Catalog item
Request a quoteBEAM,STRUCTURAL
9540FSC
01NCB code
015-5004Item number
NIIN 01-015-5004
- DEMIL code
- A
Identification
- Item name code
- 37018
- PINC
- 0037018
- Criticality code
- X
- II
- 0
- DEMIL code
- A
- NIIN assigned
- 22-JAN-76
- Precious metals indicator
- U
- ADP equipment code
- 0
- Hazardous material indicator
- N
- Last known source of supply
- FGZ
Part numbers
| Part number | CAGE | CAGE status | RNCC | RNVC | Document availability code | RNAAC | RNFC | RNSC |
|---|---|---|---|---|---|---|---|---|
| 1MA160E03-10065 | 76301 THE BOEING COMPANY DIV DEFENSE | A | 3 | 2 | 4 | 9Z | 1 | A |
| NAS344-43 | 80205 NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE | A | 3 | 1 | 2 | 9Z | 1 | D |
| QQ-A-200/13 | 81349 MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | A | 4 | 1 | 4 | 9Z | 1 | D |
Characteristics
| FABRICATION METHOD | EXTRUDED |
|---|---|
| OVERALL HEIGHT | INCHES NOMINAL 1.125 |
| LENGTH | FEET MINIMUM 10.000 AND FEET MAXIMUM 12.000 |
| LEFT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.078 |
| RIGHT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.078 |
| BASIC SHAPE STYLE | |
| FIRST TIP RADIUS | INCHES NOMINAL 0.078 |
| LEG THICKNESS | INCHES NOMINAL 0.078 |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 0.875 |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 0.875 |
| 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 1.750 |
| WEIGHT PER UNIT MEASURE | POUNDS PER LINEAR FOOT 0.266 |
| FIRST TIP STYLE | |
| THIRD TIP RADIUS | INCHES NOMINAL 0.039 |
| 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 7178 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE QQ-A-200 TO 13 |
| SPECIFICATION/STANDARD DATA | PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD 80205-NAS344 |
| NONDEFINITIVE SPEC/STD DATA | TEMPER T6511 |
Freight
- ACTY CD
- ZG
Related items
Standardization
- Item standardization code
- 2
- Orig stdzn dec
- KZ
- Dt stdzn dec
- 27-DEC-1979
- NIIN status code
- 6
History
Identification changes
- Item name code
- 37018
- Item standardization code
- 2
- DEMIL code
- A
- Criticality code
- X
- Precious metals indicator
- U
- Cancelled date
- 10-JUN-2026
- NIIN status code
- 6
Past part numbers
| Part number | CAGE | RNCC | RNVC |
|---|---|---|---|
| QQ-A-200/13 | 81349 MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | 4 | 1 |
| NAS344-43 | 80205 NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE | 3 | 1 |
| 1MA160E03-10065 | 76301 THE BOEING COMPANY DIV DEFENSE | 3 | 2 |
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