ADS-27A-SP, AERONAUTICAL DESIGN STANDARD STANDARD PRACTICE: REQUIREMENTS FOR ROTORCRAFT VIBRATION SPECIFICATIONS, MODELING, AND TESTING (02 MAY 2006)
ADS-27A-SP, AERONAUTICAL DESIGN STANDARD STANDARD PRACTICE: REQUIREMENTS FOR ROTORCRAFT VIBRATION SPECIFICATIONS, MODELING, AND TESTING (02 MAY 2006). This standard practice presents the vibration related
requirements for the development and qualification of rotorcraft, rotor craft subsystems, and equipment to be installed on rotorcraft, including external stores. Gunfire induced vibration qualification, when appropriate, should be in accordance with the vibration tests of MIL-STD-810. The development process follows the engineering System Specification (system procurement) or
Production Specification (item procurement). Prior to a Request
for Proposal (REP) release, the Government defines its
engineering specification based on MIL-STD-961. Competing
contractors base their proposed engineering specification on the
Government specification, their interpretation of the
specification and the peculiarities of their proposed hardware.
The contractual engineering specification is negotiated based on
cost, technology, and specification considerations between
contractors and Government prior to contract award. The companion
document to the engineering specification is the Airworthiness
Qualification Specification (AQS) which describes the analysis
and testing required at each step of the development process to
show that the contractor's design will be able to meet the intent
of the engineering systems specification. The AQS is negotiated
in concert with the engineering specification and should reflect
state-of-the-art design, analysis, and testing techniques.
Equipment to be developed and qualified requires different
development and qualification strategies depending on the
complexity of the system or item and trade-offs between
development costs, production costs, rotorcraft weight penalties
associated with over-design and performance and reliability
penalties associated with under-design.