| AIRCRAFT LOCATION | AFT FUSELAGE |
| AIRCRAFT MISSION DESIGN SERIES | C-130J |
| HOLE QUANTITY | 2 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5599 ASSN STD SINGLE MATERIAL RESPONSE OR AMS5581 ASSN STD SINGLE MATERIAL RESPONSE |
| III MATERIAL | NICKEL ALLOY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPENSATOR-LOW PRESSURE DUCT |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL LENGTH | 18.000 INCHES NOMINAL |
| SPECIAL FEATURES | INSIDE DIAMETER 3.000 INCHES NOMINAL; OVERALL DIAMETER 6.190 INCHES NOMINAL; OPERATING TEMPERATURE 670.0 DEGREES F; DESIGN OPERATING PRESSURE 50.0 POUNDS PER SQUARE INCH(PSI) AT 670.0 DEGREES F; PROOF PRESSURE 75.0 PSI; BURST PRESSURE 150.0 PSI; CAN WITHSTAND NEGATIVE PRESSURE 13.5 PSI AT ROOM TEMPERATURE; VOLUMETRIC LEAKAGE 0.241 STANDARD CUBIC FEET OF AIR PER MINUTE; FLOW RATE 150.0 POUNDS PER MINUTE; FLOWS IN EITHER DIRECTION; ALLOWABLE CORRECTED PRESSURE DROP 0.250 PSI; OPERATING ALTITUDE 1500.0 FEET TO 42000.0 FEET |