PartsTable
Technical Data Sheet
Download PDF

68A250667-2004 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

68A250667-2004: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 12.700 INCHES NOMINAL IN, overall_length: 15.800 INCHES NOMINAL IN, special_features: P/O -1004 COVER-ACCESS,UPR SKIN;CFT, aircraft_location: COVER, material_thickness: 0.100 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-294-9702, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS
68A250667-2004
NSN: 1560-01-294-9702
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7075
overall_width12.700 INCHES NOMINAL IN
overall_length15.800 INCHES NOMINAL IN
special_featuresP/O -1004 COVER-ACCESS,UPR SKIN;CFT
aircraft_locationCOVER
material_thickness0.100 INCHES NOMINAL IN
aircraft_station_numberFSA509.500 TO FS626.900
aircraft_mission_design_seriesF-15
material_document_and_classificationQQ-A-250/24-T76 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-294-9702
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 68A250667-2004 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
AIRCRAFT STATION NUMBER: FSA509.500 TO FS626.900
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/24-T76 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.100 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: COVER
•
MATERIAL: ALUMINUM ALLOY 7075
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERFSA509.500 TO FS626.900
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/24-T76 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH15.800 INCHES NOMINAL IN
OVERALL WIDTH12.700 INCHES NOMINAL IN
MATERIAL THICKNESS0.100 INCHES NOMINAL IN
SPECIAL FEATURESP/O -1004 COVER-ACCESS,UPR SKIN;CFT
AIRCRAFT LOCATIONCOVER
MATERIALALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIESF-15
OTHER ITEMS IN FSC 1560 — Airframe Structural Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
1560-00-000-0047 1560-00-001-1849 1560-00-001-1850 1560-00-001-1851 1560-00-001-2368 1560-00-001-2478 1560-00-001-2479 1560-00-001-2480
SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — mutilation + specific procedure
Ready to buy 68A250667-2004?
Compare prices from verified sellers on eBay
Buy on eBay →
As an eBay Partner, PartsTable may earn a commission. Your price is not affected.
FREQUENTLY ASKED QUESTIONS
What is 68A250667-2004?
68A250667-2004 is a PLATE,STRUCTURAL,AIRCRAFT.
What is the NSN for 68A250667-2004?
68A250667-2004 is cataloged in the U.S. Government catalog under NSN 1560-01-294-9702. This indicates validated use in U.S. government and defense supply chains.
Community Feedback
Leave a Comment
Comments are reviewed before appearing. You will receive an email to verify before your comment appears.

Request a Quote — 68A250667-2004