Catalog item
Request a quoteBEAM,STRUCTURAL
9540FSC
01NCB code
435-9666Item number
NIIN 01-435-9666
- Unit price
- $16.05
- 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
- 07-SEP-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 | $16.05 | 0 | U | 0 | N | --SBQ-E | $0.00 | F |
| 01-APR-2009 | DF | J | F59 | FT | 0.0000 | $16.05 | 0 | U | 0 | N | --SBQ-E | $0.00 | I |
Part numbers
| Part number | CAGE | CAGE status | RNCC | RNVC | Document availability code | RNAAC | RNSC |
|---|---|---|---|---|---|---|---|
| AMS-QQ-A-200/11 | 81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC | R | 5 | 9 | E | ZZ | B |
| CVC10050-111CA | 80378 TRIUMPH AEROSTRUCTURES, LLC DBA TRIUMPH AEROSTRUCTURES - VOUGHT INTEGRATED PROGRAMS DIVISION | A | 3 | 2 | E | ZZ | |
| QQ-A-200/11 | 81348 FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | A | 5 | 9 | E | ZZ | B |
| AMS-QQ-A-200/11 | 0U583 SAE INTERNATIONAL DBA SAE INTERNATIONAL | A | 3 | 1 | E | ZZ | |
| CVC10050-111CAX144 | 14153 DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA | A | 5 | 2 | 5 | ZZ |
Characteristics
| FABRICATION METHOD | EXTRUDED |
|---|---|
| OVERALL HEIGHT | INCHES NOMINAL 2.190 |
| LENGTH | FEET NOMINAL 12.000 |
| LEFT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.125 |
| BASIC SHAPE STYLE | |
| RIGHT SIDE BOTTOM FLANGE THICKNESS | INCHES NOMINAL 0.125 |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.090 |
| FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.090 |
| WEB FLANGE THICKNESS | INCHES NOMINAL 0.125 |
| TOP FLANGE WIDTH | INCHES NOMINAL 0.750 |
| BOTTOM FLANGE WIDTH | INCHES NOMINAL 1.310 |
| FIRST TIP STYLE | |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| LEFT TOP INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| RIGHT BOTTOM INSIDE ANGLE | DEGREES NOMINAL 84.0 |
| HEAT TREATMENT | O-ANNEALED |
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE QQ-A-200 TO 11 |
| NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
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
- 07-SEP-1996
- NIIN status code
- 0
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