Mfg Part Number: 8895
NSN : 9540-00-892-4755
NIIN : 008924755
CAGE Code : 77783
Manufacturer: Alcoa Reynolds Metals Company
Item Name : Beam Structural
Here at Internet For Aviation, we have 8895 Beam Structural from Alcoa Reynolds Metals Company, 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 8895 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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We pride ourselves in our abilities to deliver quality superior grade aviation parts in a timely schedule. Thanks to the various supply chain locations that we have across the United States. We can execute fast shipping times that outpace our competitors. Unlike other competitors, we can promise same day shipping and delivery right to the very place you need. We’re leaders in our industry thanks to our parts streamlining process which includes quick stock and acquisition of the certified product and fast shipping. For whatever needs you have, be they Beam Structural and 8895 parts, we can procure and deliver in a schedule that fits with you! Contact us today for an immediate quote!
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.281 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.345 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.500 INCHES NOMINAL |
| BQJK | LEFT SIDE TOP FLANGE TIP THICKNESS | 0.250 INCHES NOMINAL |
| BQKH | ERR DEFAULT | ERR DEFAULT |
| BQKH | LEG TIP THICKNESS | 0.250 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CSTQ | RIGHT TOP INNER FACE TO OUTER FACE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED AND ARTIFICALLY AGED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/9 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/9 FED SPEC 1ST MATERIAL RESPONSE |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.281 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.281 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.345 INCHES NOMINAL |
| BQJM | RIGHT SIDE TOP FLANGE TIP THICKNESS | 0.250 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.808 POUNDS PER LINEAR FOOT |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRYX | LEFT TOP INNER FACE TO OUTER FACE ANGLE | 90.0 DEGREES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 6063 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| ABKW | OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
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