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MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | B1B |
SR-5 | DESIGN CONTROL REFERENCE | L9604-101-001-1 |
SR-5 | THE MANUFACTURERS DATA | |
FEAT | SPECIAL FEATURES | CONSISTS OF A TEST CONSOLE APPROX108.000 IN. W X 72.000 IN. D X 78.000 IN. H; OPERATOR CONSOLE APPROX 24.000 IN. W X 24.000 D X 65.000 H; REMOTE PWR SUPPLY SKID, APPROX 120.000 W X 72.000 IN. D X 84.000 IN. H; REQUIRES 460 VAC, 200 AMPS, 3 PHASE 60 HZ (NON-HAZARD AREA); 120 VAC, 15 AMPS, 1 PHASE, 60 HZ; PNEUMATIC REQUIREMENTS, PURGE AIR, 3000 SCFM MAXIMUM AT ATMOSPHERIC PRESSURE; EXHAUST AIR, 800 SCMF MAXIMUM , LESS THAN 0.001 IN. WATER RESTRICTION; SHOP AIR, 60 TO 120 PSIG, 20 SCFM MAXIMUMM CONSUMPTION, DEW POINT LESS THAN 40 DEG. F; COOLING WATER, 85 GPM MAXIMUM AT 45 DEG. F |
SR-5 | MANUFACTURERS CODE | 96362 |
FTLD | III FUNCTIONAL DESCRIPTION | THE AIRCRAFT FUEL COMPONETS TEST SYSTEM (AFCTS)(HIGH FLOW) WILL PERFORMANCE TEST AND EVALUATE ACFT. FUEL COMPONETS CHARACTERIZED BY HIGH FLOWS (UP TO 750 GPM) THE AFCTS IS PRIMARILY TO SUPORT TEST AND EVALUATION OF IN-TANK REFUELING AND FUEL TRANSFER COMPONETS WHICH REQUIRE OPEN LOOP OPERATION |
L961463 | L961463 | L961464 | L961465 |
L961465 | L961467 | L961466 | L961463 |
L961468 | L961466 | L961466 | L961465 |
L961463 | L961467 | L961468 | L961465 |
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