## 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

- 1311 21

2 5 th November 20 13



### 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 e n gine

mount (P/N 26

- 7

- 1200

- 000) a crack w as found

. Tecnam prescribes to perform a dedicated inspec tion 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 (whic hever occurs first) a fter 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 : 

### N il

REFERENCES : 

### P2006T Maintenance Manual doc. no. 2006/4 5

– last issue;

P2006T Aircraft Parts Catalogue doc. no. 2006/46

– last issue;

PUB

. AFFECTED : Nil

## 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

- 1311 21

2 5 th November 20 13



### 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 b oth LH and RH engine mounts ( with particular attention of the nodes hig hlighted in the following pictures ) for cracks and deformation , use a torch light and/ or mirrors if needed ;

Figure 1

– Engine Mount no des

.



### 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 003 9 0823 62 28 99

E

- mail airworthiness@tecnam.com

# Occurrence Report Date:

Aircraft Type: Engine No.1 type:

Serial No. “ Serial No.

Registration markings: “ Time Since New:

A/C Time Since New: “ Ti me 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 AVAI LABLE 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.