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1560-01-498-5643

Aircraft Stiffener Rib

1560014985643 014985643 5HL88160-108

A vertical, relatively short, rib located in a fuselage, nacelle, pod, and the like. It follows the periphery and provides additional rigidity. It may join various components such as stringers, longerons, and the like. It is supplementary to the frames and blukheads. See also RIB (1), AIRFOIL. View more Aircraft Stiffener Rib

1560-01-498-5643 RIB,STIFFENER,AIRCRAFT 1560014985643 014985643

Managed by United States
NSN Created on 29 Jun 2002
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
1560-01-498-5643 RIB,STIFFENER,AIRCRAFT 1560014985643 014985643 1/1
NSN 1560-01-498-5643 (Generic Image) 1/1

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5HL88160-108 A vertical, relatively short, rib located in a fuselage, nacelle, pod, and the like.
United States (US) 4. 1560-01-498-5643 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-498-5643 Demil Restrictions 1560-01-498-5643

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: P | PMIC: A | EDC: A | ADPEC: 0

1560-01-498-5643 is a Aircraft Stiffener Rib that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.

1560-01-498-5643 HTS and ScheduleB Import and Export 1560-01-498-5643

1560-01-498-5643 End Users End Users 1560-01-498-5643

US Air Force (FLL5)
Effective Date:
1 Jun 2002

1560-01-498-5643 Manufacturers Approved Sources 1560-01-498-5643

1560-01-498-5643 Technical Data Datasheet 1560-01-498-5643

Characteristic
Specifications
FIIG
A11400
Material [MATT]
Titanium Alloy
Overall Length [ABHP]
27.000 Inches Nominal
Overall Width [ABMK]
6.000 Inches Nominal
End Item Identification [AGAV]
F-22 Raptor
Part Name Assigned By Controlling Agency [CXCY]
Fitting Assy-Aft Mlg Uplock

1560-01-498-5643 Management Data Management Data 1560-01-498-5643

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Dec 2011
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
FR
F-22 AIRCRAFT
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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1560-01-498-5643 Freight Data Freight Information 1560-01-498-5643

1560-01-498-5643 has freight characteristics.. 1560-01-498-5643 has a variance between NMFC and UFC when transported by rail and the description should be consulted.