(3) Install the DYNAMOMETER - SAFETY STAY (98D07103000000) on the safety stay.
R **ON A/C 001-049, 051-099, 101-149, 201-299,
Subtask 07-11-00-582-053
B. Reaction at the Jacking Points
NOTE : The maximum permitted aircraft weight for the jacking procedure is
____
59000 kg (130072.6980 lb).
(1)
Make sure that you do not apply more than the safe load at each jacking point.
(2)
At the point at FR8:
-the permitted load is 6800 daN (15287.0052 lbf)
(3)
At the points at Ribs 9, left and right wings:
-the permitted load is 28500 daN (64070.5365 lbf)
(4)
At the point between FR73 and FR74:
-the permitted load is 2000 daN (4496.1780 lbf)R **ON A/C 151-199, 401-499,
Subtask 07-11-00-582-053-A
B. Reaction at the Jacking Points NOTE : The maximum permitted aircraft weight for the jacking procedure is
____
57000 kg (125663.4540 lb).
(1)
Make sure that you do not apply more than the safe load at each jacking point.
(2)
At the point at FR8:
-the permitted load is 6800 daN (15287.0052 lbf)
(3)
At the points at Ribs 9, left and right wings:
-the permitted load is 28500 daN (64070.5365 lbf)
(4)
At the point between FR73 and FR74:
-the permitted load is 2000 daN (4496.1780 lbf)
**ON A/C 301-399,
Subtask 07-11-00-582-053-B
B. Reaction at the Jacking Points NOTE : The maximum permitted aircraft weight for the jacking procedure is
____
69000 kg (152118.9180 lb).
(1)
Make sure that you do not apply more than the safe load at each jacking point.
(2)
At the point at FR8:
-the permitted load is 6800 daN (15287.0052 lbf)
(3)
At the points at Ribs 9, left and right wings:
-the permitted load is 33400 daN (75086.1726 lbf)
(4)
At the point between FR73 and FR74:
-the permitted load is 2000 daN (4496.1780 lbf)
R EFF : 151-199, 301-399, 401-499, 07-11-00Page 209 Aug 01/05 CES **ON A/C ALL
TASK 07-11-00-581-001
Lifting for Aircraft Maintenance Operations
WARNING : BEFORE YOU LIFT THE AIRCRAFT WITH JACKS:
_______
-MAKE SURE THAT THE WEIGHT OF FUEL IS APPLIED EQUALLY ON THE TWO SIDES OF THE AIRCRAFT CENTERLINE.
R WARNING : MAKE SURE THAT THE AIRCRAFT IS STABLE:
_______ R - BEFORE YOU PUT IT ON JACKS R - DURING ALL THE TIME IT STAYS ON JACKS.
CAUTION : YOU MUST NOT LIFT THE AIRCRAFT WITH THE SAFETY STAY.
_______
CAUTION : DO NOT USE THE TAIL SAFETY STAY WHEN THE AIRCRAFT IS ON ITS WHEELS.
_______
CAUTION : BEFORE YOU LIFT OR YOU LOWER THE AIRCRAFT MAKE SURE THAT THERE IS NO
_______ EQUIPMENT ADJACENT TO IT (THAT CAN CAUSE DAMAGE). MAKE SURE THAT NO OTHER WORK IS BEING DONE.
CAUTION : REMOVE THE SAFETY STAY BEFORE YOU DO THE LANDING GEAR EXTENSION AND
_______ RETRACTION TESTS. DAMAGE TO THE FUSELAGE CAN OCCUR IF THE AIRCRAFT MOVES DURING THE TESTS.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific hydraulic jacks
No specific safety barriers
No specific safety stay
No specific warning notices
No specific wheel chocks
No specific access platform 2.30 m (7 ft. 7 in.)
No specific access platform 3.55 m (11 ft. 8 in.)
98D07103000000 1 DYNAMOMETER - SAFETY STAY
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
98D07103500000 1 JACK ADAPTER - FUSELAGE 98D07104000000 1 JACKING PAD SET 98D07104000001 1 JACKING PAD SET 98D07104081000 1 JACKING PAD SET
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-57-00-200-001 Aircraft Stability 07-11-00-582-002 Jacking - General 08-21-00-200-001 Quick Leveling Using the Attitude Monitor 32-00-00-481-001 Installation of the Safety Devices on the Landing
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