| 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) | 00-727-8537 (007278537) |
| NCB Code | USA (00) |
| Manufacturer | Alcoa Reynolds Metals Company, Aluminum Co Of America, American Society For Testing, Hiller Aircraft Corporation, Federal Specifications, Cessna Aircraft Company, Hughes Missile Systems Co, General Dynamics Corporation, Reynolds Metals Co, International Light Metals Corp, Society Of Automotive Engineers Inc, Transtar Metals Corp, Tracor Flight Systems Inc, The Boeing Company |
| Associated Parts Numbers of NSN 9540-00-727-8537 | ||||||
|---|---|---|---|---|---|---|
| Part Number | Manufacturer | Item Name | Cage Code | Type | Status | RFQ |
| 4091 | alcoa reynolds metals company | angle structural | 77783 | A | A | RFQ |
| 22385 | aluminum co of america | angle structural | 01634 | A | Y | RFQ |
| 22885 | aluminum co of america | angle structural | 01634 | A | Y | RFQ |
| ASTM B221 | american society for testing | angle structural | 81346 | F | A | RFQ |
| FS10101-1008-1 | hiller aircraft corporation | angle structural | 89446 | A | A | RFQ |
| QQA200-2 | federal specifications | angle structural | 81348 | A | A | RFQ |
| S107 | cessna aircraft company | angle structural | 71379 | A | A | RFQ |
| E121108 | hughes missile systems co | angle structural | 14170 | A | R | RFQ |
| S179 | cessna aircraft company | angle structural | 71379 | A | A | RFQ |
| E121108 | general dynamics corporation | angle structural | 0wlu1 | A | F | RFQ |
| 4091 | reynolds metals co | angle structural | 01484 | A | H | RFQ |
| 15751 | international light metals corp | angle structural | 27610 | A | F | RFQ |
| AMS-QQ-A-200 2 ALLOY 2014 TMPR T | society of automotive engineers inc | angle structural | 81343 | A | R | RFQ |
| 60-138 | transtar metals corp | angle structural | 29321 | A | A | RFQ |
| PA4064 | transtar metals corp | angle structural | 06012 | F | F | RFQ |
| E121108 | tracor flight systems inc | angle structural | 7b709 | A | R | RFQ |
| AMS-STD-184 | society of automotive engineers inc | angle structural | 81343 | A | R | RFQ |
| PA4065 | transtar metals corp | angle structural | 06012 | F | F | RFQ |
| BAC1503 1511 | the boeing company | angle structural | 81205 | A | A | RFQ |
| AMS QQ A 200 2 | society of automotive engineers inc | angle structural | 81343 | A | R | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 0.750 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| AGTA | BASIC SHAPE STYLE | ANGLE |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.062 INCHES NOMINAL |
| AJJB | FIRST TIP RADIUS | 0.031 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.130 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.031 INCHES NOMINAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T4 TEMPER |
| ABMK | OVERALL WIDTH | 1.000 INCHES NOMINAL |
| ADXL | LEFT SIDE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| AJGP | BASE FLANGE THICKNESS | 0.062 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-4 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2014 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/2 FED SPEC SINGLE MATERIAL RESPONSE |
| Relevant Components for NSN - 9540-00-727-8537, 9540007278537 | ||||
| 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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