68A321566-2002 — FITTING,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

68A321566-2002: FITTING,STRUCTURAL COMPONENT,AIR.

FITTING,STRUCTURAL COMPONENT,AIR. Key specifications include height: 0.910 INCHES NOMINAL IN, material: ALUMINUM ALLOY 2124, overall_width: 1.470 INCHES NOMINAL IN, overall_length: 1.810 INCHES NOMINAL IN, special_features: U/O F-15E CUM210&UP, F-15I CUM10&UP, F-15S CUM37&UP; NHA 68A321307, aircraft_location: STRINGER8. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-476-2152, 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

68A321566-2002

NSN: 1560-01-476-2152
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)

SPECIFICATIONS

height	0.910 INCHES NOMINAL IN
material	ALUMINUM ALLOY 2124
overall_width	1.470 INCHES NOMINAL IN
overall_length	1.810 INCHES NOMINAL IN
special_features	U/O F-15E CUM210&UP, F-15I CUM10&UP, F-15S CUM37&UP; NHA 68A321307
aircraft_location	STRINGER8
surface_treatment	ANODIZE
side_for_which_designed	RIGHT SIDE
aircraft_mission_design_series	F-15
material_document_and_classification	MMS149 PLATE MFR REF SINGLE MATERIAL RESPONSE
surface_treatment_document_and_classification	PS13201TYPE II ASSN STD SINGLE TREATMENT RESPONSE
NSN	1560-01-476-2152

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: PS13201TYPE II ASSN STD SINGLE TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: MMS149 PLATE MFR REF SINGLE MATERIAL RESPONSE

•

HEIGHT: 0.910 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE

•

AIRCRAFT LOCATION: STRINGER8

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	PS13201TYPE II ASSN STD SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	MMS149 PLATE MFR REF SINGLE MATERIAL RESPONSE
OVERALL LENGTH	1.810 INCHES NOMINAL IN
OVERALL WIDTH	1.470 INCHES NOMINAL IN
HEIGHT	0.910 INCHES NOMINAL IN
SPECIAL FEATURES	U/O F-15E CUM210&UP, F-15I CUM10&UP, F-15S CUM37&UP; NHA 68A321307
SURFACE TREATMENT	ANODIZE
AIRCRAFT LOCATION	STRINGER8
MATERIAL	ALUMINUM ALLOY 2124
SIDE FOR WHICH DESIGNED	RIGHT SIDE

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 68A321566-2002?

68A321566-2002 is a FITTING,STRUCTURAL COMPONENT,AIR.

What is the NSN for 68A321566-2002?

68A321566-2002 is cataloged in the U.S. Government catalog under NSN 1560-01-476-2152. This indicates validated use in U.S. government and defense supply chains.

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68A321566-2002 — FITTING,STRUCTURAL COMPONENT,AIR

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