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11. If Smoke Continues:
A. Electric Masters Left, Right, AUX Power Switch......................
........................................................ ON (AS APPROPRIATE)
B. ESS AC and DC Buses..................................................AUTO
C. Pressurization Control...............................................MANUAL
At Power Distribution Box (PDB):
CAUTION: DO NOT ATTEMPT TO RESET ANY POPPED CIRCUIT
BREAKERS.
D. ESS AC and ESS DC Circuit Breakers....................................
.................................PULL AND RESET ONE (1) AT A TIME
Allow sufficient time (approximately thirty [30] seconds) for
smoke to stop between each PULL and RESET.
CAUTION: PULLING ESS DC BUS PILOT CIRCUIT BREAKER
2 WILL DISABLE MANUAL CONTROL OF PRESSURIZATION
SYSTEM. RESELECT AUTO MODE IF PULLING THIS CIRCUIT
BREAKER STOPS SMOKE.
If smoke stops after any one (1) circuit breaker is pulled:
E. Proceed to nearest suitable airport and land.
NOTE: See Master Table of Electrical Component Availability,
page EA-22, to assist in determining inoperative items with a
specific CB pulled.
F. Yaw Damper and / or Mach Trim Limits...................................
...............................................OBSERVE AS APPROPRIATE
G. Pressurization Control....................................................AUTO
(IF AVAILABLE, PILOTS PHASE A CB, ESS AC SECTION)
H. Windshield Heat...........OFF TWO (2) SECONDS, THEN ON
I. FGC CBs............. PULL AND/OR RESET (AS NECESSARY)
(FGC #1: CPO, A-7; FGC #2: CPO, B-7)
12. If Smoke Still Continues:
A. Electrical System......................................................................
............................RETURN TO NORMAL CONFIGURATION
B. Windshield Heat...........OFF TWO (2) SECONDS, THEN ON
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page ED - 8 May 30/02
Electrical Smoke / Fire: Source Unknown, ctd… AFM 4-12-50
C. FGC CBs ............ PULL AND/OR RESET (AS NECESSARY)
D. Check for another source of smoke.
E. Proceed to nearest suitable airport and land.
END
Engine Fire Warning System Malfunction AFM 4-13-10
In the event of a single FIRE TEST LOOP light:
1. Lighted Fire Test Switchlight ................................................PRESS
If warnings illuminate:
A. Fire Test Switch ...................................................... RELEASE
B. Faulty Loop With Fault Switch On FIRE DETECTION Panel ..
..................................................................................DISABLE
If warnings DO NOT illuminate:
A. Fire Test Switch ...................................................... RELEASE
B. Engine Fire Checklist (Page ED-3) ......................COMPLETE
END
Fire Detection System Fault AFM 3-13-20
Each of the two (Loop A and Loop B) fire detection loops of each
engine is provided with a fault discriminator circuit. Fault indicators
and a single test button to test all four loops are located in the
ENGINE CONTROL section of the overhead panel.
If a fire detection loop develops a fault, the associated amber fault
light will illuminate and an amber ENG FLT LOOP ALRT caution
message with the associated tone will be generated. Since both loops
must sense a fire or overheat in order to trigger an engine fire
warning, the faulty loop will preclude that capability until it has been
isolated from the system. The faulty loop is isolated and fire detection
system is restored to normal operation by pressing the amber FAULT
switchlight, at which time the OFF portion of the switchlight will
illuminate.
END
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page ED - 9
Engine Overheat AFM 4-21-10
For engine overheat (L-R ENGINE HOT red warning message on
CAS and associated warning tone), proceed as follows:
1. Engine Bleed .......................................OFF (AFFECTED ENGINE)
2. Power Lever ................................ RETARD (AFFECTED ENGINE)
If engine overheat message is extinguished, continue operating
with reduced engine power.
If light persists, immediately proceed as follows:
3. HP Fuel Cock .........................................................................SHUT
NOTE: If HP fuel cock lever is jammed and cannot be closed, pull FIRE
handle.
4. Power and Trim .......................................................AS REQUIRED
5. Gear and Flaps........................................................AS REQUIRED
6. Engine Failure / Shutdown Inflight Checklist (Page EC-6) ...............
.....................................................................................COMPLETE
　
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