Mfg Part Number: AMS-QQ-A-200 5
Alternate P/N: AMSQQA2005
NSN : 9540-00-542-2758
NIIN : 005422758
CAGE Code : 81343
Manufacturer: Society Of Automotive Engineers Inc
Item Name : Beam Structural
Here at Internet For Aviation, we have AMS-QQ-A-200 5 Beam Structural from Society Of Automotive Engineers Inc, 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 AMS-QQ-A-200 5 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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| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.016 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.970 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/5, ALLOY 5086 |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/5, ALLOY 5086 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | H111 TEMPER |
| ABRY | LENGTH | 20.000 FEET MINIMUM AND 30.000 FEET MAXIMUM |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.188 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.016 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 3.000 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | H-111 STRAIN HARDENED |
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