| Item Name | Angle Structural |
| INC Code | 37017 |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Metal |
| National Item Identification Number (NIIN) | 00-288-1145 (002881145) |
| NCB Code | USA (00) |
| Manufacturer | Airforce-Navy Aeronautical Design Standard, Alcoa Reynolds Metals Company, American Society For Testing, Boeing Company The, Hiller Aircraft Corporation, Federal Specifications, Lockheed Martin Corporation, Chase Aircraft Co Inc, International Light Metals Corp, Society Of Automotive Engineers Inc |
| Associated Parts Numbers of NSN 9540-00-288-1145 | ||||||
|---|---|---|---|---|---|---|
| Part Number | Manufacturer | Item Name | Cage Code | Type | Status | RFQ |
| AND10133-2004 | airforce-navy aeronautical design standard | angle structural | 99237 | NSN | Avl | RFQ |
| 1822 | alcoa reynolds metals company | angle structural | 77783 | A | A | RFQ |
| ASTM B221 | american society for testing | angle structural | 81346 | F | A | RFQ |
| 1047972 | boeing company the | angle structural | 88277 | A | A | RFQ |
| 110-503062 | hiller aircraft corporation | angle structural | 89446 | A | A | RFQ |
| QQ-A-200/3 | federal specifications | angle structural | 81348 | A | A | RFQ |
| 2-1327 | lockheed martin corporation | angle structural | 38597 | A | A | RFQ |
| CDS148 | chase aircraft co inc | angle structural | 81025 | NSN | Avl | RFQ |
| 12551 1 | international light metals corp | angle structural | 27610 | A | F | RFQ |
| AMS-QQ-A-200 3-T3511-0.250X2X10 | society of automotive engineers inc | angle structural | 81343 | A | R | RFQ |
| AMS-QQ-A-200 3 | society of automotive engineers inc | angle structural | 81343 | A | R | RFQ |
| 1245442 | boeing company the | angle structural | 88277 | A | A | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |
| ADXL | LEFT SIDE FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | ANGLE |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL |
| AJGP | BASE FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| AJJB | FIRST TIP RADIUS | 0.250 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 1.110 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.250 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQK | SECOND TIP STYLE | UPPER RADIUS |
| CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3511 TEMPER |
| Relevant Components for NSN - 9540-00-288-1145, 9540002881145 | ||||
| 9540-01-419-5436 (9540014195436) | 9540-00-355-9508 (9540003559508) | 9540-00-540-5696 (9540005405696) | 9540-01-247-2816 (9540012472816) | |
| 9540-01-316-8247 (9540013168247) | 9540-00-145-8447 (9540001458447) | 9540-01-070-2164 (9540010702164) | 9540-01-276-0089 (9540012760089) | |
| 9540-01-496-2506 (9540014962506) | 9540-00-145-5802 (9540001455802) | 9540-01-276-0956 (9540012760956) | 9540-00-005-6284 (9540000056284) | |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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