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MRC | Criteria | Characteristic |
---|---|---|
SUPP | III SUPPLEMENTARY FEATURES | INPUT POWER FOR TEST SET SUPPLIED BY NSN 6230-00-752-2082, GASEOUS NITROGEN WILL BE PROVIDED BY NSN 3655-01-038-5125, THE TEST UNIT WILL INCORPORATE A LOW PRESSURE SYSTEM DESIGNED TO ACCEPT AIR PRESSURES UP TO 150 PSIG AND REGULATE THE OUTPUT PRESSURE IN THE RANGE OF 0 TO 75 PSIG WHILE MEASURING THE FLOW RATE OVER 0.1 SCFM (O TO 75 PSIG). THE TEST MEDIUM AIR (AIR/GN2) SHALL BE DRY AND FILTERED THROUGH A NOMINAL 200 MICRON FILTER |
AKWC | ELECTRICAL POWER SOURCE RELATIONSHIP | OPERATING |
FEAT | SPECIAL FEATURES | MFG NAME TEST SET, LINE OBSTRUCTION FLOW AND LEAK, C/O CONSOLE ASSY 1; CABLE ASSY 1; FLEXIBLE HOSE ASSY 3; QUICK DISCONNECT, SOCKET 1; QUICK DISCONNECT, PLUG 1; REDUCER 1; ID PLATE 1; ID TAG 3; SLEEVE 3 |
ANPZ | INCLOSURE FEATURE | SINGLE ITEM W/HOUSING |
ACYN | AC VOLTAGE RATING | 120.0 VOLTS NOMINAL |
ABGL | WIDTH | 42.000 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | B-1B AIRCRAFT AGE, B-1B FUEL SYSTEM AND ENVIRONMENTAL CONTROL SYSTEM |
ACZB | FREQUENCY RATING | 60.0 HERTZ NOMINAL |
FTLD | III FUNCTIONAL DESCRIPTION | TEST SET IS USED TO PERFORM CONFIDENCE LEAK CHECK ON THE ENVIRONMENTAL CONTROL SYSTEM(ECS) TO VERIFY THAT THE LEAKAGE FROM THE PNEUMATIC COMPONENTS, DUCTING OR LINES ARE WITHIN ALLOWABLE LIMITS; TO TEST FUNCTIONAL STATUS OF BACKUP PRESSURE REGULATORS AND SHUTOFF VALVES AND TO TEST FOR PRESSURE LEAK AND LINE OBSTRUCTION OF THE FUEL SYSTEM AND THE NITROGEN PRESSURE SYSTEM |
FAAZ | PHASE | SINGLE |
HGTH | HEIGHT | 60.000 INCHES NOMINAL |
RDAL | III REFERENCE DATA AND LITERATURE | SERD41A37C |
AQXY | TEST TYPE FOR WHICH DESIGNED | USED TO PERFORM PNEUMATIC LEAK TESTING OF ECS AND FUEL SYSTEMS ON THE B-1B AIRCRAFT |
AQXZ | OPERATING TEST CAPABILITY | PRESSURE GAGES RANGE 0 TO 200 PSIG; FLOWMETER RANGE 0.06 TO 126 SCFM |
ABRY | LENGTH | 66.000 INCHES NOMINAL |
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