Copy · TECNAM Service Bulletin SB 748-CS-Ed 1 Rev 0 · 3 pages

© Tecnam. Filed by the FAA in regulations.gov docket FAA-2025-2266; AD 2025-17-13 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

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SERVICE BULLETIN

N° SB 748 – CS – Ed 1 Rev 0 Date: 22/04/2024 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-748-240422 Page 1 / 1 MOD. PD-006-03 rev.2 data: 18/11/13

SERVICE BULLETIN Edition 1 Rev.0 MANDATORY by the AD No. yyyy-xxxx May become MANDATORY after EASA evaluation RECOMMENDED …………………………. INFORMATION …………………………………………

SUBJECT: P-Mentor new Seat design

SCOPE: Tecnam would like to inform its customers that in accordance with design changes MOD2002/339 and MOD2002/342, several improvements have been introduced on the P-Mentor seat, particularly a new seat covering installation. This new installation aims to avoid covering the seat structure on the lower side, which is painted black like the floor panel. The bottom cushion is attached to the metallic structure using Velcro-type fasteners. Additionally, the new seat includes two locking pins controlled by a single lever mechanism located on the seat front side to simplify pilot operation during seat adjustments..

Further details are included in the Appendix of this SB.

APPLICABILITY: All Tecnam P-Mentor which Does not embody the MOD2002/339 and MOD2002/342

TIME OF COMPLIANCE: At customer's choice.

MANPOWER: 2 Hour

REQUIRED MATERIAL: Kit SB 748 (working instructions are included in AMM ATA 25)

TOOLING: Nil.

WEIGHT AND BALANCE: Nil.

REFERENCES: P-Mentor AMM last issue;

MOD2002/339 MOD2002/342

PUB. AFFECTED: Nil

For further information please contact TECNAM:

• Kit order: spareparts@tecnam.com Tel: 0039 0823 622297

• Technical Support: technical.support@tecnam.com Tel: 0039 0823 997538

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-TECNAM QUALITY AIRCRAFT SINCE 1948 SERVICE BULLETIN N° SB 748 - CS - Ed 1 Rev 0 Date: 22/04/2024 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-748-240422 Page 1 / 1 Figure 4 - Post MOD configuration Seat structure Assembly Figure 3 - Post Mod configuration Seat assembly MOD. PD-006-03 rev.2 data: 18/11/13

SERVICE BULLETIN Edition 1 Rev.0

SERVICE BULLETIN

N° SB 748 – CS – Ed 1 Rev 0 Date: 22/04/2024 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-748-240422 Page 1 / 1 MOD. PD-006-03 rev.2 data: 18/11/13

SERVICE BULLETIN Edition 1 Rev.0