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GEAR
HYD
ICE
IND/RECORD
LIGHTS
NAV
OIL
OXYGEN
THRUST REV
P I LOT T R A I N I N G GU I D E
EMERGENCY EQUIPMENT
8-22 For Training Purposes Only
Sept 04
PAGE INTENTIONALLY LEFT BLANK
Vol. 2
Sep 09/02
ABNORMAL PROCEDURES 05--02--3
In--Flight Engine Failures
Flight Crew Operating Manual
CSP C--013--067
”Half Bank”:
G Speed < V2 + 10
TAKE-OFF --- ENGINE FAILURE AFTER V1
PF:
G Rotate
towards FD
PF:
G “Gear
Up”
PF:
G V2
G “Speed Mode”
PF:
G Call Lateral Mode
as required
600 feet AGL
PF:
G “Autopilot On”
PF:
G Call for immediate action items
Acceleration ALT
(1,000’ AAE)
PF:
G Call Flaps
on schedule
PF:
G “Max Continuous Thrust”
G Set thrust levers to CLIMB detent
PNF:
G “V1”
PNF:
G “Rotate”
PNF:
G “Positive Rate”
G Climb at VT
PNF:
G State malfunction
Engine Failure
PF:
G MAX Thrust
PF:
G “What’s the
problem?”
PNF:
G Identify mulfunction
PF:
G Engage ALT
G Call for QRH Procedure (s)
G “Climb Check”
For Training Purposes Only
Sept 04
9-i
P I LOT T R A I N I N G GU I D E
FIRE PROTECTION
Chapter 9: Fire Protection TABLE OF CONTENTS
Page
Introduction .........................................................................................................................9-1
Flight Compartment Fire Warning .................................................................................9-2
Fire Detecting System...................................................................................................9-2
Main Wheel Well Overheat Warning .............................................................................9-2
Fire Agent Discharge Indication....................................................................................9-2
Smoke Detection...........................................................................................................9-2
Portable Fire Extinguishers ...........................................................................................9-2
Description ..........................................................................................................................9-3
System Overview Schematic ........................................................................................9-3
FIDEEX Control Unit ..................................................................................................... 9-4
Main Engine Fire Detection...........................................................................................9-5
Engine FIDEEX Control Schematic......................................................................... 9-6
APU Compartment Fire Detection.................................................................................9-7
APU FIDEEX Control Schematic ............................................................................9-8
Main Wheel Well (MWW) Overheat Detection ..............................................................9-9
Smoke Detection......................................................................................................... 9-10
Fire Handles................................................................................................................ 9-12
Engine Fire.................................................................................................................. 9-13
APU Fire......................................................................................................................9-14
Shutoff Valves (SOV).................................................................................................. 9-15
Fire Extinguisher Assembly......................................................................................... 9-16
Fire Extinguisher Discharge Bottles ...................................................................... 9-16
Fire Extinguisher Gauges...................................................................................... 9-17
Main Engine Fire Extinguishing............................................................................. 9-18
APU Compartment Fire Extinguishing .................................................................. 9-20
APU FIDEEX/FADEC Interface............................................................................. 9-20
Pilot-Initiated Test ....................................................................................................... 9-21
　
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