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Page Title:
Starter, Air Turbine, Accessory Drive Combination, Aircraft Engine, Model ATS/AD-3 |
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|  MIL-S-22518 /3(AS)
19 March 1982
MILITARY SPECIFICATION SHEET
STARTER, AIR TURBINE, ACCESSORY DRIVE COMBINATION,
AIRCRAFT ENGINE, MODEL ATS/AD-3
This specification sheet is approved for use by 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 complete requirements for procuring the starter described
herein shall consist of this document and the latest issue of
Specification MIL-S-22518(AS).
REQUIREMENTS
Applicable paragraphs
of MIL-S-22518A(AS)
3.8.1
Envelope:
Figure 1
Wt, Max (Lb); 33
3.7
4.5.19
Aircraft Model: EA-6B
4.5.20
Engine Model: J52
3.8.2.1
Accessory Drive:
Engine: Figure 1
pad "B": Figure 1
3.5.5
Rotation Viewed from Pad "B" End:
Pad "A": Clockwise
3.9.1
Pad "B": Counterclockwise
Ambient Temperature Operating Range (F):
3.3.2
Starter: -65 to +160
Accessory Drive: -65 to +250
3.3.2
Exposure Temperature Range
-100 to +275
3.3.2.2
Control Valve:
3.5.7
Opening Rate, Max:
22 psig per second
pressure rate for
first 0.5 second;
full open in 3 to 5 seconds
Closing Rate, Max: 0.5 second
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