Catalog item
Request a quoteBEAM,STRUCTURAL
9540FSC
01NCB code
035-8128Item number
NIIN 01-035-8128
- DEMIL code
- A
Identification
- Item name code
- 37018
- PINC
- 0037018
- Criticality code
- X
- II
- 0
- DEMIL code
- A
- NIIN assigned
- 16-FEB-77
- Precious metals indicator
- U
- Hazardous material indicator
- N
Part numbers
| Part number | CAGE | CAGE status | RNCC | RNVC | Document availability code | RNAAC | RNFC | RNSC |
|---|---|---|---|---|---|---|---|---|
| AMS-QQ-A-200/11 | 81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC | R | 5 | 9 | E | ZZ | B | |
| QQ-A-200/11 | 81348 FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | A | 5 | 9 | 4 | 9Z | 1 | B |
| AND10136-2406 | 99237 AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | A | 4 | 1 | 4 | 9Z | 1 | D |
| AMS-QQ-A-200/11 | 0U583 SAE INTERNATIONAL DBA SAE INTERNATIONAL | A | 3 | 1 | E | ZZ |
Characteristics
| FABRICATION METHOD | EXTRUDED |
|---|---|
| OVERALL HEIGHT | INCHES NOMINAL 1.625 |
| LENGTH | FEET MINIMUM 10.000 AND FEET MAXIMUM 212.000 |
| LEFT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.156 |
| RIGHT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.156 |
| BASIC SHAPE STYLE | |
| FIRST TIP RADIUS | INCHES NOMINAL 0.156 |
| LEG THICKNESS | INCHES NOMINAL 0.156 |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 1.250 |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 1.250 |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.125 |
| FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.125 |
| TOP FLANGE WIDTH | INCHES NOMINAL 2.500 |
| WEIGHT PER UNIT MEASURE | POUNDS PER LINEAR FOOT 0.740 |
| FIRST TIP STYLE | |
| THIRD TIP RADIUS | INCHES NOMINAL 0.078 |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| THIRD TIP STYLE | |
| RIGHT TOP INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| LEFT TOP INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED AND STRESS RELIEVED BY STRETCHING |
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE QQ-A-200 TO 11 |
| NONDEFINITIVE SPEC/STD DATA | TEMPER T6511 |
MOE rules
- MOE rule
- ZG01
- MOE CD
- ZG
- Date assigned
- 01-APR-91
- PICA
- ZG
- PICA LOA
- 81
- Auth collab
- ZG
Freight
- ACTY CD
- DX
Related items
Standardization
- Item standardization code
- 2
- Orig stdzn dec
- KZ
- Dt stdzn dec
- 03-JAN-1980
- NIIN status code
- 0
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