Airplane Flight Manual

covered in the items contained herein. For limitations, procedures and performance not contained in this supplement, consult the manual proper. I. LIMITATIONS: The following limitation are to be observed in the operation of this airplane equipped with a Continental TSI0-520-D Turbocharged engine. A. Engine Limits: Take-off and maximum continuous operation: 285 hp. 2700 rpm, full throttle: B. Propeller: Manufactured by McCauley Industrial Corporation Hub 2A36C82 3A32C76-T Blade 84B-2 82NB-2 Manufactured by Hartzel Propeller, Incorporated Hub PHC-A3VF-4 Blade V8433-4R FAA APPROVED: REVISED: 12-02-65 03-01-66 REVISED: 05-11-66 REVISED: 12-29-66 REVISED: 10-25-67 REVISED: REVISED: 11-18-69 OCT 17 1995 Page 1 of 8 GARRETT AVIATION SERVICES FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT ΤΟ BEECH MODEL S35 BONANZA BEECH MODEL V35 BONANZA BEECH MODEL V35A BONANZA BEECH MODEL V35B BONANZA MODIFIED IN ACCORDANCE WITH STC SA1035WE C. Power Plant Instruments: Fuel Flow: Green Arc or Bank (operating range) 6.9 to 24.3 gph or 41.4 to 145.8 pph; Red Line (max) 18.2 psi; Red Line (min) 1.5 psi. Manifold Pressure: Green Arc or Line (normal operating range) 15 to 32.5 in. Hg; Red Radial or Line (max) 32.5 in. Hg. D. Airspeed Limits: E. Above 22,500 ft. reduce VNE speed 5 mph per 1,000 feet. Max. power continuous climb SL 12,000 Ft. 112 IAS min. ft. 125 IAS min. Placards: AUXILIARY FUEL PUMP OPERATION In full view of pilot: 1,000 feet." On engine control "Forward Cowl Flaps Above 12,000 - "High boost, Off, Low Boost." "Above 22,500 ft. reduce VNE speed 5 mph per pedestal: "Alternate Air, Pull and Release", Pull Open" . II. PROCEDURES: NOTE: 1. This aircraft has not been evaluated by the FAA above 25,000 feet. 2. Flight operation is not recommended above 10,000 ft., unless a satisfactory oxygen supply is available for all occupants. FAA APPROVED: 12-02-65 REVISED: 03-01-66 REVISED: 05-11-66 REVISED: 12-29-66 REVISED: 10-25-67 REVISED: 11-18-69 OCT 17 1995 REVISED: Page 2 of 8 GARRETT AVIATION SERVICES FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT ΤΟ BEECH MODEL S35 BONANZA BEECH MODEL V35 BONANZA BEECH MODEL V35A BONANZA BEECH MODEL V35B BONANZA MODIFIED IN ACCORDANCE WITH STC SA1035WE A. NORMAL: FUEL SYSTEM To start the engine: position throttle half open, turn auxiliary fuel pump switch to "High Boost". When the fuel flow reaches 8 gph, turn auxiliary fuel pump switch to "OFF". Reduce throttle to idle position. Engage starter, opening throttle approximately 3 to 4 turns. Hot engine starting: auxiliary fuel pump, momentarily to "High Boost" immediately before engaging starter; after engine starts turn auxiliary fuel pump switch to "Low Boost" as needed to purge vapor from system. Turn on "Low Boost" in climb above 8,000 feet altitude. NOTE: In hot weather "Low Boost" should be used as needed during hot engine starts. Use "Low Boost" as needed to purge vapor during ground operation, take-off and climb. CAUTION: Do not over-prime engine. In the event of flooding, place mixture in idle-cut-off and operate starter until excess fuel is removed, then repeat hot engine starting procedure. Auxiliary pump switch in "High Boost" position with engine driven pump operating may give over-rich mixture and as a result a slight or even a complete power loss may occur. When switching tanks, if fuel tank is allowed to run completely dry, it may be necessary to turn auxiliary pump to "Low Boost" position and place mixture control to full rich to aid in restart. Close throttle as necessary to prevent engine overspeed on restarting; turn pump to "OFF" position after engine restarts. OIL SYSTEM - CAUTION - When oil temperature is in the low operating range apply full throttle slowly to avoid engine overboost above 32.5 inches M.P. FAA APPROVED: 12-02-65 REVISED: 05-11-66 REVISED: 12-29-66 REVISED: 10-25-67 REVISED: 11-18-69 REVISED: 11-09-71 REVISED: OCT 17 1995 Page 3 of 8 GARRETT AVIATION SERVICES FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT ΤΟ BEECH MODEL S35 BONANZA BEECH MODEL V35 BONANZA BEECH MODEL V35A BONANZA BEECH MODEL V35B BONANZA MODIFIED IN ACCORDANCE WITH STC SA1035WE MIXTURE CONTROL: Full rich for all powers above (75%). Seventy-five percent or below, lean to fuel flow gauge for power selected. COWL FLAP: Rear cowl flaps to be open for take off and climb, closed for cruise. Front cowl flaps to be used as necessary to control engine temperatures, with rear cowl flaps open. B. EMERGENCY: WARNING If a turbocharger failure is the result of a loose, disconnected and/or burned through exhaust, then a serious fire hazard exists. If a failure in the exhaust system is suspected in flight, shut the engine down and LAND AS SOON AS POSSIBLE. If a suspected exhaust system failure occurs before takeoff, DO NOT FLY THE AIRCRAFT. If a suspected Lubrication for the turbocharger and turbocharger control is supplied by the aircraft engine lubrication system. Failure of the turbocharger and/or turbocharger control lubrication system could cause loss of aircraft engine oil supply. turbocharger or turbo-charger control lubrication system failure occurs, LAND AS SOON AS POSSIBLE. If a suspected turbocharger or turbocharger control lubrication system failure occurs before takeoff, DO NOT FLY THE AIRCRAFT. NOTE: A turbocharger malfunction at altitude above 10,000 ft. could result in an overly rich mixture which could cause a partial power loss and rough running engine and/or a complete loss of engine power. - or COMPLETE LOSS OF ENGINE POWER If a suspected turbocharger turbocharger waste gate control system failure results in a complete loss of engine power, the following procedure is recommended: FAA APPROVED: REVISED: 12-02-65 10-25-67 REVISED: REVISED: 11-18-69 OCT 17 1995 Page 4 of 8 Mixture Throttle. GARRETT AVIATION SERVICES FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT TO BEECH MODEL S35 BONANZA BEECH MODEL V35 BONANZA BEECH MODEL V35A BONANZA BEECH MODEL V35B BONANZA MODIFIED IN ACCORDANCE WITH STC SA1035WE Propeller. Mixture. Continue flight. IDLE CUTOFF CRUISE ....... FULL FORWARD ADVANCE slowly until engine re-starts LAND AS SOON AS POSSIBLE PARTIAL LOSS OF ENGINE POWER - If the turbocharger waste control fails in the OPEN position, a partial loss of engine power may result (ENGINE REVERTS TO NORMALLY ASPIRATED OPERATION). The following procedure is recommended if a suspected turbocharger/wastegate control failure results in a partial loss of engine power: Throttle. Mixture. Propeller. Continue flight. ENGINE POWER OVERBOOST - AS REQUIRED AS REQUIRED AS REQUIRED LAND AS SOON AS POSSIBLE If the turbocharger wastegate control fails in the CLOSED position, an engine power overboost condition may be experienced. The following procedure is recommended for an overboost condition: Throttle... REDUCE as necessary to keep manifold pressure within limits. NOTE: Expect manifold pressure response to throttle movements sensitive. to be OCT 17 1995 FAA APPROVED: Page 5 of 8 GARRETT AVIATION SERVICES FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT ΤΟ BEECH MODEL S35 BONANZA BEECH MODEL V35 BONANZA BEECH MODEL V35A BONANZA BEECH MODEL V35B BONANZA MODIFIED IN ACCORDANCE WITH STC SA1035WE Propeller. Mixture. Continue flight. AS REQUIRED AS REQUIRED LAND AS SOON AS POSSIBLE FUEL SYSTEM - Turn auxiliary fuel pump to "Low Boost" or as needed in case of loss of fuel pressure. "high Boost" EMERGENCY DESCENT - Idle power, gear down 165 IAS. FAA APPROVED: REVISED: 12-02-65 OCT 17 1995 Rocco Lippis FOR: Charles R. Hawks, Chief Aircraft Engineering Division WE100 Western Region Federal Aviation Agency Page 6 of 8 GARRETT AVIATION SERVICES FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT ΤΟ BEECH MODEL S35 BONANZA BEECH MODEL V35 BONANZA BEECH MODEL V35A BONANZA BEECH MODEL V35B BONANZA MODIFIED IN ACCORDANCE WITH STC SA1035WE LOG OF REVISIONS PAGE NUMBER FAA APPROVAL DATE OF REVISION DESCRIPTION Page 1 Rocco Lippis March 01, 1966 Revised Para A Engine Limits Page 2 Page 1 Rocco Lippis May 11, 1966 Page 2 Page 3 Revised Para D Airspeed Limits Revised I Limitations Revised Para D Airspeed Limits Revised Para E Placards Revised II Procedures Page 1 Rocco Lippis December 29, 1966 Revised I Page 2 Limitations Para A Removed Manifold Pressure Limitations Para B Added Propeller All Pages Rocco Lippis October 25, 1967 Added Model V35A FAA APPROVED DATE: 12-02-65 REVISED: OCT 17 1995 Page 7 of 8