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CV-2B Pilot's Takeoff List

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Marco Schanzenbach
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46 views50 pages

CV-2B Pilot's Takeoff List

Uploaded by

Marco Schanzenbach
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© © All Rights Reserved
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Beene Rae E CV.2B PILOT’S CHECKLIST July 1964 PREFLIGHT INSPECTION (DAY AND NIGHT) COCKPIT CHECK - BEFORE START NORMAL START AND TAXIING ENGINE RUNUP TAKEOFF, IN FLIGHT, LANDING, AND... [ ENGINE SHUTDOWN AND SECURING AIRCRAFT EMERGENCY - ENGINE FAILURE AND AIRSTART EMERGENCY - PROPELLER FAILURE ———_ MERGER BBS 2 LIC LeeaeM ae ; = EMERGENCY - FIRE - FUEL FORCED LANDING - DITCHING - BAILOUT ENGINE HANDLING CHART SS Se 8 Be BB — PILOT'S COMPARTMENT 1. DA Form 2408 - Check. a. Status today. b. Servicing. c. Weight and balance forms, if applicable. Battery master switch - OFF. Ignition switches - OFF. Flap selector - Full down. Crew oxygen masks - Check condition (3) (60- 3762 through 62-4171). Hydraulic hand pump handle - Stowed. Oxygen supply valve - As desired (62-4172 and subsequent). 8. Hydraulic panel, check - a. Hand pump selector - Normal system. b. Emergency landing gear down, selector - OFF. c. Nosewheel down selector - OFF. d. Brake accumulator charging selector - OFF. 9. Portable oxygen unit - Check. 10. Portable fire extinguisher - Check (1). PREFLIGHT INSPECTION (DAY AND NIGHT) . OP wD => BEEBE — = = 6. Empennage - a. Vertical stabilizer, rudder, and trim tab - Condition, tab locks removed. b. Horizontal stabilizer, fairings, elevators, trim tabs - Condition, tab locks removed. c. Taillight - Condition. 7. Cargo door - Condition; ramp extensions - Stowed and secured. 8. Cargo and passengers - Secure. 9. Passenger briefing. NIGHT OPERATIONS Prior to the preflight inspection, preceding a night flight, the following will be accomplished: 1. Upon entering the flight compartment - Flight compartment dome light - ON, red or white as desired. 2. Battery master switch - Battery master. 3. Check lights for proper operation as follows: ae b. Panel lights' rheostats (4) - Check full range; leave as desired. Anticollision lights (2) - Check ON, return to: OFF, Warning light switch (1) - Check dim posi- tion, leave as desired. Wing and taillights (3) - Leave ON. Standby compass lights - Check emergency, return to normal. (1) Magnetic compass. (2) Airspeed indicator. (3) Altimeter. (4) Turn/bank indicator. Wing inspection lights (2) - Check ON, return. to OFT. Formation lights - Check bright and dim position, return to OFF. Landing lights (2) - Check ON, return to OFF. Taxi light (1) - Check ON, leave as desired. Utility lights (4) - Check operation, leave as desired. BEBen2 BB = = k. Emergency hydraulic selector panel lights (2) - Check for illumination when panel door is raised 1. Cabin dome lights (7) - Check operation, leave as desired m. Emergency exit lights (5) - Check operation, return to OFF, n. Rear entrance lights (1) - Check operation, leave as desired. 0. Cargo loading light (1) - Check operation, leave as desired. CAUTION: When cargo loading light is in stowed position, insure that the light beam is directed away from the cabin roof. Battery master switch - OFF or as desired for preflight inspection. CAUTION: If battery master switch remains at battery master posi- tion during preflight inspection, use extreme caution while in vicinity of propellers. COCKPIT CHECK BEFORE STARTING ENGINES 1. Pilot and copilot seats - Adjust. . Rudder pedals - Adjust. 3. Safety belts and shoulder harness - Fasten and adjust. 4. Parking brake - ON. 5. Cockpit air control selector handles - As desired. 6. Nosewheel steering switch - ON. 7. Oil dilution switches - OFF. 8. Accessories compartment vent door's switch - As desired (60-3762 and subsequent). 9. Hot fuel prime switch - OFF (60-3762 and subsequent). 10. Feather dilution switch - OFF (61-2595 and subsequent). ll. Battery master switch - OFF. 12. Windshield wiper switch - OFF. 13. Windshield heat switch - OFF. 14. Instrument light rheostats - OFF (4). 15. Anticollision light switch - OFF. 16. Warning lights intensity switch - Bright. COCKPIT CHECK - BEFORE START NORMAL START AND TAXIING __ENGINE RUNUP TAKEOFF, IN FLIGHT, LANDING, AND... ENGINE SHUTDOWN AND SECURING AIRCRAFT _ EMERGENCY - ENGINE FAILURE AND AIRSTART | 17. Wing and taillights' switch - OFF. 18. Standby/compass light switch - NORM. 19. Wing inspection light switch - OFF. 20. Formation lights switch - OFF (63-9718 and subsequent). 21. All radio switches - OFF. 22. Pilot's flight instruments - Check, set altimeter. 23. Gyro compass switch - Slave. 24. Pilot's oxygen regulator supply switch - OFF (62-4172 and subsequent). 25. Fuel booster pump switches - OFF. 26. Fuel tank selector switch - Normal. 27. Troop-jump and pendulum release switches - OFF. 28. Engine instruments - Check. 29. Electrical power panel - a. D.C, generator switches - ON and guarded (2). b. Inverter switch - OFF. 30. Deicing panel - a. Pitot heater switch - OFF. b. Propeller anti-icing switch - OFF. c. Wing-and-tail mode switch - OFF. BEEREEReBEREB A | SE, 32. 33's 34. 35., 36. Ste 38. 39. 40. Copilot's oxygen regulator supply switch - OFF (62-4172 and subsequent). Copilot's flight instruments - Check, set altimeter. Thrust indicator free-stream pressure selector - Normal. Feather dilution switch - OFF (60-3762 through 61-2594). ; Autofeathering switch - OFF. Clocks - Check and set (2). Emergency panel - a. Cockpit and cabin heater fire extinguisher switches - Down and guarded (2). b, Fuel and oil emergency shutoff switches - Down and guarded (4). c. Fire-pull T-bar handles -In andhorizontal (2). Wheel brakes emergency lever - Forward and secured. Standby compass - Check. Overhead console - a. Carb air induction switches - Ram. b. Carb hot-air levers - Cold. c. Flap selector lever - Up. d. Ignition switches - OFF. Taxi and landing light switches - OFF. Mixture control levers - Idle cutoff. Propeller levers - Maximum increase. Gust lock handle - Locked. Throttles - Closed. Landing gear selector - Down. Sor Bt rho BEFORE STARTING Landing gear ground safety locks - Verify removed (3). Pitot head covers - Verify removed (6). Wheel chocks - As desired. Fireguard - Posted. Propellers - Clear, Battery master switch - Battery master. D.C. warning and indicating lights - Check ON (13). Hydraulic low pressure (2). Landing gear down (3). Fuel low pressure (2). Oil low pressure (2). Generator failure (2). Main inverter failure (1). 26 VAC failure light (1). Tanne gear warning horn test switch - Test - Check for illumination of gear selector lever light. Throttles - Open to gust lock. mo poop ga NORMAL START AND TAXIING ENGINE RUNUP TAKEOFF, IN FLIGHT, LANDING, AND... ENGINE SHUTDOWN AND SECURING AIRCRAFT _ EMERGENCY - ENGINE FAILURE AND AIRSTART | EMERGENCY - PROPELLER FAILURE P&CP 10. If external power is to be used - Battery master switch - OFF. Generator switches - OFF. External power - Connected. Inverter switch - STBY, check standby light illuminates - OFF. Check failure light illuminates and standby light goes out - Switch to MAIN - Check standby and failure light go out - Leave switch at main. P STARTING THE ENGINES 1. Start left engine as follows: Note. If external power is used, start right | engine first and disconnect external power before starting left engine. Pr a. Left fuel booster pump switch - Normal. CP b. Inverter switch to MAIN - Note fuel and manifold pressures' register. Return to OFF (with external power; merely note pressures), BEEBE AH if c. Starter switch - L. Turn prop through 15 blades on initial start any day (6 blades on later starts) to check for hydraulic lock. Do not operate starter for more than 30 seconds, allow 1 minute for cooling. cP d. Left ignition switch - Both (at re- quired blade count). P e. Vibrator switch - L. J f. Primer switch - L, as required. P Starter and vibrator switches - Release as engine starts. a= h. Throttle - Adjust for 800 rpm. CE i. Mixture control lever - Auto-lean, when engine running smoothly on prime. P j- Primer switch - Release when rpm starts to drop. CP 2. Inverter switch - Main. P. 3. Oil pressure - 30 psi minimum. CAUTION: No oil pressure - shut engine d at once. P 4, Left fuel booster pump switch - OFF. P 5. Repeat starting procedure for right engine (if external power was used - disconnect, turn battery master switch ON, generator switches ON). » 6. Engine ground operation - Warm up at 1200 rpm until oil temperature reaches 40°C. (For operation in ex- treme temperatures, refer to opera- tor's manual. ) BEFORE TAXIING CP l. FM switch - ON. 2 2. A.C. and D.C, check - (29 items). Low oil level (2) Windshield heat (2). Troop-jump lights (6). Fuel low level (2). Fuel quantity indicating system (2). Marker beacon (1). Autofeather (1). Prop reverse (2). Cockpit heater fire (1). Prop oil (1). oe bo hoe ao op k. Engine fire detection system (4). 1. Prop oil (1). m. Cabin heater fire (1). n. Doors unlocked (1). o. Ramp door 15°-position (1). p. Alarm bell - Check operation. cP 3. Communications equipment and naviga- tional radios - ON as desired. a. Radar inverter - ON. b. Radar function switch - STBY. P&CP 4. Flight and engine instruments - Check all indications, verify altimeter setting on call-up to tower. iP 5. Hydraulic system pressure - 3000 psi approximately. PB 6. Brake system pressure - 3000 psi approximately. cc 7, Wheel chocks - Removed and secured. cc 8. Cargo and passenger doors - Closed. cc 9. Secured for taxi - Reported by crew chief. P I g brake - Release P 2. Throttles - Adjust as necessary. P 3. Wheel brakes - Check operation. P&CP 4. Flight instruments - Check during turns. P 5. Head into wind, nosewheel centered before stopping. P 6. Parking brake - ON. BREere-PfEt7 BRE EEEEA — GF. cP cP ENGINE RUNUP 1. Verify area in rear is clear for runup. . Mixture control levers - Auto-rich. 3. Throttles - Set at 1200 rpm, adjust friction levers. a. Wing flaps - Check full range; re- turn to full up. Ignition switches - Check ground out. Mixture control - Check, adjust friction levers. Fuel crossfeed - Check. Voltammeters - (1) Voltage readings - 28V 4 0.5V. (2) Ammeter readings coincide within 10%. (3) Left generator switch - OFF. Note left ammeter drops to zero and right ammeter shows increased reading. Check that automatic change-over to standby inverter occurs and that the standby light illuminates. Left generator switch - ON. ENGINE RUNUP TAKEOFF, IN FLIGHT, LANDING, AND... ENGINE SHUTDOWN AND SECURING AIRCRAFT _ EMERGENCY - ENGINE FAILURE AND AIRSTART _ EMERGENCY - PROPELLER FAILURE GP cP P&CP hi. (4) Repeat (3) for right generator. Pitot heat - Check. Wing-and-tail deicing pumps - (1) Mode switch - MAN. (2) Deicing pressure 14-16 psi, suction 4-6" Hg. (3) Check operation - As desired. (4) Mode switch - OFF. Heater intake anti-icing switches - Check. Temperature check - (1) Oil temperature 40°C minimum. (2) Cylinder, head temperature 120°C minimum. Gust lock handle - Unlocked. Throttles - Set at 1900 rpm - ae b. Props - Minimum decrease; rpm drops to 1300. Check 3 times on initial runup for conventional sys- tem. For reverse prop system, check | time. Adjust friction. Carburetor heat - Check. Throttles - 2200 rpm - a. Manifold pressure - approximately field barometric pressure. SS ee cP ane & Sh A Thrust indicators - Check for similar readings. Ignition system - Check magnetos, one atatime. Drop not over 100 rpm max (40 rpm differential). Throttles closed - Check - a. bs oy d Idling - 550 + 25 rpm. Generator warning lights illuminated. Standby inverter light illuminated. Reverse prop system - (1) Carb air induction switches - Filter: (2) Throttles - Reverse idle. Check feather buttons and re- verse prop indicators illumi- nate. (Move throttles to rear to insure freedom of movement. (3) Throttles - Normal idle. (4) Carb air induction switches - As desired. Propeller autofeathering system - Check: Note. If autofeather system inoperative, perform manual check at 1900 rpm. a. Throttles - Set at 1200 rpm, Pp b. Autofeathering switch - ON, check indicator light illuminates. c. Throttle - P (1) Open right throttle until left feathering button pulls in. (Thrust pressure differential of 45 +2 1/2% should be indicated, )} P (2) Return to 1200 rpm. cP (3) Simultaneously pull out the button to arrest feathering cycle after 200 rpm drop. P d. Autofeathering switch - OFF - then ON. e. Repeat procedure for right system. P 9. Autofeathering switch - OFF. P 10. Gust lock handle - Locked. cP 11. Mixture control levers - Auto-lean if delay is anticipated prior to completion of takeoff check. , i i on Pn BEEBEBEEEE |= — TAKEOFF CHECK Pp 1. Trim - Check (3) - a. Elevator - Takeoff range. b. Rudder - Neutral. c. Aileron - Check operation - Set to neutral. CP 2. Carb air induction switches - As desired. CP. 3. Carburetor heat - Cold. CP 4. Wing flaps - As desired. cP 5. Mixture control levers - Auto-rich. CP 6. Propeller - Maximum increase. ie 7. Autofeathering switch - ON. P 8. Fuel booster pumps - Normal. - 9. Fuel tank selector - Normal. P 10, Windshield heat - Normal. Pp 11. Hydraulic pressure indicator - 3000 psi. Cr 12. Anticollision light - ON. P&CP 13. Engine instruments - Check - a. All warning lights out. b. Fuel quantity. P&CP 14. Flight instruments - Check to include flap position indicator. P 15. Stall warning system - Check. P&CP 16. Windows - Secured or as desired. TAKEOFF, IN FLIGHT, LANDING, AND... | ENGINE SHUTDOWN AND SECURING AIRCRAFT J EMERGENCY - ENGINE FAILURE AND AIRSTART EMERGENCY - PROPELLER FAILURE oe MERGENCY - HYDRAULIC SYSTEM P&CP 17. Emergency overhead escape hatch - Recheck locked. P 18, Parking brakes - Release. Ee 19. Taxi onto runway. LINEUP CHECK P 1. Line up with takeoff runway and unlock gust lock handle. P 2. Check flight controls. P&CP 3. Shoulder safety harness inertia reel - Locked. AFTER TAKEOFF P&CP 1. Gear and flaps - Up. P&CP 2. Climb power - As required. P&CP 3. Shoulder safety harness inertia reel - As desired. Pp 4, Autofeathering switch - OFF after re- ducing to desired climb power. GP 5. Radar function switch - As desired. NORMAL CRUISE : 1. Level off - obtain cruise airspeed. P&CP 2. Normal cruise power - Check cruise chart. 2 3. Fuel booster pumps - OFF if below 10, 000 feet. cP 4, Mixture control levers - Auto-lean if cylinder head temp below 232°C. CP 5. Carburetor heat - As required. GP 6. Fasten seat belt and no smoking sign switches - As desired. BEFORE LANDING 13) 1. Throttles - Reduce power as necessary. GP 2. No smoking and fasten seat belt sign switches - ON. CP 3. Carb air induction switches - As desired. Carburetor heat - As desired. Mixture control levers - Auto-rich. Fuel booster pumps - Normal. Fuel tank selector - Normal. Hydraulic pressures - 3000 psi (2). Nosewheel steering switch - ON. Radar function switch - STBY. Landing gear selector - Down - IAS 120 knots or below. Landing gear down check - a. Visually check each main gear down. P&CP b, Check indicator lights (3). cP Lao] UW add dd Q Om ty NS Fovengae P&CP c. Check hydraulic pressure. P&CP d. Check indicator light out in selector handle. cc e. Gear down and locked report from crew chief. CP 13, Flaps - As desired - IAS 105 knots or below. 14, Final approach check - GP a. Propeller selector levers - Full increase on final. P&CP b. Recheck gear indicator lights ON (3). P&CP c. Recheck hydraulic pressures. cP 15. Landing lights - As desired. P 16. Accessories compartment vent doors - As desired. P&CP 17. Shoulder safety harness inertia reel - Locked, AFTER LANDING PB 1, Gust lock handle - Locked before turn- ing off runway. cP 2. Taxi light and landing lights - As required. GP 3. Carb air induction switches - As desired. cP 4. Flap selector lever - Up. Sseoaooe- se; cP CP cP GP ESE = Mixture control lever - Auto-lean. Fuel booster pump switches - OFF. Windshield heat switch - OFF. Anticollision light switch - OFF. Deicing switches - OFF. Radio switches - OFF or as desired. Taxi to parking area. Nosewheel - Centered before stopping aircraft. Parking brake - ON. BEB EBEEB EE — ENGINE SHUTDOWN P 1. Throttles - Set at 1200 rpm. P 2. Cylinder head temperature - Allow engine to cool below 200°C. cP 3. Ignition switches - Ground-out check. cP 4, Radio switches - OFF. cP 5. Inverter switch - OFF. cP 6. Fasten seat belt and no smoking sign switches - OFF. cP 7. FM power switch - OFF. cP 8. Mixture control levers ~- Idle cutoff. ce 9. Ignition switches - OFF when props stop turning. = 10. Fuel tank selector switch - OFF. P 1l. Battery master switch - OFF. SECURING AIRCRAFT cc 1, Landing gear - Chocked and tied down as required. cc 2. Parking brake - As desired. cc 3, All switches - OFF. cc 4, Landing gear safety lock pins - Installed. cc 5. Pitot head covers - Installed. cc 6. Doors and hatches - Closed. P&CC 7. DA Form 2408 - Complete. ENGINE SHUTDOWN AND SECURING AIRCRAFT | EMERGENCY - ENGINE FAILURE AND AIRSTART | EMERGENCY - PROPELLER FAILURE 2LRICA ULIC SYSTEM EMERGENCY - FIRE - FUEL FORCED LANDING - DITCHING - BAILOT LN HAN ENGINE FAILURE ABOVE TAKEOFF SPEED (BASIC SINGLE-ENGINE PROCEDURE) 1. Maintain aircraft control. Determine which engine is out. Note, Ifit becomes necessary to shut down an engine while in flight, due to an engine malfunction, the following procedure should be preceded by selecting the mixture control lever of the mal- functioning engine to the idle cutoff position. 3. Malfunctioning engine (low-thrust indication) - Feather propeller, 4. Operative engine - METO power (minimum) - a. Mixture control lever - Auto-rich. b. Propeller - 2550 rpm. c. Throttle - 42.5" Hg at sea level. - d. Fuel booster pump - Normal. 5. Landing gear and flaps - Up. 6. Inoperative engine - Shut down - a. Throttle - Closed. b. Propeller lever - Full decrease. c. Mixture control lever - Idle cutoff. 7. Clean-up - As desired. a. Fuel emergency shutoff switch - UP. (If engine fire, oil emergency shutoff switch UP also. ) b. Fuel booster pump switch - OFF. c. Ignition switch - OFF. EMERGENCY - ENGINE FAILURE AND AIRSTART | EMERGENCY - PROPELLER FAILURE a RICA Generator switch - OFF. Fuel tank selector switch - As required. Secondary bus reset switch - Up, if required. Nonessential electrical bus services - OFF. Operative engine power - Adjust as required. Po hoa ENGINE FAILURE DURING TAKEOFF ROLL Close throttles and apply brakes. ENGINE FAILURE AFTER TAKEOFF 1. Adjust power and maintain aircraft control. 2. Land if runway length permits or if safe single- engine speed is not obtainable. 3. If runway length does not permit safe landing and safe single-engine speed is obtained - a. Continue flight and perform basic single- engine procedure. b. Initiate climb when safe single-engine speed is attained. ENGINE FAILURE DURING FLIGHT Time and altitude permitting, check the engine systems to ascertain the cause of the failure and determine whether or not normal operation can be restored. If not, accomplish the basic single- engine procedure. BEBERESBE A= ENGINE RESTART IN FLIGHT Airspeed - 130 knots IAS maximum. Throttle - Closed. Propeller control lever - Full decrease. Mixture control lever - Idle cutoff. Ignition switch - Both. Fuel emergency shutoff switch - Down, Fuel booster pump switch - Normal. Autofeathering switch - OFF. Propeller feathering button - Depress for con- ventional system; pull for reverse system. (Release before 800 rpm.) 10. Mixture control lever - Auto-rich. 1l. Throttle - Advance slightly. 12. Temperatures - Check. 13. Propeller control lever - Required rpm. 14. Throttle - Advance to required manifold pressure. 15. Trim - Reset. 16. Fuel booster pump switch - OFF. 17. Generator switch - ON. 18. Secondary bus reset switch - Down. SOON DAR WN SINGLE-ENGINE APPROACH 1. Accomplish basic single-engine procedure as required. 2. Use normal traffic pattern. Landing gear - Extend when desired. Flaps - Use a maximum of 15° until landing assured. *Airspeed - 75 knots (A), 85 knots (B) on final. Turns - Avoid steep turns in pattern. *Speeds appropriate to 26,000# (A), speeds appropriate to 28,500# (B). SINGLE-ENGINE GO-AROUND Throttle - Takeoff power. Landing gear and wing flaps - Up. Rudder trim - Reset. Attitude - Maintain level flight. Airspeed - Commence climb at 75 knots IAS (A) or 85 knots IAS (B). Increase to 95 knots in both cases. Engine power - METO setting after safe climb has been established. 2. Sr BEBEHEs # PROPELLER FAILURE (OVERSPEEDING) Throttles - Retard - Reduce. speed. Propeller control lever (defective propeller) - Exercise pitch control. Propeller feathering button - Depress. PROPELLER RUNAWAY (REFUSES TO FEATHER) NOW Reset feather circuit breaker. Ignition switch - OFF. Fuel emergency shutoff switch - Up. Passengers - Evacuate from propeller plane of rotation. Airspeed - Just above safe single-engine speed. Reattempt feathering. If feathering attempt unsuccessful - Land as soon as practicable. Note. Prop oil low-level light illuminates - moni- tor engine tachometer. If rpm fluctuates more than 200 rpm, shut engine down and feather propeller. EMERGENCY - PROPELLER FAILURE Ads SYSTEM ss MERGEN a HYDRAULIC SYSTEM EMERGENCY - FIRE - FUEL _ FORCED LANDING - DITCHING - BAILOUT ae ENGINE HANDLING CHART ONE-GENERATOR FAILURE Generator switch - Check on. Generator field relay circuit breaker - Reset - One reset only should be made. 3. Generator switch - Reset. If warning light does not go out, proceed as follows: 4, Generator switch - OFF. 5. Switch off all unnecessary services. 6. Secondary bus reset switch - As desired. Ne Note. The secondary bus is automatically de- energized when one generator fails. Action (6) is carried out only if certain services from the sec- ondary bus are necessary for the flight. These services are windshield heat controls and inverters, main inverter, rear utility receptacles, windshield wipers, wing and tail deicing, pitot heat, cabin and cockpit heating, aileron trim control and indicator, and main inverter relay. 7. Ammeter - Check for overload. Do not allow ammeter loading for operating generator to exceed 300 amps. TWO-GENERATOR FAILURE 1. Generator switches - Check on. 2. Generator field relay circuit breaker - Reset - Only one reset should be made. EMERGENCY - ELEC EMERGENCY - HYDRAULIC SYSTEM EMERGENCY - FIRE - FUEL FORCED LANDING - DITCHING - BAILOUT _ ENGINE HANDLING CHART 3. Generator switches - Reset. If warning lights do not go out, proceed as follows: 4. Emergency bus switch - Emergency. 5. Battery master switch - OFF. Note. Emergency bus is now energized from the battery. CAUTION: With the emergency bus in operation and battery master switch off, propeller feathering pumps and fuel booster pumps are inoperative. 6. Switch off any unnecessary services to conserve the battery. AMMETER FAILURE If the ammeter for either generator registers zero but other electrical indications are normal, check for a faulty ammeter gage as follows: 1. Generator switch for appropriate generator - OFF. z. Ammeter - Check for increased reading on ammeter for other generator. 3. Generator switch - Reselect ON if reading in- creases. An increased reading will indicate that both generators are operating and that the fault is in the ammeter circuit. MAIN INVERTER FAILURE Inverter circuit breakers - Reset. D.C, power circuit breakers - Reset. Inverter switch - Select OFF then return to main. If standby light remains out - Leave switch at main. If standby light comes on - Select switch to STBY. STANDBY INVERTER FAILURE Inverter circuit breakers - Reset. D.C. power circuit breakers - Reset. Inverter switch - Select OFF then main. If the A.C. failure light comes ON - Select inverter switch OFF, 26 VOLT A.C, TRANSFORMER FAILURE If the 26 VAC warning light comes on while either inverter is operating properly, select the instru- ment transformer switch from main to standby. LANDING GEAR EMERGENCY LOWERING Note. If loss of engine driven hydraulic pump pres- sures have resulted - (1) Check circuit breakers and hydraulic system's reservoir; (2) if a leak in the system is discovered, the hydraulic pressure shutoff valve must be selected to OFF. 1. Nose gear - a. Landing gear selector - Down. b. Hand pump operation - (1) Hand pump selector - Emergency system. (2) Emergency landing gear down, selector handle - ON. (3) Nosewheel down hand pump selector - ON. (4) Hand pump - Operate until nose gear locked down. c. Emergency air bottle - (1) Emergency landing gear down selector handle - ON. (2) Nosewheel emergency down (air) selec- tor - Pull and hold out until green nose- wheel down light comes on. 2. Main gear - a. Landing gear selector lever - Recheck down. b. Emergency landing gear down selector handle - ON. c. Main gear emergency extension handle - Pull. EMERGENCY - HYDRAULIC SYSTEM EMERGENCY - FIRE - FUEL FORCED LANDING - DITCHING - BAILOUT _ ENGINE HANDLING CHART WING FLAPS EMERGENCY OPERATION (Use only in event of loss of both engine-driven hydraulic pumps. ) 1. Flap selector lever - As required. 2. Hand pump selector - Normal system. 3. Hand pump - Operate as required. WHEEL BRAKES EMERGENCY OPERATION 1. Hand pump selector - Normal system. (Emer- gency system in event of system fluid leak.) ’ 2. Brake accumulator hand pump charging selector - ON. Hand pump - Operate as required. Use brakes sparingly. Wheel brakes emergency lever - Pull if extra braking required. Ook Ww NOSEWHEEL STEERING Will be ineffective without system pressure. In this event the nosewheel steering switch must be selected to OFF. ENGINE FIRE .E (GROUND) If fire develops during starting, discontinue prim- ing, but keep engine cranking until it starts or until fire recedes. If the engine is already running when fire develops, open throttle and attempt to blow it out. If the ground crew signal to shut down the en- gine, immediately execute the following: Mixture control lever - Idle cutoff. Fuel and oil emergency shutoff switches - Up. Fuel booster pump switch - OFF. Ground crew - Fight fire. Fire-pull T-bar - Pull. Ignition switch - OFF. Generator switch - OFF. Battery master switch - OFF. Abandon aircraft. OMAIRKHPWNHE ENGINE FIRE (FLIGHT) Mixture control lever - Idle cutoff. Fuel and oil shutoff switch - Up. Propeller feathering button - Depress. Fuel booster pump switch - OFF. Zones 2 and 3 fire, continue as follows: Fire-pull T-bar - Pull. Second shot - If required. Complete engine shutdown procedure. RON NDU EMERGENCY - FIRE - FUEL FORCED LANDING - DITCHING - BAILOU! NG CH COMBUSTION HEATER FIRE FLIGHT COMPARTMENT HEATER Heater master switch - OFF. Flight compartment air control handle - Pull to close. Flight compartment heater extinguisher switch - Up. CABIN HEATER. Heater master switch - OFF. Cabin air control handle - Pull to close. Cabin heater extinguisher switch - Up. FUEL SYSTEM EUEL PRESSURE DROP Engine operating normally - a. Make a visual check for the presence of streaming fuel vapor, signs of fire, or other evidence of a fuel leak. (1) Ifa leak is found, shut down the engine as soon as possible, (2) If a leak is not found, maintain a watch for fire and shut down the engine com- pletely before entering the traffic pattern. Engine stops operating - a. Throttle - Closed. b. Fuel system controls - Check. c. Fuel booster pump switch - High (only after visual inspection for fuel leak). If the condition persists - d. Fuel booster pump switch - OFF. e. Fuel selector switch - To feed both engines from other tank. f. Fuel booster pump switch for good tank - High while cross-selection is made. If the condition still persists - g- Shut down the engine. ; * FORCED LANDING - DITCHING - BAILOUT ENGINE HANDLING CHART BEEBEEBEEBEEE SE FORCED LANDING 1. Alarm bell - Six rings. . No smoking and fasten seat belt switch - ON. 3. Radio - TRANSMIT DISTRESS. IFF master control to EMERGENCY. 4, Heater master switches - OFF. 5. Nonessential electrical services - OFF. 6. Safety harness and inertia reel - Adjusted and locked. 7. Landing gear - Down. 8. Wing flaps - As desired. 9. Engine controls - As for normal landing. 10. Generator switches - OFF. ll. Emergency bus switch - Emergency. 12. Battery master switch - OFF (daytime only). If at night - electrical switching as follows: 13. Generator switches - OFF. 14. Emergency bus switch - Emergency. 15. Secondary bus switch - Reset. 16. Battery master switch - Battery master. 17. Just before touchdown - Battery master switch - OFF, DITCHING (To be accomplished as a last resort. ) Prepare aircraft as in forced landing, except as follows: 1. Landing gear - Up. 2. Flaps - 40° (all weights) on final approach. FORCED LANDING - DITCHING - BAILOU' BAILOUT 1. Radio - TRANSMIT DISTRESS. IFF master control to EMERGENCY. 2. Exits - Jettison cabin emergency door, right- hand passenger door. Open cargo doors. 3. Alarm bell - One long ring to execute bailout ouder’. 4, If time permits - Set trim, feather propeller, operate fuel and oil shutoff switches, ignition and electric - all OFF, battery master switch - OFF last. Penn ff > > *porayxD uo dw “ul 0s paacxe sou oq “OPHOYE [IN4- "Ld f ——*LVD PAS #2129 3,01 4209 40} GW “UY g*9 sODLIGNS “pPauew aySijy 385 “LVD PHS 240g" 3, OL 422 404 GW “UY! ¢°O PPY | “yea; 000’9] 24099 sbulyes soy 6-7 dua y Ity 9405 Pig 404 uaas6 asp Soinssasg PjoyiuDW "| ‘SNavw3aa o08L 0081 0081 (xOuddy) 008L SONVA “XVW 008L 0081 0061 H7E(00R O'€¢ | 0002 O'SE | Osec 006 GWi1D TVWYON Zy {OSC oozL | dOW Os j00z Osh | 440A NVL (SANIONA Z) anion anoy sed 41a Do SUNLVAAdWAL AVG GUVGNVILS a1 dHa (0001 X) SGNLILIV LV 'SSAad “NVW XYW CONS ZWZ-0002- ‘AVG “G1is) NOGAVD w-DHd YOd LUVHD ONITGNVH INION| Sa OU et ts oa FRRSBBRRANA TAKE-OFF DISTANCE TO CLEAR 50 FT LANDING DISTANCE TO CLEAR 50 FT ICAO Standard Atmosphere ICAO Standard Atmosphere Dry Air Zero Wind Clear 50 Fe -Feet 30-Knot Wind Clear 50 Ft “Feet Pressure Flaps | Altitude -Feet Pressure | Zero Wind | 30-Knot Wind Weight Flaps | Altitude Clear 50 Ft | Clear 50 Ft -Feet -Feet -Feet NORMAL TECHNIQUE NORMAL TECHNIQUE 28,500 7° | Sea Level 2000 1220 28,500 30° | Sea Level 1790 1000 5000 2650 1620 5000 2010 1160 26,000 15° | Sea Level 1490 790 26,000 40° | Sea Level 1540 830 5000 1675 910 5000 1750, 950 23,000 15° | Sea Level 1305 660 23,000 40° | Sea Level 1440 750 5000 1470 765 5000 1620 870 SHORT-FIELD TECHNIQUE SHORT-FIELD TECHNIQI | 28,500 | 25° | Sea Level 1205 640 28,500 | 40° | Sea Level 1245 660 5000 1605 880 5000 1420 780 | 26,000 | 30° | Sea Level 1110 430 26,000 | 40° | Sea Level 1030 470 5000 1500 630 5000 1160 570 23,000 30° | Sea Level 840 290 23,000 40° | Sea Level 950 5000 1110 430 5000 1060 TM 55-1510-206-10CL TAKE-OFF DATA CARD CONDITIONS Gross Weight LB Field Length FT OAT EC. Dew Point sf Specific Humidity LB/LB Pressure Altitude FT Headwind Component KTS (at 50 ft) TAKE-OFF Normal Short field Take-off Distance FT FT (to clear 50 ft) Take-off Ground Run Soe ee ee Speed at Take-off KIAS ______ KIAS Speed at 50 ft —____ KIAS KIAS LANDING IMMEDIATELY AFTER TAKE-OFF Normal Shortfield Approach Speed KIAS KIAS Landing Distance Pr FT (to clear 50 ft) Landing Ground Roll Fr Ee N-14 TM 55-1510-206-10CL LANDING DATA CARD CONDITIONS Gross Weight ee See Field Length NENT s er Fi OAT eS, Pressure Altitude Fr Headwind Component eh eG (at 50 fe) LANDING Normal Shortfield Approach Speed KIAS KIAS Landing Distance FT FT (to clear 50 fr) Landing Ground Roll FT FT Bee fF 2 SS =! aF-727 OXYGEN DURATION IN HOURS THREE CREW MEMBERS CYLINDER: CONSTANT FLOW 1-TYPE AN6025 AX646-18 SYSTEM GAGE GAGE PRESSURE - 7S! ALTITUDE (FEET) 20,000 25,000 2.6 30,000 2.2 1.2 CYLINDERS: DILUTER DEMAND 2-TYPE AN6025 AX386 SYSTEM ALTITUDE GAGE PRESSURE - PSI (FEET) 0.8 0.7 0.4 3.3 2.9 18 0.8 0.7 0.5 36 3.2 2.0 0.9 0.8 0.5 4.0 3.6 2.2 1 1.0 0.6 44 3.9 25 2 Wd 0.7 46 4d 2.5 15 1.3 0.8 AQ 3.8 24 2.0 1.8 Md 24 21 1.3 2.6 24 15 2.6 24 1.5 NOTE: UPPER FIGURES INDICATE DILUTER SWITCH AT “100% OXYGEN” LOWER FIGURES INDICATE DILUTER SWITCH AT “NORMAL OXYGEN” anaes

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