Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER DUCT
2840-00-022-9492 A cylindrical shaped item or a segment thereof designed to direct air into or around a CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. The internal iar is divided and directed to the burning chamber(s). The external air is used for cooling purposes.
Alternate Parts: 586899, 586899, 2840-00-022-9492, 00-022-9492, 2840000229492, 000229492
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 27, 1967 | 00-022-9492 | 52524 ( DUCT, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-022-9492
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 586899 | 85291 | B. H. AIRCRAFT COMPANY, INC. |
| 586899 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-022-9492
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 3.651 INCHES MINIMUM AND 3.671 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF-30 |