L1804021-019 — RIB,STIFFENER,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

L1804021-019: RIB,STIFFENER,AIRCRAFT.

The RIB,STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 9.250 INCHES NOMINAL IN, overall_length: 36.000 INCHES NOMINAL IN, special_features: -019 OPP -020; RIB--QQ-A-250/12 AL BARE SH ALY 7075-0, aircraft_location: AFT--NO. 1 FLAP, WING PANEL, material_thickness: 0.055 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 1560-01-595-4355, 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

L1804021-019

NSN: 1560-01-595-4355
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_width	9.250 INCHES NOMINAL IN
overall_length	36.000 INCHES NOMINAL IN
special_features	-019 OPP -020; RIB--QQ-A-250/12 AL BARE SH ALY 7075-0
aircraft_location	AFT--NO. 1 FLAP, WING PANEL
material_thickness	0.055 INCHES NOMINAL IN
aircraft_mission_design_series	B1-B ACFT
material_document_and_classification	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	RIB, AFT
NSN	1560-01-595-4355

COMPONENT DIAGRAM

KEY FEATURES

•

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

•

MATERIAL THICKNESS: 0.055 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: AFT--NO. 1 FLAP, WING PANEL

•

MATERIAL: ALUMINUM ALLOY 7075

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	36.000 INCHES NOMINAL IN
OVERALL WIDTH	9.250 INCHES NOMINAL IN
MATERIAL THICKNESS	0.055 INCHES NOMINAL IN
SPECIAL FEATURES	-019 OPP -020; RIB--QQ-A-250/12 AL BARE SH ALY 7075-0
AIRCRAFT LOCATION	AFT--NO. 1 FLAP, WING PANEL
PART NAME ASSIGNED BY CONTROLLING AGENCY	RIB, AFT
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	B1-B ACFT

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)

Ready to buy L1804021-019?

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 L1804021-019?

L1804021-019 is a RIB,STIFFENER,AIRCRAFT.

What is the NSN for L1804021-019?

L1804021-019 is cataloged in the U.S. Government catalog under NSN 1560-01-595-4355. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

L1804021-019 — RIB,STIFFENER,AIRCRAFT

Request a Quote — L1804021-019