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MIL-T-27305 Revision C, December 16, 1987
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TRANSMITTER, RATE OF FLOW
Includes all amendments and changes through Validation Notice 3, February 10, 2015
Additional Comments: INACTIVE FOR NEW DESIGN
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This specification covers the requirements for turbo-jet engine, aircraft rate-of-fuel flow mass transmitters, designated TRUE-31A/A.

Transmitters shall be one of the following types, as specified (see 6.2):
    TRU-31A/A-1        0 to 1,200 pph range
    TRU-31A/A-2        0 to 1,800 pph range
    TRU-31A/A-3        0 to 2,500 pph range
    TRU-31A/A-4        0 to   800 pph range
    TRU-31A/A-5        0 to 4,000 pph range
    TRU-31A/A-6        0 to 5,000 pph range
    TRU-31A/A-7        0 to   400 pph range
    TRU-31A/A-8        0 to 5,000 pph range