Catalog item
Request a quoteBEAM,STRUCTURAL
9540FSC
01NCB code
353-5562Item number
NIIN 01-353-5562
- DEMIL code
- A
Identification
- Item name code
- 37018
- PINC
- 0037018
- Criticality code
- X
- II
- 0
- DEMIL code
- A
- NIIN assigned
- 12-FEB-92
- Precious metals indicator
- A
- ADP equipment code
- 0
- Hazardous material indicator
- N
- Last known source of supply
- S9I
Part numbers
| Part number | CAGE | CAGE status | RNCC | RNVC | Document availability code | RNAAC | RNSC |
|---|---|---|---|---|---|---|---|
| 60-6404 | 29321 TRANSTAR METALS CORP | A | 3 | 1 | E | KZ | |
| 4E-817 | 43999 THE BOEING COMPANY DIV LEGACY AM&M | A | 3 | 1 | 5 | KZ | |
| AMS-QQ-A-200/3 | 81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC | R | 5 | 9 | E | ZZ | B |
| QQ-A-200/3 | 81348 FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | A | 5 | 9 | E | KZ | B |
| AMS-QQ-A-200/3 | 0U583 SAE INTERNATIONAL DBA SAE INTERNATIONAL | A | 3 | 1 | E | ZZ |
Characteristics
| FABRICATION METHOD | EXTRUDED |
|---|---|
| OVERALL HEIGHT | INCHES NOMINAL 5.000 |
| LENGTH | FEET MINIMUM 10.000 AND FEET MAXIMUM 12.000 |
| LEFT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.150 |
| RIGHT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.150 |
| BASIC SHAPE STYLE | |
| LEG THICKNESS | INCHES NOMINAL 0.150 |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 2.500 |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 2.500 |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.250 |
| FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.250 |
| TOP FLANGE WIDTH | INCHES NOMINAL 5.000 |
| WEIGHT PER UNIT MEASURE | POUNDS PER LINEAR FOOT 1.804 |
| FIRST TIP STYLE | |
| FIRST TIP INNER RADIUS | INCHES NOMINAL 0.031 |
| FIRST TIP OUTER RADIUS | INCHES NOMINAL 0.031 |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| THIRD 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 |
| HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-200 TO 3 |
| NONDEFINITIVE SPEC/STD DATA | TEMPER T8511 |
MOE rules
- MOE rule
- YA01
- MOE CD
- YA
- Date assigned
- 01-JUL-01
- PICA
- YA
- PICA LOA
- 81
- Auth collab
- YA
Freight
- ACTY CD
- KH
Related items
Standardization
- Item standardization code
- 5
- Orig stdzn dec
- 97
- Dt stdzn dec
- 12-FEB-1992
- NIIN status code
- 0
Request a quote
Your request goes to A-DEFENSE, a US Defense supplier in Texas, who will reply by email.