...S 430W 916 1 GENERAL 916 3 916 2 LIMITATIONS 916 3 916 2 1 Placards 916 4 916 3 EMERGENCY ABNORMALPROCEDURES 916 4 916 3 1 Emergency Procedures 916 4 916 3 2 Abnormal Procedures 916 4 916 4 NORMALPROCEDURES 916 5 916 5 PERFORMANCE 916 5 916 6 WEIGHT CENTER OF GRAVITY 916 5 916 7 SYSTEM DESCRIPTION 916 5 916 7 1 Key and Knob Functions 916 5 916 7 2 Default Nav Page 916 7 ...

Page 204: ...Section 916 GARMINGNC420W GNS430W 916 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 205: ...oftwareversion3 0andisnot suitable for earlier software versions Some differences in operation may be observed when comparing the information in this supplement to later software versions Verify the information hereinwiththe400WSeriesPilot sGuide Reference P N190 00356 00applicableRevision you received with your unit There you will also find further information 916 2 LIMITATIONS The system must ut...

Page 206: ...te LOSSOFINTEGRITYMONITORING If Loss of Integrity Monitoring message is displayed revert to an alternate means of navigation appropriatetotherouteandphaseofflightorperiodicallycross checktheGPSguidancetoother approvedmeansofnavigation LOSS OF GPS SIGNAL DURING ACROBATICS When performing acrobatics the GPS signal can get lost 1 Reset switch OFF and ON the unit to regain the GPS signal SEARCHINGANEA...

Page 207: ...desired flight plan and press MENU to display the flight plan catalog options 4 Turn the large right knob to highlight Activate Flight Plan and press ENT 5 Press and hold the CLR key to open the default NAV page 916 5 PERFORMANCE Notaffected 916 6 WEIGHT CENTEROFGRAVITY Refer to the equipment list in Section 6 of this Handbook 916 7 SYSTEMDESCRIPTION 916 7 1 KEYANDKNOBFUNCTIONS LEFT HANDKEYSANDKNO...

Page 208: ...an entry Press and hold this key to immediatelydisplaytheDefaultNavigationPage regardlessofwhichpageiscurrentlydisplayed Theenterkey ENT isusedtoapproveanoperationorcompletedataentry Itisalsousedtoconfirm information such as during power on Thelargerightknobisusedtoselectbetweenthevariouspagegroups NAV WPT AUXorNRST With the on screen cursor enabled the large right knob allows you to move the curs...

Page 209: ...TheGNC420W GNS430WpowerandCOMvolumearecontrolledusingthepower volumeknob at the top left corner of the unit Turning it clockwise will turn unit power on and increase the COM radio volume After turning the unit on a welcome page will be displayed while the unit performs a self test followed by the database confirmation pages which show the current database informationontheNavDatacard withthevalidop...

Page 210: ...Section 916 GARMINGNC420W GNS430W 916 8 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 211: ...917 6 917 5 PERFORMANCE 917 6 917 6 WEIGHT CENTER OF GRAVITY 917 6 917 7 SYSTEM DESCRIPTION 917 6 917 7 1 General 917 6 917 7 2 Pitot Obstruction Monitor Configuration 5 only 917 6 917 7 3 Databases EFD1000 500 MFD Only 917 7 917 7 4 RSM GPS Usage 917 8 917 7 5 Operation on Internal Battery 917 8 917 7 6 Geographic Reservation 917 9 917 7 7 HazardAwareness EFD1000 PFD PRO and MFDs ONLY 917 9 917 7...

Page 212: ...Section 917 ASPENEFD1000 500System 917 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 213: ...D1000MFDcaninstantlyreverttoafully functionalflight display generated from ADAHRS data completely independent of that generated by the PFD The EFD1000 Pilot PFD is a Flight Display with Attitude indicator heading indicator and moving map The Pilot PFD cannot be installed with an EFD1000MFD TheEFD500isafullyfunctionalMFDwithallthecapabilityoftheEFD1000MFDexceptreversion HSI RemoteSensorModule RSM C...

Page 214: ...enequipmentforthe300LT Refer totheEquipmentListinSection6toverify whichconfigurationisactuallyinstalledinyouraircraft Figure 1 provides a block diagram of a complete EFD1000 500 System installation 917 2 LIMITATIONS This supplement does not grant approval for IFR operations The Aspen flight displays have been installed on a no hazard no credit basis Therefore the information provided by these inst...

Page 215: ...Section 917 ASPENEFD1000 500System Page Date 19 February 2014 917 5 Pilot s Operating Handbook US EXTRA330LX Figure1 EquipmentConfiguration ...

Page 216: ...ndicator Shouldoneorbothoftheselinesbecomeblocked suchasmightoccur duetoaninadvertenticingencounterorfromwatertrappedinthelines thenboththeEFD1000PFD and the EFD1000 MFD along with the primary indicators of airspeed and altitude could display erroneousairspeedandaltitudeinformation Furthermore becausetheEFD1000usespitotandstaticpressuresaspartoftheADAHRSattitude solution loss or corruption of the ...

Page 217: ... and will continue to detect obstructions in the pitot system that might occur However post landing the monitor remains active and as the airplane slows below 30 KIAS the systemwillpostaredXinplaceoftheattitudeandheadinginformationandpostthe CHECKPITOT HEAT message Inthiscircumstance restoringtheGPSsystem orcyclingpowertotheaffected EFD1000 will restore normal monitor operation In some acrobatic m...

Page 218: ...wer is removed or degraded Transitionthresholdsandtimeswillvaryasafunctionoftheinputvoltagetothedisplay which can be observed via the Menu Power Settings Page Database Type Includes Update Cycle Database Provider Limitations Terrain High resolution terrain data for Americas International or Worldwide geographic regions Terrain depiction is limited to the region between 65 deg N orth latitude to 65...

Page 219: ...etect this condition and compensate for the reduced magnetic fields The system can continue to operate for a short time without reference to magnetic North but must be able to periodically resolve the magnetic vector to continue operations IftheEFD1000isunabletoresolvetheearth smagneticfieldfortwominutes thesystemwillswitch to and annunciate Free Gyro Mode In this mode the ADAHRS continues to prov...

Page 220: ...te reference to the ownship position for navigation or maneuvering is prohibited The intended function of Aerodrome Moving Map Display AMMD is to help flight crew orient themselves on the airport surface and improve pilot positional awareness during taxi operations AMMD function is not sufficient to be used as the basis for maneuvering and shall not be used for navigation This application is limit...

Page 221: ...wledge this operational limitation by pressing either MODE SYNC knob EvolutionSyntheticVisionisacomputer generatedimageoftheexternalscenetopographyfrom theperspectiveoftheflightdeck derivedfromaircraftaltitude high precisionnavigationsolution and database of terrain obstacles and cultural features such as runways Evolution Synthetic Visioncreatesanimagerelativetoterrain obstaclesandairportswithint...

Page 222: ...ing System An annunciator willindicatethatTWSisinhibited TWScanbeinhibitedforallapplicationsexceptSyntheticVision by selecting SV ONLY When TWS is inhibited no terrain warning is provided Terrain obstaclecautionandwarningmessagesaregeneratedduetonearbyterrainorobstacles On a non precision approach a terrain caution or warning is probable depending on the rate of descenttowardtheterrain Landingsatm...

Page 223: ...Table of Contents Paragraph Page SECTION 919 LANDING LIGHT 919 1 GENERAL 919 3 919 2 LIMITATION 919 3 919 3 EMERGENCYPROCEDURES 919 3 919 4 NORMALPROCEDURES 919 3 919 5 PERFORMANCE 919 3 919 6 WEIGHT AND BALANCE 919 3 919 7 DESCRIPTION OF THE SYSTEM 919 3 919 8 HANDLING SERVICINGAND MAINTENANCE 919 4 ...

Page 224: ...919 2 Page Date 19 February 2014 Section 919 Landing Light Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 225: ...be integrated in the RH lower cowling 919 2 LIMITATION Nochange 919 3 EMERGENCYPROCEDURES Nochange 919 4 NORMALPROCEDURES Nochange 919 5 PERFORMANCE Nochange 919 6 WEIGHTANDBALANCE Refer to the Equipment List in section 6 of this Handbook 919 7 DESCRIPTIONOFTHESYSTEM The landing light is controlled by the LANDING LIGHT switch on the right instrument panel The system is protected by the LANDING LIG...

Page 226: ...919 4 Page Date 19 February 2014 Section 919 Landing Light Pilot s Operating Handbook US EXTRA330LX 919 8 HANDLING SERVICINGANDMAINTENANCE Nochange ...

Page 227: ...AIRTOWHOOK Table of Contents Paragraph Page SECTION 920AIRTOW HOOK 920 1 GENERAL 920 3 920 2 LIMITATIONS 920 3 920 3 EMERGENCYPROCEDURES 920 4 920 4 NORMALPROCEDURES 920 4 920 5 PERFORMANCE 920 5 920 6 WEIGHT AND BALANCE 920 7 920 7 DESCRIPTION OF THE SYSTEM 920 7 920 8 HANDLING SERVICINGAND MAINTENANCE 920 7 ...

Page 228: ...Section 920 Airtow Hook 920 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 229: ...aking piece weak links Length of the synthetic tow between 40 m 130 ft and 60 m 195 ft Ultimate load of the air tow max 850 kp 1875 lbs If tows with higher ultimate load are used a breaking piece weak links of max 850 kp 1875 lbs must be interconnected For a safe air towing the following points must be observed 1 seat 2 seats Max Takeoff Weight 820 kg 1813 lbs 870 kg 1924 lbs Max Empty Weight 701 ...

Page 230: ...ng PERFORM AS PRACTICAL 920 4 NORMALPROCEDURES Preflight inspection starting procedures take off procedure and the following climbing flight have to be carry out in accordance with Chapter 4 Normal procedure In addition to this procedures the following points have to be observed A PRIOR TO THE TAKE OFF A release test needs to be conducted to determine safe release operation The test shall be made ...

Page 231: ... grass dry and paved level runway no wind takeoff weight of the towing aircraft 820Kg 1808lbs Liftoff speed T O 68 KIAS 126 Km h indicated Obstacle clearance speed over 15m 50ft 74 KIAS 137 Km h indicated For every 5 kts 9 km h headwind the takeoff T O distance can be decreased by 5 For every 2 kts 4 km h tailwind up to 10 kts 19 km h the T O distance is increased by 10 CAUTION All values are vali...

Page 232: ...t m ft SL 176 577 287 942 196 643 320 1050 217 712 355 1165 240 787 393 1289 265 869 433 1421 291 955 476 1562 2000 610 205 673 334 1096 228 748 373 1224 253 830 414 1358 280 919 458 1503 309 1014 505 1657 340 1115 555 1821 4000 1219 239 784 391 1283 267 876 436 1430 296 971 484 1588 328 1076 535 1755 362 1188 591 1939 398 1306 650 2133 6000 1829 280 919 458 1503 313 1027 511 1677 347 1138 567 186...

Page 233: ...with m 600 kg 1323 lbs PA 0 C 32 F OAT 10 C 50 F 20 C 68 F 30 C 86 F ft m ft min m s ft min m s ft min m s ft min m s ___SL 1280 6 5 1210 6 1 1150 5 8 1080 5 5 1000 305 1210 6 1 1145 5 8 1080 5 5 1015 5 2 2000 610 1140 5 8 1080 5 5 1010 5 1 950 4 8 3000 914 1080 5 5 1005 5 1 940 4 8 880 4 5 4000 1219 1005 5 1 935 4 7 870 4 4 810 4 1 5000 1524 935 4 7 870 4 4 800 4 1 740 3 8 6000 1829 865 4 4 800 4...

Page 234: ...It is mounted at the tail spring rear end aft the tail wheel and activated with a yellow handle located at the rear seat cockpit via a bowden cable 920 8 HANDLING SERVICINGANDMAINTENANCE Service and maintenance needs to be conducted in accordance with the latest operation handbook Typ E 85 of the manufacturer TOST GmbH Germany Additionally during the 100 h inspection the bowden cable and the relea...

Page 235: ... EMERGENCY ABNORMALPROCEDURES 922 6 922 3 1 Emergency Procedures 922 6 922 3 2 Abnormal Procedures 922 6 922 4 NORMALPROCEDURES 922 7 922 5 PERFORMANCE 922 7 922 6 WEIGHT CENTER OF GRAVITY 922 8 922 7 SYSTEM DESCRIPTION 922 8 922 7 1 Touchscreen Key and Knob Functions 922 8 922 7 2 Secure Digital Card 922 9 922 7 3 Selecting com nav frequencies 922 9 922 7 4 Remote transponder operation 922 10 922...

Page 236: ...Section 922 GARMINGTN635 650 750 922 2 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

Page 237: ...sponder GTX 33 The GTN 650 750 also feature NAV functionality Additionally the GTN 750 can be used to display Charts and to control the optional GMA 35 remote audio panel Thissupplementiswrittenformainsoftwareversion2 00 GPSsoftwareversion4 0 COMsoftware version2 01andNAVsoftwareversion6 01andisnotsuitableforearliersoftwareversions Some differencesinoperationmaybeobservedwhencomparingtheinformatio...

Page 238: ...nd compatible databases must be installed and contain current data Thenavigationdataincl forfinalapproachsegmentsprovidedbytheGTNseries e g movingmap CDI depiction is for situational awareness only and should not be relied upon for navigation Do not use SafeTaxi or ChartView functions as the basis for ground maneuvering SafeTaxi and ChartViewaretobeusedforthepilottoorienthimselfontheairportsurface...

Page 239: ...o serve as a situational awareness tool only By itself it may not provideeithertheaccuracyorthefidelityonwhichtobasedecisionsandplanmaneuverstoavoid terrain or obstacles 922 2 4 TRAFFIC TISONLY TrafficmaybedisplayedontheGTNwhenconnectedtoanapprovedoptionalTIStrafficdevice This systemiscapableofprovidingtrafficmonitoringandalertingtothepilot Trafficshownonthedisplay mayormaynothavetrafficalertingav...

Page 240: ...S OF REMOTE AUDIO PANEL FUNCTIONS IF INSTALLED WITH GTN 750 PullINTERCOMcircuitbreaker N O T E This procedure will restore COM operation on the GTN 750 The intercom functions will not be available 922 3 2 ABNORMALPROCEDURES GPSNAVIGATIONINFORMATIONNOTAVAILABLEORINVALID IfGTN635 650 750GPSnavigationinformationisnotavailableorinvalidtheGTNwillenteroneof two modes Loss of Integrity LOI mode or Dead R...

Page 241: ...op of the list is the nearest airport To review the other nearest airports touch the Up and Down keys to scroll through the list 3 Touch the desired airport to select it The selected airport will be displayed in the Waypoint page 4 Touch the Activate key or press the small right knob to activate the selection 5 The Map page will now be displayed with the new Direct To course 922 4 NORMALPROCEDURES...

Page 242: ...inger in the desired direction Touchscreen keys are placed at the lower portion of the display The keys vary depending on the page selected Touch the key to perform the function or access the described information You can return to the previous page or exit the current function by touching the Back key KEYS QuicklyreturntotheHomepagebypressingtheHOMEkey PressandholdtheHOMEkeytoreach the Map page T...

Page 243: ...ke the NAV window active for editing The standby frequency in blue is active for editing Turn the large right knob to select the desired megahertz MHz value Turnthesmallrightknobtoselectthedesiredkilohertz kHz value Pressthesmall right knob to transfer the standby frequency to the active window USINGTOUCHSCREEN Touch the Standby window A pull down keypad will appear with the current Standby freque...

Page 244: ...aremotetransponder GTX33 canbecontrolledviatheGTN635 650 750unit Touch thetransponderwindowtoenterthetrnasponderoperationpage Seefigures3and4fortheGTN 6xx and the GTN 750 respectively IDENT 1 Touch the IDENT key once to reply with an identifying squawk code 2 The IDENT key text will change to green to indicate active Ident Figure 4 GTN 750 XPDR Operation ...

Page 245: ...ated ALTITUDEREPORTING 1 Touch the Altitude Reporting key for Mode C operation 2 The transponder will be On and will transmit its squawk code and altitude when interrogated An ALT annunciation will appear when the squawk code is transmitted VFR 1 Touch the VFR key to set the VFR squawk code 1200 or 7000 depending on location see below SELECTINGASQUAWKCODE Theselectedsquawkcodewillalwaysbeinuse Asy...

Page 246: ...acking capabilities of the ATC facility therefore care should be taken when making routine code changes N O T E WhenanAspenEFD1000PFDisinstalled itisusedastheencodedaltitudesource Donot power down the Aspen PFD while using the Garmin GTN 635 650 750 unit or the Garmin GTX 33 remote transponder 922 7 5 REMOTEAUDIOPANELOPERATION GTN750ONLY The remote audio panel GMA 35 can be operated from the GTN 7...

Page 247: ... selection off 3 Touch the Crew Intercom key to toggle activation of the Crew Intercom allowing the Pilot and Co Pilot to talk to each other 4 Touch the desired Pilot and Co Pilot Radio selections Figure 5 GTN 750 Audio Panel Operation 3 The selected Mic will be shown in the MIC window MONITOR 1 Monitor is automatically selected for the associated Com Mic Radio 2 Touch the Mon key to toggle betwee...

Page 248: ...uelch level automatically When enabled the Auto Squelch key will display a green bar 6 Touch the Squelch arrows to set the desired Squelch level 7 Touch the Back key to return to the Intercom Setup page 8 Touch the Music 1 or Music 2 keys to set their configuration 9 Select the recipients for Music Distribution by touching any combination of the Pilot and Co Pilot keys 10 Touch the Radio and or In...

Page 249: ... be used as an airport moving map display AMMD SafeTaxiandChartviewaretobeusedbytheflightcrewtoorientthemselvesontheairportsurface to improve pilot situational awarness during ground operations 922 7 9 TRAFFICDISPLAY OPTIONAL Traffic may be displayed on the GTN when connected to an approved TIS traffic device e g GTX 330orGTX33 TheTISinformationisonlyavailableintheUS TheGarminGTN6xxor7xxCockpit Re...

Page 250: ...Section 922 GARMINGTN635 650 750 922 16 Page Date 19 February 2014 Pilot s Operating Handbook US EXTRA330LX Left blank intentionally ...

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