| Item Name | Beam 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) | 00-106-0503 (001060503) |
| NCB Code | USA (00) |
| Manufacturer | Federal Specifications, Boeing Company The, Sae International, Society Of Automotive Engineers Inc |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| QQ-A-200/13 | federal specifications | beam structural | 81348 | RFQ |
| 1M5599 | boeing company the | beam structural | 76301 | RFQ |
| AMS QQ A 200 13 | sae international | beam structural | 0u583 | RFQ |
| 32-05339-203 | boeing company the | beam structural | 76301 | RFQ |
| AMS-QQ-A-200 13 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.000 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.000 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 4.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.415 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY 7178 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/13 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZK | SPECIFICATION/STANDARD DATA | 76301-1-5599 MANUFACTURERS STANDARD |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |
| Relevant Components for NSN - 9540-00-106-0503, 9540001060503 | ||||
| 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) | |
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