9767112-101 — BRACKET,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9767112-101: BRACKET,STRUCTURAL COMPONENT,AIR.

BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.800 INCHES NOMINAL IN, overall_length: 3.300 INCHES NOMINAL IN, special_features: DIM. ARE STOCK MATERIAL.

FOR 2024 CLAD ALUMINUM CHEMCICAL CONVERSON COAT PER MIL-C-5541 CLASS 1A A, aircraft_location: FAIRING-FLAP, surface_treatment: ANODIZE AND DICHROMATE. This part is cataloged in the U.S. Government catalog under NSN 1560-01-571-9604, 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

9767112-101

NSN: 1560-01-571-9604
FSC: 1560 — Airframe Structural Components
CAGE: 51563 — ROHR, INC. DBA ROHR INDUSTRIES INC DIV ROHR INC., A PART OF COLLINS AEROSPACE (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	2.800 INCHES NOMINAL IN
overall_length	3.300 INCHES NOMINAL IN
special_features	DIM. ARE STOCK MATERIAL. FOR 2024 CLAD ALUMINUM CHEMCICAL CONVERSON COAT PER MIL-C-5541 CLASS 1A A
aircraft_location	FAIRING-FLAP
surface_treatment	ANODIZE AND DICHROMATE
material_thickness	0.063 INCHES NOMINAL IN
aircraft_mission_design_series	F-15
material_document_and_classification	QQ-A250/4 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-A-250/5 CLAD FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	BRACKET ASSEMBLY
surface_treatment_document_and_classification	MIL-A-8625 TYPE II CLASS 1 MIL SPEC SINGLE TREATMENT RESPONSE
NSN	1560-01-571-9604

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: MIL-A-8625 TYPE II CLASS 1 MIL SPEC SINGLE TREATMENT RESPONSE

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A250/4 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-A-250/5 CLAD FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.063 INCHES NOMINAL IN

•

SURFACE TREATMENT: ANODIZE AND DICHROMATE

•

AIRCRAFT LOCATION: FAIRING-FLAP

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	MIL-A-8625 TYPE II CLASS 1 MIL SPEC SINGLE TREATMENT RESPONSE
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A250/4 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-A-250/5 CLAD FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	3.300 INCHES NOMINAL IN
OVERALL WIDTH	2.800 INCHES NOMINAL IN
MATERIAL THICKNESS	0.063 INCHES NOMINAL IN
SPECIAL FEATURES	DIM. ARE STOCK MATERIAL. FOR 2024 CLAD ALUMINUM CHEMCICAL CONVERSON COAT PER MIL-C-5541 CLASS 1A A
SURFACE TREATMENT	ANODIZE AND DICHROMATE
AIRCRAFT LOCATION	FAIRING-FLAP
PART NAME ASSIGNED BY CONTROLLING AGENCY	BRACKET ASSEMBLY
MATERIAL	ALUMINUM ALLOY 2024

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

Ready to buy 9767112-101?

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 9767112-101?

9767112-101 is a BRACKET,STRUCTURAL COMPONENT,AIR.

What is the NSN for 9767112-101?

9767112-101 is cataloged in the U.S. Government catalog under NSN 1560-01-571-9604. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

9767112-101 — BRACKET,STRUCTURAL COMPONENT,AIR

Request a Quote — 9767112-101