drawing approval sheet doa easa 21.j · doa easa 21.j.628 drawing approval sheet drawing number:...

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DOA EASA 21.J.628 DRAWING APPROVAL SHEET DRAWING NUMBER: MMRO-C-0121-MD-0703 DRAWING TITLE:PAX SEATS INSTL A320 ISSUE DATE COMPILED BY CHECKED BY STRESSED BY CVE/APPROVED 1 25/03/2019 Dmitrij Nazarenko Gytis Leonavicius Crawford Murray Crawford Murray - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - The drawing referenced in this document has been reviewed in accordance with Magnetic MRO DO design process and found to be compliant with the applicable requirements. MMRO/DF/016 ISSUE 1

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Page 1: DRAWING APPROVAL SHEET DOA EASA 21.J · doa easa 21.j.628 drawing approval sheet drawing number: mmro-c-0121-md-0703 drawing title:pax seats instl a320 issue date compiled by checked

DOA EASA 21.J.628 DRAWING APPROVAL SHEET

DRAWING NUMBER: MMRO-C-0121-MD-0703

DRAWING TITLE:PAX SEATS INSTL A320

ISSUE DATE COMPILED BY CHECKED BY STRESSED BY CVE/APPROVED

1 25/03/2019 Dmitrij Nazarenko Gytis Leonavicius Crawford Murray Crawford Murray

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The drawing referenced in this document has been reviewed in accordance with Magnetic MRO DO design process and found to be compliant with the applicable requirements.

MMRO/DF/016 ISSUE 1

Page 2: DRAWING APPROVAL SHEET DOA EASA 21.J · doa easa 21.j.628 drawing approval sheet drawing number: mmro-c-0121-md-0703 drawing title:pax seats instl a320 issue date compiled by checked

1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

A A

B B

C C

D D

E E

F F

REMOVE ALL BURRS

& SHARP EDGES

PROJECTION

EASA APPROVAL EASA.21J.628

© MAGNETIC MRO

ALL RIGHTS RESERVED.

MAGNETIC MRO OWN THE

COPYRIGHT OF THIS DRAWING

WHICH IS SUPPLIED IN CONFIDENCE

ON THE EXPRESS CONDITION THAT

IT IS NOT USED, REPRODUCED OR

COMMUNICATED TO ANY OTHER

PERSON WITHOUT PERMISSION IN

WRITING FROM THE OWNER.

ALL DIMENSIONS IN IN

UNLESS OTHERWISE STATED

of

DO NOT SCALE

DRG No:

Title:

Date: Date: Date:

ISO 2678 MK

TOLERANCES-

UNLESS STATED:

Upper Assembly:Size:

WARNING - COMPUTER

PRODUCED DRAWING,

NO MANUAL ALTERATION

Scale:

Vaike-Sojamae 1A, 11415Tallinn, Estonia

Tel: +372 6401 119Fax: +372 6401 116

Drawn: Checked by: Stressed by:

Sheet:

Date:

CVE/Approved by:

PAX SEATS INSTL A320

MMRO-C-0121-MD-0703 01 05

A3 1:1 Material: N/A TOP ASSEMBLY

D. NAZARENKO G. LEONAVICIUS C. MURRAY C. MURRAY

20 MAR 2019 20 MAR 2019 20 MAR 2019 20 MAR 2019

1 16 882157-418 SEAT ASSY - R/H STD TPL, NRW AFT, NO TBL, NO RCL - ZODIAC AEROSPACE1 15 882157-417 SEAT ASSY - L/H STD TPL, NRW AFT, NO TBL, NO RCL - ZODIAC AEROSPACE1 14 882157-412 SEAT ASSY - R/H STD TPL, NRW, 4" RCL - ZODIAC AEROSPACE1 13 882157-411 SEAT ASSY - L/H STD TPL, NRW, 4" RCL - ZODIAC AEROSPACE1 12 882157-430 SEAT ASSY - R/H STD TPL, AFT EXIT, NO OTB ARM, 4” RCL - ZODIAC AEROSPACE1 11 882157-429 SEAT ASSY - L/H STD TPL, AFT EXIT, NO OTB ARM, 4” RCL - ZODIAC AEROSPACE1 10 882157-428 SEAT ASSY - R/H STD TPL, EXIT, NO OTB ARM, NO RCL - ZODIAC AEROSPACE1 9 882157-427 SEAT ASSY - L/H STD TPL, EXIT, NO OTB ARM, NO RCL - ZODIAC AEROSPACE1 8 882157-426 SEAT ASSY - R/H STD TPL, FWD EXIT, OTB LTD RCL - ZODIAC AEROSPACE / RCL TO BE LOCKED1 7 882157-425 SEAT ASSY - L/H STD TPL, FWD EXIT, OTB LTD RCL - ZODIAC AEROSPACE / RCL TO BE LOCKED

24 6 882157-424 SEAT ASSY - R/H STD TPL, 4" RCL - ZODIAC AEROSPACE24 5 882157-423 SEAT ASSY - L/H STD TPL, 4" RCL - ZODIAC AEROSPACE1 4 882157-422 SEAT ASSY - R/H F/R TPL, IAT, 4” RCL - ZODIAC AEROSPACE1 3 882157-421 SEAT ASSY - L/H F/R TPL, IAT, 4” RCL - ZODIAC AEROSPACE- 2 - - - -- 1 MMRO-C-0121-MD-0703-01 INSTALLATION - PASSENGER SEATS A320 - -

QTY ITEM NO PART NUMBER DESCRIPTION MATERIAL MANUFACTURER / REMARKS

GENERAL NOTES:

1. DIMENSIONS OF SEAT STATIONS ARE TAKEN FROM CENTERLINE FRONT OF FOOT STUD.

2. ENSURE HEAD-STRIKE OF PASSENGERS IN FRONT ROW IS PREVENTED: THE POINT AT WHICH THE SEAT BACK MEETS THE SEAT CUSHIONEXCEEDS A MINIMUM OF 35 INCHES FROM THE MONUMENT IN FRONT. THIS DISTANCE ALSO TAKES INTO ACCOUNT HIGH MOUNTED LITERATUREPOCKETS AND OTHER FITMENTS ON THE MONUMENT

3. ENSURE THE CENTER AISLE EXCEEDS THE MINIMUM REQUIREMENTS OF 15 INCHES WIDE UP TO A HEIGHT OF 25 INCHES FROM THE FLOOR AND 20INCHES WIDE ABOVE 25 INCHES FROM THE FLOOR. THIS INCLUDES ANY RUB STRIPS.

4. ENSURE ALL EMERGENCY EXITS ARE ACCESSIBLE I.A.W. JAR/CS 25.813 AS FOLLOWS:

4.1. THE PATHWAY TO ALL TYPE C EXITS IS MINIMUM 20" WIDE UNOBSTRUCTED ACCESS LEADING TO EXIT(S) WITH ASSIST SPACE OF 12" X 20" ONONE SIDE OF THE PATHWAY.

4.2. THE PATHWAY TO ALL TYPE III EXITS IS MINIMUM OF 10" WIDE UNOBSTRUCTED ACCESS LEADING TO EXIT(S).

5. ENSURE A SERVICEABLE (E)TSO-C13D CERTIFIED PASSENGER LIFE VEST IS INSTALLED IN EACH PASSENGER LIFE VEST STOWAGE.

6. ALL PASSENGER SEAT LAP BELTS MUST BE (E)TSO-C22G CERTIFIED.

7. SEATS HAVE FOLLOWING:

7.1. SEAT ROW 11 -7.1.1. NO RECLINE CAPABILITY;7.1.2. ONE WAY TABLE LATCH;

7.2. SEAT ROW 12 -7.2.1. NO OUTBD ARMREST;7.2.2. NO RECLINE CAPABILITY;7.2.3. ONE WAY TABLE LATCH;

7.3. SET ROW 13 -7.3.1. NO OUTBD ARMREST.

8. ON ROW 11 SEATS P/N 882157-405 AND 882157-406 RECLINE TO BE LOCKED. INSTALL RECLINE LOCK I.A.W. ZODIAC AEROSPACE MODEL Z100 CMM25-20-46.

9. ALL SEATS HAVE NO BREAKOVER CAPABILITY.

10. PASSENGER SERVICE CHANNEL IS NOT AFFECTED BY THIS CHANGE. EXISTING PASSENGER SERVICE CHANNEL LAYOUT IS PROVIDED FORREFERENCE ONLY.

SEATS GLOSSARYR/H RIGHT HANDL/H LEFT HANDTPL TRIPLEIAT IN ARMREST TABLESTD STANDARDNRW NARROWTBL BACKREST TABLEOTB OUTBOARDLTD LIMITEDRCL RECLINE

REVISION HISTORY ISSUE DATE

Initial issue 1 20 MAR 2019

Page 3: DRAWING APPROVAL SHEET DOA EASA 21.J · doa easa 21.j.628 drawing approval sheet drawing number: mmro-c-0121-md-0703 drawing title:pax seats instl a320 issue date compiled by checked

FA

G1

LA

FA

FA

G5

C14 C16 C18 C20 C21 C23 C24 C25 C26 C27 C28 C29 C30 C31 C32 C33 C34 C35 C36 C37

C38

C39

C40

C41 C42 C43 C44 C45 C46 C47 C48 C49 C50 C51 C70C52 C53 C54 C55 C56 C57 C58 C59 C60 C61 C62 C63 C64 C65 C66 C67 C68 C69C12

TYPE

C E

XIT

L/H &

R/H

LD

LE

FA

CBA

FED

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30FA

STA

321.1

"[81

55.9

MM]

STA

344"

[8737

.6 MM

]

TYPE

III E

XIT

L/H &

R/H

TYPE

III E

XIT

L/H &

R/H

TYPE

C E

XIT

L/H &

R/H

STA

630"

[1600

2 MM]

STA

667"

[1694

1.8 M

M]

STA

703"

[1785

6.2 M

M]

STA

848"

[2153

9.2 M

M]

STA

1184

"[30

073.6

MM]

STA

1207

"[30

657.8

MM]

4 6 6 6 6 6 6 6 6 6 8 10 12 6 6 6 6 6 6 6 6 6 6 6 6 6 6 6 14 16

3 5 5 5 5 5 5 5 5 5 7 9 11 5 5 5 5 5 5 5 5 5 5 5 5 5 5 5 13 15

NRNR

NRNR

NRNR

NRNR

NR

NRNR

NR

NRNR

NR

NRNR

NR

FA

STA

518"

[1315

7.2 M

M]

REMOVE ALL BURRS

& SHARP EDGES

PROJECTION

EASA APPROVAL EASA.21J.628

© MAGNETIC MRO

ALL RIGHTS RESERVED.

MAGNETIC MRO OWN THE

COPYRIGHT OF THIS DRAWING

WHICH IS SUPPLIED IN CONFIDENCE

ON THE EXPRESS CONDITION THAT

IT IS NOT USED, REPRODUCED OR

COMMUNICATED TO ANY OTHER

PERSON WITHOUT PERMISSION IN

WRITING FROM THE OWNER.

ALL DIMENSIONS IN IN

UNLESS OTHERWISE STATED

of

DO NOT SCALE

DRG No:

Title:

Date: Date: Date:

ISO 2678 MK

TOLERANCES-

UNLESS STATED:

Upper Assembly:Size:

WARNING - COMPUTER

PRODUCED DRAWING,

NO MANUAL ALTERATION

Scale:

Vaike-Sojamae 1A, 11415Tallinn, Estonia

Tel: +372 6401 119Fax: +372 6401 116

Drawn: Checked by: Stressed by:

Sheet:

Date:

CVE/Approved by:

PAX SEATS INSTL A320

MMRO-C-0121-MD-0703 02 05

840x297 MM 1:1 Material: N/A TOP ASSEMBLY

D. NAZARENKO G. LEONAVICIUS C. MURRAY C. MURRAY

20 MAR 2019 20 MAR 2019 20 MAR 2019 20 MAR 2019

LEGEND:

IN-ARMREST TABLE

ATTENDANT SEAT

EMERGENCY EGRESS PATH

ASSIST SPACE 12" x 20"

NO RECLINE

FA

1

1

2

2

3

3

4

4

5

5

6

6

7

7

A A

B B

C C

D D

E E

F F

8 9 10 11 12 13 14 15 16

8 9 10 11 12 13 14 15 16

NR

REVISION HISTORY ISSUE DATE

Initial issue 1 20 MAR 2019

-01 - A320 PASSENGER SEATS INSTALLATION

180 Y/C CONFIGURATION

29" x 6 = 174"L/H & R/H

28 x 4 = 112"L/H & R/H

37"L/H & R/H

36"L/H & R/H

29" x 5 = 145"L/H & R/H

28" x 12 = 336"L/H & R/H

5 64.1 9

Page 4: DRAWING APPROVAL SHEET DOA EASA 21.J · doa easa 21.j.628 drawing approval sheet drawing number: mmro-c-0121-md-0703 drawing title:pax seats instl a320 issue date compiled by checked

CL

PASSENGER/SERVICE FWD EXIT

LAV

FWD PARTITION

CLTYPE III

OVERWINGEMERGENCY EXIT

CLTYPE III

OVERWINGEMERGENCY EXIT

21 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30

4L3RH3L3

RH

4"4L3

RH LCDWA

3RH 3LLCD 3

RH 4L1"

3RH 3L

4"3

RH 4L 3RH 3L LCD 3

RH 4L2"

3RH 3L

2"3

RH 4L LCD 3RH 3L

6"4L3

RH

4"3

RH 3L 4L3RH LCD 3

RH 3L 4L3RH

4"3

RH 3L 4L3RH LCD 3

RH 3L 4L3RH

2"3

RH 3L 4L3RH LCD 3

RH 3L 4L3RH

1"3

RH 3L 4L3RH LCD 3

RH 3L 4L3RH

3RH 3L

2"

REMOVE ALL BURRS

& SHARP EDGES

PROJECTION

EASA APPROVAL EASA.21J.628

© MAGNETIC MRO

ALL RIGHTS RESERVED.

MAGNETIC MRO OWN THE

COPYRIGHT OF THIS DRAWING

WHICH IS SUPPLIED IN CONFIDENCE

ON THE EXPRESS CONDITION THAT

IT IS NOT USED, REPRODUCED OR

COMMUNICATED TO ANY OTHER

PERSON WITHOUT PERMISSION IN

WRITING FROM THE OWNER.

ALL DIMENSIONS IN IN

UNLESS OTHERWISE STATED

of

DO NOT SCALE

DRG No:

Title:

Date: Date: Date:

ISO 2678 MK

TOLERANCES-

UNLESS STATED:

Upper Assembly:Size:

WARNING - COMPUTER

PRODUCED DRAWING,

NO MANUAL ALTERATION

Scale:

Vaike-Sojamae 1A, 11415Tallinn, Estonia

Tel: +372 6401 119Fax: +372 6401 116

Drawn: Checked by: Stressed by:

Sheet:

Date:

CVE/Approved by:

PAX SEATS INSTL A320

MMRO-C-0121-MD-0703 03 05

840x297 MM 1:1 Material: N/A TOP ASSEMBLY

D. NAZARENKO G. LEONAVICIUS C. MURRAY C. MURRAY

20 MAR 2019 20 MAR 2019 20 MAR 2019 20 MAR 2019

1

1

2

2

3

3

4

4

5

5

6

6

7

7

A A

B B

C C

D D

E E

F F

8 9 10 11 12 13 14 15 16

8 9 10 11 12 13 14 15 16

REVISION HISTORY ISSUE DATE

Initial issue 1 20 MAR 2019

EXISTING PASSENGER SERVICE CHANNEL LAYOUT

180 Y/C CONFIGURATION

R/H SHOWN, L/H SIMILAR

(SHOWN FOR REFERENCE ONLY)

LEGEND TABLEITEM DESCRIPTION SIDE VIEW

1 INFILL PANEL 1"

2 INFILL PANEL 2"

3 INFILL PANEL 4"

4 INFILL PANEL 6"

5 OXYGEN MASK CONTAINER(3 MASKS)

6OXYGEN MASK CONTAINER(4 MASKS)

7PSIU COMBI PANEL(3 READING LIGHTS)

8PSIU COMBI PANEL(NSFSB SIGN; 3 READINGLIGHTS; SPEAKER)

9 GASPER PANEL(3 NOZZLES)

10 MONITOR

11 PARTITION PANEL

2"

4"

3L

4L

WA

LCD

3

3

6"

1"

OXYGEN MASK DROP LOCATION

TYP. DETAIL

IN LINE WITH SEATREFERENCE POINT (SRP)

OXYGEN MASK

OXYGEN MASKCONTAINEROXYGEN MASK MUST

NOT FALL FWD OFRECLINE SEAT BACK

OXYGEN MASK DROP AREA

10

Page 5: DRAWING APPROVAL SHEET DOA EASA 21.J · doa easa 21.j.628 drawing approval sheet drawing number: mmro-c-0121-md-0703 drawing title:pax seats instl a320 issue date compiled by checked

CL

PASSENGER/SERVICE FWD EXIT

1

FWD PARTITION

LAV

30

CL

TYPE IIIOVERWING

EMERGENCY EXITCL

TYPE IIIOVERWING

EMERGENCY EXIT

11 12 13

1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

A A

B B

C C

D D

E E

F F

REMOVE ALL BURRS

& SHARP EDGES

PROJECTION

EASA APPROVAL EASA.21J.628

© MAGNETIC MRO

ALL RIGHTS RESERVED.

MAGNETIC MRO OWN THE

COPYRIGHT OF THIS DRAWING

WHICH IS SUPPLIED IN CONFIDENCE

ON THE EXPRESS CONDITION THAT

IT IS NOT USED, REPRODUCED OR

COMMUNICATED TO ANY OTHER

PERSON WITHOUT PERMISSION IN

WRITING FROM THE OWNER.

ALL DIMENSIONS IN IN

UNLESS OTHERWISE STATED

of

DO NOT SCALE

DRG No:

Title:

Date: Date: Date:

ISO 2678 MK

TOLERANCES-

UNLESS STATED:

Upper Assembly:Size:

WARNING - COMPUTER

PRODUCED DRAWING,

NO MANUAL ALTERATION

Scale:

Vaike-Sojamae 1A, 11415Tallinn, Estonia

Tel: +372 6401 119Fax: +372 6401 116

Drawn: Checked by: Stressed by:

Sheet:

Date:

CVE/Approved by:

PAX SEATS INSTL A320

MMRO-C-0121-MD-0703 04 05

A3 1:1 Material: N/A TOP ASSEMBLY

D. NAZARENKO G. LEONAVICIUS C. MURRAY C. MURRAY

20 MAR 2019 20 MAR 2019 20 MAR 2019 20 MAR 2019

FRONT ROW SEATS

CLEARANCE ENVELOPER/H SIDE SHOWN

L/H SIDE OPPOSITE

OVERWING EXIT SEATS

EXIT PATH CLEARANCE ENVELOPER/H SIDE SHOWN

L/H SIDE OPPOSITE

LAST ROW SEATS

CLEARANCE ENVELOPER/H SIDE SHOWN

L/H SIDE OPPOSITE

FRONT STUD ATTACHMENT

TYP. DETAIL

STA

321.1

"[81

55.9]

CRP

14.5"

2.4"

35"

HEADSTRIKEARC

STA

344"

[8737

.6]

STA

1184

"[30

073.6

]

STA

1207

"[30

657.8

]

20.9"

2.1"

FWD

SEAT TRACK(REF)

SEAT(REF)

TYP. FOOT STUD

STA

344"

[8737

.6]

STA

630"

[1600

2]

STA

667"

[1694

1.8]

STA

703"

[1785

6.2]

22.4" 22.2"

11.9" 11.1"

2.7" 2.7"

14.7"

2

1

7.2 7.37.14.2 9

REVISION HISTORY ISSUE DATE

Initial issue 1 20 MAR 2019

Page 6: DRAWING APPROVAL SHEET DOA EASA 21.J · doa easa 21.j.628 drawing approval sheet drawing number: mmro-c-0121-md-0703 drawing title:pax seats instl a320 issue date compiled by checked

CLAISLE

TYPE III EXIT20" x 36"

TYPE III EXIT20" x 36"11 12 13

1

1

2

2

3

3

4

4

5

5

6

6

7

7

8

8

A A

B B

C C

D D

E E

F F

REMOVE ALL BURRS

& SHARP EDGES

PROJECTION

EASA APPROVAL EASA.21J.628

© MAGNETIC MRO

ALL RIGHTS RESERVED.

MAGNETIC MRO OWN THE

COPYRIGHT OF THIS DRAWING

WHICH IS SUPPLIED IN CONFIDENCE

ON THE EXPRESS CONDITION THAT

IT IS NOT USED, REPRODUCED OR

COMMUNICATED TO ANY OTHER

PERSON WITHOUT PERMISSION IN

WRITING FROM THE OWNER.

ALL DIMENSIONS IN IN

UNLESS OTHERWISE STATED

of

DO NOT SCALE

DRG No:

Title:

Date: Date: Date:

ISO 2678 MK

TOLERANCES-

UNLESS STATED:

Upper Assembly:Size:

WARNING - COMPUTER

PRODUCED DRAWING,

NO MANUAL ALTERATION

Scale:

Vaike-Sojamae 1A, 11415Tallinn, Estonia

Tel: +372 6401 119Fax: +372 6401 116

Drawn: Checked by: Stressed by:

Sheet:

Date:

CVE/Approved by:

PAX SEATS INSTL A320

MMRO-C-0121-MD-0703 05 05

A3 1:1 Material: N/A TOP ASSEMBLY

D. NAZARENKO G. LEONAVICIUS C. MURRAY C. MURRAY

20 MAR 2019 20 MAR 2019 20 MAR 2019 20 MAR 2019

TABLE 1. AISLE WIDTH

ROWDIM 'A'

(MIN. 15")DIM 'B'

(MIN. 20")DIM 'C'

(MAX. 25")1 16.84 20.64 24.70

2-28 17.04 20.84 24.5029 16.64 20.44 24.5030 17.64 21.44 24.50

OVERWING EXIT CLEARANCE ENVELOPE

TYP. TYPE III EXIT

AISLE WIDTH CLEARANCE ENVELOPE

TYPICAL, SEE TABLE 1 FOR DIMENSIONS

LBL 5

0.87"

LBL 3

0.12"

RBL 3

0.12"

RBL 5

0.87"

DIM

'C'

DIM 'A'

DIM 'B'

22.4"UPRIGHT / NO RECLINE

3.6"17

"TY

P. U

NCOM

PRES

SED

CUSH

ION

HEIG

HT

22.2"UPRIGHT / NO RECLINE

0.19"

14.7"

TYP.

SEA

T ST

RUCT

URE

HEIG

HT

SEAT STRUCTURE MAY OVERLAPEXIT PANEL UP TO THIS LINE

MAX.

14.8"

MAX.

18.8"

COMPRESSIBLE SEATCUSHION MAY ENCROACHUP TO THIS LINE IFPASSAGEWAY IS ≥ 10"

22.3"

24.3"

EXIT FRAMEPANEL

OUTBD SEATSMAY NOT ENCROACHBEYOND THIS LINE

7.1

7.2 7.37.1

3

8

REVISION HISTORY ISSUE DATE

Initial issue 1 20 MAR 2019