Socket Head Screw - Length: 3/8", Thread: 6-32, Socket Head Screw, Drilled Head, Cadmium Plated Alloy Steel
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Detail
Characteristic
END ITEM IDENTIFICATIONW/S:HELICOPTER, MH-53E; AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIRCRAFT, OSPREY V-22A, AIR FORCE; HELICOPTER, CARRIER BASED ASW, SH-60F; HELICOPTER, SEARCH AND RESCUE, HH-60H; AIRCRAFT, OSPREY V-22A, MARINE CORPS; AIRCRAFT, AIRLIFTER C-17A; ENGINE, AIRCRAFT, TF-33-P-7 (C-1411A/B); HELICOPTER, ADVANCE ATTACK, AH-1WFASTENER LENGTH0.345 INCHES MINIMUM AND 0.375 INCHES MAXIMUMHARDNESS RATING38.0 ROCKWELL C MINIMUM OVERALL AND 45.0 ROCKWELL C MAXIMUM OVERALLHEAD DIAMETER0.218 INCHES MINIMUM AND 0.226 INCHES MAXIMUMHEAD HEIGHT0.134 INCHES MINIMUM AND 0.138 INCHES MAXIMUMHEAD STYLEFLAT CHAMFERHOLE CONFIGURATION STYLEROUND INTERNAL HEXAGONHOLE DIAMETER0.036 INCHES NOMINALHOLE TYPEDRILLEDHOLE QUANTITY2INTERNAL DRIVE STYLEHEXAGONNONDEFINITIVE SPEC/STD DATA6 TYPEMATERIAL DOCUMENT AND CLASSIFICATION66 FED STD SINGLE MATERIAL RESPONSE OVERALLMATERIALSTEEL OVERALLMINIMUM TENSILE STRENGTH180000 POUNDS PER SQUARE INCHMINIMUM YIELD STRENGTH155000 POUNDS PER SQUARE INCHNOMINAL THREAD DIAMETER0.138 INCHESSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-416 TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALLSURFACE TREATMENTCADMIUM OVERALL AND CHROMATE OVERALLTHREAD CLASS3ATHREAD LENGTH0.283 INCHES MINIMUMTHREAD DIRECTIONRIGHT-HANDTHREAD SERIES DESIGNATORUNCTHREAD QUANTITY PER INCH32SPECIFICATION/STANDARD DATA80205-NAS1352 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARDWIDTH ACROSS FLATS0.109 INCHES MINIMUM AND 0.111 INCHES MAXIMUMEND ITEM IDENTIFICATIONW/S:HELICOPTER, MH-53E; AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIRCRAFT, OSPREY V-22A, AIR FORCE; HELICOPTER, CARRIER BASED ASW, SH-60F; HELICOPTER, SEARCH AND RESCUE, HH-60H; AIRCRAFT, OSPREY V-22A, MARINE CORPS; AIRCRAFT, AIRLIFTER C-17A; ENGINE, AIRCRAFT, TF-33-P-7 (C-1411A/B); HELICOPTER, ADVANCE ATTACK, AH-1WFASTENER LENGTH0
Socket Head Screw - Length: 3/8", Thread: 6-32, Socket Head Screw, Drilled Head, Cadmium Plated Alloy Steel
Detail
Characteristic
END ITEM IDENTIFICATIONW/S:HELICOPTER, MH-53E; AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIRCRAFT, OSPREY V-22A, AIR FORCE; HELICOPTER, CARRIER BASED ASW, SH-60F; HELICOPTER, SEARCH AND RESCUE, HH-60H; AIRCRAFT, OSPREY V-22A, MARINE CORPS; AIRCRAFT, AIRLIFTER C-17A; ENGINE, AIRCRAFT, TF-33-P-7 (C-1411A/B); HELICOPTER, ADVANCE ATTACK, AH-1WFASTENER LENGTH0.345 INCHES MINIMUM AND 0.375 INCHES MAXIMUMHARDNESS RATING38.0 ROCKWELL C MINIMUM OVERALL AND 45.0 ROCKWELL C MAXIMUM OVERALLHEAD DIAMETER0.218 INCHES MINIMUM AND 0.226 INCHES MAXIMUMHEAD HEIGHT0.134 INCHES MINIMUM AND 0.138 INCHES MAXIMUMHEAD STYLEFLAT CHAMFERHOLE CONFIGURATION STYLEROUND INTERNAL HEXAGONHOLE DIAMETER0.036 INCHES NOMINALHOLE TYPEDRILLEDHOLE QUANTITY2INTERNAL DRIVE STYLEHEXAGONNONDEFINITIVE SPEC/STD DATA6 TYPEMATERIAL DOCUMENT AND CLASSIFICATION66 FED STD SINGLE MATERIAL RESPONSE OVERALLMATERIALSTEEL OVERALLMINIMUM TENSILE STRENGTH180000 POUNDS PER SQUARE INCHMINIMUM YIELD STRENGTH155000 POUNDS PER SQUARE INCHNOMINAL THREAD DIAMETER0.138 INCHESSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-416 TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALLSURFACE TREATMENTCADMIUM OVERALL AND CHROMATE OVERALLTHREAD CLASS3ATHREAD LENGTH0.283 INCHES MINIMUMTHREAD DIRECTIONRIGHT-HANDTHREAD SERIES DESIGNATORUNCTHREAD QUANTITY PER INCH32SPECIFICATION/STANDARD DATA80205-NAS1352 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARDWIDTH ACROSS FLATS0.109 INCHES MINIMUM AND 0.111 INCHES MAXIMUMEND ITEM IDENTIFICATIONW/S:HELICOPTER, MH-53E; AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIRCRAFT, OSPREY V-22A, AIR FORCE; HELICOPTER, CARRIER BASED ASW, SH-60F; HELICOPTER, SEARCH AND RESCUE, HH-60H; AIRCRAFT, OSPREY V-22A, MARINE CORPS; AIRCRAFT, AIRLIFTER C-17A; ENGINE, AIRCRAFT, TF-33-P-7 (C-1411A/B); HELICOPTER, ADVANCE ATTACK, AH-1WFASTENER LENGTH0.345 INCHES MINIMUM AND 0.375 INCHES MAXIMUMHARDNESS RATING38.0 ROCKWELL C MINIMUM OVERALL AND 45.0 ROCKWELL C MAXIMUM OVERALLHEAD DIAMETER0.218 INCHES MINIMUM AND 0.226 INCHES MAXIMUMHEAD HEIGHT0.134 INCHES MINIMUM AND 0.138 INCHES MAXIMUMHEAD STYLEFLAT CHAMFERHOLE CONFIGURATION STYLEROUND INTERNAL HEXAGONHOLE DIAMETER0.036 INCHES NOMINALHOLE TYPEDRILLEDHOLE QUANTITY2INTERNAL DRIVE STYLEHEXAGONNONDEFINITIVE SPEC/STD DATA6 TYPEMATERIAL DOCUMENT AND CLASSIFICATION66 FED STD SINGLE MATERIAL RESPONSE OVERALLMATERIALSTEEL OVERALLMINIMUM TENSILE STRENGTH180000 POUNDS PER SQUARE INCHMINIMUM YIELD STRENGTH155000 POUNDS PER SQUARE INCHNOMINAL THREAD DIAMETER0.138 INCHESSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-416 TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALLSURFACE TREATMENTCADMIUM OVERALL AND CHROMATE OVERALLTHREAD CLASS3ATHREAD LENGTH0.283 INCHES MINIMUMTHREAD DIRECTIONRIGHT-HANDTHREAD SERIES DESIGNATORUNCTHREAD QUANTITY PER INCH32SPECIFICATION/STANDARD DATA80205-NAS1352 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARDWIDTH ACROSS FLATS0.109 INCHES MINIMUM AND 0.111 INCHES MAXIMUM
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规格:
Sold In
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N/A
Per Package
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Inventory
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0
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Estimated Ship Date
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N/A
Ships in 1 Business Day
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Thread Size
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N/A
0.1380-32
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Material
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N/A
Steel Alloy
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Length
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N/A
3/8 in
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Drilling
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N/A
Drilled Head
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Head Type
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N/A
Socket
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Industry Standards/Certification
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N/A
NAS1352
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Weight
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N/A
0.002 lb
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Alternate Part Number
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N/A
MS24677-7 MS24677-7
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NSN
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N/A
5305-00-058-2067
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NIIN
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N/A
00-058-2067
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Part # Unpunctuated
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N/A
NAS135206H6P
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Minimum Order Note
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N/A
Minimum order is 10. Must order in increments of 1.
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Country of Origin
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N/A
USA
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特征:
Detail
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Characteristic
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END ITEM IDENTIFICATION | W/S:HELICOPTER, MH-53E; AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIRCRAFT, OSPREY V-22A, AIR FORCE; HELICOPTER, CARRIER BASED ASW, SH-60F; HELICOPTER, SEARCH AND RESCUE, HH-60H; AIRCRAFT, OSPREY V-22A, MARINE CORPS; AIRCRAFT, AIRLIFTER C-17A; ENGINE, AIRCRAFT, TF-33-P-7 (C-1411A/B); HELICOPTER, ADVANCE ATTACK, AH-1W | FASTENER LENGTH | 0.345 INCHES MINIMUM AND 0.375 INCHES MAXIMUM | HARDNESS RATING | 38.0 ROCKWELL C MINIMUM OVERALL AND
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