My Quote Request
1560-01-157-1581
20 Products
9-66803-1
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011571581
NSN
1560-01-157-1581
9-66803-1
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011571581
NSN
1560-01-157-1581
MFG
THE BOEING COMPANY DBA BOEING
Description
AIRCRAFT LOCATION: STIFFENER TIE FITTING ON NACELLE STRUT
AIRCRAFT MISSION DESIGN SERIES: KC-135
DESIGN CONTROL REFERENCE: 9-66803-3
MANUFACTURERS CODE: 81205
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-267 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 1.140 INCHES NOMINAL
OVERALL LENGTH: 5.080 INCHES NOMINAL
OVERALL WIDTH: 1.580 INCHES NOMINAL
SPECIAL FEATURES: T4 TEMPER;OPPOSITE -4
THE MANUFACTURERS DATA:
Related Searches:
9-66803-3
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011571581
NSN
1560-01-157-1581
9-66803-3
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011571581
NSN
1560-01-157-1581
MFG
THE BOEING COMPANY DBA BOEING
Description
AIRCRAFT LOCATION: STIFFENER TIE FITTING ON NACELLE STRUT
AIRCRAFT MISSION DESIGN SERIES: KC-135
DESIGN CONTROL REFERENCE: 9-66803-3
MANUFACTURERS CODE: 81205
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-267 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL THICKNESS: 1.140 INCHES NOMINAL
OVERALL LENGTH: 5.080 INCHES NOMINAL
OVERALL WIDTH: 1.580 INCHES NOMINAL
SPECIAL FEATURES: T4 TEMPER;OPPOSITE -4
THE MANUFACTURERS DATA:
Related Searches:
4P52148-106B
SKIN,AIRCRAFT
NSN, MFG P/N
1560011571587
NSN
1560-01-157-1587
MFG
LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN
Description
DESIGN CONTROL REFERENCE: 4P52148-106B
III END ITEM IDENTIFICATION: C-5 ACFT
MANUFACTURERS CODE: 98897
SPECIAL FEATURES: USED AS PANEL ON OUTBOARD PYLON
THE MANUFACTURERS DATA:
Related Searches:
68A780614-2007
COLLAR
NSN, MFG P/N
1560011572423
NSN
1560-01-157-2423
MFG
BOEING COMPANY THE DBA BOEING
Description
DESIGN CONTROL REFERENCE: 68A780614-2007
III END ITEM IDENTIFICATION: F-15 ACFT
MANUFACTURERS CODE: 76301
THE MANUFACTURERS DATA:
Related Searches:
35-10701-2204
LONGERON
NSN, MFG P/N
1560011572430
NSN
1560-01-157-2430
MFG
THE BOEING COMPANY DBA BOEING
Description
AIRCRAFT LOCATION: 16 DEG. LONGERON ASSEMBLY,UPPER COWL PANEL ASSEMBLY
III END ITEM IDENTIFICATION: B-52
SIDE FOR WHICH DESIGNED: RIGHT SIDE
SPECIAL FEATURES: OPPOSITE ASSEMBLY -2003
Related Searches:
35-8678-2
COVER,ACCESS,AIRCRAFT
NSN, MFG P/N
1560011572550
NSN
1560-01-157-2550
MFG
THE BOEING COMPANY DBA BOEING
Description
DESIGN CONTROL REFERENCE: 35-8678-2
FSC APPLICATION DATA: GROUND STARTER ON B-52 ACFT
LENGTH: 11.200 INCHES NOMINAL
MANUFACTURERS CODE: 81205
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-362,2024-0 FED SPEC ALL MATERIAL RESPONSES
PERIPHERAL SHAPE STYLE: 119 IRREGULAR PENTAGON, FIVE HOLES
SECURING DEVICE TYPE: SPECIAL
THE MANUFACTURERS DATA:
WIDTH: 6.700 INCHES NOMINAL
Related Searches:
39-18418-3
FORMER,AIRCRAFT
NSN, MFG P/N
1560011572598
NSN
1560-01-157-2598
MFG
THE BOEING COMPANY DBA BOEING
Description
AIRCRAFT MISSION DESIGN SERIES: B-52
DESIGN CONTROL REFERENCE: 39-18418-3
MANUFACTURERS CODE: 81205
MATERIAL: ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-267,F-2.30 FED SPEC SINGLE MATERIAL RESPONSE
SPECIAL FEATURES: MADE FROM BAC 1512-3356 X .80
THE MANUFACTURERS DATA:
Related Searches:
458-50503-1
LATCH,PRESSURE RELI
NSN, MFG P/N
1560011572601
NSN
1560-01-157-2601
MFG
THE BOEING COMPANY DBA BOEING
Description
GENERAL CHARACTERISTICS ITEM DESCRIPTION: ADDITIONAL REFERENCE- FSCNM 9U774,P/N L1000-101
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III FUNCTIONAL DESCRIPTION: USED AS STRUT PRESSURE RELIEF LATCH
MANUFACTURERS CODE: 82918
MFR SOURCE CONTROLLING REFERENCE: 458-50503-2
SPEC/STD CONTROLLING DATA:
Related Searches:
458-50503-2
LATCH,PRESSURE RELI
NSN, MFG P/N
1560011572601
NSN
1560-01-157-2601
MFG
THE BOEING COMPANY DBA BOEING
Description
GENERAL CHARACTERISTICS ITEM DESCRIPTION: ADDITIONAL REFERENCE- FSCNM 9U774,P/N L1000-101
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III FUNCTIONAL DESCRIPTION: USED AS STRUT PRESSURE RELIEF LATCH
MANUFACTURERS CODE: 82918
MFR SOURCE CONTROLLING REFERENCE: 458-50503-2
SPEC/STD CONTROLLING DATA:
Related Searches:
9483-12
LATCH,PRESSURE RELI
NSN, MFG P/N
1560011572601
NSN
1560-01-157-2601
MFG
AVIBANK MFG. INC.
Description
GENERAL CHARACTERISTICS ITEM DESCRIPTION: ADDITIONAL REFERENCE- FSCNM 9U774,P/N L1000-101
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III FUNCTIONAL DESCRIPTION: USED AS STRUT PRESSURE RELIEF LATCH
MANUFACTURERS CODE: 82918
MFR SOURCE CONTROLLING REFERENCE: 458-50503-2
SPEC/STD CONTROLLING DATA:
Related Searches:
L1000-101
LATCH,PRESSURE RELI
NSN, MFG P/N
1560011572601
NSN
1560-01-157-2601
MFG
SILTEC CORP
Description
GENERAL CHARACTERISTICS ITEM DESCRIPTION: ADDITIONAL REFERENCE- FSCNM 9U774,P/N L1000-101
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III FUNCTIONAL DESCRIPTION: USED AS STRUT PRESSURE RELIEF LATCH
MANUFACTURERS CODE: 82918
MFR SOURCE CONTROLLING REFERENCE: 458-50503-2
SPEC/STD CONTROLLING DATA:
Related Searches:
65C18229-626
PANEL ASSEMBLY,DOOR
NSN, MFG P/N
1560011572602
NSN
1560-01-157-2602
MFG
THE BOEING COMPANY DBA BOEING
Description
DESIGN CONTROL REFERENCE: 65C18229-650
GENERAL CHARACTERISTICS ITEM DESCRIPTION: C/O OUTER SKIN 1 EA,INNER SKIN 1 EA,CORE 1 EA,DOUBLER 6 EA,ZEE MEMBER 4 EA; NHA 65C18229-604; OPPOSITE P/N -625
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III FUNCTIONAL DESCRIPTION: USED AS PANEL ASSEMBLY ON DOOR ASSEMBLY OF INBD STRUT TRAILING EDGE FAIRING
MANUFACTURERS CODE: 82918
THE MANUFACTURERS DATA:
Related Searches:
65C18229-650
PANEL ASSEMBLY,DOOR
NSN, MFG P/N
1560011572602
NSN
1560-01-157-2602
MFG
THE BOEING COMPANY DBA BOEING
Description
DESIGN CONTROL REFERENCE: 65C18229-650
GENERAL CHARACTERISTICS ITEM DESCRIPTION: C/O OUTER SKIN 1 EA,INNER SKIN 1 EA,CORE 1 EA,DOUBLER 6 EA,ZEE MEMBER 4 EA; NHA 65C18229-604; OPPOSITE P/N -625
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III FUNCTIONAL DESCRIPTION: USED AS PANEL ASSEMBLY ON DOOR ASSEMBLY OF INBD STRUT TRAILING EDGE FAIRING
MANUFACTURERS CODE: 82918
THE MANUFACTURERS DATA:
Related Searches:
65C18727-601
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011572606
NSN
1560-01-157-2606
65C18727-601
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011572606
NSN
1560-01-157-2606
MFG
THE BOEING COMPANY DBA BOEING
Description
DESIGN CONTROL REFERENCE: 65C18727-601
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III SUPPLEMENTARY FEATURES: FUNCTIONAL DESCRIPTION:USED AS CLAMP ASSEMBLY FOR WIRE SUPPORT ON STRUT
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: C/O 1 PAD AND 1 PLATE; PLATE-AL ALLOY SHEET 2024-T3 PER QQ-A-250/5,HEAT TREATED TO T81,4.600 IN. LG,1.600 IN. W,0.063 IN. THK; PAD-SILICONE SPONGE PER BMS1-60,TYPE 1,2.600 IN. LG,1.600 IN. W,0.500 IN. THK
THE MANUFACTURERS DATA:
Related Searches:
65C18727-601
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011572606
NSN
1560-01-157-2606
65C18727-601
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011572606
NSN
1560-01-157-2606
MFG
THE BOEING COMPANY DBA BOEING
Description
DESIGN CONTROL REFERENCE: 65C18727-601
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III SUPPLEMENTARY FEATURES: FUNCTIONAL DESCRIPTION:USED AS CLAMP ASSEMBLY FOR WIRE SUPPORT ON STRUT
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: C/O 1 PAD AND 1 PLATE; PLATE-AL ALLOY SHEET 2024-T3 PER QQ-A-250/5,HEAT TREATED TO T81,4.600 IN. LG,1.600 IN. W,0.063 IN. THK; PAD-SILICONE SPONGE PER BMS1-60,TYPE 1,2.600 IN. LG,1.600 IN. W,0.500 IN. THK
THE MANUFACTURERS DATA:
Related Searches:
65B94303-1
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011572607
NSN
1560-01-157-2607
65B94303-1
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011572607
NSN
1560-01-157-2607
MFG
THE BOEING COMPANY DBA BOEING
Description
DESIGN CONTROL REFERENCE: 65B94303-1
III END ITEM IDENTIFICATION: ACFT MODEL C/KC-135
III SUPPLEMENTARY FEATURES: FUNCTIONAL DESCRIPTION:USED AS ENGINE NOSE COWL FORWARD FAIRING SUPPORT FITTING ASSEMBLY
MANUFACTURERS CODE: 82918
SPECIAL FEATURES: C/O FITTING 1 EA,BUSHING 1 EA,PIN 1 EA,FLANGED BUSHING 2 EA,BOLT 1 EA,WASHER 2 EA
THE MANUFACTURERS DATA:
Related Searches:
68A325505-2032
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011572608
NSN
1560-01-157-2608
68A325505-2032
SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT
NSN, MFG P/N
1560011572608
NSN
1560-01-157-2608
MFG
BOEING COMPANY THE DBA BOEING
Description
(NON-CORE DATA) FSC APPLICATION DATA: AIRCRAFT STRUCTURAL COMPONENT
DESIGN CONTROL REFERENCE: 68A325505-2032
III END ITEM IDENTIFICATION: F-15 ACFT
MANUFACTURERS CODE: 76301
SPECIAL FEATURES: FUNCTION-ACCESS COVER SUPPORT; DIM.-7.000 IN. LG,7.000 IN. W,0.050 IN. THK; MATL-2024-O ALUMINUM ALLOY PER QQ-A-250/4 COND O
THE MANUFACTURERS DATA:
Related Searches:
99T26753
TUBE ASSY,INSULATED
NSN, MFG P/N
1560011573697
NSN
1560-01-157-3697
MFG
HITCO CARBON COMPOSITES INC.
Description
TUBE ASSY,INSULATED
Related Searches:
16B6508-13
COVER,ACCESS
NSN, MFG P/N
1560011573830
NSN
1560-01-157-3830
MFG
LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN DIV LOCKHEED MARTIN AERONAUTICS COMPANY
Description
DESIGN CONTROL REFERENCE: 16B6508-13
MANUFACTURERS CODE: 81755
MATERIAL: ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4-T62 FED SPEC SINGLE MATERIAL RESPONSE
PERIPHERAL SHAPE STYLE: 122 OVAL, MULTI HOLES
THE MANUFACTURERS DATA:
Related Searches:
16B6508-13
COVER,ACCESS
NSN, MFG P/N
1560011573830
NSN
1560-01-157-3830
MFG
SONACA SA
Description
DESIGN CONTROL REFERENCE: 16B6508-13
MANUFACTURERS CODE: 81755
MATERIAL: ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4-T62 FED SPEC SINGLE MATERIAL RESPONSE
PERIPHERAL SHAPE STYLE: 122 OVAL, MULTI HOLES
THE MANUFACTURERS DATA: