Airframe Structural Components: 527-13360-1, 527-13366-1, 527-13385-2

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
527-13360-1
527133601
1560-01-592-6415Skin, AircraftEND Item Identification: KC-135 aircraft
Aircraft Mission Design Series: KC-135
Special Features: Next high assy 527-13359
The Boeing Company (82918)

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527-13360-2
527133602
1560-01-591-8014Skin, AircraftThe Boeing Company (82918)

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527-13365-3
527133653
1560-01-592-6406Skin, AircraftEND Item Identification: KC-135
Part Name Assigned BY Controlling Agency: Skin panel installation
The Boeing Company (82918)

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527-13365-4
527133654
1560-01-591-6105Installation kit, Tank, Fuel, AircrEND Item Identification: KC-135 acft
Special Features: Kit fastener
Part Name Assigned BY Controlling Agency: Skin panel installation 41 section sta 259.5-360 lh 41-7 rh 41-8
The Boeing Company (82918)

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527-13365-8
527133658
1560-01-591-6131Parts kit, FastenerEND Item Identification: KC-135(K) A-3-4
Part Name Assigned BY Controlling Agency: Skin panel installation 41 section sta 259.5-360
The Boeing Company (82918)

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527-13366-1
527133661
1560-01-592-6453Skin, AircraftEND Item Identification: KC-135 aircraft
Aircraft Mission Design Series: KC-135
Part Name Assigned BY Controlling Agency: Skin panel
The Boeing Company (82918)

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527-13366-2
527133662
1560-01-591-8013Skin, AircraftThe Boeing Company (82918)

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527-13381-1
527133811
1560-01-592-8957Skin, AircraftThe Boeing Company (81205)

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527-13381-2
527133812
1560-01-592-8941Skin, AircraftThe Boeing Company (81205)

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527-13382-3
527133823
1560-01-592-3998Parts kit, FastenerEND Item Identification: KC-135
Part Name Assigned BY Controlling Agency: Skin panel instl 43 section sta 360-395 L.H. 43-1 R.H. 43-2
END Item Name: KC-135
The Boeing Company (81205)

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527-13382-4
527133824
1560-01-592-4729Skin, AircraftEND Item Identification: KC-135
Aircraft Mission Design Series: KC-135 acft
Special Features: C/O hardware kit; RIVET-100 deg hd
The Boeing Company (81205)

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527-13382-7
527133827
1560-01-592-3987Parts kit, FastenerEND Item Identification: KC-135
Special Features: C/O filler-taper; revet 100 deg hd
Part Name Assigned BY Controlling Agency: Skin panel installation 43 section sta 360-395 L.H. 43-1 R.H. 43-2
The Boeing Company (81205)

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527-13382-8
527133828
1560-01-592-4771Skin, AircraftEND Item Identification: KC-135
Aircraft Mission Design Series: KC-135 acft
Special Features: Hardware kit R.H., filler-taper
The Boeing Company (81205)

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527-13383-1
527133831
1560-01-592-2749Skin, AircraftEND Item Identification: KC-135 acft
Aircraft Mission Design Series: KC-135
Special Features: Nha 527-13382 effectivity spares; heat treat T3
The Boeing Company (81205)

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527-13384-3
527133843
1560-01-592-0470Skin, AircraftAircraft Mission Design Series: KC-135 acft
Aircraft Location: Section 43
Part Name Assigned BY Controlling Agency: Skin panel installation
The Boeing Company (82918)

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527-13384-4
527133844
1560-01-592-1721Skin, AircraftAircraft Mission Design Series: KC-35
Special Features: U/O KC-135
Aircraft Location: Section 43
The Boeing Company (82918)

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527-13384-7
527133847
1560-01-592-7330Skin, AircraftEND Item Identification: Used on KC-135 acft
Aircraft Mission Design Series: KC-135 acft
Special Features: C/O stiffener no. 6 L.H. aft, no. 4, .4 L.F cover, N. 2 L.H. aft, no 3 L.H. aft; splice plate, stiffener L.H. fwd, no. 2 .NO6; filler-tapered, spanel detailed R.H., BOLT-100 deg hd, bolt-hex DRIVE-100 deg hd, filler-laminated, collar, RIVET-100 deg hd
The Boeing Company (82918)

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527-13384-8
527133848
1560-01-592-0013Skin, AircraftAircraft Mission Design Series: KC-135 acft
Aircraft Location: Section 43
Part Name Assigned BY Controlling Agency: Skin panel installation
The Boeing Company (82918)

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527-13385-1
527133851
1560-01-591-8029Skin, AircraftThe Boeing Company (82918)

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527-13385-2
527133852
1560-01-591-8030Skin, AircraftThe Boeing Company (82918)

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  • We solve sourcing challenges for 527-13360-1, 527-13360-2, 527-13365-3, 527-13365-4, 527-13365-8, 527-13366-2, 527-13382-4, 527-13382-7, 527-13384-4, 527-13385-2 - NSN parts, hard to find, long lead time and obsolete components.