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1560-01-489-1076

20 Products

64-1061

CHORD

NSN, MFG P/N

1560014891076

NSN

1560-01-489-1076

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64-1061

CHORD

NSN, MFG P/N

1560014891076

NSN

1560-01-489-1076

MFG

THE BOEING COMPANY DBA BOEING

64-1061-3006

WEB,STRUCTURAL COMPONENT,AIRCRAFT

NSN, MFG P/N

1560014891063

NSN

1560-01-489-1063

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64-1061-3006

WEB,STRUCTURAL COMPONENT,AIRCRAFT

NSN, MFG P/N

1560014891063

NSN

1560-01-489-1063

MFG

THE BOEING COMPANY DBA BOEING

64-1061-3008

CHORD

NSN, MFG P/N

1560014891076

NSN

1560-01-489-1076

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64-1061-3008

CHORD

NSN, MFG P/N

1560014891076

NSN

1560-01-489-1076

MFG

THE BOEING COMPANY DBA BOEING

5-89355-77

WINDSHIELD ASSEMBLY,AIRCRAFT

NSN, MFG P/N

1560014891079

NSN

1560-01-489-1079

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5-89355-77

WINDSHIELD ASSEMBLY,AIRCRAFT

NSN, MFG P/N

1560014891079

NSN

1560-01-489-1079

MFG

THE BOEING COMPANY DBA BOEING DIV BOEING COMMERCIAL AIRPLANES

5-89355-77

WINDSHIELD ASSEMBLY,AIRCRAFT

NSN, MFG P/N

1560014891079

NSN

1560-01-489-1079

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5-89355-77

WINDSHIELD ASSEMBLY,AIRCRAFT

NSN, MFG P/N

1560014891079

NSN

1560-01-489-1079

MFG

THE BOEING COMPANY DBA BOEING

64-1061

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891124

NSN

1560-01-489-1124

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64-1061

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891124

NSN

1560-01-489-1124

MFG

THE BOEING COMPANY DBA BOEING

64-1061-3011

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891124

NSN

1560-01-489-1124

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64-1061-3011

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891124

NSN

1560-01-489-1124

MFG

THE BOEING COMPANY DBA BOEING

64-1061

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891139

NSN

1560-01-489-1139

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64-1061

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891139

NSN

1560-01-489-1139

MFG

THE BOEING COMPANY DBA BOEING

64-1061-3003

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891139

NSN

1560-01-489-1139

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64-1061-3003

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891139

NSN

1560-01-489-1139

MFG

THE BOEING COMPANY DBA BOEING DIV BOEING COMMERCIAL AIRPLANES

64-1061-3003

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891139

NSN

1560-01-489-1139

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64-1061-3003

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014891139

NSN

1560-01-489-1139

MFG

THE BOEING COMPANY DBA BOEING

114S5910-97

BRACKET,STRUCTURAL COMPONENT,AIRCRAFT

NSN, MFG P/N

1560014891190

NSN

1560-01-489-1190

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114S5910-97

BRACKET,STRUCTURAL COMPONENT,AIRCRAFT

NSN, MFG P/N

1560014891190

NSN

1560-01-489-1190

MFG

THE BOEING COMPANY DBA BOEING

5HP71201-113

INTERCOSTAL,AIRCRAFT

NSN, MFG P/N

1560014891349

NSN

1560-01-489-1349

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5HP71201-113

INTERCOSTAL,AIRCRAFT

NSN, MFG P/N

1560014891349

NSN

1560-01-489-1349

MFG

THE BOEING COMPANY DBA BOEING

Description

AIRCRAFT LOCATION: SIDE LINK
AIRCRAFT MISSION DESIGN SERIES: F/A-22 RAPTOR
DESIGN CONTROL REFERENCE: 5HP71201-113
III END ITEM IDENTIFICATION: F-22 RAPTOR
MANUFACTURERS CODE: 81205
MATERIAL: TITANIUM ALLOY
MATERIAL THICKNESS: 2.500 INCHES NOMINAL
OVERALL LENGTH: 20.000 INCHES NOMINAL
OVERALL WIDTH: 4.000 INCHES NOMINAL
PART NAME ASSIGNED BY CONTROLLING AGENCY: INTERCOASTAL,FTG
SPECIAL FEATURES: 5PTM7T01 6-2222 STA TITUNIUM PLATE
THE MANUFACTURERS DATA:

5HP71201-114

INTERCOSTAL,AIRCRAFT

NSN, MFG P/N

1560014891353

NSN

1560-01-489-1353

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5HP71201-114

INTERCOSTAL,AIRCRAFT

NSN, MFG P/N

1560014891353

NSN

1560-01-489-1353

MFG

THE BOEING COMPANY DBA BOEING

Description

AIRCRAFT LOCATION: SIDE LINK
AIRCRAFT MISSION DESIGN SERIES: F-22 RAPTOR
DESIGN CONTROL REFERENCE: 5HP71201-114
III END ITEM IDENTIFICATION: F-22 RAPTOR
MANUFACTURERS CODE: 81205
MATERIAL: TITANIUM ALLOY
MATERIAL THICKNESS: 2.500 INCHES NOMINAL
OVERALL LENGTH: 20.000 INCHES NOMINAL
OVERALL WIDTH: 4.000 INCHES NOMINAL
PART NAME ASSIGNED BY CONTROLLING AGENCY: INTERCOASTAL, FTG
SPECIAL FEATURES: 5PTM7T01 6-2222 STA TITUNIUM PLATE
THE MANUFACTURERS DATA:

5HF75115-101

HINGE,DOOR,AIRCRAFT

NSN, MFG P/N

1560014891495

NSN

1560-01-489-1495

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5HF75115-101

HINGE,DOOR,AIRCRAFT

NSN, MFG P/N

1560014891495

NSN

1560-01-489-1495

MFG

THE BOEING COMPANY DBA BOEING

Description

AIRCRAFT MISSION DESIGN SERIES: F/A-22 RAPTOR
III END ITEM IDENTIFICATION: F/A-22 RAPTOR
III PART NAME ASSIGNED BY CONTROLLING AGENCY: GOOSENECK
MATERIAL: ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION: AMS4050 7050-T7451 ASSN STD SINGLE MATERIAL RESPONSE
SPECIAL FEATURES: HINGE- ACCESS DOOR

6279-42105-1

DOOR,ACCESS,AIRCRAFT

NSN, MFG P/N

1560014891625

NSN

1560-01-489-1625

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6279-42105-1

DOOR,ACCESS,AIRCRAFT

NSN, MFG P/N

1560014891625

NSN

1560-01-489-1625

MFG

L-3 COMMUNICATIONS CORPORATION D IV INTEGRATED SYSTEMS - GREENVILLE

5HP71236-117

INTERCOSTAL,AIRCRAFT

NSN, MFG P/N

1560014891670

NSN

1560-01-489-1670

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5HP71236-117

INTERCOSTAL,AIRCRAFT

NSN, MFG P/N

1560014891670

NSN

1560-01-489-1670

MFG

THE BOEING COMPANY DBA BOEING

Description

AIRCRAFT MISSION DESIGN SERIES: F-22 RAPTOR
DESIGN CONTROL REFERENCE: 5HP71236-117
III END ITEM IDENTIFICATION: F-22 RAPTOR
MANUFACTURERS CODE: 81205
THE MANUFACTURERS DATA:

160J611335-13

SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT

NSN, MFG P/N

1560014895350

NSN

1560-01-489-5350

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160J611335-13

SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT

NSN, MFG P/N

1560014895350

NSN

1560-01-489-5350

MFG

NORTHROP GRUMMAN SYSTEMS CORPORATION DIV NORTHROP GRUMMAN AEROSPACE SYSTEMS

Description

AIRCRAFT LOCATION: WING CTR. PANEL FRONT-SPAR WEB
AIRCRAFT MISSION DESIGN SERIES: -10A
AIRCRAFT STATION NUMBER: WS44.5 TO WS54.0
DESIGN CONTROL REFERENCE: 160J611335-13
MANUFACTURERS CODE: 26512
MATERIAL: ALUMINUM ALLOY 7075
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A/200-11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 0.094 INCHES NOMINAL
OVERALL LENGTH: 15.000 INCHES NOMINAL
SIDE FOR WHICH DESIGNED: BOTH SIDES
SPECIAL FEATURES: AND WS79.0 LH;AL SHP/T6511;DIMENSIONS ARE STOCKSIZE,AND 10136-1702; NHA-2; MANF. SUGGEST NAME(TEE-SPCL,A/OA-10A WING CTR. PANEL REPAIR-FRT. SPAR WEB)
THE MANUFACTURERS DATA:

160J611335-11

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014895351

NSN

1560-01-489-5351

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160J611335-11

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014895351

NSN

1560-01-489-5351

MFG

NORTHROP GRUMMAN SYSTEMS CORPORATION DIV NORTHROP GRUMMAN AEROSPACE SYSTEMS

Description

AIRCRAFT LOCATION: WING CTR. PANEL-FRT. SPAR WEB
AIRCRAFT MISSION DESIGN SERIES: A-10A
AIRCRAFT STATION NUMBER: WS44.5 TO WS54.0
DESIGN CONTROL REFERENCE: 160J611335-11
MANUFACTURERS CODE: 26512
MATERIAL: ALUMINUM ALLOY 7075
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 0.100 INCHES NOMINAL
OVERALL LENGTH: 15.000 INCHES NOMINAL
OVERALL WIDTH: 6.000 INCHES NOMINAL
SIDE FOR WHICH DESIGNED: BOTH SIDES
SPECIAL FEATURES: AND WS79.0 LH; DIM. ARE STOCKSIZE; NHA -2; STRENGTH T6 BARE; MANF. SUGGESTED NAME(A/OA-10A WING CTR. PANEL-FRT. SPAR WEB)
THE MANUFACTURERS DATA:

160J611335-23

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014895352

NSN

1560-01-489-5352

View More Info

160J611335-23

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014895352

NSN

1560-01-489-5352

MFG

NORTHROP GRUMMAN SYSTEMS CORPORATION DIV NORTHROP GRUMMAN AEROSPACE SYSTEMS

Description

AIRCRAFT LOCATION: WING CTR. PANEL-FRT. SPAR WEB
AIRCRAFT MISSION DESIGN SERIES: A-10A
AIRCRAFT STATION NUMBER: WS44.5 TO WS54.0
MATERIAL: STEEL CORROSION RESISTING
MATERIAL DOCUMENT AND CLASSIFICATION: MIL-S-25043 MIL SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 0.090 INCHES NOMINAL
OVERALL LENGTH: 8.000 INCHES NOMINAL
OVERALL WIDTH: 5.200 INCHES NOMINAL
SIDE FOR WHICH DESIGNED: BOTH SIDES
SPECIAL FEATURES: CRES,SH,17-7PH,COND A;NHA -7; ANDWS79.0 LH; MANF. SUGGESTED NAME(A/OA-10A WING CTR PANEL REPAIR-FRT SPAR WEB

160J611335-23

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014895352

NSN

1560-01-489-5352

View More Info

160J611335-23

PLATE,STRUCTURAL,AIRCRAFT

NSN, MFG P/N

1560014895352

NSN

1560-01-489-5352

MFG

MIDWEST METALS

Description

AIRCRAFT LOCATION: WING CTR. PANEL-FRT. SPAR WEB
AIRCRAFT MISSION DESIGN SERIES: A-10A
AIRCRAFT STATION NUMBER: WS44.5 TO WS54.0
MATERIAL: STEEL CORROSION RESISTING
MATERIAL DOCUMENT AND CLASSIFICATION: MIL-S-25043 MIL SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 0.090 INCHES NOMINAL
OVERALL LENGTH: 8.000 INCHES NOMINAL
OVERALL WIDTH: 5.200 INCHES NOMINAL
SIDE FOR WHICH DESIGNED: BOTH SIDES
SPECIAL FEATURES: CRES,SH,17-7PH,COND A;NHA -7; ANDWS79.0 LH; MANF. SUGGESTED NAME(A/OA-10A WING CTR PANEL REPAIR-FRT SPAR WEB