EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

PAGE : 1 of 17

This document is EADS SOGERMA property and can't be copied or transmitted without authorization. 

TITLE : EQUIPMENT/FURNISHINGS - COCKPIT SEAT - INSPECTION OF ACTUATOR 

1. PLANNING INFORMATION

A. EFFECTIVITY

This service bulletin is applicable to cockpit seats P/N: 

Captain seat 2510112 series First Officer seat 2510113 series

2510112-41-11 2510112-51-11 2510112-55-11 2510113-41-11 2510113-51-03 2510113-55-04 

2510112-41-12 2510112-51-12 2510112-55-13 2510113-41-12 2510113-51-11 2510113-55-05 

2510112-43-01 2510112-53-01 2510112-55-14 2510113-43-01 2510113-51-12 2510113-55-11 

2510112-43-04 2510112-53-02 2510112-55-15 2510113-43-04 2510113-53-01 2510113-55-13 

2510112-43-07 2510112-53-03 2510112-61-01 2510113-43-07 2510113-53-02 2510113-55-14 

2510112-43-11 2510112-53-04 2510112-61-02 2510113-43-11 2510113-53-03 2510113-55-15 

2510112-43-12 2510112-53-06 2510112-63-01 2510113-43-12 2510113-53-04 2510113-61-01 

2510112-43-13 2510112-53-07 2510112-63-02 2510113-43-13 2510113-53-05 2510113-61-02 

2510112-43-14 2510112-53-11 2510112-63-03 2510113-43-14 2510113-53-06 2510113-63-01 

2510112-43-16 2510112-53-12 2510112-63-04 2510113-43-15 2510113-53-07 2510113-63-02 

2510112-43-17 2510112-53-13 2510112-63-06 2510113-43-16 2510113-53-11 2510113-63-03 

2510112-45-01 2510112-53-14 2510112-63-07 2510113-43-17 2510113-53-12 2510113-63-04 

2510112-45-03 2510112-53-16 2510112-65-01 2510113-45-01 2510113-53-13 2510113-63-05 

2510112-45-11 2510112-53-17 2510112-65-03 2510113-45-03 2510113-53-14 2510113-63-06 

2510112-45-13 2510112-55-01 2510112-65-04 2510113-45-11 2510113-53-15 2510113-63-07 

2510112-45-14 2510112-55-02 2510112-65-05 2510113-45-13 2510113-53-16 2510113-65-01 

2510112-45-15 2510112-55-03 2510113-45-14 2510113-53-17 2510113-65-03 

2510112-51-01 2510112-55-04 2510113-45-15 2510113-55-01 2510113-65-04 

2510112-51-02 2510112-55-05 2510113-51-01 2510113-55-02 2510113-65-05 

2510112-51-03 2510113-51-02 2510113-55-03 

B. CONCURRENT REQUIREMENTS 

Service Bulletin 2510112-25-813 must be applied before or in conjunction with the 

present SB. 

C. REASON

(1) History 

During a high angle take off, a first officer seat moved to the rear position step by 

step under the weight of the occupant without intervention on seat control 

commands. After this incident, the seat has been inspected. 

The horizontal actuator was found damaged. Inside the actuator, a bevel gear, 

normally attached with the disc key, was found jammed on the actuator shaft. The 

internal disc key was found broken, metallic particles between bevel gear and 

shaft made a friction and jammed the parts. 

Under this configuration and in normal condition, the seat operates correctly but if 

a strong weight is applied the seat can move backwards without control. Root 

cause of this disc key break-off is an over-torque applied on the actuator output 

shaft following misalignment between the electrical micro-switch stop and the end 

stop. This misalignment has been corrected through SB 2510112-25-813. 

However SB 2510112-28-813 does not request to check the condition of the 

actuator disk key. Investigations have shown that the new event is linked to the 

fact that the actuator was damaged prior to VSB 2510112-25-813 application. 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

PAGE : 2

This document is EADS SOGERMA property and can't be copied or transmitted without authorization. 

(2) Objective/Action 

Based on the information detailed above, EADS SOGERMA informs the 

operators that an inspection of seats is highly recommended in order to check the 

integrity of the horizontal actuator. A test must be applied to the seat to ensure 

that actuator is not damaged and make sure that locking function is still 

operational. A calibrated tensile test sample must be installed on the seat to test 

the actuator at a high torque to check the resistance of this disc key. 

(3) Advantages 

The inspection with the calibrated tensile test sample ensures that actuator is 

serviceable. The test is non destructive for the actuator. If the actuator is 

compliant with the directives of this Service Bulletin, it guarantees that the seat is 

serviceable and complies with the flight safety rules. 

D. DESCRIPTION

This Service Bulletin gives instructions to: 

− Install the calibrated test sample. 

− Do the operational test. 

− Return the seat to the serviceable condition. 

− Apply the identification label. 

E. APPLICATION

(1) Classification 

− Recommended 

(2) Accomplishment timescale 

Accomplishment of this Service Bulletin must be done at the first opportunity. 

After application, complete and return imperatively report sheet to EADS 

SOGERMA (Refer to the last page of this Service Bulletin for further details). 

F. APPROVAL

The modification procedures described in this VSB have been reviewed and 

technically accepted by Airbus Design Office to apply to the Airbus fleet affected. 

This SB does not contain any change information that revises the equipment 

definition covered by Airbus approved modifications. 

G. MANPOWER

1 fitter/mechanic 

Approximate time: 

− To do the test : 20 minutes (For one seat) 

− Replace the seat : Refer to AMM task 25-11-11 for Captain seat 

 Refer to AMM task 25-11-12 for First/Officer seat 

 (Removal / Installation on A/C) 

− Replace the actuator : 30 minutes (For one seat) 

H. WEIGHT AND BALANCE

None. 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

PAGE : 3

This document is EADS SOGERMA property and can't be copied or transmitted without authorization. 

I. DATA ON ELECTRICAL LOAD ANALYSIS

None. 

J. REFERENCES

− EADS SOGERMA CMM : 

 25-11-19 for 2510112-XX / 2510113-XX seat series (XX= 41, 43, 51, 53, 61, 63) 

 25-11-22 for 2510112-X5 / 2510113-X5 seat series (X= 4, 5, 6) 

K. OTHER DOCUMENTS CONCERNED

None. 

L. INTERCHANGEABILITY OF PARTS

None. 

2. INFORMATION ON MATERIAL

A. MATERIAL - COST AND AVAILABILITY

The modification kits can be ordered at our logistic centres: 

For Europe 

EADS SOGERMA 

ZONE INDUSTRIELLE DE L’ARSENAL 

CS 60109 

17303 ROCHEFORT CEDEX - France 

Phone : (33).5.46.82.83.04 or (33).5.46.82.85.41 

Fax : (33).5.46.82.83.24 

SITA Code : RCOSSCR 

Spec 2000: RCOSSCR 

E-mail addresses : SCOD1@sogerma.eads.net

For USA, CANADA, CENTRAL AND SOUTH AMERICA 

BARFIELD INC 

(on behalf of EADS SOGERMA) 

4101 N.W. 29th Street 

MIAMI - FLORIDA 33142 

USA 

Phone: (1).305.871.3900 

Fax: (1).305.894.5451 

SPEC2000: MIABFCR 

E-mail : mario.ross@barfieldinc.com

larry.vaquero@barfieldinc.com
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

PAGE : 4

This document is EADS SOGERMA property and can't be copied or transmitted without authorization. 

For ASIA & PACIFIC 

ELTRA AERONAUTICS (S) PTE LTD (CAGE Code: QB280) 

(On behalf of EADS SOGERMA) 

102EPASIR PANJANG ROAD 

#08-03 CITILINK WAREHOUSE COMPLEX 

SINGAPORE 118529 

Phone: +65.6275.0600 

Fax: +65.6275.6066 

SITA: SINSAXD 

SPEC2000: SINSAXD 

E-mail : customer.service@eltra.com.sg

For MIDDLE EAST 

TUFUL WORLD TRADING 

(On behalf of EADS SOGERMA) 

Dubai Office : 

RM. 405 AL ETHIAD BLDG. OPPOSITE 

OF DEIRA CITY CENTER 

PO BOX 28812 

DUBAI, UNITED ARAB EMIRATES 

Sharjah Warehouse : 

P6-140 SHARJAH International Airport Freezone 

PO BOX 121065 

SHARJAH, UNITED ARAB EMIRATES 

Phone: +971.6 5578146 

Fax: +971.6 5578156 

E-mail : tufultrd@eim.ae

Cost: The kit price will not exceed 773 USD (Price condition 2012) 

Availability: 7 days upon receipt of purchase order. 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

PAGE : 5

This document is EADS SOGERMA property and can't be copied or transmitted without authorization. 

B. NECESSARY MATERIAL FOR EACH EQUIPMENT

(1) Modification kit P/N: 25-898-9000 

Valid for one Captain or First Officer seat. 

PART NUMBER Qty DESCRIPTION 

ET3-010-030-09 1 PLATE, INFORMATION 

2510112299-20 1 SAMPLE, TENSILE TEST 

AN3-25A 1 SCREW, HEX. HEAD 

NAS1801-08-14 1 SCREW, HEX. HEAD 

NAS517-2-6 1 SCREW, CSK HEAD 

NAS1149F0363P 1 WASHER, TH 1.6MM 

NAS1149DN832K 1 WASHER, TH 0.8 MM 

(2) Consumable (Local Purchase) 

P/N DESIGNATION Qty SOURCE

LOCTITE 241 SEALANT, ANAEROBIC AR F7121 

MOLIKOTE® Longterm W2 GREASE AR F7286

C. TOOLING

Standard tooling. 

3. OPERATING INSTRUCTIONS

A. PRELIMINARY STEPS

The work of this Service Bulletin can be done in a certified repair shop or in the A/C. 

Refer to CMM 25-11-19 or 25-11-22 for help. 

(1) Move the seat to the upper position to get access to the lower face of seat base. 

B. OPERATING PROCEDURE

NOTE : Keep all parts. The exceptions are annotated in the procedure detailed 

below. Before disassembly, put marks on all the parts to help re-assembly 

and prevent errors.
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

PAGE : 6

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(1) Test of horizontal electrical motion, refer to Fig. 1 

(a) Apply power to the seat to be tested. 

(b) Press on the switch S8 to the rear direction (RWD), the seat must move to the 

rear direction. 

(c) Press on the switch S8 to the front direction (FWD), the seat must move to 

the front direction. 

(d) Cut off the power after the test. 

WARNING :IF THE SEAT DOESN'T MOVE IN THE DESIRED DIRECTION, DO NOT 

DO THE INSPECTION. THAT CAN CAUSE DAMAGE TO THE SEAT. 

YOU MUST REPAIR THE SEAT, REFER TO THE APPLICABLE CMM. 

TEST OF HORIZONTAL ELECTRICAL MOTION 

FIGURE 1 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

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(2) Installation of tensile test sample, refer to Fig. 2 

(a) Move the seat to the rear position with mechanical control. 

(b) Remove the screw (1) and discard it. 

NOTE : You can use an impact screwdriver to remove the screw (1). 

(c) Remove the screw (2) and the washer (3). 

(d) Clean the area with a cloth. 

(e) Install the tensile test sample (4) P/N: 2510112299-20 on the seat base with 

the screw (5) P/N: NAS1801-08-14 and the washer (6) P/N: 

NAS1149DN832K. Do not tighten the screw (5). 

(f) Move the seat with mechanical control in order to position the free hole of 

actuator in contact with the tensile test sample (4). 

(g) Install the screw (7) P/N: AN3-25A and the washer (8) P/N: NAS1149F0363P 

to attach the tensile test sample (4) on the actuator. 

(h) Tighten the screw (5) from 2,5 to 3 Nm (22 to 26 In.lbf) and screw (7) from 4 

to 5 Nm (35 to 44In.lbf). 

(3) Testing of actuator, refer to Fig 3 

WARNING : MAKE SURE THAT YOU PRESS THE SWITCH S8 TO THE REAR

DIRECTION. YOU CAN DAMAGE THE TENSILE TEST SAMPLE 

AND THE ACTUATOR IF SWITCH IS ACTIVATED IN THE WRONG 

DIRECTION. 

(a) Apply power to the seat to be tested. 

(b) Press on the switch S8 to the rear direction (RWD) in order to break the 

tensile test sample by the actuator power. 

(c) Cut off the power after the test. 

(d) Test result: 

− The tensile test sample is broken, the seat is serviceable. 

− The tensile test sample is not broken, the actuator runs but the seat does not 

move, that show that the actuator is damaged .The seat is unserviceable. 

In case of unserviceable seat, two possibilities: 

1 Replace the seat by a serviceable one (tested in accordance with this SB). 

2 Remove the seat from A/C and replace the actuator. (Refer to § (5)) 

(4) Removal of tensile test sample and close up, refer to Fig.4 

(a) Remove the screw (1), the washer (2), the half part of tensile test sample (3). 

(b) Remove the screw (4), the washer (5), the half part of tensile test sample (6). 

(c) Install the new screw (7) P/N: NAS517-2-6. 

(d) Install the existing screw (8) with washer (9) on the actuator. 

(e) Discard the screws (1 and 4), the washers (2 and 5) and the tensile test 

sample parts (3 and 6). 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

PAGE : 8

This document is EADS SOGERMA property and can't be copied or transmitted without authorization. 

INSTALLATION OF TENSILE TEST SAMPLE 

FIGURE 2 

4 

4 

1 

2 

3 

5 

6 

7 

8 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

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TESTING OF ACTUATOR 

FIGURE 3 

Switch S8 

TENSILE TEST SAMPLE BROKEN
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

PAGE : 10

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REMOVAL OF TENSILE TEST SAMPLE AND CLOSE UP 

FIGURE 4 

8 

9 

6 

4 

5 

7 

3 

1 

2 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

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(5) Replacement of actuator, refer to Fig. 5 

NOTE : Replacement must be done only if actuator is damaged. 

WARNING : MAKE SURE THAT POWER IS CUT OFF BEFORE ANY 

INTERVENTION ON SEAT. 

(a) Removal of actuator 

1 Disconnect the connector X4 (1) from the actuator (2). 

2 Removal of control cable 

a For a captain seat 

1 Remove the nut (3) and the screw (4). 

2 Remove the nut (5), the washer (6), the screw (7) and the washer 

(8), remove the cable bracket (9). 

b For a first officer seat 

1 Remove the nut (18) from the cable (19). 

3 Removal of actuator 

a Remove the nut (10), the washer (11), the screw (12) and washer (13). 

b Remove the screws (14) and the washers (15), remove the actuator (2). 

4 Removal of actuator pinion and control cable lever 

a Remove the screw (20) and remove the washer (21). 

b Remove the needle bearing (22) and the inner bush (23) of needle 

bearing. 

c Remove the pinion (24) from the actuator shaft (25). 

d Keep the disc key (26) in place on the actuator shaft (25) with a piece of 

adhesive tape, tie cable, etc... 

e Remove the elastic ring (27) and remove the control cable lever (17). 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

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(b) Installation of new actuator 

1 Installation of pinion and cable control lever on a new actuator 

a Remove the protection on the actuator shaft (25), check that the disc 

key (26) is installed. 

b Install the pinion (24) on the actuator shaft (25). 

c Install the inner bush (23) of needle bearing on the actuator shaft (25). 

d Install the needle bearing (22). Apply grease MOLIKOTE long term W2. 

e Install the washer (21) and the screw (20). Apply LOCTITE 241 on the 

screw (20). 

f Install the cable control lever (17) on the actuator (2). 

g Lock the cable control lever (17) with the elastic ring (27). 

2 Installation of actuator 

a Install the actuator (2) on the seat. Engage the pinion in the rack. 

b Attach the actuator (2) with the screws (14) and the washers (15). 

c Attach the actuator (2) with the screw (12), the washer (13), the washer 

(11) and the nut (10). 

d Tighten the screws (12 and 14) from 2,5 to 3 Nm (22 to 26 In.lbf). 

3 Installation of control cable 

a For a captain seat 

1 Install the cable bracket (9) on the actuator (2) with the screw (7), 

the washer (8), the washer (6) and the nut (5). Tighten the screw (7) 

from 2,5 to 3 Nm (22 to 26 In.lbf). 

2 Install the screw (4) on the actuator lever (16) and on the control 

cable lever (17). 

3 Install the nut (3) on the screw (4), adjust the nut (3) in order to get a 

minimum clearance. 

b For a first officer seat 

1 Install the nut (18) on the control cable lever (17). 

2 Adjust the nut (18) in order to get a minimum clearance. 

4 Connect the connector X4 (1) to the actuator (2). 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

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View A 

REPLACEMENT OF ACTUATOR 

FOR A CAPTAIN SEAT 

FIGURE 5 (SHEET 1 OF 3) 

3 

9 

5 

6 7 

8 

4 

1 

A

10 

11 

12 

13 

2 

14

15

14

15

7 

8 

16

17 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

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INITIAL ISSUE : APR 25/12 SB 2510112-25-898

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View B 

REPLACEMENT OF ACTUATOR 

FOR A FIRST OFFICER SEAT 

FIGURE 5 (SHEET 2 OF 3) 

1 

2 

18 

19

14 

15 

14 

15 

10 

11 

12 

13 

10 

11 

12 

13 

10 

11 

B 

14

15

17 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

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INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

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REPLACEMENT OF ACTUATOR 

ACTUATOR PINION REMOVAL / INSTALLATION 

FIGURE 5 (SHEET 3 OF 3) 

20

21

22

23

24

25

26

17 

27
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

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C. IDENTIFICATION

After application of this Inspection Service Bulletin, the seat is compliant with the 

directives of the inspection (Actuator tested or replaced) and must be identified. 

(1) Check on the seat if information plate (1) P/N: ET3-010-030-09 is existing near 

the identification plate, if not bond a new information plate. 

(2) Write on the information plate (1) P/N: ET3-010-030-09 with indelible ink: 

− The SB application date MMM DD/YY 

− Write INSPECTED in the New P/N compartment. 

− The reason: ISB 2510112-25-898 Applied

INFORMATION PLATE 

IDENTIFICATION 

FIGURE 6 

A

ISB 2510112-25-898 

applied 

DATE INSPECTED 
EADS SOGERMA (F4643) Z.I. de l’arsenal 

CS. 60109 - 17303 ROCHEFORT CEDEX - FRANCE 

TEL : 33.5.46.82.84.84 - SITA Code : RCOSSCR 

FAX : 33.5.46.82.88.13

INSPECTION SERVICE BULLETIN 

INITIAL ISSUE : APR 25/12 SB 2510112-25-898

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4. INSPECTION REPORT SHEET

After application of ISB 2510112-25-898, please send us back a copy duly completed of 

this Inspection Report Sheet. 

(1) Customer identification

Customer: Aircraft model: Aircraft MSN: 

 

(2) Cockpit seat

Seat P/N of Seat Seat S/N

Captain 2510112-__ - __ 

First Officer 2510113-__ - __ 

(3) Customer remarks

(4) Please, date, sign and send to:

EADS SOGERMA

Mr Alain CANIVET 

Product Support Department 

Z.I DE L'ARSENAL- C.S.60109 

17303 ROCHEFORT CEDEX 

FRANCE 

Fax : 33.5.46.82.88.13 

E-mail: alain.canivet@sogerma.eads.net

Person in charge

of SB application