Part Details | FLAT PANEL AIRCRAFT PLYWOOD
5530-00-266-4016 A panel composed of an assembly of plies of veneer joined in a hot plate press with a water-resistant thermosetting adhesive. Except for special constructions, the grain of alternate plies is at right angles. The face, back, and inner plies may be of various softwood or hardwood species. This plywood is usually intended for use in the fabrication of structural or highly stressed aircraft parts.
Alternate Parts: 3731535, 373153-5, MILP6070, MIL-P-6070, MILDTL6070, MIL-DTL-6070, 5530-00-266-4016, 00-266-4016, 5530002664016, 002664016
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 55 | JAN 01, 1961 | 00-266-4016 | 34669 ( PLYWOOD, AIRCRAFT, FLAT PANEL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5530-00-266-4016
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 373153-5 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| MIL-P-6070 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-DTL-6070 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5530-00-266-4016
| Characteristic | Specifications |
|---|---|
| TYPICAL WOOD PRODUCTS USE | FABRICATION OF STRUCTURAL OR HIGHLY STRESSED AIRCRAFT PARTS |
| THICKNESS-LOCATION AND MEASURING METHOD | AADSD0.565 INCHES MINIMUM AND AADSD0.615 INCHES MAXIMUM |
| WIDTH-LOCATION AND MEASURING METHOD | DSD48.000 INCHES NOMINAL |
| MEASURING METHOD AND LENGTH | SD6.000 FEET NOMINAL |
| SPECIFICATION/STANDARD DATA | 81349-MIL-P-6070 GOVERNMENT SPECIFICATION |
| NONDEFINITIVE SPEC/STD DATA | 1 GROUP |