| 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) | 00-145-8413 (001458413) |
| NCB Code | USA (00) |
| Manufacturer | Federal Specifications, Boeing Company The, Sae International, Society Of Automotive Engineers Inc, Aluminum Co Of America |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| QQ-A-200/3 | federal specifications | angle structural | 81348 | RFQ |
| 1E65 | boeing company the | angle structural | 43999 | RFQ |
| AMS-QQ-A-200 3 | sae international | angle structural | 0u583 | RFQ |
| AMS-QQ-A-200 3 | society of automotive engineers inc | angle structural | 81343 | RFQ |
| 24768 | aluminum co of america | angle structural | 01634 | RFQ |
| QQ-A-267 | federal specifications | angle structural | 81348 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDEDEXTRUDED |
| ABKW | OVERALL HEIGHT | 0.750 INCHES NOMINAL0.750 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 | 0.125 INCHES NOMINAL0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | ANGLEANGLE |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.063 INCHES NOMINAL0.063 INCHES NOMINAL |
| AJGP | BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL0.125 INCHES NOMINAL |
| AJJB | FIRST TIP RADIUS | 0.063 INCHES NOMINAL0.063 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.242 POUNDS PER LINEAR FOOT0.242 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | RIGHT QUARTER RADIUSRIGHT QUARTER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.063 INCHES NOMINAL0.063 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICALNOT IDENTICAL |
| CNQK | SECOND TIP STYLE | UPPER RADIUSUPPER RADIUS |
| CQHP | LEFT INSIDE ANGLE | 97.0 DEGREES NOMINAL97.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-4 SOLUTION HEAT TREATEDT-4 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSEQQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T4 TEMPERT4 TEMPER |
| Relevant Components for NSN - 9540-00-145-8413, 9540001458413 | ||||
| 9540-01-448-3440 (9540014483440) | 9515-00-529-0433 (9515005290433) | 9510-00-950-0977 (9510009500977) | 9535-00-529-7803 (9535005297803) | |
| 9515-01-191-8796 (9515011918796) | 9535-01-471-1102 (9535014711102) | 9530-00-228-9322 (9530002289322) | 9515-01-483-6859 (9515014836859) | |
| 9510-00-229-4784 (9510002294784) | 9515-00-071-1190 (9515000711190) | 9540-01-471-8194 (9540014718194) | 9535-00-596-2076 (9535005962076) | |
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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