Beechcraft Bonanza V35B Pilot Operating Handbook Download Page 13

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Beechcraft V35B Bonanza
Pilot Operating Handbook

- 12 -

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

CYLINDER HEAD TEMPERATURE

Operating Range (Green Arc)

300° to 460°Fj149° to 238°C

Maximum Temperature (Red Radial)

525°F;274°C

MANIFOLD PRESSURE

Operating Range (Green Arc)

15 to 29.6 in. Hg

Maximum (Red Radial)

29.6 in. Hg

FUEL PRESSURE

Minimum (Red Radial)

9 psi

Operating Range (Green Arc)

11 to 14 psi

Maximum (Red Radial)

14 psi

WEIGHT AND CENTER OF GRAVITY

Maximum Take-off and Landing Weight

2650 lbs

Maximum Ramp Weight

2660 lbs

Zero Fuel Weight

No Structural Limitation

Datum is 83.1 inches forward of center line through forward jack points.

MAC leading edge is 66.7 inches aft of datum. MAC length is 65.3 inches.

CG LIMITS (Gear Down)

Forward:

75.9 inches aft of datum to 2140 lbs with straight line
variation to 83.7 inches at 2650 lbs.

Aft:

85.4 inches aft of datum to 2405 lbs with straight line
variation to 84.4 inches at 2650 lbs.

Summary of Contents for Bonanza V35B

Page 1: ......

Page 2: ...tor 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 EULA 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...

Page 3: ...Beechcraft V35B Bonanza Pilot Operating Handbook 2 3 View Diagram ...

Page 4: ...INE 11 FUEL 11 OIL 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...

Page 5: ... 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 BRAKES 29 GROUND CONTROL 30 ELECTRICAL SYSTEM 30 GENERATOR 30 LIGHTING SYSTEM 31 INTERIOR LIGHTING 31 EXTERIOR LIGHTING 31 HEATING AND VENTILATION ...

Page 6: ...ation 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 usa...

Page 7: ...l 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 re...

Page 8: ... corrected for position and instrument error In this 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 TERMIN...

Page 9: ... 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 Limits The extreme center of gravity locations within which the airplane must be operated at a given weight Usable Fuel Fuel available for flight planning Unusable Fuel Fuel remaining after a runout test has been completed in accordance with government...

Page 10: ...chcraft V35B Bonanza Pilot Operating Handbook 9 Maximum Landing Weight Maximum weight approved for the landing touchdown Zero Fuel Weight Weight exclusive of usable fuel This space left intentionally blank ...

Page 11: ...Maneuvering VA 113 130 114 131 Do not make full or abrupt control movements above this speed Maximum Flap Extension Extended VFE 91 105 91 105 Do not extend flaps or operate with flaps extended above this speed Maximum Landing Gear Operating Extended VLO and VLE 109 125 110 127 Do not extend retract or operate with landing gear extended above this speed except in emergency AIRSPEED INDICATOR MARKI...

Page 12: ...nuous operation 2050 rpm Full throttle NOTE 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 FUEL 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 m...

Page 13: ...C Maximum Temperature Red Radial 525 F 274 C MANIFOLD PRESSURE Operating Range Green Arc 15 to 29 6 in Hg Maximum Red Radial 29 6 in Hg FUEL PRESSURE Minimum Red Radial 9 psi Operating Range Green Arc 11 to 14 psi Maximum Red Radial 14 psi WEIGHT AND CENTER OF GRAVITY Maximum Take off and Landing Weight 2650 lbs Maximum Ramp Weight 2660 lbs Zero Fuel Weight No Structural Limitation Datum is 83 1 i...

Page 14: ...not be flown unless all equipment was operable With appropriate limitations the operation of every system or component installed in the airplane is not necessary when the remaining operative instruments and equipment provide for continued safe operation Operation in accordance with limitations established to maintain airworthiness can permit continued or uninterrupted operation of the airplane tem...

Page 15: ...DLE CUT OFF 2 Fuel Selector Valve OFF 3 Battery Generator and Ignition Switches OFF 4 Extinguish with Fire Extinguisher ENGINE FAILURE ON TAKE OFF DURING GROUND ROLL 1 Throttle CLOSED 2 Braking MAXIMUM 3 Fuel Selector Valve OFF 4 Battery and Generator Switches OFF If airborne and insufficient runway remains for landing 1 Fuel Selector Valve SELECT OTHER MAIN TANK 2 Auxiliary Wobble Fuel Pump PUMP ...

Page 16: ...ANK MORE NEARLY FULL NOTE If the failure was due to the fuel metering valve sticking in the full open position the carburetor will deliver an excess of fuel with constant flooding Shutting off fuel momentarily will clear the engine and may restore normal operation by allowing the spring in the carburetor to reseat the valve c Throttle 1 4 INCH OPEN d Mixture FULL RICH e Auxiliary Wobble Fuel Pump ...

Page 17: ...down 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 approximately 3 inches open but the flight characteristics of the airplane will not be affected except that rate of climb will be reduced Return to the field in a n...

Page 18: ...er one or two minutes switch back to cold air If manifold pressure rises higher than the point observed before applying carburetor heat carburetor icing is indicated c Apply carburetor heat immediately until icing conditions no longer exist Use high power settings and lean mixtures to produce maximum heat under possible icing conditions EMERGENCY SPEED REDUCTION In an emergency the landing gear ma...

Page 19: ... CABIN a Parking Brake SET b Control Lock REMOVE c All Switches OFF d Emergency Locator Transmitter ARMED 2 RIGHT FUSELAGE a Baggage Compartment Door SECURE b Static Pressure Button UNOBSTRUCTED 3 EMPENNAGE a Control Surfaces CHECK b Tie Down REMOVE c Position Light CHECK BEFORE STARTING 1 Seat Belts and Shoulder Harnesses FASTEN 2 Parking Brake SET 3 All Avionics OFF 4 Circuit Breakers IN 5 Landi...

Page 20: ...arter Button Press until engine starts 7 Primer Brief shots until engine starts firing NOTE If a false start occurs or the starter button is released after the ignition switch has been turned to the BOTH position the ignition switch must be turned to the BATT position before the starter button will again energize the starter NOTE If starting fuel pressure is low maintain pressure with auxiliary wo...

Page 21: ...ET a Aileron NEUTRAL b Elevator 00 30 nose down for aft loading 10 Flaps UP 11 Door and Windows SECURE 12 Seat Belts and Shoulder Harnesses SECURE NOTE All reclining seats must be in the upright position during take off 13 Controls FREE 14 Mixture FULL RICH or as required by field elevation 15 Brakes RELEASED 16 Instruments CHECK make final check of manifold pressure fuel pressure and rpm at the s...

Page 22: ...g 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 AP PROACH SPEED 9 Propeller a Manual Hold to HI RPM until maximum is attained b Automatic Propeller Control APC Select AUTO CLIMB NOTE For Balked Landing advance throttle retract gear and flaps select AUTO TAKE OFF moni tor engine RPM and do not exce...

Page 23: ...a 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 addition to several radio navigation combinations optional instruments for which openings are provided in the instrument panel include a vac...

Page 24: ...Gauge 30 Alt Air Source 4 Altimeter 13 CHT Gauge 22 Batter Bus Volts 31 Audio Panel 5 Manifold Pressure 14 Battery Bus Amps 23 Elevator Trim 32 GNS 480 GPS 6 Tachometer 15 Left Fuel Qty 24 Cowl Flaps Ctrl 33 NAV COM Radio 7 OAT Gauge 16 Wing Tanks Qty 25 Flaps Ctrl 34 DME Radio 8 RMI 17 Right Fuel Qty 26 Gear Ctrls 35 ADF Radio 9 Turn Coordinator 18 Starter Magnetos 27 Throttle 36 Autopilot ...

Page 25: ...grouped together immediately above the control console The engine gauge cluster includes the fuel quantity and fuel pressure gauges oil pressure gauge the oil temperature and cylinder head temperature indicators and ammeter MANIFOLD PRESSURE GAUGE AND TACHOMETER The manifold pressure gauge and tachometer are mounted in the instrument panel proper The tachometer is driven by a flexible shaft from t...

Page 26: ...flaps should be open during ground operation take off and climb OIL SYSTEM In the Bonanza s oil system oil is fed to the engine oil pump from a supply tank mounted just above and behind the engine The return oil is picked up by a scavenging pump and returned to the supply tank passing through a cooler which is an integral part of the tank The oil tank capacity is 2 1 2 gallons The filler neck of t...

Page 27: ... heavy cable required to carry the high amperage of the starter circuit The starter is actuated by a key type momentary on switch located on the left of the control column To energize the starter circuit rotate the ignition switch to the START position and hold Before starting it is necessary that the subpanel battery switch be turned on ...

Page 28: ...he propeller uses a Beech R203 100 hub with either R201 217 88 or R203 218 88 blades FUEL SYSTEM The airplane is designed for operation on 80A37 grade red aviation gasoline In the event this grade is not available only a higher rated fuel shall be used CAUTION Before refueling make certain the airplane and fuel dispensing unit are properly grounded Failure to do so creates a fire hazard ...

Page 29: ...ould a take off be made if the fuel indicators are in the 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 Fuel Pump switch to aid in restarting the engine Close the throttl...

Page 30: ...en the gear is up or green when it is down illuminating only when the actuator assembly reaches either extreme In addition a mechanical indicator on the floorboard beneath the control console shows the position of the nose gear Its pointer is linked by a cable to the actuating mechanism and moves simultaneously with it Limit switches and a dynamic brake automatically stop the retract mechanism whe...

Page 31: ...YSTEM The system circuitry is the single wire ground return type with the aircraft structure used as the ground return The battery ON OFF switch and the generator ON OFF switch are located on the switch subpanel on the pilot s lower panel GENERATOR Direct current electric power is supplied by a 25 ampere engine driven generator controlled by a voltage current regulator which automatically adjusts ...

Page 32: ... Two forward outlets are located above and forward of each set of rudder pedals One aft outlet is installed behind the right front seat Two outlets provide heated air for windshield defrosting HEATER OPERATION The cabin heat control is located on the lower 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 mix...

Page 33: ...Beechcraft V35B Bonanza Pilot Operating Handbook 32 ...

Page 34: ...r driven equipment is supplied by an engine driven vacuum pump An adjustable relief valve controls suction by bleeding outside air into the vacuum pump The relief valve and an oil separator which removes oil from the air are located on the forward side of the firewall A suction gauge indicates system vacuum in inches Hg This instrument is located on the instrument panel exact location may vary acc...

Page 35: ...r VFR Cruise at 11 500 feet ROUTE SEGMENT MAGNETIC COURSE DIST NM WIND 11500 FEET DIR KTS OAT 11500 FEET C ALT SETTING IN HG DEN COS COS PUB PUB TBE TBE DHT DHT AMA 1610 1530 1340 1320 1250 55 40 74 87 65 010 30 010 30 100 20 200 20 200 20 5 5 0 9 10 29 60 29 60 29 56 29 56 29 56 At Amarillo Outside Air Temperature 25 C 77 F Field Elevation 3605 ft Altimeter Setting 29 56 in Hg Wind 180 at 10 kts ...

Page 36: ...requires full throttle The manifold pressure and fuel flow may be read from either the cruise power setting table for 139 HP or 120 HP 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 SA 20 C These should be used for flight planning The IOAT values are true temperature values which have been adjusted for the...

Page 37: ...RESS FUEL FLOW PPH GPH TAS KNOTS 10 000 19 9 56 0 9 3 141 19 9 54 2 9 0 141 12 000 18 4 52 7 8 8 138 18 4 51 3 8 6 138 Interpolate for 11 500 feet and the temperature for the appropriate route segment Results of the interpolations are ROUTE SEGMENT MAN PRESS FUEL FLOW PPH GPH TAS KNOTS DEN PUB 18 8 53 3 8 9 139 PUB TBE 18 8 52 9 8 8 139 TBE DHT 18 8 52 2 8 7 139 DHT AMA 18 8 52 2 8 7 139 NOTE The ...

Page 38: ...DHT AMA 65 131 0 30 4 4 Distance required to climb has been subtracted from segment distance TIME FUEL DISTANCE ITEM TIME HRS MINS FUEL GAL DISTANCE NM Start Runup Taxi and Take off acceleration 0 05 1 4 0 Climb 0 13 2 5 25 Cruise 2 13 19 4 296 Total 2 31 23 3 321 Total Flight Time 2 hours 31 minutes Block Speed 321 NM 2 hours 31 minutes 128 knots Reserve Fuel 45 minutes at 83 HP Enter the cruise ...

Page 39: ...he example in addition to presenting an answer for a particular set of conditions also presents the order in which the graphs should normally be used Le if the first item in the example is OAT then enter the graph at the known OAT 2 The reference lines indicate where to begin following guide lines Always project to the reference line first and then follow the guide lines to the next known item 3 I...

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Page 51: ...d the license from the original computer and create a data file demonstrating this You may inquire with FSD regarding this by contacting us in the manner described below under Contacting FSD Other arrangements on subsequent to evaluation by FSD can also be made and inquiries are welcome Reproduction and Distribution You may NOT reproduce or distribute any number of copies of the SOFTWARE PRODUCT W...

Page 52: ...acting FSD 6 LIMITED WARRANTY NO WARRANTIES FSD expressly disclaims any warranty for the SOFTWARE PRODUCT The SOFTWARE PRODUCT and any related documentation is provided as is without warranty of any kind either express or implied including without limitation the implied warranties or merchantability fitness for a particular purpose or non infringement The entire risk arising out of use or performa...

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