|
|
|
National Stock Number:
1560-01-449-6570
Federal Supply Class:
1560
National Item Identification Number:
014496570
Description:
PANEL,STRUCTURAL,AIRCRAFT
Detail:
A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. It may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. It may be mounted by means of fasteners, bonding or welding. Excludes PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL.
|
Manufacturer Information:
| L3223760-077 | 43999 | THE BOEING COMPANY |
|
Techincal Specification:
| AIRCRAFT MISSION DESIGN SERIES | B-1B | | OVERALL LENGTH | 15.700 INCHES NOMINAL | | OVERALL WIDTH | 8.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED | | SPECIAL FEATURES | NUCLEAR HARDNESS CRITICAL ITEM; MANUFACTURER SUGGESTED NAME-PANEL, WEDGE, PIVOTING-UNDERWING FARING; NHA -001 ASSY; HEAT TREAT TO COND T62 PER ST0111LA0009; FINISH 11AB02; MATL: AL CLAD SH; 0 TEMPER; OPPOSITE -078 | | THICKNESS | 0.063 INCHES NOMINAL |
|
|