ZODIAC SERVICES 

ZODIAC SERVICES 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION : 3 PAGE: 1/2 THE DATA AND INFORMATION CONTAINED HEREIN ARE PROPRIETARY TO INTERTECHNIQUE. COPY AND DISTRIBUTION TO A THIRD PARTY ARE STRICTLY FORBIDDEN. PRINTED IN FRANCE

ZODIAC SERVICES 

Technical Publication Department 

61 rue Pierre Curie 

CS20001 

78373 PLAISIR Cedex 

FRANCE 

Phone international : + 33 1 64 34 23 23 

Fax international : + 33 1 64 34 21 08 

Web site: www.services.zodiacaerospace.com 

TRANSMITTAL SHEET 

This Transmittal Sheet applies to Revision 03, dated DEC 15/12, of Service Bulletin 320GC03Y-24-012 

REASON FOR REVISION

- Precisions added 

REVISION SEQUENCE

Initial Issue : JUL 15/12 

Issue 1 : SEP 25/12 

Issue 2 : NOV 08/12 

Issue 3 : DEC 15/12 
ZODIAC SERVICES 

ZODIAC SERVICES 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION : 3 PAGE: 2/2

THIS PAGE INTENTIONALLY LEFT BLANK
ECE AIRCRAFT SYSTEMS 

129Bd DAVOUT CS 82012 

75990 PARIS Cedex 20 

Phone: (33) 01 56 06 10 00 

Fax : (33) 01 56 06 10 10

SERVICE BULLETIN

CHALLENGER 300 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 1/22

APU, POWER CENTER, DC (AUX DCPC) 

P/N 320GC03Y04, P/N 320GC03Y05 AND P/N 320GC03Y06 

ATA 24 

Mandatory modification

Re-enforcing of PCB cover 

1. PLANNING INFORMATION

A. Effectivity 

(1) Concerned equipment 

This modification applies to Aux DCPC P/N 320GC03Y04, P/N 320GC03Y05 and P/N 

320GC03Y06. 

(2) On production line 

Applicable to Aux DCPC P/N 320GC03Y06 from S/N 518 (included).

(3) In the field 

Applicable to Aux DCPC P/N 320GC03Y04, P/N 320GC03Y05 and P/N 320GC03Y06 

before S/N 518. 

(4) Spares parts 

Applicable to operators and customer stocks Aux DCPC P/N 320GC03Y04, P/N 

320GC03Y05 and P/N 320GC03Y06 before S/N 518.

B. Concurrent Requirements 

Not applicable. 

C. Reason 

The flexibility of current PCB metallic cover does not permit, once closed, to guaranty boards 

insertion on mother board. 

A board originally not properly inserted by mistake would potentially remain in its partially inserted 

state (due to cover deformation capability), which could lead to a loss of communication and 

functional defects. 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 2/22

D. Description 

(1) Re-enforcing PCB cover to avoid its deformation and therefore to guaranty boards 

insertion. 

(2) Aux DCPC P/N 320GC03Y04 all amdt become 320GC03Y04 Amdt H.

(3) Aux DCPC P/N 320GC03Y05 all amdt become 320GC03Y05 Amdt H. 

(4) Aux DCPC P/N 320GC03Y06 all amdt become 320GC03Y06 Amdt C.

(5) Aux DCPC cover P/N GC063847Y02 becomes P/N GC063847Y03. 

E. Compliance 

Incorporation of this Service Bulletin is mandatory. It will be performed by the user of the aircraft. 

F. Approval 

The content of this Service Bulletin has been reviewed and accepted by Bombardier Aerospace. 

G. Manpower 

(1) 1 technician 

(2) Estimated time : 2 hours and 5 minutes 

H. Weight and Balance 

New cover weighs 0.57 lbs (0,26 kg) more than the old. 

I. Electrical Load Data 

Not Changed 

J. Software Accomplishment Summary 

Not applicable 

K. References 

(1) DCP EC100-11078 

(2) FEE 101483 

L. Other Publications Affected 

(1) BD-100 Aircraft Illustrated Parts Catalog - Chapter 24 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 3/22

(2) BD-100 Aircraft Maintenance Manual - Part II - Chapter 24 

M. Interchangeability and intermixability 

One way.
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 4/22

2. MATERIAL INFORMATION

A. Material – Price and Availability 

(1) Material 

P/N NOMENCLATURE QTY PRICE PER UNIT 

GC0003033Y00 Kit 1 On request 

(2) Price and Availability 

For item procurement or retrofit information, please contact: 

ZODIAC SERVICES EUROPE

61 rue Pierre Curie 

CS20001 

78373 PLAISIR Cedex 

FRANCE 

Tel: (33) (1) 64-34-23-23 

Fax: (33) (1) 64-34-21-08 

B. Industrial Support Information 

Not applicable 

C. Material Necessary for Each Component

P/N or REFERENCE QTY NAME 

GC0003033Y00 1 Kit 

Loctite 7400 AR Red Varnish 

Loctite 222E AR Threadlock 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 5/22

D. Disposition of parts 

In case of failure during the procedure causing permanent damage to the equipment, return the 

DCPC to : 

Europe customers: 

E.C.E.

271, avenue du Château Musset 

B.P. 147 

79005 NIORT CEDEX 

Tel: (33) (5) 49-33-10-40 

Fax: (33) (5) 49-33-24-16 

Middle East customers: 

IN-SERVICES MIDDLE EAST

Abu Dhabi International Airport 

Cargo Village Area – PO Box n° 106675 

ABU DHABI – UNITED ARAB EMIRATES 

Tel: (971) 2575 7088 

Fax: (971) 2575 8482 

- American customers: 

ZODIAC SERVICES AMERICAS 

W175 N5737 Technology Drive 

MENOMONEE FALLS, WI 53051 

USA 

Tel: (262) 293 1000 

Fax: (262) 293 1010 

- Asian customers: 

ZODIAC SERVICES ASIA 

36, Loyang drive 

SINGAPORE 508949 

Tel: (65) 6579 2230 

Fax: (65) 6579 2231 

E. Reidentified Parts 

(1) Aux DCPC P/N 320GC03Y04 all amdt become 320GC03Y04 Amdt H. 

(2) Aux DCPC P/N 320GC03Y05 all amdt become 320GC03Y05 Amdt H. 

(3) Aux DCPC P/N 320GC03Y06 all amdt become 320GC03Y06 Amdt C.

(4) Aux DCPC cover P/N GC063847Y02 becomes P/N GC063847Y03. 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 6/22

F. Tooling – Price and Availability 

On request. 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 7/22

3. ACCOMPLISHMENT INSTRUCTIONS

A. Job Set-up 

Refer to BD-100 Aircraft Maintenance Manual for the job set-up. 

B. Procedure 

(1) General 

N/A. 

(2) Tools required 

P/N or REFERENCE QTY NAME 

No specific 1 Electromechanical tool set 

OUT245 1 Specific tool 

OUT248 1 Specific tool 

FJ1 10-161 1 Tool holder 

22A.TJ32 1 Drill 

(3) Material and consummables required

P/N or REFERENCE QTY NAME 

GC0003033Y00 1 Kit 

Loctite 7400 AR Red Varnish 

Loctite 222E AR Threadlock 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 8/22

The kit P/N GC0003033Y00 contains : 

P/N or REFERENCE QTY NAME 

GC0003008Y00 1 Reinforcement long 

GC0003009Y00 2 Reinforcement short 

0BE61-00411 8 Rivet Ø3.2x8 Inox 

DEQ1CK030010U 20 Screw Chc M3x10 

520301-70 24 Washer Ø3 

JFCC030U 10 Washer Ø3 

JECC030U 4 Washer Ø3 

15-386 8 Cap Helavia Ø5 

ENMET12-30 10 Spacers 

GC0003074Y00 2 Stop support 

DEQ1CK030006U 4 Screw Chc M3x6 

(4) Procedure 

WARNING: OBEY ALL THE SAFETY PRECAUTIONS WHEN YOU DO MAINTENANCE 

ON OR NEAR ELECTRICAL/ELECTRONIC EQUIPMENT. IF YOU DO NOT 

OBEY THE SAFETY PRECAUTIONS, YOU CAN CAUSE INJURY TO 

PERSONS AND DAMAGE TO EQUIPMENT. 

(a) Obey all the electrical/electronic safety precautions (Refer to TASK 

24−00−00−910−801). 

(b) Obey all the electrostatic−discharge safety precautions (Refer to TASK 

24−00−00−910−802). 

WARNING: REMOVE ALL ELECTRICAL POWER FROM THE AIRCRAFT BEFORE YOU 

DO THE MAINTENANCE. PUT WARNING PLACARDS AT THE EXTERNAL 

POWER RECEPTACLE AND IN THE FLIGHT COMPARTMENT. THIS IS 

NECESSARY TO PREVENT ELECTRICAL SHOCK OR DAMAGE TO 

EQUIPMENT. 

IF YOU DO NOT DO THIS, YOU CAN CAUSE INJURIES TO PERSONS 

AND DAMAGE TO THE EQUIPMENT. 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 9/22

(a) Unlock the seven turnlock fasteners (1) : 

(b) Remove the cover assembly. 

(c) Loosen the screws (2) and the washers (3) from on the cover assembly. 

(d) Remove the cover (4) from the cover (5). 

(e) Loosen the screws (6) and the washers (7) from on the cover (5) 

(f) Remove the spacers (8) and the washers (9) from the cover (5). 

Note : Attaching parts and spacers must be discarded. 

1 

2 

3 

4 

5 6 

7 

8 

9 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 10/22

(g) Modification of the cover (5) :

1 Remove the four caps Hélavia D5 (10) : 

Note : Caps must be discarded. 

2 Position the cover (5) between the support plate drilling OUT248-1 (11) and the 

drilling backplate OUT248-2 (12) for drilling on left. 

10 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 11/22

3 Fix the support plate drilling OUT248-1 (11) and the drilling backplate OUT248-

2 (12) with the attaching screw OUT248-3 (13) : 

Note : Make sure that the attaching screw (13) and the guide pin are engaged in 

the cover (5). 

Note : Make sure that the support plate drilling OUT248-1 (11) crushes perfectly 

the cover black seal when you tighten the attaching screw OUT248-3 

(13). 

Note : Make sure that the drilling backplate OUT 248-2 (12) is adapted with the 

cover (5). 

11 

12 

5 

13 11 

12 

5 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 12/22

4 Drill (Ø3,3) vertically the cover (5) using holes of the support plate drilling 

OUT248-1 (11) (two holes ) : 

5 Loosen the attaching screw OUT248-3 (13). 

6 Remove the support plate drilling OUT248-1 (11) and the drilling backplate 

OUT248-2 (12) with attention, to prevent any damages to the cover. 

7 Debur the two holes, using conical cutter Ø 6,3. 

8 Position the cover (5) between the support plate drilling OUT248-1 (11) and the 

drilling backplate OUT248-2 (12) for drilling on right. 

11 

5 

12 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 13/22

9 Fix the support plate drilling OUT248-1 (11) and the drilling backplate OUT248-

2 (12) with the attaching screw OUT248-3 (13) : 

Note : Make sure that the attaching screw (13) and the guide pin are engaged in 

the cover (5) (on the holes of the caps (10)). 

Note : Make sure that the support plate drilling OUT248-1 (11) crushes 

perfectly the cover black seal when you tighten the attaching screw 

OUT248-3 (13). 

Note : Make sure that the drilling backplate OUT 248-2 (12) is adapted with the 

cover (5). 

10 Drill (Ø3,3) vertically the cover (5) using hole of the support plate drilling 

OUT248-1 (11) (one hole ) : 

5 

13 11 

12 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 14/22

11 Loosen the attaching screw OUT248-3 (13). 

12 Remove the support plate drilling OUT248-1 (11) and the drilling backplate 

OUT248-2 (12) with attention, to prevent any damages to the cover. 

13 Debur the hole, using conical cutter Ø 6,3. 

14 Remove the cover black seal where the stop supports (14) will come. 

Note : the stop supports will be fixed later. 

15 Remove the adhesive marks with ethylic alcohol. 

16 Position the cover (5) between the drilling gauge OUT245-1 (15) and the 

backplate OUT245-2 (16). 

14 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 15/22

17 Position the drillling gauge OUT 245-1 (15) on the cover (5). 

Note : Make sure that the attaching screws (17) and the guide pin (18) are 

engaged in the cover (5). 

18 Fix the drilling gauge OUT245-1 (15) and the backplate OUT245-2 (16) with the 

two attaching screws OUT245-3 (17) : 

5 

15 

16 

16 17 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 16/22

Note : Make sure that the backplate OUT245-2 (16) crushes perfectly the cover 

black seal (19) when you tighten the attaching screws OUT245-3 (17). 

Note : Make sure that the backplate (16) is adapted with the cover (5). 

19 Drill (Ø3,3) vertically the cover (5) using holes of the drilling gauge OUT245-1 

(15) (eight holes ) : 

20 Loosen the attaching screws (17). 

21 Remove the drilling gauge (15) and the backplate (16) with attention, to prevent 

any damages to the cover. 

5 

17 

18 

19 16

15 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 17/22

22 Debur the eight holes, inside the cover (5) (on black seal side), using conical 

cutter Ø 6,3. 

23 Remove the cover black seal (19) where the rivets will come, using punch Ø8. 

24 Remove the adhesive marks with ethylic alcohol. 

25 Make sure that the cover is clean. 

26 Install the four caps on the two stop supports (14) (two caps by support): 

Note : Make sure that caps are correctly positionned in the stop supports. 

27 Install the two stop supports (14) on the cover (5) with four washers JECC030U, 

four washers 520301-70 and four screws DEQ1CK030006U : 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 18/22

28 Tighten the four screws to 0.68 N.m (6 lbf.in). 

29 Put a drop of red varnish on the screws head. 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 19/22

30 Rivet the two short (20) reinforcements on the cover (5) with two rivets for each 

one, using riveting gun with opening Ø3,2. 

Note : engage rivets on interior side of the cover. 

31 Rivet the long (21) reinforcement on the cover (5) with four rivets, using riveting 

gun with opening Ø3,2. 

Note : engage rivets on interior side of the cover. 

20 

21 

5 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 20/22

(h) Install the four new caps Hélavia D5.

(i) Install the washers (9) and the spacers (8) on the cover (5). 

(j) Put threadlock on the screws (6).

(k) Install the washers (7) and the screws (6) on the cover (5). 

(l) Put a drop of red varnish on the screws head. 

(m) Install the cover (4) on the cover (5). 

(n) Put threadlock on the screws (2).

(o) Install the washers (3) and the screws (2) on the cover (4) 

(p) Put a drop of red varnish on the screws head. 

3 – P/N 520301-70 2 – P/N DEQ1CK030010U 

4 – Cover 

6 – P/N DEQ1CK030010U 

5 – Cover 

8 – P/N ENMET12-30 

7 – P/N 520301-70 

9 – P/N JFCC030U 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 21/22

(q) Install the cover assembly on the AUX DCPC by locking turnlock fasteners. 

(5) Marking 

Write the new amendment on the AUX DCPC on the identification label, using permanent 

marker. 

Write the new cover P/N GC063847Y03 inside the cover, using permanent marker. 

Add “R” at the end of the S/N on the identification label. 

(6) Testing and close-up 

No functional test needed. 
ECE 

AIRCRAFT SYSTEMS 

DATE: DEC 15/12 SERVICE BULLETIN: 320GC03Y-24-012

REVISION N°: 3 PAGE : 22/22

ANNEX 1 : OUT245 and OUT248

Note : dimensions are given in millimeters (mm) and in inches between brackets (po)
1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

9

9

10

10

11

11

12

12

13

13

14

14

15

15

16

16

A A

B B

C C

D D

E E

F F

G G

H H

I I

J J

K K

L L

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

Brpmond X

02/07/2012 A0

1/1

GABARIT DE PERCAGE DES TROUS DE FIXATION DES RENFORTS CAPOT/TEMPLATE FOR

DRILLING HOLES IN REINFORCED COVER/CHALLENGER 300

OUT245 1 2 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

5

2 1 9

2 1 9

7

8

7

8

6

MISE EN PLACE DU CAPOT / SETTING UP THE COVER 

970GC02Y

580

3

0

12

0

Reference of the different covers that can be drilled on assembly:

 - Ref. 970GC02Y box -> ref. cover corresponding GC057011Y

 - Ref. 975GC02Y box -> ref. cover corresponding GC057281Y

 - Ref. 320GC03Y box -> ref. cover corresponding GC063829Y

Rpfprence des diffprents capots pouvant rtre percps sur le montage:

 - rpf. boitier 970GC02Y -> rpf. capot correspondante GC057011Y

 - rpf. boitier 975GC02Y -> rpf. capot correspondante GC057281Y

 - rpf. boitier 320GC03Y -> rpf. capot correspondante GC063829Y

4

3
1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

9

9

10

10

11

11

12

12

A A

B B

C C

D D

E E

F F

G G

H H

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

Brpmond X

02/07/2012 A1

1/1

GABARIT DE PERCAGE DES TROUS DE FIXATION DES RENFORTS CAPOT/TEMPLATE FOR

DRILLING HOLES IN REINFORCED COVER/CHALLENGER 300

OUT245 2 2 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

MISE EN PLACE DU CAPOT / SETTING UP THE COVER

975GC02Y

MISE EN PLACE DU CAPOT / SETTING UP THE COVER 

320GC03Y
B-B ( 1 : 1 )

B

B

1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

9

9

10

10

11

11

12

12

A A

B B

C C

D D

E E

F F

G G

H H

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

Brpmond X

02/07/2012 A1

1/1

GABARIT DE PERCAGE DES TROUS DE FIXATION DES RENFORTS CAPOT/TEMPLATE FOR

DRILLING HOLES IN REINFORCED COVER/CHALLENGER 300

OUT245 2 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

583

3

3

12

3

2 foret 3.3

emplacement pour outil d'pbavurage / location for deburring tool

153

29

11,5

100

2

0

2

0

7,5

35

215

MARQUAGE SUR LA BOITE / MARKING ON THE BOX :

OUT245 F0214
Rep Nb REFERENCE DESIGNATION NORME UTILISATION FOURNISSEUR MASSE / WEIGHT

 21 ISO 4762 - M4 x 25 Vis cylindrique j six pans creux 0,004 kg

22 06132-040 TÇTE MOLETe POUR VIS CHC M4 / KNURLED HEAD SCREW CHC M4 NORELEM 0,001 kg

233 B45033000 CANON DE PERCAGE - DIN 179A - 3.3x8/DRILL GUIDE SUPRATEC 0,000 kg

24 B45033000 CANON DE PERCAGE - DIN 179A - 3.3x8 COURT/DRILL GUIDE SUPRATEC 0,000 kg

15 OUT245-1 PLAQUE SUPPORT PERCAGE / SUPPORT PLATE DRILLING 0,75405 kg

16 OUT245-2 CONTRE PLAQUE DE PERCAGE / DRILLING BACKPLATE 0,80193 kg

27 OUT245-3 PION DE CENTRAGE / CENTERING 0,00130 kg

28 OUT245-4 LOCATING 0,00097 kg

29 OUT245-5 CANON TARAUDE / THREADED BARREL 0,00102 kg

DESSINE PAR / DRN BY: VERIFIE PAR / CHK BY:

DATE: CLASSEMENT / USE:

TITRE / TITLE: ECH/SCALE:

TELEPHONE/PHONE: +33 01 56 06 10 00

E C E TELECOPIE/FAX: +33 01 56 06 10 10

CODE OTAN NUMERO DESSIN - DRAWING NUMBER

FICHIER:

PAGE

F0214 INDICE

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION

129 Bd Davout - B.P. 113

75960 PARIS Cedex 20 - FRANCE

/

Bremond X.

10/07/2012 OUT245

A4

1/1 NOMENCLATURE OUT245

NOMOUT245 1 1 

0

NATO CODE

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT

SHEET

REVISION
A ( 2 : 1 )

B-B ( 1 : 1 )

C-C ( 1 : 1 )

D ( 2 : 1 )

E-E ( 1 : 1 )

A

B

B

C

C

D

E

E

1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

9

9

10

10

11

11

12

12

A A

B B

C C

D D

E E

F F

G G

H H

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

EN AW-2017A T4 selon EN754

Brpmond X

10/07/2012 A1

1/1

PLAQUE SUPPORT PERCAGE / SUPPORT PLATE DRILLING

OUT245-1 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

150 mm [5.906 po]

12

0

m

m [4.7

2

4

p

o]

10

m

m [0.3

9

4

p

o]

12,6 mm [ ] 0.496 po

350 mm [13.780 po]

580 mm [22.835 po]

15,8 mm [ ] 0.622 po

38 mm [ ] 1.496 po

180,3 mm [7.098 po]

87,3 mm [3.437 po]

2,5 mm [0.098 po]

120 mm [ ] 4.724 po

2

4,5

m

m

0.9

6

5

p

o [ ]

5

3

m

m

2.0

8

7

p

o [ ]

P6 - 0

+0,02 17 x mm

[17 x P 0.236 +0.000787/0 po]

R10 mm [0.394 po]

R3 mm [0.118 po]

6 x P10 mm Dpbouchant 

[6 x  0.394 po Leading] 

12 mm [0.472 po]

292 mm [11.496 po]

2 mm [0.079 po] 12 mm [0.472 po]

2 mm [0.079 po]

2,5

m

m [0.0

9

8

p

o]

25 mm [ ] 0.984 po

34 mm [ ] 1.339 po

101 mm [ ] 3.976 po

94 mm [ ] 3.701 po

5,3 mm [ ] 0.209 po

21 mm [0.827 po]

40 mm [1.575 po]

8,66 mm [0.341 po] 10 mm [0.394 po]

R1 mm [0.039 po]

P8 mm [0.315 po]

Q8 mm [0.315 po]

R1 mm [0.039 po]

23 mm [0.906 po]

21,5 mm [0.846 po]

185 mm [7.283 po] 63 mm [2.480 po]

130 mm [ ] 5.118 po

21 mm [0.827 po]

15 mm [0.591 po]

3

0

m

m [1.181 p

o]

21 mm [0.827 po]

25 mm [0.984 po] 142 mm [5.591 po]

5 mm [0.197 po]

14 mm [0.551 po]

2

0

m

m [0.7

8

7

p

o]

7 mm [0.276 po]

7 mm [0.276 po]

LES DIFFERENTS MARQUAGES AURONT UNE PROFONDEUR DE 0.3MM

/ DIFFERENT MARKINGS WILL HAVE A DEPTH 0.0118 po

2 mm [0.079 po]

51 mm [2.008 po]

205,2 mm [8.079 po]

271,7 mm [10.697 po]

298,2 mm [11.740 po]

324,2 mm [12.764 po]

15

m

m [0.5

91 p

o]

13 mm [0.512 po]

10,4

m

m [0.4

0

9

p

o]

4 P

H6

(4

4,008

) mm

0.157 H6

(0.157

0.158

)

po

[

]

6 x

60 mm [2.362 po] 233 mm [9.173 po]

13,5

m

m [0.5

31 p

o]

223 mm [8.780 po]

13 mm [0.512 po]

16 mm [0.630 po]

2 mm [0.079 po]

10

m

m [0.3

9

4

p

o]

2

m

m [0.0

7

9

p

o]

10 mm [0.394 po]

20 mm [0.787 po]

15 mm [0.591 po]

10 mm [0.394 po]

R3 mm [0.118 po]

R3 mm [0.118 po]

R4,5 mm [0.177 po]

37 mm [1.457 po]

Masse piqce estimpe: 0,754 kg

Estimated weight: 1.540 Ib

R10

mm

[0.394 po]

R10 mm [0.394 po]

fraisurage 60 dans chaque peroage de 3.3 du cotp marquage /

60  in each countersinking bore 0.129 po marking the side 

10 mm [0.394 po]

R4 mm [0.157 po]

R2 mm [0.079 po]

L P0.03 [P0.00118]

110 mm [4.331 po] 20 mm [0.787 po]

Ch 0,5 mm X 45

[Ch 0.0196 po X 45]

6 mm [0.236 po]

2

8

m

m [1.10

2

p

o]

100 mm [ ] 3.937 po

49 mm [ ] 1.929 po

100 mm [ ] 3.937 po 109 mm [ ] 4.291 po

85 mm [ ] 3.346 po 40 mm [ ] 1.575 po

17

94 mm [ ] 3.701 po 94 mm [ ] 3.701 po

5

0

m

m 1.9

6

9

p

o [ ] 15,6

m

m

0.614

p

o [ ]

6 P H6

(6

6,01

) mm

0.236 H6

(0.23

0.2

6

37

)

po

[

]

8x

L P0,03 [0.00118]

41 m

m 1.614

p

o [ ] 5

0

m

m 1.9

6

9

p

o [ ]

15 mm [0.591 po]

5 mm [0.197 po]
1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

9

9

10

10

11

11

12

12

A A

B B

C C

D D

E E

F F

G G

H H

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

EN AW-2017A T4 selon EN754

Brpmond X

10/07/2012 A1

1/1

CONTRE PLAQUE DE PERCAGE / DRILLING BACKPLATE

OUT245-2 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

P5,2 mm Dpbouchant 

[ 0.205 po Leading] 

M4x0.7

274,00 mm [10.787 po]

17,0

0

m

m [0.6

6

9

p

o]

100,00 mm [ ] 3.937 po 100,00 mm [ ] 3.937 po

101,00 mm [ ] 3.976 po

34,00 mm [ ] 1.339 po

40,00 mm [ ] 1.575 po

25,00 mm [ ] 0.984 po

49,00 mm [ ] 1.929 po

2,5

0

m

m

0.0

9

8

p

o [ ]

38,00 mm [ ] 1.496 po

94,00 mm [ ] 3.701 po 94,00 mm [ ] 3.701 po 94,00 mm [ ] 3.701 po

130,00 mm [ ] 5.118 po

17,00 mm [0.669 po]

21,50 mm [0.846 po]

5

0,0

0

m

m 1.9

6

9

p

o [ ]

21,00 mm [0.827 po]

41,0

0

m

m 1.614

p

o [ ] 5

0,0

0

m

m 1.9

6

9

p

o [ ]

24,50 B0,02 mm [0.965 B0.001 po]

28,50 B0,02 mm [1.122 B0.001 po]

87,30 mm [3.437 po]

15,80 mm [ ] 0.622 po

M4x0.7

5x P5,3X P10 Z 12

5 x 0.209X P0.394 Z 0.224

223,00 mm [8.780 po] 60,00 mm [2.362 po] 180,00 mm [7.087 po]

11,50 mm [0.453 po]

120,00 mm [ ] 4.724 po

11,9

0

m

m

0.4

6

9

p

o [ ]

4

0,0

0

m

m [1.5

7

5

p

o]

15,00 mm [0.591 po]

12,0

0

m

m [0.4

7

2

p

o]

2

8,0

0

m

m [1.10

2

p

o]

118,0

0

m

m [4.6

4

6

p

o]

9,00 mm [0.354 po]

150,00 mm [5.906 po]

496,00 mm [19.528 po]

12,00 mm [0.472 po]

7,00 mm [0.276 po]

16,00 mm [0.630 po]

327,00 mm [12.874 po]

332,00 mm [13.071 po]

110,00 mm [4.331 po]

129,00 mm [5.079 po]

14,00 mm [0.551 po]

15,6

0

m

m

0.614

p

o [ ]

5,30 mm [ ] 0.209 po

18,00 mm [0.709 po]

205,20 mm [8.079 po]

271,70 mm [10.697 po]

298,20 mm [11.740 po]

8,0

0

m

m [0.315

p

o]

Masse piqce estimpe: 0,802 kg

estimated weight:1,768 Ib

R5,00 mm [0.197 po]

R3,00 mm [0.118 po]

4

9,0

0

m

m [1.9

2

9

p

o]

2,0

0

m

m [0.0

7

9

p

o]

P5,2 mm Dpbouchant

[ 0.205 po Leading] 

P5,2 mm Dpbouchant

[ 0.205 po Leading] 

P5,2 mm Dpbouchant

[ 0.205 po Leading] 

M4x0.7 M4x0.7

M4x0.7

M4x0.7

R3,00

mm [0.118

po]

R10,00 mm [0.394 po]

R3,00 mm [0.118 po]

M4x0.7

P48 x mm

[8 x P0.157 po]

L P0.2 [P0.079]

P417 x mm

[17 x P0.157 po]

L P0.2 [P0.079]

4 x P10 mm Dpbouchant

[4 x 6 x  0.394 po Leading] 

20,00 mm [0.787 po]

15,00 mm [0.591 po]

Ch 0,5 mm X 45

[Ch 0.0196 po X 45]
MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

X8CrNiS18.9 selon EN 10088

Brpmond X 

10/07/2012 A4

1/1

PION DE CENTRAGE / CENTERING

OUT245-3 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

P4 + 0,01

+ 0,02 mm

[P0.157 +0.0008/+0.0004 po] 5,00 mm [0.197 po]

6,00 mm [0.236 po]

60

2,00 mm [0.079 po]

Ch 0,2 mm X 45

[Ch 0.0078 po X 45]

Masse piqce estimpe: 0,001 kg

Estimated weight: 0.0022 Ib

P5,1 - 0,02

0+

 mm

[P0.201 +0/-0.0008 po]
MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

X8CrNiS18.9 selon EN 10088

Brpmond X 

10/07/2012 A4

1/1

LOCATING

OUT245-4 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

=2,00 mm [0.079 po]=

Masse piqce estimpe: 0,001 kg

Estimated weight: 0.0022 Ib

5,2 - 0,02

0+ P mm

[P0.201 +0/-0.0008 po]

P4 + 0,01

+ 0,02 mm

[P0.157 +0.0008/+0.0004 po]

60

2,00 mm [0.079 po]

6,00 mm [0.236 po]

5,00 mm [0.197 po]

Ch 0,2 mm X 45

[Ch 0.0078 po X 45]
A-A ( 3 : 1 )

A

A

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

EN AW-2017A T4 selon EN754

Brpmond X 

10/07/2012 A4

1/1

CANON TARAUDE / THREADED BARREL

OUT245-5 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

6,00 mm [0.236 po]

3,00 mm [0.118 po]

P4,2 mm

[P0.165 po]

4

M

Ch 0,2 mm X 45

[Ch 0.078 po X 45]

Masse piqce estimpe: 0,001 kg

Estimated weight: 0.0022 Ib

P9,6 mm

[P0.378 po]
1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

9

9

10

10

11

11

12

12

13

13

14

14

15

15

16

16

A A

B B

C C

D D

E E

F F

G G

H H

I I

J J

K K

L L

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

Brpmond X

02/07/2012 A0

1/1

GABARIT DE PERCAGE DES TROUS DE FIXATION DES APPUI DE CARTES/TEMPLATE FOR

DRILLING HOLES FOR FIXING SUPPORT CARD/CHALLENGER 300

OUT248 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

7 1 2

MISE EN PLACE DU CAPOT / SETTING UP THE COVER 

320GC03Y

Reference of the different covers that can be drilled on assembly:

 - Ref. 320GC03Y box -> ref. cover corresponding GC063829Y

Rpfprence des diffprents capots pouvant rtre percps sur le montage:

 - rpf. boitier 320GC03Y-> rpf. capot correspondante GC063829Y

5

PERCAGE A DROITE / DRILLING RIGHT

PERCAGE A GAUCHE / DRILLING LEFT

3

4

6
Rep Nb REFERENCE DESIGNATION NORME UTILISATION FOURNISSEUR MASSE / WEIGHT

 11 ISO 4762 - M5 x 25 Vis cylindrique j six pans creux 0.006 kg

12 06132-050 TÇTE MOLETe POUR VIS CHC M4 / KNURLED HEAD SCREW CHC M4 06132 - Knurled heads for hexagon socket screw 0.001 kg

33 B45033000 CANON DE PERCAGE - DIN 179A - 3.3x8/DRILL GUIDE SUPRATEC 0.000 kg

14 OUT248-1 PLAQUE SUPPORT PERCAGE / SUPPORT PLATE DRILLING 0.14806 kg

15 OUT248-2 CONTRE PLAQUE DE PERCAGE / DRILLING BACKPLATE 0.21003 kg

16 OUT248-3 PION DE CENTRAGE / CENTERING 0.00129 kg

17 OUT248-4 CANON TARAUDE / THREADED BARREL 0.00084 kg

DESSINE PAR / DRN BY: VERIFIE PAR / CHK BY:

DATE: CLASSEMENT / USE:

TITRE / TITLE: ECH/SCALE:

TELEPHONE/PHONE: +33 01 56 06 10 00

E C E TELECOPIE/FAX: +33 01 56 06 10 10

CODE OTAN NUMERO DESSIN - DRAWING NUMBER

FICHIER:

PAGE

F0214 INDICE

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION

129 Bd Davout - B.P. 113

75960 PARIS Cedex 20 - FRANCE

/

Bremond X.

10/07/2012 OUT245

A4

1/1 NOMENCLATURE OUT248

NOMOUT248 1 1 

0

NATO CODE

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT

SHEET

REVISION
B-B ( 1 : 1 )

B

B

1

1

2

2

3

3

4

4

5

5

6

6

A A

B B

C C

D D

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

EN AW-2017A T4 selon EN754

Brpmond X 

10/07/2012 A3

1/1

PLAQUE SUPPORT PERCAGE / SUPPORT PLATE DRILLING

OUT248-1 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

136 mm [5.354 po]

5

0

m

m [1.9

6

9

p

o]

6 mm [0.236 po]

LES DIFFERENTS MARQUAGES AURONT UNE PROFONDEUR DE 0.3MM

/ DIFFERENT MARKINGS WILL HAVE A DEPTH 0.0118 po

Masse piqce estimpe: 0.148 kg

Estimated weight: 1.540 Ib

L 0.03 [0.00118]

67 mm [2.638 po]

24,4 mm [ ] 0.961 po

5

m

m

0.19

7

p

o [ ]

13,7

m

m

0.5

3

9

p

o [ ]

61,9 mm [ ] 2.437 po 61,9 mm [ ] 2.437 po

21,5

P5 mm [0.197 po]

P4 H6 (4

4,01)

 mm 0.157 H6

(0.157

0.158

)

 po [ ]

P6 + 0

- 0,03 mm 0.236 + 0

- 0.001 po [ ]

3x 
1

1

2

2

3

3

4

4

5

5

6

6

A A

B B

C C

D D

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

Brpmond X 

10/07/2012 A3

1/1

CONTRE PLAQUE DE PERCAGE / DRILLING BACKPLATE

OUT248-2 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

Masse piqce estimpe: N/A 

estimated weight:1,768 Ib

P5,2 mm [0.205 po]

24,4 mm [0.961 po]

5

m

m [0.19

7

p

o]

13

7, m

m

0[ .5

3

9

p

o]

21,5 mm [0.846 po]

M5x0.8

61,9 mm [2.437 po]

61,9 mm [2.437 po]

P6 mm [0.236 po]

3x

6

m

m

0[ 2. 3

6

p

o]

12 mm [0.472 po] 15 mm [0.591 po]

6

m

m [0

2. 3

6

p

o]

67 mm [2.638 po]

R5 mm [0.197 po] 12 mm [0.472 po]

Ch 0,5 X 45

136 mm [5.354 po]

5

0

m

m 1[ 9. 6

9

p

o]

R2 mm [0.079 po]
MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

X8CrNiS18.9 selon EN 10088

Brpmond X 

10/07/2012 A4

1/1

PION DE CENTRAGE / CENTERING

OUT248-3 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

P4 + 0,01

+ 0,02 mm

[P0.157 +0.0008/+0.0004 po]

5 mm [0.197 po]

6 mm [0.236 po]

60

2 mm [0.079 po]

Masse piqce estimpe: 0.001 kg

Estimated weight: 0.0022 Ib

P5,1 - 0,02

0+

 mm

[P0.201 +0/-0.0008 po]
A-A ( 3 : 1 )

A

A

MATIERE/MATERIAL

TRAITEMENT/TRTMT

PROTECTION :

DESSINE PAR - DRN BY: VERIFIE PAR - CHK BY:

DATE: UTILISATION - USE:

ISO 2768-mk

NUMERO DESSIN - DRAWING NUMBER

FICHIER:

F0214

CE DOCUMENT EST LA PROPRIETE DE ECE. IL NE PEUT ETRE REPRODUIT OU COMMUNIQUE SANS AUTORISATION ECRITE PREALABLE.

THIS DOCUMENT IS ECE'S EXCLUSIVE PROPERTY. ANY COPY OR DISCLOTURE ARE SUBJECT TO ECE'S PRIOR WRITTEN CONSENT.

/

EN AW-2017A T4 selon EN754

Brpmond X 

10/07/2012 A4

1/1

CANON TARAUDE / THREADED BARREL

OUT248-4 1 1 0

ECHELLE

SCALE

CODE OTAN

NATO CODE

FORMAT

SIZE

INDICE 

REVISION

PAGE 

SHEET

TOLERENCES GENERALES 

GENERAL TOLERENCES

TITRE

TITLE

ETAT DE SURFACE 

SURFACE ROUGHNESS

SURFACE MOUILLEE 

WET AREA

ATTENTION: LES COTES INDIQUEES SONT CELLES 

OBTENUES APRES TRAITEMENT ET PROTECTION.

CAUTION: INDICATED TOLERENCE TAKE TREATMENT 

AND PROTECTION INTO ACCOUNT.

ECE - 271 Rue du chkteau Musset - 79005 NIORT - FRANCE

TELEPHONE - PHONE +33 (0) 5 49 33 10 40 - TELECOPIE - FAX +33 (0) 5 49 33 24 16

6 mm [0.236 po]

3 mm [0.118 po]

P6,2 mm

[P0.165 po]

5

M

Ch 0,2 mm X 45

[Ch 0.078 po X 45]

Masse piqce estimpe: 0.001 kg

Estimated weight: 0.0022 Ib

P9,6 mm

[P0.378 po]