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Page Title:
Final Assembly, Control C-8441 and C-8442 /AWW-4 (V) (DWG. 126AS1OO) |
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|  MIL-F-81966( AS)
TABLE 3. (CONT'D)
FINAL ASSEMBLY , CONTROL C-8441 and C-8442 /AWW-4 (V) (DWG. 126AS1OO) (Cont'd)
c.
Item 11 is to clear B
by 0.010 inch (Ref. Dwg. 126AS1OO)
106.
107.
Dimensions and weight must be as specified (Ref. Dwg. 126AS104)
108.
Aircraft power requirements and control must be as specified
(Ref. Dwg. 126AS104)
Voltage marking on edge of panel must be as specified (Ref. Dwg. 126AS104)
109.
Illuminated knob pointer dimensions and testing shall be as specified
110.
(Ref. Dwg. 126AS111)
111.
Identification plate dimensions and requirements shall be as specified
(Ref. Dwg. 126AS111)
112.
Control cover assembly dimensions and requirements shall be as specified
(Ref. Dwg. 126AS114)
Mounting plate assembly dimensions and requirements shall be as specified
113.
(Ref. Dwg. 126AS115)
Connector plate dimensions and requirements shall be as specified
114.
-
(Ref. Dwg. 126AS118)
Illuminating panel dimensions and requirements must be as specified
115.
(Ref. Dwg. 126AS120)
D.
FINAL ASSEMBLY, ADAPTER, MOUNT MX-8557 and MX-8558/AWW-4(V)
(DWG. 67A21D1-1 and 67A21D1-2)
CRITICAL - None
MAJOR -
AQL 1.0 percent cumulative for all parameters
101.
Wiring and soldering of electrical connections must be as specified
(Ref. Dwgs, 67A21D6, 67A21D7, 67A21C8, 67A21D2)
102.
Adapter shall mate with Power Supply PP-6419/AWW-4(V)
(Ref. Dwgs. 67A21D4, 67A27E1O, 67A27E11, 125AS104)
103.
Mounting plate dimensions shall be-as specified (Ref. Dwg. 67A21D4)
104.
Connector Bracket dimensions shall be as specified
(Ref. Dwgs. 67A21C5, 67A21C15)
Identification plate dimensions and requirements shall be as specified
105.
(Ref. Dwg. 67A21C9)
.
28
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