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| MIL-D-23222A(AS)
3.4.2.5
RELIABILITY AND MAINTAINABILITY. - The tests of
3.17 shall have been completed.
REQUIREMENTS PRIOR TO FIRST DELIVERIES TO OPERATIONAL
3.5
TEST AND EVALUATION FORCE (OPTEVFOR), FLEET INTRO-
DUCTION PROGRAM (FIP), AND/OR REPLACEMENT AIR GROUPS (RCVG).
3.5.1
FLIGHT MANUALS. - The contractor shall have submitted
satisfactory Flight Manuals in accordance with Spec
MIL-M-7700, containing complete descriptions of flight characteristics.
3.5.2
DYNAMIC COMPONENTS. - The contractor shall have
submitted sufficient data to permit NAVAIR to
assign retirement lives for all dynamic components of at least 1000
hours or as specified in the contract design data and test requirements
of the applicable addendum to MIL-D-8706.
3.6
REQUIREMENTS PRIOR TO CONTINUED FLEET DELIVERIES. -
The requirements of 3.4 and 3.5 shall have been
completed, and all demonstration tests which are a part of this
specification or the addendum thereto shall be completed and the
reports thereof submitted.
STRUCTURAL DEMONSTRATION
3*7
GENERAL. - The structural demonstration consists
3.7.1
of all tests and data obtained during the "duration
of the demonstration" defined in 1.3 which are structurally significant
in defining the strength, rigidity, and operating restrictions for
the helicopter. The formal structural demonstration tests to be per-
formed at NAVAIRTESTCEN shall consist of the tests of paragraphs 3.7.3
and 3.7.4.
GRADUAL APPROACH TO CRITICAL LIMITS. - All of the
3.7.1.1
combinations of gross weight, configuration, center-
of-gravity position, altitude, speed, load factor, and control motions
required to be demonstrated during the tests of 3.7.3 shall be attained
by the contractor at or near the contractor's plant prior to release
of the helicopter for the corresponding tests at NAVIRTESTCEN. During
these flights, critical limits shall be approached gradually in in-
crements as approved by the cognizant test authority.
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