-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-004B USA MIL-L-25567 TYPE I
OXYGEN LEAK DETECTOR (Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-581-001 Lifting for Aircraft Maintenance Operations 12-12-32-611-008 Hydraulic Replenishment of the MLG Two-Stage Shock
Absorber 32-11-13-000-001 Removal of the MLG Shock Absorber 32-11-13-000-003 Removal of the MLG Shock-Absorber Gland-Seals 32-11-13-400-001 Installation of the MLG Shock Absorber 32-11-13-400-003 Installation of the MLG Shock-Absorber Gland-Seals
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
12-14-32-991-019 Fig. 304
**ON A/C 301-399,
12-14-32-991-019-A Fig. 304A
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------**ON A/C ALL
12-14-32-991-020 Fig. 305
12-14-32-991-004 Fig. 306
12-14-32-991-021 Fig. 307
**ON A/C 001-003, 051-052,
12-14-32-991-005 Fig. 308 R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 401-499,
12-14-32-991-005-A Fig. 308A
**ON A/C 301-399,
12-14-32-991-005-B Fig. 308B
**ON A/C 001-003, 051-052,
12-14-32-991-025 Fig. 309 R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 401-499,
12-14-32-991-025-A Fig. 309A
**ON A/C 301-399,
12-14-32-991-025-B Fig. 309B
**ON A/C 001-003, 051-052,
12-14-32-991-027 Fig. 310 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 401-499,
12-14-32-991-027-B Fig. 310A
**ON A/C 301-399,
12-14-32-991-027-A Fig. 310B
**ON A/C ALL
3. Job Set-up
__________
Subtask 12-14-32-941-064
A. Safety Precautions
(1)
Make sure that the ground safety locks are installed on the landing gear.
(2)
Put the safety barriers in position.
(3)
On panel 400VU:
-make sure that the landing-gear control-lever 6GA is in the DOWN position.
(4)
Put a warning notice in position to tell persons not to operate:
-
the landing gear controls
-
the landing gear doors.
(5)
Put an access platform in position below the applicable shock absorber.
(6)
If the aircraft is on the ground, make sure that the wheel chocks are in position at the MLG wheels. Do not put a chock at the nosewheels.
R 1EFF : ALL 1 12-14-32Page 324 1 1 Aug 01/05 1 1 1CES 1
4. Procedure
_________
Subtask 12-14-32-210-054
A. Visual Inspection of the MLG Two-Stage Shock Absorber for Leakage of Hydraulic Fluid
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 304/TASK 12-14-32-991-019)
**ON A/C 301-399,
(Ref. Fig. 304A/TASK 12-14-32-991-019-A)
**ON A/C ALL
(Ref. Fig. 305/TASK 12-14-32-991-020)
(1)
Before you do the check and/or charge the nitrogen:
-examine the gland housing/sliding tube of the shock absorber for damage or leakage of hydraulic fluid.
(2)
If there is a leak from the gland housing and the sliding tube interface or from the gland housing and the main fitting interface:
(a) Examine the sliding tube for damage: 1 If there is damage, replace the shock absorber (Ref. TASK 32-
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