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STARTER CONTROL VALVE OPEN light on.
If light remains on or comes on after start, secure engine by pulling emergency shutdown handle.
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FUS DUCT HOT light on.
I. On ground, secure ground air-conditioning and all engine and APU bleed air, and return to the line.
II. In flight, close all engine bleed and fuselage shutoff valves.
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START VALVE light on.
Check overhead panel for individual engine start control valve open light.
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NTS INOPR. Light on.
Continue holding out on feather button. (FE)
Emergency Shutdown Handle – Pull. (FE)
Feather Button – Push. (FE)
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Crew Responsibility for Fire of Unknown Origin
Alert crew, activate the fire bill – Alerted. (CP, TC)
Cabin Exhaust Fan – OFF. (FE)
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Pressurization Loss
1) Don smoke masks
2) Alert crew
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Rapid Decompression
1. Pressurization ground check switch - TEST. (FE)
2. Ground air-conditioning switch - ON. (FE)
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Emergency Depressurization
- AUX Vent - OPEN (FE)
- OUTFLOW Valve - OPEN (FE)
- EDCs - DUMP (FE)
- AUX Vent - Close at 1" differential (FE)
- Without electrical power available:
- Free-Fall Chute - OPEN (FE)
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Emergency Descent Procedure
1) Autopilot – Disengaged. (P)
2) Power Levers – FLIGHT IDLE. (P)
3) Landing Gear Lever – As required. (CP)
4) Airspeed – As required. (P)
5) Pressurization – As required. (FE)
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Ditching Procedures
1) Alert crew time to impact – Alerted. (CP)
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Brake Fire
1) Request ground firefighting equipment. (CP)
2) Stop the aircraft. (P)
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Engine Fire on the Ground
1) Emergency Shutdown Handle – PULL. (FE)
2) HRD – Discharged. (P, FE)
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Emergency Shutdown Procedure
1) Emergency shutdown handle (on pilot command) – Pull. (FE)
2) HRD (fire only) – Discharged. (P, FE)
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Shifting to Boost Off
1) Disconnect the Autopilot
2) Attempt to obtain a safe altitude
3) Set Condition V
4) Trim tab setting – Check for normal position
If abnormal force is still present:
5) Booster shift handle – Pull
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Propeller Malfunctions
I. If rpm at or above 115 percent – Reduce airspeed (150 KIAS minimum) and perform Operation with a Pitchlocked Propeller procedure in paragraph 15.12.2. (P, FE)
II. If rpm below 115 percent – Smoothly advance power lever(s) toward cruise conditions and increase TAS, noting engine indications (normal rated power if range is a factor). (P, FE)
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Propeller Fails to Feather
1) Feather Button – In.
2) PCO – Press.
3) Alternate Bus (propellers 1 and 4) – Select.
4) PROP FEATHER circuit breakers – Check in.
5) Airspeed – Decrease toward 150 KIAS.
If feather button light remains on:
6) PROP FEATHER CONT circuit breaker – Pull.
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Flight with Cracked Windshield
1) Turn off heat of affected panels.
2) Helmets on, visors down. (P, CP, FE)
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Loss of all Airspeed Indication
1) Check pitot heat – ON. (FE)
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Windshear Escape Procedure
1) Max Power – Set. (P, FE)
2) Pitch Attitude – 10° up. (P)
3) Landing gear – UP. (P, CP)
4) FLAPS– Do not change until out of windshear. (P)
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Split-Flap
1) If uncontrollable, reset the flap handle to the previous position.
2) If controllable, land with the flap handle in the selected position.
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Stall (Not memory item)
- Simultaneously:
- 1) Disconnect autopilot
- Smoothly add symmetric power
- Relax back pressure on the yoke (16 units AOA or less)
- 2) Use rudder and aileron to leve the wings and center the ball
- 3) Gently recover pitch attitude as airspeed builds
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Out of Controlled Flight, Spiral and Spin Recovery
- 1) Power Levers - FLIGHT IDLE (P)
- 2) Flight Controls - Neutralize (P)
- 3) Airspeed, AOA, turn needle - Check (P)
- If in a spin:
- 4) Rudder - Full opposite turn needle (P)
- 5) Controls - Neutralize (P)
- 6) Unusual attitude - Recover (P)
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