 |
|||
|
Page Title:
Valve, Starter Control, Aircraft Engine, for F404 Engine/A6, F-18 Aircraft |
|
||
| ||||||||||
|
|  MIL-V-81995/6(AS)
8 March 1985
MILITARY SPECIFICATION SHEET
VALVE, STARTER CONTROL, AIRCRAFT ENGINE,
FOR F404 ENGINE/A6, F-18 AIRCRAFT
This specification 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 acquiring the starter control valve described
herein shall consist of this specification and the latest issue of
Specification MIL-V-81995.
REQUIREMENTS:
ENVELOPE:
See Figures 1, 2, and 3.
Weight: 7.5 lb maximum including Frequency Sensing Relay (FSR) and
Pneumatic Control Unit (PCU).
ATSCV
- 5.25 lbs max.
FSR
- 1.0 lbs max.
- 1.25 lbs max.
PCU
Aircraft Model: A6, F-18.
Engine Model: F404.
Inlet Air Conditions:
65 psia.
Rated Pressure:
Rated Temperature: 455F.
Maximum Continuous Temperature: 455F.
Intermittent Temperature: 1160F (1 minute max.)
Engine Interbreed Pressure:
Normal inlet pressure - 105 psia
Maximum inlet pressure - 175 psia
Minimum Pressure: 15 psig.
Proof Pressure: 205 psia.
Burst Pressure: 395 psia.
FSC 2995
1 of 16
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals