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National Stock Number: 2840-01-160-6505
Federal Supply Class: 2840
National Item Identification Number: 011606505
Description: HUB,COMPRESSOR,AIRCRAFT GAS TURB
Detail: A COMPONENT OF A ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO ATTACH TO THE FRONT AND/OR REAR OF THE ROTOR PROVIDING SUPPORT, ALIGNMENT, AND A MEANS OF ATTACHMENT FOR A SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT MAY HAVE PROVISIONS FOR INSTALLING BEARINGS, AND/OR OIL AND AIR SEALS. SEE ALSO DISK AND HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
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Manufacturer Information:
466009 | 77445 | RTX CORPORATION | 530080 | 77445 | RTX CORPORATION | 698998 | 77445 | RTX CORPORATION | 698999 | 77445 | RTX CORPORATION | 699006 | 3JVG3 | HANWHA AEROSPACE USA LLC | 699006 | 50381 | MTU AERO ENGINE COMPONENTS INC | 699006 | 77445 | RTX CORPORATION | 699008 | 77445 | RTX CORPORATION | 822621 | 77445 | RTX CORPORATION | 822635 | 77445 | RTX CORPORATION | 822636 | 77445 | RTX CORPORATION |
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Techincal Specification:
CRITICALITY CODE JUSTIFICATION | AGAV | DIAMETER | 18.802 INCHES MINIMUM AND 18.806 INCHES MAXIMUM | ENGINE SECTION LOCATION | COMPRESSOR | OVERALL LENGTH | 16.485 INCHES MINIMUM AND 16.505 INCHES MAXIMUM | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | MATERIAL | NICKEL ALLOY OVERALL | SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
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