SERVICE BULLETIN N° SB 138 – CS – Rev0
TECNAM P2006T · Service Bulletins
Overview
This service bulletin outlines the inspection requirements for the engine mount of the Tecnam P2006T aircraft. It is mandatory for all P2006T airplanes with more than 600 flight hours to perform this inspection within a specified timeframe due to a discovered crack.
- Mandatory inspection for P2006T engine mount.
- Applicable to all P2006T airplanes with over 600 flight hours.
- Inspection must be completed within 25 hours or 30 days.
- Inspection requires visual checks for cracks and deformation.
- No special tools or materials are needed for the inspection.
- Operators must report any cracks found to Tecnam.
- Record the application of the service bulletin in the aircraft log-book.
- Contact Tecnam for further information.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at regulations.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Service Bulletins
- Year ·
- 2013
- File size ·
- 118 KB
- Copy found at ·
- regulations.gov
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Tooling ·
- Nil
- Required material ·
- Nil
What is the SERVICE BULLETIN N° SB 138 – CS – Rev0?
The SERVICE BULLETIN N° SB 138 – CS – Rev0 is a service bulletins for the TECNAM P2006T, dated 2013.
What year was the SERVICE BULLETIN N° SB 138 – CS – Rev0 published?
The SERVICE BULLETIN N° SB 138 – CS – Rev0 — the TECNAM P2006T service bulletins on file — is dated 2013.
Common. More common than 89% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the TECNAM P2006T.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Subject
P2006T Engine Mount inspection due to a crack found during a 100hr inspection.
Models Affected
All P2006T airplanes having more than 600 flight hours.
Time of Compliance
Inspection must be completed within the next 25 hours or 30 days after the issue date.
Inspection Instructions
Detailed steps for aircraft preparation and engine mount inspection.
Occurrence Report
Instructions for reporting any cracks found during inspection.
Contact Information
Contact details for Tecnam's Airworthiness office for further assistance.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Inspect engine mounts for cracks and deformation.
- Report any cracks found to Tecnam immediately.
- Ensure aircraft is parked in a closed hangar during inspection.
- Follow all preparation steps before inspection.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
SERVICE BULLETIN N° SB 138 – CS – Rev0 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No. DO-138-131121 25 th November 2013 Page 1 / 3 Edition 1 Rev.0 INFORMATION RECOMMENDED MANDATORY SUBJECT: P2006T Engine Mount inspection SCOPE : During a 100hr inspection of a P2006T, on a node of the engine mount (P/N 26-7-1200-000) a crack was found. Tecnam prescribes to perform a dedicated inspection on this item for all P2006T airplanes having more than 600 flight hours within the terms herein reported. MODELS AFFECTED: All P2006T airplanes, having more than 600 flight hours. TIME OF COMPLIANCE: Within the next 25 hours or 30 days (whichever occurs first) af- ter the issue date of this SB for airplanes with more than 600 flight hours. MANPOWER: 1 man-hour. REQUIRED MATERIAL: Nil 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 SERVICE BULLETIN N° SB 138 – CS – Rev0 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No. DO-138-131121 25 th November 2013 Page 2 / 3 Edition 1 Rev.0 INSPECTION INSTRUCTIONS 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; 6) Wheels locked. 2. Inspect engine mount 1) Remove the engine cowlings upper and lower (LH and RH), according P2006T AMM; 2) Perform the visual inspection on both LH and RH engine mounts (with particular attention of the nodes high- lighted in the following pictures) for cracks and deformation, use a torch light and/or mirrors if needed; Figure 1 – Engine Mount nodes. If a crack is found, fill the occurrence report herein attached and send it to Tecnam. 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 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 (if applicable) “ 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: technical.support@tecnam.com and airworthiness@tecnam.com. Eventually by fax: +39 0823 622899 or express courier: Via Maiorise snc Capua (CE) 81043 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.