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shut off combustible fluids to the engine as quickly as possible.
FOR AN ENGINE FIRE WARNING, PROCEED AS FOLLOWS:
1. Warning Tone..........................................................................................SILENCE
2. Power Lever ...................................................................................................IDLE
NOTE:
Verify proper engine: left or right.
IF FIRE WARNING LIGHT EXTINGUISHES WITH POWER LEVER AT IDLE:
3. Fire Warning System....................................................................................TEST
IF TEST IS SATISFACTORY AND OTHER ENGINE PARAMETERS ARE NORMAL:
4. Affected Engine ..........................................................CONTINUE TO OPERATE
5. BLEED AIR (Affected Engine) .......................................................................OFF
6. ISOLATION Valve .........................................................................................OPEN
7. Altitude ................................................................MAINTAIN FL 410 OR BELOW
IF FIRE WARNING LIGHT REMAINS ILLUMINATED WITH POWER LEVER AT
IDLE:
8. HP Fuel Cock (Affected Engine).................................................................SHUT
9. FIRE Handle (Affected Engine) ...................................................................PULL
10. Fire Extinguisher ............................DISCH 1 (TURN TO EXTREME POSITION)
IF FIRE WARNING LIGHT EXTINGUISHES:
11. Fire Warning System....................................................................................TEST
IF TEST IS SATISFACTORY:
12. Affected Engine .......................................PERFORM SHUTDOWN CHECKLIST
See Section 05-10-10, Engine Failure / Shutdown In Flight.
IF TEST IS NOT SATISFACTORY OR FIRE WARNING LIGHT REMAINS
ILLUMINATED FOR 30 SECONDS FOLLOWING DISCHARGE OF FIRST FIRE
EXTINGUISHER:
13. Fire Extinguisher ............................DISCH 2 (TURN TO EXTREME POSITION)
14. ENGINE FAILURE/SHUTDOWN IN FLIGHT Checklist ....................COMPLETE
OPERATING MANUAL
EXPANDED ABNORMAL / EMERGENCY PROCEDURES 05-12-00
Page 1
May 30/02
Revision 7
See Section 05-10-10, Engine Failure / Shutdown In Flight.
WARNING
THE ENGINE MUST NOT BE RESTARTED AFTER A
FIRE WARNING. LIKEWISE, THE FIRE HANDLE
MUST NOT BE PUSHED IN.
CAUTION
THIS PROCEDURE MUST NOT BE USED FOR
INFLIGHT TRAINING. SHUTTINGDOWNAN ENGINE
BY MEANS OF THE FIRE HANDLE MAY LEAD TO
ENGINE COMPONENT DAMAGE AND VIBRATION.
05-12-20: Engine Fire On Ground
1. Airplane........................................................STOPPED / PARKING BRAKE SET
2. Power Lever ...................................................................................................IDLE
3. HP Fuel Cock................................................................................................SHUT
4. FIRE Handle ..................................................................................................PULL
5. Fire Extinguisher ............................DISCH 1 (TURN TO EXTREME POSITION)
6. Other Engine HP Fuel Cock........................................................................SHUT
IF FIRE WARNING LIGHT(S) EXTINGUISH:
7. Fire Warning System....................................................................................TEST
IF FIRE WARNING TEST IS SATISFACTORY, PROCEED TO STEP 9.
IF FIRE WARNING TEST IS NOT SATISFACTORY OR IF FIRE WARNING LIGHT
REMAINS ILLUMINATED FOR 30 SECONDS:
8. Fire Extinguisher ............................DISCH 2 (TURN TO EXTREME POSITION)
9. ELECTRIC MASTER LEFT PWR, RIGHT PWR AND AUX PWR..................OFF
10. APU MASTER Switch .........................................................PRESS / LIGHT OUT
AFTER TEN (10) SECONDS:
11. BATT 1 / BATT 2 Switches.............................................................................OFF
12. Airplane ...............................................................................................EVACUATE
05-12-30: APU Fire
1. APU Overspeed Test .................................................................................PRESS
2. APU MASTER..................................................................................................OFF
NOTE:
For airplanes SN 1041 and subsequent, and
airplanes SN 1000 through 1040 with ASC 46: After
the APU MASTER switch has been selected OFF,
RPM and EGT indication will continue for thirty (30)
seconds or until RPM decreases below 10%.
OPERATING MANUAL
05-12-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 2
May 30/02
Revision 7
3. APU FIRE Extinguisher.............................................................................PRESS
　
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