17P2A6011-6 Panel Structural Aircraft with NSN 1560013704092 by Boeing Company The

Part Number: 17P2A6011-6
Alternate P/N: 17P2A60116
Manufacturer: Boeing Company The
NIIN: 013704092
CAGE Code: 88277
FSG: 15 Aircraft and Airframe Structural Components
Country: USA
NCB Code: 01

At Orbit NSN, we offer an expansive inventory of Panel Structural Aircraft components by Boeing Company The, including part number 17P2A6011-6, and many others. On this page, you can complete and submit a quote request form for this part number and others with the NSN 1560013704092 to receive a customized solution within 15 minutes or less of submission. All we ask is that you include relevant information while filling out this form, such as your desired part quantity and budget parameters, so our dedicated staff can best respond with a quote that suits your needs and restrictions alike.

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Quality is the cornerstone of our operations at Orbit NSN, and as such, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation, in addition to adhering to a strict NO CHINA SOURCING policy. To make your search simple, our catalogs feature items with CAGE Code 88277 and FSC 1560 Airframe Structural Components so that you always know you are procuring the exact items you need. To learn more about components with the NSN 1560-01-370-4092, such as this part manufactured by Boeing Company The, give us a call or email at any time, and a dedicated team member will be more than happy to assist you however they can through the procurement process. Get started today to see why our customers continue to rely on our top-notch products and services for all their operational needs.

NSN Information for Part Number 17P2A6011-6 with NSN 1560-01-370-4092, 1560013704092

NSNFSCNIINCLSHazmatDEMILCancelled NSN
1560-01-370-4092

Item PartTypeName:

PANEL,STRUCTURAL,AIRCRAFT

15600137040920P
CIICHCCESDPMICCriticalityENAC
UA0
Part NumberISCRNVCRNCCHCCMSDSSADC
17P2A6011-661CA

Characteristics Data of NSN 1560-01-370-4092, 1560013704092

MRCCriteriaCharacteristic
SR-5Design Control Reference Or Manufacturers Code
SFTTSurface TreatmentPRIMER EPOXY
CZDJAircraft LocationCENTER FUSELAGE FILLET,LOWER
MDCLMaterial Document And ClassificationDMS1974 MFR REF 1ST MATERIAL RESPONSE AND
SR-5Design Control Reference Or Manufacturers Code88277
STDCSurface Treatment Document And ClassificationMIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND
SR-5Design Control Reference Or Manufacturers Code17P2A6011-216
STDCSurface Treatment Document And ClassificationMIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE
MDCLMaterial Document And ClassificationDMS2288 MFR REF 3RD MATERIAL RESPONSE
CZEKAircraft Mission Design SeriesC-17A
MATTMaterialPLASTIC ARAMID
MATTMaterialALUMINUM ALLOY 1145 AND
CZEJAircraft Station NumberFS 910.500 TO FS 918.500
FEATSpecial FeaturesNHA 17P2A6011-214;PANEL INSTL-FILLET,LWR Y=910.500 THRU Y=981.500
MATTMaterialPLASTIC POLYAMIDE AND
MDCLMaterial Document And ClassificationDMS2302 MFR REF 2ND MATERIAL RESPONSE AND
MRCDecoded RequirementClear Text Reply
AARNFabrication MethodCOMPOSITE
AARNFabrication MethodLAMINATED AND
BWJFSide For Which DesignedRIGHT SIDE

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