| 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) | 01-086-7557 (010867557) |
| NCB Code | USA (01) |
| Manufacturer | Federal Specifications, Sae International, Airforce-Navy Aeronautical Design Standard, Society Of Automotive Engineers Inc, Lockheed Martin Corporation |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| QQ-A-200/8 | federal specifications | beam structural | 81348 | RFQ |
| AMS QQ A 200 8 | sae international | beam structural | 0u583 | RFQ |
| AND10138-1305 | airforce-navy aeronautical design standard | beam structural | 99237 | RFQ |
| AMS QQ A 200 8 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| K50B114T6511 | lockheed martin corporation | beam structural | 81755 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.375 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
| AJJB | FIRST TIP RADIUS | 0.078 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.250 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 1.250 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.353 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.078 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQK | SECOND TIP STYLE | UPPER RADIUS |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/8,ALLOY 6061 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER |
| Relevant Components for NSN - 9540-01-086-7557, 9540010867557 | ||||
| 9535-00-225-6717 (9535002256717) | 9540-01-009-7327 (9540010097327) | 9520-00-961-8960 (9520009618960) | 9510-00-226-4458 (9510002264458) | |
| 9540-01-037-7606 (9540010377606) | 9505-00-963-5236 (9505009635236) | 9530-00-060-4869 (9530000604869) | 9540-01-446-7172 (9540014467172) | |
| 9540-01-593-6916 (9540015936916) | 9520-01-613-3613 (9520016133613) | 9510-00-528-7541 (9510005287541) | 9535-00-950-5251 (9535009505251) | |
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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