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Technical Data Sheet
PartsTable / COMPONENT / 35-35424-2
35-35424-2 ✓ Verified by PartsTable
— · PIPE SECTION
WHAT YOU NEED TO KNOW
Schedule = wall thickness, NOT diameter Nominal pipe size != actual OD
Sch 40 and Sch 80 same OD, different wall
PRODUCT OVERVIEW

The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include aircraft_mission_design_series: KC-135. This product is currently in active production with full OEM support.

This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 4710-00-073-3209, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS
35-35424-2
NSN: 4710-00-073-3209
FSC: 4710
CAGE: 13446 — PERKINS ENGINES INC (USA)
SPECIFICATIONS
aircraft_mission_design_seriesKC-135
NSN4710-00-073-3209
COMPONENT DIAGRAM
PIPE SECTION — SCHEDULE = WALL THICKNESS WALL: — OD: — LENGTH: — — — PN: 35-35424-2 · OEM ⚠ VERIFY BEFORE ORDERING Schedule = wall thickness, NOT pipe diameter. Sch 40 and Sch 80 have the same OD but different wall thickness. Nominal pipe size ≠ actual OD — a 1" pipe is actually 1.315" OD ✓ BROKER TIP Sch 40 = standard wall, Sch 80 = heavy wall (higher pressure), Sch 160 = extra heavy. Seamless pipe is required for high-pressure applications — welded pipe has lower ratings PARTSTABLE TECHNICAL DRAWING — NOT TO SCALE
KEY FEATURES
•
NOMINAL THREAD SIZE: 0.500 INCHES SINGLE END IN
•
THREAD SERIES DESIGNATOR: UNS SINGLE END
•
TUBE OUTSIDE DIAMETER: 0.250 INCHES NOMINAL IN
•
MATERIAL: STEEL SINGLE END
•
WALL THICKNESS: 0.072 INCHES NOMINAL IN
•
END CONNECTION STYLE: SWIVEL NUT, COMPRESSION SINGLE END
•
SEAT RADIUS: 0.125 INCHES NOMINAL SINGLE END IN
TECHNICAL CHARACTERISTICS (FLIS)
NOMINAL THREAD SIZE0.500 INCHES SINGLE END IN
THREAD SERIES DESIGNATORUNS SINGLE END
TUBE OUTSIDE DIAMETER0.250 INCHES NOMINAL IN
MATERIALSTEEL SINGLE END
MATERIALSTEEL TUBING
WALL THICKNESS0.072 INCHES NOMINAL IN
END CONNECTION STYLESWIVEL NUT, COMPRESSION SINGLE END
SEAT RADIUS0.125 INCHES NOMINAL SINGLE END IN
THREAD CLASS3B SINGLE END
DESIGN FORMPREBENT
VERIFIED SUBSTITUTES & CROSS-REFERENCES 8
1-2645Interchangeable
interchangeable cross-reference
interchangeable
15905Interchangeable
interchangeable cross-reference
interchangeable
35-35424-2Interchangeable
interchangeable cross-reference
interchangeable
H01226Interchangeable
interchangeable cross-reference
interchangeable
012645Interchangeable
interchangeable cross-reference
interchangeable
K-RV15LInterchangeable
interchangeable cross-reference
interchangeable
LIFECYCLE
StatusACTIVE
AvailabilityOEM and secondary market
RoHS CompliantEAR99Not HAZMAT
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FREQUENTLY ASKED QUESTIONS
What is 35-35424-2?
35-35424-2 is a FORMER,AIRCRAFT.
What parts can replace 35-35424-2?
There are 8 known substitutes for 35-35424-2: 1-2645, 15905, 35-35424-2 and 5 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 35-35424-2?
35-35424-2 is cataloged in the Federal Logistics Information System (FLIS) under NSN 4710-00-073-3209. This indicates validated use in U.S. government and defense supply chains.
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✓ Validated with multiple authoritative sources, including Government, OEM, and Certified sources.
PartsTable Design LLC · partstable.com
Last verified: July 2026