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Aerospace extrusion · AND10141 series

AND10141-1402

Tee - Bulb aluminium extrusion · 1.5 × 1.125 in (38.1 × 28.575 mm)

2024 · 6061 · 7075Full material certificationAS9120B approved
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AND10141-1402 Aluminum Tee - Bulb extrusion profile diagram
Aluminum Tee - Bulb – typical profile. Dimensions for AND10141-1402 below.

AND10141-1402 Tee - Bulb Aluminium Extrusion

AND10141-1402 is an aerospace aluminium tee - bulb extrusion with nominal dimensions of 1.5 × 1.125 in (38.1 × 28.575 mm) and a 90° included angle. It is part of the AND10141 series of standard aircraft extrusion shapes. Aerocom Metals can source AND10141-1402 in the alloy, temper and length you need, supplied with full material certification and traceability from our AS9120B and ISO 9001:2015 approved quality system.

A1.5"38.1 mm
B1.125"28.575 mm
T10.06"1.524 mm

AND10141-1402 dimensions

ABCDTT1T2T3RR1R2R3R4R5Deg.
1.51.1250.1880.060.050.0940.060.010.09490. 00

AND10141-1402 specification summary

Part numberAND10141-1402
Standard / seriesAND10141
ProfileTee - Bulb
Dimension A1.5 in (38.1 mm)
Dimension B1.125 in (28.575 mm)
Dimension D0.188 in (4.7752 mm)
Dimension T10.06 in (1.524 mm)
Dimension T20.05 in (1.27 mm)
Dimension R0.094 in (2.3876 mm)
Dimension R10.06 in (1.524 mm)
Dimension R20.01 in (0.254 mm)
Dimension R30.094 in (2.3876 mm)
Angle90°
MaterialAerospace aluminium alloys – typically 2024, 6061 and 7075
Typical tempers2024-T3511, 6061-T6511, 7075-T6511, 7075-T73511 and O (annealed)
Material specificationsAMS-QQ-A-200/3 (2024), AMS-QQ-A-200/8 (6061), AMS-QQ-A-200/11 (7075), AMS4165 and equivalents
SupplyMill lengths or cut to length on request
CertificationSupplied with material test certificates and full traceability (AS9120B / ISO 9001:2015)

Alloy, temper and specification are confirmed at quotation to suit your drawing requirements.

About the AND10141 series

AND10141 is an Army-Navy (AN) drawing standard covering extruded aluminium bulb tee sections for aircraft structures. Each dash number defines a specific cross-section size, and the shape is commonly supplied in 2024, 6061 and 7075 aluminium alloys in tempered or annealed (O) condition.

Choosing an alloy for AND10141-1402

2024 is a high-strength aluminium-copper alloy with excellent fatigue resistance, widely used for fuselage stringers, frames and wing structure, usually supplied as 2024-T3511. 7075 is one of the strongest aluminium alloys, used for highly stressed structural parts; 7075-T73511 offers improved resistance to stress corrosion cracking. 6061 combines good strength with excellent corrosion resistance and weldability, making it a common choice for secondary structure and interiors. Read more in our 2024, 7075 and 6061 guides.

Request a quote for AND10141-1402

Tell us the alloy, temper, quantity and lengths you need for AND10141-1402 and our team will come back with price and lead time. Email [email protected], call +44 (0) 2476 645 551 or use the enquiry form below.

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