(c)
Wipe the surface of the inner cylinder again with a clean cloth to remove all of the fluid from the leak.
(d)
Monitor the inner cylinder where it meets with the outer cylinder for 15 minutes. 1) Make sure the extension of the inner cylinder does not
change during this time. 2) Make a second record of the number of drops which come from the seals during the 15 minutes. 3) Make a record of the location of the leak.
(e)
Calculate the average of the number of drops which came from the seals from both of the 15 minute measurements.
NOTE: If the average is less than 30 drops during the 15
____ minutes time, the shock strut is serviceable. If the leakage flows continuously from the seals or leakage is greater than 30 drops during the 15 minutes time, then the shock strut is not serviceable.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-02
ALL ú ú 01 Page 218 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 212-117
(5) If the leakage stopped, do the step that follows:
CAUTION: A DEFLATED OR FLAT SHOCK STRUT CAN CAUSE DAMAGE DURING
_______ LANDING. IF THE AIRPLANE LANDED WITH A DEFLATED OR FLAT SHOCK STRUT, DO A HARD LANDING INSPECTION PER AMM 05-51-41/201 TO MAKE SURE THERE IS NO DAMAGE.
(a) Continue to monitor the shock strut for leakage on subsequent landings. If you see more signs of leakage, do the entire leak check procedure again.
S 612-118
(6) If there was leakage between 1 and 15 drops during the 15 minute period, do the steps that follow:
NOTE: 20 drops is equal to 1.0cc.
____
CAUTION: A DEFLATED OR FLAT SHOCK STRUT CAN CAUSE DAMAGE DURING
_______ LANDING. IF THE AIRPLANE LANDED WITH A DEFLATED OR FLAT SHOCK STRUT, DO A HARD LANDING INSPECTION PER AMM 05-51-41/201 TO MAKE SURE THERE IS NO DAMAGE.
(a)
Continue to monitor the shock strut for leakage on subsequent landings. After 10 days service the shock strut with nitrogen and make sure the "X" dimension in the servicing chart is correct (AMM 12-15-03/301).
(b)
After 20 days deflate the shock strut and add oil until it is completely full. Then service the shock strut with nitrogen (AMM 12-15-03/301).
(c)
Do the 10 and 20 day servicing steps again until you change the seals.
S 612-119
(7) If there was leakage between 16 and 30 drops during the 15 minute period, do the steps that follow:
NOTE: 20 drops is equal to 1.0cc.
____
CAUTION: A DEFLATED OR FLAT SHOCK STRUT CAN CAUSE DAMAGE DURING
_______ LANDING. IF THE AIRPLANE LANDED WITH A DEFLATED OR FLAT SHOCK STRUT, DO A HARD LANDING INSPECTION PER AMM 05-51-41/201 TO MAKE SURE THERE IS NO DAMAGE.
(a) Continue to monitor the shock strut for leakage on subsequent landings. After 5 days service the shock strut with nitrogen and make sure the "X" dimension in the servicing chart is correct (AMM 12-15-03/301).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-11-02
ALL ú ú 01 Page 219 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(b)
After 10 days deflate the shock strut and add oil until it is completely full. Then service the shock strut with nitrogen (AMM 12-15-03/301).
(c)
Do the 5 and 10 day servicing steps again until you change the seals.
S 982-120
(8)
If the leakage was more than 30 drops during the 15 minute period, the shock is not serviceable. You must replace the seals.
F.
Put the Airplane back to its Usual Condition.
S 092-080
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：747-400 AMM 飞机维护手册 起落架 LANDING GEAR 1(94)
