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737
Flight Manual
Continental
ENGINES, APU
Sec. 2.7 TOC-1
Rev. 11/15/02 #41
2.7 – ENGINES, APU
TABLE OF CONTENTS
APU DETECTOR INOPERATIVE.......................................................... 1
>@BCD APU FAULT.............................................................. 1
APU FIRE (INFLIGHT) ........................................................................... 2
APU GEN OFF BUS LIGHT FAILS TO ILLUMINATE
DURING START .............................................................................. 3
> APU HIGH OIL TEMP ....................................................................... 3
APU LOW OIL PRESSURE ................................................................... 4
APU OVERSPEED ................................................................................. 4
APU STARTER FAILS TO ENGAGE..................................................... 4
BATTERY START (EXTERNAL OR APU ELECTRICAL
POWER NOT AVAILABLE) ............................................................. 5
BCD EEC ALTERNATE MODE ................................................... 7
ENGINE / APU FIRE ON GROUND....................................................... 8
BCD ENGINE CONTROL ............................................................ 8
ENGINE FAILURE/FIRE/SHUTDOWN/ SEVERE
DAMAGE/SEPARATION ................................................................. 9
Engine Failure After V1 Procedure................................................ 12
Engine Failure On Final Approach ................................................ 17
ENGINE FIRE / OVERHEAT DETECTOR FAULT ............................. 18
ENGINE HIGH OIL TEMPERATURE................................................... 18
ENGINE LIMIT / SURGE / STALL ....................................................... 19
ENGINE LOW OIL PRESSURE........................................................... 20
ENGINE OIL FILTER BYPASS............................................................. 21
ENGINE OIL PRESSURE IN THE YELLOW BAND ........................... 21
ENGINE OVERHEAT ........................................................................... 22
ENGINES, APU
Sec. 2.7 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
ENGINE OVER TEMPERATURE DURING
TAKEOFF OR INFLIGHT............................................................... 22
ENGINE START - AIR START (BOTTLE PRESSURE) ..................... 23
ENGINE START - CROSSBLEED START ......................................... 23
ENGINE START – FIRE DURING START.......................................... 24
>>@ ENGINE START - HIGH ALTITUDE .................................. 25
ENGINE START - IN FLIGHT .............................................................. 26
ENGINE START – NON NORMAL ...................................................... 28
ENGINE START - START VALVE DOES NOT OPEN....................... 29
ENGINE START - START VALVE OPEN LIGHT ON OR START
VALVE FAILS TO CLOSE BY >>@ 50%
BCD 60% N2 ......................................................................... 29
HIGH ENGINE VIBRATION.................................................................. 30
>>@ LOW IDLE............................................................................ 31
MANUAL START / INOPERATIVE STARTER VALVE....................... 31
ONE ENGINE INOPERATIVE APPROACH AND LANDING ............. 33
ONE ENGINE INOPERATIVE APPROACH AND
LANDING PROCEDURE............................................................... 39
ILS - One Engine Inoperative ......................................................... 39
Go-Around (One Engine Inop)....................................................... 39
Non-Precision Approach One Engine Inoperative ........................ 42
>>@ POWER MANAGEMENT CONTROL
(PMC) INOPERATIVE.................................................................... 45
Takeoff............................................................................................ 45
Inflight ............................................................................................. 45
REVERSER LIGHT ON........................................................................ 46
REVERSER UNLOCKED (INFLIGHT) ................................................ 47
TWO ENGINE FLAMEOUT.................................................................. 48
737
Flight Manual
Continental
ENGINES, APU
Sec. 2.7 Page 1
Rev. 11/15/02 #41
ENGINES, APU
APU DETECTOR INOPERATIVE
The APU DET INOP light illuminated indicates the APU fire detection system is
inoperative.
APU Switch..................................................................................................OFF
　
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