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Socket Head Screw - NAS1352-06H6P
NAS1352-06H6P 8/15/2024
零售价: 请询价
数量:库存充足 状态:
品牌: 类别:螺钉
地点:上海

商家信息

易材航空科技(上海)有限公司

姓名:

Alice 17821328436

电话:

17821328436

邮箱:

alice@airparts.cn

网址:

地址:

中国﹒上海市浦东新区浩宇路919号一谷一园大厦318

产品名称:
型号:
供应商:
所在地:
发布时间: 8/15/2024
供应商信息
公司名称:易材航空科技(上海)有限公司
地址:中国﹒上海市浦东新区浩宇路919号一谷一园大厦318
邮编:
网址:
联系人:Alice 17821328436
电话:
传真:
邮箱:alice@airparts.cn
详细介绍
技术参数
相关文件
Socket Head Screw - Length: 3/8", Thread: 6-32, Socket Head Screw, Drilled Head, Cadmium Plated Alloy Steel more 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 less

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