| Item Name | Angle Structural |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Base Metal |
| National Item Identification Number (NIIN) | 00-145-8435 (001458435) |
| NCB Code | USA (00) |
| Manufacturer | The Boeing Company, Aluminum Co Of America, Society Of Automotive Engineers Inc, Sae International, Boeing Company The, Federal Specifications |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| BAC1504-2563 | the boeing company | angle structural | 82918 | RFQ |
| 13642 | aluminum co of america | angle structural | 01634 | RFQ |
| AMS-QQA200-11 | society of automotive engineers inc | angle structural | 81343 | RFQ |
| AMS QQA200 11 | sae international | angle structural | 0u583 | RFQ |
| 1M314 | boeing company the | angle structural | 76301 | RFQ |
| QQA200-11 | federal specifications | angle structural | 81348 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDEDEXTRUDED |
| ABKW | OVERALL HEIGHT | 0.875 INCHES NOMINAL0.875 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 1.000 INCHES NOMINAL1.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM12.000 FEET MAXIMUM |
| ADXL | LEFT SIDE FLANGE THICKNESS | 0.078 INCHES NOMINAL0.078 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | ANGLEANGLE |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL0.125 INCHES NOMINAL |
| AJGP | BASE FLANGE THICKNESS | 0.078 INCHES NOMINAL0.078 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.190 POUNDS PER LINEAR FOOT0.190 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE ENDSQUARE END |
| CMZZ | SECOND TIP RADIUS | 0.156 INCHES NOMINAL0.156 INCHES NOMINAL |
| CNNZ | SECOND TIP DIAMETER | 0.171 INCHES NOMINAL0.171 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICALNOT IDENTICAL |
| CNQK | SECOND TIP STYLE | UPPER BULBOUSUPPER BULBOUS |
| CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-1 SOLUTION HEAT TREATED AND T-1 SOLUTION HEAT TREATED AND ARTIFICALLY AGEDARTIFICALLY AGED |
| MATT | MATERIAL | ALUMINUM ALLOYALUMINUM ALLOY |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPERT6 TEMPER |
| Relevant Components for NSN - 9540-00-145-8435, 9540001458435 | ||||
| 9515-01-536-3375 (9515015363375) | 9515-00-814-7221 (9515008147221) | 9530-00-237-0734 (9530002370734) | 9540-00-197-9847 (9540001979847) | |
| 9520-01-274-4554 (9520012744554) | 9515-00-061-4892 (9515000614892) | 9530-01-135-8297 (9530011358297) | 9535-01-581-6877 (9535015816877) | |
| 9510-00-541-9207 (9510005419207) | 9540-01-071-2142 (9540010712142) | 9530-00-060-5585 (9530000605585) | 9530-00-233-1340 (9530002331340) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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