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28 Cards in this Set
- Front
- Back
- 3rd side (hint)
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ALT WARN
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Cabin altitude exceeds 12,500 ft.
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Non-Mem:
Don/deploy oxygen maks and/or descend to a lower alt. |
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AP DISC
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Autopilot has been disconnected by means other than depressing pilot AP/YD DISC switch.
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Non-Mem:
1. AP/YD Disc 2. Retrim A/C 3. Reengage AP (As required). |
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AP TRIM FAIL
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Trim will not run or running opposite direction from commanded.
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1. AP/YD DISC - Depress fully
2. Use Manual trim wheel for trim changes. |
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L/R BL AIR FAIL
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Indicates a possible rupture of bleed air line downstream of the engine firewall.
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1. Engine instruments - monitor.
2. Bl Air Switch (affected eng) - INSTR/ENVIR - OFF (RS) 3. Cabin PX - Checked |
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L/R CHIP DET
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Metal particles may be present in the propeller reduction gearbox.
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*Emergency Engine Shutdown CL - Execute
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FIRE L/R ENG
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Illumination of the FIRE warning light is usually the first indication of engine compartment fire.
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*1. Ground - EESD on Deck CL - Execute
*2. Flight - EESD CL - Execute |
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L/R FUEL PRESS
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Affected side has pressure below 10+- 1psi.
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1. Check for Leak
2. If Leak: EESD Deck/Flight 3. No Leak: -STBY PUMP - ON -FUEL PRESS light - out 4. Light on: Time 10 hrs for suc. feed. |
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INST INV
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Loss of 115 Vac power supply. Either inverter is capable of supplying the full amount of normally required single phase AC power.
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1. Select opposite inverter.
2. Land ASAP |
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BATTERY CHG
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In excess of 7 volt charge for 6 seconds.
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Perform condition check in NATOPS
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CABIN DOOR
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Cabin/cargo door open or not secure.
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1. Crew - Seatbelts Fastened.
2. Cabin - Depressurize. |
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EXT PWR
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External Power source is connected at the external receptacle.
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Light will extinguish when power source is disconnected.
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FDR Fault
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Recorder or data input faulty.
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N/A
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GPWS INOP
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Rad alt, altimeter adapter, or air data computer faulty
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Note GPWS Inop
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L/R ICE VANE
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Affected engine ice vane has not attained proper position.
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1. Visually check bypass door and check ITT/Torque ind.
If Failure: 2. Airspeed - 160 KIAS or less. 3. Ice vane CB- Pulled. 4. ICE VANE - MANUAL PULLED. 5. Airspeed - Resume. |
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L/R NAC LOW
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Affected tank has <247 lbs (30 min).
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1. Land ASAP
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DUCT OVERTEMP
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Excessive bleed air temp in cain heating duct system.
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1. Ensure floor vents not obstructed.
(Abridged) 2. Decrease Env. Temp. 3. Light still on - BL Air Env off one at a time. 4. Light still on - Both off. |
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L/R DC GEN
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Generator Failure.
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1. Starter Switch - Check OFF
2. Generator - OFF, reset, ON. If no reset- 3. Gen - off 4. Inverter - opposite 5. Curr Lim - Checked. 6. Decr Load |
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PROP SYNC ON
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Ldg gear extended with prop sync system ON.
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1. Prop Sync - OFF.
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RVS NO READY
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Props not at HIGH with ldg gear extended.
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1. PROP levers - HIGH RPM. (PF)
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AIR COND N1 LOW
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Right (#2) eng rpm too low for air cond compressor to operate.
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1. Advance n1 on right (#2) to min of 61%.
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L/R AUTOR FEATHER
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Autofeather armed with power levers above 90% N1.
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L/R BLEED AIR OFF
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Affected environmental bleed air valve is closed.
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CAUT LGND OFF
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Caution annunciator is turned off.
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ELECT TRIM OFF
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Electrim trim is off.
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FUEL CROSSFEED
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Crossfeed valve is energized.
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L/R IGNITION ON
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Affected starter/ignition siwtch is in the engine/ignition mode or auto ignition system is armed and engine torque is below 410(+-50) ft-lb.
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LDG/TAX LTS
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Lights are on with landing gear retracted.
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PASS OXY ON
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Passenger oxygen system charged.
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