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rs· J, /9

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. ,~l'\.L '-" ')b(k Rll Required?

,( .D Write Yes or No:

Continuation Sheet (;lc;i),-J ~

Numbers: "l:9fe7 t,/S""q(/)7-

Rectification:

t2-if,"J,.;.,J ,;- 1 A V ,.,/ M, L_ · .) l".S.S ~ :(.J~ }I.. ' • n oi _,.. J/)', ,,,, );rn i·k T :.A .... J - .J ,./ ,;~ .::'IS, t..__ • hr,. ,),. , .- R 1) j:F ~ ·· .5 3 -~ 3 '> <.,., , i .. . I C~nf ; / • ,-i_ j,.J ' ll lt,Av..i:.;.:..c; ?a.J<I ,.ss~ '7 rt.,~b

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1

)ehh 11olrcl ... j -Iii..!. -J;,,,,~ . I .!W l<i,-~

¢>!5 hi/ Zo l c;- -Approved D.it.1 or Manual Reference: 6,..,:i.,.J,,,~ ~o ~ , -.s 1-f:,J Se,/,'., h ! ' S~1{I : / ~-W : lt W<JI'( Zc, /4< ;.,

l :,'x..)(l, '7

Calihralcd ID Number ID !\'umber !DNwnbcr Tools Tool Description: AV WH Tool De~criplio71: Tool Description: Used: j ol';,.1;, 1k"'\~ Cal Due: s/~ Cal Due: Cal Due:

Qty Description Pos P/N Off: PIN On: SIN Off SIN On Batch No.

I I /,_,. - .S~Jt.~ - - I~ ·-

I Pr; ---- - - CIMD '-/(r7q7 ~ 1-z.~,.,,r - - -

Pans Contimutinn I Sheets I I I I Ops Check rr.m,forrcd Leak Check Transferred Puncl Clo:.ur~ Transferred SOR Required To \Vork Card Nu. ru Work C.ml No. To Work Curd No.

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:Date: I<( /1'1 IJ!/ I ) . ,t Date: 1Datc. ,..,, - • _...., - S , </.b7.1./2dr:

'ORM 409 US {EV. I

COPY {\\'HITE). CUSTOMER COPY (BUH) · CO:-i l KOLLED

YesD

AVMAX

Additional Work:

RecrificaLion:

Additional Work:

Tool Description:

roR~l 403

Re,·isNJn I: 10 Jan 07

CONTINUATION SHEET 615902

Ajrcraft SIN Work Order Work Card

C upy I (White) to Customer

JS"

Date:

/(M,4-{t~

l.D. No.

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Copy 2 \Yellow) Controlled

RH Block

Planned By:· P, t...0 J..rs-K'1

RII Block

Planned By: D

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CUSTOMER: AVMAX

DA TE: OM2/201S

AIRCRAFr INFORMATION:

AIRCRAFT lYPE: DuhS-300

FAA CRU ~853X AEROWELD, INC.

NDTREPORT

AIRCRAFT REGISTRATION NUMBER: N387CA

SERIAL NUMBER: 954

NDT EQUIPMENT USED:

P.O. No. 126856

W.0; No. AIS-305

PENETRANT O MAGND'IC PARTICLE O EDDY CURRENT 181 ULTRASONIC O RADIOGRAPH 0

TIDRMOGRAPB D OTHER D ----------------INSTRUMENT: Olympa Nortec 500D

INSTRUMENT SDllAL NUMBI.R: N500Xl718R010717

NEXT CAL DUE: 88l0&'15

DESCRIPTION OF WORK PERFORMED:

Performed IIFEC oa puaes oa puaen1~ aeat raB IA W Bombardier RD 8-~3-833 1beet 1 section!.

No c~du Jncllcatecl :at ~ U.e. Work Card: 2171 /

NAME: Chril Mana SIGNA TIJRE:

NDT Level. II

AERIOWILD,INC -433 BREESPORT ISAN ANTONIO, TEXAS 7821e I PHONE 210-690-7888 I FAX: 210-3e6-2618

Fo,m AW-1 (&'12)

BOMBARDIER 1 TITLE

REP

., .1.n ~,. ~Yo.I· Care; A1,:~1c~t-'.l Dat.i lr,r ~c7~.:-:-..,.,..._.--=~J IN/0

GENERIC PERMANENT REPAIR FOR CORROSION DAMAGE TO INBOARD SEAT RAILS, PIN 85322516 AND PIN 85331409.

2 RD NUMBER

8-53-833

3 SECTION 4 SHEET

5 PRIME DESIGN ACT(VITY 6 ADDITIONAL LIMITATIONS

BOMBARDIER INC., DOWNSVIEW 71867

NONE

9 DESCRIPTION

7 SERIES

DIIC-8 SERIES MODEL 300 301/311/314/315

1

8 APPLICABILITY

SIN ALL

The following sheets detail Blend Limits for corrosion damage to Inboard Seat Rails,

PIN 85322516 and P/N 85331409.

The procedure involves blending out all corrosion, within limits provided, then re­

protecting the affected areas.

The details of this procedure are covered by RDB-53-833 section 1.

Sheet 1 Sheet 1A Sheet 1B Sheet 2 Sheet 3

Issue 7 ISSl,IQ 3 Issue 2 Issue 6 Issue 4

At RD Issue 7: • RD redrawn to convert to

electronic format.

1

• Note 1 added from sheet 1A Issue 2 on sheet 2.

• Sheet 1 is now at Issue 7. • Sheet 1A is cancelled at Issue 3.

Approx. repair location • Sheet 1 B is cancelled at Issue Z. • Sheet Z is now at Issue 6.

• Sheet 3 is now at Issue 4.

At Issue 7 RD re-drawn to convert to electronic format. No change to repair intent or methodology.

10 ISSUE 7

11 DATE 17 May 2014

12 PREPARED BY PRAJWALB.

13 STRESS

16 DESIGN AUTHORITY

14

15

17 DAO ALJTHORITY

18 fvl THE TECHNICAi. CONTEl'fT OF IS DOCUMENT IS APPROVED UNDER THE ~ DESIGN AUTHORITY OF lRANSPORT CANADA DESIGN APPROVAL

OF.GANl3ATION DAO NO. 9:Kl-02

D BA ENGINEERING DISPOSITION FOR APPROVAL BY OPERATOR'S LOCP.!.. .A.!RWO~TH!NESS AUTHO~l:Y

T:·1\9 REPAIR DRAWIN'.i HAS &E!.M PREPARED ON TI« BASIS 0, Nfl~TION SUPPLIED 10 BO .... >-RO',ER INC. BY TliE OP!:AATOR OR HIS AGENT. IT IS THE RESPONS181lrrY Of Yl1f OPERA TOR OR HIS ACEHT TO 1/ERIFY 1'HA T lHE "Fa-TION SUPPllfO IS COIM'l.£TE ANO ACCURATE. Ba.eAAOE/1 IMC. OOES NOT AC= AE.SP0NSIBlllTY FOR 1'HY CCNSEOLENCE RESUlTt<G FROM ..cow>.E'l'E ()R INACCURATE REPOR'TING OF n<E

CAW.AGE I OtSCRD'.ANCY .

BT0214-11 MW REV 2006-08

THE LNFOfUMTlON, TECHNICAL CATA AND DESIGNS OISCLOSEO HEREIM AAE THE. EXq_USIVE PROPERTY Of' BOM8ARDIEflt INC OR CONr AIH PROPfUET ARY RlCHTS OF OTHERS M'O ARE NO I TO BE USED 0A DtSCt..OSEO TO OTHERS Wm-K)VT THE W RITif.H CONSENT OF BOMISAROIE.A INC. THE REClPIEMT Of/I rn,s OOCU1,£HT 8Y ITS Rl!TeNllON AAO use AGREES 10 HOUl IN CONfll'lf.NCI! THE TECHNICAL DATA N<J oes1GNS CCNTA»ff!o Hl!RL'N. THE FOREGOtNG $NAU NOT Ji,,S>P\. v TO PERSONS HA\llNG PROPRlflARY' RIGHTS TO SUCH INFORMATION T'fCH.CAL DATA OR SUD< DES.ONS TO THE 00£"1' n<AT SUOi RIGKTS EXJST. ' O.:l.'.m.27 REV 19W-01

© Bombardier Inc.

).J 7 /

I I

1·

BOMBARDIER REPAIR DRAWING (RD)

t--10_1s_su_E-+ __ 4_----1------1--------J1----_J 2 RD NUMBER

8-53-833

3 SECTION 4 SHEET

1 3

GENERAL NOTES 1. Blend and polish out all damage as shown below. Do not increase depth of material

removed. Surface finish to be 125 RMS or better. Maximum depth of material removed, x = As noted on sheet 2. Minimum thickness of material remaining = As noted on sheet 2.

increase depth of material removed. x = depth of blend out Blend out all damage as shown. Do not~

,c -------- ---- ------ - -= .~t I I

20x Min. / 50x Max.

2. Crack detect using preferred Eddy Current method, per PSM 1-83-7 A, Section 51-00-06 or fluorescent dye penetrant method. No cracks permitted.

3. All bare metal to be finished with Alodine, Epoxy Primer, and Polyurethane Enamel. Except, in Slot as noted on sheet 2.

i. Alodine per Structural Repair Manual, PSM 1-83-3, Chapter 51-20-16.

ii. Epoxy prime per Structural Repair Manual, PSM 1-83-3, Chapter 51-20-36.

iii. Apply Polyurethane Enamel per Structural Repair Manual, PSM 1-83-3, Chapter 51-20-51.

4. On completion of repair apply thin coat of Corrosion inhibiting Compound· LPS-3, Dinitrol AV58-2 or equivalent - per Maintenance Manual, PSM 1-83-2, Chapter 20-16-01, over affected areas of the repair.

BT0214-13 MW REV 2006-08

.BOMBARDIER REPAIR DRAWING (RD)

r-10_1_ss_u_E-t-__ 6_-+-----l----+--------l 2 RD NUMBER

8-53-833

3 SECTION 4 SHEET

0.020" Max. Except for details

7 in note 1.

t

0.060" Min. remaining, 0.020" Max. blend depth typical.

1

liAlodine only all surfaces in slot .

fil0.460" Max.

0.020" Max.~ {Typ.) \ ,----0.020" Max.

~~"~ i

-0.440" Min. remaining.

I

TYPICAL SEAT RAIL SECTION

1

I .__ 0.180" Min .

remaining.

P/N 85322516 (X197-X424) AND P/N 85331409 (X424-X588).

2

0 Note 1: Maximum depth of blend out on top surface increased to 0.020" was 0.010", between X197.0 and X588.0. Except, a maximum blend out of 0.010" only is permitted in any aircraft that are presently configured, or might in the future be configured, to install a five-abreast seat.

0 At Issue 6 of sheet 2: Added Note 1 from sheet 1A, Issue 2 (sheet 1 A is now deleted at Issue 3) .

BT0214·13 MW REV 2006--08

1 •

I