SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1
TECNAM P-2006T · Service Bulletins
Overview
This service bulletin provides mandatory inspection instructions for the exhaust pipes of the Tecnam P2006T aircraft. It outlines the steps to be taken if cracks or defects are found during the inspection, as well as the compliance timeline and contact information for technical support.
- Mandatory inspection of exhaust pipes for all P2006T aircraft.
- Inspection must be completed within 25 flight hours or 30 days.
- Visual inspection required for all 4 exhaust pipes.
- Contact Tecnam for evaluation if defects are found.
- No special tools or materials are required for the inspection.
- Record the application of the service bulletin in the aircraft log-book.
- Report any cracks using the provided occurrence report.
- Aircraft must be parked in a closed hangar for inspection.
Document
Source
Originally published by regulations.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Service Bulletins
- Year ·
- 2014
- File size ·
- 721 KB
- Publisher ·
- regulations.gov
- Language ·
- en
What is the SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1?
The SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 is a service bulletins for the TECNAM P-2006T, dated 2014.
Where does the SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 come from?
This copy of the SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 was originally published by regulations.gov and is hosted on Sprinkle as a free, searchable reference copy.
What year was the SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 published?
The SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 — the TECNAM P-2006T service bulletins on file — is dated 2014.
Most owners only have the POH. Here's the essential set for the TECNAM P-2006T.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P-2006Tmanuals & documents
- SPECTRUM AIRWAYS TECNAM P2006T NORMAL PROCEDURESChecklist
- CHECK LISTChecklist
- TECNAM P2006T CHECK LISTChecklist
- Normal Check List P2006TChecklist
- Aircraft Flight ManualPilot's Operating Handbook
- Aircraft Flight ManualPilot's Operating Handbook
- Section 9 - Supplements - Delta AviationFlight Manual Supplement
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In this document
Inspection Instructions
Details the preparation steps for the aircraft and the procedure for inspecting the exhaust pipes.
Time of Compliance
Inspection must be completed within the next 25 flight hours or 30 days after the issue date.
Applicability
This bulletin applies to all P2006T aircraft.
Required Material
No special materials are required for the inspection.
Tooling
No special tooling is required for the inspection.
Occurrence Report
Operators must fill out and send an occurrence report if cracks are found.
Safety notes
- Ensure the engine is cool before inspection.
- Park the aircraft in a closed hangar.
- Make sure landing gear is down and locked.
- Turn off the master switch and starter relay breaker before inspection.
Full document text
SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 Date: 25 09 2014 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-170-140925 Page 1 / 4 MOD. PD-006-03 rev.2 data: 18/11/13 SERVICE BULLETIN Edition 1 Rev.1 For further information please contact TECNAM: Tel: 0039 0823 622297 – Kit order 0039 0823 997538 – Technical Support Fax: 0039 0823 622899 E-mail: technical.support@tecnam.com MANDATORY by the AD No.yyyy-xxxx May become MANDATORY after EASA evaluation RECOMMENDED …………………………. INFORMATION ………………………………………… SUBJECT: P2006T Exhaust pipes inspection SCOPE: During a pre-flight inspection of a P2006T, a cracked exhaust pipe p/n 26-7-1800-1 was found. Tecnam prescribes to perform a dedicated inspection on the exhaust pipes for all P2006T. If deformation, cracks or other defects are found, please contact technical.support@tecnam.com for an evaluation. APPLICABILITY: All P2006T aircraft. TIME OF COMPLIANCE: Within the next 25 flight hours or 30 days (whichever occurs first) after the issue date of this SB. MANPOWER: 0.5 man-hours. REQUIRED MATERIAL: Nil. TOOLING: Nil. WEIGHT AND BALANCE: Nil. REFERENCES: Refer to the instruction contained in the following pages of this document. PUB. AFFECTED: P2006T AMM – Aircraft Maintenance Manual. P2006T IPC – Illustrated Parts Catalogue. SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 Date: 25 09 2014 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-170-140925 Page 2 / 4 MOD. PD-006-03 rev.2 data: 18/11/13 SERVICE BULLETIN Edition 1 Rev.1 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 the exhaust pipes Note Make sure the engine is cool before proceed with the following inspection 1) Remove the engine cowlings upper and lower (LH and RH), according P2006T AMM; 2) Perform the visual inspection on all 4 exhaust pipes for each engine (with particular attention of the welded points highlighted in the following pictures) for cracks and deformation, use a torch light and/or mirrors if needed; Fig.1 Rear left exhaust pipe SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 Date: 25 09 2014 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-170-140925 Page 3 / 4 MOD. PD-006-03 rev.2 data: 18/11/13 SERVICE BULLETIN Edition 1 Rev.1 Fig.2 Rear right exhaust pipe Fig.3 Front left and right exhaust pipes 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. SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1 Date: 25 09 2014 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-170-140925 Page 4 / 4 MOD. PD-006-03 rev.2 data: 18/11/13 SERVICE BULLETIN Edition 1 Rev.1 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 Of- fice 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 in- formation 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.