Mfg Part Number: 4E-817
Alternate P/N: 4E817
NSN : 9540-01-353-5562
NIIN : 013535562
CAGE Code : 43999
Manufacturer: Boeing Company The
Item Name : Beam Structural
Here at Internet For Aviation, we have 4E-817 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 4E-817 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 |
---|---|---|
ABKW | OVERALL HEIGHT | 5.000 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.150 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.150 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.500 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.250 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 1.804 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBJ | FIRST TIP OUTER RADIUS | 0.031 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/3 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T8511 TEMPER |
AARN | FABRICATION METHOD | EXTRUDED |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.150 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.500 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.250 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 5.000 INCHES NOMINAL |
CNBD | FIRST TIP INNER RADIUS | 0.031 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
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