# Tecnam Service Bulletin 128-CS: No revision named - Rights: © Tecnam. Filed by the FAA in regulations.gov docket FAA-2013-0888; AD 2014-02-07 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Tecnam Service Bulletin 128-CS](https://openairdocs.org/service-documents/tecnam/128-cs.md) - Title as filed: U.S. DOT/FAA - SB 128 - CS - P2006T Lower link inspection - replacement - ed1r0 - Pages: 3 - PDF: https://openairdocs.org/files/sha256/d0/ec/d0ecab9a2d5c1f2bb4de15f566f666dd15a963add9ef78acce5eda18140dfc5d - Page: https://openairdocs.org/service-documents/tecnam/128-cs/file/d0ecab9a2d5c ## Text Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 SERVICE BULLETIN N° SB 128 – CS – Rev0 The technical content of this document is approved under the authority of DOA. EASA.21J.335 Approval No. DO-128-130422 15th May 2013 Page 1 / 3 Edition 1 Rev.0 INFORMATION  RECOMMENDED  MANDATORY  SUBJECT: P2006T Lower link inspection/replacement, as applicable SCOPE: During an inspection of a P2006T, on the NLG lower link two cracks were found. The part involved is related to old link assy (P/N 26-8-1417-000), replaced by SB-104-CS, whatever revi- sion. Tecnam prescribes to perform a dedicated inspection on NLG lower link (P/N 26-8-1417-1) on airplanes which don’t embody SB104-CS, whatever revision, within the terms herein reported. Additionally Tecnam prescribes, at same time, to apply the KIT SB128-CS (which includes new link assy P/N 26 -8-8000-000) to all P2006T airplanes which don’t embody SB 104 -CS Ed.2 Rev. 1. This SB supersedes SB 104-CS Ed.2 Rev.1 Nevertheless, Tecnam reminds owners/operator s to respect the scheduled maintenance program as provided by AMM, chapters 04 and 05. MODELS AFFECTED: All P2006T airplanes, which don’t embody the SB 104- CS Ed.2 Rev.1 TIME OF COMPLIANCE: Inspection, if applicable, to be performed within the next 25 flight hours or 30 days (whichever occurs first) after the issue date of this SB. Replacement to be performed within the next 50 flight hours or 60 days (whichever occurs first) after the issue date or this SB. MANPOWER: 6 man-hours. REQUIRED MATERIAL: KIT no. SB128-CS, including:  KIT no. SB 104-CS (Job card no. 442) if not embodied yet;  KIT no. SB 104-CS/2 (Job card no. 528);  KIT no. SB 109-CS (Job card no. 468) if not embodied yet. TOOLING: Nil WEIGHT AND BALANCE: Nil REFERENCES: P2006T Maintenance Manual doc. no. 2006/45 – last issue; P2006T Aircraft Parts Catalogue doc. no. 2006/46 – last issue; PUB. AFFECTED: Nil ### Page 2 SERVICE BULLETIN N° SB 128 – CS – Rev0 The technical content of this document is approved under the authority of DOA. EASA.21J.335 Approval No. DO-128-130422 15th May 2013 Page 2 / 3 Edition 1 Rev.0 INSPECTION/REPLACEMENT INSTRUCTIONS (as applicable) 1. Aircraft preparation 1) Park the aircraft in a closed hangar; 2) Make sure that landing gear is down and locked (Master Switch ON: LG advisory lights must be ON); 3) MASTER SWITCH: OFF; 4) STARTER RELAY BREAKER: OFF; 5) PARKING BRAKE: ON; 2. Inspect nose landing gear lower link 1) Remove the inspection cap F2 (refer to P2006T AMM, ATA 6) 2) Identify the Lower link (see following figure 1); 3) Visually inspect both sides of the lower link for cracks and deformation; Figure 1 – Inspection item If a crack was found complete the occurrence report hereby attached and send it Tecnam. 3. Terminating action - Kit no. SB 128-CS installation 1) Follow instructions contained in the applicable kit/s and perform scheduled maintenance as provided by AMM, chapters 04 and 05. Record the application of the present Service Bulletin on the aircraft log-book. For further information please contact TECNAM: Tel 0039 0823 620134 Fax 0039 0823 622899 E-mail airworthiness@tecnam.com ### Page 3 Occurrence Report Date: Aircraft Type: Engine No.1 type: Serial No. “ Serial No. Registration markings: “ Time Since New: A/C Time Since New: “ Time Since Overhaul: “ Cycles since new: “ Cycles since new Affected Item (if applicable) Engine No.2 type: “ ATA Chapter “ Serial No. “ Time Since New: “ Time Since New: “ Time Since Overhaul: “ Time Since Overhaul: “ Cycles since new: “ Cycles since new: Place: Operator’s name: “ contacts: Ph: Fax. “ contact person: Mobile: Description: List of Damaged areas: Operator’s Preliminary Investigation No. of died persons: Hull loss: No. of injured persons AOG: Acc./s.Inc./Inc (ICAO A13) - - Possible cause: Action to be done: Action taken: Operators must fill this “Occurrence Report” as soon as possible and send preferably via e -mail to the TECNAM Office of Airworthiness: airworthiness@tecnam.com . Eventually by fax: +39 081 7584528 or express courier: 1°trav. Via Giovanni Pascoli n°1 Casoria (NA) 80026 ITALY ANY MATERIAL AVAILABLE LIKE PHOTO, VIDEO, DRAWINGS ETC. IS WELCOME. Disclaimer: Costruzioni Aeronautiche TECNAM s.r.l. declines any responsibility for late, incomplete or not-true information provided. Using of this form for occurrence reporting is mandatory as per Tecnam/DOA procedures. Tecnam will adopt the date and hour of receiving of this form duly filled as a reference in later pertinent activities. While filling this form: fields not applicable must not be left blank but marked with n.a. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.