Mfg Part Number: 1MA160D05-10228
Alternate P/N: 1MA160D0510228
NSN : 9540-01-496-1374
NIIN : 014961374
CAGE Code : 76301
Manufacturer: Boeing Company The
Item Name : Beam Structural
Here at Internet For Aviation, we have 1MA160D05-10228 Beam Structural from Boeing Company The, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific 1MA160D05-10228 to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-496-1374 Item Description: Beam Structural | 9540 | 014961374 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | U | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1MA160D05-10228 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075,TEMPER T73511 |
| BRFD | WEIGHT PER UNIT MEASURE | 0.533 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.420 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| HEAT | HEAT TREATMENT | T-73511 SOLUTION HEAT TREATED |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ABKW | OVERALL HEIGHT | 2.073 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.190 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.530 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FEAT | SPECIAL FEATURES | ANGLE ENDS ARE RADIUS PER DATA PROVIDED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
| AJJP | LEG THICKNESS | 0.142 INCHES NOMINAL |
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