Socket Head Screw - Length: 5/8", Thread: 10-32, Socket Head Screw, Cadmium Plated Alloy Steel more5305000580505CategoryDescriptionEND ITEM IDENTIFICATIONW/S:AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); MISSILE, ALL-WEATHER ANTI-SHIP, HARPOON (AGM-84); TRAINER, B-1B AIRCRAFT; TORPEDO, MK-48; ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); MISSILE, AIR-TO-AIR, PHOENIX (AIM-54); ENGINE, AIRCRAFT, TF33-100 (E3A/B/C)FASTENER LENGTH0.595 INCHES MINIMUM AND 0.625 INCHES MAXIMUMHARDNESS RATING36.0 ROCKWELL C MINIMUM OVERALL AND 45.0 ROCKWELL C MAXIMUM OVERALLHEAD DIAMETER0.303 INCHES MINIMUM AND 0.312 INCHES MAXIMUMHEAD HEIGHT0.185 INCHES MINIMUM AND 0.190 INCHES MAXIMUMHEAD STYLEFLAT CHAMFERINTERNAL DRIVE STYLEHEXAGONMATERIALSTEEL OVERALLMINIMUM TENSILE STRENGTH180000 POUNDS PER SQUARE INCHMINIMUM YIELD STRENGTH155000 POUNDS PER SQUARE INCHNOMINAL THREAD DIAMETER0.190 INCHESSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONAMS-QQ-P-416, TY 2, CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALLSURFACE TREATMENTCADMIUM OVERALL AND CHROMATE OVERALLTHREAD CLASS3ATHREAD DIRECTIONRIGHT-HANDTHREAD LENGTH0.533 INCHES MINIMUM AND 0.625 INCHES MAXIMUMTHREAD SERIES DESIGNATORUNRFTHREAD QUANTITY PER INCH32SPECIFICATION/STANDARD DATA80205-NAS1357 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARDWIDTH ACROSS FLATS0.156 INCHES MINIMUM AND 0.159 INCHES MAXIMUMEND ITEM IDENTIFICATIONW/S:AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); MISSILE, ALL-WEATHER ANTI-SHIP, HARPOON (AGM-84); TRAINER, B-1B AIRCRAFT; TORPEDO, MK-48; ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); MISSILE, AIR-TO-AIR, PHOENIX (AIM-54); ENGINE, AIRCRAFT, TF33-100 (E3A/B/C)FASTENER LENGTH0.595 INCHES MINIMUM AND 0.625 INCHES MAXIMUMHARDNESS RATING36.0 ROCKWELL C MINIMUM OVERALL AND 45.0 Socket Head Screw - Length: 5/8", Thread: 10-32, Socket Head Screw, Cadmium Plated Alloy Steel 5305000580505CategoryDescriptionEND ITEM IDENTIFICATIONW/S:AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); MISSILE, ALL-WEATHER ANTI-SHIP, HARPOON (AGM-84); TRAINER, B-1B AIRCRAFT; TORPEDO, MK-48; ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); MISSILE, AIR-TO-AIR, PHOENIX (AIM-54); ENGINE, AIRCRAFT, TF33-100 (E3A/B/C)FASTENER LENGTH0.595 INCHES MINIMUM AND 0.625 INCHES MAXIMUMHARDNESS RATING36.0 ROCKWELL C MINIMUM OVERALL AND 45.0 ROCKWELL C MAXIMUM OVERALLHEAD DIAMETER0.303 INCHES MINIMUM AND 0.312 INCHES MAXIMUMHEAD HEIGHT0.185 INCHES MINIMUM AND 0.190 INCHES MAXIMUMHEAD STYLEFLAT CHAMFERINTERNAL DRIVE STYLEHEXAGONMATERIALSTEEL OVERALLMINIMUM TENSILE STRENGTH180000 POUNDS PER SQUARE INCHMINIMUM YIELD STRENGTH155000 POUNDS PER SQUARE INCHNOMINAL THREAD DIAMETER0.190 INCHESSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONAMS-QQ-P-416, TY 2, CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALLSURFACE TREATMENTCADMIUM OVERALL AND CHROMATE OVERALLTHREAD CLASS3ATHREAD DIRECTIONRIGHT-HANDTHREAD LENGTH0.533 INCHES MINIMUM AND 0.625 INCHES MAXIMUMTHREAD SERIES DESIGNATORUNRFTHREAD QUANTITY PER INCH32SPECIFICATION/STANDARD DATA80205-NAS1357 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARDWIDTH ACROSS FLATS0.156 INCHES MINIMUM AND 0.159 INCHES MAXIMUMEND ITEM IDENTIFICATIONW/S:AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); MISSILE, ALL-WEATHER ANTI-SHIP, HARPOON (AGM-84); TRAINER, B-1B AIRCRAFT; TORPEDO, MK-48; ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); MISSILE, AIR-TO-AIR, PHOENIX (AIM-54); ENGINE, AIRCRAFT, TF33-100 (E3A/B/C)FASTENER LENGTH0.595 INCHES MINIMUM AND 0.625 INCHES MAXIMUMHARDNESS RATING36.0 ROCKWELL C MINIMUM OVERALL AND 45.0 ROCKWELL C MAXIMUM OVERALLHEAD DIAMETER0.303 INCHES MINIMUM AND 0.312 INCHES MAXIMUM less
友情提醒：产品介绍及参数仅供参考，如需该件号：NAS1351-3-10P 的详细技术规格，请随时联系我们>>>，航空器材网将为您提供精准的技术支持和解决方案。
规格：
|
Sold In
|
N/A
Per Package
|
|
Inventory
|
0
|
|
Estimated Ship Date
|
Ships within 10-14 days
|
|
Thread Size
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N/A
0.1900-32
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|
Material
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N/A
Steel Alloy
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|
Length
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N/A
5/8 in
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|
Drilling
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N/A
Undrilled 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
NAS1351
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Weight
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N/A
.005 lb
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|
Alternate Part Number
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N/A
Possible
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|
NSN
|
N/A
5305-00-058-0505 5305-00-891-5519
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|
NIIN
|
N/A
00-058-0505 00-891-5519
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|
Part # Unpunctuated
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N/A
NAS1351310P
|
|
Minimum Order Note
|
N/A
Minimum order is 10. Must order in increments of 1.
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|
Country of Origin
|
N/A
USA
|
特征： | 5305000580505 | | Category | Description | | END ITEM IDENTIFICATION | W/S:AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); MISSILE, ALL-WEATHER ANTI-SHIP, HARPOON (AGM-84); TRAINER, B-1B AIRCRAFT; TORPEDO, MK-48; ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); MISSILE, AIR-TO-AIR, PHOENIX (AIM-54); ENGINE, AIRCRAFT, TF33-100 (E3A/B/C) |
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