|
|
|
National Stock Number:
1560-01-568-1092
Federal Supply Class:
1560
National Item Identification Number:
015681092
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:
| L3226402-012 | 43999 | THE BOEING COMPANY |
|
Techincal Specification:
| AIRCRAFT LOCATION | FWD NACELLE DUCT VANE | | AIRCRAFT MISSION DESIGN SERIES | B-1B ACFT | | AIRCRAFT STATION NUMBER | YN99.75 TO YN143.00 | | OVERALL LENGTH | 38.900 INCHES NOMINAL | | OVERALL WIDTH | 7.600 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL ASSY | | SPECIAL FEATURES | N/A L3226401; U/O 1 AND SUB; -11 OPPOSITE; T3; CORE IS BIAS WEAVE GLASS REINFORCED PHENOLIC; C/O ALLOY SH, CORE, CHANNELS, CLEIPS, RIVETS, PLUGS |
|
|