tinittd,swa of i!.m btpaltllltnt of 1:mlulportation ... · installation of combined exhaust gas and...

15
SA2557NM tinittd,Swa of I!.m Btpaltllltnt of 1:mlUlportation -:fCdcraI ~\liation 5!dministmtion ~upplcmcntGI 1tJ!pC «icrtlfirGtc ~ yL~«44;~-/Q K S AVIONICS INC. 25216 Cypress Avenue Hayward, California 94544 ~a-a/Jk~~./kr~r./k~~~~-:d./k~.-.d~ ~A4-..yu.-#~~,/k~~AY'~4~9.-6 23 ~./k Federal Aviation ~;r,,?6;.>w> ~9~-Y~~,' J/ak, ~" See Attached Master Eligibility List No, 2557 See Attached Master Eligibility List No, 2557 See Attached Master Eligibility List No, 2557 Installation ofK S Avionics EGT/CHT-2() combined eXhaust gas and cylinder head temperature monitoring system in accordance with K S Avionics Inc, Drawing No, A600TD-(**) Rev I, dated October 3, 1994 or later FAA Approved revision, -:£'~.-.d~...d~ " This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effects upon the airworthiness of that airplane, Original cylinder head temperature head equipment, if required by the original type design, must remain installed and operable, See continuation page 3. ,,- Jk~~k.-.dJk"'0/0-1'7~u.-~,h<ch-""./k/"", ••• /~~.,,,,/..k//~;~~#/ .•••. 4/~ ~~~ 4~~~k""'L/kru~.6f/~.;,k/~Y'Jk ..rUm'n,;,""'/',~-/1k June 29, 1984 April 29, 1985 January 12, 1995 .'1IJ#'~Hr/;""1"1£ .rt/Nu;n~hw4,~ ~>~' ]\fa; ger, PropUftJ6'l'!'B'tanch Los Angeles Aircraft Certification Office (TltI~) Any alteration of this certificate is punishable ~JJ a ,fine of not txutding '1.000. or imprisonment not txcetding 3 years, or both. This urlijicau m~, INIraruf"wi in a£cordanctwilh FAR 2/.47. C\ t&~ II Page 1of 3 J)"": ,f I fAAPe- 8110-2 (10-681

Upload: habao

Post on 07-May-2018

216 views

Category:

Documents


1 download

TRANSCRIPT

SA2557NM

tinittd ,Swa of I!.mBtpaltllltnt of 1:mlUlportation -:fCdcraI ~\liation5!dministmtion

~upplcmcntGI 1tJ!pC «icrtlfirGtc~

yL~«44;~-/Q K S AVIONICS INC.25216 Cypress AvenueHayward, California 94544

~a-a/Jk~~./kr~r./k~~~~-:d./k~.-.d~

~A4-..yu.-#~~,/k~~AY'~4~9.-6 23 ~./k Federal Aviation

~;r,,?6;.>w>

~9~-Y~~,'J/ak,~"

See Attached Master Eligibility List No, 2557See Attached Master Eligibility List No, 2557See Attached Master Eligibility List No, 2557

Installation ofK S Avionics EGT/CHT-2() combinedeXhaust gas and cylinder head temperature monitoring system in accordance with K S AvionicsInc, Drawing No, A600TD-(**) Rev I, dated October 3, 1994 or later FAA Approved revision,

-:£'~.-.d~...d~ " This approval should not be extended to other specific airplanesof these models on which other previously approved modifications are incorporated, unless it isdetermined that the interrelationship between this change and any of those other previouslyapproved modifications will introduce no adverse effects upon the airworthiness of that airplane,

Original cylinder head temperature head equipment, if required by the original type design, mustremain installed and operable, See continuation page 3.

,,-Jk~~k.-.dJk"'0/0-1'7~u.-~,h<ch-""./k/"",•••/~~.,,,,/..k//~;~~#/ .•••.4/~

~~~ 4~~~k""'L/kru~.6f/~.;,k/~Y'Jk ..rUm'n,;,""'/',~-/1k

June 29, 1984

April 29, 1985 January 12, 1995

.'1IJ#'~Hr/;""1"1£ .rt/Nu;n~hw4,~

~>~']\fa; ger, PropUftJ6'l'!'B'tanchLos Angeles Aircraft Certification Office

(TltI~)

Any alteration of this certificate is punishable ~JJ a ,fine of not txutding '1.000. or imprisonment not txcetding 3 years, or both.This urlijicau m~,INIraruf"wi in a£cordanctwilh FAR 2/.47.

C\ t&~IIPage 1 of 3 J)"":

, f I

fAAPe- 8110-2 (10-681

tlnlttd .sma of I!mrmBtparnnrnt of 1:ransportation-.:frotml alliation administration

~upplcmmnll 1t~P(ctcrtifirQt((Q:ontinuation ~cct)

JV~ SA2557NM

Limitations and Conditions (continued):

A copy of pages I & 3 of this STC must be included in the permanent records of each airplanemodified in accordance with this STC.

CHT and EGT limits must be maintained using the original (Primary) aircraft CHT and EGTgages, if installed.

Required Equipment:

Systems coveredby drawings:

A600TD-2X4 ()

A600TD-2X6 ( )

FAA Approved Airplane FlightManual Supplement / SupplementalAirplane Flight Manual:

A9003-4, Initial Issue, dated12-2-94 or later FAA Approved revision

A9003-6, Initial Issue, dated12-2-94 or later FAA Approved revision

- END-

Any alleration of this certificate is punishable by afine oj not exceeding 11,000, or imprisonment not exceeding 3 years, or both.FAA FORM 8110-2_1 (10-651) This ,erliji£ate may be transftrred in Quorda1l&e wilh FAR 21.47.

PAGE 3 OF 3 PAGES

."

Page I of 13

FAA APPROVED

K S AVIONICS

MASTER ELIGIBILITY LIST

NO. 2557

INSTALLATION OF COMBINED EXHAUST GAS

AND

CYLINDER HEAD TEMPERATURE MONITORING SYSTEM

STCNUMBER: SA2557NM

DATED: 4-29-85

REVISION: C

DATE: FEB 222007 .YJ-A";"" - ( 'f.> L-

This Master Eligibility List consists of 13 pages

Jan 24 07 05:3Sp

REVISION NO.

Nrc

Ksa Nicad

REVIS ION LOGTO FA~ APPROVED

~~STER ELIGIBILITY LIStNO. 2557

REVISION DATE

1 510 782-0329

Page 2 of 13

REVISION

In it i a I Re leas e

p.9

A

B

c

~ 12 1995

Aug 07 2000

fEB 22 2007ft- 1+••••• -1~l-

Addi tion of certainaircraft models andinstallation of alt-ernate systans =veredby DI'lgsA60aro- 2X4 ()and A60OTD-2X6 ().

Addition of aircraftmodels on nages 9 and 13.

Addition of Cessna206H and T206H modelson page 7.

[L[n: LISTUJ

ll..

OJC\IC'JoI

C\ICDt-

o~UJ

~

"tJrou.~z:ro1/1><:

<;TC SA2557NM

HAKE

Aero Commander

Aero Commander(Heyers)

Aero Commander

Aero C<mrander

SCCATA-GroupAEROSPATIALE

scx:ATA-GroupAEROSPATIALE

Av ions pierre

.Beech

HASTER ELI

HODEL

100,I00A,100-180

200, A,B,C,D

500,500BU,S.520,5GO5GOA,-E,

560F,6BO,680-E,F,FL, FL (Pl; 720

SODA685

TB-10

TB-20,21

R21GO

CI7L,SC17L,C17B,SCI7B

C17R,SC17RDI7R017 A

I'. C •

1A21

3A1B

6AI

2A4

6Al2M

AS1EU

AS lEU

A48 EU

ATCG02

ATCG046387 I 3

TOP DRAWING NOS.

AGOOTD-2(L)-2S4(LJ-2X4D

AGOOTD-2(L)-2SG(L)-2XGB

AGOOTD-2T(L)-2ST(L)-2l'S6 (L)-2srS6 (Ll-2XGD

A60OTD-2T(Ll-2ST(Ll-2TS6(Ll-151'56 (Ll-2X6B

A60OTD-2(L)-254(L)-2X4D

A60OTD-2(L)-256(Ll-2X6D

AGOOTD-2(L)-2S4(L)-2X4D

AGOOTD-2(L)

Page 3 of 13

APPROVED

4-29-85

4-29-85

4-29-85

4-29-85

1-12-95

1-12-95

4-29-85

4-29-85

".- -_ ...._----- ...__ .._-------------- -------

ll..UJC'J

UJot-o-toC\I

Cro"1

Beech

------------------------ --

18A,S18A 63018D,S18D,AIBA,SA18A A684AI8D,SA18D

I 8 S, B.18 S 7 1 0DlBC,DI8S ,E1BS ,EI8S- A765-9700,G18S,H18,C-4SG,TC-45G,C-45H,TC-45H,TC-45J,JRB-G.3N,3NH.3TH.RC-~5J.UC-45J

D1BC-T 770CI8S A757

AGOOTD-2TE L)-2ST(L)

4-29-85

STC SA2557NH HASTER ELIGIBIV 1STPage 4 of 13<D HAKE HODEL T,C, TOP DRAI/ING NOS, APPROVED"-

Beech 23,A2J-19,19A,BI9, AICE A600TD-2( L) 4-29-85H19A,A2J-Z4,B23. -254(L)C23,A24,A24R,B24R -2X40C24R(])

Beech A23,A23A AlQ; AG00ID-2 (L) 4-29-85N('J

.-2S4 (L)

0

-2X4BI

NIIIr-

Beech 35;A3S-G35:3SR; A600TO-2(L) 4-29-85A77 70

JS-J] ,AJ], B)J JA1S -256(L)~111

CJ3,CJJA;EJJ,A,C: -2X6B~FJJ,A,C:GJ3;H,J,K,M,N,P,5,VJS;VISA,B;36,A36;AJ6TC;BJ6TC

Beec h 4S,A4S,D4S SA) AGOOTD-Z( L) . 4-29-85-256(L)-2X6BBeech 50,B50:DSO,A,B.E, SA4 A600TO-2T(L) 4-29-85E-S990;ESO,F,G,H,J -25T(L)-21S6(L)-25TS6(L)-2X6D1) Bee ch 95,B95,B95A,D9~,E95 JAl6 AGOOTD- 2T( L) 4-29-95

~

-25T(L)u

-21S4(L).-z:

-2S1S4(L)~

-2X40~:< Beech 95-55,-A55,-B55,-B55A, 3Al6 A60lJID-.2T(L) 4-29-85-B55B,-eS5,-eSsA;D55, -2Sr(L)D55A;E55,ES~;59,5BA -2TS6(LI"-

-2sr56 (I,)to

:-2X6BM

'Beech..56TC,A56TC 3Al6 A60fJID-2T(L) 4-29-95

n

-2sr(L):J~

-2TS6(L):J

-2sr56 (L)•-2X6D~

(

~

I1

Page 5 of 10

N 5TC 5A2557NM HASTER ~~lGIBI~lTY ~I5T0.. I

MAKE MODE~ To C. TOP DRAWING NOS. ,\PPROVED

Beech 5BP,58PA,58TC A23CE A600TD-2T(I.) 4-29-8558TCA -25T( ~)

OJ -2TS6(L)N -2STS6(L)('J - -2XEBaI 8eech 60,A60,B60 Al2CE A600TD-2T(L) 4-29-85NtIl -2ST{L)t'- -2T56{L)a -2STS6{~)~ -2X6DI!l

Beech 65;A65;A65-B200; 30\20 A600TD-2T(L) 4-29-85~ 65-BO,ABO.-A80-BBOO, -2ST{L)-B80.-88;70 -2TS6(L)

-2STS6{L)-2X6D

Beech I 76 A29CE A600TD-2T(L) 4-29-85-2ST(L)-2T51,(L)-2STS4{L)-2X4D

Beech I 77 AJOCE A600TD-2(~) 4-29-85-2S4(~)

1l -2X4Drou Bellanca 14-13; l4-l3-2, 773 A600TD-2(~) 4-29-85.~ l4-l3-3,14-IJ-3W -2S6(L)z: -2X6Aro 7AC,7BCN, A600TD-2(~) 4-29-85III Bellanca 759~ 7CeM, 7D C, 7EC, 7ECA. -2S4(L)

7FC,7JC,757ACs,7CCMs,7CCs -2X4EBellanca 7OC,70CA,70CAA,7OCB, 759 A60CTID- 2(L) 4-29-85

0.. 7OCBA,7OCBC,?He -254 (L)t'- -2X4DI!l..N Bellanca 8KCAB, 8GCBC A2lCE A600rD-2(~) 4-29-85a -2S4(L)t'- -2X4Da

Bellanca 14""19 -2,-3 lA3 A600rD-2(~) 4-29-85I!l -30\;l7-)0 -2S6(~)N

c -2X6B .. . . -- - ..- - -- - .ro.,

Page 6 r["- 5TC 5A2557NM MAST •. ~LIGIBILITY LISTQ.

APPROVEDMAKE MODEL T. C. TOP DRAWING NOS.:

Bellanca 14-19;17-31,-31TC 1A3 A600ID-2(L) 4-29-85-256 (L)-2X6DC1l Cessna 152,A152 JAl~ . A60OID-2(L) 4-29-85N

('J i -2541L)0I -2X4DN

CD150,150A-II,J-M; 3A19 A600TD-2( L) 4-29-85["- Cessna

I A1S0K,L,H -2S4(L)0"

-2X4E~In Cessna 170,170A,B 799 A600TD-2(L) 4-29-85~

-2S6(L)-2X6ECessna 172 thru 172H 3A12 A600TD-2( L) 4-29:..85-2S6(L)-2XGECessna 1721 thru 172Q 3A12 A600TD-2(L) 4-29-85-2S4(L)-2X4DCessna 175,A,B,C;PI72D; 3Al7 A600TD-2(L) 4-29-85-2S6(L)-2X6E-

"ll Cessna "R172E,F,G,H,J,K 3Al7 A600ID-2 (L) 4-29-85III

-256 (L)u".•

-2X6Bz:III Cessna 172 RG 3A 17 A600TD-2( L) 4-29-85VI

l<: -2S4(L)-2X4D

Cessna 180;180A-ll,J,K SA6 A600TD-2(L) 4-29-85Q.

-2S6(L)to('J -2X6B.. Cessna 182;182A-H,J-N,P, 3A13 A600TD-2(L) 4-29-85In0 . Q, R -2S6( L)["- -2X6B0 Cessna R182,T182,TR182 3Al3 A600ID-21L) 4-29-85oj"

-256 (L)N

c -2X6DIII...,

STC SA2557tU1 MASTE IGIBILITY LISTPage7 of13

MAKE

Cessna

Cessna

Cessna

Cessna

Cessna

Cessna

Cessna

Ce 5 sn a

Cessna

Cessna

MODEL, T.C.

185;185A-E;AI85E,F 3A24188;188A,B;A188, A9CEA.B;TI88C

177, A, B A13CE

177RG A20CE

190;195,A.B A790

206,H*;P206,A-E; A4CEU206,A-G;TP206A-E;TU206A-G;T206H*

207,A;T207,A A16CE

210.A-N,J-N;210-5; 3A21210-5A;T210F-N.J-N;P210N

n03 A34CE

305A.C,D,F 5A5

305B,E 3A14

TOP DRAWING NOS.

A600TD-2( L)-2S6(L)-2X6B

A600TD-2~(L)-284 (Ll-2X4D

A600TD-2( L)

A600TD-2( L)-2S6(L)-2X6B-2X6D*

A600TD-2(L)-2S6-(L)-2X6B

A600TD-2(L)-2S6(L)-2X6B

A600TD-2T( L)-2ST(L)-2TS6(L)-2X6B

A600TD-2(L)-2S6(L)-2X6B

A600TD-2(L)-2S6(L)-2X6B

APPROVED

4-29-85

4-2~85

4-29-854-29-85

FE'" ' "I ' r# ~!J ~,t,tUJI )/'f/M"'-'''''-4-29-85

4-29-85

4-29-85

4-29-85

4-29-85

*Top Drawing A600TD-2X6D applicable to Cessna 206H and T206H modelsin place of -2X6B. TD's -2(L) & -2S6(L) apply to all 206 models.

Cessna

Cessna

310,A-L,N,P,Q.R;E310H,J;310J-l;T310P,Q,R,

320.A-F;'320-1,335,340,340A

3AI0

3A25

A600TD-2T(L)-2ST(L)-2TS6(L)-2STS6(L)-2X6B

A600TD-2T(L)-2ST(L)-2TS6(L)-2STS6(L)-2X6B

4-29-85

4-29-85

Page B d0~

STC SA2557NMHASTER ELIGIBILITY L1STD..

HAKE HODEL T.C. TOP 0RAW ING NOS. APPROVEDCessna. 336 A2eE A600TD-2T(L) 4-29-85-ZST(L)OJ

-ZTS6( L)Nt'l -

-ZSTS6(L)0

-2X6BIN Cessna 337.A-H;H337B; A6CE A600TD-2T(L) 4-29-85(Xlr-

T337B-H;T337H-SP; -ZST( L)0 P337H -ZTS6(L)~

-2STS6(L)lIJ

-2X6B~Ces~na 404 AZ5CE A600TD-ZT(L) 4-29-85

-ZST( L)-2TS6(L)-ZSTS6(L)-2X6BCessna 40l.A.B;40Z. A7eE A600TD-2T( L) 4-29-85A-C;4Il,A;4l4, -ZST(L)A; ,4Z1 ,A-C -ZTS6(L)-ZSTS6(L)-2X6BCarmander 112,112B,112TC,112TCA AI2SO A60OJ.'D-2 (L)1l Aircraft-284 (L)••u-2X4D

.~z: Ccnmnder . 114,l14A,l14B AI2SO A60OJ.'D-2 (L)•• Aircraft

-286 (L)III

-2X6D~

Dellavilland DHC-2 ,HK-I, II, III A806 A600TD-Z(L) 4-29-85D.. DeHav illand DHC-3 A815 A600TD-Z(L) 4-29-85r-t'l

"G r umm a n..AA-l,-IA.-IB, All EA A600TD-Z(L) 4-29-85

lIJ

-.1C-ZS4(L)

0

-2X4Dr-

A600TO-Z(L)0 Grumman AA-S,-5A,-5B AI6EA 4-Z9-85...

-ZS4(L)N

-2X4Dc••...,

STC SA2557NHHASTen ELIG[BILITY LIST

~~D..

HAKE HODEL T.C. TOP DRAWING NOS.

Page '1)

APPROVEDGrumman GA-7

Lake (Consolidated LA-4,-4A,-4P,Aeronautics, Inc. -4-200

[J1NcryoI

NIIIr-o~111

~

1)~UM

z:~~l.:

D..r-cry

111or-a

•••N

C~...,

-~..- -. -. - ..

Lake (ConsolidatedAeronautics, Inc.

Maule

Mau!,e

Haule

l'laule

Haule

Mooney

'Mooney

Mooney

NaVLon

250

H- 5 -180 C ,-21<11'C,~~6-180,MX-7-160,C.-ISOAC, ~180B,-18OC,~DIT-7-160,-180,ABeeDee M-4;M-4,C,S,T

M-4-18OC,S,T;~4-220,M-4-22OC,S,T;H-5-22OC

~4-210,M-4-21OC,S,T;~5-2IOC

~5-235C,M-6- 235M-7-235B,-235Ci-260,C,Ml'-7-235 ,-260H20, A-J

H20K

H22

Nav i on t A iD,E/F ,Gill

AI7S0

( I Al 3 )

IAll

3A23

3A23

3A23

3A23

3A23

2A3

2A3

A6SW

A78 Z

A6 OOTD- 2T( L)-2ST(L)-2TS4(L)-2STS4(L-)--2)(4D

A600TD-2(L)-2S4(L)-2)(40

A6aOTD-2( L)-2S6(L)-2X6D

A600TD-2(L)=254 (Ll-2X4D

A60aro - 2 (Ll-256 (Ll-2XGE

A60aro -2 ILl-256 (Ll-2X6A •

A60lfl'D- 2 (L)-256 (Ll-2X6B

A60lfl'D-2 (Ll-2S6 (Ll-2)(6D

A600TD-2( LI-2S4(L)-2X4C

A600TD-2( L)-ZS6(L)-2X6B

A600TD-2(L)-ZS6(L)-2X6C

A600TD-2(L)-2S6(L)_?V=

4-29-85

4-29-85

4-29-85

8-7-00

4-29-85

4-29-85

4-29-85

8-7-00

4-29.-85

4-29-85

4-29-85

4-29-85

OJ STC SA2557NM HASt. ELIG IBIL It'i LIST Pag" lOaf L~

"- HAKE HODEL T.e. TOP DRAWING NOS . APPROVED. Navion Navion B A782 MOaI'D -2 (L) 4-29-85

-2S6 (T,)-2X6D(1J

A600TD-2(L) 4-2~--B5OJ Piper PA-Ia,S,A,"IOS", IA2C'1

S"105", II 12511• Sit 12511 -2S4( L) .0I AS'11251',"13S".StI135", -2X4DOJ

AS" 1 J 5 II I II 150" • A" 15 0 II JOJr-

Sit 150 It , AS" 1 5 0 II

0~Piper PA-ZO.S ,"115" •5" 115" , lA4 A600TD-2{ L) 4-29-a5

1I1

~ 11135",511135" -2S4(L)-2X4DPiper PA-Z2,-10a, lA6 A600TD-2T(L) 4-29-85-135, S-135, :"ZS4(L).-150,S-150, -2X4D-160,5-160

Piper PA-23. -160 lA10 A600TD-2T(L) 4-29-85-2sT( L)-ZTS4 (L)-2STS4( L)-2X4DPiper PA-Z3 ,-235, lAI0 A600ID-2T( L) 4-29-85

"0III -Z50,PA-EZ3-Z50 -ZST(L)u

-ZIS6(L).~z:

-2SIS6(L)III-2X6D\Il Piper PA-Z4-Z50,260 lA15 A600ID-2(L) 4-29-85

~

-2S6(L)-2X6DPiper PA-Z4 -180 1A 15 A600TD-Z( L) 4-29-85"- -ZS4(L)r--2X4DC'1.. Piper PA-24-400 lAl5 A600TD-Z(L) 4-29-851I1

0

A600TO:"'2(L)Piper PA-25 2A8 4-29-85r-

-2S4(L)0

<t A600TD-2X4DOJ

cIII.,

_. - . - -- ----- -- ..•_.__ ._.- ... -.._---. -._- ._- ._--.- ---. -- - - --_._.- ...('l STC SA2557NM MA51 ;LrG I-a [1.1ry 1.[5T Page 11 of 1:>-

MAKE MODEL T.C. rop DRAWING NOS. APPROVED"-Piper PA-25-235,-260 2AI0 A600TD-2( I.) 4-29-85

-256(1.)-2X6DPiper PA-28-235,-236 2A13 A600TD-2( L) 4-29-85(1J

-256 (I.)N

- -2X6D('l0

4-29-85I Pi~ PA-28-Z01,-201T; 2AlJ A60aro -2 (I.)NCD PA-28R-201T,Rr-ZOlT -2S6(L)•••

-2X6B0- piper PA-28-140,-150 2AI3 A600TD-2( I.) 4-29-85III

-160,-151,-161, -254(L)- -180,-181;5-160, -2X4D-IBO;R-1BO,-200,Piper PA-30,-39,-40 AIEA A600TD-2T(L) 4-29-B5-25T(L)-2T54(L)-25T54(L)-2X4DPiper PA- 31P A8EA A600TD-2T( L) 4-29-85-2ST (L)-2T56(1.)-2ST56(L)-2X6D1l Piper PA-32-260, A350 A600TD-2( L)

III

4-29-85u

-300,-301, -256( L)- ..z: -301T;5-300, -2X6DIII R-300,R-301,

•VI R-301T,RT-300,~

RT- 300T

"- Piper PA-34-200 A7S0 A600TD-2T( I.) 4-29-85CD

-25T(L)('l

-2TS4(L).. .III

25TS4(L)0

-2X4D••• Piper PA-34-200T, A7S0 A600TD-2T( L) 4-29-850

-220T -25T(L).,-

-2T56(L)N

c-25T56(L)III

-2l{6B" -_ ..-. . _ .... --- _.- - _.- ----_ .. ._. ---._._------ -----

-'!!IlaIJlE ..__ -, )--_ •.•~.-':~~--_._~';"~''':;=_._~_.~_.~-~......._.,--.,... ., ---,. - ~. ,~,._~~_._.•.._-~.._._._, ..~..---.,..~~...".."'""--.~_._-_.•_.-._- .

q--lL STC SA2557NM MASTER ELIGI5IL~TY LIST . Pare 12 of 13

MAKE MODEL r. C. TOP DRAWING NOS. APPROVEDPiper PA-38-112 Al8S0 A600TD- 2(L) 4-29-85

-254(L)-2X4DIII 4-29-85N Piper PA-44-180, Al950 A600TD-ZT(L)C'1 -180T -2ST"(L)0I -2TS4( L)N -ZST54(L)O:lC" -2X4Da Piper PA-46-310p Az550 A600TD- Z(L) 4-29-85- -Z56( L)III -2XGB- Piper PA-46-350P A2S00 A60lJID-2 (Ll 1-1z-95

-256 (LI-2X6D

Piper PA-60-600,-601 AI7WE A600TD-ZT(L) 4-Z9-85-60IP,-602P, -25T(L)-700P -ZT56(L)

-Z5TS6(L)-2X6D

pitts 5-15,-IT,-2, AS SO A600TD-Z(L) 4-29-85-ZA -Z54([.)

-2X4D1]1110 pi tt8 S-2S, '-ZB A8S0 A600TD-Z(L) 4-29-85'"z: -Z56([.)-2X6D111 4-29-85III Republic RC-3 A769 A600TD-Z(L)'" (STOL) -ZS6(L)

-2XGASt inson 108,-I,-Z ,-3 ,S 767 A600TD-Z(L) 4-29-85

lL -Z56(L)al -2XGAC'1 ' - Swi ft ---- GC-IA 766 A600TD-Z(L) 4-29-85.. .III -Z54(L)a -2X4EC" , Swift GC-IB 766 A600TD-Z(L) 4-29-85a -ZS6(L)q- -2XGEN Siai Marchetti S.205-ZZ/R A9EU A600TD-Z(L) 4-79-85c -zS6(L) (\111'1 -2XGA ;'I

!

1I1 STC 5A2557NM MAS., ELIGIBIL1..TY I.ISI Page 13 "6f .LJ~

"- MAKE lIODEL T.C. TOP DRAWING NOS. APPROVED

Aeonacchi S. p •A. F.260B, F. 26OC, AlOEU A60arD-2 (L) 8-7-00(Siai ~larchetti) SF.260D F.260E, F.260F . -2S6(JJ),

-2XGD(])N

White International A-I, A-1A* A22NM" AGOarD-2(Ll 1-IL-95t'1a (Christen, Aviat)

-2S4 {Ll *IN

-2X4DIII['- Taylo=aft FI9 1A9 AGOarD-2 (L) 1-12-95a

-2S4 {T,l~-2X4E1I1

~ Taylorcraft F2l,F2lA,B;F22,F22A,B,C lA9 A60arD-2 (Ll 1-12-95

-254 eLl-2X4D

- EM) -

"tlIIIo

"..z:III~~

"-IIIt'1

1I1a['-o.•.N

CIII.,

*White International mx1el A-lA approval date