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1420-01-118-2701
Airframe Structural Panel
1420011182701 011182701 232-31555-4
A preformed item which may be any shape, having a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose any portion of the fuselage or to fabricate partitions or compartments within a wing, empennage, fuselage or nacelle. It may have holes drilled or cut to accommodate items, but will have no items mounted on it, except bracket(s) or other facilities for its own mounting or support. It may be mounted by fasteners, bonding, or welding. Excludes COVER, ACCESS; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL; COVER, ACCESS, GUIDED MISSILE; PANEL, STRUCTURAL, AIRCRAFT. View more Airframe Structural Panel
January 2023
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Related Documents 1420-01-118-2701 1+ Documents (More...)
RQST NE Updated Every Day 1420-01-118-2701 RQST Updated Every Day 1420-01-118-2701 RQST NE Restrictions
1420-01-118-2701 DEMIL: A | DEMILI : | CRITICALITY : X | HMIC : N | PMIC : A | EDC: A | ADPEC : 0 1420
Restrictions 1420-01-118-2701
1420-01-118-2701 is a Airframe Structural Panel that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1420-01-118-2701
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1420-01-118-2701
- MOE Rule:
- WN01
- Effective Date:
- 1 Dec 1998
Approved Sources 1420-01-118-2701
- Part Number
- Manufacturer
- Status
- 232-31555-4
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1420-01-118-2701
- Characteristic
- Specifications
- FIIG
- Specifications
- A23900
- End Item Identification [AGAV]
- Agm-86B Missile
- General Characteristics Item Description [TEXT]
- Consists Of 1 Side Panel Rh P/N 232-31074-8; 1 Plate Assy Rh P/N 232-31556-2
- Functional Description [FTLD]
- Right Hand Installation
- Reference Data And Literature [RDAL]
- T.O.21M-Agm86-4-1 Fig 2-22
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Freight Information 1420-01-118-2701
1420-01-118-2701 has freight characteristics.. 1420-01-118-2701 has a variance between NMFC and UFC when transported by rail and the description should be consulted.