Mfg Part Number: 1583
NSN : 9540-00-542-2759
NIIN : 005422759
CAGE Code : 01634
Manufacturer: Aluminum Co Of America
Item Name : Beam Structural
Here at Internet For Aviation, we have 1583 Beam Structural from Aluminum Co Of America, 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 1583 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 |
---|---|---|
STRUCTURAL | AARN | FABRICATION METHODEXTRUDED |
STRUCTURAL | ABKW | OVERALL HEIGHT1 500 INCHES NOMINAL |
STRUCTURAL | ABRY | LENGTH10 000 FEET MINIMUM AND 12 000 FEET MAXIMUM |
STRUCTURAL | ADXR | LEFT SIDE TOP FLANGE THICKNESS0 188 INCHES NOMINAL |
STRUCTURAL | ADXS | RIGHT SIDE TOP FLANGE THICKNESS0 188 INCHES NOMINAL |
STRUCTURAL | AGTA | BASIC SHAPE STYLET SHAPE |
STRUCTURAL | AJJP | LEG THICKNESS0 188 INCHES NOMINAL |
STRUCTURAL | BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1 000 INCHES NOMINAL |
STRUCTURAL | BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1 000 INCHES NOMINAL |
STRUCTURAL | BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGELEG0 188 INCHES NOMINAL |
STRUCTURAL | BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGELEG0 188 INCHES NOMINAL |
STRUCTURAL | BQJG | TOP FLANGE WIDTH2 000 INCHES NOMINAL |
STRUCTURAL | BRFD | WEIGHT PER UNIT MEASURE0 760 POUNDS PER LINEAR FOOT |
STRUCTURAL | CMZY | FIRST TIP STYLESQUARE END |
STRUCTURAL | CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL |
STRUCTURAL | CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL WFIRST TIP |
STRUCTURAL | CRZC | RIGHT TOP INSIDE ANGLE90 0 DEGREES NOMINAL |
STRUCTURAL | CSMZ | LEFT TOP INSIDE ANGLE90 0 DEGREES NOMINAL |
STRUCTURAL | HEAT | HEAT TREATMENTH-111 STRAIN HARDENED |
STRUCTURAL | MATT | MATERIALALUMINUM ALLOY 5086 |
STRUCTURAL | MDCL | MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-2005 FED SPEC 1ST MATERIAL RESPONSE |
STRUCTURAL | ZZZT | NONDEFINITIVE SPECSTD DATAH111 TEMPER |
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