| 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) | 00-542-2766 (005422766) |
| NCB Code | USA (00) |
| Manufacturer | Aluminum Co Of America, Federal Specifications, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp, Alcoa Reynolds Metals Company |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 853G | aluminum co of america | beam structural | RFQ |
| QQ-A-200/5 | federal specifications | beam structural | RFQ |
| AMS-QQ-A-200 5 | sae international | beam structural | RFQ |
| AMS-QQ-A-200 5 | society of automotive engineers inc | beam structural | RFQ |
| PA14820 | transtar metals corp | beam structural | RFQ |
| 4712 | alcoa reynolds metals company | beam structural | 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 | 0.281 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.281 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.281 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.500 INCHES NOMINAL |
| BQJK | LEFT SIDE TOP FLANGE TIP THICKNESS | 0.250 INCHES NOMINAL |
| BQJM | RIGHT SIDE TOP FLANGE TIP THICKNESS | 0.250 INCHES NOMINAL |
| BQKH | LEG TIP THICKNESS | 0.250 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.890 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 |
| CRYX | LEFT TOP INNER FACE TO OUTER FACE ANGLE | 90.0 DEGREES NOMINAL |
| CSTQ | RIGHT TOP INNER FACE TO OUTER FACE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | H-111 STRAIN HARDENED |
| MATT | MATERIAL | ALUMINUM ALLOY 5086 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/5 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | H111 TEMPER |
| Relevant Components for NSN - 9540-00-542-2766, 9540005422766 | ||||
| 9545-01-709-0704 (9545017090704) | 9545-01-667-3043 (9545016673043) | 9545-01-467-6270 (9545014676270) | 9545-01-465-1537 (9545014651537) | |
| 9545-01-465-1511 (9545014651511) | 9545-01-465-0887 (9545014650887) | 9545-01-419-4042 (9545014194042) | 9545-01-355-8884 (9545013558884) | |
| 9545-01-354-7652 (9545013547652) | 9545-01-351-1477 (9545013511477) | 9545-01-341-4256 (9545013414256) | 9545-01-306-9961 (9545013069961) | |
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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