Using the Request for Quote (RFQ) form provided on this page, you can request competitive procurement options on part number L5301158-003 with rapid responses always offered by our staff. To ensure that you locate and procure exactly what you need with ease, we list parts with as much information as we can. For example, part number L5301158-003 It is listed as Screw Shoulder. component manufactured by Boeing Company The, specifically under CAGE Code 43999. It is also accompanied by the NSN 5305016059163 for ease of organization, the first digits of the NSN indicating that the part belongs to FSC 5305 Screws.
NSN Information for Part Number L5301158-003 with NSN 5305-01-605-9163, 5305016059163
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5305-01-605-9163 Item Description: Screw Shoulder | 5305 | 016059163 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
L5301158-003 | 5 | 2 | 3 |
Characteristics Data of NSN 5305-01-605-9163, 5305016059163
MRC | Criteria | Characteristic |
---|---|---|
AAJF | THREAD DIRECTION | RIGHT-HAND |
AASK | HEAD STYLE | FLAT CHAMFER |
AASL | HEAD DIAMETER | 1.000 INCHES NOMINAL |
AATX | SHOULDER LENGTH | 1.250 INCHES NOMINAL OVERALL |
AHYM | NOMINAL THREAD DIAMETER | 0.500 INCHES |
ASDB | WIDTH ACROSS FLATS | 0.500 INCHES MINIMUM AND 0.504 INCHES MAXIMUM |
CSYT | CHAMFER ANGLE | 45.0 DEGREES NOMINAL |
MATT | MATERIAL | TITANIUM OVERALL |
THSD | THREAD SERIES DESIGNATOR | UNJF |
AAJD | THREAD CLASS | 3A |
AASA | THREAD LENGTH | 0.060 INCHES MAXIMUM |
AASB | FASTENER LENGTH | 2.060 INCHES NOMINAL |
AASU | HEAD HEIGHT | 0.156 INCHES NOMINAL |
AATN | SHOULDER DIAMETER | 0.735 INCHES MINIMUM AND 0.750 INCHES MAXIMUM OVERALL |
ABQZ | INTERNAL DRIVE STYLE | HEXAGON |
AGAV | END ITEM IDENTIFICATION | B1-B ACFT |
CMLP | THREAD QUANTITY PER INCH | 20 |
CWYB | SHOULDER SHAPE | ROUND OVERALL |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BOLT, TRUNNION-INSTRUMENT PANEL FLAT STA |