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|  MIL-D-23222A(AS)
2.1.1
(Cont)
STANDARDS
MIL-STD-250
Aircrew Station Controls and Displays for
Rotary wing Aircraft
MIL-STD-704
Electric Power, Aircraft, Characteristics and
Utilization of
Reliability Evaluation from Demonstration Data
MIL-STD-757
MIL-STD-800
Procedure for Carbon Monoxide Detection and
Control in Aircraft
MIL-STD-850
Aircrew Station Vision Requirements for Military
Aircraft
MIL-STD-877
Antenna Subsystems, Airborne, Criteria for Design
and Location of
MIL-STD-14 (2
Human Engineering Design criteria for Military
Systems Equipment and Facilities
STANDRD DRAWINGS
MS-33575
Dimensions, Basic, Cockpit, Helicopter
(When requesting specifications, refer to both title and number. Copies
of this specification and applicable specification may be obtained upon
application to the Commanding Officer, Naval Publications and Forms
Centers 5801 Tabor Ave., Philadelphia, Pennsylvania, 19120 (Code 56).
2.1.2
PUBLICATIONS. -The following publications of
the issue in effect on date of invitation for bids,
form a part of this specification to the extent specified herein.
NAVAIR Instruction
13100.4
Navy Contract Demonstration Requirements; Admini-
tration of Documentation stemming from and
relating thereto
13100.5
MIL-D-8708, Demonstration Requirements for Air-
planes, and MIL-D-23222, Demonstration
Requirments for Helicopters; the administra-
tion of
l3100.7
Release of Naval Aircraft for Trials and Fleet
Use; Policy Regarding
13900.1A
Special Flight-Test instrumentation of the Naval
Air Test Center; Accountability and handling
procedures for
2.2
OTHER DOCUMENTS. - The following documents form
a part of this specification. Unless otherwise
indicated, the issue in effect on date of invitation forbids shall
apply.
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