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Page Title:
MODIFICATION PROCEDURES: (Cont) |
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  MWO 1- 520-251-20-01
1
10. MODIFICATION PROCEDURES: (Cont)
Install or remove laminated shims (8) (as required) from lower bracket so that slider
(4)
plate will attain a tight fit.
.75 LG machine screws (9) through upper bracket with
Install two
(5)
screw heads on the inside of the bracket.
Install two No. 10, Type A flat washers (10) and two
hex nuts (11) on
(6)
screws and hand tighten.
.75 LG machine screws (12) through lower bracket with
Installtwo
(7)
screw heads on the inside of the bracket.
Install two No. 10, Type A flat washers (13) and two
hex nuts (14)
(8)
on screws and hand tighten.
Torque four nuts to 25 INCH-POUNDS.
(9)
(10) Inspect (QA).
Moment
In
Chart C
No
Items
Weight
Arm
Aircraft
Entry
BRACKET ASSEMBLY,
KEVLAR PANEL
82.2
0.8
1
D
(Date)
M48 BLOWER PLATE
ASSEMBLY
1
143.3
1.4
E
-3503 (Date)
Description
Weight Change
Current Total Basic
of Article or
Added
Removed
I
Aircraft
Modifica-
Arm Moment Weight Arm Moment Weight Moment Index
IN
tion
I
BRACKET
ASSEMBLY
1
82.2
0.8
82.2
0.8
(Date)
PILOT SLID-
ERPLATE
1
143.3
1.4
143.3
(Date)
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