Part Number
Definition:
A CONTINUOUS COMBUSTION TYPE ENGINE. CONSISTS PRIMARILY OF A COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE; CHAMBER, COMBUSTION, NONAIRCRAFT GAS TURBINE ENGINE AND A TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. IT MAY HAVE A FAN SECTION. AIR IS COMPRESSED AND HEATED BY A COMBUSTIBLE FUEL AND EXPANDED THROUGH THE TURBINE. IT IS DESIGNED TO FURNISH A SOURCE OF ROTARY SHAFT AND/OR PNEUMATIC POWER. THE PNEUMATIC POWER IS OBTAINED BY A BLEEDOFF OF THE ENGINE COMPRESSOR. FOR A COMPLETE OPERATING POWER UNIT, MOUNTED ON A BASE, SEE POWER UNIT, GAS TURBINE ENGINE.
CAGE Information
| Code | Company |
|---|---|
| 99193 | HONEYWELL INTERNATIONAL INC. DBA HON |
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 |
|---|---|---|
| ABKW | OVERALL HEIGHT | 17.700 INCHES MINIMUM AND 18.700 INCHES MAXIMUM |
| FUEL | FUEL TYPE | JET FUEL |
| ABMK | OVERALL WIDTH | 25.500 INCHES MINIMUM AND 26.500 INCHES MAXIMUM |
| AAXX | MOUNTING TYPE | AIRCRAFT |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | II TYPE |
| FEAT | SPECIAL FEATURES | CURRENT TYPE:DC; FURNISHED ITEMS:GEARBOX ASSEMBLY, PERMANENT MAGNETIC GENERATOR, OIL PUMP ASSEMBLY, FUEL CONTROL, PNEUMATIC TURBINE STARTER; INCLOSURE:NOT INCLUDED; AIR FLOW RATE:302.1 LBS PER MINUTE; DISCHARGE PRESSURE RATING:65.77 PSI; VOLTS IN VOLTAGE:22.0 LOWEST 29.0 HIGHEST; NUCLEAR HARDNESS CRITICAL ITEM |
| ZZZK | SPECIFICATION/STANDARD DATA | 81349-MIL-P-8686 GOVERNMENT SPECIFICATION |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ENGINE ASSEMBLY |
| RDAL | REFERENCE DATA AND LITERATURE | AF TO. 1B-2A-4-49 |
| AXKD | POWER OUTPUT FOR WHICH DESIGNED | PNEUMATIC |
| AGAV | END ITEM IDENTIFICATION | B-2 AIRCRAFT |
| TEST | TEST DATA DOCUMENT | 1W025-DAA3243+003G SPECIFICATION |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| ABHP | OVERALL LENGTH | 45.460 INCHES MINIMUM AND 46.460 INCHES MAXIMUM |