Thank you for taking interest in The Boeing Company part number 65-1046-174, which is listed with the NSN 1560-01-538-2319 and a product description of “Fitting Structural Component Air.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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MRC | Criteria | Characteristic |
---|---|---|
FEAT | Special Features | THE OPPOSITE PART NUMBER IS 65-1046-173; BOND PER BAC5514-551, TYP 2, GRADE 5-AFTER BONDING, STRIP PER BAC5771 AND FINISH PER F-2, 26; CAUTION-INSURE POSITIVE ELECTRICAL CONTACT TO EACH SPLICE PLATE DURING RE-ANDOZING PROCESS; PRIOR TO ADHESIVE CURE CYCLE, ADHESIVE PRIMER OVERSPRAY MUST BE REMOVED WITH MEK SOLVENT WIPE; APPLY FAYING SURFACE SEAL(PRO-SEAL 898) BETWEEN SKIN AND - 110 DOUBLER; EXCESS SEALANT TO BE FLUSH WITH OUTSIDE CONTOUR; CONNECT UPPER WING PANELS AND DISTRIBUTES AERODYNAMIC LOADS FROM UPPER WING STRUCTURE; MATERIALS:ASSEMBLY OF 7075-T6 ALUMINUM |
CZDJ | Aircraft Location | UPPER WING STATION 360 |
AGAV | End Item Identification | MODEL 707, E-3(707 AWACS), E-6(J-STARS) |
CXCY | Part Name Assigned By Controlling Agency | SPLICE PLATE ASSEMBLY, UPPER WING STATION 360 |
MATT | Material | ALUMINUM ALLOY 7075 |
MRC | Decoded Requirement | Clear Text Reply |
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