# Tecnam Service Bulletin 748-CS: No revision named

- Rights: © 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.
- Document: [Tecnam Service Bulletin 748-CS](https://openairdocs.org/service-documents/tecnam/748-cs.md)
- Title as filed: TECNAM Service Bulletin SB 748-CS-Ed 1 Rev 0
- Pages: 3
- PDF: https://openairdocs.org/files/sha256/e0/0c/e00c312bff9b12ee96c351cf2e5b93e28f7822e3246cfa8a768030e47ebe6ad7
- Page: https://openairdocs.org/service-documents/tecnam/748-cs/file/e00c312bff9b

## Text

Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

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 accord-
ance with design changes MOD2002/339 and 
MOD2002/342, several improvements have been introduced 
on the P-Mentor seat, particularly a new seat covering in-
stallation. 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 metal-
lic 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

### Page 2 (OCR)

-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

### Page 3

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

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