SAIB CE-04-20
Current · Issued 11/20/2003 · SOCATA TBM 700 · FAA DRS
SAIB CE-04-20 — Open on drs.faa.gov ↗
The FAA-published PDF is the authoritative source.
Bulletin text · verbatim from the FAA PDF · 13 paragraphs · 261 words
No. CE-04-20 November 20,2003 www.faa.gov - Search "SAIBs" This is information only. Recommendations aren’t mandatory.
Introduction
This Special Airworthiness Information Bulletin alerts you, owners and operators of SOCATA Model TBM 700 airplanes, that SOCATA has issued Service Bulletin (SB) No. SB 70-102, titled “Check and Correction of C6 and C8 Cross – Beam Bolt Tightening”, dated April 2003. The SB notifies owners and operators of a rotating cross-beam bolt due to insufficient torque applied at the time of production.
Background
The French DGAC has issued an Airworthiness Directive (AD) 2003-271(A), dated July 23, 2003, referencing the SB. SOCATA listed the SB as “Mandatory” for aircraft serial numbers 121-159, 161-211, 213-239, and 241-249.
Recommendation
We aren’t issuing an AD at this time, but highly recommend that you accomplish the inspections per the required compliance time in the SB.
For Further Information Contact
Gunnar Berg, Aerospace Engineer, FAA Small Airplane Directorate, ACE-112, 901 Locust, Room 301, Kansas City, MO 64106. Telephone: (816)-329-4059, Fax: (816)-329-4090; email: [email protected]
Contact SOCATA for copies of the SB at EADS SOCATA, Direction des Services, 65921 Tarbes Cedex 9, France; phone: 33 (0) 5 62.41.73.00; fax: 33 (0) 5 62.41.76.54; telex: 532 835 F.
Internet Connection
For Internet downloads, of SOCATA SB go to http://www.socata.eads.net ;highlight SUPPORT; click on ONLINE DOCS; fill out first name, last name, country, and your e-mail address; click on CONTINUE.
The SOCATA Users Group Organization go to http://socata.org/ and click on RESOURCES. Select Online SB or SL Index from there select the SB or SL that you need for your make and model airplane.