2 Emergency/ Abnormal Procedures

Question 1

TAIL COMPARTMENT TEMP HIGH (21.4)

Answer 1

Pneumatic Cross Feed levers……CLOSE
Airfoil Anti-Ice SW’s……OFF
Both Air Cond. supply SW’s…..HP BLEED OFF

Question 2

CABIN ALT/RAPID DEPRESSURIZATION (21.2)

Answer 2

Oxygen mask and Interphone…….ON/100%

Fine dust from a rapid decompression may trigger a false smoke detector alarm in lavatories. If necessary, pull CALL SYSTEM CB (P-37)

Question 3

AC POWER FAILURE-COMPLETE LOSS (24.2)

Answer 3

EMERGENCY POWER……ON

If emergency buses are not restored, pull battery direct bus feed CB reset lever (floor between captain’s seat and center console)

Question 4

ELECTRICAL SMOKE OF UNKNOWN ORIGIN: (24.4)

Answer 4

Oxygen Masks, Smoke Goggles and Interphone…..ON/100%

Question 5

AIR CONDITIONING SMOKE/FUMES: (26.2)

Answer 5

Oxygen Masks, Smoke Goggles and Interphone……..ON/100%

Question 6

SMOKE/FUMES REMOVAL - PRESSURIZED: (26.5)

Answer 6

Oxygen Masks, Smoke Goggles and Interphone……..ON/100%

Warning: DO NOT DEPLOY PASSENGER OXYGEN MASK

Question 7

SPOILER FLOAT: (27.2)

Answer 7

Flap slat Handle…….RETRACT 28*/LAND

Rapid roll develops during flap extension beyond 28*

Question 8

STABILIZER RUNAWAY: (27.2)

Answer 8

Autopilot……..DISCONNECT
Control Wheel Trim Switches……….TRIM IN OPPOSITE DIRECTION OF RUNAWAY
DO NOT USE LONGITUDINAL TRIM (suitcase) HANDLES TO OPPOSE RUNAWAY

Question 9

SMOKE/FUMES REMOVAL - UNPRESSURIZED: (26.5)

Answer 9

Oxygen Masks, Smoke Goggles and 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.

Question 10

UNCONTROLLED RUDDER MOVEMENT: (27.3)

Answer 10

Rudder Hydraulic Control Lever…….MANUAL

Question 11

BRAKE FAILURE on GROUND: (32.2)

Answer 11

Brake pedal pressure………RELEASE
Anti-Skid Switch…….OFF
Brake pedal pressure…….REAPPLY

Question 12

WHEEL NOT TURNING LIGHT ILLUMINATED: (32.12)

Answer 12

DURING TAKEOFF IF AIRSPEED LESS THAN V1-20Kts

• Rejected takeoff
• Return to the ramp and determine cause

Question 13

APU FIRE: (49.2)

Answer 13

APU fire control switch…….OFF and AGENT ARM
If APU fire annunciator remains illuminated
- APU fire agent 1 or 2 …….DISCHARGE
If APU fire remains illuminated after 30 seconds
- Remaining APU fire agent switch…….DISCHARGE

Question 14

ENGINE FIRE: (72.2)

Answer 14

Throttle (Affected Engine)……IDLE

Question 15

ENGINE FLAMEOUT - BOTH ENGINES: (72.4)

Answer 15

Emergency power…..ON

Ignition…………OVERRIDE

Question 16

ENGINE FLAMEOUT/FAILURE/SHUTDOWN: (72.3)

Answer 16

If flameout suspected:
Ignition …..OVERRIDE
Fuel supply…..CHECK

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.

Question 17

TAILPIPE FIRE: (72.6)

Answer 17

Throttle (Affected engine)……IDLE

Question 18

THRUST REVERSER EXTENSION - IN FLIGHT (72.7)

Answer 18

Throttle/Reverse lever (Affected engine)…..IDLE/FULL DOWN

Question 19

HOT START: (72.19)

Answer 19

Fuel control lever (Affected engine) ………..OFF

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

Question 20

HUNG START: (72.19)

Answer 20

Hydraulic pump switch (Affected engine)……OFF

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

Question 21

NO START: (72.20)

Answer 21

Fuel control lever (Affected engine)…..OFF

No increase in EGT within 20 seconds from fuel ON.

Question 22

OIL PRESS LOW AFTER START (On Ground): (72.20)

Answer 22

If oil pressure below 40 psi

- Fuel control lever (Affected engine)……OFF