Copy · U.S. DOT/FAA - Service Bulletin No. 102 - CS - Rev 2 · 4 pages

© Tecnam. Filed by the FAA in regulations.gov docket FAA-2012-1173; AD 2013-04-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

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COSTRUZIONI AERONAUTICHE

TECNAM SERVICE BULLETIN N° SB 102 - CS - Rev2 Approved by TECNAM-under DOA certificate EASA.21J.335 N° DO-102-120626 26h June 2012 Rev1. 29th June 2012 Rev2. 03" July 2012 Page 1 / 3

INFORMATION RECOMMENDED MANDATORY SUBJECT: P2006T Aileron hinge supports inspection SCOPE: During an inspection of a P2006T, on the LH aileron hinge support outboard side (P/N 26-1-1082-1/3) were found multiple cracks.

Tecnam prescribes to perform a dedicated inspection on all Aileron hinge supports (P/N 26-1-1082-1/3, P/N 26-1-1081-1/3, P/N 26-1-1081-2/4, P/N 26-1-1082-2/4) within the terms herein reported.

MODELS AFFECTED: P2006T airplanes, all S/N TIME OF COMPLIANCE: Within the next 25 hours or 30 days (whichever occurs first) after the issue date of this SB for airplanes with more than 600 flight hours.

Repeat the inspection during each the scheduled 100 flight hours/yearly inspection.

MANPOWER: 0.2 man-hours.

REQUIRED MATERIAL: Nil TOOLING: Nil WEIGHT AND BALANCE: Nil REFERENCES: P2006T Maintenance Manual doc. Nr 2006/45 PUB. AFFECTED: Nil Rev. 2, 3rd July 2012 Edition 1 Rev.2

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COSTRUZIONI AERONAUTICHE TECNAM SERVICE BULLETIN N° SB 102 - CS - Rev2 Approved by TECNAM-under DOA certificate EASA.21J.335 N° DO-102-120626 26th June 2012 Rev1. 29th June 2012 Rev2. 03r July 2012 Page 2 / 3

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;

2. Inspect ailerons supports hinges

1) Rotate LH aileron in full up position;

2) Identify the LH aileron hinge support P/N 26-1-1082-1/3 outboard side (see following figure 1);

P/N 26-1-1082-3 P/N 26-1-1082-1 I FW LH Aileron hinge - Tip side LH Aileron Figure 1 - Inspection items identification

3) Inspect (using a high spot light if required) the I.H aileron hinge support P/N 26-1-1082-1/3 outboard side for absence of cracks (refer to inspection points indicated in the following figure 2).

Inspection points Figure 2 - Inspection points Rev. 1, 29th June 2012 Edition 1 Rev.2

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COSTRUZIONI AERONAUTICHE

TECNAM SERVICE BULLETIN N° SB 102 - CS - Rev2 Approved by TECNAM-under DOA certificate EASA.21J.335 N° DO-102-120626 26h June 2012 Rev1. 2gth June 2012 Rev2. 03r July 2012 Page 3 / 3

4) Operate the same inspection for the LH aileron hinge support P/N 26-1-1081-1/3 inboard side for absence of cracks:

5) Rotate the RH aileron in full up position;

6) Identify the RH aileron hinge support P/N 26-1-1082-2/4 outboard side;

7) Inspect (using a high spot light if required) the RH aileron hinge support P/N 26-1-1082-2/4 outboard side for absence of cracks (refer to inspection points indicated in the following figure 2);

8) Operate the same inspection for the RH aileron hinge support P/N 26-1-1081-2/4 inboard side for absence of cracks;

If a crack is found during inspection required by this SB, the part must be considered unserviceable and please contact Costruzioni Acronautiche TECNAM for replacement instructions and accomplish them accordingly.

Complete the occurrence report hereby attached and send it 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 Rev. 2, 3rd July 2012 Edition 1 Rev.2

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COSTRUZIONI AERONAUTICHE Occurrence Report Date:

• TECNAM 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:

No. of injured persons Acc./s.Ine./Inc (ICAO A13) Possible cause:

Action to be done:

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.