Part identity
01-0109-020
Sheet Metal
Lockheed Martin Corp Div Lockheed Martin Aeronautics Company
Avg quote: 14 minFulfilled from Anaheim, CAAS9120:2025 · ISO 9001 · FAA AC 00-56BC of C, lot & date code with every line
Part description
Sheet Metal
ASAP supports this specific part for replacement, spare-pool replenishment, retrofit, and urgent maintenance requirements. Quote requests can include alternate MPN, condition preferences, certification needs, and plant-specific receiving instructions so procurement gets a clear sourcing response before purchase.
Specifications
Certifications & documentation
- UL Recognized
- CE
- C of C available on request
LM
Manufacturer
Lockheed Martin Corp Div Lockheed Martin Aeronautics Company
Authorized-distributor or qualified-aftermarket source. Parts shipped from this manufacturer include full traceability paperwork and counterfeit-mitigation per SAE AS6081.
View manufacturer profile →NSN Information for Part Number 01-0109-020 with NSN 9535-01-353-5541, 9535013535541
Characteristics Data of NSN 9535-01-353-5541, 9535013535541
| MRC | Criteria | Characteristic |
|---|---|---|
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
| AGXW | PHYSICAL FORM | FLAT STOCK |
| AQQR | EDGE TYPE | SHEARED |
| AARN | FABRICATION METHOD | ROLLED |
| CQHQ | MINIMUM YIELD STRENGTH | 14000 POUNDS PER SQUARE INCH |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T0 TEMPER |
| ABRY | LENGTH | 12.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 INCHES NOMINAL |
| CQBC | MINIMUM TENSILE STRENGTH | 32000 POUNDS PER SQUARE INCH |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/4 ASSN STD SINGLE MATERIAL RESPONSE |