Techincal Specification:
| FUNCTIONAL DESCRIPTION | USED TO PRESSURE TEST AIRCRAFT FUEL TANKS WITH HELIUM. RECOMMENDED FOR USE ON THE FOLLOWING FUEL SYSTEMS, F4,F5, F15, F16, F18, F22, F35, A10, C130, P3 AND OTHER SMALL AIRFRAMES AND/OR SYSTEMS. ALL OTHERS SEE NSN 6635-01-517-0575. AIRCRAFT SPECIFIC TOOL KITS MUST BE ACQUIRED FROM AIRCRAFT SYSTEM PROGRAM OFFICES (SPO), FOR FULL EQUIPMENT FUNCTIONALITY | | OVERALL HEIGHT | 12.000 INCHES NOMINAL | | OVERALL LENGTH | 31.500 INCHES NOMINAL | | OVERALL WIDTH | 21.000 INCHES NOMINAL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | PORTABLE MFLD FILLING/INJECTION CASE | | REFERENCE DATA AND LITERATURE | AEROWING DOC TECH 073 | | RELATIONSHIP TO SIMILAR EQUIPMENT | SAME AS 5180-14-542-4696 | | SPECIAL FEATURES | INCLUDES POWER CORD, HELIUM REGULATOR, GROUND WIRE, COMPRESSED AIR CONNECTOR, FILLING HOSE CONNECTION, MEASUREING LINE CONNECTION HOSES, SAFETY INTERFACES, PURGING HOSE, INJECTION NOZZLE, INJECTION HOSE, GAS BOTTLE STRAP, CPL CONNECTOR. REQUIRES DRY DEGREASED COMPRESSED AIR AT MAX 120PSI AND COMPRESSED HELIUM BOTTLE |
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