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74A170728-2002 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

74A170728-2002: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 68.310 INCHES NOMINAL IN, aircraft_location: AFT, LWR SKIN SPLICE, AILERON, material_thickness: 0.190 INCHES NOMINAL IN, aircraft_station_number: XW154.0 TO XW222.2, end_item_identification: F/A-18 HORNET AIRCRAFT. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-394-0141, 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
74A170728-2002
NSN: 1560-01-394-0141
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7075
overall_length68.310 INCHES NOMINAL IN
aircraft_locationAFT, LWR SKIN SPLICE, AILERON
material_thickness0.190 INCHES NOMINAL IN
aircraft_station_numberXW154.0 TO XW222.2
end_item_identificationF/A-18 HORNET AIRCRAFT
side_for_which_designedRIGHT SIDE
aircraft_mission_design_seriesF/A-18
material_document_and_classificationQQ-A-250/24 COND T76 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-394-0141
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 74A170728-2002 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
AIRCRAFT STATION NUMBER: XW154.0 TO XW222.2
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/24 COND T76 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.190 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: AFT, LWR SKIN SPLICE, AILERON
•
MATERIAL: ALUMINUM ALLOY 7075
•
SIDE FOR WHICH DESIGNED: RIGHT SIDE
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERXW154.0 TO XW222.2
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/24 COND T76 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH68.310 INCHES NOMINAL IN
MATERIAL THICKNESS0.190 INCHES NOMINAL IN
AIRCRAFT LOCATIONAFT, LWR SKIN SPLICE, AILERON
END ITEM IDENTIFICATIONF/A-18 HORNET AIRCRAFT
MATERIALALUMINUM ALLOY 7075
SIDE FOR WHICH DESIGNEDRIGHT SIDE
AIRCRAFT MISSION DESIGN SERIESF/A-18
OTHER ITEMS IN FSC 1560 — Airframe Structural Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
1560-00-003-1977 1560-00-003-3257 1560-00-004-4244 1560-00-005-7280 1560-00-006-0576 1560-00-006-6538 1560-00-007-9578 1560-00-009-4192
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 — mutilation
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FREQUENTLY ASKED QUESTIONS
What is 74A170728-2002?
74A170728-2002 is a PLATE,STRUCTURAL,AIRCRAFT.
What is the NSN for 74A170728-2002?
74A170728-2002 is cataloged in the U.S. Government catalog under NSN 1560-01-394-0141. This indicates validated use in U.S. government and defense supply chains.
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