7008-32-000-4044 — FITTING,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

7008-32-000-4044: FITTING,STRUCTURAL COMPONENT,AIR.

FITTING,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 12.625 INCHES NOMINAL IN, overall_length: 13.940 INCHES NOMINAL IN, special_features: ALTERNATE MATERIAL AL7075 PER QQ-A-250/12,T651; U/O MH-60G 57 AND UP; NEXT HIGHER ASSY 70083-20004-012 G, aircraft_location: LOWER COCKPIT PROBE SUPPORT, material_thickness: 0.370 INCHES MINIMUM AND 0.380 INCHES MAXIMUM IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-433-5630, 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

7008-32-000-4044

NSN: 1560-01-433-5630
FSC: 1560 — Airframe Structural Components
CAGE: 78286 — SIKORSKY AIRCRAFT CORPORATION DBA SIKORSKY AIRCRAFT CORP (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	12.625 INCHES NOMINAL IN
overall_length	13.940 INCHES NOMINAL IN
special_features	ALTERNATE MATERIAL AL7075 PER QQ-A-250/12,T651; U/O MH-60G 57 AND UP; NEXT HIGHER ASSY 70083-20004-012 G
aircraft_location	LOWER COCKPIT PROBE SUPPORT
material_thickness	0.370 INCHES MINIMUM AND 0.380 INCHES MAXIMUM IN
aircraft_station_number	COCKPIT STA205
aircraft_mission_design_series	MH-60G G
material_document_and_classification	QQ-A-250/12,T7351 FED SPEC SINGLE MATERIAL RESPONSE
NSN	1560-01-433-5630

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: COCKPIT STA205

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/12,T7351 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.370 INCHES MINIMUM AND 0.380 INCHES MAXIMUM IN

•

AIRCRAFT LOCATION: LOWER COCKPIT PROBE SUPPORT

•

MATERIAL: ALUMINUM ALLOY 7075

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	COCKPIT STA205
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/12,T7351 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	13.940 INCHES NOMINAL IN
OVERALL WIDTH	12.625 INCHES NOMINAL IN
MATERIAL THICKNESS	0.370 INCHES MINIMUM AND 0.380 INCHES MAXIMUM IN
SPECIAL FEATURES	ALTERNATE MATERIAL AL7075 PER QQ-A-250/12,T651; U/O MH-60G 57 AND UP; NEXT HIGHER ASSY 70083-20004-012 G
AIRCRAFT LOCATION	LOWER COCKPIT PROBE SUPPORT
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	MH-60G G

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 7008-32-000-4044?

7008-32-000-4044 is a FITTING,STRUCTURAL COMPONENT,AIR.

What is the NSN for 7008-32-000-4044?

7008-32-000-4044 is cataloged in the U.S. Government catalog under NSN 1560-01-433-5630. This indicates validated use in U.S. government and defense supply chains.

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7008-32-000-4044 — FITTING,STRUCTURAL COMPONENT,AIR

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