NSN 9540-01-469-9501
Part Details | STRUCTURAL BEAM
9540-01-469-9501 A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: For the letter H, both flanges of the H section are equal or longer than the width measured along the axis of the web; for the letter I, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters T and Z, on nonferrous type, the web is usually at right angles to the flanges. Letter H section may have a maximum of 5 percent slope on the inside face of the flanges.
Alternate Parts: AND101401404, AND10140-1404, AND101401404QQA20011T73511, AND10140-1404/QQ-A-200/11-T73511, QQA20011T73511, QQ-A-200/11-T73511, AMS101401404, AMS10140-1404, AMSQQA20011T73511, AMS-QQ-A-200/11-T73511, AMS4617, 9540-01-469-9501, 01-469-9501, 9540014699501, 014699501
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | DEC 01, 1999 | 01-469-9501 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
I SHAPE
RIGHT QUARTER RADIUS
LEFT QUARTER RADIUS
RIGHT QUARTER RADIUS
LEFT QUARTER RADIUS
RIGHT QUARTER RADIUS
LEFT QUARTER RADIUS
RIGHT QUARTER RADIUS
LEFT QUARTER RADIUS
Cross Reference | NSN 9540-01-469-9501
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10140-1404 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| AND10140-1404/QQ-A-200/11-T73511 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
| QQ-A-200/11-T73511 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS10140-1404 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-200/11-T73511 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS4617 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-469-9501
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 11 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| LENGTH | 32.900 INCHES NOMINAL |
| BASIC SHAPE STYLE | I SHAPE |
| OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| LEFT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE BOTTOM LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| WEB FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| TOP FLANGE WIDTH | 2.500 INCHES NOMINAL |
| BOTTOM FLANGE WIDTH | 2.500 INCHES NOMINAL |
| LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| LEFT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | LEFT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.010 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | RIGHT QUARTER RADIUS |
| SECOND TIP RADIUS | 0.010 INCHES NOMINAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/SECOND TIP |
| SPECIAL FEATURES | WEAPONS SYSTEM IS AIRCRAFT, B-2 BOMBER (ATB) |
| SPECIFICATION/STANDARD DATA | 81348-QQ-A-200 TO 11E TO CANCELED TO GOVERNMENT SPECIFICATION AND 99237-AND10140 GOVERNMENT STANDARD |
| END ITEM IDENTIFICATION | ACFT CEN SEC |