(d)
Set the L and R PACK switches to OFF.
(e)
Stop the APU (Ref 49-11-00/201).
(f)
Set the APU BLEED switch to OFF.
S 862-026
(16)
Start the engines and let the engines operate at ground idle speed (Ref 71-00-00/201).
S 862-027
(17)
Operate the air conditioning packs:
NOTE: This procedure uses the engine bleed air to remove the
____ oil contamination from the conditioned air in the airplane.
(a)
Set the position of these switches on the P5-10 overhead panel as follows: 1) L and R PACK switches to AUTO 2) BLEED 1 and 2 switches to ON
(b)
Let the air conditioning packs operate until the conditioned air in the airplane has no smell of the oil contamination.
(c)
Set the L and R PACK switches to OFF.
S 862-028
(18)
Stop the engines (Ref 71-00-00/201).
S 862-029
(19)
Set these switches to OFF on the P5-10 overhead panel:
(a)
L and R PACK switches
(b)
RECIRC FAN
S 212-030
(20) Examine these components for oil contamination:
(a) Heat exchangers
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
21-00-01
ALL ú ú 03 Page 204 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(b) Coalescer bags in the water separators
S 102-032
(21)
Do the procedure again, if required, until the conditioned air in the airplane has no smell of the oil contamination.
S 412-033
(22)
Close the access doors to the air conditioning bays.
S 862-034
(23)
Remove the electrical power if it is not necessary (Ref 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
21-00-01
ALL ú ú 03 Page 205 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AIRPLANE ABILITY TO MAINTAIN CABIN PRESSURE
___________________________________________ IN FLIGHT ON SINGLE PACK OPERATION - TROUBLE SHOOTING
_____________________________________________________
1. General_______
A. Trouble shooting the airplane ability to maintain cabin pressure in flight on a single pack operation involves the air cycle system, the pneumatic supply system, the pressurization control system, and various airplane openings that could possibly be a source of leakage. An understanding of how the different components are interrelated as well as the function of each is needed to locate and correct problems in either system.
2. Preparation for Trouble Shooting________________________________
A. Supply electrical power (AMM 24-22-00/201).
B. Make sure that all air conditioning circuit breakers are on.
C. Make sure that all pressurization control system circuit breakers are on.
3. Trouble Shooting Chart (Fig. 101)
______________________
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
21-00-05
ALL ú ú 01 Page 101 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SYSTEM REQUIREMENT MINIMUM YES NO REQUIREMENT SATISFIED
SINGLE PACK - LOW FLOW ABLE TO MAINTAIN CABIN CONFIDENCE IS HIGH THAT CONFIDENCE IS LOW THAT
MODE DIFFERENTIAL PRESSURE OF AIRPLANE WILL MAINTAIN AIRPLANE WILL MAINTAIN
3.9 - 4.1 PSID AND CABIN PRESSURE WITH SINGLE PACK PRESSURE ON SINGLE PACK
RATE OF CHANGE IS NO IN HIGH FLOW MODE WHILE IN THE HIGH FLOW MODE AT
MORE THAN -100 FEET/ AT CRUISE. CRUISE. EMPHASIS NEEDS
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 空调 AIR CONDITIONING 1(19)
