Catalog item
Request a quoteBEAM,STRUCTURAL
9540FSC
01NCB code
430-5412Item number
NIIN 01-430-5412
- Unit price
- $83.05
- Unit of issue
- FT
- Source of supply
- F59
- DEMIL code
- A
Identification
- Item name code
- 37018
- PINC
- 0037018
- Criticality code
- X
- II
- 0
- DEMIL code
- A
- NIIN assigned
- 01-MAY-96
- Precious metals indicator
- A
- ADP equipment code
- 0
- Hazardous material indicator
- N
Management
| Effective date | Major organizational entity | Acquisition advice code | Source of supply | Unit of issue | Unit of measure quantity | Unit price | Quantity per unit pack | Controlled inventory item code | Shelf-life code | Recoverability code | Management control | Net price | USC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 01-APR-2009 | DF | J | F59 | FT | 0.0000 | $83.05 | 0 | U | 0 | N | --SBQ-E | $0.00 | F |
| 01-APR-2009 | DF | J | F59 | FT | 0.0000 | $83.05 | 0 | U | 0 | N | --SBQ-E | $0.00 | I |
Part numbers
| Part number | CAGE | CAGE status | RNCC | RNVC | Document availability code | RNAAC | RNSC |
|---|---|---|---|---|---|---|---|
| CVC10030-12CJ | 80378 TRIUMPH AEROSTRUCTURES, LLC DBA TRIUMPH AEROSTRUCTURES - VOUGHT INTEGRATED PROGRAMS DIVISION | A | 3 | 2 | E | ZZ | |
| AMS-QQ-A-200/15 | 81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC | R | 5 | 9 | E | ZZ | B |
| QQ-A-200/15 | 81348 FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | A | 5 | 9 | E | ZZ | B |
| AMS-QQ-A-200/15 | 0U583 SAE INTERNATIONAL DBA SAE INTERNATIONAL | A | 3 | 1 | E | ZZ |
Characteristics
| FABRICATION METHOD | EXTRUDED |
|---|---|
| OVERALL WIDTH | INCHES NOMINAL 2.500 |
| LENGTH | FEET NOMINAL 12.000 |
| LEFT SIDE FLANGE HEIGHT | INCHES NOMINAL 2.000 |
| RIGHT SIDE FLANGE HEIGHT | INCHES NOMINAL 2.250 |
| LEFT SIDE FLANGE THICKNESS | INCHES NOMINAL 0.125 |
| RIGHT SIDE FLANGE THICKNESS | INCHES NOMINAL 0.125 |
| END ITEM IDENTIFICATION | B-2 BOMBER |
| BASIC SHAPE STYLE | |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 1.008 |
| LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 0.992 |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 1.128 |
| RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 1.122 |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.125 |
| FILLET RADIUS WHERE BOTTOM LEFT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.125 |
| FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.125 |
| FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.125 |
| WEB FLANGE THICKNESS | INCHES NOMINAL 0.125 |
| FIRST TIP STYLE | |
| FIRST TIP INNER RADIUS | INCHES NOMINAL 0.020 |
| FIRST TIP OUTER RADIUS | INCHES NOMINAL 0.020 |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| RIGHT TOP INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| LEFT TOP INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| LEFT BOTTOM INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| RIGHT BOTTOM INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED |
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE QQ-A-200 TO 15 |
| NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER T76511 |
MOE rules
- MOE rule
- FNN5
- MOE CD
- DF
- AMC
- 0
- AMSC
- 0
- Date assigned
- 01-JUN-03
- IMC
- B
- PICA
- TN
- PICA LOA
- 06
- Auth collab
- TN TU
- Fmr MOE rl
- FGKZ
Service data
Air Force
- Budget
- S
- MMAC
- BQ
- PVC
- E
- ERRC
- N
Freight
- ACTY CD
- KH
Related items
Standardization
- Item standardization code
- 5
- Orig stdzn dec
- 97
- Dt stdzn dec
- 01-MAY-1996
- NIIN status code
- 0
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