Term
| CABIN ALT/ RAPID DEPRESSURIZATION |
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Definition
Fine dust from a rapid decompression may trigger a false smoke detector alarm in lavatories. If necessary, pull CALL SYSTEM CB (P-37).
1. Oxygen Masks & Interphone ..................... ON/100% |
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Term
| TAIL COMPARTMENT TEMP HIGH |
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Definition
1. Pneumatic Cross Feed Levers ........................ CLOSE
2. Airfoil Anti-ice Switch(es) ................................. OFF
3. Both Air Conditioning Supply Switches .. HP BLEED OFF |
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Term
| AC POWER FAILURE - COMPLETE LOSS |
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Definition
1. EMERGENCY POWER ................................ ON
If emergency busses are not restored, Pull Battery Direct Bus Feed CB reset lever (floor between captain’s seat and center console). |
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Term
| ELECTRICAL SMOKE OF UNKNOWN ORIGIN |
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Definition
| 1. Oxygen Masks, Smoke Goggles & Interphone ....................... ON/100% |
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Term
| AIR CONDITIONING SMOKE / FUMES |
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Definition
| 1. Oxygen Mask, Smoke Goggles & Interphone ....................... ON/100% |
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Term
| SMOKE / FUMES REMOVAL – PRESSURIZED |
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Definition
WARNING: DO NOT DEPLOY PASSENGER OXYGEN MASKS.
1. Oxygen Mask, Smoke Goggles & Interphone ..................... ON/100% |
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Term
| SMOKE / FUMES REMOVAL – UNPRESSURIZED |
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Definition
This procedure is usable only at low altitudes to remove smoke/fumes from the cockpit only. Descend as required. ELECTRICAL FIRE and AIR CONDITIONING SMOKE procedures must be used as required, prior to using this procedure. Do not use this procedure to remove smoke or fumes from cabin as they will be drawn into the cockpit.
1. Oxygen Masks, Smoke Goggles & Interphone ................. ON/100% |
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Term
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Definition
Rapid roll develops during flap extension beyond 28º:
1. Flap Slat Handle.........RETRACT 28º/LAND |
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Term
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Definition
Fuel flow abnormally high (above 1000 pph) or EGT rapidly approaches ground starting limitations.
1. Fuel Control Lever Affected Engine ......................... OFF |
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Term
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Definition
Avoid manual pitch inputs until autopilot is disconnected. Extended trim operation may result in trim motor thermal shutdown. Trim motor operation may resume after sufficient cooling period.
1. Autopilot ......... DISCONNECT
2. Control Wheel Trim Switches ..................... TRIM IN OPPOSITE DIRECTION OF RUNAWAY
Do not use Longitudinal Trim (suitcase) Handles to Oppose Runaway. |
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Term
| UNCONTROLLED RUDDER MOVEMENT |
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Definition
| 1. Rudder Hydraulic Control Lever ................. MANUAL |
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Term
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Definition
1. Brake Pedal Pressure ............................ RELEASE
2. Anti-Skid Switch ............ OFF
3. Brake Pedal Pressure ........................... REAPPLY |
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Term
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Definition
1. DURING TAKEOFF IF AIRSPEED LESS THAN V1 - 20 Kits
a. Reject Takeoff
b. Return to the Ramp and Determine Cause |
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Term
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Definition
1. APU Fire Control Switch ................ OFF & AGENT ARM
2. If APU FIRE Annunciator Remains Illuminated
a. APU Fire Agent 1 or 2 Switch .................. DISCH
3. If APU FIRE Annunciator Remains Illuminated After 30 Seconds
a. Remaining APU Fire Agent Switch ............................. DISCH |
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Term
| ENGINE FLAMEOUT / FAILURE / SHUTDOWN |
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Definition
An engine flameout will be indicated by N 1 and N2 windmilling, residual fuel flow and oil pressure. If ART activation, good engine parameters may flash on the EDP.
1. If Flameout Suspected:
a. Ignition ........................... OVERRIDE
b. Fuel Supply ............................. CHECK |
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Term
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Definition
| 1. Throttle ........................ IDLE |
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Term
| THRUST REVERSER EXTENSION - IN FLIGHT |
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Definition
| 1. Throttle/Reverse Lever (Affected Engine) ................. IDLE/FULL DOWN |
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Term
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Definition
Engine is unable to accelerate to the normal idle N2 RPM.
1. Affected Engine Hydraulic Pump Switch ............... OFF |
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Term
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Definition
| 1. Throttle (Affected Engine) ................................ IDLE |
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Term
| ENGINE FLAMEOUT - BOTH ENGINES |
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Definition
1. Emergency Power ..................................... ON
2. Ignition ........................... OVERRIDE |
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Term
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Definition
No increase in EGT within 20 seconds from fuel ON.
1. Fuel Control Lever Affected Engine ..................... OFF |
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Term
| OIL PRESSURE LOW AFTER START (on ground) |
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Definition
1. If Oil Pressure below 40 PSI
a. Fuel Control Lever Affected Engine ...................... OFF |
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