Thank you for your interest in part number 17P6P5606-506, a component manufactured by Boeing Company The that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 1560-01-505-1458 and features the description “Panel Structural Aircraft.” To request a quote for part number 17P6P5606-506, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 1560-01-505-1458 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from Boeing Company The, which is associated with the CAGECode 88277. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 1560 Airframe Structural Components part number 17P6P5606-506.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-505-1458 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 015051458 | 0 | P | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
17P6P5606-506 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
MDCL | Material Document And Classification | QQ-A-250/5-T3 FED SPEC SINGLE MATERIAL RESPONSE |
CZEK | Aircraft Mission Design Series | C-17A |
MRC | Decoded Requirement | Clear Text Reply |
MATT | Material | ALUMINUM ALLOY 2024 |
CXCY | Part Name Assigned By Controlling Agency | PANEL INSTL-STRUC.OUTBD TE,FLAP |
FEAT | Special Features | ASAME AS -504 EXCEP ECN SHOWN; NHA17N6P0639-535; EFFECTIVITY 17A067-184;C/O 1 DOUBLER, STOCKSIZE .125 X 4 X5; 14 SHIM, STOCKSIZE .065X 1.25 X 12, 1 SHIM .065 X 1.5 X 9, 1 TE ASSY; MISC. HARDWARE |
CZDJ | Aircraft Location | OUTBD TE, OUTBD FLAP |
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