Chapter 9 Emergency Procedures (updated 14 NOV 2016)

Question 1

EMERGENCY SHUTDOWN

Answer 1

1) POWER lever (affected engine) - FLT IDLE.
2) Condition lever (affected engine) - FUEL SHUTOFF.
3) PULL FUEL OFF handle (affected engine) - Pull.

Question 2

SMOKE & FUMES ACTIONS

Answer 2

1. Crew oxygen masks & goggles - 100% and ON.
2. ICS switch - MASK. Establish communications.
   3) DOME light switch - ON.
   4) EMER LTS switch - ON.
   5) FASTEN BELT switch - ON.

Question 3

ENGINE MALFUNCTION BEFORE V1

Answer 3

1. POWER levers (4) - DISC.
2. Braking - As required.
3. Reverse - As required.

Question 4

ENGINE MALFUNCTION AT OR AFTER V1

Answer 4

1) POWER levers (4) - Maximum available.
2) LANDING GEAR (after positive rate of climb) - UP.
3. Airspeed - Climb at V2.
4) Confirm - Autofeather, no fire.

If engine failure, no feather:

5) Condition lever (failed engine) - FUEL SHUTOFF.

Above 400’ AGL:

6. Airspeed - Accelerate to Vclimb.
   7) FLAPS (on profile) - Select up.
   8) EMERGENCY SHUTDOWN (affected engine) - Complete.
   9) EXTG switch (if required) - FWD BTL, wait 30 seconds, if fire persists - EXTG switch - AFT BTL.

Question 5

ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT

Answer 5

1) SYNCHROPHASE switch - OFF.
2. Power - As required.
3) Affected Engine - Identify
4) EMERGENCY SHUTDOWN (affected engine) - Complete.

Question 6

TWO ENGINES MALFUNCTION OPERATIONS

Answer 6

1. Condition levers (FWD 3) - MAX RPM.
2. Power - Maximum Available.

Caution: ENGINE BLEED switches on operating engines off to avoid reducing potential power available. (paraphrased)

3. Complete appropriate memory items / checklist for second engine malfunction

Question 7

TWO ENGINE GO-AROUND OR MISSED APPROACH PROCEDURE

Answer 7

1. POWER levers (4) - Maximum available.
2. LANDING GEAR - Up.
   3) FLAPS - Up.
   4) Airspeed - 118 KIAS.
3. Bank Angle - 30* maximum.

Warning:

• With #1 and #2 engines inop, flaps cannot be retracted from 15* or 25* position, but will retract from 45* when selected to 25* position. Do not attempt GO-AROUND with Flaps Extended and #1 and #2 Engines inop.
• With #3 and #4 engines inop, the gear cannot be retracted following extension by the alternate method. Do not attempt GO-AROUND with LANDING GEAR DN and #3 and #4 Engines inop.

Question 8

ALL ENGINES INOPERATIVE

Answer 8

Airspeed - 1.3Vs (for appropriate weight / flap setting)

Question 9

OVERTEMPERATURE (OTHER THAN STARTING)

Answer 9

1) ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT checklist - Complete.

Question 10

ENGINE Ng OVERSPEED

Answer 10

1) SYNCHROPHASE switch - OFF.
2) POWER lever (affected engine) - FLT IDLE.

If there is no response to power lever movement:

3) PULL FUEL OFF handle (affected engine) - Pull.

Below 1,500 FT/LB Torque:

4) Condition lever (affected engine) - FUEL SHUT OFF.

Question 11

ABNORMAL OIL PRESSURE
#1, #2, #3, or #4 ENG OIL PRESS caution light on:

Answer 11

If Engine OIL PRESS confirmed below 75 PSI:

1) Complete ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT checklist

Question 12

ABNORMAL OIL TEMPERATURE

Answer 12

If Engine OIL TEMP remains above 99*C for more than 15 minutes:

1) Complete ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT checklist

Question 13

PROPELLER OVERSPEED

Answer 13

1) SYNCHROPHASE switch - OFF.
2. POWER lever (affected engine) - FLT IDLE.
3. Airspeed - Reduce.
4) Condition lever (affected engine) - START & FEATHER.

If propeller does not feather:

5) Condition lever (affected engine) - FUEL SHUT OFF.

Question 14

ENGINE FIRE OR SEVERE ENGINE DAMAGE - ON THE GROUND

Answer 14

After aircraft is stopped and EMERG BRK set to PARK:

1. POWER levers (4) - FLT IDLE.
2. Condition levers (4) - FUEL SHUTOFF.
3. PULL FUEL OFF handle (Illuminated) - Pull.
4. EXTG switch - FWD BTL (wait 5 sec.), AFT BTL.
5. APU STOP switch - Press for one second. (if applicable)
6. Notify ATC and Crew of impending evacuation.
7. Master BATTERY switch - OFF.
8. DC EXT PWR switch - OFF. (if applicable)
9. Evacuate Aircraft.

Question 15

ENGINE FIRE OR SEVERE ENGINE DAMAGE - IN FLIGHT

Answer 15

1) SYNCHROPHASE switch - OFF.
2. Power - As required.
3) Affected Engine - Identify.
4) EMERGENCY SHUTDOWN (affected engine) - Complete.
5) EXTG switch - FWD BTL. (wait 30 seconds) if fire persists - AFT BLT.

Question 16

APU FIRE OR SEVERE ENGINE DAMAGE

Answer 16

1. APU FIRE PUSH switch light - Press for 1 second and release.
2. APU ON indicator - Not illuminated.

If APU FIRE PUSH indicator is still illuminated:

3. APU FIRE BOTTLE switch - Activate.
4. Master BATTERY switch - OFF.
5. DC EXT PWR switch - OFF.
6. APU DC GEN ON switch - Off.
7. Evacuate aircraft.

Question 17

FIRE DETECTION SYSTEM FAILURE

Answer 17

Caution: The following check must be executed within a period of time not to exceed 60 seconds.

1) DETECTOR LOOPS switch - Select Non-Illuminated Loop Position.
2) FIRE WARN Test - Conduct.

Question 18

FUSELAGE FIRE OR SMOKE EMERGENCIES
  - AFT BAG SMOKE
  - IN FLIGHT COMPARTMENT
  - IN CABIN
  - UNKNOWN SOURCE OF SMOKE
ELECTRICAL SYSTEM SMOKE OR FIRE
  - IN FLIGHT

Answer 18

1. SMOKE & FUMES ACTIONS - Complete.

Question 19

RIGHT DC BUS FAULT

Answer 19

DC BUS followed by : SEC INV, AUX INV, R STALL WARNING, #3 DC GEN, #4 DC GEN, PITOT HEAT - caution lights on:

1) DOME light switch - DOME.
2) PANEL LIGHTING circuit breakers (8), center ovhd panel - Pull.

Question 20

INVERTER FAILURES

• PRI INV caution light on or
• AUX INV caution light on

Answer 20

1) 115V BUS TIE circuit breaker (2nd row right ovhd panel) - Pull.

Question 21

INVERTER FAILURES

- SEC INV caution light on

Answer 21

1) INV SEL switch - R BUS.

2) 115V BUS TIE circuit breaker (2nd row right ovhd panel) - Pull.

Question 22

TWO INVERTERS FAILED

Answer 22

Second INVERTER caution light on:

1) DOME light switch - DOME.
2) PANEL LIGHTING circuit breakers (8), center ovhd - Pull.

Question 23

ROLL AXIS JAM OR MALFUNCTION - CONTROL WHEEL IMMOVABLE

Answer 23

1. Autopilot - Disengage.
2. Call out “ROLL JAM.”
3. ROLL DISC T handle - Pull and rotate 90*. Pilot with unjammed wheel has control.

Question 24

ROLL SPLR SWITCH LIGHT ON

Answer 24

1. Autopilot - Disengage.

2. ROLL SPLR switch light - PUSH OFF.

Question 25

ELEVATOR CONTROL JAM IN FLIGHT

Answer 25

1. Autopilot - Disengage.
2. Control column - Apply pressure, Call out “PITCH JAM HELP.”
3. Airspeed and flap setting - Maintain.
   4) Control column - Apply pressure against jam.

If jam persists, relax control column force momentarily.

5. PITCH DISC T handle - Pull and rotate 90*
6. Pilot with free control column flies aircraft.

Question 26

AIRCRAFT ROLLS WITH NO CONTROL WHEEL INPUT

Answer 26

1. Autopilot - Disengage.

Question 27

FAILURE OF ANY ONE TRAILING FLAP SEGMENT TO RETRACT FROM 45* TO 25*

Answer 27

1. Airspeed on go-around - 98 KIAS maximum.

Question 28

AILERON TRIM TAB RUNAWAY or
RUDDER CONTROL MALFUNCTION or
RUDDER TRIM ACTUATOR RUNAWAY

Answer 28

1. Autopilot - Disengage.

Question 29

CABIN PRESSURIZATION LOST WHEN OPERATING ABOVE 10,000 FEET - CABIN PRESS caution light on

Answer 29

1. Crew Oxygen Masks - 100% and On, Establish Communications.

Question 30

EMERGENCY DESCENT - NO STRUCTURAL DAMAGE INVOLVED

Answer 30

1) SYNCHROPHASE switch - OFF.
2. POWER levers - FLT IDLE.
3. Condition levers - MAX RPM.
4. Airspeed - Vmo.

Question 31

EMERGENCY DESCENT - STRUCTURAL DAMAGE INVOLVED

Answer 31

1) SYNCHROPHASE switch - OFF.
2. POWER levers - FLT IDLE.
3. Condition levers - MAX RPM.
4. Airspeed - 124 KIAS.
5) FLAP selector - Select 15. (below 147 KIAS)
6) LANDING GEAR handle - DN. (below 147 KIAS)
7) FLAP selector - Select 25. (below 124 KIAS)