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Beechcraft V35B Bonanza FlightSim Developers
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Beechcraft V35B Bonanza, Pilot Operating Handbook, BEECHCRAFT Bonanza V35B. THANK YOU for displaying confidence in us by selecting our V35B Bonanza for Microsoft Flight. Simulator Our design and technical team have utilized their skills and years of experience to ensure. that the Bonanza meets the high standards of quality and performance for which FlightSim Developers. airplanes have become famous throughout the world, IMPORTANT NOTICE. This handbook must be read carefully by the owner and operator in order to become familiar with the. operation of the V35B Bonanza The handbook presents suggestions and recommendations to help. enhance your simulation experience and efficiently operate the aircraft. All rights reserved per the terms of the End User License Agreement found at the end of this manual. No part of this manual may be scanned reproduced copied transmitted distributed downloaded or. used for any purpose without the express written consent of FSD International Inc. Information contained herein is subject to change without notice. USE OF THE HANDBOOK, The Pilot s Operating Handbook is designed to maintain documents necessary for the safe and efficient. operation of the Bonanza, Beechcraft V35B Bonanza, Pilot Operating Handbook. 3 View Diagram, Beechcraft V35B Bonanza, Pilot Operating Handbook.
Table of Contents, BEECHCRAFT Bonanza V35B 1, Section I General 5. DESCRIPTIVE DATA 5, PROPELLER 5, OIL CAPACITY 5, CABIN DIMENSIONS 5. Terminology And Symbols 6, GENERAL AIRSPEED TERMINOLOGY 6. METEOROLOGICAL TERMINOLOGY 7, POWER TERMINOLOGY 7, ENGINE CONTROLS AND INSTRUMENTS 7. WEIGHT AND BALANCE TERMINOLOGY 8, Section II Limitations 10.
AIRSPEED LIMITATIONS 10, AIRSPEED INDI CATOR MARKINGS 10. POWER PLANT LIMITATIONS 11, PROPELLER 11, POWER PLANT INSTRUMENT MARKINGS 12. WEIGHT AND CENTER OF GRAVITY 12, APPROVED MANEUVERS 2650 POUNDS 13. FLIGHT LOAD FACTORS 2650 POUNDS 13, REQUIRED EQUIPMENT FOR VARIOUS CONDITIONS OF FLIGHT 13. Emergency Procedures 14, EMERGENCY AIRSPEEDS 14, ENGINE FIRE GROUND 14.
ENGINE FAILURE ON TAKE OFF 14, ENGINE MALFUNCTION IN FLIGHT 14. ENGINE FAILURE 14, DISCREPANCY CHECKS 14, AIR START PROCEDURE 15. ENGINE FIRE FLIGHT 15, EMERGENCY DESCENT 15, MAXIMUM GLIDE CONFIGURATION 16. EMERGENCY LANDING 16, GEAR UP LANDING 16, UNLATCHED DOOR IN FLIGHT 16. GENERATOR OUT PROCEDURE 16, INDUCTION SYSTEM ICING 17.
EMERGENCY SPEED REDUCTION 17, Normal Procedures 18. SPEEDS FOR SAFE OPERATION 18, Beechcraft V35B Bonanza. Pilot Operating Handbook, PREFLIGHT INSPECTION 18, BEFORE STARTING 18. STARTING 19, BEFORE TAKE OFF 20, TAKE OFF 20, DESCENT 21. BEFORE LANDING 21, SHUTDOWN 21, Systems Description 22.
TRIM CONTROL 22, WING FLAPS 22, INSTRUMENT PANEL 22. ENGINE INSTRUMENTS 24, MANIFOLD PRESSURE GAUGE AND TACHOMETER 24. ENGINE CONTROLS 25, THROTTLE MIXTURE AND PROPELLER 25. COWL FLAPS 25, OIL SYSTEM 25, STARTER 26, PROPELLER 27. FUEL SYSTEM 27, FUEL QUANTITY 28, FUEL TANK SELECTION 28.
FUEL REQUIRED FOR FLIGHT 29, LANDING GEAR SYSTEM 29. CONTROL SWITCH 29, POSITION INDICATORS 29, WARNING HORN 29. GROUND CONTROL 30, ELECTRICAL SYSTEM 30, GENERATOR 30. LIGHTING SYSTEM 31, INTERIOR LIGHTING 31, EXTERIOR LIGHTING 31. HEATING AND VENTILATION SYSTEM CABIN HEATING 31, PITOT AND STATIC SYSTEM 33.
VACUUM SYSTEM 33, STALL WARNING 33, Performance 34. INTRODUCTION TO PERFORMANCE AND FLIGHT PLANNING 34. Beechcraft V35B Bonanza, Pilot Operating Handbook, Section I General. DESCRIPTIVE DATA, The V35B Bonanza is powered by either a Continental E185 1 or E185 8 six cylinder engine rated for a. maximum take off power of 185 hp at 2300 rpm max one minute The maximum continuous rating is. 165 hp at 2050 rpm, Beech electrically controlled variable pitch two blade 88 inch diameter propeller with Beech pitch. control motor and spinner The propeller uses a Beech R203 100 hub with either R201 217 88 or R203. 218 88 blades, Aviation Gasoline 80 87 red minimum grade or alternate grades 100LL blue or 100 130 green.
Standard fuel system Two 20 gallon tanks in wings Total 34 gallons usable. Optional fuel system Two 20 gallon main tanks in wings and either one 10 gallon or one 20 gallon. auxiliary tank installed 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, Maximum Ramp Weight 2660 lbs. Maximum Take Off Weight 2650 lbs, Maximum Landing Weight 2650 lbs. CABIN DIMENSIONS, Length 6 ft 11 in, Height 4 ft 2 in. Width 3 ft 6 in, Entrance Door 36 in x 37 in, Volume 16 5 cu ft. Capacity 270 lbs, Baggage Door 22 5 in x 18 5 in, Beechcraft V35B Bonanza.
Pilot Operating Handbook, TERMINOLOGY AND SYMBOLS, GENERAL AIRSPEED TERMINOLOGY. CAS Calibrated Airspeed is the indicated speed of an airplane corrected for position and. instrument error Calibrated airspeed is equal to true airspeed in standard atmosphere at sea. 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 exp ressed in knots, TAS True Airspeed is the airspeed of an airplane relative to undisturbed air which is the CAS. corrected for altitude temperature and compressibility. VA Maneuvering Speed is the maximum speed at which application of full available aerodynamic. control will not overstress the airplane, VFE Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a. prescribed extended position, VLE Maximum Landing Gear Extended Speed is the maximum speed at which an airpla ne can be.
safely flown with the landing gear extended, VLO Maximum Landing Gear Operating Speed is the maximum speed at which the landing gear. can be safely extended or retracted, VNE Never Exceed Speed is the speed limit that may not be exceeded at any time. VNO Maximum Structural Cruising Speed is the or Vc 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 Stalling Speed or the minimum steady flight speed at which the airplane is controllable in the. landing configuration, VX Best Angle of Climb Speed is the airspeed which delivers the greatest gain ot altitude in the. shortest possible horizontal distance, Vy Best Rate of Climb Speed is the airspeed which delivers the greatest gain in altitude in the.
shortest possible time, Beechcraft V35B Bonanza, Pilot Operating Handbook. METEOROLOGICAL TERMINOLOGY, ISA International Standard Atmosphere in which. 1 The air is a dry perfect gas, 2 The temperature at sea level is 15 Celsius 59 Fahrenheit. 3 The pressure at sea level is 29 92 inches Hg 1013 2 millibars. 4 The temperature gradient from sea level to the altitude at which the temperature is 56 5 C. 69 7 F is 0 00198 C 0 003566 F per foot and zero above that altitude. OAT Outside Air Temperature is the free air static temperature obtained either from in flight. temperature indications adjusted for instrument error and compressibility effects or ground. meteorological sources, Indicated The number actually read from an altimeter when the barometric sub scale has been set to. Pressure 29 92 inches of mercury 1013 2 millibars, Pressure Altitude measured from standard sea level pressure 29 92 in Hg by a pressure or.
Altitude baro metric altimeter, Station It is the indicated pressure altitude corrected for position and instrument error In this. Pressure Handbook altimeter instrument errors are assumed to be zero Position errors may be. obtained from the Altimeter Correction Chart Actual atmospheric pressure at field elevation. Wind The wind velocities recorded as variables on the charts of this handbook are to be understood. as the headwind or tailwind components of the reported winds. POWER TERMINOLOGY, Take off Maximum power rating limited by time. Maximum Highest power rating not limited by time, Continuous. Cruise Power recommended for cruise climb, ENGINE CONTROLS AND INSTRUMENTS. Throttle Used to control power by introducing fuel air mixture into the intake passages of the. Control engine Settings are reflected by readings on the manifold pressure gauge. Mixture This control is used to set fuel to air ratio in all modes of operation. Control and cuts off fuel completely for engine shut down. EGT Exhaust Gas Temperature Indicator This indicator is used to identify the lean and best. power fuel air mixtures for various power settings. Tachometer Indicates the rpm of the engine propeller. ADI Automatic Direction Indicator artific ial horizon. RMI Radio Magnetic Indicator, Beechcraft V35B Bonanza.
Pilot Operating Handbook, WEIGHT AND BALANCE TERMINOLOGY. Reference An imaginary vertical plane from which all horizontal distances are measured for balance. Datum purposes, Station A location along the airplane fuselage usually given in terms of distance from the reference. Arm The horizontal distance from the reference datum to the center of gravity C G of an item. Moment The product of the weight of an item multiplied by its arm Moment divided by a constant is. used to simplify balance calculations by reducing the number of digits. Airplane The point at which an airplane would balance if suspended Its distance from the reference. Center of datum is found by dividing the total moment by the total weight of the airplane. C G Arm The arm obtained by adding the airplane s individual moments and dividing the sum by the. total weight, C G The extreme center of gravity locations within which the airplane must be operated at a. Limits given weight, Usable Fuel available for flight planning. Unusable Fuel remaining after a runout test has been completed in accordance with governmental. Fuel regulations, Standard Weight of a standard airplane including unusable fuel full operating flu ids and full oil.
Basic Standard empty weight plus optional equipment. Payload Weight of occupants cargo and baggage, Useful Difference between take off weight or ramp weight if applicable and basic empty weight. Maximum Maximum weight approved for ground maneuvering It includes weight of start taxi and. Ramp run up fuel, Maximum Maximum weight approved for the start of the take off run. Beechcraft V35B Bonanza, Pilot Operating Handbook, Maximum Maximum weight approved for the landing touchdown. Zero Fuel Weight exclusive of usable fuel, This space left intentionally blank. Beechcraft V35B Bonanza, Pilot Operating Handbook, Section II Limitations.
The limitations included in this section have been approved by the Federal Aviation Administration. The following limitations must be observed In the operation of this airplane. AIRSPEED LIMITATIONS, SPEED REMARKS, KNOTS MPH KNOTS MPH. Never Exceed 176 202 177 204 Do not exceed this speed in. VNE any operation, Maximum Structural 139 160 140 161 Do not exceed this speed. Cruising VNO or Vc except in smooth air and then, only with caution. Maneuvering 113 130 114 131 Do not make full, VA or abrupt control. movements above, this speed, Maximum Flap 91 105 91 105 Do not extend flaps or operate.
Extension Extended with flaps extended above, VFE this speed. Maximum Landing 109 125 110 127 Do not extend retract or operate. Gear Operating with landing gear extended, Extended VLO and VLE above this speed except in. AIRSPEED INDICATOR MARKINGS, MARKING SIGNIFICANCE, KNOTS MPH KNOTS MPH. White Arc 49 91 56 105 45 91 52 105 Full Flap Operating Range. Green Arc 58 139 67 160 54 140 62 161 Normal Operating Range. Yellow Arc 139 176 160 202 140 1 77 161 204 Operate with caution only in. smooth air, Red Line 176 202 177 204 Maximum speed for ALL operations. Beechcraft V35B Bonanza, Pilot Operating Handbook, POWER PLANT LIMITATIONS.
A35 Continental E 185 1 or E 185 8, one minute 2300 rpm Full throttle. Maximum continuous, operation 2050 rpm Full throttle. B35 Continental E185 8 S N 51220 and above, one minute 2450 rpm Full throttle. Maximum continuous, operation 2050 rpm Full throttle. Other engines 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 Supplemental. Type Certificate, Aviation Gasoline 80 87 red minimum grade or alternate grades 100LL blue or 100 130 green See.
Engine Manufacturer s Bulletin, Ashless dispersant oils must meet Continental Motors Corporation Specification MHS 24A. Beech two blade 88 inch diameter max propeller, Beechcraft V35B Bonanza. Pilot Operating Handbook, POWER PLANT INSTRUMENT MARKINGS. OIL TEMPERATURE, Caution Yellow Radial 100 F 38 C, Operating Range Green Arc 100 to 225 F 38 to 107 C. Maximum Red Radial 225 F 107 C, OIL PRESSURE, Minimum Pressure Red Radial 30 psi.
Operating Range Green Arc 30 to 60 psi, Maximum Pressure Red Radial 80 psi. TACHOMETER, Operating Range Green Arc 1300 to 2050 rpm. Cautionary Range Yellow Arc 2050 to 2300 rpm, Maximum RPM Red Radial 2300 rpm. Beechcraft V35B Bonanza Pilot Oper ating Handbook 5 Section I General DESCRIPTIVE DATA ENGINE The V35B Bonanza is powered by either a Continental E185 1 or E185 8 six cylinder engine rated for a maximum take off power of 185 hp at 2300 rpm max one minute The maximum continuous rating is 165 hp at 2050 rpm PROPELLER

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