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Page Title:
Starter, Aircraft Engine, Hydraulic, For T64 Engine |
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|  MIL-S-22999/2A(AS)
6 June 1986
SUPERSEDING
MIL-S-22999/2(AS)
15 June 1981
MILITARY SPECIFICATION SHEET
STARTER, AIRCRAFT ENGINE, HYDRAULIC, FOR T64 ENGINE
This specification is approved for use within the Naval Air
Systems Command, Department of the Navy, and is available
for use by all Departments and Agencies of the Department
of Defense.
The requirements for acquiring the starter described herein shall consist of
this specification and the latest issue of MIL-S-22999.
REQUIREMENTS:
Figures 1 and 2
Envelope:
Wt, max dry (lb): 20.0
Model CH-53
Aircraft:
Model T64
Engine:
Meet requirements of MS14118(AS)
Quick-attach-detach
mounting:
Engine accessory drive: The starter shall be suitable for mounting on an
AND20002, Type II-S drive, except that the stud location shall be changed to
position two studs on the vertical center line.
Rotation viewed from anti-output shaft end: Clockwise
Ports:
Conform to: Inlet - AND1OO5O-10; Outlet - MS33649-12
Ambient temperature operating range ("F): -65 to +275
Exposure temperature range ("F): -103 to +275
Overspeed limit, min peak no-load speed (rpm): 8000
Inlet pressure at zero fluid flow, max (psig): 4400
Rated inlet pressure (psig):
3750 +50, -0
Rated outlet pressure (psig): 5O +15, -O
lof6
FSC 299
Approved for public release; distribution is unlimited
DISTRIBUTION STATEMENT A.
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