tec/05-003.6 dent and buckle chart index revision 2 part … · 2020. 8. 20. · dent and buckle...

Part I - GENERAL

AC type MSN Registration Date

Chart

Ref.Date Raised

Logged on

DocumentDamage location

Description of

Damage

Area and depth of

DamageAllowable iaw Classification Limitation Status Date Closed

Logged on

DocumentRemarks

1 10-Nov-08TIMCO NRC 35250

/ DF050

APU Outlet Skin

Empennage DentDent Appr 2.5" SRM 51-31-01 PAGE 220223

Minor

CAT AClosed 12-Dec-08 TIMCO NRC 35250

Further inspection found no

dent in area.

2 16-Jul-03Mexicana NRC

0614M020 / FD01

BS 1600 - BS 1620; S27R -

S28RDent

L = 3' W = 2" D = 0.062"

A/Y = 32SRM 53-00-01 fig 101

Minor

CAT AClosed 21-Jul-03

Mexicana NRC

0614M020 / FD01See also D098


0614M021 / FD02

BS 1640 - BS 1660; S21R -

S22RDent

L = 2.133' W = 2.229" D =

0.035"

A/Y = 60

SRM 53-00-01 fig 101Minor


Mexicana NRC

0614M021 / FD02Xfer R105


0614M022 / FD03

BS 1660 - BS 1680; S21R -

S22RDent

L = 3.017"' W = 2.8" D =

0.06"SRM 53-00-01 fig 101 Closed 21-Jul-03

Mexicana NRC

0614M022 / FD03

Has been repaired. See

repair 105


0614M024 / FD05BS 1400, S29L - S30L Dent

D = 0.020", L = 1.199", N =

1.293"

A/Y = 59

SRM 53-00-01 pg 103Minor


Mexicana NRC

0614M024 / FD05

Has been repaired.

See repair 106


0614M023 / FD06BS 1675 AND S27L - S28L. Dent

L = 0.6 W = 0.744" D =

0.014"

A/Y = 42



Mexicana NRC

0614M023 / FD06

See also D054

See R193


0614M106 / FD07BS 1963.8 - BS 1992 Dent

Dent, L = 3.225", W =

1.532", D = 0.049"

A/Y = 31



Mexicana NRC

0614M106 / FD07

8 11-Jan-00

Challenge Air Cargo

Work Item Seq 0481 /

FD08

BS 580 - BS 600; S27L - S28L Dent SRM 53-00-01 fig 101Minor

CAT AClosed 27-Jan-00

Challenge Air Cargo

Work Item Seq 0481 /

FD08

9 01-Aug-03Mexicana Work Card

O614M132 / FD09BS 600; S18L - S19L Dent

H L = 1.8", W = 1.5", D =

0.05"FAA 8110-3

Minor

CAT AClosed 05-Aug-03

Mexicana Work Card

O614M132 / FD09

Has been repaired. See

repair 107


O614M132 / FD10BS 520 & BS 600; S18L - S19L 2 Dents

L = 5.4' W = 2.5" D = 0.08"

A/Y = 31FAA 8110-3

Minor


Mexicana Work Card

O614M132 / FD10


FD-11

BS 1540 - BS 1560; S28R -

S29R2 Dents

A/ L = 4' W = 2.5" D = 0.53"

A/Y = 47

B/ L=2' W=1.5" D=0.017"

A/Y = 88



Mexicana Work Card

FD-11

12 19-Jan-00CAC 2000-6133

Seq 0587 / FR09BS 310.5; S18L - S19L Scratch rework SRM 53-00-01 fig 101

Minor


CAC 2000-6133

Seq 0587 / FR09


FD-13

BS 1520 - BS 1540; S20R -

S21RDent

L = 0.4'', dia. D = 0.006"

A/Y = 66SRM 53-00-01 FIG101

Minor


Mexicana Work Card

FD-13

14 12-Nov-08Timco NRC 35465

/ FD14

APU Access door RH

Dent 33" aft of Leading Edge,

6" down from hinge on External

Skin

DentA = 1.5" Y = 0.053"

A/Y = 28

SRM 52-40-01

SRM 51-70-01

Minor

CAT AClosed 02-Dec-08

Timco NRC 35465

/ FD14Rework to within limits

15 11-Jan-00

Challenge Air Cargo

Work Item Seq 0482

/ FR01

BS 1300 - BS 1360; S25L -

S25RScratches and dents SRM 53-00-01 fig 101

Minor


Challenge Air Cargo

Work Item Seq 0482

/ FR01

Has been reworked. See

repair 108

16 05-Jan-00

Challenge Air Cargo

Work Item Seq 0068

/ FR02

BS 1360 - BS 1400; S28L -

S28RDent

L = 20", W = 0.6", Dmax =

0.030"

A/Y = 20

SRM 53-60-01

SRM 51-40-02

Minor


Challenge Air Cargo

Work Item Seq 0068

/ FR02

Rework to within limits

Xfer to R195


FD-12BS 350 - BS 365; S17L - S19L Dent

L = 0.5" dia.. D = 0.013"

A/Y = 38SRM 53-00-01 fig 101

Minor


Mexicana Work Card

FD-12

18 11-Jan-00CAC 2000-5179

Seq 0488 / FR04

BS 590 - BS 600; S27L - S29L

Scratch ReworkScratch rework SRM 53-00-01 fig 101

Minor


CAC 2000-5179

Seq 0488 / FR04

See also D074

Not visible 30 Apr 15

ASL Airlines Belgium

MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012

DENT AND BUCKLE CHART INDEX

05 May 2020

61139.58 T.T. / 24419 T.C.Boeing B757-200 OE-LFB

Revision Dent & Buckle Index sheet of OE-LFB D&B Chart 20200505.xls 1 of 19

Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020


19 11-Jan-00CAC 2000-5177

Seq 0486 / FR05

BS 480 - BS 500; S27R - S28R

Scratch ReworkScratch rework SRM 53-00-01 fig 101

Minor

CAT AClosed 07-Feb-00

CAC 2000-5177

Seq 0486 / FR05

See also D045

Not visible

20 11-Jan-00CAC 2000-5048

Seq 0357 / FR06

BS 1374 - BS 1409; S28L -

S28RDent + Scratch rework

L = 17.625", W = 0.7", D =

0.036"

A/Y = 19



CAC 2000-5048

Seq 0357 / FR06

Rework to within limits

Xfer to R243

21 11-Jan-00CAC 2000-5178

Seq 0487 / FR07

BS 1500 - BS 1520; S25R -

S26RScratch rework SRM 53-00-01 fig 101

Minor


CAC 2000-5178

Seq 0487 / FR07

22 12-Jan-00CAC 2000-5170

Seq 0479 / FR08BS 1708; S20R - S21R Scratch rework SRM 53-00-01 fig 101

Minor


CAC 2000-5170

Seq 0479 / FR08Not visible 30 Apr 15

23 19-Jan-00CAC 2000-6128

Seq 0585 / FR03

BS 329 - BS 330.25; S18L

Scratch ReworkScratch rework SRM 53-10-01 PAG 189

Minor


CAC 2000-6128

Seq 0585 / FR03

24 17-Jul-03Mexicana Work Card

O614M033 / HSD01

RH Horizontal Stabiliser

Dent on Leading Edge at STA.

175.45

Dent

L = 0.79'' W = 0.7" D =

0.023"

A/Y = 30

SMR 55-10-01 fig 101Minor


Mexicana Work Card

O614M033 / HSD01


O614M034 / HSR01


Rework on Leading Edge at

STA 135.45

Scratch

0.365" x 0.089" x 0.005"

A/Y = 17

1.063" x 0.106" x 0.0004"

A/Y = 265



Mexicana Work Card

O614M034 / HSR01

See also D080 + D081

Re- Assessed @ phase in

SN000020 / 09 / SN001909


O614M034 / HSR02


Rework on Leading Edge at

STA 204

Scratch

0.213" x 0.065" x 0.008"

A/Y = 8

within limit



Mexicana Work Card

O614M034 / HSR02


SN000020 / 10 / SN001910

NOT VISIBLE


WCMD-01

Slat No. 10

Dent on Top of Trailing Edge.Dent

Dia. = 1" 0 = 0.03"

A/Y = 33SRM 57-43-02 FIG101

Minor


Mexicana Work Card

WCMD-01


WCMD-02

Slat No. 6

Several Dents Due to Hail

Damage on Trailing Edge

Multiple Dentsdia. = 0 .1" D = 0.002"

A/Y = 50SRM 57-43-02 fig 101

Minor


Mexicana Work Card

WCMD-02


WCMD-03

Slat No. 5

SEVERAL Dents DUE to Hall

DAMAGE on Trailing Edge.

Multiple Dentsdia. = 0 .1" D = 0.002"

A/Y = 50SRM 57-43-02 fig 101

Minor


Mexicana Work Card

WCMD-03

30 11-Jan-00

Challenge Air Cargo

Work Item 2000-5176

Seq 0485

/ CNA0325-07

Engine No. 1 Exhaust Nozzle

Assy

3:30 o'clock, Scratch on

Fairing.

Scratch L = 4.5" D = 0.004" SRM 54-40-01 fig 101Major


Challenge Air Cargo

Work Item 2000-5176

Seq 0485

/ CNA0325-07

ENG1 SN 0325


ID CNA0325-08


Assy

8.30 o'clock, Dent on Bond

Panel.

DentL = 1.5" dia. D = 0.02"

A/Y = 75SRM 54-40-01 fig 101

Minor


Mexicana Work Card

ID CNA0325-08

ENG1 SN 0325



ID CNA0325-09


Assy

9:00 o'clock, Dent on Bond

Panel.

Dent L = 0.75" dia. D = 0.007"

A/Y = 107SRM 54-40-01 fig 101

Minor


Mexicana Work Card

ID CNA0325-09

ENG1 SN 0325



ID CNA0325-10


Assy


Panel. s/n 0325

DentL = 0.75" dia. D = 0.005"

A/Y = 150SRM 54-40-01 fig 101

Minor


Mexicana Work Card

ID CNA0325-10ENG1 SN 0325


Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020



ID CNA0325-11


Assy


Panel Inner Skin.

Dent DIA = 0.32" D = 0.015 SRM 54-40-01 fig 101Minor


Mexicana Work Card



ID CNA0325-13


Assy

10 o'clock, Dent on Bond Panel

Inner Skin.

Dent L= 0.22"' D=0.015" SRM 54-40-01 fig 101Minor


Mexicana Work Card



ID CNA0325-14


Assy


Panel Inner Skin.

Dents 2 EAa/ L= 0.20"' D=0.015"

b/ L= 0.15"' D=0.015"SRM 54-40-01 fig 101

Minor


Mexicana Work Card


37 11-Jan-00

CAC 2000-5171 Seq

0480

Mexicana Work Card

ID CNA0329-02

Engine No. 2

Dent on CNA LID Bond Panel

9 o'clock.

Dent L=0.9" W=0.5" D=0.028" SRM 54-40-01 fig 101Minor


CAC 2000-5171 Seq

0480

Mexicana Work Card

ID CNA0329-02

ENG2 SN 0329


ID CNA0329-03

Engine No. 2


4:30 o'clock.

Dent L = 0.2" dia. D = 0.004" SRM 54-40-01 fig 101Minor


Mexicana Work Card



ID CNA0329-04

Engine No. 2

Dents on CNA LID Bond Panel

3:30 o'clock.

Dents

A/ L = 07" dia. D = 0.024

B/ L = 0.5" dia. D = 0.014"

C/ L =0.7" W=0.3'' D=0.011"



Mexicana Work Card

ID CNA0329-04

ENG2 SN 0329

See also D040


ID CNA0329-05

Engine No. 2

Dents on CNA LID Bond Panel

3:30 o'clock.

DentsA/ L = 0.3" dia D= 0.020"

B/ L = 0.2" dia D = 0.014"SRM 54-40-01 fig 101

Minor


Mexicana Work Card

ID CNA0329-05

ENG2 SN 0329

See also D039


ID CNA0329-06

Engine No. 2


9 o'clock.

Dent L = 0.7'' W = 0.2" D = 0.024" SRM 54-40-01 fig 101Minor


Mexicana Work Card


42 12-Jun-12ATC Lasham NRC

487320 Item 1BS 216.5, S23L - 24L Dent

A = 0.4", Y = 0.003"

A/Y = 133SRM 53-00-01

Minor

CAT AClosed 19-Jun-12

ATC Lasham NRC

487320 Item 1Not visible 30 Apr 15


487320 Item 2BS 290.5 LH NLG Door Dent

A = 1.1" Y = 0.01"

A/Y = 110SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 2


487320 Item 3BS 316, S21R - S22R Dent

A = 0.4" Y = 0.008"

A/Y = 50SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 3


487320 Item 4BS 486, S27R - S28R Dent

A = 1.5" Y = 0.014"

A/Y = 107SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 4

Double entry

See D019


487320 Item 5BS 539, S28R - S29R Dent

A = 0.5" Y = 0.014"

A/Y = 35SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 5See also D075

47 08-Jan-14 ADAT NRC 1073 BS 589, S29R - S30R DentA = 1", Y = 0.018"

A/Y = 55SRM 53-00-01-1A-1

Minor

CAT AClosed 16-Jan-14 ADAT NRC 1073


487320 Item 8BS 582; S27L - S28L Dent

A = 1.3" Y = 0.017"

A/Y = 76SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 8


487320 Item 9BS 1394; S30L - S29L Dent

A = 1.7" Y = 0.032"

A/Y = 53SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 9Xfer to R243


487320 Item 10BS 1423; S29L - S30L Dent

A = 1.7" Y = 0.012"

A/Y = 141SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 10See also R243


Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020



487320 Item 11BS 1402; S29L - S30L Dent

A = 1.6" Y = 0.014"

A/Y = 114SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 11

See also D005 & D073

See R106


487320 Item 12BS 1620; S29L - S30L Dent

A = 1" Y = 0.032"

A/Y = 31SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 12See R197


487320 Item 13BS 1617; S29L - S30L Dent

A = 2.3" Y = 0.024"

A/Y = 95SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 13See R197


487320 Item 14BS 1677, S27L, S28L Dent

A = 0.6" Y = 0.015"

A/Y = 40SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 14

Double entry

See D006

See R193


487320 Item 15BS 1677, S28L, S29L Dent

A = 0.4" Y = 0.005"

A/Y = 80SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 15See R193


487320 Item 16BS 1695, S27L, S28L Dent

A = 0.6" Y = 0.013"

A/Y = 46SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 16See R193


487320 Item 17BS 1650, S30 Dent

A = 1.5" Y = 0.02"

A/Y = 75SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 17See R093


487320 Item 18BS 1509, S21R, S22R Dent

A = 0.7" Y = 0.01"

A/Y = 70SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 18


487320 Item 19BS 1510, S21 R, S22R Dent

A = 0.5" Y = 0.005"

A/Y = 100SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 19


487320 Item 20BS 1514, S25R, S26R Dent

A = 0.5" Y = 0.009"

A/Y = 55SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 20


487320 Item 21BS 475, S15L, S16L Dent

A = 0.5" Y = 0.006"

A/Y = 83SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 21


487320 Item 22BS 260, S17L, S16L Dent

A = 0.9" Y = 0.011"

A/Y = 81SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 22

63 01-Dec-14

RH Stabiliser

Dent Leading Edge Skin

Sta.130.00

Dent A = 35, Y = 0.8 SRM 55-10-01 Rev. 85


SN000020 / 11 / SN001911

NOT VISIBLE

64 01-Dec-14

RH Stabiliser

Dent Leading Edge Skin, Sta.

320.00

Dent A = 40, Y = 0.8 SRM 55-10-01 Rev. 85 Replaced by D097

65 05-Jan-14 ADAT NRC 1021 BS 1612; S28R - S29R DentA = 3.15", Y = 0.014"

A/Y = 225

SRM 51-70-01-2R-1-D

SRM 53-00-01-1A

Minor


66 05-Jan-14 ADAT NRC 1019 BS 1604; S28R - S29R DentA = 3.4", Y = 0.040"

A/Y = 85SRM 53-00-01-1A

Minor


67 08-Jan-14 ADAT NRC 1069 BS 1510; S29L - S30L DentA = 1.0", Y = 0.018"

A/Y = 55SRM 53-00-01-1A-1

Minor

CAT AClosed 16-Jan-14 ADAT NRC 1069 See R217

68 05-Jan-14 ADAT NRC 1023 BS 1511; STR29 - S30R DentA: 0,800", Y: 0,025"

A/Y= 32SRM 53-00-01-1A-1

Minor


See also D101

See R217

69 08-Jan-14 ADAT NRC 1066 BS 705; S23 - S24L DentA = 1", Y = 0.002"

A/Y = 500SRM 53-00-01-1A-1

Minor


70 08-Jan-14 ADAT NRC 1067 BS 715; S19L - S20L DentA = 1", Y = 0.020"

A/Y = 50SRM 53-00-01-1A-1

Minor


71 08-Jan-14 ADAT NRC 1068 BS 460 - 480 EE door DentA = 1.6", Y = 0.034"

A/Y = 47SRM 52-40-01-1A-2

Minor

CAT AClosed 16-Jan-14 ADAT NRC 1068 Not visible 30 Apr 15


487320 Item 6BS 596, S26R - S27R Dent

A = 1" Y = 0.0095"

A/Y = 105SRM 53-00-01

Minor


ATC Lasham NRC

487320 Item 6


Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020


73 08-Jan-14 ADAT NRC 1070 BS 1407, S29L - S30L Dent A = 1.7", Y = 0.022" A/Y = 77 SRM 53-00-01-1A-1Minor


See also D051

/ R178 & R243

74 08-Jan-14 ADAT NRC 1071 BS 598, S28L - S29L DentA = 0.8", Y = 0.012"

A/Y = 66SRM 53-00-01-1A-1

Minor


Double entry

See D018

75 08-Jan-14 ADAT NRC 1072 BS 539, S28R - S29L DentA = 1", Y = 0.015"

A/Y = 66SRM 53-00-01-1A-1

Minor


Double entry

See D046

76 09-Jan-14 ADAT NRC 6017

Slat No. 7

wedge top surface

1/ 15" from I/B

2/ 40" from O/B

3/ 6" from O/B

3 Dents

1/ A = 0.4", Y = 0.014"

A/Y = 28.5

2/ A = 0.4", Y = 0.015"

A/Y = 26.6

3/ A = 0.5", Y = 0.018"

A/Y = 27.7

SRM 57-43-02-1A-1Minor

CAT AClosed

16/01/2014

11/02/2019

ADAT NRC 6017

ACE DR 095261

P/N 114N4005-178A S/N

A2-0294 OFF

P/N 114N4005-178A S/N

A2-0250 ON

77 09-Jan-14 ADAT NRC 6020

Slat No. 8

TEWedge Upper Skin on I/B

Edge

Dent filledA = 0.5", Y = 0.022"

A/Y = 22.72SRM 57-43-02-1A-1

Minor

CAT AClosed

16/01/2014

11/02/2019

ADAT NRC 6020

ACE DR 095265

P/N 114N4004-166A S/N

A2-0297 OFF

P/N 114N4004-172A S/N

A2-0514 ON

78 09-Jan-14 ADAT NRC 5014Slat No. 2

Wedge Upper SurfaceDent filled

A = 0.5", Y = 0.018"

A/Y = 27.7

SRM 57-43-02-1A Fig 101 Sht

3

SRM 51-70-01 Para 4C

Minor


PN 114N4003-171 SN ??

See also D079 and R073 +

R190

79 07-Jan-14ADAT NRC 5002

ADAT EER27346

Slat No. 2

Nose Skin Blend Repairs x 2

@ OSS 605.30 and OSS

617.30

15 Blends

SR 3-2597704425

GMO- SKK-14-0004-*

with 8100-9

Minor


ADAT NRC 5002

ADAT EER27346

PN 114N4003-171 SN ??

See also D078 and R073 +

R190


ADAT EER 27358


Scratch long sides of Leading

Edge Panel 342BR

Sctratch

SR 3-2603761422

GMO- SKK-14-0006-*

with RDR

Minor


ADAT NRC 3019

ADAT EER 27358See also D025 + D081


ADAT EER 27358


Erosion on Leading Edge

Panel 342BR

Blends

SR 3-2603761422

GMO- SKK-14-0006-*

with RDR

Minor


ADAT NRC 3020

ADAT EER 27358See also D025 + D080

82 12-Jan-14 ADAT NRC 4016


Assy

3.00 o'clock positions.

2 Dents

1/ L=0.6'', W=0.5" ,

D=0.005''

2./ L=1 .6'', W=1", D=0.018"'


CAT AClosed 16-Jan-14 ADAT NRC 4016 See also D031 + D032

83 12-Jan-14 ADAT NRC 4023Engine No. 2

CAN at 3 o'clock locations4 Dents

1/ 0.450'' x 0.400" x 0.012''

2/ 0.400'' x 0.250" x 0.0075''

3/ 0.850'' x 0.500" x

0.0095''

4/ 0.400'' x 0.250" x

0.0015''




CAN at 9 o'clock locations2 Dents

1./ 0.450'' x 0.25" x 0.0125''

2/ 0.400'' x 0.25" x 0.0012''SRM 54-40-01-1A

Minor



Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020



CAN at 11 o'clock locationDent 0.450'' x 0.400" x 0.010'' SRM 54-40-01-1A

Minor


86 09-Jan-14 ADAT NRC 4026

Engine No. 2

I/B T/R Skin at 9 o'clock

location

2 DentsSRM 54-30-01-1A-1

SRM 54-30-01-2R-1 Repair 1

Minor

CAT AClosed 16-Jan-14 ADAT NRC 4026 See R126


ADAT EER 27359

LH Horizontal Stabiliser

L/E Panels 332BL, 332CL

332DL

lower surface

Blends

SR 3-2602117571

GMO-SKK-14-0005-*

with RDR

Minor


ADAT NRC 3018

ADAT EER 27359


ADAT EER 27347

Left Wing Lower Surface

between Rib 1 and 2 from

Stringer U-16 to U-24 mating to

Fairing 193FL Seal

Scratch blend out rework size 32" x 0.8"

SR 3-2597594345

GMO-SKK-14-0003-*

with 8100.9

Major

CAT AClosed 08-Apr-15

GMO-SKK-14-0003-14

with 8100-9New 8100-9 : Cat A

89 01-Dec-14 BS 500; S16L Dent

SRM 53-00-07

SR 3-3097595674

AWW-AWW-15-0002-*

Requires repair per SRM 53-

00-01-R7

Xfer to R194

90 11-Nov-08TIMCO NRC 34982

TIMCO WO 318002

Lower fwd fuselage below

main cargo door scuff plat. BS

600-612

3 Dents

1/ A=2.3" , Y=0.045"

A/Y = 51

2/ A=1.41" , Y = 0023"

A/Y = 61

3/ A=1.41" , Y = 0023"

A/Y = 61

53-00-01 fig 101 detail IIIMinor

CAT AClosed 16-Dec-08

TIMCO NRC 34982

TIMCO WO 318002

91 NRC 4016Dent eng 1 CNA outer surface

at 9 o'clock position

L: 0,6 W:0,5 depth: 0,005

L: 1,6 W: 1 depth 0,018

SRM 54-40-01-1-0 fig 101 SH

4

92 NRC 4017Gouge eng 1 CNA trailing edge

@ 6 o'clockBlend out L: 0,75 depth 0,08

SRM 54-40-01-1-0 fig 101 SH

4

Minor

Cat AClosed 12-Jan-14 NRC 4017 SN 0325

93 05-Jan-14 NRC 4024Gouge eng 2 CNA trailing edge

@ 7 o'clockBlend out L: 0,75 depth 0,08

SRM 54-40-01-1-0 fig 101 SH

4

Minor

Cat AClosed 12-Jan-14 NRC 4024 SN 0329

94 05-Jan-14 NRC 4012Eng 1 inlet cowl lip scratch @

6 o' clock positionBlend out

W: 0.4"

nom thickness 0.091"

removed 0.002"

SRM 51-10-02Minor

Cat AClosed 09-Jan-14 NRC 4012

Part replaced

See R223

95 05-Jan-14 NRC 4025ESN 30770 Inlet Cowl Lip

- 6:00 o'clock, scratchBlend out

nom thickness 0.092"

removed 0.003"SRM 54-10-01-A2

Minor

Cat AClosed 09-Jan-14 NRC 4025 ENG2 SN 0329


ID CNA0325-12

ESN 30769 Common Nozzle

Assy s/n 0325

- 7:00 o'clock, Trail of Lightning

Strikes

Blend out

A/ L: 0,1," D: 0,005"

B/ L: 0,3 " D: 0,01"

C/ L: 0,35" D: 0,007"

D/ L: 0,5" D: 0,035;"

E/ L: 0,35" D: 0,023"


Cat AClosed 05-Aug-03

Mexicana Work Card


97 17-Feb-15 Cardiff NRC0010856RH Stabiliser

LESkin Sta 320.00Dent

A = 0.75" Y = 0.022"

A/Y = 34SRM 55-10-01-A1

Minor

Cat BClosed 02-Apr-16 LG 000156 Replaces D064

98 20-Apr-15 TFLB 24868029-3Fuselage BS1600/1620 S-

28R/29RDent

A = 2.40" Y = 0.028"

A/Y = 85SRM 53-00-01

Minor

Cat AClosed 20-Apr-15 TFLB 24868029-3 See also D002

99 20-Apr-15 TFLB 24868030-1ENG 2 I/B fan cowl

approx 8 o'clockDent SRM 54-20-01

Minor

Cat AClosed 20-Apr-15 TFLB 24868030-1

100 20-Apr-15 TFLB 24868030-2Fuselage BS1408

S-24L/25LDent

A = 0.30" Y = 0.0065"

A/Y = 46SRM 54-20-01

Minor



Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020


101 20-Apr-15 TFLB 24868030-3Fuselage BS1500

S-29R/30RDent

A = 0.50" Y = 0.008"

A/Y = 62SRM 53-00-01

Minor


See also D068

See R217

102 20-Apr-15 TFLB 24868031-1 Fuselage BS1410 S-25L/26L DentA = 0.20" Y = 0.009"

A/Y = 22SRM 53-00-01

Minor

Cat AClosed See R204

103 20-Apr-15 TFLB 24868031-3Fuselage BS1380/1400 S-

24L/25LDent

A = 0.20" Y = 0.009"

A/Y = 22SRM 53-00-01

Minor


104 20-Apr-15

Fuselage FWD cargo door cut

out fwd edge

blend out @ S-24R

Blend out 1.20" x 0.061" x 0.200"

SR 3-3223961678

AWW-AWW-15-0021-*

with 8100-9

Minor

Cat CSNT DB-LFB-104 Open See R224

105 06-May-15

SN000020 /

SN001985 +

M467030

BS1578 S-29R/30R Dent3.50" x 1.50" x 0.020"

A/Y = 75SRM 53-00-01-A1

Minor

CAT AClosed 15-May-15

SN000020 /

SN001985 +

M467030

See D149

106 23-Apr-15SN000020 / 53 /

SN001955BS 260/263 S-19L/20L Buckle

0.75" x 0.039"

A/Y = 19SRM 53-00-01-A1

Minor


107 05-May-15SN000020 / 15 /

SN001915

LH I/B aft flap lower surface

O/B side

11" from O/B ; 13.78" from TE

Dent (filled)7.87" x 4.33 " x 0.142"

A/Y = 30SRM 57-53-01-A1

Minor

Cat B5700EXP01 Open Filled dent

108 05-May-15SN000020 / 16 /

SN001916

RH I/B aft flap lower surface

O/B side

27.56" from O/B ; 23.62" from

TE

Dent23.62" x 5.91 " x 0.079"

A/Y = 74SRM 57-53-01-A1

Minor

Cat B5700EXP02 Open See also R202

109 23-Apr-15SN000020 / 57 /

SN001959 (D)BS1510 S-29R/30R Dent

0.472" x 0.022"

A/Y = 21SRM 53-00-01-A1

Minor


110 23-Apr-15SN000020 / 57 /

SN001959 (C)BS1510 S-29R/30R Dent

0.315" x 0.024"

A/Y = 13SRM 53-00-01-A1

Minor

Cat AOpen See R217

111 23-Apr-15SN000020 / 57 /

SN001959 (B)BS1510 S-29R/30R Dent

0.591" x 0.031"

A/Y = 18SRM 53-00-01-A1

Minor

Cat AOpen See R217

112 23-Apr-15SN000020 / 57 /

SN001959 (A)BS1510 S-29R/30R Dent

0.551" x 0.015"

A/Y = 36SRM 53-00-01-A1

Minor

Cat AClosed 05-May-15

SN000020 / 57 /

SN001959 (A)See R217

113 04-May-15 M467026

ENG 2 I/B fan cowl

surface damage @

9 o'clock

Nick 0.236" x 0.079" x 0.039" SRM 54-20-01-A1Minor

Cat AClosed 05-May-15

114 05-May-15SN000020 / 15 /

SN001915


(wheel area)Dent

1.968" x 0.004"

A/Y = 137SRM 57-53-01-A1

Minor

Cat B5700EXP01 Open See also D115

115 05-May-15SN000020 / 15 /

SN001915


(wheel area)Dent

3.150" x 0.004"

A/Y = 787SRM 57-53-01-A1

Minor

Cat B5700EXP01 Open See also D114

116 23-Apr-15SN000020 / 54 /

SN001956

BS 1520

S24R - S25RBuckle

SRM 53-00-01-A1

Flagnote H

Minor


SN000020 / 54 /

SN001956

117 23-Apr-15SN000020 / 55 /

SN001957

BS 1540

S25R - S26RBuckle

SRM 53-00-01-A1

Flagnote H

Minor


SN000020 / 55 /

SN001957

118 23-Apr-15SN000020 / 56 /

SN001958

BS 1580

S25R - S26RBuckle

SRM 53-00-01-A1

Flagnote H

Minor


SN000020 / 56 /

SN001958

Blended

Not visible

119 15-May-15SN000020 /

SN001983

BS460/480

S-23R - 24RDent

1.50" x 1.00" x 0.010"

A/Y = 100SRM 53-00-01-A1

Minor


SN000020 /

SN001983

120 15-May-15

SN000020 /

SN001983 +

SN001984

BS480/500

S-23R - 24RDent

0.75" x 0.50" x 0.006"

A/Y = 83SRM 53-00-01-A1

Minor


SN000020 /

SN001983 +

SN001984


Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020


121 15-May-15SN000020 /

SN001982

BS460/480

S-26R - 27RDent

1.00" x 0.75" x 0.003"

A/Y = 250SRM 53-00-01-A1

Minor


SN000020 /

SN001982

122 15-May-15SN000020 /

SN001981

BS460/480

S-27R - 28RDent

2.000" x 0.016"

A/Y = 125SRM 53-00-01-A1

Minor


SN000020 /

SN001981

123 15-Jul-15

IBERIA FR

006700133849

LFB-020

Fuselage

BS620/640 S-18R/196RBlend out

nominal thickness 0.080"

remaining thickn 0.072"Rev 93 SRM 53-00-01-A1

Minor

Cat AClosed 22-Jul-15

IBERIA FR

006700133849

LFB-020

124 15-Jul-15

IBERIA FR

006700133882

LFB-023

Fuselage

BS720/740 S-23R/24RBuckle

1.00" x 1.00" x 0.015"

A/Y = 66Rev 93 SRM 53-00-01-A1

Minor


IBERIA FR

006700133882

LFB-023

125 15-Jul-15

IBERIA FR

006700133886

LFB-028

Fuselage

BS440/480 S-14R/15RDents 4 EA

1/ 2.00" x 0.50" x 0.007"

A/Y = 71

2/ 2.00" x 0.50" x 0.007"

A/Y = 71

3/ 2.00" x 0.50" x 0.006"

A/Y = 83

4/ 2.00" x 0.50" x 0.007"

A/Y = 71

Rev 93 SRM 53-00-01-A1Minor


IBERIA FR

006700133886

LFB-028

126 15-Jul-15

IBERIA FR

006700133857

LFB-032

Fuselage crown area

BS 960 thru 1440 and S-3L

thru S-2R

Blend outs 15 EA

max depth 0.006"

less than 10% original

thickness



IBERIA FR

006700133857

LFB-032

127 22-Jul-15

IBERIA FR

006700133990

LFB-053

LH aft W-t-B fairing

slight corrosion on formed

angle BS1037/1060

Blend out

6.50" x 2.00" x 0.008"

nominal thickness 0.100"

remaining thickness 0.092"


Cat AClosed 08-Aug-15

IBERIA FR

006700133990

LFB-053

128 02-Jul-15

IBERIA FR

006700133937

LFB-054

LH wing fixed LE

gouge OSS 838Blend out

SRM 57-41-01

SRM 51-70-06 Para 4

SRM 51-70-17 Para 4G

Minor


IBERIA FR

006700133937

LFB-054

129 21-Jul-15

IBERIA FR

006700133934

LFB-47

WR0000399242

ENG 1 LH TR

outer skin @ 10 o'clockDent

3.00" x 1.00" x 0.050"

A/Y = 200AMM 71-11-01

Minor


IBERIA FR

006700133934

LFB-47

WR0000399242

Only paint damage

130 03-Jan-16 SRP 7712Fuselage

BS640/660 S-22L/23LDent

0.250" x 0.002"

A/Y = 500

SRM 53-30-01-A1

SRM 53-00-01-A1

Minor

Cat AClosed 03-Jan-16 SRP 7712


BS700/720 S-23L/24LBuckle

SRM 53-30-01-A1

SRM 53-00-01-A1

Minor



BS324/333 S-16L/17LDent

2.00" x 1.00" x 0.007"

A/Y = 142

SRM 53-10-01-A1

SRM 53-00-01-A1

Minor



BS333/345 S-22L/23LDents 2EA

0.250" x 0.002"

A/Y = 500

1.000" x 0.009"

A/Y = 111

SRM 53-30-01-A1

SRM 53-00-01-A1

Minor



BS368 S-17L/18LDent

0.250" x 0.008"

A/Y = 31

SRM 53-30-01-A1

SRM 53-00-01-A1

Minor



BS1540/1560 S-26RBuckle

SRM 53-60-01-A1

SRM 53-00-01-A1

Minor


136 03-Jan-16 SRP 7714

Fuselage

BS1370/1405 S-28L/27R

(2 parallel lines)

Scratch39" x 2.5" x 0.030" (max)

A/Y = 83

SRM 53-60-01-A1

SRM 53-00-01-A1

Minor

Cat AClosed 03-Jan-16 SRP 7714 See R195 & R243


Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020


137 19-Mar-16 SRP 7378

Fuselage

BS223/231 above S-20R

Birdstrike

Dent4.60" x 3.50" x 0.025"

A/Y = 140SRM 53-00-01 AD1 Detail III

Minor

Cat AClosed 19-Mar-16 SRP 7378

138 19-Mar-16 SRP 7379

Fuselage

BS215/223 above S-20R

Birdstrike

Dent4.80" x 2.60" x 0.085"

A/Y = 30.5SRM 53-00-01 AD1 Detail III

Flagnote J

Minor

Cat AClosed 19-Mar-16 SRP 7379

Dent more than wavines

limit per SRM 51-10-01

Fig 3

139 16-Jul-17 ACE DR 084254Fuselage at BS351 between

S15L - S16LDent

2.83" x 1.89" x0.02"

A/Y = 94.5SRM 53-00-01 AD1 Detail III

Minor

Cat AClosed 17-Jul-17 ACE DR 084254

140 16-Jul-17 ACE DR 084255Fuselage at BS410 between

S9L - S10LDent

1.40" x 0.02"


Minor


141 03-Aug-17 ACE DR 084314ENG 2 Outb T/R sleeve Aft

inner side Dent 1.0" x 0.5" x0.07" MM 78-31-23 Page 602

Minor

Cat AClosed 03-Aug-17 ACE DR 084314

142 19-Nov-17HAITEC WO

13212/0000-0002

Fuselage between BS1480 &

BS1500 and S24R - S25RDent

4.25" x 0.118"

A/Y = 36.01

SRM 53-60-03

SRM 53-00-01

Minor

Cat AClosed 19-Nov-17

HAITEC WO

13212/0000-0002

143 16-Jul-17 ACE DR 084329

LH Inboard flap Upper skin

corroded at line of the front

spar

Blend Out X Max = 0.012"SRM 57-53-01 AD1 Fig 101

Detail I, Note N

Minor


144 14-Jul-17 ACE DR 084326/1

LH Wing Upper skin Several

surface corrosion marks Inb of

W/S 369.5

Blend outs 17 EATotal Max loss =

0.0415 sq inchSRM 57-20-01 AD1 Table 1

Minor

Cat AClosed 16-Jul-17 ACE DR 084326/1

145 14-Jul-17 ACE DR 084326/2

LH Wing Upper skin Several

surface corrosion marks

between W/S 369.5 and W/S

481.5

Blend outs 3 EATotal Max loss =

0.0076 sq inchSRM 57-20-01 AD1 Table 1

Minor

Cat AClosed 16-Jul-17 ACE DR 084326/2

146 26-Jun-16 SRP 7762

ENG 1 nose cowl

Replacement with 3 items

-2 gauges on lip skin @ RAD

270 (WO it 560)

-scratches (WO it 570)

-dishing @ RAD 120 (WO it

560)

Gauges

Scratches

Dishing

-0.2" x 0.1" x 0.010"

0.3" x 0.1" x 0.010"

-…………….

-0.8" x 0.7"

Bombardier Aerospace

STC ST02102NY

BOMBARDIER WO 30076501

Minor

Cat AClosed 26-Jun-16 SRP 7762

OFF PN LJ39448 SN

SB/RR/4188

ON PN LJ50958 SN

SB/RR/4044

Post SB RE.211-71-H438

and AD 2014-09-07 per

Bombardier Aerospace

STC ST02102NY

See also R223

147 17-Jul-17 ACE DR 081501

Surface corrosion on wing

upper surface at STA 1040

under wing to body fairing

Blend Out X Max = 0.015" SRM 57-20-01 AD1 Table 1Minor

Cat AClosed 07-Aug-17 ACE DR 081501

NOT ON DWG

No sticker installed

148 16-May-18 SN 006279

RH Engine Outboard, Fan

Cowl Panel inboard lower side

corroded

Blend Out X Max = 0.01" SRM 54-20-01 AD1Minor

Cat AClosed 21-May-18 SN 006279

RE-ASSESSMENT DONE


149 10-Mar-18 SRP 14442-1Fuselage BS1576.5 S-

29R/30RDent

2.36" x 0.866" x0.026"


Minor

Cat AClosed 10-Mar-18 SRP 14442-1


Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020


150 30-Jun-18HAITEC NRC 13795 -

0009

Fuselage

BS1380/1400 S-29R/30RDent

A = 0.581" Y = 0.03"

A/Y = 19.37

Rev 98 SRM 53-00-01-AD1

Detail III

Minor

Cat CDB-LFB-150 Open See R243

151 30-Jun-18HAITEC NRC 13795 -

0013

Fuselage

BS1380/1400 S-29R/30RDent

A = 1.118" Y = 0.029"

A/Y = 37.87

Rev 98 SRM 53-00-01-AD1

Detail III

Minor

Cat AClosed 30-Jun-18

HAITEC NRC 13795 -

0013See R243

152 24-Jan-19 ACE DR 095053

Main Cargo Floor surface

corrosion btw STA 320 & STA

620

Blend out 3,14" x 1" x 0,02" SRM 53-00-51 AD1 Detail IIIMinor

Cat AClosed 30-Jan-19 ACE DR 095053

NOT ON DWG


153 16-Jan-19 ACE DR 095298

Surface corrosion btw STA 620

& 640 RH on the side wall

support frame

Blend out 1" x 1" x 0,001" SRM 53-00-07 AD1 Detail I & IIMinor

Cat AClosed 29-Jan-19 ACE DR 095298

NOT ON DWG


154 01-Feb-19 ACE DR 095084Fuselage at STA 232, LH Lwr

Section LBL 15Dent

1.1" x 0.8" x 0.007"


Minor

Cat AClosed 05-Feb-19

155 01-Feb-19 ACE DR 095083Fuselage at STA 322, btw S-

18L/19LDent

Dia. 0.85" x 0.01"


Minor


156 31-Jan-19 ACE DR 095082Fuselage at STA 1537, btw S-

23R/24RDent

1.2" x 0.9" x 0.012"


Minor



28L/29LDent

Dia. 0.9" x 0.001"


Minor


158 31-Jan-19 ACE DR095080Fuselage at STA 257; 28"

above S-20L LapjointDent

Dia. 0.8" x 0.009"


Minor



4R/5RDent

1.6" x 0.9" x 0.009"


Minor


160 23-Jan-19 ACE DR 095249

Surface corrosion at the main

Cargo floor structure Btw STA

1720 & STA 1681

Blend out1.0" x 1.0" x 0.02"

A/Y = 50SRM 53-00-51 AD I Detail III

Minor

Cat AClosed 30-Jan-19

NOT ON DWG



Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020


161 01-Feb-19 ACE DR 095085Fuselage at STA 1907,

WL262, LH sideDent

Dia. 0.75" x 0.018"

A/Y = 41

SRM 53-80-01 AD, Table I,

Detail IV

Minor


162 22-Jan-19 ACE DR 095124Surface corrosion in the CTR

wing zone at the floor structureBlend outs 3 EA

1: 2.51" x 1.18" x 0.02"

A/Y = 59

2: 1.18" x 1.18" x 0.001"

A/Y = 1180

3: 1.14" x 0.39" x 0.005"

A/Y = 78

SRM 53-00-51 AD I Detail IIIMinor


NOT ON DWG


163 17-Jan-19 ACE DR 095232

FWD Cargo Comp, #3 L/H

Strap at Floor-to-side wall

panel cracked

Blend outLenght: 1.97"

Depth 0.05"SRM 53-00-53 AD I Detail III

Minor


NOT ON DWG


164 23-Jan-19 ACE DR 095250

Surface corrosion at the main

Cargo floor structure Btw STA

1580 & STA 1600 near LBL

45.7

Blend outs 2 EA

1: 1.77" x 0.78" x 0.02"

A/Y = 39

2: 1.37" x 0.59" x 0.005"

A/Y = 118

SRM 53-00-53 AD I Detail IIIMinor


NOT ON DWG


165 14-Jan-19 ACE DR 095259

Keel beam access panels

support frame doublers

corroded on L/H side (3ea of

doublers)

Blend out Material Loss Max 3% SRM 53-30-12 AD I Detail IVMinor


NOT ON DWG


166 14-Jan-19 ACE DR 095260

Keel beam access panels

support frame doublers

corroded on R/H side (3ea of

doublers)

Blend out Material Loss Max 4% SRM 53-30-12 AD I Detail IVMinor


NOT ON DWG


167 14-Jan-19 ACE DR 095283

FWD LWR Wing to Body

fairing Drain Mast bracket

corroded

Blend outMaterial Loss Max 4%

1.253" X 0.853"SRM 53-00-71 AD I

Minor


NOT ON DWG


168 14-Jan-19 ACE DR 095317

RH AFT W-t-B fairing structure

at STA 1220 Btw BL0 and

BL30.75 corroded

Blend out Material Loss Max 8% SRM 53-00-71 AD IMinor


NOT ON DWG


169 21-Jan-19 ACE DR 0015049

Intercostal at STA 620 btw

S22R and S21R corrodded

(FWD Cargo Door AFT side)

Blend out 1.65" x 0.4" x 0.01" SRM 53-00-04 AD1 Detail IIMinor


NOT ON DWG


170 14-Jan-19 ACE DR 095279LH Side #2 Ball Panel Upper

SkinDent Dia = 2" SRM 53-00-50 AD1

Minor


NOT ON DWG



Part I - GENERAL


Chart

Ref.Date Raised

Logged on


Description of

Damage

Area and depth of


Logged on

DocumentRemarks


MSN 24868

TEC/05-003.6

REVISION 2

19 JUL 2012


05 May 2020


171 16-Jan-19 ACE DE 095296

Intercostal at AFT Cargo Door

Cut-Out btx STA 1380 and

STA 1360 & S27L AFT corner

corroded

Blend out 2.16" x 1.97" x 0.03" SRM 53-00-04 AD1 Detail IIMinor


NOT ON DWG


172 23-Jan-19 ACE 095125

The LH Landing Gear Trunion

Door Inboard FWD corner

(Seal Retainer) is damaged

Blend out 0.75" x 0.09"SRM 52-80-02 AD4 Fig. 101

Detail VI

Minor


NOT ON DWG


173 02-Jun-19 SRP 12868 Item 08

RH Horiz Stab Leading Edge

Center Panel, 40" from Panel

Inb Edge

Dent0.75" x 0.75" x 0.022"

A/Y = 34SRM 55-10-01 ADI Rev 105

Minor

Cat AClosed 02-Jun-19

174

175

176

177

178

179

180

181


Part I - GENERAL


Boeing B757-200 MSN 24868 OE-LFB05 May 2020

61139.58 T.T. / 24419 T.C.

Dent & Buckle CHART DRAWINGS

TEC/05-003.6

REVISION 2

19 JUL 2012ASL Airlines Belgium

Left Side View

X

Dashed line means not visible from the exterior Y

73 7

8

10

17

12 18

23 132 155

42 43

50

61 62

69

70

71

90 100 126

127

130 131

134

140

158 154 161

157

139

Revision Dent & Buckle Drawings sheet of OE-LFB D&B Chart 20200505.xls 13 of 19

Part I - GENERAL



61139.58 T.T. / 24419 T.C.


TEC/05-003.6

REVISION 2


Right Side View

2 65 66 98

11 117 135

13 116 156

14 19

157

21 60

22 44 46 72

58

59

47

118 149

119 thru 122

123

124

125 126

137

138

142

159


Part I - GENERAL



61139.58 T.T. / 24419 T.C.


TEC/05-003.6

REVISION 2


Front View

95

146

146


Part I - GENERAL



61139.58 T.T. / 24419 T.C.


TEC/05-003.6

REVISION 2


RH LHWing Surface Bottom

88

107 108 114 115


Part I - GENERAL



61139.58 T.T. / 24419 T.C.


TEC/05-003.6

REVISION 2


LH RHWing Surface Top View

27

28 29

78 79

128

144

145

143


Part I - GENERAL



61139.58 T.T. / 24419 T.C.


TEC/05-003.6

REVISION 2


LH RH RH LH

Horizontal Stab.Top View

Horizontal Stab.Bottom View

24

173 25

26

87

97

80

81


Part I - GENERAL



61139.58 T.T. / 24419 T.C.


TEC/05-003.6

REVISION 2


Engine #1 Side View

Engine #2 Side View

30 31

32

33

34

35

37

38

39

85

92

93

36

99

82

84

41 40

83

113

96

141 148


tec/05-003.6 dent and buckle chart index revision 2 part … · 2020. 8. 20. · dent and buckle...

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