DI ENVR 82270 数据项说明(DID)飞机集成系统气候试验报告(2019年5月17日)

ID:44101

大小:0.02 MB

页数:6页

时间:2023-03-17

金币:20

上传者:战必胜
DATA ITEM DESCRIPTION
Title: AIRCRAFT INTEGRATED SYSTEMS CLIMATIC TEST REPORT
Number: DI-ENVR-82270
Approval Date: 20190517
AMSC Number: F10035
Limitation: N/A
DTIC Applicable: No
GIDEP Applicable: No
Preparing Activity: 11 (AFLCMC/EZFS)
Project Number: ENVR-2019-007
Applicable Forms: N/A
Use/Relationship: The Aircraft Integrated Systems Climatic Test Report describes the climatic
testing of a fully equipped, flight-worthy aircraft. The climatic tests assess the effects of climate
on performance, operability, and maintainability of the aircraft and its impacts on aircraft
systems and subsystems, to include: propulsion, auxiliary power, engine power, flight controls,
fuels, environmental control and thermal management, hydraulics, cockpit instruments,
displays and controls, ice protection, airframe, ventilation and drainage, avionics, armament,
vehicle management, ground support equipment, low observable and final finish systems, and
electrical power.
Climatic testing also ascertains the effects of climate on human factors
pertaining to maintenance tasks, pre-flight and post-flight procedures, fueling and defueling,
deicing and anti-icing, loading and off-loading weapons, and rapid reaction procedures (e.g.,
quick aircraft start-up, hot-pit, etc.).
This Data Item Description (DID) contains the format, content, and intended use information for
the data deliverable resulting from the work task described in the solicitation.
Requirements:
1. Reference documents. None.
2. Format. The report shall be in the contractor’s format.
3. Content. The report shall include the following information:
a. All system, subsystem, and interface design-to climatic environment requirements.
b. The specific test objectives.
c. Identification of the test aircraft and a complete description of the aircraft systems and
subsystems tested, including all applicable engineering changes and differences from
the full-rate production configuration.
d. Test requirements, including: required test and
inspection parameters and intervals,
performance requirements, and acceptance or compliance limits (i.e., clear and verifiable
pass-fail criteria) for each aircraft system and subsystems tested and evaluated.
e. Test plans and procedures, including:
(1) A complete identification of test instrumentation, equipment, and facilities including:
(a) Nomenclature.
(b) Model or version number.
(c) Serial number.
(d) Manufacturer.
(e) Calibration status.
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