MIL H 5440G (修正1) 飞机液压系统的设计和安装要求 (1979年9月14日) [由Sae as5修正)

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时间:2023-03-23

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上传者:战必胜
MIL-H-5440G
AM8NDf4SNT1
14 September 1979
0“
MILITARY SPECIFICATION
SYDNAULJC SYSTEMS, AIRCRAFT, ‘titWSI AND II,
DSSIGN AND
INSTALLATIONREQUIREMENTS FOR
This amendment fo& a p&,’ of MilitarySpeoifiaationMIL-H-5U10G,
dated
28 November 1975, and is approvedfor use by all
Department
and Agencies of the Department of Defense
PAGE 3
2.1, under SPECIFICATIONS,
Military,delete:
‘MIL-C-8956 Clampa,Loop,Tube Supportn.
Add after MIL-F-83300:
“141L-C-85052
Clamp, Loep, Cushion, General Speoification for
#lIL-C-85052/1
ClamP, LOOP,
Tube, 17-7PH CRSS, 2750F, Fuel
Resistant. General FurDose
ilIL-C-85052/3
Clamp, Lo&p, Tube, 17-+PH CRBS, 5000F, General
Purposen.
PAGE 4
2.1 under STANDARDS, Military, delete:
WS21 105
Clamp, Loop Cushioned, Wedge, Fluid Resistant,
5000F, CRES, Type III, Claa9 B“.
PAGE
31
3.11 ,28.8 line 2, delete:
%52 1105 (NIL-C-8956, Type
III, Claas B)n and substitute:
WIL-C-85052 (MIL-C-85052/1 or MIL-C-85052/3 to be compatible with
temperature
nvironmant)”.
PAGE 32
3.11.28.9, add:
ltnwr~~e clamps shall not be used to support hydraullo tubing by adjaoent
runs of hydraulic tubing.
Where required, marriage olampa may be used to
maintain olearanoes between tubing runs.
Fsc 1650
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