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Page 1OCROpen in PDF

•TECNAM QUALITY AIRCRAFT SINCE 1948 SERVICE BULLETIN N° SB 817 - CS - Ed. 1 Rev.1 Date: 06/12/2024 Rev. 1: 11/12/2024 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-817-241206 MANDATORY by the AD No. 2024-0239 May become MANDATORY after EASA evaluation RECOMMENDED INFORMATION.

SUBJECT: P2010 & P2010TDI Rudder Pedals Torque Tube Hinges SCOPE: Following an occurrence report involving a P2010 aircraft, Tecnam identified a potential unsafe condition that may affect the Rudder Pedals Torque Tube. As a result, design change MOD2010/359 introduced an improvement to the P2010 rudder pedals torque tube hinges. To prevent similar issues across the P2010 series fleet, Tecnam mandates the installation of retainer washers (P/N 210-5-3010-001) on both the left-hand (LH) and right-hand (RH) pedal hinges.

Refer to Appendix A for a reference image of the installation. Additional details are provided in Appendix B of this document.

APPLICABILITY:

TIME OF COMPLIANCE:

MANPOWER:

REQUIRED MATERIAL:

TOOLING:

WEIGHT AND BALANCE:

All Tecnam P2010 & P2010TDI up to S/N 317 (inclusive) which do not embody MOD2010/359.

25 flight hours (FH) or 30 days, whichever occurs first, from the issuance date of this Service Bulletin 1 man-hour Kit SB 817-CS includes 4 (four) Washers (P/N 210-5-3010-

001). The related accomplishment instructions are provided in Appendix B of this document.

Nil.

REFERENCES: P2010 & P2010TDI AMM last issue;

MOD2010/359 PUB. AFFECTED: P2010 & P2010TDI IPC and AMM For further information please contact TECNAM:

• Technical Support:

• Email: technical.support@tecnam.com or Tel: 0039 0823 997538

• Spare Parts

• Email: spareparts@tecnam.com or Tel: 0039 0823 622297 Page 1/3 MOD. PD-006-03 rev.3 data: 04/03/20

SERVICE BULLETIN Edition 1 Rev.1

Page 2OCROpen in PDF

LETECNAM QUALITY AIRCRAFT SINCE 1948 SERVICE BULLETIN N° SB 817 - CS - Ed. 1 Rev.1 Date: 06/12/2024 Rev. 1: 11/12/2024 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-817-241206 Appendix A Refer to the following figure for an image of the post-mod installation, shown for reference purposes.

Retaining Page 2/3 MOD. PD-006-03 rev.3 data: 04/03/20

SERVICE BULLETIN Edition 1 Rev. 1

Page 3OCROpen in PDF

TECNAM QUALITY AIRCRAFT SINCE 1948 SERVICE BULLETIN N° SB 817 - CS - Ed. 1 Rev. 1 Date: 06/12/2024 Rev. 1: 11/12/2024 The technical content of this document is approved under the authority of DOA ref. EASA.21J.335 Approval No: DO-817-241206 Appendix B N Accomplishment Instructions Park the airplane in safe area;

2 Parking brake ON and Master Switch OFF;

3 Unscrew the bolt located on the left-hand (LH) pedal hinge.

Important: During bolt removal, carefully ensure that the bolt, washer, and nut do not drop into the floor bay.

Install the bolt on LH pedal hinge according to following picture (LH Side Shown for Reference) 210-2-4001-0011 210-5-3001-801 PDS.4 (210-5-3010-001) MS21042-5 AN5-15A 210-5-3001-80 POS.4 (210-5-3010-001) -AN960-516 NOTE: during installation procedure, pay attention to install new self-locking nut 4 Tight the bolt according to applicable torques included in AMM, ATA 20 5 Perform the instructions included in point 3,4 on RH pedal hinge too.

Performing a functional/operating check of the system, checking that retaining washers are installed properly without interference with lugs.

7 Apply the lubber line on nut and bolt thread (RH and LH side), like in Appendix A.

Page 3/3 MOD. PD-006-03 rev.3 data: 04/03/20

SERVICE BULLETIN Edition 1 Rev. 1