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MRC | Criteria | Characteristic |
---|---|---|
AGAV | III END ITEM IDENTIFICATION | F100-PW-100/200 ENGINE (F-15, F-16 ACFT) |
FTLD | III FUNCTIONAL DESCRIPTION | USED TO EVALUATE ALL INPUT SIGNALS AND OUT PUT EFFECTORS ASSOCIATED WITH THE ELECTRONIC FUEL CONTROL |
SR-5 | THE MANUFACTURERS DATA | |
FEAT | SPECIAL FEATURES | TYPE A/E24T-136; TESTER CASE 25.250 IN. L, 19.750 IN. W, 16.500 IN. H, 80 LBS; CABLE CASE WITH CABLES 24.250 IN. L, 24.500 IN. W, 10.000 IN. H, 70 LBS; 115 VOLT, 400 HZ, SINGLE PHASE |
ANPZ | INCLOSURE FEATURE | MULTIPLE ITEM W/CARRYING CASE |
SR-5 | MANUFACTURERS CODE | S7040 |
SR-5 | DESIGN CONTROL REFERENCE | PR8304392-0 |
RDAL | III REFERENCE DATA AND LITERATURE | T.O. 33D4-6-521-4 |
AQXY | TEST TYPE FOR WHICH DESIGNED | ELECTRONIC FUEL CONTROL |
SUPP | III SUPPLEMENTARY FEATURES | COMPANY ITEM NAME-TEST SET AIRCRAFT ENGINE A/E 24T-162 |
PR8388P1 | PR81670 | PR8-001XU | PR816C405PAA |
PR817C165YHC04DW4752 | PR800 | PR816C405PAA | PR8392P5 |
PR8122 | PR800FG-BSG | PR8 L | PR800FG-BSG |
PR800FG-BSG COUNCIL | PR80071 | PR800FG-BSG COUNCIL | PR81670 |
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