737-300机组操作手册Flight Crew Operations Manual FCOM 1(87)

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L
L 7
8 9 U V W X Y 7 8 9 U V W X Y
. .0 +/-Z DEL / CLR 0 +/-Z DEL / CLR
ACMS
SELCAL PUSH SELCAL
1TO 2
2
RESET EVENT PRINT
5  10 
4 
1  1  1 
5 10 15  SYS  510 15  ALTITUDE ALERT BARO REF  LEFT MODE 
+  1  INOP  +  TFR  WX/T  WX  MAP  IDNT 
0 0 --5 510 10 15 15 BOTH WX WX WX/TURB WX/TURB OUT-VAR IN-AUTO OUT-VAR IN-AUTO TEST GAIN GAIN WX INOP INOP  TEST  MODE WX WX+T 1 2  MAP  5 15 UP DN W X R D R GAIN GAIN UCAL 0  LFT TILT 15  TEST  5 15 15 UP DN GAIN UCAL GAIN 0 RGT TILT
MAP FLOOD  RL CONTROLS  MAP PANEL  GAIN -4 -5 -7 -6MIN  TILT 10 155 0 UP  5 TFR  RIGHT MODE WX/T WX MAP  5 IDNT 
-1-2 -3 MAX CAL  DN 5 15 10 
IDNT  STAB 
OFF  OFF 
3  MENU 

11
#
As installed Circled numbers refer to chapters where information on the item may be found.
Copyright . The Boeing Company. See title page for details.
1.20.12  December 6, 2002
Airplane General, Emergency
 
Equipment, Doors, Windows -Instrument Panels
737 Operations Manual
Aft Electronic Panel
OVHT DET OVHT DET
WHEEL
BELL CUTOUT
L BOTTLE R BOTTLE
WELL DISCHARGE DISCHARGE
A B A B ENGINES
FAULT DISCH DISCH DISCH
NORMAL NORMAL ET
XE
8  OVERHEAT ENG 1  L  R  INOP APU DET  OVERHEAT ENG 2  L  R  12 T ST R 
1  E R I F T H V O P O N I T L U A F TEST  DISCHARGE APU BOTTLE  (FUEL SHUTOFF) PULL WHEN ILLUMINATED FIRE SWITCHES LOCK OVERRIDE: PRESS BUTTON UNDER HANDLE  L APU 
5  01260  VHF COMM TFR COMM  18301  F H V 1 FWD AFT ARM ARMED ARMED DISCH TEST AFT NORM A B NORM A B FAULT DETECTOR DET SELECT EXT C O G R A F E R I FWD 7  TFR FREQ SEL COMM TEST  C M M O  5 
FWD  AFT  DISCH 
TEST 
AUTO  NAV  MANUAL  5  AUTO  NAV  MANUAL 
11  TEST  MAN AUTO  3  VOR UP/LT TEST  MAN AUTO  11 
VOR  UP/LT 
DME  DN/RT 
10  ILS VOR/ NAV FULL EXP NAV DH REF RST BRT VOR/ADF ILSVOR/ MAP CTR MAP ADI BRT HSI RANGE MAP PLAN NAV AID WPTRTE DATA ARPT 10 20 40 ON 80 WXR 160 320 DME DN/RT 2  STBY 21 ATC  2001  OFF 21 ALT RPTG 11  DH REF RST BRT ADI  BRT ILS VOR/ NAV FULL EXP NAV VOR/ADF ILS VOR/ MAP CTR MAP HSI RANGE MAP PLAN NAV AID WPT RTE DATA ARPT 10 20 40 ON 80 WXR 160 320  10 
ON  ON  ON  ON  ON  IDENT  REPLY  TEST  ON  ON  ON  ON  ON 
MIC SEL 
5  MIC SEL 
5  1-VHF-2  1- HF INOP FLT INT SERV INT  PA H 3  299 99  5  1-VHF-2  1- HF INOP FLT INT SERV INT PA  5 
1-  NAV- 2  1- ADF -2  MRK  F USB LSB AM  1- NAV- 2  1- ADF -2  MRK 
OFF 
RF 
R/T  MASKS  RV B  SENS  R/T  MASKS  RV B 
3  I/C  BOOM ANT ADF TEST OFF  5  9  4  I/C  299 99 BOOM 
11  F D A  01205 21 21 1 GAIN OFF TEST ANT ADF TONE 01205  15 10 5 15 1050 RUDDER TRIM  F H OFF USB LSB AM  5 
2GAIN     LEFT AILERON  RIGHT RF SENS 
1  FLOOD  PANEL  DOWN WING LEFT  DOWN WING RIGHT  LEFT NOSE  RIGHT NOSE 9 8  OVERRIDE NORM STAB TRIM  UNLOCKED CAB DOOR CAB DOOR  1 
OFF  OFF 

1
TFR
55
CV FREQ SEL O
6H
M MF
6 2
ALT RPTG
IDENT OFF ON
ATC-S
STBY L
R
STAB TRIM
FLT DK DOOR AUTO UNLKD
DENY LOCK FAIL
8
OVRD
AUTO NORM
LOCK
# As installed
Circled numbers refer to chapters where information on the item may be found.
Copyright . The Boeing Company. See title page for details.
December 3, 2004  1.20.13
Airplane General, Emergency Equipment, Doors, Windows -
 
Instrument Panels
737 Operations Manual
OVHT DET  WHEEL  BELL CUTOUT OVHT DET 
WELL  L BOTTLE R BOTTLE 
AB  A  DISCHARGED DISCHARGED B 
8  OVERHEAT ENG 1 LR DISCH NORMAL F A U L T F I R E I N P O V H T O TEST  APU DET INOP FAULT APU BOTTLE DISCHARGED  DISCH  OVERHEAT ENG 2 PULL WHEN ILLUMINATED LOCK OVERRIDE: PRESS BUTTON UNDER HANDLE L DISCH R (FUEL SHUTOFF) E X T T S T E NORMAL FIRE SWITCHES 12 ENGINES APU L R 
　
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