_______
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.
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.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
98D07103000000 1 DYNAMOMETER - SAFETY STAY
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-991-001 Fig. 201
**ON A/C 001-049, 051-099, 101-149, 201-299,
07-11-00-991-002 Fig. 202 R **ON A/C 151-199, 401-499,
07-11-00-991-002-A Fig. 202A
**ON A/C 301-399,
07-11-00-991-002-B Fig. 202B
**ON A/C ALL
3. Job Set-up
__________
Subtask 07-11-00-860-052
A. Not Applicable
4. Procedure
_________
Subtask 07-11-00-582-050
A. General Informations for Jacking
(Ref. Fig. 201/TASK 07-11-00-991-001)
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 202/TASK 07-11-00-991-002)
Location of Jacking Points
Figure 201/TASK 07-11-00-991-001
EFF : ALL 07-11-00 Page 203
Feb 01/98
CES
Different Heights of the Jacking Points
Figure 202/TASK 07-11-00-991-002
R EFF : 001-049, 051-099, 101-149, 201-299, 07-11-00Page 204 May 01/05 CES
R **ON A/C 151-199, 401-499,
(Ref. Fig. 202A/TASK 07-11-00-991-002-A)
**ON A/C 301-399,
(Ref. Fig. 202B/TASK 07-11-00-991-002-B)
**ON A/C ALL
(1) You must lift the aircraft at three points on the structure with three hydraulic jacks: - one point is under the forward fuselage at FR8,
-the two other points are under the wings at Rib 9. When the aircraft is on jacks, put a safety stay between FR73 and FR74. This prevents any accidental movement of the aircraft.
NOTE : You must not use the safety stay to lift the aircraft.
____
You can lift the aircraft with jacks when the tires and the shock
absorbers are deflated.
You can lift the aircraft at the forward jacking point only, with the
wheels of the main landing gear on the ground.
Different Heights of the Jacking Points Figure 202A/TASK 07-11-00-991-002-A
R EFF : 151-199, 401-499, 07-11-00Page 206 Aug 01/05 CES
R Different Heights of the Jacking Points
R Figure 202B/TASK 07-11-00-991-002-B
R EFF : 301-399, 07-11-00 Page 207
May 01/04
CES
(2) Specifications of the Hydraulic Jacks
-----------------------------------------------------------------| Hydraulic Jack | CAPACITY | CLOSED HEIGHT |EXTENDED HEIGHT| | Data | (MIN) | (MAX) | (MAX) | |----------------|-------------|----------------|---------------| | FWD Jacking | 6800 daN | 1500 mm | 3420 mm | | point | 15287 lbf | 59.05 in | 134.64 in | |----------------|-------------|----------------|---------------| | Wing Jacking | 33400 daN | 2500 mm | 4400 mm | | point | 75086 lbf | 98.42 in | 173.22 in | |----------------|-------------|----------------|---------------| | Safety point | 6000 daN | 2800 mm | 4600 mm | | | 13488 lbf | 110.23 in | 181.49 in | -----------------------------------------------------------------
NOTE : We recommend that each of the hydraulic jacks has load
____ indicator to monitor the load at each jacking point. If the hydraulic jacks have a load indicator, it must have two scales:
-
a scale with graduations in bars (psi),
-
a scale with graduations in daN (lbf).
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