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%

1. Pneumatic Cross Feed Levers........................... CLOSE

2. Airfoil Anti-ice Switch(es)..................................... OFF

3. Both Air Conditioning

    Supply Switches ................................. HP BLEED OFF

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).

1. Oxygen Masks,

    Smoke Goggles & Interphone................... ON/100%

1. Oxygen Masks,

Smoke Goggles & Interphone ................ ON/100%

WARNING: DO NOT DEPLOY PASSENGER OXYGEN MASKS.

1. Oxygen Masks,

Smoke Goggles & Interphone ................ ON/100%

This procedure is usable only at low altitudes to remove smoke/fumes from the cockpit only. Descend as required. ELECTRICAL SMOKE OF UNKNOWN ORIGIN 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%

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.

Rapid roll develops during flap extension beyond 28°:

1. Flap Slat Handle............................RETRACT 28°/LAND

1. Rudder Hydraulic Control Lever..................... MANUAL

1. Brake Pedal Pressure................................... RELEASE

2. Anti-Skid Switch................................................. OFF

3. Brake Pedal Pressure................................... REAPPLY

1. DURING TAKEOFF IF AIRSPEED LESS THAN V1-20Kts

a. Reject Takeoff

b. Return to the Ramp and Determine Cause

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

1. Throttle (Affected Engine)................................... IDLE

1. Emergency Power.................................................ON

2. Ignition.................................................... OVERRIDE

An engine flameout will be indicated by N1 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

1. Throttle (Affected Engine)................................... IDLE

1. Throttle/Reverse Lever

    (Affected Engine) ........................... IDLE/FULL DOWN

Fuel flow abnormally high (above 1000 pph) or EGT rapidly approaches ground starting limitations.

1. Fuel Control Lever (Affected Engine)..................... OFF

Engine is unable to accelerate to the normal idle N2 RPM.

1. Hydraulic Pump Switch (Affected Engine)............... OFF

No increase in EGT within 20 seconds from fuel ON.

1. Fuel Control Lever (Affected Engine)..................... OFF

1. If Oil Pressure below 40 PSI

a. Fuel Control Lever (Affected Engine)................ OFF