11~ VIPRD' - ~ · - ..--- / ,l -- .. AVMAX NON-RO · CONTINUATION SHEET 6155 24 AVMAX A ircraft S...
Transcript of 11~ VIPRD' - ~ · - ..--- / ,l -- .. AVMAX NON-RO · CONTINUATION SHEET 6155 24 AVMAX A ircraft S...
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AVMAX 11~ VIPRD"' · - q,., NON-ROUTINE WORK CARD -~ ~ Date: Serial Nu. S.O.W. Code Trade - A1A WorK urdcr # \V9o5o 7.oftf i,) s 55L/ tJ~~ S/m SL( 8bZSS" Reference Ta.<k/Wnrk Ca7 . E~timatcd Hrs & Customer Approval Budg~i HN & Cm,loincr App:-ov:tl
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Parts Requisition
111f<-tb.5 C} JJ-IY I I I I Numbers:
Recommended Action: tvc4'. Planned Bv:J I ~ t-1,lll~e~ S'(,'=,t
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Calibrad ID Number Tools Tool Oescriprion: Too\ Description: Used:
Col l>ue:
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r Date:
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CONTINUATION SHEET 6155 24
AVMAX Aircraft SIN Work Order Work Card
I f s '--( '-I ~02. g_s L/OS~ Page of
Additional Work: Retv /VD T \Planned By: _:! :!..L_ S ?-? J
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Tool Description: T.D. No. Rll Block Cal. Due:
Mee~~ Date:
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Additional Work: 7 ()elV"f/ Ft l',,f. J9·TeA.1~ --(. Planned By: ~ S7? /
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Tool Description: l.D. No. R.11 Block Cal. Due:
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11;1 I 11 1.' • 1,1 , •11 I ti + J,11: I ';
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PREPARED 8.8.
CHECKED
DATE Jan-98
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RDS-54-874 SECT
PAGE I
ISSUE ,r2..
The follov.-ing RD provides a permanent repair f, r nacelle lower side panel skin cracking (p/n 85410627 and 85410628) at Xn 131.50 for both fNBD and OUTBD sides of# I and # 2 nacelles.
This repair permits cutting out maximum 2 .0" of panel material at the forward upper comers of the landtng gear door opening, remaining skin and structure are inspected for cracks before an external repair doubler is installed.
This repair is applicable to both# l and # Z nacelles (INBD and OUTBD lower skin panels.}.simultaneously
The details of this procedure are covered by RD8-54-87 4 section 1. page I issue ,r' 2-page 2 issue l page 3 issue .(2.-page 4 issue I page 5 issue 1
RD ISSUE 1.. Title: Permanent repair for crack /"J----- - -,--- - ---+...----------- -4 ::~, L'ATE . I 7-Jan-98 D\- i\1>..~-"{\ damage at fwd upper corners .j)11-------+------+..:,...;..__.;...__,_-+--·---~ I-' DRAWN
of MLG door opening on both 7 1-------,-,,..,..,..-=-# ·- ++-+-------1----- ---.I ~; APPROVED # I and # 2 nacelle (Xn 131.50)
:;; ..... _____ -~J.,J-,~~!!.,,.-,1..-!!!~:..t;k~l,C,,,.,J...--.,{_ ... STRESS
D. _,.
A.
R.
REPORT NUMBER
RDS-54-874
APPLICABlLITY
DHC-8
Series 100 Models IU2/103/106
Series 200 Models 201 /202
Series 300 Models 30 l/3 l l/3 14/3 l 5
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.06.:l" lhk repair doubler (2024-:TI clad mat'I) Exlernal corners lo he .25" radius min. Form 10 conlour of nacelle.
'·-.;, - -
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Install 1-<>ff repair packer .032" thk 2024-T] ,clad material in area shown by: j l
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f-..1.l t. ·-J!'. •·· 1c(",·,.: ~
Trim out d11magcd section of lt541062S skin as shown. Use MIN .40" radius on all corners. See General Notes for detailed repair i11s1mc1ions. DO NOT CUT OR DAMAGE INTERNAL DOUBLER 85410625
UP
Lr-uo
THIS REPAIR IS CONSIDERED NULL AND VOID IF ANY INTERNAL STRUCTURE IS DAMAGED.
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--~- , , · _ii E:-.!crnal corners 10 b.! .23" rn<lius min. form
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- ,=-- -__,,.,,J I , 'I I -:1- . I J11s1all I-off repair packer .04 0" 1!!!<_702-1- . · ~.,. > ~ f' .,f- 1J -K l.?f clad11m1crial i11arc:ishownby:r:_.;:r_d.;1n ·o:g.3
\\ -~--1 ;-f---,f, r~-- 7 ;:: !i 1--6-. _ ,I ,_, ,,, -- lll',1a! i 1-o!T rcp;iir packer ,071" as req'd from ;;;- o
2IJ2-l-T.1 clad 111at'l in area <lcno1ct1 by: c .: ~ ~ ~ a l 1 I
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PREPARED 8.8.
CHECKED
DATE Jan-98
General notes:
RDS-54-874
SECT 1
PAGE -'
ISSUE
This repair may be carried out on either# 1 or# 2 nacelles (or both) on either the INBD or OUTBD side skin panels (or both) simultaneously
l . Cut out skin damage as shown on pages 2 and 3. Ensure all corner radii are min .40" Do not damage underlying doublers as specified on previous pages outside of cut-out area. Do not damage underlying door edge members.
Ensure all crack damage is removed by damage cut-out. TIDS REP AIR IS CONSIDERED NULL A.-i-m VOID IF ANY UNDERLYING STRUCTURE SUCH AS DOOR EDGE MEMBER IS DM1AGED
fl\ P n - -2 s - t 5 All cut edges are to be smooth and free of nicks. Bare edges are to be touched up with alodine and epoxy primer. After cutting away the skin ensure remairjng structure is free of any damage. Crack inspect the rernaining skin usir.g fluorescent penetrant dye or eddy current(preferred method) to ensure the remaining skin is completely free of cracks.
( __
2. Fab ric~te repair packers and external doublers from 2024-T3 clad material (QQ-A-250/5) All new parts are to be finished with alodine and epoxy primer. Enst.:re a minimum comer radius o( .25" Maintain min .050" gap
-;. 'be.t\vec:; p .ckers and cut-out edges. \
Alotiine ir, accordance with the instructions of the DASH 8 structural i@ 7 /t/1/1 (S' Av[)MAX J '
73
~:J.7',,/iPl~1.54
5 ? ·7 I
ad4~??,S J.J ... r-J./.'Jt.-1.S
repair m2. :· ·.1 :il PSM l-8(2 h· 51-20-1 6.
6\{, D o\~ J)il't L
Eroxy r .,e in accordance with the instructions of the DASH 8 structural r::pair m. ·ual PSM 1-8(2)(3)- ter - 1 -36.
0V.., \c:, (';Me_
Repair e· :;ng fa5tener dimples remaining in the skin underneath the external · air doubler i,, accordance wi th the instructions of the DASH-S ~.tr.;c iur:;;. ::iair manuai ?SM l -S(2)(3 )-3 chapter 51- I 0-2 l page 6.
~ :S") 71 6. Faysea'. a:. ~1ating surfaces with Pro Seal 870( or equivalent sealant in ., ?- /Cf/? ac..:o rdarK wnh DASH-S structural rc:pair manual PSM l-S(2)(3)-3 "" I(~ '5 chapter 5 : ·0-26.
~ S7? I
'A.? ... 141' 1t - 1 5
Fillet se:<i :. ·,:, und ,he edge5 o ft he e:-.:terna.l repair doubler w ith PR14'.?.2-82 or t C],.!i':J.1, -: in accordance wiih the instruct ion:, of che DASH 8 strnctural
. . l:., ,~ ' ' I ~ ( ' 1 )( • ) -. ' · - l ~ 0 .., -. rep::ur mar,,.::1 .)1-, 1 -.., . ·· , .) -J cnapter ) -.) -: . 1!\,\ 1
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PREPARED B.6. RD8-54-~ .
SECT I
PAGE S
ISSUE I
cm:o:i::o
DATE Jan-93-
8. Maintain a minimum of two times the fastener diameter edge distance, unless otherv..i se specified. The edge distance is measured from the center of the fastener hole to the edge of the material and must be maintained on all material through which the fasten~r passes.
9. Functionally test :tv1LG doors to ensi..: re the free operation of the door (ie no hang-up or binding) .
.......
,Rivet codes: 1 ( : I
·.,
Install CR.3214-5 rivets at new locations. (pitch to match adjacent existing fasteners)
Install CR.31 14~5 rivets at cxisti:ig locations. Hole Dia .160"/164", Csk,Dia .242"/.247".
Install N A-S 1097 AD-5 rivets at existing locations. Hole Dia .159".166", Csk Dia .. 23 l "/.236"
{nstall C?(..3214-4 rivets at existing locations. Hole Dia .. 129"/.132" Csk Dia .. 191 "i. I 96"
Refererv.: -= only
PARTS CONTINUATION SHEET 5503
Aircraft Serial No. Work Order No. Work Card No. I/Continuation Sheet . ": " 5.S-c/ I ?rtJ 2 ~ ) 40 5 8' No. I of
PARTS USED Qty Description POS PIN Off P/NOn SIN Off S/NOn Batch No.
I It.. 1T PJ-.,;i,, c- - C 1116 'lf- l'i 2. )(' 171.Y -~ '?/
l1<1T ,or' e_oAT ..__ (l?Osl'7 /')..'-/ 7 6 .f
\ Mt~,;\ - .~C) y7) •. t'i/,,1' ' --- 1)(.,,C,'75
I Me to.I - ;;ioJ 4-r3 - -~ -- ro t; 11 I _,,, c-,1=-~ ,_-c,, ·1
--I
I ··- ~-
··- - ···
·--
·- -
Fom,402 Copy l (White) · Customer Copy 2 (Yellow) - Contro lled
/ ·- -·- - - ·----- --- - ·---·- -
SHIP TO;
KAISER AM CASTLE METALS 4175 ROYAL DRIVE, SUITE 600 ALLIM/NUM KENNESAW, GA 30144
Trentwood Works - Spokane, WA 3 9215 Phone: (800) 367-2586
CERTIFIED TEST REPO SOLo··o ; RT At-.1 CASTLE & CO- SOLD TO
Serial Number 14:20 KENSINGTON RD . 4313444 A\1 mft ,.: V-1~,,:-. SUITE 220
r-.;:pr,· ... :c:~ o .. , Q;l.K BROOK! IL 60523 NC ,t/10---111r:. -
CUSTOM:R PO NUMBER: l WORK PACKAGE: I CUSTOWER PART NUMBER: I SHIP RU tlfLOAO: I GOV'T CONTRACT NJ 23984~ 77DC93 102766/13
MSER:
KAISER C1RDER NO: LINE ITEM:
1
SHIP DATE: rLLOY: 1159084 1 24-0CT-201 3 2024
WEIGHT i;HIPPEO: QUANTITY: I TRUCK B/L #: 6526 LB 2 PCS EST. 2044628
MHU 17254 i 2: LOT 663056AO: 1 pieces; MHU 172 541 3: LOT 663056AO: 1 pieces;
CLAD: I TEMPER:
ALCLAD T3
t RODUCT DESCRIPTION:
HT Coll GAUGE: OIAMET:RfWIOTH: I LENGTH: 0 .0630 IN 48.000 IN 0.000 IN
( 1.6002 W-A) (1219.2MM)
Certified Specifications ocr 2 a ' 201,1
AMS4462 CMMP 019/RevD
TestCode: 1505
AMS-QQ-A-250/5/RevA CMMP 025/RevU
Test Results
lot: 663056.AO Cast 637 Drop 99 Ingot 1
.(~STM EB/B557) (EN 2002-1 J Tens ile: Temper
T3 Dir / # Tests LT / 2 (Min:Maxl
(AS'fM ·E-125-1)---·· - - ·· · ·· - · · Chemistry: SI FE cu Ac:tual(wt%) 0. 10 0 .22 4 .5
SI FE cu 2024 MIN{wt%) 0.00 0.00 3.8 MAX(wto/o) 0.50 . 0;50 4 .9 ·
Liner Alloy : 1230 MIN(wt%) 0.00 0 .00 o.co MAX(w::% ) 0.25 0.30 0.10
MN 0.57
MN
0.30 0.9
0 .00 0.0 5
Ultir:iate KS! (IViPA) 65 .9: 66 .0 (45 4- : 455)
MG CR 1.3 0.01
ALLOY LIMITS
MG CR
1.2 0 .00 1 .B 0 .10
0.00 0 .00 0.05 0.03
Aluminum Remainder
Yield KSI (MPA) 46.4: 46.9 (320: 323)
ZN Tl 0. 12 0.02
zr, Tl
0.00 0 .00 0.25 0 .15
0 .00 o.oc 0 .05 0.03
AST\il 6 209/,C\e\ 1 0
V 0.01
V
0.0 0 0.05
0.00 0 .0 3
Meted in USA
Elongatio;i 3/o 16.4 : 18.:
ZR 0.00 TOT
ZR o rHER
0.00 lACH 0.05 TOT
0 .00 EACH 0.03 TOT
OTHER
0.04
MAX
C.05 0 .15
0.03 ('
~IPTO: <
KAISIEIJ!I FUTURE METALS INC 10401 ST A TE STREET ·ALUMINUM TAMARAC, FL 33321 Trentwood Worlts • Spokane, WA 99215
Phone: (800) 387-2588
SC>LDTO: CERTIFIED TEST REPORT FUTURE METALS INC Serial Number.iw:;,,,, 't,0,1, Caic, PO BOX26450
4256082 /,p;n:-·1ed DJi~· .: r s '--( <( 10401 STATE STREET. A/C ~6 TAMARAC, FL 33321 VJIC
VJ.'(: -----YO
CllSTOMEA PO NUM811!R: !WORK P'ACKAOE: I CUSTOM~ 1'ART NV11181!!1t: I SHIP ltUNLOAD: I OOV'T CONTIIACT NUMSER: 1U1245 102262/5 KAI~ ON>Ult NO: LINe JTeM; l - DAn: I Al.LOY: CLAD: l~R: I ~WWWIION: 1~23398 1 1-MAR-2012 2024 Cl.AD HT Flat Sheet WIEIGHT IHPP'~: QUANTITY:
I BA. NUMBER: QAUO&: I D~= I LBIG'TM: 6H07 LB 292 P~S EST. 2036017 0.0320 IN 48.000 IN 144.000 IN
MHU 1687226: LOT 5780!51A5: 101 pieees; MHU 1567248: LOT 578051Al5: 184 piece LOT 578061A4: 7 pieces;
Certlftec:I Specifications
AMS 4041/RevQ CMMP 019/RevO
TNt c;ocs.: 1505
AMS-OO-A-250/5/RevA CMMP 0215/RevU
T"tReaults
Lot: 678051A5 C.at 584 Drop 63 Ingot 4
(ASTM E8/B557J (EN 2002-1 l Tensile: Temper Cir / ti Tests Ultimate KSI (MPAJ
T3 LT / 2 (Mln:Max) 61.2 : 151 .9 (422: 427)
(ASTM E1251) Chemistry: SI FE cu MN MG CR Actuel 0 .07 o.,a 4.15 0.53 1.4 0.01
Future Metah 111114&1'6
ASTM B 209/Rev10
Mett.d In USA
Yield KSI (MPAI Elongation 'l', 41 .5: 42.3 17.8 : 19.4 (286: 292)
ZN Tl V 0 .09 0 .01 0,01
OlSIOID<rllllJI< AVMAXJACKSONVILLE AddlDO!lal ltlfo Item: 2 CUMmcrP.O. 113977 Qty l SHEET
ZR 0 .00
OTHER TOT 0 .03
Page 1 of 2
Sllil'P"' Number WA55472 Dm 110ct2012
CUSTOMER: AVMAX
,.... DATE: 04/26/2015
AIRCRAFT INFORMATION:
AIRCRAFT TYPE: Dash8-300
~FAA CRS# W2XR853X
~ AEROWELD, INC.
NDTREPORT
AIRCRAFT REGISTRATION NUl\fflER: N387CA
SERIAL NUMBER: 554
NDT EQUIPMENT USED:
--;;J,, P.O. No. 126461
- W.O. No. Al5-273
PENETRANT O MAGNETIC PARTICLE O EDDY CURRENT l:8J ULTRASONIC O RADIOGRAPH 0
THERMOGRAPH O OTHER 0 -----------INSTRUMENT: Olympus Nortec SOOD
INSTRUMENT SERIAL NUMBER: NSOOX1718R010717
NEXT CAL DUE: 08/06/15
DESCRIPTION Ol WORK PERFORMED:
Performed HFEd oi cut-out on #2 nacelle FWD OTBD corner IA W Dash8-300 NDTM part 1 51-00-06 . .,,., - - . .
· ~o cracks indicated.
· -~Work Card: 4058
NAME: Chris Mann SIGNATURE:
NDT Level II
AEROWELO, INC 433 BREESPORT BSAN ANTONIO, TEXAS 78216 Iii PHONE 210-590-7888 tl FAX: 21 0-366-2618
FormAW-1 (6/12)