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68A250550-2007 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

68A250550-2007: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 10.270 INCHES NOMINAL IN, aircraft_location: PYLON ASSEMBLY - FORWARD OUTBOARD, STA6, CFT, material_thickness: 0.125 INCHES NOMINAL IN, aircraft_station_number: STA6.000, end_item_identification: F-15 AIRCRAFT. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-445-5946, 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
68A250550-2007
NSN: 1560-01-445-5946
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7075
overall_length10.270 INCHES NOMINAL IN
aircraft_locationPYLON ASSEMBLY - FORWARD OUTBOARD, STA6, CFT
material_thickness0.125 INCHES NOMINAL IN
aircraft_station_numberSTA6.000
end_item_identificationF-15 AIRCRAFT
aircraft_mission_design_seriesF-15
material_document_and_classificationQQ-A-250/25 COND-T76 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-445-5946
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 68A250550-2007 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
AIRCRAFT STATION NUMBER: STA6.000
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/25 COND-T76 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.125 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: PYLON ASSEMBLY - FORWARD OUTBOARD, STA6, CFT
•
MATERIAL: ALUMINUM ALLOY 7075
•
AIRCRAFT MISSION DESIGN SERIES: F-15
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERSTA6.000
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/25 COND-T76 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH10.270 INCHES NOMINAL IN
MATERIAL THICKNESS0.125 INCHES NOMINAL IN
AIRCRAFT LOCATIONPYLON ASSEMBLY - FORWARD OUTBOARD, STA6, CFT
END ITEM IDENTIFICATIONF-15 AIRCRAFT
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: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 68A250550-2007?
68A250550-2007 is a PLATE,STRUCTURAL,AIRCRAFT.
What is the NSN for 68A250550-2007?
68A250550-2007 is cataloged in the U.S. Government catalog under NSN 1560-01-445-5946. This indicates validated use in U.S. government and defense supply chains.
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