The SUPPORT,SHOCK STRUT,HELICOPTER is a the manufacturer industrial component. Key specifications include end_item_identification: 1520-01-035-0266, general_characteristics_item_description: CUP-SHAPED,7 HOLES 0.250 IN. OD,CENTER APETURE 0.750 IN.
OD,PART OF MAIN LANDING GEAR IN. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 9515-00-027-0656, indicating validated use in U.S. government and defense logistics supply chains.
Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.
| end_item_identification | 1520-01-035-0266 |
| general_characteristics_item_description | CUP-SHAPED,7 HOLES 0.250 IN. OD,CENTER APETURE 0.750 IN. OD,PART OF MAIN LANDING GEAR IN |
| NSN | 9515-00-027-0656 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-18729 MIL SPEC 1ST MATERIAL RESPONSE |
| WIDTH | 36.000 INCHES NOMINAL IN |
| BASIC SHAPE STYLE | SOLID |
| SURFACE CONDITION | DESCALED OVERALL |
| LENGTH | 6.000 FEET NOMINAL FT |
| HEAT TREATMENT | ANNEALED |
| MINIMUM YIELD STRENGTH | 75000 POUNDS PER SQUARE INCH LBS |
| CROSS-SECTIONAL THICKNESS | 0.063 INCHES NOMINAL IN |
| NONDEFINITIVE SPEC/STD DATA | A CONDITION |
| MINIMUM TENSILE STRENGTH | 95000 POUNDS PER SQUARE INCH LBS |