(6)
Rigid Borescope - Model FIB 730, Richard Wolf
Medical Instruments Corp., Rosemont, Illinois
(7)
Rigid Borescope - Model FIB 740, Richard Wolf
Medical Instruments Corp., Rosemont, Illinois
(8)
Rigid Borescope - Model FIB 760, Richard Wolf
Medical Instruments Corp., Rosemont, Illinois
B. References
(1)
32-41-10/401, Main Gear Wheel Brake - Removal/Installation
(2)
32-41-10/601, Main Gear Wheel Brake - Inspection/Check
(3)
32-42-06/401, Antiskid Transducer - Removal/Installation
(4)
32-45-03/601, Tires - Inspection/Check
(5)
32-45-04/601, Wheels - Inspection/Check
C. High Energy Stop Conditional Inspection - In CAUTION Range
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
05-51-14
ALL ú ú 01 Page 202 ú Sep 20/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
1000
BRAKE COOLING SCHEDULE CATEGORY "A" BRAKES (STEEL) LB KG 260
240
220
200
180
160
140 0 2 4 6 8
OAT ALTITUDEWEIGHT
EVENT PRESSURE
AUTOBRAKE1000 FT
`C
0
20
40
60
RTO
LANDING
SETTING
BTMS
MAX 4 3 2 1
NOT ALL AIRPLANES HAVE BTMS
Brake Energy Figure 201 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
FOR AT LEAST 12 MINUTES.
K27446
ú ALL ú ú 01
05-51-14
Page 203
ú Sep 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
1000
BRAKE COOLING SCHEDULE CATEGORY "B" BRAKES (CARBON) LB KG 260
240
220
200
180
160
140 0 2 4 6 8
OAT ALTITUDE WEIGHT
EVENT PRESSURE
AUTOBRAKE 1000 FT
`C
0
20
40
60
RTO
LANDING
SETTING
MAX 4 3 2 1
NOT ALL AIRPLANES HAVE BTMS
Brake Energy Figure 201 (Sheet 2)
K27449
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
05-51-14
ALL ú ú 01 Page 204 ú Sep 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
S 582-002
WARNING: DO NOT GO NEAR THE LANDING GEAR AREA FOR 1 HOUR AFTER THE
_______ AIRPLANE HAS MADE A HIGH ENERGY STOP. INJURY TO PERSONS CAN OCCUR.
(1) Move the airplane away from the runway in use.
(a)
Do not use the brakes very much when the airplane is moved.
(b)
Do not set the parking brake.
S 882-003
(2)
Let the brakes, tires, and wheels cool so you can touch them.
S 212-004
(3)
Examine the tires (Ref 32-45-03).
S 212-005
(4)
Examine the wheels (Ref 32-45-04).
S 212-006
(5)
Examine the brakes (Ref 32-41-10).
(a) Apply the brakes fully five or six times. Monitor the brake operation and look for hydraulic leaks during the last time the brakes were applied.
NOTE:____Make sure the brakes work. Look at the movement of the brake indicator wear pins.
D. High Energy Stop Conditional Inspection - In FUSE PLUG MELT Range
S 582-007
(1) Move the airplane away from the runway in use immediately because the tires will possibly deflate.
(a) Do not set the parking brake.
WARNING: DO NOT GO NEAR THE LANDING GEAR AREA FOR 1 HOUR AFTER THE
_______ AIRPLANE HAS MADE A HIGH ENERGY STOP, UNLESS IT IS NECESSARY. IF IT IS NECESSARY, GO NEAR THE AREA VERY CAREFULLY, BUT ONLY FROM THE FRONT OR REAR OF THE TIRES. DO THIS WHEN ONE OR ALL OF THE TIRES ARE INFLATED. INJURY TO PERSONS CAN OCCUR.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 時間限制/維護檢查(19)
