HEAT OCCURS AFTER TAKEOFF, 40
EXTEND GEAR SOON FOR AT LEAST 8 MINUTES.
60
RTO
LANDING
MAX AUTO
CLEAR RUNWAY IMMEDIATELY.
UNLESS REQUIRED, DO NOT
SET PARKING BRAKE. DO NOT
4
APPROACH GEAR OR ATTEMPT
3
2
TAXI FOR ONE HOUR. TIRE,
WHEEL, AND BRAKE REPLACE-
1
MENT MAY BE REQUIRED. IF OVERHEAT OCCURS AFTER TAKEOFF, EXTEND GEAR SOON
FOR AT LEAST 12 MINUTES.
BRAKE TEMPERATURE MONITOR INDICATION MAY BE USED 10 TO 15 MINUTES AFTER AIR-PLANE HAS COME TO A COMPLETE STOP, OR INFLIGHT WITH GEAR RETRACTED TO DETERMINE RECOMMENDED COOLING SCHEDULE.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
05-51-10
ALL ú ú 01 Page 202 ú Feb 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
D. A high energy stop condition can be a refused takeoff. It can also be a stop or sequence of stops that collects energy in the CAUTION or FUSE PLUG MELT range (Fig 201). An indication that a high energy stop, or equivalent, has been made is the release of a wheel fuse plug. Energy levels are different between brakes after stops in the COOLING RECOMMENDED RANGE. One or more brakes could have absorbed energy in the CAUTION range, and one or more wheel fuse plugs released.
TASK 05-51-10-202-001
2. High Energy Stop
________________
A. Standard Tools and Equipment
(1)
Borescope - Fiber Optic Light Supply - Model BLS-97, American Cystoscope Makers Inc. Industrial Division, Pelham, New York
(2)
Borescope - Fiber Optic Light Supply - Model BLS-98, American Cystoscope Makers Inc. Industrial Division, Pelham, New York
(3)
Rigid Boroscope - Model BFO-3920A, American Cystoscope Makers Inc. Industrial Division, Pelham, New York
(4)
Flexible Boroscope - Model BF1F-3127DD, American Cystoscope Makers Inc. Industrial Division, Pelham, New York
(5)
Borescope - Fiber Light Carrier - Model FO-400-5A, American Cystoscope Makers Inc. Industrial Division, Pelham, New York
(6)
Rigid Borescope Model FIB 730, Richard Wolf Medical Instruments Corp. Rosemont, Illinois
(7)
Manifold - Landing Gear Brake Tooling - MIT 60B00150, Richard Wolf Medical Instruments Corp. Rosemont, Illinois
(8)
Rigid Borescope Model FIB 740, Richard Wolf Medical Instruments Corp. Rosemont, Illinois
(9)
Rigid Borescope Model FIB 760, Richard Wolf Medical Instruments Corp. Rosemont, Illinois
B. Consumable Materials
(1)
B00728 Solvent - Kerosene
(2)
E00002 Stripper - Turco 5351
C. References
(1)
07-11-03/201, Jacking Airplane Axles
(2)
AMM 32-41-15/401, Landing Gear Brake Unit
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
05-51-10
ALL ú ú 01 Page 203 ú Jun 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(3)
AMM 32-41-15/601, Brakes - Landing Gear
(4)
32-42-04/401, Antiskid Transducer
(5)
AMM 32-45-01/401, Main Gear Tire and Wheel
(6)
AMM 32-45-03/601, Wheels
(7)
AMM 32-45-04/601, Tires
(8)
51-21-01/701, Interior and Exterior Finishes (Paint Stripping)
D. High Energy Stop Conditional Inspection - In COOLING RECOMMENDED Range
S 212-029
(1) Do the steps that follow for the Figure 201 Cooling Recommended range:
(a)
Move the airplane away from the runway.
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 限制/維護(hù)檢查(29)
