tec/05-003.3 dent and buckle chart index … · tec/05-003.3 18-jun-08 dent and buckle chart index...

18-Jun-08

DENT AND BUCKLE CHART INDEX

**Report all dimensions in inches**

TNT Airways S.A.

TEC/05-003.3

REVISION 2

Registration: OO-THA Total Time: 34473,00Aircraft MSN: 35232 Total Cycles: 4507Aircraft Type: B747-4HAF Date: Balthazar BONNEFOY

Reported

16/11/2015

p

Item Location Type Dimensions Class Approval basis Reported on SRP / NRC Status

1LH Below Crew Door

BS 420 - BS440STR 28A - STR 30

Dent / Scratch

L = 6.500"A = 2.000"Y = 0.040"A/Y = 50

N/A

Reworked per SRM 53-00-01 Fig 101

Table 1 iaw SRM 53-10 01

920 FH151 FC

14/04/2007

KLM NRC 40LS5001

visit ref 035700

Closed

Remarks

Material removed = 0.008" - -

Limitation Tracking

A/Y = 50 10-01 035700

2RH Outer Skin

BS 375 Dent

L = 5.000"A = 4.000"Y = 0 100" N/A

Allowable per SRM 53-00-01 Fig 101

Table 1 iaw SRM 53-

1379 FH216 FC SRP 0437

item 10 Closed -- -STR 41 - STR 42 Y = 0.100

A/Y = 40Table 1 iaw SRM 53

10-01 31/05/2007 item 10

3RH Outer Skin

BS 03 D

L = 2.200"A = 1.400" N/A

Allowable per SRM 53-00-01 Fig 101 3399 FH

13 FC SRP 304450 Cl d3 BS 503 STR 39 - STR 40

Dent A 1.400Y = 0.040"A/Y = 35

N/A 53 00 01 Fig 101 Table 1 iaw SRM 53-

10-01

513 FC28/11/2007

SRP 304450 item 03 Closed

RH Fuselage Outer A 1 800" Reworked per SRM 4575 FH

SRP 305998 item 04

- --

4

gSkin

BS 520 - BS 540STR 32 - STR 34

ScratchA = 1.800"Y = 0.008"A/Y = 225

N/A

p53-00-01 Fig 101

Table 1 iaw SRM 53-20-01

4575 FH685 FC

06/04/2008

KLM NRC 40-S5001

visit ref 038775

Closed- - -

TNT Airways S.A Revision 34 of 23

18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p

Item Location Type Dimensions Class Approval basis Reported on SRP / NRC Status RemarksLimitation Tracking

5LH Outer Skin

BS 2250STR 29

ScratchA = 6.000"Y = 0.010"A/Y = 600

N/A

Allowable per SRM 53-00-01 Fig 101

Table 1 iaw SRM 53-60 01

7936 FH1164 FC

12/01/2009

SRP 306976 item 04 Closed -- -

60-01

6 LH Wing Landing Gear Lower Strut Door Dent L = 1.000"

Y = 1 ply N/A

Temporary Allowable per SRM 51-70-02 Table 1

7938 FH1164 FC

KLM NRC 09WK5001vi

sit ref 040769 and Open

Covered per Repair File Item No 17

Q-Task:Q-2009-74-0001

Inspection at every A-check and final repair at next C-

Gear Lower Strut Door Y = 1 ply Item 18 iaw SRM 52-80-02

12/01/2009 09-M5001 visit ref 041120

LH Inboard Mid Flap Lower side D

A = 1,181"Y 0 023" N/A

Temporary Allowable per SRM 10617 FH

1 28 FC

KLM NRC 11-S5001 O

File Item No. 17

Covered per RepairInspection at every A-check d fi l i t t C Q-Task:

Q 2009 74 0001check

7 Lower sidePN 65B02025-213A

SN 695

Dent Y = 0,023"A/Y = 50

N/A Allowable per SRM 57-53-01 Fig 101

Item 1

1528 FC11/10/2009

11 S5001 visit ref 042863

Open

RH O t Ski A 3 800" Allowable per SRM 10617 FH KLM NRC

Covered per Repair File Item No. 18and final repair at next C-

check

Q Task:Q-2009-74-0025

8RH Outer Skin

BS 368STR 14 - STR 15

DentA = 3,800"Y = 0,080"A/Y = 47

N/A

p53-00-01 Fig 101

Table 1 iaw SRM 53-10-01

10617 FH1528 FC

11/10/2009

40-S5001 visit ref 042863

Closed -- -


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


Dent A:L = 2,440"A = 0,860"Y = 0,011"

Dent B:

9

LH Inboard Mid Flap Lower side

PN 65B02025-213ASN 695

Dent-

Birdstrike

L = 3,010"A = 2,750"Y = 0,055"

Dent C:L = 1,290"A = 0,900"Y = 0,011"

D t D

Minor

Temporary allowable till next C

check with repetitive

inspections as per Boeing Message

TNB-TNB-10-0010-

11705 FH1664 FC

12/01/2010

SRP 309714 Item 01 Open

Dent A, B, C and D are within Dent E.

-Covered per Repair

File Item No. 19

DVI every 7 days, tap test every 14 days and final repair at next C-check

Q-Task:Q-2009-74-0033 REV01

Dent D:A = 1,250"Y = 0,025"

Dent E:L = 12,990"A = 9,050"Y = 0,078"

06B

10LH FuselageSTA 515.5STR 27A

DentA = 2,125"Y = 0,0049"A/Y = 434

N/A

Allowable per SRM 53-00-01 Fig 101 Detail 3 iaw SRM 53-10-01 Fig 101

12171 FH1722 FC

16/02/2010

KLM NRC 40-S5001

visit ref 043693

Closed- - -

11

RH Inboard Aft Flap Lower SideWBL 387.5

PN 65B02070-76ASN 698

DentA = 1,772"Y = 0,059"A/Y = 30

N/A

Temporary Allowable per SRM 57-53-01 Fig 101 Item 1 Flagnote C

12171 FH1722 FC

16/02/2010

KLM NRC 12-S5001

visit ref 043693

Open

Covered per Repair File Item No. 20

-Flap installed on OO-THB; Repair File Item

No 102

Inspection at every A-check and final repair at next C-

check

Q-Task:Q-2010-74-0008

No. 102


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


12

RH Inboard Aft FlapUpper Panel Assy

P/N: 65B02070-76AS/N: 000701

Dents-

Hail Strike

Appendix 1-

Not visible Potted per SRM 51-

N/A

Allowable per Boeing Service Request ID 1-

1571993697 and

8256 FH1114 FC

22/06/2009

KLM NRC 12GM5002

visit ref 042115

OpenDVI and tap test at next two

subsequent C-checksQ-Task:

Q-2010-74-0006

Flap from OO-THB; Installed on25-09-2010

-Flap installed on OO-

S/N: 000701 70-01 par 4C RDR 042115

13

RH Inboard TE Aft Flap Lower SurfaceP/N: 65B02070-76A Dent

L = 8.500"A = 5.000"Y = 0 157" N/A


15893.47 FH

2193 FC SRP 313176 OpenFlap installed on OO-THC; Repair File Item

THC; D&B File Item No. 12

Dent is structurally acceptable for 10 days of

continue service before final repair with DVI inspection

DMI:D05455 for DVI

andQ-Task:P/N: 65B02070 76A

S/N: 000701Y = 0.157A/Y = 32

Request ID 11780079815

2193 FC13/01/2011

14RH Wing

T B d F i i P l H l ( 2) ø1 = 0.394" N/ATemporary repaired i SRM 3 00 0

16035 FH2213 FC SRP 313 08 O

No. 23

Final repair at next A-check DMI: Covered per Repair

repair, with DVI inspection every 2 days of operations for any further degradation

Q Task:Q-2010-74-0029 for final

repair

14 To Body Fairing Panel 194CR

Holes (x2) ø1 0.394ø2 = 0.787" N/A iaw SRM 53-00-70

Fig 2012213 FC

26/01/2011SRP 313508 Open

Final repair at next A check input

DMI:D05480


Fan Blade replaced during KLM visit ref

15

Engine #2 Fan Blade Position 1P/N: 1338M51P05S/N: MFR61818

Dent Chord = 0.236"L = 0.394" N/A

Allowable per AMM 72-31-02/601FF

Rev 70

16170 FH2231 FC

08/02/2011SRP 313284 Closed--

during KLM visit ref 044870 dated

20/02/2011New part installed:P/N: 1338M51P05S/N: MFR33070


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


16

RH Inboard Aft Flap at WBL 382.5 and 426

on lower side flap skinP/N: 65B02070-76A

Dents (x2)

At WBL 382.5:A = 0.709"Y = 0.008"A/Y = 90

At WBL 426:A 1 3 8"

N/A

Allowable per SRM 57-53-01 Allowable Damage General Figure 101 Page 102 Fl C

16287 FH2245 FC

20/02/2011

KLM NRC 12-M5003

visit ref 0448 0

OpenInspection at every A-check and final repair at next C-

check

Q-Task:Q-2011-74-0004

Covered per Repair File Item No. 47P/N: 65B02070 76A

S/N: 000707 A = 1.378"Y = 0.020"A/Y = 70

102 Flagnote C Detail 4

20/02/2011 044870

17Behind LH Side of

Nose Radome at 10 Scratches (x3)L1 = 2.500"L2 = 4.500" N/A

Allowable per SRM 52-00-01 Allowable Damage 1 Figure

16357.72 FH

2255 FC SRP 308234 Closed

check

- -Scratches only affect

paint, no skin o'clock position

( )L3 = 6.000"

g g101 iaw SRM 52-30-

01

2255 FC01/03/2011

18

LH Side Nose Radome just below forward side of 10 Paint Peeling 1.000" x 0.500" N/A Allowable per AMM

16357.72 FH SRP 308234 Closed- - Covered per Repair

p ,damage depth

18 forward side of 10 o'clock lightning strike

strip

Paint Peeling 0.500" x 0.500" N/A 53-52-01 Page 701 2255 FC01/03/2011

SRP 308234 Closed

19

RH Fuselage Outer Skin Dent

A = 0,590"Y 0 0118" N/A

Allowable per SRM 53-00-01 Allowable Damage 1 Table 1

17524.29 FH SRP 308364 Closed

- - File Item No. 119

19 STA 460STR 36

Dent Y = 0,0118"A/Y = 50

N/A Damage 1 Table 1 Detail 3 iaw SRM

53-10-01

2426 FC06/06/2011

Item 08 Closed- - -


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


20 Bulk Cargo Door Sill Scuff Plate Dent

A = 1,770"Y = 0,059"A/Y = 30

N/A

Allowable per SRM 53-60-15 Allowable Damage 1 Detail 6 page 109/111 and Detail 11 page 113

17524.29 FH

2426 FC06/06/2011

SRP 308365 Item 09 Closed- - -

Detail 11 page 113

21

Fuselage Skin Lower Forward Side Forward

Cargo Door SillSTA 580

Scratch

L = 1,900"W = 0,600"D = 0,000"(No depth)

N/A

Allowable per SRM 53-00-01 Allowable Damage 1 Table 1

Detail 2

17685.34 FH

2445 FC19/06/2011

SRP 308563 Item 02 Closed- -

No structure damage found, no visible

metal deformation, only paint damage

22

RH Outboard Aft Flap between WBL 822.00 and 770.00 on upper

f Dents (x3)

Dent 1 = 0.787" x 1.181" x

0.004"Dent 2 =

0.787" x 0.984" x N/A


2038643278 and RDR iaw SRM 57-53 01 All bl

17966 FH2475 FC

KLM NRC 12-S5001

i i f OpenInspection at every A-check and final repair at next C- Q-Task:

Q 2011 74 0012Covered per Repair

Fil It N 4822 surfaceP/N: 65B01970-210A

S/N: 690

Dents (x3) 0.787 x 0.984 x 0.004"

Dent 3 = 0.787" x 0.787" x

0.004"

N/A 53-01 Allowable Damage General Figure 101 Page 102 Flagnote C

Detail 11

2475 FC14/07/2011 visit ref

045332

Open

Dent 1 = Allowable per Boeing Service

and final repair at next Ccheck Q-2011-74-0012 File Item No. 48

23

LH Outboard Aft Flap between WBL 822.00 and 770.00 on upper

surfaceP/N: 65B01970-209A

S/N: 689

Dents (x3)

1.575" x 1.969" x 0.004"

Dent 2 = 0.787" x 0.787" x

0.008"Dent 3 =

0.787" x 0.787" x 0 004"

N/A

Boeing Service Request ID 1-

2038643278 and RDR iaw SRM 57-53-01 Allowable Damage General Figure 101 Page 102 Flagnote C

17966 FH2475 FC

14/07/2011

KLM NRC 11-S5001

visit ref 045332

OpenInspection at every A-check and final repair at next C-

check

Q-Task:Q-2011-74-0013


0.004 Detail 11


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


24

RH Fuselage Skin STA 1810 beside the FWD Edge of the Aft Cargo Door at Lower

Section

Scratch L = 0.500"D = 0.000" N/A


101 Table 1 Detail 1 iaw SRM 53 60 01

18318.86 FH

2538 FC09/08/2011

SRP 312941 Item 02 Closed- -

Damage not deep enough for

measurementSection iaw SRM 53-60-01

25

Engine #4 Primary Exhaust

Outer Sleeve Skin at 7 Dent ø = 0.256"D = 0 035" N/A

Allowable per SRM 54-41-30 Allowable Damage 1 Figure 101 Detail 2 Page

19266 FH2647 FC SRP 316085

Item 1 Closed- -

Primary Exhaust replaced, ref SRP

316993 Item 02 dated 14/11/2011Outer Sleeve Skin at 7

o'clock positionD 0.035 101 Detail 2 Page

103 and 104 FlagNote N

19/10/2011 Item 1

RH Wing Leading No dimensions Allowable per SRM KLM NRC

New part installed:P/N: 015U1547-432

S/N: 0989A

Performed penetrant inspection iaw SOPM

26Edge Variable

Camber Flap Number 22 at Folding Nose Skin Inboard Side

Dent

No dimensions available, KLM

stated dent within limits

N/A


101 Table 1 Detail 3

18897 FH2605 FC

21/09/2011

KLM NRC 12-S5001

visit ref 045585

Closed

inspection iaw SOPM 20-20-02 and no cracks found, ref

KLM NRC 12-S5002 visit ref 045585

- -

27

LH Horizontal Stabilizer on Leading Edge Skin at STAB

STA 425

Dent

L = 2.047"W = 1.260" (A)D = 0.039" (Y)

A/Y = 32

N/A



19809 FH2708 FC

02/12/2011

KLM NRC 08CS5001

visit ref 045787

Closed-

Reassessed during D-check.

No structure damage found, no visible

metal deformation.

-


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


28RH Wing

Gear Inner Cylinder at the Chrome Layer

Scratch

L = 7,677"D = 0.014"

Distance from the N/A


2099176546 and

20247 FH2764 FC

19/01/2012

KLM NRC 10WM5006

visit ref Open

Perform repeat inspection of the scratch for additional damage every C-check until

h h l f h

AMP Task Reference:32-000-RPR-01

Not recorded in the D&B Chart Drawing

-RH Inner Cylinder

replaced during KLMthe Chrome Layer yoke is 8.660" RDR iaw AMM 32-00-03

19/01/2012 046100

29 Fuselage Skin RH ScratchL = 1,654"W = 0 591" N/A


21030,19 FH

KLM NRC 40-S5001 Closed- - -

the overhaul of the gear replaced during KLM visit ref 047191 dated

07/02/2013

29 side STA 550 STR 34 Scratch W = 0,591D = 0,004"

N/A 101 Table 1 Detail 5 and 11 iaw SRM 53-

20-01

2863 FC24/04/2012

visit ref 046345

Closed

RH Horizontal Hole Allowable per SRM 55-10-30 Allowable 21623.85

FH SRP 348774 Covered per Repair30 Stabilizer Tip Aft

Fairing

-Lightning

Strike

D = 0,25" N/A Damage 1 Figure 101 Page 102

Flagnotes D and H

FH2939 FC

30/06/2012

SRP 348774 Item 04 Closed

LH F l SkiBurned Spots

( 15)Allowable per

B i S i 21623.85

Covered per Repair File Items No. 82

Final repair at next A-check, t t d 150 fli ht C d R i

- -

31LH Fuselage Skin

between STA 464 and STA 920

(x15)-

Lightning Strike

No dimensions available Minor

Boeing Service Request ID 1-

2262728497 and RDR

21623.85 FH

2939 FC30/06/2012

SRP 348774 Item 03 Open

not to exceed 150 flight cycles, with detailed visual inspection every 50 flight

cycles

Q-Task:Q-2012-74-0006

Covered per Repair File Items No. 59

until 72


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


32

LH Horizontal Stabilizer on Leading Edge Skin at STAB

STA 400

Dent

L = 2,000"W = 1,000" (A)D = 0,006" (Y)

A/Y = 167

N/A



21549 FH2928 FC

23/06/2012

KLM NRC 08-S5001

visit ref 046472

Closed- -

Reassessed during D-check.

No structure damage found, no visible STA 400 A/Y = 167 101 Table 1 Detail 5 046472

33RH Wing

Kreuger Flap Panel DentL = 2,559"W = 2,559" N/A


26097 FH3506 FC

KLM NRC 12-S5001

visit ref ClosedCovered per Repair

File Item No 87- Q-2014-74-0004

metal deformation.

#15 D = 0,035" 101 Detail 3 iaw SRM 57-43-02

19/09/2013 visit ref 047584

34

Engine #3 SN 706791

Fan Blade Position 2 DistorsionW = 0,590"D = 0,039" N/A

Allowable per AMM 72-31-02/603

26097 FH3506 FC

KLM NRC 93-M5001

visit ref Closed

File Item No. 87

- Covered per Fan Blade File Item 1-

P/N: 1338M51P05S/N: MFR60089

Area C §2.D.(o).2 19/09/2013 visit ref 047584

35Engine #3

RH reverser sleeve RH side at 5 o'clock

Lightning strike L=1,377"D=0,275" N/A

Reworked per MRAS CMM 78-32-32 §P p508 fig 504

26637 FH3572 FC

13/11/2013

KLM NRC 93-S5001

visit ref Closed- -

Blade File Item 1

-RH side at 5 o'clock 32 §P p508 fig 504 13/11/2013 047625


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


36LH Fuselage skin

STA 500-510 Str L27A- 2x Dents

Dent dimension 1A=2,5"

Y=0,025"A/Y=100

N/A


28014 FH3747 FC

TAECO NRC

UDL7829visit Closed -- -

L29 Dent Dimension 2A=2,7"

Y=0,023"A/Y=117

101 Table 1 Detail 3 iaw SRM 53-10-01

06/05/2014 visit 2013030000

3

L= 0 80" Allowable per SRMTAECO

NRC

37Engine #3

Exhaust sleeve Outer Skin at 7 O'Clock

2x Dents

L 0,80W= 0,30" (A)D= 0,017" (Y)

A/Y = 17,6

N/A

Allowable per SRM 54-45-30 ADL 1 Detail 7 Fig, 101

Flag note N

28014 FH3747 FC

06/05/2014

NRCUDL9130

visit 2013030000

3

Closed

5 o'clock Pos:

-- -

38

Engine #3Exhaust sleeve Outer Skin L/E at 5 O'Clock

and 7 O'Clock Position

2x Chafing

L= 0,71"W= 0,67"D= 0,010"

7 o'clock Pos:L= 0,63"W= 0,55"D= 0 015"

N/A


2793978747 and RDR

28014 FH3747 FC

06/05/2014

TAECO NRC

UDL8835visit

20130300003

OpenQ747000051

Perform Detail visual inspection to the damaged

area's every C-check, which is 10 000 FH or 24 months

-

D 0,015

39Engine #2

Exhaust sleeve Outer Skin at 6 O'Clock

2x Dents

L= 0,410"W= 0,320" (A)D= 0,020" (Y)

A/Y = 16

N/A

Dents within limits iaw SRM 54-45-30 ADL 1 Detail 7 Fig,

101 Flag note N

28014 FH3747 FC

06/05/2014

TAECO NRC

UDL9577visit

20130300003

Closed-- -

3


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


40Engine #1

LH & RH core cowl E ternal S rface

Scratch D = 0,002" N/A

Allowable per SRM 54-45-01 Allowable

Damage 1 Table

28014 FH3747 FC

06/05/2014

Taeco NRC UDL0709 Closed- -

Removed material Original Thicness

=0.044" Remain ThicnessExternal Surface g

101 Detail 2 Fig 101 06/05/2014

LH F l Ski

Allowable per SRM 53-00-01 Allowable D 1 T bl 1 28014 FH T NRC

Remain Thicness =0.042"

41 LH Fuselage Skin at MED 5L cutout mid Scratch D= 0,005" N/A Damage 1 Table 1

Detail 2 iaw SRM 53-60-01 ALD Fig

101

3747 FC06/05/2014

Taeco NRC UDL6763 Closed

Allowable per SRM 53 00 01 allowable

- - 0.005" removed.

42RH Fuselage SkinSTA 540-560 STR

44L Nick D= 0,008" N/A

53-00-01 allowable damage 1 Fig 101 table 1 detail 2 iaw SRM 53-20-01 Fig

101

28014 FH3747 FC

06/05/2014

Taeco NRC UDL8488 Closed- -

Removed materialO/T =0.090" R/T=0.082"

Removed material

43LH Upper Wing to

Body Fairing Panel 291GL

2x scratches D1= 0,005"D2= 0,007" N/A

Allowable per SRM 53-00-70 allowable damage 1 Fig 101 Detail 8 iaw SRM 53-20-70 Fig 101

28014 FH3747 FC

06/05/2014

Taeco NRC UDL8504 Open

Inspection every A-check and final repair at next C-

check

Q-Task:Q747000067

Removed material FWD area

O/T=0.165" R/T=0.160"

AFT area O/T=0.165" R/T=0.158"


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


44 Engine #4Fan Blade Position 16 Distorsion

L = 1,200"W = 0,375"D = 0,039"

Area D

N/AAllowable per AMM

72-31-02/603 §2.D.(o).1

29058 FH3865 FC

23/07/2014

KLM NRC 94-S5001

visit ref 047880

Closed- - Covered per Fan Blade File Item 3

Area D 047880

45 RH Wing to Body Fairing Panel 194DR Hole Ø= 0,25" N/A

Allowable per SRM 53-00-70 allowable damage 1 Fig 101 Table 1 note C iaw

30527 FH4028 FC SRP 355542

Item 2 OpenInspection every A-check and final repair at next C- Q-Task:

Q747000072 -Fairing Panel 194DR Table 1 note C iaw

SRM 53-60-70 Fig 101

05/12/2014 Item 2

46Engine #3

I l C l A i DØ = 0.98" (A)D 0 01 " (Y) N/A

Allowable per SRM 54-15-01 allowable 30792 FH

40 6 FC

KLM NRC 93-M5002 Cl d

Inspection every A-check d fi l i t t C Q-Task: Covered per Repair

check Q747000072

46 Inlet Cowl Accoustic panel at 6 o'clock

Dents D = 0.017" (Y)A/Y = 57,6

N/A 54 15 01 allowable damage 1 Table

104 note 5 Detail 5

4056 FC07/01/2015

93 M5002 visit ref 047986

Closed

LH Horizontal St bili L di L = 2.000" Allowable per SRM 30792 FH KLM NRC

and final repair at next C-check

Q Task:Q747000078


47Stabilizer on Leading Edge Skin at STAB

STA 156,28Panel 331AL

Dent W = 2.500" (A)D = 0.080" (Y)A/Y = 31,25

N/A

p55-10-01 Allowable Damage 1 Figure


30792 FH4056 FC

07/01/2015

08CS5001 visit ref 047986

Closed- - -


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


48Engine #3

Fan Cowl Leading Erosion

ENG #3L = 76.000" N/A


Damage 1 §3.D 30792 FH4056 FC

KLM NRC 93-M5001 ClosedFinal repair at next A-check Q-Task:

Fan Cowl replaced during KLM visit ref

048063 dated 01-04-201548 Fan Cowl Leading

edgeErosion W = 0,050"

D= 3,663"

N/A Table 1 and EDF KLM-CC2-2015-

001R0

4056 FC07/01/2015 visit ref

047986

Closed

Allowable per SRM Fan Cowl replaced d i KLM i it f

Final repair at next A check Q747000076 2015New Fan Cowl:

P/N : 224-2202-507S/N: 0688

49Engine #4

Fan Cowl Leading edge

Erosion

ENG #4L = 61.000"W = 0,064"D= 3,710"

N/A

p54-25-01 Allowable

Damage 1 §3.D Table 1 and EDF KLM-CC2-2015-

001R0

30792 FH4056 FC

07/01/2015

KLM NRC 94-M5001

visit ref 047986

Closed

Allowable per SRM Fan Cowl replaced

Final repair at next A-check Q-Task:Q747000077

during KLM visit ref 048063 dated 01-04-

2015New Fan Cowl:

P/N : 224-2281-501S/N: 3476001

50Engine #1

OUTBD Fan Cowl FWD Leading edge

Edge protector missing L = 53.000" N/A


Damage 1 and temporary repair

approved per EDF KLM-CC2-2015-

006R0

30228 FH3998 FC

11/11/2014

SRP 355724 ClosedFinal repair at next A-check Q-Task:Q747000075

Fan Cowl replaced during KLM visit ref

048063 dated 01-04-2015

New Fan Cowl:P/N : 224-2280-501

S/N: 4831001

51 Engine #4Fan Blade Position 17 Distorsion

L = 2,244"D = 0,098"

Area DN/A

Allowable per AMM 72-31-02/603

§2.D.(o).1

31703 FH4153 FC

01/04/2015

KLM NRC 94-S5001

visit ref 048063

Closed- - Covered per Fan Blade File Item 4


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


52Engine #1

INBD Core COWL Door

Scratch D = 0,002" N/A


Damage 1 Table 101 Detail 2 Fig 101

32629 FH4264 FC

10/06/2015

KLM NRC 91-S5001

visit ref 048108

Closed- - -

101 Detail 2 Fig 101 048108

53 Engine #1Fan Blade Position 3 sharp

L = 0,173"D = 0,019" N/A Allowable per AMM

72-31-02/ §D (1) (e)

32629 FH4264 FC

KLM NRC 942-M5002

visit ref Closed- Covered per Fan Blade File Item 5-

Fan Blade Position 3 Area C 72 31 02/ §D.(1).(e) 10/06/2015 visit ref 048108

Blade File Item 5


18-Jun-08



TNT Airways S.A.

TEC/05-003.3

REVISION 2


Reported

16/11/2015

p


54

55

656

57


TNT Airways S.A. 18-Jun-08

DENT AND BUCKLE CHART DRAWINGTEC/05-003.3

REVISION 2

**R t ll di i i i h **

Registration: OO-THA Total Time: 34473,00Aircraft MSN: 35232 Total Cycles: 4507Aircraft Type: B747-4HAF Date: Balthazar Bonnefoy16/11/2015


17

LH SIDE1 1036 4342

TNT Airways S.A. Revision 34 of 23



REVISION 2




LH SIDE

5 41




REVISION 2




21

RH SIDE

19 823429




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RH SIDE 20 24




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26

30 45

47




REVISION 2




53

40

39




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REVISION 2




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34

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tec/05-003.3 dent and buckle chart index … · tec/05-003.3 18-jun-08 dent and buckle chart index...

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