## SERVICE BULLETIN

N° SB 128

– CS

– Rev0

The technical content of this document is approved under the authority of DOA. EASA.21J.335

Approval No. DO

- 128

- 130422

1 5 t h May 20 13



### Page 1 / 3

Edition 1 Rev .0 INFORMATION 

###  RECOMMENDED 

###  MANDATORY 

### 

SUBJECT : 

### P2006T Lower link inspection /replacement, as applicable

SCOPE : 

### During an inspection of a P2006T

, on the NLG lower link two

cracks w ere found

. The part involved is related to old link assy

( P/N 26

- 8

- 1417

- 000) , replaced by SB

- 104

- CS

, whatever rev ision

. Tecnam prescribes to perform a dedicated inspection on NLG

lower link ( P/N 26

- 8

- 1 417

- 1 ) on airplanes which don’ t embody

SB104

- CS

, whatever revision, within the terms herein reported.

Additionally Te cna m p rescribe s , at same time, to apply the KIT

SB128

- CS (which includes new link assy P/N 26

- 8

- 8000

- 000)

to all P2006T airplanes which don’t embody SB 104

- CS Ed.2

Rev. 1

. This SB supersedes SB 104

- CS Ed.2 Rev.1

Nevertheless , Tecnam reminds owners/operator s to respect the

scheduled maintenance progra m as provided by AMM, chapters

0 4 and 05.

MODELS AFFECTED : 

### All P2006T airplanes

, which don’t embody the SB 104

- CS

Ed.2 Rev.1

TIME OF COMPLIANCE : 

### Inspection , if applicable, to be performed w ithin the ne xt 25

flight hours or 3 0 days (whichever occurs first) after the issue

date of this SB

. Replacement to be performed with in the next 50 flight hours or

6 0 days (whichever occurs first) after the issue date or this SB.

MANPOWER : 6 man

- hours

.

REQUIRED MATERIAL : 

### KIT no. SB128

- CS

, includ ing :

 KIT no. SB 104

- CS (Job card no. 442) if not embodied yet;

 KIT no. SB 104

- CS/2 (Job card no. 528);

 KIT no. SB 109

- CS (Job card no. 468) if not embodied yet.

TOOLING : 

### Nil

WEIGHT AND BALANCE : 

### N il

REFERENCE S : 

### P2006T Maintenance Manual doc. no. 2006/45

– last issue;

P2006T Aircraft Parts Catalogue doc. no. 2006/46

– last issue;

PUB

. AFFECTED : Nil

## SERVICE BULLETIN

N° SB 128

– CS

– Rev0

The technical content of this document is approved under the authority of DOA. EASA.21J.335

Approval No. DO

- 128

- 130422

1 5 t h May 20 13



### Page 2 / 3

Edition 1 Rev .0 

### INSPECTION /R EPLACEMENT INSTRUCTIONS ( as applicable)

1. Aircraft preparation

1) Park the aircraft in a closed hangar ;

2) Make sure that lan ding 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 ;



### 2

. Inspect nose landing gear lower link

1) Remove the inspection cap F2 (refer to P2006 T AMM , ATA 6 )

2) Identif

y the Lower link (see following figure 1);

3) Visually inspect both side s of the lower link for cracks and deformation ;

Figure 1

– Inspection item

If a crack was found c omplete the occurrence report hereby attached and send it Tecnam.



### 3. Terminating action

- Kit no. SB 128

- CS installation

1) Follow instructions contained in the applicable kit/s and perform scheduled maintenance as pro vided by

AMM, chapters 04 and 0 5

.

Record the application of the present Service Bulletin on the aircraft log

- book.



### For further information please contact TECNAM:

Tel 0039 0823 620134

Fax 0 039 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: “ Time Since Overhaul:

“ Cycles since new: “ Cycles since new

Affected Item (if applicable) Engine No.2 type:

“ 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 los s:

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

Airworthines s: airworthiness@tecnam.com

. Eventually by fax: +39 081 7584528 or express courier: 1°trav. Via Giovanni Pascoli n°1 Casoria (NA) 80026 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 h our 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.