Part Number
Definition:
THE PORTION OF A ENGINE, GAS TURBINE, NONAIRCRAFT IN WHICH FUEL IS BURNED. IT MAY BE AN ANNULAR TYPE IN WHICH THE SPACE BETWEEN THE CIRCULAR INNER AND OUTER CYLINDERS FORM THE BURNING CHAMBER OR IT MAY BE THE MULTI-ARRANGEMENT CAN TYPE IN WHICH SEPARATE CAN LIKE BURN CYLINDERS ARE POSITIONED IN A CIRCULAR ARRANGEMENT WITHIN AN INNER AND OUTER CASE.
CAGE Information
| Code | Company |
|---|---|
| 77445 | UNITED TECHNOLOGIES CORPORATION DBA |
Federal Supply Class
Title
GAS TURBINES AND JET ENGINES; NO
Inclusions:
INCLUDES AIRFLOW DEFLECTORS; COMBUSTION CHAMBERS, COMPRESSORS, TURBINES, ACCESSORY GEAR BOXES AND THEIR COMPONENTS.
Exclusions:
EXCLUDES COMPONENTS FOR GAS TURBINES AND JET ENGINES, AIRCRAFT PRIME MOVER (FSC 2840); ENGINE FUEL SYSTEMS (FSC 2910); ENGINE ELECTRICAL SYSTEMS (FSC 2920); ENGINE COOLING SYSTEMS (FSC 2930); ENGINE AIR/OIL CLEANERS/FILTERS/STRAINERS (FSC 2940); ENGINE ACCESSORIES (AIR DUCT HEATERS, ENGINE MOUNTED CONTROL ASSEMBLIES) (FSC 2990).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| ABHP | OVERALL LENGTH | 11.980 INCHES MINIMUM AND 12.040 INCHES MAXIMUM |
| ABHP | OVERALL LENGTH | 11.980 INCHES MINIMUM AND 12.040 INCHES MAXIMUM |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CHAMBER-COMBUSTION, 5, ASSEMBLY OF |