Tubing Type | O.D. (In.) | Wall (In.) | Part No. |
---|---|---|---|
304 Seamless | 3/8 | .035 | 03-16045-7 |
If manufacturing test reports are required, there is a minimum $15.00 charge per order. Please indicate in the special instructions box at the time of order that certs are required. |
Great material and service is always top notch!
Good material and nice finish
I always get tubing from aircraft spruce. Its great quality and arrives at my house in less than 2 days.
Have bought this tubing in many sizes . Bends and flares nicely . I will buy more . Shipping is very fast .
Was presented and arrived on time
As advertised
Please note, Aircraft Spruce Australia'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 Australia 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.
Yes, but a heavy duty flaring tool designed for stainless steel must be used.
Yes, it is annealed material.
Yes, Part # 03-16560 tubing is annealed.
The ID can be calculated as the OD minus the Wall Thickness. 03-16540 has ID 1.222" and 03-16300 has ID 1.715".
Yes, we can coil 304 up to 3/8 inch thickness for shipping. Be advised that requesting this material coiled makes the material final sale. We will not accept returns on coiled 304.
Yes, this is printed on the tubing.
Its cold drawn and seamless so we would imagine it would be fit for pressurized use, but we cannot comment on its particular application for aerospace fuel lines. The customer needs to make this determination. The working pressure is 8800 PSI, and bust pressure 13,700PSI. This is a safety factor of 1.0.