68A332027-1005 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A332027-1005: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 6061, overall_width: 8.000 INCHES NOMINAL IN, overall_length: 20.000 INCHES NOMINAL IN, special_features: REQUESTEDNAME:CLOSURE,VERTICAL, aircraft_location: VERTICAL STABILIZER,LEADING EDGE, material_thickness: 0.071 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-441-3129, 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

68A332027-1005

NSN: 1560-01-441-3129
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 6061
overall_width	8.000 INCHES NOMINAL IN
overall_length	20.000 INCHES NOMINAL IN
special_features	REQUESTEDNAME:CLOSURE,VERTICAL
aircraft_location	VERTICAL STABILIZER,LEADING EDGE
material_thickness	0.071 INCHES NOMINAL IN
aircraft_mission_design_series	F-15I
material_document_and_classification	QQ-A-250/11,T6 FED SPEC SINGLE MATERIAL RESPONSE
surface_treatment_document_and_classification	ANODIZE PER PS13201 TYPE I CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
NSN	1560-01-441-3129

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: ANODIZE PER PS13201 TYPE I CLASS 1 MFR REF SINGLE TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/11,T6 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.071 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: VERTICAL STABILIZER,LEADING EDGE

•

MATERIAL: ALUMINUM ALLOY 6061

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	ANODIZE PER PS13201 TYPE I CLASS 1 MFR REF SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/11,T6 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	20.000 INCHES NOMINAL IN
OVERALL WIDTH	8.000 INCHES NOMINAL IN
MATERIAL THICKNESS	0.071 INCHES NOMINAL IN
SPECIAL FEATURES	REQUESTEDNAME:CLOSURE,VERTICAL
AIRCRAFT LOCATION	VERTICAL STABILIZER,LEADING EDGE
MATERIAL	ALUMINUM ALLOY 6061
AIRCRAFT MISSION DESIGN SERIES	F-15I

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: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 68A332027-1005?

68A332027-1005 is a PLATE,STRUCTURAL,AIRCRAFT.

What is the NSN for 68A332027-1005?

68A332027-1005 is cataloged in the U.S. Government catalog under NSN 1560-01-441-3129. This indicates validated use in U.S. government and defense supply chains.

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68A332027-1005 — PLATE,STRUCTURAL,AIRCRAFT

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