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Page Title:
Test Procedures for Aircraft Cabin Pressurizing and Air Conditioning Systems |
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MIL-T-18606(Aer)
31 March l955
MILITARY SPECIFICATION
TEST PROCEDURES FOR AIRCRAFT
CABIN PRESSURIZING AND AIR CONDITIONING SYSTEMS
scope
1.
MILITARY
.
Transparent Area, Anti-Ioing, Defrosting
MIL-T-5842A
and Defogging Systems, General Specification for
PUBLICATIONS
AIR FORCE - NAVY AERONAUTICAL BULLETIN
3.
REQUIREMENTS
3.1 General test equipment and requirements.
3.1.1
Suitable instrumentation shall be installed to determine the weight
flow of air~ the
temperature differential, and the pressure drop throghh each of the
of the systems, The accuracy of these measurements should be within
major components
plus or minus 5
percent.
3.1.2 System performance tests shall be conducted with a minimum of 75 per-
cent of passenger and crew accommodations occupied during cooling tests and a maximum
Of 30 percent of the passonger accommodations occupied during heating tests.
3.1.3 Instrumentation shall be provided to determine the temperature dia-
tribution from forward to rear and top to bottom of all occupied spaces within the air
plane.
3.2.4 Equipment shall be provided to determine the direction of flow and the
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