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IF N2 Is Below >>@ 15%; BCD 11% With APU Air
Available:
Throttles................................................................................CLOSED
Wing Anti-Ice Switch ..................................................................OFF
Pack Switches ...............................................................................OFF
APU Bleed Air Switch...................................................................ON
Ignition Select Switch ...............................................................BOTH
Either Start Switch .....................................................................GRD
At A Minimum Of >>@ 15% N2; BCD 11% N2:
(Continued)
OR
OR
~
737
Flight Manual
Continental
ENGINES, APU
Sec. 2.7 Page 51
Rev. 11/15/02 #41
Start Lever.................................................................IDLE DETENT
Monitor engine instruments. If no increase in EGT is observed
within 30 seconds, return start lever to CUTOFF and start switch to
OFF.
IF Engine Starts:
Accomplish ¶ above.
IF First Start Attempt Is Not Successful:
Repeat above steps on other engine.
IF Second Attempt Is Not Successful:
Accomplish the ENGINE START - INFLIGHT checklist.
IF APU Bleed Air Is Unavailable OR N2 Is Above >>@ 15% N2;
BCD 11% N2 :
Note: If altitude permits, with no APU Bleed Air available,
accelerate to a speed where N2 Is Above >>@ 15%
N2; BCD 11% N2 :
Throttles................................................................................CLOSED
Wing Anti-Ice Switch ..................................................................OFF
Pack Switches ...............................................................................OFF
Ignition Select Switch ...............................................................BOTH
Start Switches................................................................................FLT
Start Lever.................................................................IDLE DETENT
Monitor engine instruments. If no increase in EGT is observed
within 30 seconds, return start lever(s) to CUTOFF.
IF Engine Starts:
Accomplish ¶ above.
IF Neither Engine Starts:
Accomplish the ENGINE START - INFLIGHT checklist.
* * * *
~
OR
ENGINES, APU
Sec. 2.7 Page 52
Rev. 11/15/02 #41
Continental
737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
FIRE PROTECTION
Sec. 2.8 TOC-1
Rev. 11/15/02 #41
2.8 – FIRE PROTECTION
TABLE OF CONTENTS
AIR CONDITIONING SMOKE........................................... SEE SEC. 2.2
APU FIRE (INFLIGHT) ...................................................... SEE SEC. 2.7
>>@ CARGO FIRE DETECTION INDICATION
WITH NO FIRE WARNING.............................................................. 1
BCD CARGO FIRE DETECTOR FAULT .................................... 1
>>@ CARGO FIRE INDICATION ................................................. 2
BCD CARGO FIRE INDICATION................................................. 4
>>@ CARGO FIRE LOOP FAILURE............................................ 5
ELECTRICAL FIRE / SMOKE........................................... SEE SEC. 2.6
ENGINE / APU FIRE ON GROUND.................................. SEE SEC. 2.7
ENGINE FAILURE/FIRE/SHUTDOWN SEVERE
DAMAGE/SEPARATION ............................................SEE SEC. 2.7
FIRE DURING START.......................................................SEE SEC. 2.7
LAVATORY SMOKE PROCEDURE...................................................... 6
Smoke Detector False Activation .................................................... 6
SMOKE / FUMES REMOVAL ................................................................ 7
WHEEL WELL FIRE........................................................SEE SEC. 2.14
FIRE PROTECTION
Sec. 2.8 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
FIRE PROTECTION
Sec. 2.8 Page 1
Rev. 11/15/02 #41
FIRE PROTECTION
>>@ CARGO FIRE DETECTION
INDICATION WITH NO FIRE WARNING
The DET light has illuminated in a single loop causing the Master CAUTION and
OVHT/DET to illuminate.
ARM Selector Switch ............................................................................. AUTO
Test Switch................................................................................................ PUSH
Verify normal system test.
Test Switch........................................................................................RELEASE
　
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