Alternative NSN: 5340-01-254-1470 |
Item Name: Seat Helical Compre |
FSG: 53 Hardware and Abrasives |
Federal Supply Class (FSC): 5340 Hardware Commercial |
NIIN: 012541470 |
NCB Code: USA (01) |
Manufacturers: Boeing Company The |
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Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
68A412739-2001 | Boeing Company The | seat helical compre | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AAWY | COUNTERBORE DIAMETER | 1.7500 INCHES NOMINAL |
ABKW | OVERALL HEIGHT | 0.9000 INCHES NOMINAL |
ABPR | FIRST STEP DIAMETER | 2.6050 INCHES MINIMUM AND 2.6150 INCHES MAXIMUM |
ABPS | FIRST STEP LENGTH | 0.1200 INCHES NOMINAL |
ABXV | BORE DIAMETER | 1.5000 INCHES NOMINAL |
AMFZ | SECOND END DIAMETER | 1.9650 INCHES MINIMUM AND 1.9750 INCHES MAXIMUM |
APGF | DESIGN TYPE | SOLID |
BBRB | END DIAMETER | 1.6850 INCHES MINIMUM AND 1.6950 INCHES MAXIMUM |
BZDH | DISTANCE FROM END TO FIRST STEP | 0.1900 INCHES NOMINAL |
BZDL | COUNTERBORE LENGTH | 0.4000 INCHES NOMINAL |
FEAT | SPECIAL FEATURES | FIRST STEP DIAMETER UNDERCUT AND RELIEVED SHOULDER;BOTH ENDS COUNTERSINK 30.0 DEG |
MATT | MATERIAL | ALUMINUM ALLOY 7075 OR ALUMINUM ALLOY,QQ-A-200/11,T73511 OR T7351 OR T73 OR T7351 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/9, ALLOY 7075, T7351 FED SPEC 1ST MATERIAL RESPONSE |
SFTT | SURFACE TREATMENT | ANODIZE |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | PS15548,MCDONNEL AIRCRAFT CO MFR REF SINGLE TREATMENT RESPONSE |
STYL | STYLE DESIGNATOR | SEAT |
5305-00-000-0094 (5305000000094) |
5305-00-001-1366 (5305000011366) |
5305-00-001-1367 (5305000011367) |
5305-00-001-1568 (5305000011568) |
5305-00-001-1569 (5305000011569) |
5305-00-001-1837 (5305000011837) |
5305-00-001-1918 (5305000011918) |
5305-00-001-1926 (5305000011926) |
5305-00-001-1948 (5305000011948) |
5305-00-001-1963 (5305000011963) |
5305-00-001-2011 (5305000012011) |
5305-00-001-2012 (5305000012012) |
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