# Tecnam Mandatory Service Bulletin 138-CS: No revision named

- Rights: © Tecnam. Filed by the FAA in regulations.gov docket FAA-2014-0156; AD 2014-11-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Tecnam Mandatory Service Bulletin 138-CS](https://openairdocs.org/service-documents/tecnam/138-cs.md)
- Title as filed: SB 138 - CS - P2006T Engine Mount Inspection   - ed1r0
- Pages: 3
- PDF: https://openairdocs.org/files/sha256/7a/cf/7acf00bd74eba3c271ab735f148a8d85a596528414cd2499b8bcf33c5a99c547
- Page: https://openairdocs.org/service-documents/tecnam/138-cs/file/7acf00bd74eb

## Text

Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

SERVICE BULLETIN 
 
                                                                                                                       N° SB 138 – CS – Rev0 
  
The technical content of this document is approved under the authority of DO A ref. EASA.21J.335  
 Approval No. DO-138-131121    
25th November 2013 
                                   
Page 1 / 3 
 
Edition 1 Rev.0 
 
INFORMATION  RECOMMENDED  MANDATORY  
      
 
SUBJECT: P2006T Engine Mount inspection 
  
SCOPE: During a 100hr inspection of a P2006T, on a node of the engine 
mount (P/N 26-7-1200-000) a crack was found. 
Tecnam prescribes to perform a dedicated inspection on t his 
item for all P2006T airplanes having more than 600 flight hours 
within the terms herein reported. 
 
  
MODELS AFFECTED: All P2006T airplanes, having more than 600 flight hours. 
 
  
TIME OF COMPLIANCE: Within the next 25 hours or 30 days (whichever occurs first) af-
ter the issue date of this SB for airplanes with more than 600 
flight hours. 
 
  
MANPOWER: 1 man-hour. 
  
REQUIRED MATERIAL:  Nil 
  
TOOLING: Nil 
  
WEIGHT AND BALANCE: Nil 
 
 
REFERENCES: P2006T Maintenance Manual doc. no. 2006/45 – last issue; 
P2006T Aircraft Parts Catalogue doc. no. 2006/46 – last issue;  
  
PUB.  AFFECTED: Nil

### Page 2

SERVICE BULLETIN 
 
                                                                                                                       N° SB 138 – CS – Rev0 
  
The technical content of this document is approved under the authority of DO A ref. EASA.21J.335  
 Approval No. DO-138-131121    
25th November 2013 
                                   
Page 2 / 3 
 
Edition 1 Rev.0 
 
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 engine mount  
1) Remove the engine cowlings upper and lower (LH and RH), according P2006T AMM; 
2) Perform the visual inspection on both LH and RH engine mounts (with particular attention of the nodes high-
lighted in the following pictures) for cracks and deformation, use a torch light and/or mirrors if needed;  
 
   
  
 
Figure 1 – Engine Mount nodes. 
 
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. 
 
 
 
 
For further information please contact TECNAM: 
Tel 0039 0823 620134 
Fax 0039 0823 622899 
E-mail  airworthiness@tecnam.com

### Page 3

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 Office 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 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.

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