Citation preview

NSA9117

IDENTIFICATION PLATE AIRCRAFT AND CONSTITUENT ASSEMBLIES

Issue :

BF

Date :

Sep 15

Page :

1/42

SUMMARY 1 -

GENERAL

2 -

REFERENCE SYSTEM

3 -

IDENTIFICATION PLATES PRODUCTION DIRECTIVES

4 -

LAY-OUT AND DEFINITION OF THE PLATES

5 -

OLD PRODUCTIONS (Not to be used, not to be supplied)

6 -

MANUFACTURERS

AMENDMENT RECORD SHEET 1 -

GENERAL The purpose of this document is to specify and define the identification plate to be used for: . Aircraft: - Manufacturer, - Owner. . Assemblies/sub-assemblies such as: - Doors, - Flaps, - Slats, etc.... . VU . VE . The manufacturer's code. . Concessions record. . Record of production/service bulletins modifications. . Completion rules for Airbus identification plates are detailed in A1056.

The content of this document is the property of AIRBUS FRANCE. It is supplied in confidence and commercial security on its contents must be maintained. It must not be used for any purpose other than that for which it is supplied nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from AIRBUS FRANCE. AIRBUS FRANCE Trade Secrets or Commercial or Financial information, 5 U.S.C. (b) (4).  AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

2

Important notes:

2 -

Manufacturer code (MFR) is defined by NCAGE code, which replaces the previous NSCM manufacturer code (Nato Supply Codes for Manufacturer). MFR (NCAGE) for Airbus S.A.S. -all Airbus proprietary part- to be written on concerned plates is: FAPE3. Plates with former FSCM can be “used as long as supplies last”.

REFERENCE SYSTEM 2.1 - General A specific part number (PN) shall be allocated to each type of plate according to its definition. The PN and suffix shall appear on the plate. 2.2 - Part number (PN) structure Example of part number identification to be used on drawing schedules: NSA9117-60, Plate Example of part number construction: The suffix shall identify the partner and country which has production responsibility. 2.3 - Suffix (for procurement purposes) (identification plate NSA9117: see page 16) NSA9117

-

60

F Suffix

Basic reference

(for procurement purposes) (see § 2.3)

Plate type (see § 3.1)

Note: Attention restricted usage: This data plate is only procurable by AIRBUS recognized repair stations in accordance with procedures agreed between, AIRBUS, the REPAIR STATION and the local CIVIL AVIATION AUTHORITY. Table 1 SUFFIX F E S D N B I C T P A V

3 -

ENTITY / INDUSTRIAL AIRBUS France AIRBUS UK AIRBUS Spain AIRBUS Germany FOKKER SONACA ALENIA FLABEL TAI MTAD DENEL AEROSUD

COUNTRY France England Spain Germany Nederland Belgium Italy Belgium Turkey Spain South Africa South Africa

IDENTIFICATION PLATES PRODUCTION DIRECTIVES 3.1 - General characteristics

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

3

Table 2 PLATE TYPE New production DEFINITION TYPE OF OF Old Used by production IDENTIFICATION CHARACTERS AIRBUS F France -

08

01

-07, -09

-01 26

-01 06

-02

-

-05 -75

03 -

-78

-

M5

M1

M7

M3

M6

M2

M8

M4

-60, -66

-

-20 -26 -72 -79 -73

-64

-23 -28 -76 -77 -22 -27 -24

-65

-25

-63 -69 -62, -67

-29 -04

-61 -70 -71 -74 -55, -57, -58, -59

-10 -11

-12

Corrosion Resistant Steel Z10CNT18 or Equivalent Aircraft constituent assemblies

Photoengraved or printed

-12

Photoengraved

-

-

-

-

-

-

-

THICKNESS (mm)

0,05

White 350 gsm Matt Card

0,5 0,07

0,5

Rivet

-

-12

FIXING METHOD

As per Small constituent NSA931025-06 assemblies Photoengraved Polyester Bonding (small VU) foil self-adhesive Manufacturer's Photoengraved code As per or Bonding* NSA931029-01R Printed Concessions White 350 gsm Temporary as Printed Matt Card appropriate Modifications Rivet Service bulletins Small items Bonding* Modifications Aluminium Service bulletins A5 Except small or items equivalent Photoengraved

-

-21

MATERIAL

Printed Aircraft constituent assemblies (hot area)

Polyester foil Polyimide Aluminium A5 or equivalent As per NSA931025-01

Z10CNT18 or Z3CN18 50 hbars

0,8

Bonding self-adhesive* Bonding*

0,07 0,1 0,07 to 0,13

Rivet

0,5

Bonding*

0,07 to 0,13

Rivet

0,5

Bonding*

0,15 to 0,27

-42 -30, -40, -41, Engraved Rivet 0,8 Aircraft -48 -43, -44, -45, manufacturer -49 -46, -47, -68 -56 -50, -51, -53 Aircraft owner -54 -31, -32, -52 -23 Large or small Photoengraved Polyester Bonding -63 -28 -13 aircraft 0,07 or printed foil self-adhesive* -80 assemblies * Note: - Use qualified material for bonding. - Plates shall be varnished after installation when installed in slight synthetic hydraulic fluid splashing areas, then clear varnish.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

4

3.2 - Ground color - Matt black

: -01, -02, -04, -06, -07, -08, -09, M5, M6, M7, M8, -20, -21, -22, -23, -24, -25, -26, -28, -29, -40, -42, -43, -44, -45, -46, -47, -48, -49, -60, -61, -62, -64, -65, -66, -67, -68, -70, -71, -72, -73, -74, -76, 77, -79, 80

- Metal protection

: -50, -51, -53, -54, -55, -56, -57, -58, -59

- Red

: -03, -05, -75

- Yellow

: -78

1)

3.3 - Window and character color - Metal

: -01, -02, -03, -04,-05, -06, -07, -08, -09, M5, M6, M7, M8, -20, -21, -22, -23, -24, -25, -26, -28, -29, -40, -42, -43, -44, -45, -46, -47, -48, -49, -60, -61, -62, -63, -64, -65, -66, -67, -68, -69, -70, -72, -71, -73, -74, -75, 76, 77, 79, 80

- Red

: -50, -51, -53,-54, -55, -56, -57, -58, -59, -78

- Black

: -78

- White

: -78

1)

1)

1)

Shall be in accordance with FED STD 595. Red(11310) Yellow(13591) Black(17038)

3.4 - Window and character thickness (engraved) Make impression between 0,1 and 0,4 mm. (In depth for -50, -51, -53, -54, -55, -56, -57; -58, -59 Raised for -21, -42, -43, -44, -45, -46, -47, -48, -49, -61, -68, -70, -71, and -74). 3.5 - Note For plates -50, -51, -53, -54, -55, -56, -57, -58, -59 engraved faces shall be polished. For plates -21, -42, -43, -44, -45, -46, -47, -48, -49, -50, -51, -53, -54, -55, -56, -57, -61, -68, 70, -71, -73, -74 back side shall be cadmium plated. 3.6 - Characters "Folio Bold Condensed" type A B C D E F

10.8C (h = 2,1mm) 10.10C (h = 2,5 mm) 10.12C (h = 3,1 mm) 10.14C (h = 3,7 mm) 10.12C (reduced scale 0,5 ) 10.14C (reduced scale 0,5 )

"AIRBUS France" type According to character types defined on the "cahier des normes de la marque" available at Standardization departments. J K

(h = 1,8 mm) (h = 2,5 mm)

AIRBUS FRANCE 1988. All rights reserved

NSA9117

L M

Issue :

BF

Page :

5

(h = 3 mm) (h = 3,5 mm)

"ALENIA" type As per "ALENIA" documentation P (h = 3,5 mm) "AIRBUS Germany" type J K L

As per DIN 1451-1E1,8 As per DIN 1451-1E2 As per DIN 1451-1E2

"AIRBUS UK" type K L

A I R B U S U K

(h = 1,9 mm) (h = 2,4 mm)

3.7 - Mass Table 3 PLATE CODE No.

MASS (g)

01 - 02 - 03 - 04 - 05 - 06 - 07 - 08 - 09 - 26 - 75

0,06

M1 - M5

2,8

M3 - M7

0,3

M2 - M6

0,9

M4 - M8

6,3

10 - 11 - 20 - 24 - 26 - 60 - 64 – 66 – 72 -79

2,5

12 - 22 - 25 - 27 - 62 - 65 - 67

0,3

30 - 40

33

41 - 42 - 43 - 44 - 45 - 46 - 47 - 48 - 49 - 68 - 70 – 71 - 74

32

31 - 32 - 50 - 51 - 52 – 53 - 54 - 55 - 56 - 57 - 58 - 59

34

13 - 23 - 28 - 63 – 69 – 76 -77 -78

0,2

21 - 61

11,5

29

5,0

73

16.5

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

6

4 -

LAY-OUT AND DEFINITION OF THE PLATES 4.1 - Manufacturer's identification

M

P

AEROSPATIALE ATR - ALENIA TOULOUSE - 31060 FRANCE - EUROP (F6198)

NSA9117-42

A/C MODEL AND TYPE MFG SERIAL N° (MSN) TYPE CERTIFICATE N° AEROSPATIALE PRODUCTION DGAC ORGANIZATION APPROVAL NUMBER PO6 DATE

NSA9117 - 42 M

ATR BLAGNAC - 31712 FRANCE - EUROP (FB429) A/C MODEL AND TYPE NSA9117-48

MFG SERIAL N° (MSN) TYPE CERTIFICATE N° PRODUCTION APPROVAL

F.G.054

JAR 21G NUMBER

NSA9117 - 48

DATE

ATR BLAGNAC - 31712 FRANCE - EUROP (FB429)

NSA9117-49

A/C MODEL AND TYPE MFG SERIAL N° (MSN) TYPE CERTIFICATE N° PRODUCTION APPROVAL PART 21G NUMBER DATE

FR.21G.0054 NSA9117 - 49

Figure 1(continued)

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

7

2 holes for rivets Ø 1,6 100 37

5

14,5 4

4

4

35

29,5

24

18,5

4

1,5 25

32

12* 108 118

Dimensions in mm. *For plate -49: 28 mm. Figure 1 (continued)

AIRBUS FRANCE 1988. All rights reserved

1,5

=

12

1,5

1,5

50

=

0,5

3

NSA9117 Issue :

BF

Page :

8

AIRBUS S.A.S. BLAGNAC - 31707 FRANCE-EUROPE (MFR: FAPE3) A/C MODEL AND TYPE MFR SERIAL N° (MSN)

NSA9117-70

EASA TYPE CERTIFICATE N°

PRODUCTION ORGANIZATION APPROVAL NUMBER NSA9117-70

2 holes for rivets Ø 1,6 100 37

5

14,5 4

4

4

=

12

32

1,5 108 118

Dimensions in mm. Figure 1 (continued)

AIRBUS FRANCE 1988. All rights reserved

12

1,5

1,5

1,5

24

18,5

29,5

39

43

50

=

0,5

3

NSA9117 Issue :

BF

Page :

9

AIRBUS MILITARY S.L. 28022 MADRID - SPAIN - EUROPE A/C MODEL AND TYPE NSA9117-74

MFR SERIAL N° (MSN) CERTIFICATE OF DESIGN AIRBUS DEFENCE AND SPACE S.A.U. PRODUCTION ORGANISATION APPROVAL NUMBER NSA9117-74

2 holes for rivets Ø 1,6 100 37

4

4

39

0,5

5

4

1,5

1,5

50

43

35

29,5

24

18,5

=

3

=

12

32

1,5 108 118

Dimensions in mm. Figure 1 (continued)

AIRBUS FRANCE 1988. All rights reserved

12

NSA9117 Issue :

BF

Page :

10

ATR BLAGNAC - 31712 FRANCE - EUROP (FB429) A/C MODEL AND TYPE MFG SERIAL N° (MSN) TYPE CERTIFICATE N° PRODUCTION APPROVAL PART 21G NUMBER

NSA9117-71

FR.21G.0054 NSA9117 - 71

2 holes for rivets Ø 1,6 100 37

5

14,5 4

4

4

35

29,5

24

18,5

28 108 118

Dimensions in mm. Figure 1 (concluded)

AIRBUS FRANCE 1988. All rights reserved

1,5

=

12

1,5

1,5

50

=

0,5

3

NSA9117 Issue :

BF

Page :

11

4.2 - Owner identification

D

NSA9117-55

AIRBUS

MSN NSA9117- 55

REGISTRATION OWNER C

CAGE ADDRESS AIRWORTHINESS CERTIFICATE

ATR

MSN

REGISTRATION NSA9117-56

NSA9117- 56

OWNER CAGE ADDRESS AIRWORTHINESS CERTIFICATE

AIRBUS

MSN

REGISTERED OWNER NSA9117-58

CAGE ADDRESS AIRWORTHINESS CERTIFICATE

Figure 2 (continued)

AIRBUS FRANCE 1988. All rights reserved

NSA9117- 58

REGISTRATION

C

NSA9117 Page :

12

For plates -55 and -56

62 30

27

30

3 3 3

35

6

25

4

8

8

4

4

56

12

4

4

10

3

4

5

4

BF

r6

Issue :

2

8

4 holes for rivets Ø 1,6

106

For plate -58

25

51

20 2

Dimensions in mm. Figure 2 (continued)

AIRBUS FRANCE 1988. All rights reserved

8

NSA9117 Issue :

BF

Page :

13

NSA9117-54

AIRBUS MILITARY S.L.

D

VERSION

MSN

NSA9117- 54

REGISTRATION OWNER C

CAGE ADDRESS

C

AIRWORTHINESS CERTIFICATE

62

For plates -54

35 27

r6

6

25

30

1 1

1 4

8

8

4

4

56

12

4

35 2 106

Dimensions in mm. Figure 2 (concluded)

AIRBUS FRANCE 1988. All rights reserved

8

4 holes for rivets Ø 1,6

4

1

10

4

4

4

27

5

NSA9117 Issue :

BF

Page :

14

NSA9117-57 D

MSN

C

CAGE NSA9117-57

AIRBUS REGISTRATION OWNER ADDRESS OWNER ADDRESS OWNER ADDRESS

AIRWORTHINESS CERTIFICATE

MSN

REGISTRATION REGISTERED OWNER ADDRESS NSA9117-59

CAGE

REGISTERED OWNER ADDRESS REGISTERED OWNER ADDRESS AIRWORTHINESS CERTIFICATE Figure 3 (continued)

AIRBUS FRANCE 1988. All rights reserved

NSA9117-59

AIRBUS

C

NSA9117

24

16

Page :

15

10 25

1

12

115

Dimensions in mm.

*For plate -59: 40 mm. Figure 3 (concluded)

AIRBUS FRANCE 1988. All rights reserved

6

1

12

103

1,5

6

6

4

20*

1

56

12

1

10

1

4

1,5

4 holes for rivets Ø 1,6

19

BF

4

24

Issue :

NSA9117 Issue :

BF

Page :

16

4.3 - Constituent assemblies identification (except small VU panels) 3

1

6

8

K

NSA9117-60F

A/C PN

MFR DESCR. SER. N° CA CODE MFG DATE NSA9117-60F

4

5

B A/C PN

MFR DESCR. SER. N° CA CODE MFG DATE

C

NSA9117-62F

2

NSA9117-62F

7

NSA9117-61F

E

NSA9117-63D NSA9117-69

Legend 1

NSA9117-69D

-

A/C model and type

-

Serial number

-

NCAGE code (Airbus S.A.S.): FAPE3

-

Manufacturer date

-

Part number

-

Inscription stamp / mark

-

Constituent Assembly code

-

Assembly / subassembly / element description

75 35

0,5

30

1,1

7

6 5

1

r5

1

1

3,8

3,8

3,8

12

1

16

3

1,1

3,8

1

3,8

1

30

3,8

2 holes for rivets Ø 1,6

3,5

23

30

27

r2

33

Dimensions in mm. Figure 4

AIRBUS FRANCE 1988. All rights reserved

70

NSA9117

3

See note 4

4

1

NSA9117-20F

A/C PN

MFR DESCR. SER. N° MFG DATE

K

C

See note 4

BF

Page :

17

B

A/C PN

MFR DESCR. SER. N° MFG DATE

NSA9117-22F

2

Issue :

E

NSA9117-22F 5

7

NSA9117-21F NSA9117-23D NSA9117-76D

A/C PN

MFR DESCR. SER. N° MFG DATE

NSA9117-23D

6

NSA9117-20F

Legend 2

-

A/C model and type

-

Serial number

-

NCAGE code (Airbus S.A.S.): FAPE3

-

Manufacture date

-

Part number

-

Inscription stamp / mark

-

Assembly / subassembly / element description

75

1

16

0,925

r5

0,5

5

3

1,15

2 holes for rivets Ø 1,6

0,925

0,925

3,8

3,8 3,8

3,8

3,5

27

25

33

r2

25

0,925

6

1,15

35 30

3,8

12 7

Dimensions in mm. Figure 5

AIRBUS FRANCE 1988. All rights reserved

70

NSA9117 BF

Page :

18

2

1

3

4

7

6

NSA9117-64F

-

9

NSA9117-64F

A/C MFR PN DESCR. SER. N° CA CODE FOR A/C MSN Legend 3 MFG DATE

K

8

B

A/C MFR PN DESCR. SER. N° CA CODE FOR A/C MSN MFG DATE

C

5

NSA9117-65F

Issue :

E

NSA9117-65F

-

A/C model and type NCAGE code (Airbus S.A.S.): FAPE3 Part number Assembly / subassembly / element description

-

Serial number Manufacture date Inscription stamp / mark Constituent Assembly code Manufacturer serial number

30

5

1

1

0,5

7

6

1,1

35

3,8

12

3,8

2 holes for rivets Ø 1,6

1

16

3

1,1

3,8

3,8

3,5

23 27

34,8

33

Dimensions in mm.

r2

34,8

3,8

r5

1

3,8

3,8

75

Figure 6

AIRBUS FRANCE 1988. All rights reserved

70

NSA9117

4

1

A/C PN

8

NSA9117-24F

K

NSA9117-24F

MFR DESCR. SER N° FOR A/C MSN MFG DATE

3

6

5

C

BF

Page :

19

B

MFR DESCR. SER N° FOR A/C MSN MFG DATE

7

A/C PN

NSA9117-25F

2

Issue :

E

NSA9117-25F

Legend 4

-

A/C model and type

-

Serial number

-

NCAGE code (Airbus S.A.S.): FAPE3

-

Manufacture date

-

Part number

-

Inscription stamp / mark

-

Manufacturer serial number

-

Assembly / subassembly / element description

75

0,5

30

5

1

r5

1

1

7

6

1,1

3,8

3,8

3,8

35

30

3,8

12

3,8

2 holes for rivet Ø 1,6

1

16

1,1

3,8

3 3,5

23

30

27

r2

33

Dimensions in mm. Figure 6

AIRBUS FRANCE 1988. All rights reserved

70

NSA9117 Page :

20 2 See note 4

3

8

A/C PN

MFR PN MECA DESCR. SER. N° CA CODE MFG DATE 6

NSA9117-66F

1

9

K

5

4

B

See note 4

A/C PN

MFR PN MECA DESCR.

C

NSA9117-67F

BF

NSA9117-66F

Issue :

SER. N° CA CODE MFG DATE

7

NSA9117-67F

E

Legend 5

-

A/C model and type

-

Serial number

-

NCAGE code (Airbus S.A.S.): FAPE3

-

Manufacture date

-

Part number

-

Inscription stamp / mark

-

Reference of mechanical assembly

-

Constituent Assembly code

-

Assembly / subassembly / element description

75

0,925

r5

0,5 0,925

1,15

3,8 2 holes for rivets Ø 1,6

16

0,925

3,8 3,8 3,8

3,8

34,725

3,8

1

5

0,925

1,15

30

3,8

7

6

0,925

35

0,925

12

3 3,5

27

34,725

33

r2

Dimensions in mm. Figure 7

AIRBUS FRANCE 1988. All rights reserved

70

NSA9117

See note 4

B

3

4

1

A/C SER

DMF

2

BF

Page :

21

8

MFR NSA9117-72

K

Issue :

Production Data

PNR/CA CODE DESCR. Spare Data

PN DESCR. NSA9117-72F /-73

7

6

E

5

Legend 6



- A/C type and make



-

Part Number Constituent assemblies code



- NCAGE code



-

Assembly / Subassembly / element description



- Manufacturer's date



-

Part number



- Serial number



-

Inscription stamp / mark

75

2 holes for rivets Ø 1,6

38

Dimensions in mm. Figure 8

AIRBUS FRANCE 1988. All rights reserved

0,925

32

1,15

11,025 11,025

12

0,925

6

0,925

12

0,925

8

0,925

3,8

3,8

12

1,15

32

3,8

3,8

3,8

34,725

3,8

16

8

NSA9117 BF

Page :

22 See note 4

K

3

B

4

1

A/C SER

DMF

2

8

MFR NSA9117-79

Issue :

Production Data

PNR/CA CODE DESCR. Spare Data

PN DESCR. NSA9117-79

7

6

E

5

Legend 7



- A/C type and make



-

Part Number Constituent assemblies code



- NCAGE code



-

Assembly / Subassembly / element description



- Manufacturer's date



-

Part number



- Serial number



-

Inscription stamp / mark

75

2 holes for Ø 3,2

38

Dimensions in mm. Figure 10

AIRBUS FRANCE 1988. All rights reserved

11,025 11,025

0,925

32

1,15

12

0,925

6

0,925

12

0,925

8

0,925

3,8

3,8

12

1,15

32

8

3,8

3,8

3,8

34,725

3,8

16

NSA9117

4

6

NSA9117-27F

K

5

8

7

Page :

23

B

See note 4

MFR PN MECA DESCR. SER. N° MFG DATE

BF

A/C PN

NSA9117-26F

3

A/C PN

MFR PN MECA DESCR. SER. N° MFG DATE

C

1

See note 4

NSA9117-27F

2

Issue :

E

NSA9117-26F

Legend 8

-

A/C model and type

-

Serial number

-

NCAGE code (Airbus S.A.S.): FAPE3

-

Manufacture date

-

Part number

-

Inscription stamp / mark

-

Reference of mechanical assembly

-

Assembly / subassembly / element description

75

2 holes for rivets Ø 1,6

27

5

r5

0,925

0,925

0,5

1,15

16

1

0,925

3,8 3,8

3,8

3 3,5

30

33

r2

30

0,925

30

0,925

7

6

1,15

3,8

35

3,8

3,8

12

Dimensions in mm. Figure 11

AIRBUS FRANCE 1988. All rights reserved

70

NSA9117 BF

Page :

24 K

NSA9117-28D

C

NSA9117-77D

3

B

1

4

A/C PN DESCR. SER. N° MFG DATE

2

MFR INDEX

5

6

NSA9117-28D

Issue :

7

8

E

Legend 9

-

A/C model and type

-

Serial number

-

NCAGE code (Airbus S.A.S.): FAPE3

-

Manufacture date

-

Part number

-

Inscription stamp / mark

-

Reference of mechanical assembly

-

Release (index / revision) of the drawing number

70

27 33

16 1

Dimensions in mm. Figure 12

AIRBUS FRANCE 1988. All rights reserved

25

0,925

0,925

0,925

0,925

3,5

1,15

8

14

3,8 r2

3,8

3,8

3,8

3,8

20

12

1,15

10

35

NSA9117

K

Issue :

BF

Page :

25

B

NSA9117-29S SER. N° WEIGHT

17

E

35 5

44

22

3,8TYP

20

1,1

C

NSA9117-29S

PN DATE

r5

1,1

0,925 TYP

Ø 1,6

3

5

2 20

20

16

70 Dimensions in mm. Figure 13

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

26

4.4 - Small VU 3,5

42

9

SERIAL N° NSA9117-08D

0,5

NSA9117-08D NSA9117-01D

15

0,5

E

B PN

J

3,5

E

PN

J

52

0,5

B

60

SERIAL N° NSA9117-01F

33

18,5

NSA9117-01F 6

12,5

5

16,8

16,2

3,5

4 NSA9117-07 CA CODE

P/N S/N

4

Manufactured for MSN

4

NSA9117-07

27,3

13

5,7

10,5

NSA9117-26

ATR CA CODE

P/N S/N

Manufactured for

60

MSN

33

18,5

NSA9117-26 6

12,5

5

16,8

16,2

3,5

4 NSA9117-09

P/N CA CODE

S/N

4

Manufactured for MFR

4 27,3

13

NSA9117-09 (see note)

5,7

10,5

Note: Only for change VU interchangeability. Figure 14 Example of part number construction (for procurement purposes):

NSA9117

-

07

F

1 Manufacturer code

Basic reference

Without : manufacturer A 1

Plate type Suffix

AIRBUS FRANCE 1988. All rights reserved

: manufacturer B

NSA9117 Issue :

BF

Page :

27

4.5 - Manufacturer's code LK NSA9117-02D

CMS

3,5

52

0,5

42

3,5

NSA9117-02D

9 0,5

SERIAL N° NSA9117-02F

NSA9117-02F

15

0,5

Figure 15 Table 4 MANUFACTURERS

ADDITIONAL INFORMATIONS

MANUFACTURERS

AIRBUS France

CMS

ALENIA

AIRBUS UK

FLABEL

-

AIRBUS Spain AIRBUS Germany

TAI

LK

FOKKER

-

MTAD DENEL

-

SONACA

ADDITIONAL INFORMATIONS

AEROSUD

4.6 - Concessions

CONCESSION NSA9117-05

A

30

NSA9117-05

CONCESSION NSA9117-75

A

Note 2: For other dimensions, see figure 13.

NSA9117-75

Figure 16 4.7 - Installation condition 18 ALLOCATED TO MSN NSA9117-04F

NSA9117-04F Note 3: For other dimensions, see figure 13. Dimensions in mm. Figure 17

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

28

4.7.1 - Record of production modifications and service bulletins (except for small elements) 1

See note 4

2

MFR BASIC PN PRODUCTION MODIFICATION OR SERVICE BULLETIN ACCOMPLISHMENT

3 NSA9117M8F See legend 8

1 2 3 4 5

6 7 8 9 10 SUF. MOD. DATE NSA9117M8F

4

5

6

7

See note 4 MFR BASIC PN

L

B

PRODUCTION MODIFICATION OR SERVICE BULLETIN ACCOMPLISHMENT

C

4 holes for rivets Ø 1,6

3 3

6 7 8 9 10 SUF. MOD. DATE

A

NSA9117M6F

42 37

9

2

4

15

4

r2

0,5

NSA9117M6F

1 2 3 4 5

0,5

B

4 4 4 4 2

47

47 100

Dimensions in mm. Figure 18

AIRBUS FRANCE 1988. All rights reserved

2

0,75

4

23PM

45

r7

NSA9117 Issue :

BF

Page :

29

PRODUCTION MODIFICATION OR SERVICE BULLETIN ACCOMPLISHMENT

1

MFR BASIC PN

K

NSA9117-M5F

MFR BASIC PN

PRODUCTION MODIFICATION OR SERVICE BULLETIN ACCOMPLISHMENT

1

2

2

3

3

3

4

5

6

7

NSA9117-M5F

NSA9117-M7F

4.8 - Record of production modifications and service bulletins for small elements See note 4 1 See note 4 F 2

E

NSA9117-M7F

Legend 9



- Line reference number for modification

- Embodiment date - Inscription stamp / mark

- Production / spares suffix 80 22

6

0,75

15

15

0,75

0,75

9 0,75

r6 3

1,5

10

4

1

1

4

4

25

3

1,5

20

5

0,5

2 holes for rivets Ø 1,6

6

2,2



- Assembly number (P/N) concerned

- Modification number

0,6



 

- NCAGE code (Airbus S.A.S.): FAPE3

2,2

 

Note 4 : According to responsible partner :

4 65

Dimensions in mm. Figure 19

Table 5 PARTNER AIRBUS France AIRBUS UK AIRBUS Spain AIRBUS Germany FOKKER SONACA ALENIA FLABEL TAI MTAD DENEL AEROSUD

AIRBUS FRANCE 1988. All rights reserved

COUNTRY France England Spain Germany Nederland Belgium Italy Belgium Turkey Spain South Africa South Africa

NSA9117 Issue :

BF

Page :

30

5 -

OLD PRODUCTIONS (NOT TO BE USED, NOT TO BE SUPPLIED) See table 2 for the equivalent new plates. 5.1 - Aircraft or manufacturer identification

NSA9117-30

AIRBUS INDUSTRIE MANUFACTURER'S NAME NSA9117-30

AIRBUS INDUSTRIE

NSA9117-40

a e ro sp a tia le -

ALENIA

NSA9117-41

Figure 20

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

31

AEROSPATIALE - ALENIA TOULOUSE - 31060 FRANCE - EUROP (F6198) A/C MODEL AND TYPE NSA9117-45

MFG SERIAL N° (MSN) TYPE CERTIFICATE N° AEROSPATIALE PRODUCTION

ORGANIZATION APPROVAL NUMBER FG004 DATE

NSA9117 - 45

AEROSPATIALE MATRA ATR - ALENIA TOULOUSE - 31060 FRANCE - EUROP (FAD84) A/C MODEL AND TYPE NSA9117-46

MFG SERIAL N° (MSN) TYPE CERTIFICATE N° PRODUCTION APPROVAL

F.G.054

JAR 21F NUMBER DATE

NSA9117 - 46

EADS ATR - ALENIA TOULOUSE - 31060 FRANCE - EUROP (FAD84) A/C MODEL AND TYPE NSA9117-47

MFG SERIAL N° (MSN) TYPE CERTIFICATE N° PRODUCTION APPROVAL

F.G.054

JAR 21F NUMBER DATE

NSA9117 - 47

Figure 21

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

32

AIRBUS BLAGNAC - 31700

NSA9117-43

FRANCE-EUROPE (FA849)

A/C MODEL AND TYPE MFG SERIAL N° (MSN) TYPE CERTIFICATE N° PRODUCTION ORGANIZATION APPROVAL NUMBER DATE

NSA9117-43

AIRBUS BLAGNAC - 31700 FRANCE-EUROPE (FA849) FINAL ASSEMBLY LINE OF HAMBURG (GERMANY) A/C MODEL AND TYPE NSA9117-44

MFG SERIAL N° (MSN) TYPE CERTIFICATE N° TYPE DESIGN RESPONSIBLE DGAC PRODUCTION ORGANIZATION LBA.G.0009 APPROVAL NUMBER DATE NSA9117-44

AIRBUS BLAGNAC - 31700 FRANCE-EUROPE (FA849) FINAL ASSEMBLY LINE OF HAMBURG (GERMANY)

NSA9117-68

A/C MODEL AND TYPE MFG SERIAL N° (MSN) TYPE CERTIFICATE N° TYPE DESIGN RESPONSIBLE DGAC PRODUCTION ORGANIZATION APPROVAL NUMBER DATE

NSA9117-68

Figure 22

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

33

5.2 - Owner identification

NSA9117-31

AIRCRAFT NSA9117-31

A 300

TYPE CERTIFICATE N°

NSA9117-32

AIRCRAFT NSA9117-32

A 310

TYPE CERTIFICATE N°

NSA9117-52

MSN NSCM

AIRBUS

NSA9117-52

REGISTRATION OWNER ADDRESS OWNER ADDRESS OWNER ADDRESS

AIRWORTHINESS CERTIFICATE Figure 23

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

34

NSA9117-50

AIRBUS

MSN NSA9117- 50

REGISTRATION OWNER NSCM ADDRESS AIRWORTHINESS CERTIFICATE

NSA9117-51

ATR

MSN NSA9117- 51

REGISTRATION OWNER NSCM ADDRESS AIRWORTHINESS CERTIFICATE

NSA9117-53

MSN NSCM

AIRBUS

NSA9117-53

REGISTRATION OWNER ADDRESS OWNER ADDRESS OWNER ADDRESS

AIRWORTHINESS CERTIFICATE Figure 24

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

35

ASSY N° SERIAL N°

SOCIETENATIONALEINDUSTRIELLE

DATEOFMAN.

a e ro sp a tia le ASSY N° SERIAL N°

DATEOFMAN.

NSA9117-10

NSA9117-12

Replaced by :

Replaced by :

ASSY N° SERIAL N°

SOCIETE NATIONALE INDUSTRIELLE

DATE OF MAN.

a e ro sp a tia le

NSA 9117 -1 2

a e ro sp a tia le

TYPE OF MATERIAL

SOCIETENATIONALEINDUSTRIELLE

ASSY N° SERIAL N° DATE OF MAN.

NSA9117-10

NSA9117-12 AEROSPATIALE PN

DEUTSCHEAIRBUSGMBH

NSA 9117 -1 1D

TYPE OF MATERIAL

NSA 9117 -1 2

NSA 9117 -1 0

a e ro sp a tia le

TYPEOFMATERIAL

SOCIETENATIONALEINDUSTRIELLE

NSA 9117 -1 0

TYPE OF MATERIAL

TYPEOFMATERIAL

5.3 - Constituent assemblies identification

ASSY N° SERIALN°

NSA9117-06

CA CODE

NSA9117-06

ATR

DATE OF MAN.

NSA9117-06F

NSA9117-11

PN SER IAL N°

CA CODE

NSA9117-06F Figure 25

5.4 - VU identification ASSYN°

aerospatiale

SERIAL N°

NSA9117-01

DEUTSCHE AIRBUS GMBH

NSA 9117 -1 3D

TYPE OF MATERIAL

SER IAL N°

ASSY N° SERIAL N° ELEC MARK

DATE

NSA9117-13D Figure 26 Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

36

5.5 - Record of production modifications and service bulletins S O C I E T E N A T I O N A L E IN D U S T R I E L L E

a e ro sp a tia le

NSA9117-M4

M O D IF IC A T IO N S

1 2 3 4 5 6

7 8 9 10 11 12 NSA9117-M4

S O C IE T E N A T I O N A L E IN D U S T R I E L L E

a e ro sp a tia le M O D I F I C A T IO N S

7 8 9 10 11 12

NSA9117-M2

1 2 3 4 5 6

NSA9117-M2

M O D IF IC A T IO N S

1 2 3

SOCIETE NATIONALE INDUSTRIELLE

a e ro sp a tia le

M O D IF IC A T IO N S

1 2 3

NSA9117-M1

NSA9117-M3 Figure 27

5.6 - Concessions C O N C E S S IO N

A IR C R A F T

N S A 9 1 1 7 0 3

N S A 9 1 1 7 0 3 Figure 28

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA 911 7-M 3

a e rosp a tia le

NSA 911 7-M 1

SOCIETE NATIONALE INDUSTRIELLE

NSA9117 Issue :

BF

Page :

37

NSA9117-78

150 10

R10 20

NSA9117-78

12

30

12

30

12

42

2 Holes Dia 5mm Figure 29

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

12

15

85

7

1

5 5

5

1

5

1

20

2

10

75

NSA9117 Issue :

BF

Page :

38

REPAIR STATION PN SERIAL o N NSA9117-80

52,0

3,5

42,0

13,5

REPAIR STATION PN SERIAL o N 3,5

NSA9117-80

Dimensions in mm

Figure 30: NSA9117-80

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117

6 -

Issue :

BF

Page :

39

MANUFACTURERS Refer to the list of qualified manufacturers and products.

AMENDMENT RECORD SHEET Issue

Modified paragraph

N.08.88

2

Modification summary On drawings : letters F, S, E, D, N, B, I, deleted.

3

Justification Telefax BAe of 11.12.87

D for item No. 11 deleted. "or equivalent" added for plates in A5. Thickness modified : 0,07 changed to 0,07 to 0,013 for plates 22 and 12.

P.09.88

3

R.06.91

S.02.92

"or printed" added.

TE423/037/87-HAM

3.2

-23 for matt black ground color added.

TK422M046/91-HAM

3.3

-23 for metal window added.

1, 3.1, 3.2, 3.3, Plates -21, -24, -25, -26, -27 and -52 added. 3.7, 4.4 4.2

F.A.I. report No. 627.015/91

On plate FSCM changed to NSCM.

ATA/Spec 2000

AERITALIA changed to ALENIA. T.05.92

4.1, 5.1 4.7

Plate -41 replaced by -42. Plate -04 added.

A/DQ/QM request Base LC/CA No. 696.565/92

U.07.92

Plate -52 replaced by -53.

A 300 - A 310 Dispute No. 262229

V.06.93

§ 3.4 modified. 4.3, 5.3

Constituent Assembly code added.

A/DO/G request

Plates -01, -20, -21, -22, -24, -25, -26 and -27 replaced by plates -06, -60, -61, -62, -64, -65, -66 and -67. W.01.94

4.1, 5.1

Plate -40 replaced by plate -43.

Airbus Industrie request Ref. 6720676/93

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

40

AMENDMENT RECORD SHEET Issue

Modified paragraph

Y.02.94

4.1

Modification summary Print area added on plate -43.

Justification Airbus Industrie request Ref. 6720676/93

Plates –01, -20, -21, -22, -24, -25, -26 and

Z.07.95

TF3 - WG1 decision

-27 valid again. Writing modified : aerospatiale changed to AEROSPATIALE. DEUTSCH AIRBUS changed to DAIMLER BENZ AEROSPACE AIRBUS. AA.07.96

2.3

Note added.

4.3

For identification plates -60, -61, -62, -20,

Item 830 - TF3 WG1

-21, -22, -23, -64, -65, -24, -66, -67, -26, -27 : "Type / model aircraft" changed to "A/C type and make (AIRBUS, ATR ...)". AB.06.97

Plate -44 added.

DA request Point 830 - TF3 WG1

AC.01.98

Plate -45 added.

P.M. T 5012 Mod. 4950

AD.10.00

Plate -45 replaced by plate -46.

ATR Mod. 5115

Plates -08D and -07 added.

Mod. 27156

Plate -06 deleted.

DA request

Logo modified : "AEROSPATIALE" changed to "EADS AIRBUS".

AE.01.01

Plate -46 replaced by plate -47.

Mod. 5270

Table 2 : suffix D for plates -08 and -01

Item 09-24

deleted.

TF3 WG1

Plate -01 added in old production. AF.05.01

Plate -48 added.

Mod. ATR No. 5333

AG.11.01

Plate -09 added.

Mod. 12492

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

NSA9117 Issue :

BF

Page :

41

AMENDMENT RECORD SHEET Issue

Modified paragraph

AH.03.02

Modification summary For plate -48 : address modified and

Justification Mod. 05333

JAR 21F NUMBER changed to JAR 21G NUMBER.

AJ.12.02

Plate -07 modified.

Mod. 27156

Plate -06 updated. Plate -63 added.

AI-D request

AK.02.03

Plate -26 added.

ATR

AL.05.04

Figure 4 modified.

ATR

Plate -49 added. Modification in table 2. AM.09.04

Plate -68 added.

Draft

In page 6 note deleted.

AN.04.05 AP.12.05 AQ.01.07

Mod. 34800

Partner suffix C, T, P, A and V added. 3.2, 3.3

Plate –66 and –67 added

A400M request A-UK request

Plate -70 added. Plates 43, 44 and 68 changed from § 4.1 to § 5.1.

AR.03.07

Plates -03, -50, -51 and -53 (old version) replaced by -05, -55, -56 and -57 (new version).

AS.06.07

Plates -58, -59 added.

AT.02.08

Plate -42 modified: MATRA deleted. Plates -28 and -71 added.

AU.08.08

Plates -29S and -75 added.

AV.11.08

Table 2 modified for plate -29 : Bonding changed to Rivet and 0,07 to 0,13 mm changed to 0,5 mm.

AW.04.10

Plate -69 added.

AX.11.10

Plate -69 splitted in -76 and -77

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved

Eurocopter request

NSA9117 Issue :

BF

Page :

42

AMENDMENT RECORD SHEET Issue AY.07.12

Modified paragraph

Modification summary

Justification

Modification of “AIRBUS” logo and typography. Plate -72 added.

AZ.02.13

-78 Allocation of Concession Outstanding Added. -79 Added. Plate -54 and -74 added.

BA.03.13

Added plate -54 to section 3.3 and 3.5 Added modified information in Table 2 for 78

BB.05.13

Added Colour and window information for 78 Corrected Figure 29 for final design of label 78

BC.09.13

Corrected Table 2 for -02, -05, -75 for column Type of Characters to read, Photoengraved or Printed.

BD.02.15

Amended NSA9117-74 to include “AIRBUS DEFENCE AND SPACE S.A.U.”

BE.07.15

Label -73 added

Required for A330 NEO pylon application

BF.09.15

Label -80 added

For requirement see CPPR request 4499

Note : Modification to the last standard issue are indicated by a vertical line in the margin.

AIRBUS FRANCE 1988. All rights reserved