My Quote Request
1560-01-187-5513
20 Products
65-6245-2001
RIB,STIFFENER,AIRCRAFT
NSN, MFG P/N
1560011875513
NSN
1560-01-187-5513
MFG
THE BOEING COMPANY DBA BOEING
Description
AIRCRAFT MISSION DESIGN SERIES: KC-135
DESIGN CONTROL REFERENCE: 69-6245-1
MANUFACTURERS CODE: 81205
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQA-A-250 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 0.050 INCHES NOMINAL
OVERALL LENGTH: 15.000 INCHES NOMINAL
OVERALL WIDTH: 6.400 INCHES NOMINAL
THE MANUFACTURERS DATA:
Related Searches:
69-6245-1
RIB,STIFFENER,AIRCRAFT
NSN, MFG P/N
1560011875513
NSN
1560-01-187-5513
MFG
THE BOEING COMPANY DBA BOEING
Description
AIRCRAFT MISSION DESIGN SERIES: KC-135
DESIGN CONTROL REFERENCE: 69-6245-1
MANUFACTURERS CODE: 81205
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQA-A-250 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 0.050 INCHES NOMINAL
OVERALL LENGTH: 15.000 INCHES NOMINAL
OVERALL WIDTH: 6.400 INCHES NOMINAL
THE MANUFACTURERS DATA:
Related Searches:
69-6245-2
RIB,STIFFENER,AIRCRAFT
NSN, MFG P/N
1560011875514
NSN
1560-01-187-5514
MFG
THE BOEING COMPANY DBA BOEING
Description
AIRCRAFT MISSION DESIGN SERIES: KC135
DESIGN CONTROL REFERENCE: 69-6245-2
MANUFACTURERS CODE: 81205
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 0.050 INCHES NOMINAL
OVERALL LENGTH: 15.000 INCHES NOMINAL
OVERALL WIDTH: 6.500 INCHES NOMINAL
THE MANUFACTURERS DATA:
Related Searches:
69-6245-2002
RIB,STIFFENER,AIRCRAFT
NSN, MFG P/N
1560011875514
NSN
1560-01-187-5514
MFG
THE BOEING COMPANY DBA BOEING
Description
AIRCRAFT MISSION DESIGN SERIES: KC135
DESIGN CONTROL REFERENCE: 69-6245-2
MANUFACTURERS CODE: 81205
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 0.050 INCHES NOMINAL
OVERALL LENGTH: 15.000 INCHES NOMINAL
OVERALL WIDTH: 6.500 INCHES NOMINAL
THE MANUFACTURERS DATA:
Related Searches:
L5873113-003
STABILIZER,HORIZONTAL
NSN, MFG P/N
1560011876368
NSN
1560-01-187-6368
MFG
BOEING COMPANY THE DBA BOEING
Description
STABILIZER,HORIZONTAL
Related Searches:
74A585004-2003
MANIFOLD ASSEMBLY,F
NSN, MFG P/N
1560011876579
NSN
1560-01-187-6579
MFG
BOEING COMPANY THE DBA BOEING
Description
DESIGN CONTROL REFERENCE: 74A585004-2003
III END ITEM IDENTIFICATION: AIRCRAFT MODEL F-18
MANUFACTURERS CODE: 76301
THE MANUFACTURERS DATA:
Related Searches:
L-60080-1
FLANGE,ATTACHMENT,MOLDED TANK
NSN, MFG P/N
1560011876619
NSN
1560-01-187-6619
L-60080-1
FLANGE,ATTACHMENT,MOLDED TANK
NSN, MFG P/N
1560011876619
NSN
1560-01-187-6619
MFG
AMERICAN FUEL CELL AND COATED FABRICS COMPANY DBA AMFUEL
Description
ACTIVE FACE DESIGN: RAISED
DESIGN CONTROL REFERENCE: L-60080-1
III END ITEM IDENTIFICATION: AIRCRAFT MODEL F-18
MANUFACTURERS CODE: 05476
THE MANUFACTURERS DATA:
Related Searches:
62022-19
BOARD,BACKING
NSN, MFG P/N
1560011877686
NSN
1560-01-187-7686
MFG
AMERICAN FUEL CELL AND COATED FABRICS COMPANY DBA AMFUEL
Description
DESIGN CONTROL REFERENCE: 62022-19
III END ITEM IDENTIFICATION: AIRCRAFT MODEL F-18
MANUFACTURERS CODE: 05476
THE MANUFACTURERS DATA:
Related Searches:
74A230784-2003
SKIN,AIRCRAFT
NSN, MFG P/N
1560011877689
NSN
1560-01-187-7689
MFG
BOEING COMPANY THE DBA BOEING
Description
III END ITEM IDENTIFICATION: AIRCRAFT MODEL F-18
SPECIAL FEATURES: TITANIUM PER MIL-T-9046,TYPE 1,COMP B
Related Searches:
74A230784-2003
SKIN,AIRCRAFT
NSN, MFG P/N
1560011877689
NSN
1560-01-187-7689
MFG
NORTHROP GRUMMAN SYSTEMS CORPORATION DIV INTEGRATED SYSTEMS SECTOR
Description
III END ITEM IDENTIFICATION: AIRCRAFT MODEL F-18
SPECIAL FEATURES: TITANIUM PER MIL-T-9046,TYPE 1,COMP B
Related Searches:
74A230784-2004
SKIN,AIRCRAFT
NSN, MFG P/N
1560011877690
NSN
1560-01-187-7690
MFG
BOEING COMPANY THE DBA BOEING
Description
III END ITEM IDENTIFICATION: AIRCRAFT MODEL F-18
SPECIAL FEATURES: TITANIUM PER MIL-T-9046,TYPE 1,COMP B
Related Searches:
74A230784-2004
SKIN,AIRCRAFT
NSN, MFG P/N
1560011877690
NSN
1560-01-187-7690
MFG
NORTHROP GRUMMAN SYSTEMS CORPORATION DIV INTEGRATED SYSTEMS SECTOR
Description
III END ITEM IDENTIFICATION: AIRCRAFT MODEL F-18
SPECIAL FEATURES: TITANIUM PER MIL-T-9046,TYPE 1,COMP B
Related Searches:
406-040-741-102
SUPPORT ASSY
NSN, MFG P/N
1560011877833
NSN
1560-01-187-7833
MFG
BELL HELICOPTER TEXTRON INC.
Description
SUPPORT ASSY
Related Searches:
3E42114-107
PANEL,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878196
NSN
1560-01-187-8196
3E42114-107
PANEL,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878196
NSN
1560-01-187-8196
MFG
LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN
Description
AIRCRAFT LOCATION: TRIM PAN,EMERGENCY ESCAPE HATCH
AIRCRAFT MISSION DESIGN SERIES: C-141
DESIGN CONTROL REFERENCE: 3E42114-107
III PART NAME ASSIGNED BY CONTROLLING AGENCY: TRIM PAN
MANUFACTURERS CODE: 98897
MATERIAL: GLASS FIBER AND PLASTIC POLYESTER
MATERIAL DOCUMENT AND CLASSIFICATION: MIL-F-9084 MIL SPEC 1ST MATERIAL RESPONSE AND MIL-A-7575 MIL SPEC 2ND MATERIAL RESPONSE
OVERALL LENGTH: 23.260 INCHES NOMINAL
OVERALL WIDTH: 23.260 INCHES NOMINAL
THE MANUFACTURERS DATA:
Related Searches:
65C18554-616
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878211
NSN
1560-01-187-8211
65C18554-616
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878211
NSN
1560-01-187-8211
MFG
THE BOEING COMPANY DBA BOEING
Description
(NON-CORE DATA) SUPPLEMENTARY FEATURES: USED AS RH LIP SPLICE ON LIP ASSEMBLY OF INLET COWL
DESIGN CONTROL REFERENCE: 65C18554-616
III END ITEM IDENTIFICATION: ACFT MODEL KC-135
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: AL ALLOY 2219-0 SHEET QQ-A-250/30; HEAT TREATED TO COND T62; 20.000 IN. LG,7.300 IN. W,0.071 IN. THK; FINISH F-2.20 AND DESOTO HI TEMP PRIMER PER BAC5710; -616 SAME AS -16 EXCEPT FINISH; NHA 65C18554-605
THE MANUFACTURERS DATA:
Related Searches:
65C18554-616
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878211
NSN
1560-01-187-8211
65C18554-616
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878211
NSN
1560-01-187-8211
MFG
THE BOEING COMPANY DBA BOEING
Description
(NON-CORE DATA) SUPPLEMENTARY FEATURES: USED AS RH LIP SPLICE ON LIP ASSEMBLY OF INLET COWL
DESIGN CONTROL REFERENCE: 65C18554-616
III END ITEM IDENTIFICATION: ACFT MODEL KC-135
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: AL ALLOY 2219-0 SHEET QQ-A-250/30; HEAT TREATED TO COND T62; 20.000 IN. LG,7.300 IN. W,0.071 IN. THK; FINISH F-2.20 AND DESOTO HI TEMP PRIMER PER BAC5710; -616 SAME AS -16 EXCEPT FINISH; NHA 65C18554-605
THE MANUFACTURERS DATA:
Related Searches:
65C18554-615
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878212
NSN
1560-01-187-8212
65C18554-615
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878212
NSN
1560-01-187-8212
MFG
THE BOEING COMPANY DBA BOEING
Description
(NON-CORE DATA) SUPPLEMENTARY FEATURES: USED AS LH LIP SPLICE ON LIP ASSEMBLY OF INLET COWL
DESIGN CONTROL REFERENCE: 65C18554-615
III END ITEM IDENTIFICATION: ACFT MODEL KC-135
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: AL ALLOY 2219-0 SHEET PER QQ-A-250/30; HEAT TREATED TO COND T62; 20.000 IN. LG,7.300 IN. W,0.071 IN. THK; FINISH F-2.20 AND DESOTO HI-TEMP PRIMER PER BAC5710; -615 SAME AS -15 EXCEPT FINISH; NHA 65C18554-605
THE MANUFACTURERS DATA:
Related Searches:
25-2377-810
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878213
NSN
1560-01-187-8213
25-2377-810
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878213
NSN
1560-01-187-8213
MFG
THE BOEING COMPANY DBA BOEING
Description
(NON-CORE DATA) SUPPLEMENTARY FEATURES: USED AS SPLICE PLATE ON NOSE COWL ASSEMBLY
DESIGN CONTROL REFERENCE: 25-2377-810
III END ITEM IDENTIFICATION: ACFT MODEL B-52
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: AL ALLOY SHEET 2024-0,0 TEMPER PER QQ-A-362; HEAT TREATED TO COND T4; FINISH F-2.115; 14.000 IN. LG,2.540 IN. W,0.050 IN. THK; NHA 25-2377
THE MANUFACTURERS DATA:
Related Searches:
25-2377-809
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878214
NSN
1560-01-187-8214
25-2377-809
PLATE,STRUCTURAL,AIRCRAFT
NSN, MFG P/N
1560011878214
NSN
1560-01-187-8214
MFG
THE BOEING COMPANY DBA BOEING
Description
(NON-CORE DATA) SUPPLEMENTARY FEATURES: USED AS SPLICE PLATE ON NOSE COWL ASSEMBLY
DESIGN CONTROL REFERENCE: 25-2377-809
III END ITEM IDENTIFICATION: ACFT MODEL B-52
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: AL ALLOY SHEET 2024-0 PER QQ-A-362,0 TEMPER; HEAT TREATED TO COND T4; FINISH F-2.115; 12.000 IN. LG,2.540 IN. W,0.050 IN. THK; OPPOSITE P/N -808; NHA 25-2377
THE MANUFACTURERS DATA:
Related Searches:
25-6061-1
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011878221
NSN
1560-01-187-8221
25-6061-1
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011878221
NSN
1560-01-187-8221
MFG
THE BOEING COMPANY DBA BOEING
Description
DESIGN CONTROL REFERENCE: 25-6061-1
III END ITEM IDENTIFICATION: ACFT MODEL B-52
III SUPPLEMENTARY FEATURES: FUNCTIONAL DESCRIPTION:USED AS SUPPORT BRACKET ON LATERAL CONTROL TRIM CENTERING
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: C/O 1 BRACKET,2 BEARINGS,1 SWAGING RING,3 STEEL WIRE SLEEVES; OPPOSITE P/N -2; BRACKET MADE FROM MAGNESIUM ALLOY SAND CASTING PER QQ-M-56; NHA 25-6060
THE MANUFACTURERS DATA: