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8895 by Alcoa Reynolds Metals Company with NSN 9540-00-892-4755 Available Quote Now!

Mfg Part Number: 8895

NIIN : 008924755

CAGE Code : 77783

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!

  Cross Reference Parts List for NSN 9540008924755

Characteristics Data of NSN 9540-00-892-4755, 9540008924755

MRCCriteriaCharacteristic
AARNFABRICATION METHODEXTRUDED
ADXRLEFT SIDE TOP FLANGE THICKNESS0.281 INCHES NOMINAL
AGTABASIC SHAPE STYLET SHAPE
BPXDLEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.750 INCHES NOMINAL
BPXJFILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.345 INCHES NOMINAL
BQJGTOP FLANGE WIDTH1.500 INCHES NOMINAL
BQJKLEFT SIDE TOP FLANGE TIP THICKNESS0.250 INCHES NOMINAL
BQKHERR DEFAULTERR DEFAULT
BQKHLEG TIP THICKNESS0.250 INCHES NOMINAL
CMZYFIRST TIP STYLESQUARE END
CNQLTHIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL W/FIRST TIP
CSTQRIGHT TOP INNER FACE TO OUTER FACE ANGLE90.0 DEGREES NOMINAL
HEATHEAT TREATMENTT-6 SOLUTION HEAT TREATED AND ARTIFICALLY AGED
MATLMATERIALALUMINUM ALLOY, QQ-A-200/9
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200/9 FED SPEC 1ST MATERIAL RESPONSE
ABRYLENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
ADXSRIGHT SIDE TOP FLANGE THICKNESS0.281 INCHES NOMINAL
AJJPLEG THICKNESS0.281 INCHES NOMINAL
BPXLFILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.345 INCHES NOMINAL
BQJMRIGHT SIDE TOP FLANGE TIP THICKNESS0.250 INCHES NOMINAL
BRFDWEIGHT PER UNIT MEASURE0.808 POUNDS PER LINEAR FOOT
CNQJSECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
CRYXLEFT TOP INNER FACE TO OUTER FACE ANGLE90.0 DEGREES NOMINAL
MATTMATERIALALUMINUM ALLOY 6063
ZZZTNONDEFINITIVE SPEC/STD DATAT6 TEMPER
ABKWOVERALL HEIGHT1.250 INCHES NOMINAL
BPXGRIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.750 INCHES NOMINAL

  Corresponding National Stock Number to 8895



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