Beechcraft Bonanza V35B-TC Owner'S Manual Download

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Summary of Contents for Bonanza V35B-TC

Page 1: ...NLJ ech Gircrah nr pnration ...

Page 2: ...f each 25 or 24 gallon main tank is 22 gallons 2 Maximum usable fuel of each 39 or 40 gallon main tank is 37 gallons 3 Approximate reduction in range with full fuel due to change in usable fuel is a 13 on 22 gallon main tank system b 9 on 37 gallon main tank system 4 On ModelsK 35 M 35 33 and A33 Owners Manuals reduce range by an additional 190 statute miles to account for climb and 45 minutes res...

Page 3: ...o be familiar with the applicable Federal Aviation Regulations concerning operation and maintenance of the airplane and FAR Par 91 General Operating and Flight Rules Likewise your aircraft must be operated and maintained in accordance with FAA Airworthiness Directives which may be issued against your BEECHCRAFT The operation care and maintenance of your airplane after it is delivered to you is you...

Page 4: ...i through iii 1 1 through 1 21 2 1 through 2 6 3 1 through 3 7 4 1 through 4 6 5 1 through 5 7 6 1 through 6 21 7 1 through 7 9 8 1 through 8 3 I A Bonanza V358 TC Original Original Original Original Original Original Original Original Original Original Original ...

Page 5: ...f Systems 1 1 SECTION II Operating Check Lists 2 1 SECTION Ill Normal Procedures 3 1 SECTION IV Emergency Procedures 4 1 SECTION V Limitations 5 1 SECTION VI Performance 6 1 SECTION VII Optional Equipment 7 1 SECTION VIII Servicing 8 1 Turbo Bonanza V35B TC ...

Page 6: ...aps up Gear and Flaps down 74 mph 64 knots CAS 63 mph 55 knots CAS RANGE Includes allowance for starting taxi take off climb and 45 minute reserve 55 Power 198 mph TAS 24 000 feet 550 st mi 478 naut mi 49 gallons 1070 st mi 930 naut mi 80 gallons TAKE OFF DISTANCE 20 Flaps Sea LevelStandard Conditions Ground run 964 Total distance over 50 foot obstacle 1320 LANDING DISTANCE 30 Flaps Sea LevelStand...

Page 7: ...7 7 91 7 l 1 33 5 5 Turbo Bonanza V35B TC iii ...

Page 8: ...the engine for high altitude operation The compressor and its housing are between the ambient air intake and the induction air manifold They are part of the exhaust system and utilize the t1ow of exhaust gases to drive the compressor WASTE GA TE AND EXHAUST BY PASS Waste gate position regulates output of the turbine and therefore the compressed air available to the engine The waste gate is a butte...

Page 9: ...ined when at full throttle the desired manifold pressure is no longer attainable at a given rpm This altitude will vary considerably with air temperature rpm fuel flow and airspeed The following steps illustrate the operation of the system 1 Induction air is taken in through the air filter and ducted to the compressor 2 The induction air is then compressed and ducted to the engine 3 As the waste g...

Page 10: ... INDUCTION AIR COMPRESSED AIR EXHAUST GASES c ALTERNATE AIR DOOR VARIABLE ABSOLUTE PRESSURE CONTROLLER EXHAUST BY PASS WASTE GATE ACTUATOR WASTE GATE TURBOCHARGER SCHEMAT IC ...

Page 11: ...pressor resulting in an increase in manifold pressure The increase in manifold pressure creates a higher mass flow through the engine causing higher turbine speeds and thus further increasing manifold pressure This characteristic may be used to best advantage by allowing the aircraft to accelerate to cruise speed after leveling off and prior to reducing power ENGINE RESPONSE AT HIGH ALTITUDE Respo...

Page 12: ...arm and position the control column as desired The aileron trimmer on the control column hub should be held until the column is repositioned RUDDER PEDALS To adjust the rudder pedals press the spring loaded lever on each pedal arm and move the pedal forward or aft The adjustment lever can also be used to place the right hand set of rudder pedals against the floor when not in use TRIM CONTROLS Elev...

Page 13: ...e adjustments are accomplished by rotating the knob if oil pressure is lost the propeller will go to the full low pitch high rpm position This is because propeller high pitch low rpm is obtained by governor boosted engine oil pressure working against the centrifugal twisting movement of the blades ALTERNATE AIR A pull and release handle below the propeller control can be used to force open the alt...

Page 14: ...gnment and re latch LANDING GEAR SYSTEM CONTROL SWITCH The landing gear is controlled by a two position switch on the right side of the subpanel The switch handle must be pulled out of the safety detent before it can be moved to the opposite position POSITION IND CA TORS The landing gear position indicator lights are located adjacent to the landing gear switch handle Three green lights one for eac...

Page 15: ...r will pop out under overload conditions MANUAL EXTENSION The landing gear can be manually extended by operating a handcrank at the rear of the front seats This procedure is described in Section IV BRAKES The brakes on the main landing gear wheels are operated by applying toe pressure to the rudder pedals The parking brake push pull control is located on the left side of the lower subpanel To set ...

Page 16: ...cold weather The oil temperature operating range is Ioo F to 240 F Monitor the oil temperature gage after starting to assure temperature is above minimum before advancing the throttle and on descending with power reduced to avoid overcooling MANIFOLD PRESSURE AND FUEL FLOW INDICATOR The manifold pressure portion of this instrument indicates the pressure of the fuel air mixture entering the engine ...

Page 17: ...1 10 J Ci O 000 ...

Page 18: ...h a flush type filler cap A visual measuring tab is attached to the filler neck to indicate different levels of servicing The engine driven fuel injector pump delivers approximately 10 gals of excess fuel per hour which bypasses the fuel control and returns to the tank being used Three fuel drains are provided one in each fuel sump on the underside of each wing and one at the fuel system low point...

Page 19: ...11111u 1 E I I _ 11111111111111111111111111111111111 E I I i _________ i I _______ I i L H FUELCELL i l LJ __ __ _ I i I H FUELCELL i 24 5 GALS USAIU STD i 1 I 24 5 GALS USAILE STD 40 GALS tUSAILE OPT i re _ _ __ V N i 40 GALS USAlf E 0 1 VENt111L81 tu111 DRAINQ i i QoRAIN Jcii 11 VENT CHECK STRAINER STl AINElt CHECK VALVE i i VALVE SEAL 1111111 DRAIN 11111 veNt vENt C m r 1 m 31 t m 31 C ...

Page 20: ...ngine oil system is the full pressure wet sump type and has a 12 quart capacity Oil operating temperatures are controlled by an automatic thermostat bypass control The bypass control willlimit oil flow through the oil cooler when operating temperatures are below normal and will permit the oil to bypass the cooler if it should become blocked A full flow integrally mounted oil filter is provided See...

Page 21: ... a malfunction occurs and the light is illuminated and the malfunction cannot be corrected the light can be turned off by pressing its face If an overvoltage condition occurs in flight I Reset the overvoltage relay by momentarily turning the BATTERY switch to OFFthen to ON 2 If the overvoltage condition does not recur continue to use the alternator 3 Should the overvoltage condition persist tum th...

Page 22: ...to the OAT EXTERIOR L Gf lTING The switches for all of the exterior lights are located on the left Each switch is the circuit br akcr vhich 111 open the s vitch if overloaded or shorted The exterior lights consist of navigation lights on the and tail cone and a landing light in the fuselage nose section The landing light can be used for both approach and taxiing For longer battery and lamp service...

Page 23: ... _ FRESH AIR INTAKE NOSE MIXER VALVE COLD POSITION HEATEDAIR INDIVIDUAL OVERHEAD FRESHAIR OUTLETS OPTIONAL OVERHEAD FRESH AIR FIXED EXHAUST n OVERHEAD FRESH AIR SCOOP Q 7 J SHUTOFF VALVE FIXED EXHAUST I REAR OF HAT SHELF 1 16 Turbo Bonanza V35B TC ...

Page 24: ...vents located on the firewall forward of the rudder pedals deliver heated air to the forward cabin when the CABIN HEAT CONTROLis pulled out To deliver heated air to the aft seat outlets pull the AFT CABIN HEAT CONTROL For maximum heat the control is pulled fully out To obtain heated air for defrosting the windshield the DEFROST CONTROL out It may be necessary to vary or close the AFT CABIN HEAT CO...

Page 25: ...er in the overhead panel In addition a fixed exha 1stis provided through the rear of the hat shelf STALL WARNING HORN A stall warning horn on the forward side of the instrument panel sounds a warning signal while there is ample time for the pilot to correct his attitude The horn is triggered by a sensing vane on the leading edge of the left wing and is equally effective at all flight attitudes wei...

Page 26: ... adequate for continuous use to 30 000 feet The oxygen cylinder is located beneath the cover under the front seats The system is available with either four five or six outlets and with either 38 49 or 114 cu ft oxygen cylinder Supply of oxygen to the system is controlled by a shut off valve on the oxygen console The pressure gage indicates the supply of oxygen available 1850 psig is nominal pressu...

Page 27: ... 3 Plug in the mask hose and check for oxygen flow 4 Discontinue use by unplugging the mask and closing the console valve DURATION 1 Prior to flight check for adequate oxygen supply for the number of people at the planned altitude and trip duration 2 Check supply pressure convert to percent of capacity read duration chart multiply by percent of capacity 2000 2 f C 1500 I 0 25 50 75 100 PERCENT OFF...

Page 28: ... 7 u I 5 8 5 5 3 6 7 0 4 4 Example People Gage Pressure Percent Capacity front chart Cylinder Capacity Altitude planned flight Duration full cylinder Duration 80 full 20 000 7 0 3 5 2 3 1 7 1 4 1 1 9 1 4 5 3 0 2 2 1 8 1 5 21 2 10 6 7 0 5 3 4 2 3 5 Turbo Bonanza V358 TC 25 000 30 000 5 8 5 1 2 9 2 5 1 9 1 7 1 4 1 2 1 1 1 0 9 8 7 5 6 6 3 7 3 3 2 5 2 2 1 8 1 6 1 5 1 3 1 2 1 1 17 6 15 4 8 8 7 7 5 8 5 ...

Page 29: ...5B TC This information is based on the recommendations and data compiled by Beech Aircraft Corporation pilots and is intended to assist you in developing a systematic and safe flying technique Made carefully these checks will not only help prevent a mishap or malfunction but will also aid in reducing maintenance costs Turbo Bonanza V35B TC 2 1 ...

Page 30: ...ing Brake SET b Control Lock REMOVE c All Switches OFF NOTE ALT switch may remain in the ON position except in an emergency 2 RIGHT FUSELAGE a Baggagecompartment door SECURE b Static pressure button UNOBSTRUCTED 2 2 Turbo BonanzaV35B TC ...

Page 31: ...HECK Remove Cover d Fuel Tank CHECK QUANTITY e Fuel Filler Cap SECURE 7 LEFT LANDING GEAR a Wheel Well Door Tire and Strut CHECK b Fuel Sump DRAIN c Fuel Selector Valve Sump DRAIN Cover SECURE 8 NOSE SECTION a Cowl Flaps CHECK b Engine Oil CHECK Cap SECURE c Left Cowling SECURE d Propeller CHECK e Wheel Well Doors Tire and Strut CHECK f Landing lights CHECK g Induction Air Intake CLEAR h Engine CH...

Page 32: ...r HIGH RPM 3 Throttle Approximately 1 2 inch open 4 Auxiliary Fuel Pump HI until fuel flow peaks then OFF 5 Throttle Approximately 1 4 inch open 6 Key Lock Switch START POSITION release to BOTH position when engine fires 7 In event of overprime condition a Mixture IDLE CUT OFF b Throttle OPEN c Key Lock Switch START POSITION d As engine fires reduce throttle to IDLE and advance the mixture control...

Page 33: ...ront seats are occupied 11 Flaps CHECK and SET 12 Door and Windows SECURE 13 Seat Belts SECURE 14 Controls FREE 15 Mixture FULL RICH 16 Brakes RELEASED 17 Instruments Check make final check of manifold pressure fuel flow and rpm at the start of the take off run NOTE Add the last 1 1 2 inches of throttle slow y to avoid overboosting the engine when the oil is cold BEFORE LANDING 1 Fuel Selector Val...

Page 34: ... HIGH RPM 5 Throttle CLOSE 6 Mixture IDLE CUT OFF 7 Key Lock Switch OFF after engine stops 8 Battery and Alternator switches OFF 9 Control Lock INSTALL if conditions warrant 10 Release brakes and install wheel chocks if the aircraft is to be left unattended 2 6 Turbo Bonanza V358 TC ...

Page 35: ...t rpm first then manifold pressure Makepower reductions with manifold pressure first then rpm STARTING Refer to the Starting Check List in Section II Makesure that the area around the propeller is clear and free from loose objects Avoid operating the engine on loose gravelor sand Each cranking period should be limited to 30 seconds Allow the starter to cool for 3 to 5 minutes between cranking peri...

Page 36: ...hrottle and full rich operation is recommended during take off CAUTION Neveruse more than 20 flap for any take off Normal take off should be made with flaps up Obstacle take off should be made with 20 flaps Apply take off power and release the brakes Hold the airplane in a near level flight attitude during the take off run until the appropriate airspeed is attained then smoothly and positively app...

Page 37: ...nce are well within the normal operating limitations of the airplane and the pilot For maximum range level flight cruise operations should be at the lowest power that will satisfy the speed requirements The Cruise Operation Graph in Section Vl willbe helpful in obtaining the desired performance Rapid attainment of cruise speed with llllmmum trim adjustment can be achieved by climbing above the des...

Page 38: ...ff The wing contour may be changed by these formations sufficiently that its lift qualities are considerably disturbed and sometimes completely destroyed Complete your normal preflight procedures including a check of the flight controls for complete freedom of movement Conditions for accumulating moisture in the fuel cells are most favorable at low temperatures due to the condensation increase in ...

Page 39: ...ing 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 the plugs STARTING ENGINE Using External Power 1 Connect an external power unit to the aircrafl s optional external power receptacle or to the battery 2 Battery and Alternator Swi...

Page 40: ...ge cylinder 4 Check oil temperature and pressure Both the engine and the turbo charger system depend upon the proper functioning of the oil system TAKE OFF Should the landing gear become wet from running through water or ice delay retraction until the gear has had time to dry It is possible for the gear or the gear doors to freeze in the up position if the gearsare retracted when wet PROPELLER In ...

Page 41: ...omatically and the induction system will operate on alternate air Due to the loss of ram effect a slight drop in manifold pressure will be noted Should the alternate air source door become frozen in the closed position pull and release the T handle below the propeller control The pull and release control actuates a break open lever to force open the door in the air intake duct DESCENT Throughout t...

Page 42: ...osition approximately 3 inches open but the flight characteristics of the airplane wili not be affected Return to the field in a nonnal manner If practicable during the landing flare out have a passenger hold the door to prevent it from swinging open In an emergency it is possible to close the door in flight as follows 1 Slow to approximately 90 mph 78 kts IAS 2 Open the storm window to reduce cab...

Page 43: ... handcrank handle at rear of front seats 4 Engage handcrank and turn counterclockwise as far as possible approximately 50 turns 5 Check mechanical indicator to make certain that gear is down 6 If electrical system is operative check landing gear position light and warning horn 7 Disengagehandcrank Always keep the handcrank strapped in the disengaged position when not in use Do not retract the land...

Page 44: ...d then OFF c Throttle ADVANCE to desHed power f Mixture Control LEAN for altitude as desired 2 Fuel Flow Gage CHECK fuel flow abnormally low a Auxiliary Fuel Pump ON b Mixture Control FULL RJCH c Auxiliary Fuel Pump OFF if performance does no1 improve in a few moments 3 Rough Running Engine a Mixture Control FULL R1CH then lean to altitude if necessary b Keylock Switch CHECK for BOTH position FORC...

Page 45: ...s can be accomplished manually 4 Keylock switch OFF 5 Throttle CLOSED 6 Do not attempt to restart engine GLIDE DISTANCE 35 30 000 25 000 I 20 000 e 15 000 i l 10 000 5000 SL 0 4 4 ASSOCIATED CONDITIONS GEAR UP FLAPS UP COWL FLAPS CLOSED PROPELLER FULL HIGH PITCH LOW RPM GLIDE SPEED 122 MPR IAS NOTES 1 GLIDE DISTANCE IS APPROXIMATELY 2 STATUTE MILES PER 1000 FF ET 2 INCREASE GLIDE DISTANCE APPROXIM...

Page 46: ...ectrical operation of the aircraft on the battery Alternator failure will be indicated by the illumination of the ALT OUT warning light located on the instrument panel below the flight instmments When an alternator failure occurs in flight all non essential electrical load should be discontinued to conserve the battery life EMERGENCY STATIC AIR SOURCE OPTIONAL LIMITATIONS There is a placard to the...

Page 47: ... 83 72 97 102 91 115 120 llO 134 129 153 172 191 215 ALTIMETER CORRECTION EMERGENCY STATIC AIR SOURCE GEAR DOWN FLAPS DOWN 76 95 113 ERROR IN ALTITUDE INDICATION FEET STORM WINDOW CLOSED STORM WINDOW OPEN GEAR UP GEAR DOWN GEAR UP GEAR DOWN FLAPS UP FLAPS DOWN FLAPS UP FLAPS DOWN FEET FEET FEET FEET 4 19 54 15 18 14 69 42 32 0 88 56 53 73 101 123 Actual Altitude Higher Than Indicated Altitude Actu...

Page 48: ... Range Green Arc Maximum Pressure Red Radial Fuel Flow Minimum Red Radial Operating Range Green Arc Maximum Red Radial Tachometer Normal Operating Range Green Arc Maximum Red Radial Cylinder Head Temperature Normal Operating Range Green Arc Maximum Temperature Red Radial Manifold Pressure Normal Operating Range Green Arc Maximum at Sea Level Red Radial Turbo Bonanza V35B TC 100 F 100 to 240 F 240 ...

Page 49: ... Maximum Structural Cruising Speed 190 mph l65 kts APPROVED MANEUVERS 3400 POUNDS MANEUVER Chandelle Steep Turn Lazy Eight Stall Except Whip Spins are prohibited DESIGN LOAD FACTORS 3400 lb 4 4G positive maneuvering load factor with flaps up ENTRY SPEED CAS 152 mph 132 knots 152 mph 132 knots 152 mph 132 knots Use Slow deceleration 2 G positive maneuvering load factor with flaps down WEIGHT AND CE...

Page 50: ...ad moments 2 Record the weight and corresponding moment of each useful load item to be carried These values are found on the Useful Load Weight and Moments Table 3 Total the weight and moment columns The total weight must not exceed the maximum allowable gross weight for take off and the total moment must be within the minimum and maximum moments shown on the Gross Weight Moment Llmits Envelope Th...

Page 51: ...203 221 248 270 293 315 338 360 Front Seats 4 RearSeats 5 Fifth and Sixth Fwd PositionAft Position Seats 6 ARM 85 ARM 121 ARM 136 ARM 150 Weight Moment WeiSiht Moment Moment Weight Moment 120 102 120 145 163 30 45 130 111 130 157 177 40 60 140 ll9 140 169 190 50 75 150 128 150 182 204 60 90 160 136 160 194 218 70 105 170 145 170 206 231 80 130 180 153 180 218 245 90 135 190 162 190 230 258 100 150...

Page 52: ...75 54 73 60 90 65 87 70 105 76 102 80 120 86 116 90 135 97 131 100 150 108 145 110 165 119 160 120 180 130 174 130 195 140 189 140 210 151 203 150 225 162 218 160 240 173 232 170 255 184 247 180 270 194 261 190 285 205 276 200 300 216 290 210 315 305 220 330 319 230 345 334 240 360 348 250 375 363 260 390 377 270 405 392 Turbo Bonanza V35B TC 5 5 ...

Page 53: ... the gross weight moment limits table 10 Less fuel 49 gals 11 Total at landing check this point on the gross weight moment limit table SAMPLE WEIGHT LBS 2110 23 294 340 340 70 3177 294 2883 AIRPLANEYOUR MOMENT WEIGHT 100 Lbs 1652 6 221 L U 398 98 2665 221 2444 AIRPLANE MOMENT 100 When the rear seats are removed subtract their respective weights and moment 100 from the FAA Certificated Weight and M...

Page 54: ...00 2700 2600 2500 2400 2300 2200 2100 2000 74 76 78 CENTER OF GRAVITY INCHES AFT OF DATUM ENVELOPE BASED ON THE FOLLOWING WEIGHT AND CENTER OF GRAVITY LIMIT DATA LANDING GEAR DOWN en 0 P I i S i µ1 WEIGHT CONDITION 3400 LB MAX TAKE OFF LANDING FORWARD C G LIMIT 82 1 AFT C G LIMIT 84 4 3000 LB 78 0 85 7 2900 LB OR LESS 77 0 85 7 Turbo Bonanza V35B TC 5 7 ...

Page 55: ...tual conditions must be made AIRSPEEDS 3400 POUNDS TAKE OFF SPEEDS IAS Normal take off 0 flaps Take off Climb out at 50 feet Obstacle take off 20 flaps Take off Climb out at 50 feet 82 mph 71 knots 93 mph 81 knots 77 mph 67 knots 77 mph 67 knots CLIMB SPEEDS IAS with gearand flaps up Cruising climb speed 28 in Hg at 2500 rpm Best Rate of climb Speed 5000 ft Best Angle of ClimbSpeed 5000 ft LANDING...

Page 56: ... FLAPS UP ON 61 mph 63 mph 71 mph 86mph 53 kts 55 kts 61 kts 75 kts 74mph 76mph 86mph 105 mph OFF 64 kts 66 kts 74 kts 91 kts GEAR AND FLAPS DOWN ON 50mph 52mph 58mph 71 mph 44 kts 45 kts 51 kts 62 kts 63mpn 65mph 73 mph 89mph OFF 55 kts 57 kts 64 kts 78 kts 6 2 Turbo Bonanza V35B TC ...

Page 57: ...ower Setting Sea Level 2000 ft Horsepower Setting 4000 ft 6000 ft Horsepower Setting 10 000 ft 15 000 ft Horsepower Setting 20 000 ft 25 000 ft Range 75 Maximum Continuous Power Range 65 Maximum Continuous Power Range 55 Maximum Continuous Power Range 45 Maximum Continuous Power Normal Landing Distance Obstacle Landing Distance Turbo Bonanza V35B TC 6 4 6 5 6 6 6 7 6 8 6 9 6 10 6 11 6 12 6 13 6 14...

Page 58: ...DIRECTION AND FLlGHT PATH 20 HEADWIND COMPONENT CROSSWIND COMPONENT 9 5 KNOTS 3 5 KNOTS t H l l t HHIH 4 1 200 H Wtt W 14 1 µ 1 W l i W l 30 H l l H if d o _IH HH H _ _IH _ H H µ IH 1 H __ lw 6 n i_ t_t_ _ _ _ w 1 t H t t 11 r t l l _1 t N t 1 1 1 t_ HH Q l d 90 0 10 20 30 40 50 60 CROSSWIND COMPONENT KNOTS Turbo Bonanza V35B TC ...

Page 59: ... 50 FT IAS TAKE OFF SPEED ASSUMES ZERO INSTR ERROR WEIGHT UFT OFF 50 FEET POUNDS MPH KNOTS MPH KNOTS 3400 81 70 92 80 3200 79 69 90 78 3000 76 66 87 76 2800 73 63 84 73 2600 70 61 80 70 2400 67 58 77 67 I r 1 r 1 f C z 75 F 4000 FT 3200 LBS 10 KNOTS 2190 FT 1292 FT 79 MPH 90 MPH 6000 E r 1 t I 5000 H PRESSURE lff LTITUD FEET 8000 i l 6000 4000 2000 SL 1It r r t _ j ISA L l fl l L__ __ __ t 1JL I I...

Page 60: ...0 FT OVER A 50 FT OBSTACLE IAS TAKE OFF SPEED WEIGHT ASSUMES ZERO INSTR ERROR POUNDS LIFT OFF 50 FEET MPH KNOTS MPH KNOTS 3400 77 67 77 67 3200 75 65 75 65 3000 72 63 72 63 2800 69 60 69 60 2600 66 57 66 57 2400 63 55 63 55 T i i ti I fz1 f fi z t tl l ti fz1 t tl tl I 1 i PRESSURE I ALTITUDE FEET I t t 8000 6000 4 i 4000 F 2000 L ISA ttrt I I I I I 0 20 40 60 80 100 24 26 28 30 32 34 0 10 20 30 7...

Page 61: ...0 8000 4000 s L 80 MAXIMUMCLIMB CLIMB SPEEDS ASSOCIATED CONDITIONS POWER WEIGHT GEAR FLAPS MAXIMUM CONTINUOUS POWER 3400 LBS UP UP BEST ANGLE BEST RATE OF CLIMB OF CUMB 90 100 1 0 1 0 INDICATED AIRSPEED MPH Turbo Bonanza V35B TC 130 6 7 ...

Page 62: ...0 l 0 16000 i 00 12000 0 6 8 MAXIMUMCLIMB RATE OF CLIMB ASSOCIATED CONDITIONS POWER FLAPS GEAR AIRSPEED 500 MAXIMUM CONTINUOUS POWER UP UP BEST RATE OF CLIMB SPEED 1000 1500 RATE OF CLIMB FT Mlli Turbo Bonanza V35B TC 2000 2500 ...

Page 63: ...g t0J t cf I t g 0 MCP 75 80 85 C CRUISE CLIMB TIME FUELAND DISTANCE GROSS WEIGHT 3400 LBS CLIMB SPEED 130 MPH lASl MP RPM 24 5 2500 26 0 2500 28 0 2500 1 Wt 0 Turbo Bonanza V35B TC FUEL FLOW 17 7 18 8 20 3 0 g 0 U 0 0 0 0 0 0 0 6 9 ...

Page 64: ...0 171 5 65 2300 185 6 70 2400 200 7 75 2500 214 POWER CAN BE ATTAINED Bf J C ASING ENGINE RPM t H t H t H t f h n 30000 F Lt 28000 D 24000 tP 22000 I 2000 s L J Jdtl tJ tt 1 tJ t t 1 i i w jC ttttµ 1 ttt 4tW tj tttt i tt t t t t l l tl tt 1 tt1 tl 180 200 220 240 140 160 TRUE AIRSPEED MPH 6 10 Turbo Bonanza V35B TC ...

Page 65: ... 14 13 12 11 10 9 FUELCONSUMPTION VS BRAKE HORSEPOWER TAKE OFF 100 95 90 85 PER CENT MAXIMUM CONTINUOUS POWER 80 75 C I 65 e 55 45 i 4 t 1 120 130 140 150 180 170 180 190 200 210 2 0 230 240 1250 260 I270 1280 I29l BRAKE HORSEPOWJ R Turbo Bonanza V358 TC 6 11 ...

Page 66: ...RPM RPM 75 214 15 7 23 4 25 5 20 65 85 13 7 20 8 22 6 23 8 55 157 I l 8 18 3 19 7 20 7 45 128 10 0 15 9 17 l 17 8 75 214 15 7 24 1 26 4 J 65 185 l3 21 4 23 3 24 5 55 157 11 8 18 8 20 2 21 3 45 128 10 0 16 2 I 7 4 18 1 75 214 15 7 24 8 20 65 185 13 7 21 9 23 9 25 2 55 157 11 8 19 2 20 7 21 8 45 128 10 0 16 4 17 6 18 4 75 214 15 7 25 5 40 65 185 l 22 5 24 6 25 9 55 157 11 19 7 21 3 22 5 45 128 10 0 ...

Page 67: ...HP GAL HR RPM RP RPM 75 214 15 7 23 0 25 2 26 5 20 65 185 13 7 20 2 21 9 23 1 55 157 11 8 17 9 19 3 20 3 45 128 10 0 l5 7 16 8 I7 6 75 214 15 7 23 7 26 0 0 65 185 13 7 20 8 22 6 23 9 55 157 11 8 18 3 19 8 20 9 45 128 10 0 16 1 17 2 18 I 75 214 15 7 24 5 20 65 185 13 7 21 4 23 3 24 7 55 157 11 8 18 8 20 3 21 4 45 128 10 0 16 5 17 7 18 6 75 214 15 7 25 3 40 65 185 13 7 22 0 24 0 25 4 55 157 11 8 19 ...

Page 68: ... 9 20 24 7 I 26 0 2L3 22 3 18 5 19 4 40 22 0 t 60 22 0 18 9 I 19 9 26 4 80 22 6 I 23 8 19 3 20 3 75 65 45 75 65 5 l 45 75 i 65 l 4 I 55 l 7 i 55 4_ 65 75 65 55 45 7l4 185 I 128 l 14 85 714 iS5 I I 214 _un 157 l 4 I iss 128 214 l 8 j 7 l28 I i u L8 tn rJ 1 1 7 11 I_ J 1 10 0 1 7 1 1 11 8 l0 0 i l 3 7 11 1n o l 7 I3 7 i ltJ 0 1 75 I 14 l 1 7 I 1 5 l 1 i 51 1 i r t _j I 4 i I 128 1 52 23 0 0 2 l 7 9 ...

Page 69: ...ETTING TSIO 520 D 25 000 FEET OAT I FUEL MPAT MPAT MPAT 7 FLOW 2500 2300 2200 OF I BHP BHP GAL HR RPM RPM RPM 75 214 15 7 24 9 80 65 185 13 7 20 6 55 157 11 8 18 2 20 4 45 128 10 0 15 3 16 4 j 75 214 15 7 25 9 I 60 65 185 13 7 21 6 55 157 11 8 18 6 21 3 45 128 10 0 15 7 16 9 i 75 214 15 7 40 65 185 13 7 22 7 55 157 11 8 19 1 45 128 I0 0 16 2 17 4 75 214 15 7 20 65 185 13 7 55 I57 J 1 8 19 6 45 128...

Page 70: ...1111111 TRUE AIRSPEED MPH 230 225 I I 218 I I 1 r 212 c I I 0 I I I 0 205 l 1 l 198 Ll 191 200 400 600 RANGE STATUTE MILES f d 0 00 800 1000 ASSOCIATED CONDITIONS CLIMB 2500 RPM POWER 28 0 IN HG WEIGHT 3400 LBS FUEL CONSUMPTION 15 7 GPH NOTE RANGE INCLUDES START TAXI AND CLIMB WITH 45 MIN RESERVE AT 45 MAXIMUM CONTINUOUS POWER ...

Page 71: ...l J J L l LJ l l U TRUE AIRSPE D MPH 221 L 218 ll 212 f f l I I 206 c3 J L L 200 L LL 194 1 _ LJ 188 I _ 181 200 400 600 800 RANGE STATUTE MILES i 0 co 1000 ASSOCIATED CONDITIONS CLIMB POWER WEIGHT FUEL CONSUMPTION fQll 2500 RPM 28 0 IN HG 3400 LBS 13 7 GPH RANGE INCLUDES START TAXI AND CLIMB WITH 45 MIN RESERVE AT 45 MAXIMUM CONTINUOUS POWER ...

Page 72: ... I I I I I I I I I I TRUE AIRSPEED MPH 201 t I I 1198 11 195 191 t rt _l_ J 186 c3 r ai 0 o _ o 75 H I i ctl69 t 200 400 600 800 RANGE STATUTE MILES f 0 c o I 1000 ASSOCIATED CONDITIONS CLIMB 2500 RPM POWER 28 0 IN HG WEIGHT 3400 LBS FUEL CONSUMPTION 11 8 GPH RANGE INCLUDES START TAXI AND CLIMB WITH 45 MIN RESERVE AT 45 MAXIMUM CONTINUOUS POWER ...

Page 73: ...RSPEED MPH 154 f I I I I 164 rtt 166 t 164 j j c I I I i 0 162 I I I 158 I I I 154 200 400 600 800 RANGE STATUTE MILES _ _ c 0 C0 1000 ASSOCIATED CONDITIONS CLIMB 2500 RPM POWER 28 0 IN HG WEIGHT 3400 LBS FUEL CONSUMPTION 10 0 GPH NOTE RANGE INCLUDES START TAXI AND CLIMB WITH 45 MIN RESERVE AT 45 MAXIMUM CONTINUOUS POWER ...

Page 74: ...RY SURFACE OVER A 50 FT OBSTACLE 1475 FT SPEED IAS AS TABULATED NOTE GROUND ROLL IS APPROX 53 OF TOTAL LANDING DISTANCE OVER A 50 FT OBSTACLE GROUND ROLL 53 OF 1475 782 FT IAS APPROACH SPEED 87 MPH IAS WEIGHT POUNDS LA SAPPROACH SPEED ASSUMES ZERO INSTR ERROR 3400 3200 3000 2800 2600 MPH 90 87 84 81 78 75 KNOTS 78 76 73 70 68 65 0 20 40 60 80 100 24 26 28 30 32 34 0 10 20 30 OAT F WEIGHT X 100 POU...

Page 75: ...000 550 FT JAS APPROACH SPEED 76 MPH BRAKING MAXIMUM NOTE GROUND ROLL IS APPROX 55 OF TOTAL LANDING DISTANCE OVER A 50 FT OBSTACLE IAS APPROACH SPEED WEIGHT ASSUMES ZERO INSTR ERROR POUNDS MPH KNOTS 3400 80 76 3200 78 68 3000 76 66 2800 73 63 2600 70 61 2400 67 58 i r i r i C C z z r i r i fa fa PRESSURE ALTITUDE FEET 8000 6000 4000 2000 SL ISA 4 r I I I 0 20 40 60 80 10024 26 28 30 32 34 0 10 20 ...

Page 76: ...ating at a throttle position corresponding to approximately 18 inches or less of manifold pressure 2 Landing Gear Retraction With the landing gear safety system ON OFF switch in the ON position the landing gear will not retract unless 1 The landing gear position switch is in the UP position 2 The airspeed is above approximately 90 mph IAS and 3 The engine is operating at a throttle position corres...

Page 77: ... gear position switch The ON OFF switch returns normally to the ON position unless the pilot places the switch in the OFFposition 5 Landing gearcircuit breaker IN before take off PRESSURESYSTEM Pressure for gyroscopic flight instruments and other pressure operated optional equipment is supplied by an engine driven pressure pump Pressure is controlled by an adjustable pressure regulator on the forw...

Page 78: ... have a standard AN type plug check the polarity and connect the positive lead from the external power source to the positive battery terminal and the negative lead to the negative battery terminal EMERGENCY STATIC AIR SOURCE Operation of the emergency static air system is described in Section IV EmergencyProcedures ELECTRIC ELEVATOR TRIM A system OFF ON control switch is located on the instrument...

Page 79: ...at 1650 F which is the maximum allowable for this installation For level flight at 75 power or less the EGT unit should be used in the following manner l Lean the mixture until temperature peaks on the EGT gage Record peak temperature by moving the hand to coincide with the star on the dial face at the peak The hand is moved by turning the adjusting screw on the front of the gage NORMAL CRUISEMIXT...

Page 80: ... system NORMAL 1 To place the system in operation move propeller deice switch to the ON position The system may be operated continuously in flight and will function automatically until the switch is turned OFF 2 Propeller imbalance may be relieved by varying rpm Increase rpm briefly and return to desired setting repeating if necessary NOTE Do not operate the system with the engine inoperative EMER...

Page 81: ... To place the system in operation move the propeller deice switch to the ON position The system may be operated continuously in flight and will function automatically until the switch is turned off 2 Propeller imbalance may be relieved by varying rpm Increase rpm briefly and return to desired setting repeating if necessary 3 Do not attempt to operate the system with engine inoperative 4 The use of...

Page 82: ...ility Augmentation Disconnect when depressed 2 Stability Augmentation ON OFF switch located on the right circuit breaker panel provides complete system disengagement when in the OFF position 3 ROLLTRIMknob provides command trim function Clockwise rotation allows trim to the right counter clockwise rotation allows trim to the left EMERGENCY 1 In the event of an electrical malfunction the Stability ...

Page 83: ...PlLOT S NOTES 7 8 Turbo Bonanza V35B TC ...

Page 84: ...Pl LOT S NOTES Turbo Bonanza V358 TC 7 9 ...

Page 85: ...serial number appears on the model designation placard attached to the side of the fuselagejust under the baggage door GROUND HANDLING The three view drawing shows the minimum hangar clearances for a standard airplane Allowances must be made for any special radio antennas TOWING One man can move the airplane on a smooth and level surface using the hand tow bar furnished with the loose equipment At...

Page 86: ...ft 3 Using nylon line or chain of sufficient strength secure the airplane at the three points provided DO NOTOVERTIGHTEN if the line at the rear of the fuselage is excessively tight the nose may rise and produce lift due to the angle of attack of the wings 4 Releasethe parking brake If extremely high winds are anticipated a vertical tail post can be installed at the rear tie down lug and a tie dow...

Page 87: ... fuel cellscompletely empty for more than a few days as the cell inner liners may dry out and crack permitting fuel to diffuse through the wallsof the cell after refueling If the cells are to be left empty for a week or more a thin coating of light engine oil should be sprayed flushed or rubbed onto the inner liner of the cells FUEL DRAINS Open the three snap type fuel drains daily to purge any co...

Page 88: ...l door Sump capacity is 12 quarts The oil and the oil filter should be changed every l 00 hours under normal operating conditions To assure complete drainage the engine should be at operating temperature 1 Remove the access plate from the engine cowl on the lower right side 2 Locate the oil sump drain plug at the low point of the engine sump 3 Remove the plug button below the sump drain and insert...

Page 89: ...hecked frequently for obstructions RECHARGING THE BATTERY UsingExternal Power 1 Connect an auxiliary power unit to the airplane s external power receptacle or to the battery terminals 2 Battery switch OFF 3 Set the output of the unit at 13 75 to 14 25 volts 4 External power unit ON 5 After battery has been charged turn the external power unit OFF and disconnect from the airplane TIRES An inflation...

Page 90: ...aterial from the exposed piston with a soft cloth moistened with hydraulic fluid To Replenish Strut Hydraulic Fluid 1 Remove the air valve cap depress the valve core and allow the strut to fully compress 2 Raise and block the strut 1 4 inch from the compressed position WARNING Do not remove the valve body assembly until all air pressure has been released or it may blow off causing injury to person...

Page 91: ...reen should be washed with soap and water every 100 hours of normal operation If the aircraft is operated in dusty conditions the filter should be cleaned more frequently The in line filter is located between the pressure regulator and the instruments This filter should be changed every 300 hours of operation INDUCTION AIR FILTER This filter should be inspected for foreign matter at least once dur...

Page 92: ...o prevent damage to the system 3 Closethe cylinder shutoff valveand the console panel shutoff valve 4 Slide the pilot s or copilot s seat aft until the filler valve is clear then remove the cap from the filler valveand attach the recharging outlet 5 Open the cylinder shutoff valve and slowly fill the cylinder to 1850 50 psi at a temperature of 70 F This pressure may be increased an additional 3 5 ...

Page 93: ...d the ground polarity of the alternator are the same 2 When connecting a booster battery be sure to connect the negative battery terminals together and the positive battery terminals together 3 Whenusing a battery charger connect the positive lead of the chargerto the positive battery terminal and the negative lead of the charger to the negativebattery terminal 4 Do not operate an alternator on op...

Page 94: ...ant that all nicks and scratches be smoothed out and polished Your BEECHCRAFT Certified Service Station will be glad to answer any questions concerning propeller blade repair WARNING When working on a propeller always make certain that the ignition switch is off and that the engine has cooled completely WHEN MOVING A PROPELLER STAND IN THE CLEAR there is always some danger of a cylinder firing whe...

Page 95: ...rface with clean water or a mild soap solution then rub lightly with a grit free soft cloth sponge or chamois Use trisodium phosphate completely dissolved in water to remove oil and grease film To remove stubborn grease and oil deposits use hexane aliphatic naphtha or methanol Rinse with clean water avoid prolonged rubbing CAUTION Do not use gasoline benzene acetone carbon tetrachloride fire extin...

Page 96: ...EL 3 C a CLEANFUELINJECTIONCONTROLVALVESCREEN jl 12 CD CLEANINDUCTIONAIR FILTER 13 g Ql 50 Hrs DRAINSTATICAIR LINES 7 LUBRICATEELEVATORTABCONTROL E N Ql LUBRICATELANDINGGEARUPLOCKROLLERS M w C1I CD CHANGEENGINEOIL 11 i CHANGEENGINEOIL FILTER 4 100 Hrs CLEANFUEL SELECTORVALVESTRAINER 9 CLEANPRESSUREPUMPINTAKEFILTER 5 LUBRICATEAILERONCONTROLLINKAGE L LUBRICATECABINDOORMECHANISM F ...

Page 97: ...RPEDALS SERVICEFLAPMOTORGEARBOX 300 Hrs SERVICELANDINGGEARMOTORREDUCTIONGEARS SERVICELANDINGGEARACTUATORGEARBOX CHANGEPRESSURESYSTEMIN LINEFILTER 1000Hrs LUBRICATEELEVATORTABMECHANISM LUBRICATEFLAPACTUATORS ASREQ LUBRICATETHEMAGNETOBREAKERPOINTS Numbersrefer to the ServicingPoints Diagram Letters refer to the LubricationPoints Diagram Pressurelubricate prelubed sealedbearingwith MIL G 23827greasea...

Page 98: ...LUBRICATION POINTS A D E B 8 14 Turbo Bonanza V358 TC ...

Page 99: ...K L HANO OR PACK I FLUID CONTAINER 0 p Q ZERK FITTING SQUIRT CAN NOTE Letters are keyed to the Service Schedule Numbers refer to items in the Consumable Materials Chart Turbo Bonanza V358 TC 8 15 ...

Page 100: ...SERVICING POINTS I I 8 16 Turbo Bonanza V35B TC ...

Page 101: ... No 20 5 Engine Oil SAE No 30 Below 40 F SAE No 50 Above 40 F 6 Engine Fuel Grade 100 130 Green 7 Solvent Federal Specification P D 680 8 Lubricant SAE No 20 9 Lubricant Mobil Compound GG 10 Lubricating Oil Gear MIL L 6086 Grade M 11 Grease Aircraft and Instrument MIL G 23827 tl2 Lubricant Rubber Seal Oakite 6 Compound 13 Naphtha Aliphatic Federal Specification TT N 95 Turbo BonanzaV35B TC 8 17 ...

Page 102: ...Breathing MIL O 27210 In extremely cold climates use MIL G 23827 grease in place of MIL G 7711 These greasesharmful to paint Use only detergent oil Continental Motors Corp Spec MHS 24A See servicingdata and Approved Engine OilsChart If 100 130 grade fuel not available use 115 145 grade fuel purple tProduct of Oakite Products Inc New York 6 New York ttFor sealing threads on oxygen lines To be used ...

Page 103: ...dition On condition On condition On condition On condition On condition On condition POWER PLANT Every 1500 hours On condition Engine vibration isolator mounts Exhaust system Starter Alternator OilCooler Propeller Propeller controls Propeller governor Fuel Pressure Pump On condition On condition Inspect at engine overhaul overhaul or replace on condition On condition On condition replace when cont...

Page 104: ...ure indicator Tachometer Flap position indicator Free air temperature indicator All hose Pressure system filter Air pressure regulator valve On condition On condition Every 2000 hours On condition Every 2000 hours Every 2000 hours Every 2000 hours FUEL SYSTEM On condition On condition On condition On condition Inspect every 600 hours Overhaul every 1200 hours Every 1200 hours On condition INSTRUME...

Page 105: ...l and replacement times are considered a guide only and are not mandatory Various climatic and other conditions may either extend or decrease these times When inspections and service experience indicate overhaul or replacement periods may be adjusted accordingly All items not included in this listing are to be overhauled or replaced when necessary The recommended engine overhaul period is made on ...

Page 106: ...eries D Esso Aviation and Enco Avia tion in grades E65 E80 EIOOand E120 Kendall Aviation Oil Type D Phillips 66 Aviation Oil Type A replaces RD Aviation Oil Aeroshell Oil W Grade 120 Nominal SAE 60 Military Grade 1120 Grade 100 Nominal SAE 50 Military Grade 1100 Grade 80 Nominal SAE 40 Military Grade 1080 Grade 65 Nominal SAE 20 or 30 Military Grade 1065 Aero Red Band HD SAE 50 Aero Gray Band HD S...

Page 107: ...Aircraft Engine Oil Premium AD Grades 65 80 100 Ashless Detergent Oils NOTE This chart lists all oils which were certified as meeting the requirements of Continental Motors Corporation Specification MHS 24A at the time this manual was published Any other oil which conforms to this specification may be used Turbo Bonanza V358 TC 8 23 ...

Page 108: ... Instrument light post Landing gear position light Landing gear visual indicator light Landing light nose section Landing light nose shock strut Navigation light tail cone Navigation light wing Rotating beacon Grimes Rotating beacon Whelen Strobe lights Bullock 8 24 Turbo BonanzaV35B TC NUMBER 330 89 1813 GE 53 1816 330 330 53 4313 4313 93 1512 A 7079B 12 WRM 44 R4316 ...

Page 109: ...t Exhaust Vents Fresh Air Outlets Ventilation Check Lists Before Landing Before Starting Before Take Off Preflight Shutdown Starting Cleaning Engine Exterior Painted Surfaces Interior Windshield Windows Climb Speeds Cold Weather Operation Consumable Materials A B C Turbo Bonanza V35B TC 5 2 6 l l 6 l 14 4 5 l 2 5 2 l 13 8 5 8 5 1 8 8 7 8 24 4 1 1 18 1 18 1 17 2 5 2 4 2 5 2 2 2 6 2 4 8 11 8 10 8 11...

Page 110: ...vator Trim Emergency Descent Exit Static Air Source Procedures Engine Cleaning Cold Weather Operation Fire Instruments Limitations Malfunction in Flight Oils Approved Response at High Altitude Starting Warm Up Exhaust Gas Temperature Indicator D E 8 26 Turbo Bonanza V35B TC 1 5 8 2 1 5 1 6 1 5 1 6 1 7 1 2 3 3 7 5 7 6 3 7 4 5 4 1 1 13 7 3 4 5 4 5 4 5 4 1 8 11 3 4 4 4 1 9 5 1 4 3 8 22 1 4 2 4 3 1 3 ...

Page 111: ...Distance Ground Handling Heating and Ventilating System Operation Schematic Horn Landing Gear Warning Stall Warning Induction Air Filter Servicing Induction System Icing Instrument Markings Eng Instrument Panel Instruments Engine F G H Turbo Bonanza V35B TC 4 5 1 15 7 3 8 5 1 6 1 5 1 5 1 11 1 11 1 9 1 11 1 12 8 3 1 l l J 4 4 8 1 1 15 1 17 1 16 1 18 1 18 8 7 3 7 _5 1 1 10 1 9 5 1 8 27 ...

Page 112: ...on Indicators Safety Switch Warning Horn Lighting Exteior Interior Limitaitons Airspeed Approved Maneuvers Engine Instrument Markings Eng Weight and Balance Load Factors Lubrications Points Magnetos Minor Maintenance Maintenance Minor Alternators J L M 8 28 Turbo Bonanza V35B TC 8 11 1 14 8 2 8 24 2 5 4 3 4 5 6 1 1 7 1 8 1 8 7 1 1 8 4 2 1 7 1 7 1 8 1 15 1 14 5 1 5 2 5 2 5 1 5 1 5 3 5 2 8 15 8 9 8 ...

Page 113: ...ng Take Off Oil System Servicing Oils Approved Overhaul and Replacement Guide Oxygen System Duration Servicing 0 p Performance Graphs See performance graph index Powerplant Controls Preflight Inspection Pressure System Servicing Propeller Minor Maintenance Rudder Pedals R Turbo Bonanza V358 TC 8 9 8 19 8 10 8 9 5 2 14 14 1 9 14 34 6 21 3 2 6 5 1 13 84 8 22 8 19 1 19 1 21 8 8 6 3 1 6 2 2 34 7 2 8 7...

Page 114: ...eds Stall Warning Horn Starter Starting Engine Static Air Emergency Source Take Off Before Check Speeds Taxiing Tie Down Tires Servicing Towing Trim Controls Turbocharger Operational Characteristics Ventilating and Heating System s T V 8 30 Turbo Bonanza V35B TC 1 18 7 2 8 12 8 1 8 5 8 7 8 3 8 7 84 8 8 84 8 5 8 5 ii 4 1 7 7 3 3 6 2 1 18 1 14 24 34 3 5 4 5 7 3 3 2 3 6 2 5 3 6 6 1 3 1 3 6 8 2 8 5 8 ...

Page 115: ...Warm Up Engine Warning Horn Landing Gear Stall Weight Balance Windshield and Windows Cleaning Wing Flaps w Turbo Bonanza V35B TC 3 5 1 8 1 18 5 3 8 11 1 5 8 31 ...

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Beechcraft Bonanza V35B-TC, Owner'S Manual

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