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National Stock Number:
1560-01-506-8630
Federal Supply Class:
1560
National Item Identification Number:
015068630
Description:
TIP,AIRCRAFT
Detail:
A chordwise sectional unit at the outer end of a wing, stabilizer, rotor blade or other airfoil for fixed and rotary wing aircraft.
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Manufacturer Information:
| L2100204-015 | 06DM5 | INFINITY FABRICATION, INC. | | L2100204-015 | 0BT76 | PRO-FAB, LLC | | L2100204-015 | 0C7H8 | D-J ENGINEERING INC | | L2100204-015 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | L2100204-015 | 14248 | HARLOW AEROSTRUCTURES, LLC | | L2100204-015 | 1P642 | VOLUMATIC INC | | L2100204-015 | 29957 | NORDAM GROUP LLC, THE | | L2100204-015 | 2V045 | MALONES CNC MACHINING INC | | L2100204-015 | 34336 | TECT HYPERVELOCITY, INC. | | L2100204-015 | 3L665 | C. E. MACHINE CO., INC. | | L2100204-015 | 43999 | THE BOEING COMPANY | | L2100204-015 | 59213 | AERO COMPONENTS, LLC |
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Techincal Specification:
| AIRCRAFT MISSION DESIGN SERIES | B-1B | | AIRCRAFT LOCATION | TIP, HORIZONTAL STABILIZER | | CRITICALITY CODE JUSTIFICATION | FEAT | | OVERALL LENGTH | 84.000 INCHES NOMINAL | | OVERALL WIDTH | 2.000 INCHES NOMINAL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | LEADING EDGE FACE SHEET | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5, T-62 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.020 INCHES NOMINAL | | MATERIAL | ALUMINUM ALLOY 2024 | | SPECIAL FEATURES | U/0 B-1B; DIMS ARE STOCK MATERIAL; MATERIAL IS AL CLAD SHEET, HEAT TREATR TO T-62 PER ST0111LA0009, FINISH 09 PRIOR TO BONDING |
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