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Page Title:
Operating Limits for Contractor's Pilots |
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| MIL-D-23222A(AS)
(Cont)
3.1.5
(4) Flying in normal attitude is authorized with the
following Imitations:
Normal load factors greater than 1.5 and less
(a)
than 0.5 shall not be exceeded. The take-off
gross weight shall not exceed 105% of the
Basic Design Gross Weight.
An angle of bank of 30 shall not be exceeded.
(b)
Flight controls, power-plant controls, and
(c)
other systems, innovations, and/or appur-
tenances shall not be rewed or operated so
as to result in rapid or abrupt helicopter
responses.
(d) The speed in any direction at any altitude
(d)
shall not exceed 0.8 times the maximum speed
attainable at the Basic Design Gross Weight
in sustained level flight at that altitude
with normal-rated power or thrust, or the
guaranteed cruise speed, whichever is greater.
After this initial authorization for release for flight has been granted,
the NAVPRO shall release helicopters for operation to more critical
limits at the contractor's plant* only after the NAVPRO has determined
that all contractual prerequisites to such releases have been either
complied with or waived by NAVAIR, and after NAVAIR has authorized
such releases. Requests by contractors for release for first flight,
for release for operation to more critical limits at the contractor's
plant, and for release for tests at locations other than at the con-
tractor's plant, shall summarize the status of all contractual pre-
requisites to the requested release unless the required status-of-
completion information is contained in the Demonstration, Planning,
and Progress Report submitted to NAVAIR; in which case the contractor's
requests shall refer to sources of the necessary information.
OPERATING LIMITS FOR CONTRACTOR'S PILOTS. -
3.1.5.1
The operating limits for contractors' flights
shall not be more critical than any of the following:
(1) Those authorized by NAVAIR.
(2) Those authorized by the NAVPRO.
*and for tests at locations other than at the contractor' S plant,
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