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National Stock Number: 2840-01-448-7035
Federal Supply Class: 2840
National Item Identification Number: 014487035
Description: SEAL,AIR,AIRCRAFT GAS TURBINE EN
Detail: A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an ENGINE, GAS TURBINE, AIRCRAFT. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.
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Manufacturer Information:
2840PL0788966 | 9009H | INSPEKTORAT WSPARCIA SIL ZBROJNYCH | 4083197 | 77445 | RTX CORPORATION | 4083197-01 | 77445 | RTX CORPORATION |
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Techincal Specification:
CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND ABMZ AND FEAT | DESIGN TYPE | AXIAL COMPRESSOR | DIAMETER | 25.004 INCHES MINIMUM AND 25.008 INCHES MAXIMUM | ENGINE SECTION LOCATION | COMBUSTION CHAMBER | OVERALL LENGTH | 0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5599 ASSN STD 1ST MATERIAL RESPONSE OR AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL | MATERIAL | NICKEL ALLOY OVERALL | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL BRUSH,COMBUSTION CHAMBER,OUTER ASSEMBLY | STAGE NUMBER | 1 | SPECIAL FEATURES | T.O. 2J-F100-54, FIG 86, IND 19F; USE ONLY ON P/NS 4083194, 4083560, AND 4083565; CONTAINS WIRE BRUSH, 2250-2650 WIRES PER CIRCUMFERENTIAL INCH; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY; TURBINE STATOR SUPPORT AND COMBUSTION CHAMBER |
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