Beechcfaft Bonanza D35 1994 Pilot'S Operating Handbook And Faa Approved Airplane Flight Manual Download

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Summary of Contents for Bonanza D35 1994

Page 1: ...f the pilot during all flight operations This handbook includes the material required to be furnished to the pilot by CAR 3 Airplane Serial Number This handbook supersedes all BEECH published owner s manuals flight manuals and check lists issued for this airplane with the exception of FAA Approved Airplane Flight Manual Supplements COPYRIGHT BEECH 1994 PIN 35 590061 7 Issued January 1977 P N 35 59...

Page 2: ...PUBLISHED BY COMMERCIAL PUBLICATIONS BEECH AIRCRAFT CORPORATION WICHITA KANSAS 67201 U S A i eechcraft AllaylheGnCompany Member of GAMA GeoeralAvla Manufaelurers ...

Page 3: ...l must be in the airplane for all ffight operations Part Number Subject Date 35 590061 7TC1 Fuel Selector Placard 8 26 97 Installation Note This page should be filed in the front of the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual immediately fol lowing the Title page This page replaces any Log of Temporary Changes page dated prior to the date in the lower right corner of thi...

Page 4: ...T SOPERATING HANDBOOK AND FAA APPROVED AIRPLANEFLIGHTMANUAL A4 Revision July 1994 LOGOF REVISIONS Page Description Title Page Updated Page A A4 New 10 1 thru Revised Section X Safety 10 48 lnfonnation May 1994 r PAGEA ...

Page 5: ...OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL A3 Revision October 1990 LOG OF REVISIONS Page Description Title Page Updated Page A A3 New 10 1 thru Revised Section X 10 48 Safety Information October 1990 PAGEA ...

Page 6: ...H 1987 LOG OF REVISIONS Page Description Title Page Update Page A A2 New 2 7 Revise WEIGHT AND CENTER OF GRAVITY 2 8 Revise CG LIMITS 2 20 Add WARNING Placard 6 1 Update Table of Contents 6 4 Shift Material 6 5 Add WARNING 6 6 Shift Material 6 8A 6 88 6 8C 6 8D Add SAMPLE LOADINGS Page A ...

Page 7: ...ok Revise NOTE Revise Revising the Handbook Add Airplane Flight Manual Supplements Revision Record Vendor Issued STC Supplements Shift Material and Add Wing Area Revise Approved Maneuvers Revise Placards Update Table of Contents Revise Landing Gear Manual Extension Revise Emergency Landing Revise Emergency i xifs Emergency Speed Reduction and Shift Material Update Table of Contents Revise Starting...

Page 8: ...TION OR REV OF REVISION Original Title Page Original A Page Original a and b Original 1 1 thru 1 16 Original 2 1 th ru 2 20 Original 3 1 th ru 3 1b Original 4 1 thru 4 12 Original 5 1 th ru 5 30 Original 6 1 thru 6 18 Original 7 1 thru 7 34 Original 8 1 th ru 8 46 Original Section IX SeeLog of Supplements Revision 10 1 thru 10 67 March 1981 IA Page A ...

Page 9: ...mportant to have SAFETY INFORMATION in a condensed form in the hands of the pilots The SAFETY INFORMATION should be read and studied Periodic review will serve as a reminder of good piloting techniques WARNING Use only genuine BEECHCRAFT or BEECHCRAFT approved parts obtained from BEECHCRAFT approved sources in connection with the maintenance and repair of Beech airplanes Genuine BEECHCRAFT parts a...

Page 10: ...art component or structural assembly even though originally manufactured by BEECHCRAFT unsuit able and unsafe for airplane use BEECHCRAFT expressly disclaims any responsibility for malfunctions failures damage or injury caused by use of non BEECHCRAFT approved parts TABLE OF CONTENTS SECTION I General SECTION II Limitations SECTION Ill Emergency Procedures SECTION IV Normal Procedures SECTION V Pe...

Page 11: ...nts 1 6 Airplane Three View 1 6B Descriptive Data 1 7 Engine 1 7 Propeller 1 7 Fuel 1 8 Oil Capacity 1 8 Weights 1 8 Cabin Dimensions 1 8 Baggage 1 8 Specific Loadings 1 9 General Airspeed Terminology and Symbols 1 9 Meteorological Terminology 1 11 Power Terminology 1 12 Engine Controls and Instruments 1 12 Airplane Performance and Flight Planning Terminology 1 13 Weight and Balance Terminology 1 ...

Page 12: ...Section I General 1 2 BEECHCRAFT Bonanza D35 INTENTIONALLY LEFT BLANK January 1977 ...

Page 13: ...ing Handbook and FAA Approved Airplane Flight Manual and or placards located in the airplane As a further reminder the owner and operator of this airplane should also be familiar with the Federal Aviation Regulations applicable to the operation and maintenance of the airplane and FAR Part 91 General Operating and Flight Rules Further the airplane must be operated and main tained in accordance with...

Page 14: ...t nec essary documents may be maintained for the safe and efficient operation of the BEECHCRAFT Bonanza The handbook has been prepared in loose leaf form for ease in maintenance and in a convenient size for storage The handbook has been arranged with quick reference tabs imprinted with the title of each section and contains ten basic divisions Section I Section II Section Ill Section IV Section V ...

Page 15: ...ed to the holder of this manual automatically 1 Original issues and revisions of Class I and Class II Service Instructions 2 Original issues and revisions of FAA Ap proved Airplane Flight Manual Supplements 3 Reissues and revisions of FAA Approved Airplane Flight Manuals Flight Handbooks Owner s Manuals Pilot s Operating Man uals and Pilot s Operating Handbooks This service is free and will be pro...

Page 16: ...010 BEECH AIRCRAFT CORPORATION EX PRESSLY RESERVES THE RIGHT TO SUPER SEDE CANCEL AND OR DECLARE OB SOLETE WITHOUT PRIOR NOTICE ANY PART PART NUMBER KIT OR PUBLICATION REF ERENCED IN THIS HANDBOOK The owner operator should always refer to all supplements whether STC Supplements or Beech Supplements for possible placards limi tations normal emergency and other opera tional procedures for proper ope...

Page 17: ...g of Revisions is a box containing a capital letter which denotes the issue or reissue of the handbook This letter may be suffixed by a number which indicates the numerical revision When a revision to any information in the handbook is made a new Log of Re visions will be issued All Logs of Revisions must be re tained in the handbook to provide a current record of ma terial status until a reissue ...

Page 18: ...the descriptive listing NOTE Upon receipt of a new or revised supplement compare the Log page just received with the existing Log page in the manual Retain the Log page with the latest date on the bottom of the page and discard the other log VENDOR ISSUED STC SUPPLEMENTS When a new airplane is delivered from the factory the handbook delivered with it contains either an STC Supple mental Type Certi...

Page 19: ...BEECHCRAFT Bonanza D35 INTENTIONALLY LEFT BLANK Revised March 1983 Section I General 1 6A ...

Page 20: ...I Section I General WING AREA 177 6 sq ft BEECH CRAFT BonanzaD35 32 9 7 8 t 9 1 2 r F 0 0 I 9 7 1 8 1 6B Revised March 1983 ...

Page 21: ...in the FAA Aircraft Specification A 777 or approved by Sup plemental Type Certificate PROPELLER Beech electrically controlled variable pitch two blade 88 inch diameter propeller with Beech pitch control motor and spinner The propeller uses a Beech 215 109 hub with 215 207 88 blades OR Beech electric constant speed two blade 88 inch di ameter propeller using Beech 215 107 hub and 215 207 88 blades ...

Page 22: ...allon or one 20 gallon auxiliary tank in stalled in the baggage compartment All of the capacity of the 10 gallon tank is usable The 20 gallon tank adds 19 gallons usable fuel to the system OIL CAPACITY The oil capacity is 10 quarts WEIGHTS Maximum Ramp Weight 2735 lbs Maximum Take Off Weight 2725 lbs Maximum Landing Weight 2725 lbs CABIN DIMENSIONS Length 6 ft 11 in Height 4 ft 2 in Width 3 ft 6 i...

Page 23: ...ere at sea level GS Ground Speed is the speed of an airplane relative to the ground IAS Indicated Airspeed is the speed of an airplane as shown on the airspeed indicator when corrected for instrument error IAS values published in this handbook assume zero instrument error KCAS Calibrated Airspeed expressed in knots KIAS Indicated Airspeed expressed in knots TAS True Airspeed is the airspeed of an ...

Page 24: ...eed is the maximum speed at which the landing gear can be safely extended or retracted VNE Never Exceed Speed is the speed limit that or Ve may not be exceeded at any time VNo Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air and then only with caution Vs Stalling Speed or the minimum steady flight speed at which the airplane is controllable Vso Stalli...

Page 25: ... that altitude OAT Outside Air Temperature is the free air static temperature obtained either from inflight temperature indications adjusted for instrument error and compressibility effects or ground meteorological sources Indicated Pressure Altitude The number actually read from an altimeter when the barometric sub scale has been set to 29 92 inches of mercury 1013 2 millibars Pressure Altitude J...

Page 26: ...power rating not limited by time Power recommended for cruise climb ENGINE CONTROLS AND INSTRUMENTS Throttle Control Mixture Control EGT Exhaust Gas Temperature Indicator 1 12 Used to control power by intro ducing fuel air mixture into the intake passages of the engine Settings are reflected by readings on the manifold pressure gage This control is used to set fuel to air ratio in all modes of ope...

Page 27: ...nstrated Crosswind Velocity MEA Route Segment GPH January 1977 The ratio of the change in height during a portion of a climb to the horizontal distance traversed in the same time interval The demonstrated crosswind velocity is the velocity of the crosswind com ponent for which adequate control of the airplane during take off and land ing was actually demonstrated during certification tests The val...

Page 28: ...o the center of gravity C G of an item The product of the weight of an item multiplied by its arm Moment divided by a constant is used to simplify bal ance calculations by reducing the number of digits The point at which an airplane would balance if suspended Its distance from the reference datum is found by dividing the total moment by the total weight of the airplane The arm obtained by adding t...

Page 29: ...tions Weight of a standard airplane including unusable fuel full operating fluids and full oil Standard empty weight plus optional equipment Weight of occupants cargo and baggage Difference between take off weight or ramp weight if applicable and basic empty weight Maximum weight approved for ground maneuvering It includes weight of start taxi and run up fuel Maximum weight approved for the start ...

Page 30: ...Section I General 1 16 BEECHCRAFT Bonanza035 INTENTIONALLY LEFT BLANK January 1977 ...

Page 31: ... Plant Instrument Markings 2 6 Oil Temperature 2 6 Oil Pressure 2 6 Tachometer 2 7 Cylinder Head Temperature 2 7 Manifold Pressure 2 7 Instrument Vacuum 2 7 Fuel Pressure 2 7 Weight and Center of Gravity 2 7 CG Limits Gear Down 2 8 Approved Maneuvers 2725 Pounds 2 8 Flight Load Factors 2725 Pounds 2 8 Required Equipment for Various Conditions of Flight 2 8 2 15 Fuel 2 16 Placards 2 16 2 20 January...

Page 32: ...Section II Limitations 2 2 BEECHCRAFT BonanzaD35 INTENTIONALLY LEFT BLANK January 1977 ...

Page 33: ...ed in any operation Maximum 139 160 140 161 Do not exceed Structural this speed Cruising except in smooth VNO or Ve air and then only with caution Maneuvering 113 130 114 131 Do not make full VA or abrupt control movements above this speed Maximum 91 105 92 106 Do not extend Flap flaps or operate Extensiory with flaps ex Extended tended above VFE this speed Maximum 109 125 110 127 Do not extend La...

Page 34: ...MPH 56 106 66 161 Yellow Arc 139 176 160 203 140 177 161 204 c I Red Line 176 203 177 The Airspeed Indicator is marked in CAS values I 0 204 SIGNIFICANCE Full Flap Operating Range Normal Operating Range Operate with caution only in smooth air Maximum speed for ALL operations r en CD 3 n I 0 0 en al mm om C I c C I 0 C w Cl I ...

Page 35: ...ved for this model Bonanza but not installed as original equip ment These are listed in the FAA Aircraft Specification A 777 or approved by Sup plemental Type Certificate Aviation Gasoline 80 87 red minimum grade or alternate grades 100LL blue or 100 130 green See Engine Manufacturer s Bulletin OIL Ashless dispersant oils must meet Continental Motors Corporation Specification MHS 24A Refer to APPR...

Page 36: ... 207 88 blades Diameter is maximum 88 in minimum 86 in Pitch settings at 33 in sta low 12 high not under 30 NOTE Other propellers are approved for this model Bonanza but not installed as original equipment These are listed in the FAA Aircraft Specification A 777 or approved by Supple mental Type Certificate POWER PLANT INSTRUMENT MARKINGS OIL TEMPERATURE Caution Yellow Radial 100 F 38 C Operating ...

Page 37: ...mum Red Radial 29 6 in Hg INSTRUMENT VACUUM Minimum Red Radial 3 75 in Hg Operating Range Green Arc 3 75 to 4 25 in Hg Maximum Red Radial 4 6 in Hg FUEL PRESSURE Minimum Red Radial 9 psi Operating Range Green Arc 11 to 15 psi Maximum Red Radial 15 psi WEIGHT AND CENTER OF GRAVITY Maximum Take off and Landing Weight 2725 lbs Maximum Ramp Weight 2735 lbs Zero Fuel Weight No Structural Limitation Max...

Page 38: ... Use slow deceleration Minimum fuel tor above maneuvers 10gallons each main tank Spins are prohibited FLIGHT LOAD FACTORS 2725 POUNDS 4 4G positive maneuvering load factor with flaps up 2 0G positive maneuvering load factor with flaps down REQUIRED EQUIPMENT FOR VARIOUS CONDITIONS OF FLIGHT Federal Aviation Regulations 91 3 a 91 24 91 25 91 32 91 33 91 52 91 90 91 97 91 170 specify the minimum num...

Page 39: ...equired Equipment Listing does not include obviously required items such as wings rudders flaps engine landing gear etc Also the list does not include items which do not affect the airworthiness of the aircraft such as galley equipment entertainment systems passenger convenience items etc However it is important to note that ALL ITEMS WHICH ARE RELATED TO THE AIRWORTHINESS OF THE AIRPLANE AND NOT ...

Page 40: ...0 CHAPTER 23 COMMUNICATIONS VHF communications system ATA 100 CHAPTER 24 ELECTRICAL POWER Battery DC generator VFR Day VFR Night FR Day FR Night Remarks and I or Exceptions Per FAR 91 33 Per FAR 91 33 1 1 1 1 1 1 1 1 r en CD 3 I 0 0 rn IJI IJI m om I i i l I lJ 0 c n en I ...

Page 41: ...guisher ATA 100 CHAPTER 27 FLIGHT CONTROLS Elevator trim tab indicator 1 1 1 1 1 1 1 1 1 1 Per Person or Per FAR 91 33 Pilot and copilot if installed Per FAR 91 52 Optional May be inoperative for ferry flight provided tabs are visually checked in the neutral position prior to take off and checked for full range of operation 1X1 IXI om m Ill C i l m C C a w en C 3 en Cl 0 d 0 0 en ...

Page 42: ...n fuel pump Fuel quantity indicator Fuel pressure indicator ATA 100 CHAPTER 30 ICE AND RAIN PROTECTION Pitot heater VFR Day VFR Night FR Day FR Night Remarks and I or Exceptions 2 2 2 2 May be inoperative providing flap travel is visually inspected prior to take off 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 r u CD 3 n I 0 I 0 I en a mm om I I I I 0 0 l w n CJ1 I ...

Page 43: ...and instrument lights Landing light Anti collision light Position light 1 1 2 2 1 1 3 1 1 2 2 1 1 3 May be inoperative provided op erations are continued only to a point where repairs can be ac complished Gear must be left down Do not retract gear with hand crank Lights must be operative Per FAR 91 33 Per FAR 91 33 a a o m s m m C ia c m C C tl w J CTI Tl 4 r 3 I 0 m 0 0 s s en ...

Page 44: ... speed Magnetic compass Attitude indicator Turn and slip indicator Directional gyro Clock Transponder Navigation equipment VFR Day VFR Night FR Day FR Night Remarks and I or Exceptions 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 Per FAR 91 24 91 90 91 97 Per FAR 91 33 r u a 3 I 0 I 0 s Ill g J g i m om sn I c n I c C l w JI 1 ...

Page 45: ...r Vacuum gage ATA 100 CHAPTER 77 ENGINE INDICATING INSTRUMENTS Engine tachometer ind Manifold pressure indicator ATA 100 CHAPTER 79 ENGINE OIL INSTRUMENTS Oil pressure indicator Oil temperature indicator 1 1 1 1 1 1 1 1 1 1 1 1 1 1 Per FAR 91 32 1 1 1 1 1 1 al al om i m Ill C I J Ii C C D CJ1 l r 3 Cl CD 0 e 0 0 I I Ill ...

Page 46: ...k is usable The 20 gallon tank adds 19 gallons usable fuel to the system Use auxiliary fuel in level flight only and do not use for take off or landing Use at least 10 gallons from left main tank before use of auxiliary fuel or right main tank When operating fuel selector feel for detent position Do not take off when Fuel Quantity Gages indicate in Yellow Band or with less than 10 gallons in each ...

Page 47: ... Pilot s Operating Handbook and FAA Approved Airplane Flight Manual P N 35 590061 7 Issued January 1977 or Subsequent D 3401 thru D 3698 The addition of a placard to the fuel selector to warn of the no flow condition that exists between the fuel selector detents Insert this temporary change into the D35 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual immediately following page 2...

Page 48: ...On The Face Of The Fuel Selector Valve For Those Airplanes In Compliance With S B 2670 WARNING POSITION SELECTOR IN DETENTS ONLY NO FUEL FLOW TO ENGINE BETWEEN DETENTS Approved 2of2 AC Jackson Raytheon Aircraft Company DOA CE 2 P N 35 590061 7TC1 August 26 1997 ...

Page 49: ... Tanks L H TANK 17 GAL USE 10 GAL FIRST OFF A I I 1 I H TANK 17 GAL __ AUX TANK 10 GAL USE SECOND LEVEL FLIGHT ONLY On Fuel Selector Valve On Airplanes Equipped With 20 Gal Auxiliary Fuel Tanks OFF A L H TANK 17 GAL 1 I H TANK USE 10 17 GAL GAL FIRST _ __ AUX TANK 20 GAL USE SECOND LEVEL FLIGHT ONLY January 1977 2 17 ...

Page 50: ...ANDLE IN REAR OF FOR 210 180 150 120 FRONT SEAT AND TURN STEER COUNTERCLOCKWISE AS FAR FOR 90 60 30 0 AS POSSIBLE 50 TURNS STEER On Electrical Control Panel PUSH TO RESET CIRCUIT BREAKERS PULL IN CASE OF FIRE On Inner Side Of Electrical Control Panel Door TO RELEASE FLARES 1 TURN ON MASTER CIRCUIT BREAKER SWITCH 2 TURN ON SELECTOR SWITCH TO RELEASE FLARES 2 18 PUSH TO RESET AUX FUEL PUMP CIRCUIT B...

Page 51: ...IN AIRPLANE FLIGHT MANUAL MAXIMUM CAPACITY 270 POUNDS On Storm Window CAS r CAUTION DO NOT OPEN ABOVE 145 MPH 126 KNOTS L _J Below Left and Right Openable Windows After Com pliance with BEECHCRAFT Service Instructions 1241 EMERGENCY EXIT LIFT LATCH PULL PIN PUSH WINDOW OUT On Openable Windows DO NOT OPEN IN FLIGHT L _J Revised March 1983 2 19 I ...

Page 52: ...SPINS PROHIBITED NO ACROBATIC MANEUVERS APPROVED EXCEPT THOSE LISTED IN THE AIRPLANE FLIGHT MANUAL _J On Auxiliary Wobble Pump Handle I EMERGENCY FUEL PUMP In Full View on Inside of Cabin Door and on Inside of Baggage Compartment Door WARNING THISAIRPLANE IS EASILY LOADED BEYOND AFTCGLIMITS WEIGHT ANDCGMUST BEWITHIN LIMITS FOR EACH FLIGHT REFER TO PILOTS OPERATING HANDBOOK 2 20 March 1987 ...

Page 53: ...ine Failure 3 4 Discrepancy Checks 3 4 Air Start Procedure 3 5 Engine Fire Flight 3 6 Emergency Descent 3 6 Maximum Glide Configuration 3 6 Landing Gear Manual Extension 3 6 Landing Gear Retraction After Practice Manual Extension 3 7 Emergency Landing 3 8 Gear Up Landing 3 8 Unlatched Door In Flight 3 8 Emergency Exits 3 9 Generator Out Procedure 3 9 Spins 3 9 Induction System Icing 3 9 Emergency ...

Page 54: ...Section Ill Emergency Procedures BEECHCRAFT Bonanza D35 INTENTIONALLY LEFT BLANK 3 2 January 1977 ...

Page 55: ...r in the operation of the airplane Where practicable the emergencies requiring immediate corrective action are treated in check list form for easy reference and familiari zation Other situations in which more time is usually per mitted to decide on and execute a plan of action are discussed at some length ENGINE FIRE GROUND 1 Mixture IDLE CUT OFF 2 Fuel Selector Valve OFF 3 Battery Generator and I...

Page 56: ...ust be made ENGINE MALFUNCTION IN FLIGHT ENGINE FAILURE The most probable cause of engine failure would be loss of fuel flow or improper functioning of the ignition system DISCREPANCY CHECKS Rough running engine loss of engine power loss of fuel flow etc 1 Rough Running Engine a Mixture FULL RICH then lean as required b Ignition Switch CHECK on BOTH position 2 Loss of Power 3 4 a Fuel Pressure Gag...

Page 57: ...ng altitude d Select nearest landing site follow emergency landing procedures AIR START PROCEDURE a Mixture IDLE CUT OFF b Fuel Selector Valve OFF for a few seconds to clear engine then TO MAIN TANK MORE NEARLY FULL NOTE If the failure was due to the fuel metering valve sticking in the full open position the car buretor will deliver an excess of fuel with constant flooding Shutting off fuel momen ...

Page 58: ...erator and Ignition Switches OFF Extending the landing gear can be accomplished manually if desired 5 Do not attempt to restart engine EMERGENCY DESCENT 1 Power IDLE 2 Propeller HI RPM 3 Landing Gear DOWN 4 Airspeed ESTABLISH 110 kts 127 mph MAXIMUM GLIDE CONFIGURATION 1 Landing Gear UP 2 Flaps UP 3 Cowl Flaps CLOSED 4 Propeller LO RPM 5 Airspeed 105 KTS 121 MPH Glide distance is approximately 1 7...

Page 59: ...ank strapped or stowed in the disengaged position when not in use Do not retract the landing gear manually WARNING Do not operate the landing gear electrically with the handcrank engaged as damage to the mechanism could occur After emergency landing gear extension do not move any landing gear controls or reset any switches or circuit breakers until airplane is on jacks as failure may have been in ...

Page 60: ...ted landing spot 1 Throttle CLOSED 2 Mixture IDLE CUT OFF 3 Battery Generator and Ignition Switches OFF 4 Fuel Selector Valve OFF 5 Keep wings level during touchdown 6 Get clear of the airplane as soon as possible after it stops UNLATCHED DOOR IN FLIGHT If the cabin door is not locked it may come unlatched in flight This may occur during or just after take off The door will trail in a position app...

Page 61: ...failure may be indicated by the ammeter When a generator failure occurs in flight all non essential electrical load should be discontinued to conserve the battery life SPINS Spins are prohibited If a spin is entered inadvertently Immediately move the control column full forward and simultaneously apply full rudder opposite to the direction of the spin continue to hold this control position until r...

Page 62: ...r buretor icing is indicated c Apply carburetor heat immediately until icing conditions no longer exist Use high power set tings and lean mixtures to produce maximum heat under possible icing conditions EMERGENCY SPEED REDUCTION In an emergency the landing gear may be used to create additional drag Should disorientation occur under instru ment conditions the lowering of the landing gear will reduc...

Page 63: ...s for Safe Operation 4 3 Preflight Inspection 4 3 Before Starting 4 6 Starting 4 6 Before Takeoff 4 7 Take Off 4 9 Climb 4 9 Cruise 4 9 Descent 4 9 Before Landing 4 10 Shutdown 4 11 Cold Weather Operation 4 11 leing Conditions 4 11 Engine Break in Information 4 11 Revised March 1983 4 1 ...

Page 64: ...Section IV Normal Procedures BEECHCRAFT Bonanza 035 INTENTIONALLY LEFT BLANK 4 2 January 1977 ...

Page 65: ...ach Maximum Demonstrated Crosswind PREFLIGHT INSPECTION 1 CABIN a Parking Brake SET b Control Lock REMOVE c All Switches OFF 63 kts 73 mph 68 kts 78 mph 90 kts 104 mph 69 kts 79 mph 104 kts 120 mph 114 kts 131 mph 63 kts 73 mph 63 kts 73 mph 17 kts 20 mph d Emergency Locator Transmitter ARMED 2 RIGHT FUSELAGE a Baggage Compartment Door SECURE b Static Pressure Button UNOBSTRUCTED 3 EMPENNAGE a Con...

Page 66: ...emove Cover c Landing Light CHECK d Fuel Tank CHECK QUANTITY Filler Cap SECURE e Cabin Air Intake CHECK f Tie Down and Chocks REMOVE 7 LEFT LANDING GEAR a Wheel Well Door Tire and Strut CHECK b Fuel Vent CHECK c Fuel Sump DRAIN d Fuel Selector Valve Sump DRAIN Cover SECURE 8 NOSE SECTION a Left Cowl Flap CHECK b Engine Oil CHECK See Servicing Section 8 Cap and Dipstick SECURE c Left Cowl SECURE d ...

Page 67: ...uel Sump DRAIN c Wheel Well Door Tire and Strut CHECK 10 RIGHT WING LEADING EDGE a Cabin Air Intake CHECK b Tie Down and Chocks REMOVE c Fuel Tank CHECK QUANTITY Filler Cap SECURE d Landing Light CHECK 11 RIGHT WING TRAILING EDGE a Position Light CHECK b Wing Tip CHECK c Aileron CHECK d Flap CHECK CAUTION NEVER TAXI IF ANY STRUT IS FLAT January 1977 4 5 ...

Page 68: ...OFF 10 Ignition Switch BATTERY 11 Fuel Quantity Indicators CHECK QUANTITY WARNING Do not take off if gages indicate in yellow arc or with less than 10 gallons in each main tank 12 Activate the selector valve several times by rotating the handle from tank to tank to ensure that the se lector valve is free 13 Fuel Selector Valve SELECT LEFT MAIN TANK STARTING CAUTION Vernier type engine controls sho...

Page 69: ... for more than 30 seconds in any 4 minute period 7 Primer Brief shots until engine starts firing NOTE If starting fuel pressure is low maintain pres sure with auxiliary wobble fuel pump until pressure stabilizes 8 In the Event of Overprime Condition a Mixture IDLE CUT OFF b Throttle OPEN c Starter Button PRESS d As engine starts reduce throttle to IDLE and advance mixture to FULL RICH 9 Oil Pressu...

Page 70: ...Section IV Normal Procedures BEECHCRAFT Bonanza035 INTENTIONALLY LEFT BLANK 4 6B Revised March 1983 ...

Page 71: ...1200 rpm within two minutes with no additional electrical equip ment on If not turn off the battery and gen erator switches and do not take off 13 Avionics Equipment AS REQUIRED 14 Lights AS REQUIRED BEFORE TAKEOFF 1 Parking Brake SET 2 Seat Belts and Shoulder Harnesses CHECK NOTE All reclining seats must be in the upright posi tion during takeoff 3 Avionics CHECK 4 Engine Instruments CHECK 5 Flig...

Page 72: ... to the Take Off position full right 9 Magnetos CHECK at 1600 rpm Drop should not ex ceed 75 rpm on either magneto and should be within 50 rpm of each other 10 Carburetor Heat CHECK and return to COLD 11 Trim SET a Aileron NEUTRAL if installed b Elevator 0 3 nose down for aft loading 12 Flaps Check operation then UP 13 Door and Windows SECURE 14 Flight Controls CHECK PROPER DIRECTION FULL TRAVEL A...

Page 73: ...blished 4 Airspeed ESTABLISH DESIRED CLIMB SPEED when clear of obstacles 5 Propeller 2300 rpm CLIMB Climb Full Throttle 2300 rpm 1 Engine Temperatures MONITOR 2 Power SET AS DESIRED CRUISE See Cruise Power Setting Tables SECTION V 1 Cowl Flaps CLOSED 2 Power SET 3 Mixture ADJUST DESCENT 1 Power SET AS DESIRED Avoid prolonged idle set ting and low cylinder head temperatures 2 Mixture Enrich as requ...

Page 74: ...icing conditions are indicated carburetor heat may be carried however less power will be available for a go around 6 Landing Gear DOWN and CHECK Maximum extension speed 110 kts 127 mph 7 Flaps DOWN Maximum extension speed 92 kts 106 mph 8 Airspeed ESTABLISH NORMAL LANDING APPROACH SPEED 9 Propeller a Manual Hold to HI RPM until maximum is attained b Automatic Propeller Control APC Select AUTO CLIM...

Page 75: ...ixture IDLE CUT OFF 9 Ignition Switch OFF after engine stops 10 Battery and Generator Switches OFF 11 Control Lock INSTALL if conditions warrant 12 Install wheel chocks and release brakes if the airplane is to be left unattended COLD WEATHER OPERATION See Section 7 Systems ICING CONDITIONS Flight in Known Icing Conditions Prohibited ENGINE BREAK IN INFORMATION See Section 7 Systems January 1977 4 ...

Page 76: ...Section IV Normal Procedures BEECHCRAFT Bonanza D35 INTENTIONALLY LEFT BLANK 4 12 January 1977 ...

Page 77: ...e Conversion C vs F 5 12 ISA Conversion 5 13 Stall Speeds Power Idle 5 14 Wind Components 5 15 Take Off Distance 5 16 Climb 5 17 Cruise Climb 5 18 Cruise Power Settings 5 19 5 22 75 MCP Or Full Throttle 5 19 65 MCP Or Full Throttle 5 20 55 MCP Or Full Throttle 5 21 45 MCP Or Full Throttle 5 22 Cruise Speeds 5 23 Manifold Pressure vs RPM 5 24 Fuel Flow vs Brake Horsepower 5 25 Range Profile 53 Gall...

Page 78: ...SectionV Performance BEECHCRAFT BonanzaO35 TABLE OF CONTENTS Continued SUBJECT PAGE Endurance Profile 34 Gallons 5 29 Landing Distance 5 30 5 2 January 1977 ...

Page 79: ...e detailed below All examples and calculations utilize the following conditions CONDITIONS At Denver Outside Air Temperature 15 C 59 F Field Elevation 5330 ft Altimeter Setting 29 60 in Hg Wind 270 at 10 kts Runway 26L length 10 01 O ft Route of Trip DEN V81 AMA For VFR Cruise at 11 500 feet ROUTE MAGNETIC DIST SEGMENT COURSE NM DEN COS 161 55 COS PUB 153 40 PUB TBE 134 74 TBE DHT 132 87 DHT AMA 1...

Page 80: ...d subtract 100 feet from field elevation for each 1 in Hg above 29 92 Pressure Altitude at DEN 29 92 29 60 32 in Hg The pressure altitude at DEN is 320 feet above the field elevation 5330 320 5650 ft Pressure Altitude at AMA 29 92 29 56 36 in Hg The pressure altitude at AMA is 360 feet above the field elevation 3605 360 3965 ft NOTE For flight planning the difference between cruise altitude and cr...

Page 81: ...75 percent or 65 percent maximum continuous power The temperatures for cruise are presented for a standard day ISA 20 C 36 F above a standard day ISA 20 C and 20 C 36 F below a standard day ISA 20 C These should be used for flight planning The IOAT values are true temperature values which have been adjusted for the compressibility effects IOAT should be used for setting cruise power while enroute ...

Page 82: ...FLOW TAS FEET IN HG GPH KNOTS IN HG GPH KNOTS 10000 20 1 9 84 145 20 1 9 52 145 12000 18 6 9 19 142 18 6 8 91 141 Interpolate for 11 500 feet and the temperature for the appropriate route segment Results of the interpolations are 5 6 MAN FUEL ROUTE PRESS FLOW TAS SEGMENT IN HG GPH KNOTS DEN PUB 19 0 9 31 142 PUB TBE 19 0 9 23 142 TBE DHT 19 0 9 10 142 DHT AMA 19 0 9 09 142 NOTE The preceding are e...

Page 83: ...COS PUB 40 169 PUB TBE 74 127 TBE DHT 87 130 DHT AMA 65 133 FUEL TIME AT USED CRUISE FOR ALTITUDE CRUISE HRS MIN GAL 0 12 1 9 0 14 2 2 0 35 5 4 0 40 6 1 0 29 4 4 Distance required to climb has been subtracted from segment distance TIME FUEL DISTANCE TIME FUEL DISTANCE ITEM HRS MINS GAL NM Start Runup Taxi and Take off acceleration 0 00 1 7 0 Climb 0 11 2 2 21 Cruise 2 10 20 0 300 Total 2 21 23 9 3...

Page 84: ...he fuel required for the trip from the ramp weight Assumed ramp weight 2735 lbs Estimated fuel from DEN to AMA 23 9 gal 6 lbs gal 143 lbs Estimated landing weight 2735 143 2592 lbs Examples have been provided on the performance graphs The above conditions have been used throughout Rate of climb was determined for the initial cruise altitude conditions COMMENTS PERTINENT TO THE USE OF PERFORMANCE G...

Page 85: ...ide lines to the next known item 3 Indicated airspeeds IAS were obtained by using the AIRSPEED CALIBRATION Graph 4 The associated conditions define the specific conditions from which performance parameters have been determined They are not intended to be used as instructions 5 The full amount of usable fuel is available for all approved flight conditions January 1977 5 9 ...

Page 86: ... I I I I I I I I I I I I I I I I I I I I I I I I 70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 230 IAS INDICATEDAIRSPEED MPH 200 190 180 170 160 150 140 C ci 130 120 s o 100 5 90 80 70 60 IAS FLAPS C AS FLAPS DOWN 70 KNOTS 81 MPH DOWN 69 KNOTS 79 MPH 60 70 80 90 100 110 120 130 IAS INDICATED AIRSPEED KNOTS I I tI I I I I I I I I I I I I I I 70 80 90 100 110 120 130 140 150 IAS INDIC...

Page 87: ... I I I I I I I I I I I I I I 70 80 90 100110120130140150160170180190200210220230 IAS INDICATEDAIRSPEED MPH ti 10 0 10 1 zO Q 20 t u we 30 8 E 40 a o 50 u lii 60 70 80 IAS 70 KNOTS 81 MPH FLAPS DOWN INDICATED PRESSURE ALTITUDE 4500 FT ALTIMETER CORRECTION 9 FT ACTUAL PRESSURE ALTITUDE 14500 91 4491 FT FLAPS DOWN 50 60 70 80 90 100 110 120 130 140 AS INDICATED AIRSPEED KNOTS t I I I I I I I I I I I ...

Page 88: ...SectionV Performance lP i BEECHCRAFT BonanzaD35 t j tt J _c 2 rtimtttt ili iE S L I _ _ 0 0 0 0 g I 0 S33ij 30 5 12 Jimuary 1977 ...

Page 89: ...4 1 IT c I I 1111 oC I 11J Iw1 o c I n1111 I I 1 i J I 1 fff ll 1 ITT l 1111 J II ff f 1 ifi f c I j U rrf 1 h l f_ f t J L o _ o IH t l t SectionV Performance J t l 9Z l09 O 1S J J i P _ 0 1 T j _ 1 I l i ti l 0 u 00 Iw a 0 f a w 00 lw I g I iil I f L33 3an t1 L1v 31 nss31ld January 1977 5 13 ...

Page 90: ...NORMAL STALL RECOVERY TECHNIQUE MAY BE USED 2800 2600 2400 2200 WEIGHT POUNDS w z EXAMPLE WEIGHT FLAPS ANGLE OF BANK STALL SPEED 90 100 111111111111111 C w w w w 0 o rn rn J J 60 70 rn rn 60 50 50 40 10 20 30 40 50 60 ANGLE OF BANK DEGREES 2525 LBS UP 30 CAS 59 KNOTS 68 MPH IAS 60 KNOTS 169 MPH ti r n CD CD n 0 i 0 3 i g n CD a a m om i C Ill I C Ill D C l JI I ...

Page 91: ...EXAMPLE WIND SPEED ANGLE BETWEEN WIND DIRECTION AND FLIGHT PATH 20 KTS 50 HEADWIND COMPONENT CROSSWIND COMPONENT FLIGHT PATH 20 0 z 10 20 1 110 150 r 1so0 W1so 0 I I I 0 10 140 130 I I 20 CROSSWIND COMPONENTS January 1977 I I 13 KTS 15KTS I I I_ goo 100 Jl_j__j__j_J 11 o0 120 t H 1 I I 30 40 KNOTS 5 15 ...

Page 92: ... OAT PRESSURE ALTITUOE TAKE OFF WEIGHT HEAD WIND COMP GROUND ROLL TOTAL DISTANCE OVER A 50 FT OBSTACLE TAKE OFF SPEED AT LIFT OFF 50 FT l5 C 59 FJ 5650 FT 2725 LBS 9 5 KNOTS 1325 FT 2350FT I 68 KNOTS 78 MPH c c II t w w 0 cf t Jw t J ft 1 s y ffi ffi IJ LI 0 w w a a ltf A o 0 vD 40 30 20 10 0 10 20 30 40 50 2600 2400 2200 2000 0 10 20 30 0 50 I OUTSIDE AIR TEMPERATURE rv C I I I I I I I I I I I II...

Page 93: ...000 6000 8000 19000 60 50 40 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMPERATURE C t I I I I I I I I I I I I I I I I I I I I I 2600 80 60 40 20 0 20 40 60 80 100 120 OUTSIDE AIR TEMPERATURE rv F E35 KCH OAT PRESSURE ALTITUDE WEIGHT RATE OF CLIMB CLIMB GRADIENT CLIMB SPEED 1500 1400 1300 1200 1100 1000 900 I 800 700 600 i 500 15 14 13 12 11 10 9 8 7 6 I 400 300 200 100 2ko 221 00 2000 WEIGHT POUNDS 5...

Page 94: ...20 40 60 80 100 120 OUTSIDE AIR TEMPERATURErv F f EXAMPLE OAT AT TAKE OFF OAT AT CRUISE AIRPORT PRESSURE ALTITUDE CRUISE PRESSURE ALTITUDE INITIAL CLIMB WEIGHT TIME TO CLIMB 18 7 FUEL TO CLIMB 3 6 1 4 DISTANCE TO CLIMB 34 13 ffl 1 _ v1 f 0 10 20 30 40 TIME TO CLIMBrvMINUTES _ _ t I I I I I I I I I I I 0123456 7 FUEL TO CLIMBrvGALLONS _ _ t I I I I I I I I I I I I I I 0 10 20 30 40 50 607080 DISTAN...

Page 95: ...PH KTS MPH SLI 261 312150 I23 5167 0111 2113711581162l 1712150 124 2167 0111 2114011611198l3712150 I24 8167 0111 21143l165 2000 19 7 2150 23 1 67 011 2 140 161 55 13 2150 23 8 67 011 2143 165 91 33 2150 24 4 67 011 2 146 168 12 11 2150 22 7 67 011 2 142 163 48 9 2150 23 4 67 011 2145 167 84 29 2150 24 0 67 011 2 148 170 NOTES 1 FULL THROTTLE MANIFOLD PRESSURE SETTINGS ARE APPROXIMATE 2 SHADED AREA...

Page 96: ...4000 12 11 2150 20 6 58 0 9 7 133 153 48 9 2150 21 1 58 0 9 7 136 157 84 29 6000 5 15 2150 20 2 58 a 9 7 136 157 41 5 2150 20 7 58 0 9 7 139 160 77 25 8000 2 19 2150 19 9 58 0 9 7 138 159 34 1 2150 20 4 58 0 9 7 NOTES 1 FULL THROTTLE MANIFOLD PRESSURE SETTINGS ARE APPROXIMATE 2 SHADED AREA REPRESENTS OPERATION WITH FULL THROTTLE ISA 36 F 20 C ENGINE MAN FUEL SPEED PRESS FLOW RPM IN HG PPH GPH 2150...

Page 97: ... 5 1950 19 6 50 5 8 4 8000 3 19 1950 18 7 50 5 8 4 128 147 33 1 1950 19 2 50 5 8 4 10000 10 23 1950 50 5 8 4 129 148 26 3 1950 18 8 50 5 8 4 NOTES 1 FULL THROTTLE MANIFOLD PRESSURE SETIINGS ARE APPROXIMATE 2 SHADED AREA REPRESENTS OPERATION WITH FULL THROTILE TAS KTS MPH 122 140 124 143 126 145 128 147 130 150 132 ISA 36 F 20 C ENGINE MAN FUEL OAT ISPEED PRESS FLOW oF oc RPM IN HG PPH GPH 98 36 19...

Page 98: ...7 1 113 130 33 0 1950 16 7 42 3 7 1 115 132 69 20 1950 15 8 42 3 7 1 114 131 26 4 1950 16 2 42 3 7 1 116 134 62 16 1950 15 4 42 3 7 1 115 132 18 8 1950 15 8 42 3 7 1 116 134 55 13 1950 14 9 42 3 7 1 116 134 11 11 1950 15 4 42 3 7 1 117 135 47 9 1950 14 1 42 3 7 1 117 135 4 15 1950 14 9 42 3 7 1 117 135 40 5 1 FULL THROTTLE MANIFOLD PRESSURE SETTINGS ARE APPROXIMATE 2 SHADED AREA REPRESENTS OPERATI...

Page 99: ...50 RPM TEMPERATURE STANDARD DAY HSAJ tu w LL 2 w Cl I 5 w a fJ fJ LU a a 16000 15000 14000 13000 12000 11000 10000 9000 8000 7000 6000 5000 4000 3000 2000 1000 SL 100 January 1977 TRUE AIRSPEED 142 KNOTS I 11 y 0 t IL IL IL J J J Q f lt lt lt i l I f a a a 0 l 0 lt lt a C rv a 1 a rv c c Ill Ill QJ 0 1 QJ Ill I 110 120 130 140 150 TRUE AIRSPEED rv KNOTS 5 23 ...

Page 100: ...0 MANIFOLD PRESSURE vs RPM 1800 RECOMMENDED VALUES OF MANIFOLD PRESSURE AND RPM FOR CRUISE POWER SETTINGS 1900 2000 2100 ENGINE SPEED RPM 2200 ENGINE SPEED 2150 RPM MANIFOLD PRESSURE 19 IN HG WITHIN RECOMMENDED LIMITS 2300 0 C CD CD i n 0 0 3 I g n CD IJJ IJJm om I I I i l I 0 C l w en I ...

Page 101: ...15 14 J 13 w ii 12 11 10 9 8 6 FUEL FLOW vs BRAKE HORSEPOWER 65 55 EXAMPLE BRAKEHORSEPOWER 120 25 65 MCP CONDITION LEVEL FLIGHT CRUISE LEAN FUEL FLOW 9 7 GAL HR CRUISE 70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 230 BRAKE HORSEPOWER January 1977 5 25 ...

Page 102: ... WITH 45 MINUTES RESERVE FUEL AT 45 MCP Q l EXAMPLE PRESSURE ALTITUDE 11500 FT POWER SEITING FULL THAOTILE 2150 RPM RANGE 678 NM f 5 10000 R 1 i 133 116 CRUISETRUE i O AIRSPEEDrv KNOTS Cl N v I I_C LJJ l w a CJ CJ 5000 w a C SL 1 1 t1 tait 1 ta tfl 147 141 130 115 Ii fJ fJ _88 e I 500 JI145__ h1 j 126 112 0 s i 1401 i 132 122 bt 109 I I I I I 550 600 650 700 750 800 RANGE rv NAUTICAL MILES ZEROWIN...

Page 103: ...L FUEL LOADING 34 U S GAL 204 LBS 20000 f w w 15000 u 2 w 0 10000 w a en en 5000 w a a SL I I I 250 300 RANGE INCLUDES START TAXI AND CLIMB WITH 45 MINUTES RESERVE FUEL AT 45 MCP Q POWER SETIJNG FULL THROTILE 2150RPM RANGE 389 NM 116 CRUISE TRUE AIRSPEEDrvKNOTS 132fl2J09 rr 1 1 I I I I I 350 400 450 500 550 600 650 RANGErvNAUTICAL MILES ZERO WIND mm om i m m a z m 0 u l en ti I rn 0 Cl 3 I 0 I I g...

Page 104: ...OTE ENIJURANCE INCLUDES START TAXI AND CLIMB WITH 45 MINUTES RESERVE FUEL AT 45 MCP EXAMPLE PRESSUREAl TITUDE 11500 FT POWER SETIING FULL THROTILE 2150 RPM ENDURANCE 4 8 HRS 4 HRS 48 MIN w Q 5 10000 C tt 1111111111111 I 142 1tt133 116 CRUISE TRUE AIRSPEED rv KNOTS w a ffl 5000 a CL SL 3 5 z sl u a w _ 0 0 e CL I 4 0 I I 140 4 5 5 0 5 5 6 0 6 5 7 0 7 5 8 0 ENDURANCE rv HOURS o rn CD CD i 0 0 3 s CD...

Page 105: ...0 w a CJ CJ 5000 w a 0 SL I I I I 1 0 1 5 2 0 STANDARD DAY ISA NOTE ENDURANCE INCLUDES START TAXI AND CLIMB WITH 45 MINUTES RESERVE FUEL AT 45 MCP EXAMPLE PRESSUREALTITUDE 11500 FT POWER SETTING FULL THAOTILE 2150 RPM ENDURANCE 2 8 HAS 2 HAS 4B MIN CRUISE TRUE AIRSPEED KNOTS J S v 47i141 130 115 Q ti112 o I blii109 tj 2 5 3 0 3 5 4 0 ENDURANCE HOURS 4 5 m g _ l 5 0 al al om s m m n s c n C a w l 0...

Page 106: ... z l l i r 73 71 69 6B 67 OAT PRESSUREALTITUDE WEIGHT WIND COMPONENT GROUND ROLL TOTAL OVER 50 FT OBSTACLE APPROACH SPEED z u z ffilffi i It C I I I I I I I I I I I I 40 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMPERATUAE C 2600 2400 2200 2000 0 10 20 30 t I I I I I I I I I I I I I I I I I 40 20 0 20 40 60 80 100 120 OUTSIDEAIA TEMPERATURE F WEIGHTrvPQUNDS WIND COMPONENT rvKNOTS 25 C 77 FJ 3965 FT 2...

Page 107: ...g Form 6 7 Weight and Balance Loading Form 6 8 Sample Loadings 6 8A Dimensional and Loading Data 6 9 Seating Baggage and Equipment Arrangements 6 9 Useful Load Weights and Moments 6 10 6 13 Occupants 6 10 Baggage 6 10 Cargo 6 11 Usable Fuel 6 11 Oil 6 12 Auxiliary Usable Fuel 6 12 Moment Limits vs Weight Table 6 13 6 16 Center of Gravity Chart 6 17 Basic Empty Weight and Balance Form 6 18 March 19...

Page 108: ...Section VI Wt and Bal Equip List BEECH CRAFT Bonanza D35 INTENTIONALLY LEFT BLANK 6 2 January 1977 ...

Page 109: ...elage Station 76 0 The remainder of the unusable fuel to be added to a drained system is 34 5 pounds at Fuselage Station 79 1 and 3 pounds at Fuselage Station 133 0 for airplanes with 20 gallon auxiliary fuselage tank installed 3 Engine oil must be at the full level or completely drained Total engine oil when full is 22 pounds at Fuselage Station 36 1 Includes 3 pounds un drainable oil 4 To determ...

Page 110: ...eel reactions will be approximately at Fuselage Station 96 7 for main wheels and Fuselage Station 12 7 for the nose wheel 7 Jack point weighings are accomplished by placing scales at the jack points specified in step 1 above Since the center of gravity of the airplane is forward of Fuselage Station 83 1 the tail reaction of the airplane will be in an up direction This can be measured on regular sc...

Page 111: ...the aft seats and compartments It is the responsibility of the airplane operator to ensure that the airplane is properly loaded At the time of delivery Beech Aircraft Corporation provides the necessary weight and balance data to compute individual loadings All subse quent changes in airplane weight and balance are the re sponsibility of the airplane owner and or operator The basic empty weight and...

Page 112: ...he SUB TOTAL Ramp Condition 5 Subtract the fuel to be used for start taxi and take off to arrive at the SUB TOTAL Take off Condition 6 Subtract the weight and moment of the fuel in the incremental sequence in which it is to be used from the take off weight and moment The Zero Fuel Condi tion the Take Off Condition and the Landing Condi tion moment must be within the minimum and maxi mum moments sh...

Page 113: ... 6 CARGO 7 SUB TOTAL ZERO FUEL CONDITION 2072 8 FUEL MAIN 34 GAL 204 153 FUEL AUX 10 GAL 60 79 9 SUB TOTAL RAMP CONDITION 2735 2304 10 LESS FUEL FOR START TAXI AND TAKE OFF 10 8 11 SUB TOTAL TAKE OFF CONDITION 2725 2296 12 LESS FUEL LEFT MAIN 15 GAL 90 68 13 SUB TOTAL 2635 2228 14 LESS FUEL AUX 10 GAL 60 79 15 SUB TOTAL 2575 2149 16 LESS FUEL MAIN 10 GAL 60 45 17 LANDING CONDITION 2515 2104 Fuel f...

Page 114: ...REAR SEAT OCCUPANTS 4 BAGGAGE 5 CARGO 6 CARGO 7 SUB TOTAL ZERO FUEL CONDITION 8 FUEL MAIN GAL FUEL AUX GAL 9 SUB TOTAL RAMP CONDITION 10 LESS FUEL FOR START TAXI AND TAKE OFF 11 SUB TOTAL TAKE OFF CONDITION 12 LESS FUEL LEFT MAIN GAL 13 SUB TOTAL 14 LESS FUEL AUX GAL 15 SUB TOTAL 16 LESS FUEL MAIN GAL 17 LANDING CONDITION Fuel for start taxi and take off is normally 10 lbs at an average mom 100 of...

Page 115: ... following sample loadings show some of the problems associated with loading the aft seats and compartments Similar loadings should be made for your airplane Follow the loading instructions in the Pilot s Operating Handbook plus those on the sample loading form March 1987 6 BA ...

Page 116: ...ft use the position in which that seat is locat ed during flight The Basic Empty Weight Data shall be current and accurate for the airplane as equipped NOTE The addition of fuel to the above loading will move the cen ter of gravity C G forward Conversely using fuel during flight will move the airplane center of gravity aft Flight safety requires that during flight the airplane weight and center of...

Page 117: ...t and Balance Section for the latest occupant positions If the seats are ad justable fore and aft use the position in which that seat is locat ed during flight The Basic Empty Weight Data shall be current and accurate for the airplane as equipped NOTE The addition of fuel to the above loading will move the cen ter of gravity C G forward Conversely using fuel during flight will move the airplane ce...

Page 118: ...or the latest occupant positions If the seats are adjustable fore and aft use the position in which that seat is located during flight The Basic Empty Weight Data shall be current and accurate for the airplane as equipped NOTE The addition of fuel to the above loading will move the cen ter of gravity C G forward Conversely using fuel during flight will move the airplane center of gravity aft Fligh...

Page 119: ...EQUIPMENT ARRANGEMENTS PILOT F S F PASS 86 w I I E3 c i R SEAT t FS 108 PASS 116 I Fs 139 t FS 135 IJ MAXIMUM WEIGHT 270 POUNDS INCLUDING EQUIPMENT AND BAGGAGE B MAXIMUM WEIGHT 200 POUNDS FORWARD OF REAR SPAR INCLUDING EQUIPMENT AND CARGO WITH REAR SEAT REMOVED MAXIMUM WEIGHT 270 POUNDS AFT OF REAR SPAR INCLUDING EQUIPMENT AND CARGO WITH REAR SEAT REMOVED January 1977 6 9 ...

Page 120: ...70 80 90 100 110 120 130 140 6 10 Front Seat ARM 86 MOM 100 103 112 120 129 138 146 155 163 172 BAGGAGE ARM 139 Moment 100 Weight 14 150 28 160 42 170 56 180 69 190 83 200 97 210 111 220 125 230 139 240 153 250 167 260 181 270 195 Rear Seat ARM 116 MOM 100 139 151 162 174 186 197 209 220 232 Moment 100 208 222 236 250 264 278 292 306 320 334 347 361 375 January 1977 ...

Page 121: ...ight 100 Weight 100 20 22 20 27 40 43 40 54 60 65 60 81 80 86 80 108 100 108 100 135 120 130 120 162 140 151 140 189 160 173 160 216 180 194 180 243 200 216 200 270 220 297 240 324 260 351 270 364 USABLE FUEL MAIN WING TANKS ARM 75 Moment Gallons Weight 100 5 30 22 10 60 45 15 90 68 20 120 90 25 150 112 30 180 135 34 204 153 January 1977 6 11 ...

Page 122: ...AGE TANK With this item installed baggage and fuel shall not exceed 258 pounds Moment Gallons Weight 100 5 30 38 10 60 76 20 GALLON AUXILIARY BAGGAGE TANK With this item installed baggage aft of fuel tank sh a 11 not exceed 160 pounds Baggage and fuel shall not exceed 250 pounds Moment Gallons Weight 100 5 30 40 10 60 79 15 90 119 20 120 158 6 12 January 1977 ...

Page 123: ...ake off 83 2 84 3 or landing 2500 lb 80 1 85 4 2240 lb or less 76 5 85 4 Minimum Maximum Moment Moment Weight 100 100 2000 1530 1708 2010 1538 1717 2020 1545 1725 2030 1553 1734 2040 1561 1742 2050 1568 1751 2060 1576 1759 2070 1584 1768 2080 1591 1776 2090 1599 1785 2100 1607 1793 2110 1614 1802 2120 1622 1810 2130 1629 1819 2140 1637 1828 2150 1645 1836 2160 1652 1845 2170 1660 1853 2180 1668 18...

Page 124: ...14 1913 2250 1724 1921 2260 1735 1930 2270 1746 1939 2280 1757 1947 2290 1768 1956 2300 1779 1964 2310 1789 1973 2320 1800 1981 2330 1811 1990 2340 1822 1998 2350 1833 2007 2360 1845 2015 2370 1856 2024 2380 1867 2033 2390 1878 2041 I 2400 1889 2050 2410 1900 2058 2420 1911 2067 2430 1923 2075 2440 1934 2084 2450 1945 2092 2460 1957 2101 2470 1968 2109 2480 1979 2118 2490 1991 2126 6 14 January 19...

Page 125: ...14 2142 2520 2025 2150 2530 2037 2157 2540 2048 2164 2550 2060 2171 2560 2072 2179 2570 2083 2186 2580 2095 2193 2590 2107 2200 2600 2118 2208 2610 2130 2215 2620 2142 2222 2630 2154 2229 2640 2165 2236 2650 2177 2244 2660 2189 2251 2670 2201 2258 2680 2213 2265 2690 2225 2272 I 2700 2237 2279 2710 2249 2287 2720 2261 2294 2725 2267 2297 January 1977 6 15 ...

Page 126: ...this it is suggested that a running tally of equipment changes and their effect on empty weight and e g is a suitable means for meeting both requirements The current equipment list and empty weight and e g information must be retained with the airplane when it changes ownership Beech Aircraft Corporation cannot maintain this information the current status is known only to the owner If these papers...

Page 127: ... r N N 0 0 l N 8 8 tj N N Section VI Wt and Bal Equip List CXl CXl r CXl 2 CXl tj LO l CXl 0 CXl LL tj 0 CXl I LL CXl w N I u CXl z CXl I 0 CXl a 0 r LL 0 CXl a r w r I z r l w co u r r l 0 0 or 0 0 0 N 0 N N N saNnOd NI 1H813M January 1977 6 17 ...

Page 128: ...PRESSED 13 1 97 AFT 271 0 Signature REACTION SCALE NET WHEEL JACK POINTS READING TARE WEIGHT ARM MOMENT LEFT MAIN RIGHT MAIN NOSE OR TAIL TOTAL AS WEIGHED Space below provided for additions and subtractions to as weighed condition EMPTY WEIGHT DRY ENGINE OIL 22 795 UNUSABLE FUEL 36 79 2844 WITH FUSELAGE AUX TANK INSTALLED 3 133 399 BASIC EMPTY WEIGHT en I Ill n C 0 tD II c C c iii tD tD m om II r ...

Page 129: ...ts 7 7 Baggage Compartment 7 7 Flight Controls 7 8 Control Surfaces 7 8 Control Column 7 8 Rudder Pedals 7 8 Trim Control 7 9 Control Column Lock Pin 7 9 Wing Flaps 7 9 Control Switch 7 9 Position Indicators 7 9 Instrument Panel 7 10 Power Plant Description 7 11 Engine 7 11 Engine Instruments 7 11 Cluster Type Engine Instruments 7 11 Manifold Pressure and Tachometer 7 14 Engine Controls 7 14 Throt...

Page 130: ...el Quantity 7 21 Auxiliary Wobble Fuel Pump 7 21 Electric Primer 7 21 Fuel Tank Selection 7 22 Switching Fuel Tanks 7 22 Fuel Required for Flight 7 23 Landing Gear System 7 23 Control Switch 7 23 Position Indicators 7 24 Safety Switch 7 24 Warning Horn 7 24 Circuit Breaker 7 24 Manual Extension 7 25 Brakes 7 25 Ground Control 7 25 Electrical System 7 26 Battery 7 26 External Power Receptacle 7 26 ...

Page 131: ...ting and Ventilation System 7 29 Cabin Heating 7 29 Heater Operation 7 29 Cabin Ventilation 7 30 Cabin Fresh Air Outlets 7 30 Exhaust Vents 7 30 Air Conditioner 7 30 Pitot and Static System 7 31 Vacuum System 7 31 Stall Warning Indicator 7 32 Cold Weather Operation 7 32 Preflight Inspection 7 32 Engine Break in Information 7 33 January 1977 7 3 ...

Page 132: ...Section VII Systems Description BEECHCRAFT Bonanza D35 INTENTIONALLY LEFT BLANK 7 4 January 1977 ...

Page 133: ...o a recess in the door to create a flat aerodynamically clean surface To open the door from the outside lift the handle from its recess and pull until the door opens To close the cabin door from the inside observe that the door handle is in the unlocked position In this position the latch handle is free to move approximately one inch in either direction before engagement of the locking mechanism T...

Page 134: ... Only On Ground I Release latch front of bar pull bar at the bottom of the window out and upward Window will open approximately two inches To Close Window Pull inward and down on the bar at the bottom of the window Resistance will be felt as the bar moves downward Continue moving bar downward to its lowest position Check that bar is locked by the latch 7 6 NOTE Window is to be closed before and du...

Page 135: ...ibed on a placard installed below the left and right openable windows SEAT ADJUSTMENTS The front seat backs are adjustable to three positions The controls for the seat backs are levers located on the in board side of both seat backs To adjust positions lean for ward to relieve pressure on the seat back pull up on the lever and lean back to the first position Repeat the pro cedure moving the lever ...

Page 136: ...Section VII Systems Description BEECHCRAFT BonanzaD35 INTENTIONALLY LEFT BLANK 7 68 Revised March 1983 ...

Page 137: ... for pulling the door closed In the standard seating arrangement the two front seats have sockets for attaching large neck pillow style headrests SHOULDER HARNESS AND SEAT BELTS The shoulder harness is standard equipment on all seats The BEECHCRAFT Bonanza has quick release seat belt buckles which are easily adjusted and fastened The nylon webbing in colors complementing the upholstery is strong l...

Page 138: ... The throw over type control column for elevator and aileron control can be placed in front of either front seat Pull the T handle latch at the back of the control arm and position the control wheel as desired Check for full freedom of movement after repositioning the control The optional dual control column is required for flight instruction RUDDER PEDALS To adjust the rudder pedals press the spr...

Page 139: ...e control column tube assembly 3 Ensure positive retention of the lock pin by positioning the attached red plate on top of the throttle and propeller controls WING FLAPS The flaps are raised and lowered electrically by jackscrew actuators driven through flexible shafts from a single motor and gearbox under the front seat CONTROL SWITCH The flaps are controlled by a three position switch on the lef...

Page 140: ...panels which provide a compact circuit breaker group on the right side and switch panels on both sides Standard instrumentation on the Bonanza includes an airspeed indicator altimeter and electric turn and bank indicator mounted in the instrument panel magnetic compass mounted on the windshield divider a clock mounted in the instrument panel and outside air thermometer at the top of the divider In...

Page 141: ...l 5122D and above six cylinder horizontally opposed engine rated at 205 horsepower at 2600 rpm for take off max 1 min and 185 hp at 2300 rpm maximum continuous operation ENGINE INSTRUMENTS The engine instruments include cylinder head temperature oil temperature oil pressure indicators tachometer manifold pressure fuel pressure and fuel quantity indicators and an ammeter CLUSTER TYPE ENGINE INSTRUM...

Page 142: ... 6 7 8 9 10 11 rnrn CD I I I I I en n N CD 3 g en c CD oO en n s o I 0 rrif I I 711 0 0 1 1 0 _JJJ mTI CD CD m om I C II c C II c C J 13534 3 332 31 30 29 28 27 26 25 24 23 22 21 20 19 18 17 16 15 14 13 12 W T1 JI I ...

Page 143: ...24 Propeller Control Switch 8 Landing Gear Indicator Lights 25 Primer Opt 9 Instrument Lights 26 Auto Propeller Control APC Knob Opt 10 Landing Gear Switch 27 Mixture Control 11 Landing Light Switch Left 28 Starter Switch 12 Spare 29 Carburetor Heat 13 Nav Lights Switch 30 Flap Switch 14 Generator Switch 31 Cowl Flaps Control 15 Battery Switch 32 Flap Switch Lock 16 Landing Light Switch Right 33 R...

Page 144: ...TLE MIXTURE AND PROPELLER The push pull throttle and mixture controls are located on the control console These controls are released for repositioning by pushing a button on the knob With the button extended fine adjustments on the throttle are accomplished by rotating the knob clockwise to increase and counterclockwise to decrease Do not rotate clockwise with control fully advanced On the mixture...

Page 145: ...ng the engine cowling by opening the access door on the left upper cowl and the level should be checked after each flight using the dipstick fastened to the filler cap The normal oil operating level should be maintained at 8 to 10 quarts Both oil pumps the oil screen and a check valve to pre vent oil from draining from the tank into the engine sump are incorporated in the engine accessory section ...

Page 146: ...o Clo w I W J z ii IL W l a w o O o J ul I w 0 u a I Cl I 1 z I i 0 a C w zw Cl I zu w sure During possible icing conditions any such drop should be investigated immediately To check for carburetor ice in possible icing conditions a Note manifold pressure then apply full car buretor heat Manifold pressure will drop slightly Do not correct for this drop 7 1 6 January 1977 ...

Page 147: ...n type momentary on switch located on the left of the control column To energize the starter circuit rotate the ignition switch to the BATT position then press the starter button To energize the starter circuit for engine ignition rotate the ignition switch to the BOTH position before pressing the starter button Both procedures require that the subpanel battery switch be turned on PROPELLER Beech ...

Page 148: ...o the left of the throttle To select propeller rpm the switch is held in the increase or decrease rpm position until the desired rpm is obtained then the switch is returned to the center OFF position An optional governor which electronically controls the pro peller pitch change motor may be installed The governor changes the propeller blade angle with variations in load or engine output to maintai...

Page 149: ...located in the wings just outboard of the fuselage Usable fuel of each 20 gallon main tank is 17 gallons Fuel is fed from the cells to a selector valve just forward of the front seat on the left side then through a strainer to the fuel pump and the engine The fuel tank fillers are located in the wing leading edges CAUTION Do not allow bladder fuel cells to remain completely empty for any length of...

Page 150: ...ystems Description BEECH CRAFT Bonanza D35 FUEL SYSTEM SCHEMATIC TO ENGINE AUXILIARY WOBBLE FUEL PUMP c i DRAIN I VAPOR RETURN LINE FROM CARBURETOR 7 20 LEFT MAIN BAGGAGE COMPART MENT J DRAIN RIGHT MAIN January 1977 ...

Page 151: ... are sensors in each fuel tank connected to the switches and indicator The fuel level of the fuselage auxiliary cell may be read by switching the auxiliary fuel gage selector switch on the subpanel to Aux position AUXILIARY WOBBLE FUEL PUMP A manually operated pump incorporated with the fuel selector valve provides pressure for starting and emergency operation if the engine driven pump should fail...

Page 152: ...yellow band or with less than 10 gallons of fuel in each main tank SWITCHING FUEL TANKS When switching fuel tanks if one tank is allowed to run completely dry it may be necessary to place the mixture control to Full Rich position and maintain fuel pressure with the Auxiliary Wobble Fuel Pump to aid in restarting the engine Close the throttle as necessary to prevent engine overspeed on starting As ...

Page 153: ...ne must be approximately level for visual inspection of the tank If the pilot is not sure that at least 10 gallons are in each tank add necessary fuel so that the amount of fuel will be not less than 10 gallons per tank at takeoff Plan for an ample margin of fuel for any flight LANDING GEAR SYSTEM CAUTION Never taxi with a flat strut The landing gears are operated through adjustable linkage connec...

Page 154: ...its full up or full down position SAFETY SWITCH To prevent inadvertent retraction of the landing gear on the ground a main strut safety switch opens the control circuit when the strut is compressed CAUTION Never rely on the safety switch to keep the gear down during taxi or on take off landing roll or in a static position Always make certain that the landing gear switch is in the down position dur...

Page 155: ...The parking brake should be left off and wheel chocks installed if the airplane is to be left unattended Changes in ambient temperature can cause the brakes to release or to exert excessive pressures GROUND CONTROL Steering is accomplished by use of the rudder pedals through a linkage arrangement which connects the nose strut to the rudder pedal shaft Nose wheel straightening is accomplished by en...

Page 156: ...al systems BATIERY A 33 ampere hour 12 volt battery is located on the right aft side of the firewall Battery servicing procedures are described in the SERVICING section EXTERNAL POWER RECEPTACLE The external power receptacle accepts a standard AN type plug Before connecting an external power unit turn generator switch and avionic equipment OFF CAUTION A negative ground external power source is req...

Page 157: ...arged and the generator output has been adjusted by the regulator to balance the load of electrical equipment then in use LIGHTING SYSTEM INTERIOR LIGHTING Lighting for the instrument panel is furnished by a light in the cabin ceiling It is controlled by the INSTRUMENT LIGHTS rheostat control located below and to the right of the control column The cabin dome light is operated by an ON OFF switch ...

Page 158: ...Section VII Systems Description BEECHCRAFT BonanzaD35 HEATING AND VENTILATION SYSTEM SCHEMATIC 7 28 January 1977 ...

Page 159: ... is then ducted from the mixer valve to the outlets in the cabin HEATER OPERATION The cabin heat control is located on the lower right pilot s subpanel To obtain heated air to the cabin outlets pull the CABIN HEAT control The control regulates the amount of cold air that is mixed with the air from the heater muff When the control is pulled fully out the cold air is shut off and only heated air ent...

Page 160: ...ntrolled by rotating the louvered cover with the small knob on the rim The large knob in the center of this outlet is a friction lock which may be tightened to hold the valve position selected EXHAUST VENTS Air is exhausted from the cabin through two vents in the sides of the baggage compartment which flows to an exhaust vent in the belly and through an adjustable vent in the overhead panel above ...

Page 161: ... it in good working order Refer to the Beech Shop Manual for servicing instructions PITOT AND STATIC SYSTEM The pitot and static system provides a source of impact and static air for the operation of the altimeter rate of climb and airspeed indicator The pitot mast is located on the leading edge of the left wing The static system provides a source of static air to the flight instruments through a ...

Page 162: ... effective in all flight attitudes and at all weights and airspeeds Irregular and intermittent at first the warning signal will become steady as the airplane approaches a complete stall COLD WEATHER OPERATION PREFLIGHT INSPECTION In addition to the normal preflight exterior inspection remove ice snow and frost from the wings tail control surfaces and hinges propeller windshield pitot fuel vents an...

Page 163: ... for starting when available Normal engine starting procedures will ordinarily be used except extra priming may be necessary Moisture forms quickly on the spark plug electrodes during cold weather starts if the engine fails to start after three or four attempts remove at least one spark plug from each cylinder heat the plugs to dry the electrodes then attempt a start immediately after reinstalling...

Page 164: ...eet Inter rupt cruise power every 30 minutes or so by smoothly ad vancing to take off power settings for about 30 seconds then returning to cruise power settings Avoid long power off descents especially during the break in period Maintain sufficient power during descent to permit cylinder head temperatures to remain in the green arc Minimize ground operation time especially during warm weather Dur...

Page 165: ... Pilot 8 7 Alterations or Repairs to Airplane 8 7 Ground Handling 8 7 Towing 8 7 Parking 8 8 Tie Down 8 8 Main Wheel Jacking 8 9 Prolonged Out of Service Care 8 9 Storage 8 9 Flyable Storage 7 to 30 Days 8 10 Mooring 8 10 Engine Preparation For Storage 8 10 During Flyable Storage 8 10 Fuel Cells 8 11 Flight Control Surfaces 8 11 Grounding 8 11 Pitot Tube 8 11 Windshield and Windows 8 11 Preparatio...

Page 166: ...ck Strut Shimmy Damper Brakes Vacuum System Induction Air Filter To Remove and Clean the Filter Minor Maintenance Rubber Seals Generator Magnetos Propeller Blades Cleaning Exterior Painted Surfaces Windshield and Windows Interior Engine Bulb Replacement Guide Recommended Servicing Schedule Lubrication Points Consumable Materials PAGE 8 12 8 12 8 12 8 13 8 13 8 13 8 14 8 15 8 15 8 16 8 16 8 17 8 17...

Page 167: ...ued SUBJECT PAGE Overhaul or Replacement Schedule 8 39 Special Conditions Cautionary Notice 8 39 Landing Gear 8 40 Electrical System 8 40 Power Plant 8 40 Flaps and Flight Controls 8 41 Fuel System 8 41 Instruments 8 42 Miscellaneous 8 42 Approved Engine Oils 8 43 January 1977 8 3 ...

Page 168: ...Section VIII Handling Serv Maint BEECHCRAFT Bonanza D35 INTENTIONALLY LEFT BLANK 8 4 January 1977 ...

Page 169: ...with all airworthiness requirements established for this airplane All limits procedures safety practices time limits servicing and maintenance requirements contained in this handbook are considered mandatory Authorized BEECHCRAFT Parts and Service Outlets will have recommended modification service and operating procedures issued by both FAA and Beech Aircraft Corporation designed to get maximum ut...

Page 170: ...equent revisions AIRPLANE INSPECTION PERIODS 1 FAA Required Annual Inspections 2 BEECHCRAFT Recommended Inspection Guide 3 Continuing Care Inspection Guide 4 See Recommended Servicing Schedule and Overhaul or Replacement Schedule for further inspection schedules 8 6 NOTE Check the wing bolts for proper torque at the first 100 hour inspection and at the first 100 hour inspection after each reinstal...

Page 171: ...d prior to any alterations on the airplane to ensure the airworthiness of the airplane is not violated GROUND HANDLING The three view drawing in Section 1 shows the minimum hangar clearances for a standard airplane Allowances must be made for any special radio antennas and the possibility of an underinflated nose strut or tire TOWING One man can move the airplane on a smooth and level surface usin...

Page 172: ...ake handle is located on the right side of the control console To set the parking brakes pull handle back and depress both toe pedals until firm Push the handle forward to release the brakes NOTE The parking brake should be left off and wheel chocks installed if the airplane is to be left unattended Changes in ambient temperature can cause the brakes to release or to exert excessive pressures TIE ...

Page 173: ...lation to prevent damage to the landing gear door by the jack adapter and to facilitate installation of the adapter 2 Insert the main wheel jack adapter into the main wheel axle 3 A scissors type jack is recommended for raising and lowering the wheel 4 When lowering the wheel exercise care to prevent compression of the shock strut which would force the landing gear door against the jack adapter NO...

Page 174: ...educe the angle of attack of the wings Attach a line to the nose gear ENGINE PREPARA T ON FOR STORAGE Engines in airplanes that are flown only occasionally tend to exhibit cylinder wall corrosion much more than engines that are flown frequently Run engine at least five minutes at 1200 to 1500 rpm with oil and cylinder head temperatures in the normal operating range Check for correct oil level and ...

Page 175: ... engine shall be started and run The preferred method will be to fly the airplane for 30 minutes and up to but not exceeding normal oil and cylinder temperatures FUEL CELLS Fill to capacity to minimize fuel vapor and protect cell inner liners FLIGHT CONTROL SURFACES Lock with internal and external locks GROUNDING Static ground airplane securely and effectively PITOT TUBE Install cover WINDSHIELD A...

Page 176: ... warm up and install Teledyne Continental Motors recommended oil Preflight the airplane SERVICING FUEL SYSTEM FUEL CELLS See Consumable Materials for recommended fuel grades 8 12 CAUTION Never leave bladder cells completely empty for more than a few days as the cell inner liners may dry out and crack permitting fuel to diffuse through the walls of the cell after refueling If the cells are to be le...

Page 177: ... the bottom of the fuel selector valve should be removed and cleaned with solvent every 100 hours To reduce the possibility of contaminated fuel always cap any disconnected fuel lines or fittings Ordinarily the finger strainers in the fuel cell outlets should not require cleaning unless there is a definite indication of solid foreign material in the cells or the airplane has been stored for an ext...

Page 178: ...ition the oil drain tube below the tank drain and re move the oil tank drain plug 4 Locate the oil sump drain plug in the nose wheel well Remove the plug and drain residual oil from the sump 5 The pressure oil screen is located in a housing on the right rear of the engine accessory case Remove the screen and flush it thoroughly Replace the screen 6 Replace the engine sump and oil supply tank drain...

Page 179: ... be an indication that the voltage regulator requires resetting The specific gravity of the electrolyte should be checked periodically and maintained within the limits placarded on the battery The battery box is vented overboard to dispose of electrolyte and hydrogen gas fumes discharged during the normal charging operation To ensure disposal of these fumes the vent tube should be checked frequent...

Page 180: ...wheel tire should be inflated to 30 psi Maintaining proper tire inflation will minimize tread wear and aid in preventing tire failure caused from running over sharp stones When inflating tires visually inspect them for cracks and breaks NOTE Beech Aircraft Corporation cannot recommend the use of recapped tires Recapped tires have a tendency to swell as a result ofthe increased temperature generate...

Page 181: ...sed exercise care to avoid over inflating the shock strut WARNING NEVER FILL SHOCK STRUTS WITH OXYGEN 3 Remove all foreign material from the exposed piston with a soft cloth moistened with hydraulic fluid TO REPLENISH STRUT HYDRAULIC FLUID 1 Support the airplane on jacks at the wing jack points 2 Remove the air valve cap depress the valve core and allow the strut to fully deflate 3 Raise and block...

Page 182: ...n the piston rod keep fluid in the shimmy damper under pressure As fluid is lost through leakage it is automatically replenished from the reservoir until the reservoir supply is exhausted To check the fluid level in the shimmy damper insert a wire approximately 1 32 inch in diameter through the hole in the disc at the aft end of the piston rod until it touches the bottom of the hole in the floatin...

Page 183: ...id specification The brakes require no adjustments since the pistons move to compensate for lining wear VACUUM SYSTEM The vacuum system incorporates two screens a relief valve screen and an oil separator screen These screens should be cleaned every 100 hours If the airplane is operated in dusty conditions the screens should be cleaned more frequently Clean the suction relief valve screen by removi...

Page 184: ...the filter MINOR MAINTENANCE RUBBER SEALS To prevent sticking of the rubber seals around the windows doors and engine cowling the seals should be coated with Oakite 6 compound The compound is noninjurious to paint and can be removed by employing normal cleaning methods GENERATOR Since the generator and voltage regulator are designed for use on only one polarity system the following precautionary m...

Page 185: ...etos as hot whenever a switch lead is disconnected at any point they do not have an internal automatic grounding device The magnetos can be grounded by replacing the switch lead at the noise filter capacitor with a wire which is grounded to the engine case Otherwise all spark plug leads should be disconnected or the cable outlet plate on the rear of the magneto should be removed PROPELLER BLADES T...

Page 186: ...ent Fluid dispensed at high pressure could remove the protective lubri cant allowing moisture from heavy or pro longed rain to collect at hinge lines and then to freeze at low temperatures After high pressure or hand washing and at each periodic inspection lubricate trim tab hinge lines and trim tab pushrod end fittings Brayco 300 per Federal Specification VV L 800 preferred See Consumable Materia...

Page 187: ... keeping them free of dirt and grime Any rubbing of the surface should be done gently and held to a minimum to avoid damaging the paint film Rinse thoroughly with clear water Stubborn oil or soot deposits may be removed with auto motive tar removers Prior to cleaning cover the wheels making certain the brake discs are covered Attach the pitot cover securely and plug or mask off all other openings ...

Page 188: ...g conditions which might cause abrasion or premature finish deterioration Alkyd enamel lacquer and dope finishes must be polished and waxed periodically to maintain luster and to assure protection from the weather Acrylic enamel should be waxed and may be polished if desired Acrylic urethane may be waxed for protection from the elements but should not be polished unless polishing or buffing is req...

Page 189: ...ompletely dissolved in water to remove oil and grease film To remove stubborn grease and oil deposits use hexane or aliphatic naphtha Rinse with clean water avoid prolonged rubbing CAUTION Do not use gasoline benzene acetone carbon tetrachloride fire extinguisher fluid deice fluid or lacquer thinners on the windshield or windows as these substances have a tendency to soften and craze the surface I...

Page 190: ... water and allow to dry BULB REPLACEMENT GUIDE LOCATION Compass light Dome light cabin Elevator tab position indicator light Fuel pump placard light Instrument flood light overhead Landing gear position light Landing gear visual position light Landing light wing Navigation light tail cone Navigation light wing Stall warning light 8 24 NUMBER 330 89 53R 1813 89 1813 53 4522 93 1512 1813 January 197...

Page 191: ...Bottom of fuselage drain left side Service fuel cells main Top of wings leading edge Service auxiliary fuel cell Baggage compartment Check battery electrolyte Under right cowling door and thru access door in firewall Change engine oil Lower side of engine and bottom of oil supply tank Clean engine oil screens Engine accessory case LUBRICANT Number refers to item on Consumable Materials 5 6 6 See S...

Page 192: ... seats on left side Lubricate landing gear Wheel wells M retract mechanism and uplock rollers Clean fuel selector valve Left side belly strainer Clean vacuum pump Engine compartment regulator screen Lubricate aileron control Each wing L linkage Clean carburetor fuel Carburetor fuel inlet strainer LUBRICANT Number refers to item on Consumable Materials 4 7 7 4 cfl ll CD l Q 0 l l cp fl CD s Q 5 a C...

Page 193: ...e landing gear retract mechanism and uplock rollers Lubricate nose gear re tract mechanism Lubricate nose wheel steering mechanism Lubricate rudder pedals Aft edge of cabin door E Forward of instrument panel C Bottom of cowl P Ruddervator tab horn Forward of tail bulk head I Forward of tail bulk head J Edge of wheel well N R Wheel wells M Nose wheel well A Nose wheel well B Cockpit 0 4 4 4 4 3 4 3...

Page 194: ...in floor G Propeller blade bearings Propeller S Propeller actuator Propeller S mechanism Propeller actuator Propeller S bearings Tachometer drive Rear of engine Q adaptor for APC Flap motor brushes Under floor in cabin H Service flap motor gear Under floor in cabin H box Service landing gear Under floor in cabin F actuator gear box LUBRICANT Number refers to item on Consumable Materials 4 1 4 3 3 ...

Page 195: ...e main and nose Landing gear shock struts Service shimmy damper Nose gear Drain static air lines Behind left rear cabin seats Remove one end of the hose which forms the static line drain and permit the system to drain NOTE The static air line should be drained frequently during periods of high humidity Also drain the line each time the airplane is flown through heavy rain or is washed down 3 10 9 ...

Page 196: ...Section VIII Handling Serv Maint LUBRICATION POINTS A LANDING GEAR RETRACT 8 30 BEECHCRAFT Bonanza D35 January 1977 ...

Page 197: ...BEECHCRAFT BonanzaD35 B C Section VIII Handling Serv Ma int NOSE WHEEL STEERING CONTROL COLUMN LINKAGE D ELEVATOR TRIM CONTROL January 1977 8 31 ...

Page 198: ...Section VIII Handling Serv Maint BEECHCRAFT BonanzaD35 E CABIN DOOR F LANDING GEAR GEAR BOX G AUXILIARY PUMP 8 32 January 1977 ...

Page 199: ...BEECHCRAFT Section VIII Bonanza D35 Handling Serv Ma int FLAP MOTOR GEAR BOX I DIFFERENTIAL CONTROL MECHANISM J ELEVATOR TAB January 1977 8 33 ...

Page 200: ...Section VIII Handling Serv Maint K FLAP ACTUATOR L AILERON BELL CRANKS M LANDING GEAR RETRACT 8 34 BEECH CRAFT Bonanza035 January 1977 ...

Page 201: ...BEECHCRAFT BonanzaD35 Section VIII Handling Serv Maint LANDING GEAR DOOR HINGES 0 RUDDER PEDALS p COWL FLAP HINGES January 1977 8 35 ...

Page 202: ...Section VIII Handling Serv Maint BEECHCRAFT BonanzaD35 Q TACHOMETER DRIVE ADAPTER R LANDING GEAR DOORS 8 36 January 1977 ...

Page 203: ...hart No attempt has been made to update the basic number with the letter suffix that designates the current issues of the various specifications Vendors listed as meeting Federal and Military Specifi cations are provided as reference only and are not spe cifically recommended by Beech Aircraft Corporation con sequently any product conforming to the specification listed may be used The products lis...

Page 204: ...to usage of that item This determination may be made by contacting the vendor of a specific item CONSUMABLE MATERIALS ITEM MATERIAL 1 Lubricating Grease Wheel Bearing SPECIFICATION Aeroshell No 5 or MIL G 81322 CAUTION Do not mix Aeroshell No 5 with MIL G 81322 Thoroughly clean grease from bearings and bearing area before changing grease 2 Hydraulic Fluid 3 Lubricating Grease General Purpose Wide ...

Page 205: ...Oil Gear MIL L 10324 or MIL L 2105C Grade 75W 10 Grease Aircraft and Instrument MIL G 23827 t 11 Lubricant Rubber Seal Oakite 6 Compound 12 Naptha Aliphatic Federal Specification TT N 95 13 Lubricating Oil Brayco 300 per General Purpose Federal Specifi Preservative Water cation VV L 800 Displacing Low Preferred Temperature Alternates for Brayco 300 Lubricant Revised March 1983 CRC 3 36 LPS No 1 WD...

Page 206: ...mmended during break in period See servicing data If 80 87 RED grade fuel not available use 100LL BLUE or 100 GREEN grade fuel t Product of Oakite Products Inc 50 Valley Road Berkley Heights N J 07922 Product of Bray Oil Co 1925 North Marianna Los Angeles Calif 90032 Product of CRC Chemicals Inc Warminster Pa 18974 Product of LPS Research Laboratories Inc 2050 Cotner Ave W Los Angeles Calif 90025 ...

Page 207: ...s handbook are based on average usage and average environmental conditions SPECIAL CONDITIONS CAUTIONARY NOTICE Airplanes operated for Air Taxi or other than normal operation and airplanes operated in humid tropics or cold and damp climates etc may need more frequent inspections for wear corrosion and or lack of lubrication In these areas periodic inspections should be performed until the operator...

Page 208: ...y 2000 hours Every 4000 hours Every 1000 hours Every 500 hours or on condition Every 1000 hours On condition On condition On condition On condition On condition On condition On condition ELECTRICAL SYSTEM Battery master relay All other relays Voltage regulator Starter relay On condition On condition On condition On condition POWER PLANT Engine Engine controls Engine vibration isolator mounts Exhau...

Page 209: ...ls Elevator tab actuator Flap motor and drives Flap motor brushes Flap gear box Flap actuators Flap flexible shaft On condition On condition Every 2000 hours On condition Every 2000 hours Every 2000 hours Every 2000 hours FUEL SYSTEM Fuel cells Fuel quantity transmitters Fuel cell drain valve Fuel system check valves Fuel selector valve and auxiliary Wobble fuel pump All hose January 1977 On condi...

Page 210: ...n condition On condition On condition On condition On condition On condition On condition Every 100 hours On condition MISCELLANEOUS Seat belts or Shoulder Harnesses Hand fire extinguisher Cabin heating and venti lating ducts Inspect every 12 months replace on condition Inspect every 12 months recharge as necessary On condition inspect every 12 months Reference Teledyne Continental Motors Corporat...

Page 211: ...BRAND AND WEIGHT B P Aero Oil D65 80 Grade 40 Castrolaero AD Type Ill Grade 50 Castrolaero AD Type II Conoco Aero S No 65 SAE 30 Conoco Aero S No 80 SAE 40 Conoco Aero S SAE 1OW30 Delta Avoil Grades 30 40 50 Gulfpride Aviation Series D Exxon Aviation Oils In Grades E65 EBO El 00 El 20 and A100 Kendall Aviation Oil Type D Pennzoil Aircraft Engine Oil Heavy Duty Dispersant Grades 30 40 50 Phillips 6...

Page 212: ...voil 20W 40 Socony Mobil Aero Red Band HD SAE 50 Aero Gray Band HD SAE 40 Aero White Band HD SAE 30 Mobil Aero Oil 65 Ashless Mobil Aero Oil 80 Dispersant Mobil Aero Oil 100 Aviation Mobil Aero Oil 120 Engine Oil Std Oil of California RPM Aviation Oil Compounded Texaco Inc Texaco Aircraft Engine Oil DlOO Texaco Aircraft Engine Oil D80 Texaco Aircraft Engine Oil Premium AD Grades 65 80 100 Union Oi...

Page 213: ...t NOTE This chart lists all oils which were certified as meeting the requirements of Teledyne Continental Motors Specification MHS 24A at the time this handbook was published Any other oil which conforms to this specification may be used Januarv 1977 8 45 ...

Page 214: ...Section VIII Handling Serv Maint BEECHCRAFT Bonanza D35 INTENTIONALLY LEFT BLANK 8 46 January 1977 ...

Page 215: ...anual Supplements for equipment for which the vendor obtained a Supplemental Type Certificate were included as loose equipment with the airplane at the time of delivery These and other Airplane Flight Manual Supplements for other equipment that was installed after the airplane was delivered new from the factory should be placed in this Supplemental Data Section IX of this Pilot s Operating Handboo...

Page 216: ...Section IX Supplements BEECHCRAFT BonanzaD35 INTENTIONALLY LEFT BLANK 9 2 January 1977 ...

Page 217: ...nts PILOT S OPERATING HANDBOOK and FAA APPROVED AIRPLANE FLIGHT MANUAL LOG OF SUPPLEMENTS FAA Supplements must be in the airplane for flight operation when subject equipment is installed Supp Part Subject Rev Date No Number No January 1977 9 3 ...

Page 218: ...Section IX Supplements BEECHCRAFT BonanzaD35 INTENTIONALLY LEFT BLANK 9 4 January 1977 ...

Page 219: ...Circulars 10 12 FAA General Aviation News 10 15 FAA Accident Prevention Program 10 15 Additional Information 10 16 General Information on Specific Topics 10 17 Maintenance 10 17 Hazards of Unapproved Modifications 10 19 Flight Planning 10 20 Passenger Information Cards 10 20 Stowage of Articles 10 21 Flight Operations 10 21 General 10 21 Preflight Inspection 10 21 Weight and Balance 10 22 Autopilo...

Page 220: ...Spins 10 36 Descent 10 38 Vortices Wake Turbulence 10 39 Takeoff and Landing Conditions 10 40 Medical Facts for Pilots 10 40 General 10 40 Fatigue 10 41 Hypoxia 10 41 Hyperventilation 10 43 Alcohol 10 43 Drugs 10 45 Scuba Diving 10 45 Carbon Monoxide and Night Vision 10 45 Decompression Sickness 10 46 A Final Word 10 47 10 2 May 1994 ...

Page 221: ... thor oughly familiar with your airplane Know its limitations and your own Maintain your currency or fly with a qualified instructor until you are current and proficient Practice emer gency procedures at safe altitudes and airspeeds prefer ably with a qualified instructor pilot until the required action can be accomplished without reference to the manual Peri odically review this safety informatio...

Page 222: ...ion and the other operating and maintenance manu als which accompany the airplane that FAA requirements for ratings certifications and review be scrupulously com plied with and that you allow only persons who are properly licensed and rated and thoroughly familiar with the contents of the Pilot s Operating Handbook and FM Approved Air plane Flight Manual to operate the airplane IMPROPER OPERATION ...

Page 223: ... instructor until you are current Practice until you are proficient Preplan all aspects of your flight including a proper weather briefing anp adequate fuel reserves Use services available weather briefing inflight weather and Flight Service Station Carefully preflight your airplane Use the approved checklist Have more than enough fuel for takeoff plus the trip and an adequate reserve Be sure your...

Page 224: ... action can be accomplished without reference to the manual Keep your airplane in good mechanical condition Stay informed and alert fly in a sensible manner DON TS Don t take off with frost ice or snow on the airplane Don t take off with less than minimum recommended fuel plus adequate reserves and don t run the tank dry before switching Don t fly in a reckless show off or careless manner Don t fl...

Page 225: ...ilization of your airplane When the airplane was manufac tured it was equipped with one or more of the following placards Owner s Manual FAA Approved Airplane Flight Manual FAA Approved Airplane Flight Manual Supple ments Pilot s Operating Handbook and FM Approved Air plane Flight Manual Beech has revised and reissued many of the early manuals for certain models of airplanes in GAMA Standard Forma...

Page 226: ...evi sions of BEECHCRAFT Safety Communiques to BEECH CRAFT Owner addresses as listed by the FM Aircraft Reg istration Branch List and the BEECHCRAFT International Owner Notification Service List While this information is dis tributed by Beech Aircraft Corporation Beech can not make changes in the name or address furnished by the FM The owner must contact the FAA regarding any changes to name or add...

Page 227: ...request may be made by using the owner notification request card furnished with the loose equipment of each airplane at the time of delivery or by a letter requesting this service referencing the specific airplane serial number owned Write to Supervisor Special Services Dept 52 Beech Aircraft Corporation P O Box 85 Wichita Kansas 67201 0085 From time to time Beech Aircraft Corporation issues BEECH...

Page 228: ...ment regulations The regulations are designed for your protection and the protection of your passengers and the public Com pliance is mandatory AIRWORTHINESS DIRECTIVES FAR Part 39 specifies that no person may operate a product to which an Airworthiness Directive issued by the FAA applies except in accordance with the requirements of that Airworthiness Directive AIRMAN S INFORMATION MANUAL The Air...

Page 229: ...ing Radio Phraseology and Technique Mountain Flying Airport Operations Wake Turbulence Vortices Clearances and Separations Medical Facts for Pilots Preflight Bird Hazards Departures IFR Good Operating Practices En route IFR Airport Location Directory Arrival IFR All pilots must be thoroughly familiar with and use the infor mation in the AIM ADVISORY INFORMATION NOTAMS Notices to Airmen are documen...

Page 230: ...ation bookstores or at FBO s These documents are subject to periodic revision Be certain the Advisory Circular you are using is the latest revision available Some of the Advisory Circulars of interest to pilots are 00 6 00 24 00 30 00 45 00 46 20 5 20 32 20 35 20 43 20 105 20 113 20 125 10 12 Aviation Weather Thunderstorms Rules of Thumb for Avoiding or Minimizing Encounters with Clear Air Turbule...

Page 231: ...d Guide lines for the Conduct of the Biennial Flight Review 60 13 The Accident Prevention Counselor Pro gram 61 9 61 21 61 23 61 27 61 67 61 84 67 2 90 23 90 42 May 1994 Pilot Transition Courses for Complex Single Engine and Light Twin Engine Air planes Flight Training Handbook Pilot s Handbook of Aeronautical Knowl edge Instrument Flying Handbook Hazards Associated with Spins in Airplanes Prohibi...

Page 232: ...alance Handbook Maintenance and Handling of Air Driven Gyroscopic Instruments Use of Alternate Grades of Aviation Gaso line for Grade 80 87 and Use of Automotive Gasoline Noise Hearing Damage and Fatigue in General Aviation Pilots Unreliable Airspeed Indications Operational and Maintenance Practices for Emergency Locator Transmitters and Receivers Gyroscopic Instruments Good Operating Practices Im...

Page 233: ...tion specialists to each Flight Standards and General Aviation District Office to organize accident prevention program activities In addition there are over 3 000 volunteer airmen serving as accident prevention counselors sharing their technical expertise and professional knowledge with the general aviation commu nity The FAA conducts seminars and workshops and dis tributes invaluable safety infor...

Page 234: ...Gen eral Aviation Accident Prevention Program These can be obtained at FAA Offices Weather Stations Flight Service Stations or Airport Facilities Some of these are titled 12 Golden Rules for Pilots Weather or Not Disorientation Plane Sense Weather Info Guide for Pilots Wake Turbulence Don t Trust to Luck Trust to Safety Rain Fog Snow Thunderstorm TRW Icing Pilot s Weather Briefing Guide Thundersto...

Page 235: ...ted and promptly corrected Schedule your maintenance regularly and have your air plane serviced by a reputable organization Be suspicious of bargain prices for maintenance repair and inspections It is the responsibility of the owner and the operator to assure that the airplane is maintained in an airworthy condi tion and that proper maintenance records are kept Use only genuine BEECHCRAFT or BEECH...

Page 236: ...pressly disclaims any responsibility for malfunctions failures damage or injury caused by use of non BEECHCRAFT parts Airplanes operated for Air Taxi or other than normal opera tion and airplanes operated in humid tropics or cold and damp climates etc may need more frequent inspections for wear corrosion and or lack of lubrication In these areas periodic inspections should be performed until the o...

Page 237: ...er Supple mental Type Certificates STC s Before installing an STC on your airplane check to make sure that the STC does not conflict with other STC s that have already been installed Because approval of an STC is obtained by the individual STC holder based upon modification of the original type design it is possible for STC s to interfere with each other when both are installed Never install an un...

Page 238: ...te track and stations and make a list for quick reference It is strongly recommended a flight plan be filed with Flight Service Sta tions even though the flight may be VFR Also advise Flight Service Stations of changes or delays of one hour or more and remember to close the flight plan at destination The pilot must be completely familiar with the performance of the airplane and performance data in...

Page 239: ... is utilized to provide space for seat displacement If hard solid objects are stored beneath seats the energy absorbing feature is lost and severe spinal injuries can occur to occupants Prior to flight pilots should insure that articles are not stowed beneath seats that would restrict seat pan energy absorption or penetrate the seat in event of a high vertical velocity accident FLIGHT OPERATIONS G...

Page 240: ...alling speed will be higher rate of climb the cruising speed and the range of the airplane at any level of fuel will all be lower than shown in the Performance section If an airplane is loaded so that the C G is forward of the for ward limit it will require additional control movements for maneuvering the airplane with correspondingly higher con trol forces The pilot may have difficulty during tak...

Page 241: ...ribed in the Airplane Flight Manual Supplements Ensure a full understanding of the methods of engagement and disengagement of the autopi lot and trim systems Compare the descriptions and procedures contained in the Supplements to the actual installation in the airplane to ensure that the supplement accurately describes your instal lation Test that all buttons switches and circuit breakers function...

Page 242: ...t malfunction from an electric trim system malfunction The safest course is to deactivate both Do not re engage either system until after you have safely landed Then have the systems checked by a qualified service facility prior to further flight Depending upon the installation on your airplane the follow ing additional methods may be available to disengage the autopilot or electric trim in the ev...

Page 243: ...H FLT switch on the autopilot control ler if installed NOTE After the autopilot is positively disengaged it may be necessary to restore other electrical functions Be sure when the master switches are turned on that the autopilot does not re engage The above ways may or may not be available on your auto pilot It is essential that you read your airplane s AFM SUPPLEMENT for your autopilot system and...

Page 244: ...p of the air plane Airplanes are designed so that flutter will not occur in the normal operating envelope of the airplane as long as the airplane is properly maintained In the case of any airplane decreasing the damping and stiffness of the structure or increasing the trailing edge weight of control surfaces will tend to cause flutter If a combination of those factors is suf ficient flutter can oc...

Page 245: ... which could create an increased trailing edge heavy control surface and flutter If an excessive vibration particularly in the control column and rudder pedals is encountered in flight this may be the onset of flutter and the procedure to follow is 1 IMMEDIATELLY REDUCE AIRSPEED lower the land ing gear if necessary 2 RESTRAIN THE CONTROLS OF THE AIRPLANE UNTIL THE VIBRATION CEASES 3 FLY AT THE RED...

Page 246: ...Airplane may be momentarily out of control Occupants are thrown violently against the belts and back into the seat Unsecured objects are tossed about Occupants require seat belts and occasion ally are thrown against the belt Unsecured objects move about Occupants may be required to use seat belts but objects in the airplane remain at rest Thunderstorms squall lines and violent turbulence should be...

Page 247: ... an excessive airspeed you run the risk of structural damage or failure on the other hand if your air speed is too low you may stall If turbulence is encountered reduce speed to the turbulent air penetration speed if given or to the maneuvering speed which is listed in the Limitations section of the Pilot s Oper ating Handbook and FAA Approved Airplane Flight Manual These speeds give the best assu...

Page 248: ...vere downdrafts The prediction of wind shears is far from an exact science Monitor your airspeed carefully when flying near storms particularly on approach Be mentally prepared to add power and go around at the first indication that a wind shear is being encountered WEATHER RADAR Airborne weather avoidance radar is as its name implies for avoiding severe weather not for penetrating it Whether to f...

Page 249: ...ch echoes should be separated by at least 40 miles before you fly between them With weaker echoes you can reduce the distance by which you avoid them Above all rememqer this never regard any thunderstorm lightly Even when radar observers report the echoes are of light intensity avoiding thunderstorms is the best policy The following are some do s and don ts of thunderstorm avoid ance 1 Don t land ...

Page 250: ...n your shoulder harness and secure all loose objects 10 Plan and hold your course to take you through the storm in minimum time 11 To avoid the most critical icing establish a penetration altitude below the freezing level or above the level of 15 C 12 Verify that pitot heat is on and turn on carburetor heat or engine anti ice Icing can be rapid at any altitude and cause almost instantaneous power ...

Page 251: ...uld not be taken as assurance that mountain wave turbulence will not be encountered A mountain wave downdraft may exceed the climb capability of your airplane Avoid mountain wave downdrafts VFR LOW CEILINGS If you are not instrument rated do not attempt VFR on Top or Special VFR flight or clearances Being caught above a solid cloud layer when an emergency descent is required or at destination is a...

Page 252: ... interpretations illusions result and may confuse the pilot s conception of the attitude and position of his air plane Under VFR conditions the visual sense using the horizon as a reference can override the illusions Under low visibil ity conditions night fog clouds haze etc the illusions pre dominate Only through awareness of these illusions and proficiency in instrument flight procedures can an ...

Page 253: ...t should not be made or it should be discontinued as soon as possible The result of vertigo is loss of control of the airplane If the loss of control is sustained it will result in an excessive speed accident Excessive speed accidents occur in one of two manners either as an inflight airframe separation or as a high speed ground impact and they are fatal accidents in either case All airplanes are ...

Page 254: ...e deactivated by interruption of circuits circuit breakers or fuses Compliance with this requirement is especially important in all high performance single engine airplanes during simulated engine out practice or stall dem onstrations because the stall speed is critical in all low speed operation of airplanes Training should be accomplished under the supervision of a qualified instructor pilot wit...

Page 255: ...at intentional spins are entered by delib erately inducing a yawing moment with the controls as the airplane is stalled Inadvertent spins result from the same combination stall plus yaw That is why 1it is important to use coordinated controls and to recover at the first indication of a stall when practicing stalls Always remember that extra alertness and pilot techniques are required for slow flig...

Page 256: ...l avoidance is your best protection against an inadvertent spin MAINTAIN YOUR AIRSPEED In airplanes not certificated for aerobatics spins are prohib ited If a spin is entered inadvertently Immediately move the control column full forward and simul taneously apply full rudder opposite to the direction of the spin continue to hold this position until rotation stops and then neutralize all controls a...

Page 257: ...ces The larger and heavier the airplane the more pronounced and turbulent the wakes will be Wing tip vortices from large heavy airplanes are very severe at close range degenerating with time wind and distance These are rolling in nature from each wing tip In tests vor tex velocities of 133 knots have been recorded Encounter ing the rolling effect of wing tip vortices within two minutes after passa...

Page 258: ...iction Snow and ice covered runways are also hazardous The pilot should also be alert to the possibility of the brakes freezing Use caution when taking off or landing during gusty wind conditions Also be aware of the special wind conditions caused by buildings or other obstructions located near the runway MEDICAL FACTS FOR PILOTS GENERAL When the pilot enters the airplane he becomes an integral pa...

Page 259: ...system to let you know when you are not getting enough oxygen It is impossible to predict when or where hypoxia will occur during a given flight or how it will manifest itself Some of the common symptoms of hypoxia are increased breathing rate a light headed or dizzy sensation tingling or warm sensation sweating reduced visual field sleepiness blue coloring of skin fingernails and lips and behavio...

Page 260: ...at require or may require the use of supplemental oxygen should be thoroughly familiar with the operation of the airplane oxygen systems A preflight inspection of the system should be performed including proper fit of the mask The passengers should be briefed on the proper use of their oxygen system before flight Pilots who wear beards should be careful to ensure that their beard is carefully trim...

Page 261: ...slow your breathing rate until symptoms clear and then resume nor mal breathing rate Normal breathing can be aided by talk ing aloud ALCOHOL Common sense and scientific evidence dictate that you must not fly as a crew member while under the influence of alcohol Alcohol even in small amounts produces among other things A dulling of critical judgement A decreased sense of responsibility Diminished s...

Page 262: ...about one third of an ounce per hour Even after the body completely destroys a moderate amount of alcohol a pilot can still be severely impaired for many hours by hangover The effects of alcohol on the body are magnified at altitudes as 2 oz of alcohol at 18 000 feet produce the same adverse effects as 6 oz at sea level Federal Aviation Regulations have been amended to reflect the FAA s growing co...

Page 263: ... Even simple home or over the counter remedies and drugs such as aspirin _anti histamines cold tablets cough mixtures laxatives tranquil izers and appetite suppressors may seriously impair the judgment and coordination needed while flying The safest rule is to take no medicine before or while flying except after consultation with your Aviation Medical Examiner SCUBA DIVING Flying shortly after any...

Page 264: ...ogen bubble formation in body tissue as the ambient air pressure is reduced by climbing to higher alti tudes The symptoms are pain in the joints abdominal cramps burning sensations in the skin visual impairment and numbness Some of these symptoms are similar to hyp oxia The only known remedy for decompression sickness is recompression which can only be accomplished in an unpressurized airplane by ...

Page 265: ...s is even more remarkable Radar RNAV LORAN sophisticated autopilots and other devices which just a few years ago were too large ar d pro hibitively expensive for general aviation size airplanes are becoming increasingly commonplace in even the smallest airplanes It is thus that this Safety Information is directed to the pilot for it is in the area of the skill and proficiency of you the pilot that...

Page 266: ...Section X Safety Information Oeechcraft Single Engine Piston THIS PAGE INTENTIONALLY LEFT BLANK 10 48 May 1994 ...

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