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NAS1581 GA Screws

From $0.36 to $2.60
NAS1581 Dash No. Material Heat Treat Finish Grip Length Part Number Price Buy
F3T2 Plain CruciformAlloy Steel (8740)160,000 - 180,000 PSICadmium Per Ams QQ-P-416 TYPE II0.1250.487
NAS1581F3T2
$0.77
Quantity
F3T3 Plain CruciformAlloy Steel (8740)160,000 - 180,000 PSICadmium Per Ams QQ-P-416 TYPE II0.1870.549
NAS1581F3T3
$0.70
Quantity
F3T4 Plain CruciformAlloy Steel (8740)160,000 - 180,000 PSICadmium Per Ams QQ-P-416 TYPE II0.2500.613
NAS1581F3T4
$0.48
Quantity
F3T5 Plain CruciformAlloy Steel (8740)160,000 - 180,000 PSICadmium Per Ams QQ-P-416 TYPE II0.3120.675
NAS1581F3T5
$0.36
Quantity
F3T8 Plain CruciformAlloy Steel (8740)160,000 - 180,000 PSICadmium Per Ams QQ-P-416 TYPE II0.5000.863
NAS1581F3T8
$0.37
Quantity
F3R2 Ribbed CruciformAlloy Steel (8740)160,000 - 180,000 PSICadmium Per Ams QQ-P-416 TYPE II0.1250.487
NAS1581F3R2
$0.77
Quantity
F3R3 Ribbed CruciformAlloy Steel (8740)160,000 - 180,000 PSICadmium Per Ams QQ-P-416 TYPE II0.1870.549
NAS1581F3R3
$0.70
Quantity
F3R4 Ribbed CruciformAlloy Steel (8740)160,000 - 180,000 PSICadmium Per Ams QQ-P-416 TYPE II0.2500.613
NAS1581F3R4
$0.40
Quantity
C3T2Cres. (A-286)160,000 - 190,000 PSIPassivate Per Ams 27000.1250.487
NAS1581C3T2
$2.60
Quantity
C3T3Cres. (A-286)160,000 - 190,000 PSIPassivate Per Ams 27000.1870.549
NAS1581C3T3
$1.06
Quantity
C3T4Cres. (A-286)160,000 - 190,000 PSIPassivate Per Ams 27000.2500.613
NAS1581C3T4
$0.88
Quantity
Subtotal $0.00
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Overview

Offset Cruciform 100 Deg Flush Head

Material - Alloy Steel (8740) or Cres. (A-286)
Heat Treat - 160,000 - 180,000 PSI or 160,000 - 190,000 PSI
Finish - Cadmium Per AmsQQ-P-416 TYPE II or Passivate Per Ams2700

Thread: 10-32
   
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WARNING: Cancer and Reproductive Harm - www.P65Warnings.ca.gov.

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Please note, Aircraft Spruce's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.

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