EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
35-12-00
ALL ú ú 01 Page 104 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
5. Mask/Regulator Test in Non-Stowed Condition ____Applies to captain's and first officer's stations.NOTE:
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
35-12-00
ALL ú ú 01 Page 105 ú Feb 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
35-12-00
ALL ú ú 01 Page 106 ú Jun 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
6. _______________________________________________
Mask/Regulator Test at First Observer's Station
NOT OK
OK
Move oxygen dilution control to N and rotate PRESS TO TEST knob to non-EMERGENCY position. Squeeze harness inflation ears and remove mask/regulator from head. Release inflation ears.
Turn on cabin interphone and test mask microphone (Ref 23-52-00 A/T).
Stow mask/regulator in mask cup.
System is now operable.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
35-12-00
ALL ú ú 01 Page 107 ú Jun 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
7. __________________________Pressure Indication System
Close crew oxygen cylinder shutoff valve. Bleed off system pressure thru first observer's mask/regulator. Remove test gage from cylinder coupling and install plug. Open crew oxygen cylinder shutoff valve.
System is now operable.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
35-12-00
ALL ú ú 01 Page 108 ú Feb 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
PROCEDURE 1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
35-12-00
ALL ú ú 01 Page 109 ú Feb 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
TEMPERATURE - DEGREES FAHRENHEIT
-40 -22 -4 +14 +32+68 +86 +104 +122 +140
+50
2000
1900 1800 1700 1600 1500 1400 1300 1200 1100 1000 900 800 700
CREW OXYGEN CYLINDER PRESSURE - PSI
TEMPERATURE - DEGREES CELSIUS
MAXIMUM ALLOWABLE PRESSURE FOR FULLY SERVICED CREW OXYGEN CYLINDER
Crew Oxygen Cylinder - Pressure/Temperature Correction Chart Figure 106
H85641
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
35-12-00
ALL ú ú 01 Page 110 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
FLIGHT CREW OXYGEN SYSTEM - ADJUSTMENT/TEST
___________________________________________
1. General_______
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 氧氣 OXYGEN(11)
