Supplemental Type Certificate

,,/ .·April 19, 2012 !.!mA- umwv/N/.· ,., ,., /Nw,.,n.,,hrn. ,/un N ,.g,.,.,,.,:,,, . m •·01114 euo-2 1 •.. ,,//A,. .k/,,.,,/ • , • , (Title) llniteb &tatrf Cl& Revision Original Issue f §merira j)epartment of til'ansportation - jfeberal abiation §b1ninitrtration tEppe itate (ftonthtuation i>beet) SAOJ962AT Date of Issuance: April 19, 2012 (Continued): 3. A copy of this Certificate and the FAA approved Flight Manual Supplement, AFMSSR22TSSON, Revision.-, dated 0410512012, or later FAA approved revision, must be maintained as part of the pennanent records of the modified aircraft. 4. An oxygen system meeting the requirements of 14 CFR Part 23, Secs. 23.1441through23.1449 must be installed in conjunction with this STC . ./]",;;:; .. The type certification basis is as shown on TCDS A00009CH plus the equivalent level of safety to FAR 23. I091(b)(4) number ACE-06-06. -End- 0 Form Approved IElectronic Tracking Number OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION 1113012007 US Department For FAA Use Only of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration INSTRUCTIONS: Print or type all enbies. See Title 14 CFR §43.9, Part 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) Nationality and Registration Mark Serial No. USA N8AE 2999 1. Aircraft Make Model ISeries Cirrus Design CORP SR22 Name (As shown on registration certificate) Address (As shown on registration certificate) Reiss Leasing, LLC Address 1016 SPRING VILLAS PT 2. Owner City Winter Springs State FL Zip 32826 Country United States 3. For FAA Use Onlv 4.Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. D AIRFRAME (As described in Item 1 above) D D POWERPLANl D D PROPELLER Type D D APPLIANCE Manufacturer 6. Conformity Statement -A. Agency's Name and Address B. Kind of Agency Name Steve Miller x U.S. Certificated Mechanic I Manufacturer 6530 Tamea Executive Aireort R Foreign Certificated Mechanic C. Certificate No. City Tam(;!a State FL Certificated Repair Station 2700197 Zip 33610 Country United States Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the unit(s) identified in item 5 above a;1d described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Av!.3bon Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel Individual per 14 CFR Part 43 D IL( V\.A fl.. 'Lo[b App.B :J,,,_ Jl..-£/1 1-- - 7. Approval for Retum to Service Pursuant to the authority given persons specified below, the unit identified ·in item 5 was inspected in the manner prescribed Administrator of the Federal Aviation Administration and is Approved D Rejected by the FAA Flt. Standards Manufacturer Maintenance Organizi:ition I Persons Approved by Canadian Inspector Department of Transport BY Other (Specify) FAA Designee Repair Station x Inspection Authorization Certificate or Signature/Date of Authorized Individual <;f ... · Designation No. A&P 27001971A March 14, 2016 Steve Miller FAA Form 337 (10.os) "-" NOTICE Weight and balance or operating limitation changes s.'1all be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) I USA N8AE 11 /f(M/4f/2o!Ca Nationality and Registration Mark Date -Removed engine M/N 10-550-N S/N 691542. -Installed CMI rebuilt engine M/N TSI0-550-N1B S/N 1031045 IAW STC# SA03962AT-E with referance to installation Instructions IMSR22T550N. O.Ohrs Time since Rebuilt. D Additional Sheets Are Attached FAA Fonn 337 110-06) llh\ftt:b &Jallm ri hlUl'fm of <!Jmnsporlalinn-Jf.ebmd J\ufathm i\m11tdstmtfot1 Wmtt <lttttifiattt SA01708SE 9Z:1 tJJ114t.ftt> Precise Flight, Inc. 63354 Powell Butte Rd. Bend, OR 97760 IJ&"tt/te.1 • 23 tJ/de A00009CH Cirrus Design Corporation SR22 oj'de Installation of the fixed oxygen system manufactured in . accordance with Precise Flight Engineering Drawing Lists: 102NOOOO Revision A, 1OONOOOO Revision X, 027NOOOO Revision C, :026NOOOO Revision C, 020NOOOO Revision F, 010NOOOO Revision H, and i 009NOOOO Revision B or FAA approved revisions. Installed in accordance with P(ecise Flight · Engineering Drawing List102NOOOO revision A or later FAA approved revision. Maintained.in : . accordance with the Instructions for Continued Airworthiness Precise Flight Document 102NMANOQ03 Revision A, dated October 3, 2006 or later approved revision or document. mul Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this · · change and any of those other previously approved modifications, including changes in type will Introduce no adverse effect upon the airworthiness of that aircraft. · · See Continuation Sheet, page 3 9LtJ t:1 : August 1, 2006 October 4, 2006 ·-·- -···· ·:.----.. ,,. (Signature) Acting Manager, Seattle Aircraft Certification Office : (fltle) Any alteration of this certincate is punishable by a fine of not exceeding $1, 000, or imprisonment not exceeding 3 years. or both. This certificate may be transferred In accordance with FAR 21.47. FAA FORM 8110·2(10-68) .. &lldm rt 1\anmca ieparlnm l1f Olransppr1atiot1-1Jf.dmd 1\uiation - &ltpplemtntal aJmtt Q!tttifiattt (Qtnnttuuattnn i'lttet> Af'unzl'e, SA01708SE Precise Flight, Inc. Reissued: Amended: A copy of this Certificate and the FAA approved Airplane Flight Manual Supplement (AFMS), Precise Flight Document 102NMAN0001, dated October 2, 2006 or later approved revision, must be maintained as part of the permanent records for the modified aircraft. This oxygen system installation is qualified to operate up to 25,000 ft MSL but, this installation does not change the maximum operating altitude of the airplane on which it is ;installed. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. ' · . · -END- Any alteration of this certificate Is punishable by a fine of not exceeding $1,000, or Imprisonment not exceeding 3 years, or both. ,,,..,.,... FAA FoRM a110-2-1 (10-69) This certificate may be transferred In accordance with FAR 21.47. PAGE 3 OF 3 PAGES ©f J\ineriaa of 1ftrnnspnrtation - JJf eberal J\friatinn J\bminiistratinn W:upe <tiertifirate SA00296BO ,;;.J,,H//,t Avidyne Corporation 55 Old Bedford Road Lincoln, Massachusetts 01773 Qq/ /4,. r4tmy,. ,;,, d,.1'?#• ,/,.,upn fr' dt> ft.//r,Nny ,,.'7..f g,. ruff/ ITJ ..(;,,""°" mN/J. /A-, ,,,,lf.,.,./A,N-JJ ,,,.,,,,m'1f'h/J ,,/:"#},,/ ,J'.f r//A,. ,oYNfrJP#r. /l,,,.,.U/,r,n ,., .· Installation of: A00009CH Cirrus Design Corporation SR20,SR22 • Model DFC90, p/n 700-00170-000, loaded with Release 2 software (or later FAA approved release) OR • Model DFC100, pin 700-00170-001, loaded with Release 2 software (or later FAA approved release) Avidyne Corporation Autopilot as a replacement for the S-TEC System Autopilot, see Limitations and Conditions J, in accordance with the Avidyne Corporation Master Document List, Document AVDFC-019, Rev 10, dated June 24, 2013, or later FAA-approved revision . . ,,,,,/ I. Operation must be in accordance with Avidyne Corporation Aircraft Flight Manual Supplement (AFMS) as follows: For DFC90: Document 600-00249-000, Rev 03, FAA approved on June 27, 2013, or later FAA-approved revision. For DFC I00: Document 600-00271-000, Rev 02, FAA approved on December 22, 2011, or later FAA-approved revision. The AFMS must be carried in the aircraft during all flights. (Limitations and Conditions continued on Page 3 of 4) .?Jf;:J rM</bf,. JtVV'"'/,;'?. r/a/a ,J1r;f ,.;i d,. fo' 'V1/l"''-'al' ,h, #-d ,,,,,/,/ n-rrk/,., n /,..w1u.;m/,;,,,_ r/u/I" ,.;i /[, /§, • ,,//,{,. ,.y;.m,,,rae. ,./ .· October 16, 2009 ,,/N.Jurv1r_,. .• June 18, 20 I0 ,,,,.,,,.,,m.,/..·July 21, 2010; February 03, 2011, March 04, 2011, December 22, 2011, June 27, 2013 .fi? ,./&fr . gnatuTe) Robert G. Mann Manager Boston Aircraft Certification Office ).!inileb Jjbdeo ®f !.'mericn of 'atrnnsp.ortation - JJr.e.bernl !\friati.on JiupplenrentaI emwt aitrtif kah (Olontinuation SA00296BO June 27, 2013 INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of the Supplemental Type Certificate. The FAA will reissue the in the name of the transferee and forward it to him. TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number _____ _ to (Name of transferee) (Address of transferee; (Number and street> CCity, State, and zrp code) from (Name of grantor) (Print or type) (Address of grantor) (Number & street) (City, State, and ZIP code) Extent of Authority {if licensing agreement): Date of Transfer: Signature of granter (In ink): Any alteration of thls cert1f1cace ls puniShabla by a fine of not exceedi.nq $l,OOO, or lmprlson111ent not exceedlnq FM Form 8110-2-1 (10-69) Paqe 2 of 4 Thls cert.ificate m.1y be trans£erred in accordance with FAR 21. •1'7. ltnUeb .$tutee (Qf "nurica :!B.epartment nf 'mranspnrbdhtn - JJf e.b.eral ( <nnntinuati.on SA00296BO June 27, 2013 2. Maintenance must be in accordance with Instructions for Continued Airworthiness (ICA), Document AVDFC-030, Rev 04, dated May 22, 2013, or later FAA accepted revision. The ICA must be made available to the operator at the time of installation. 3. Aircraft must be configured with an existing S-TEC Manual Electric Trim (MET) System and with an existing S- TEC Autopilot as follows in order to accomplish this STC: 4. Aircraft must be configured with an existing Flight Display System as follows in order to accomplish this STC: Avidyne Corporation Autopilot Existing Flight Display System Aspen Avionics, Inc. EFDIOOO Primary Flight Display, pin 910- 00001-XXX, loaded with Release 2.6 software (or later FAA ForDFC90 approved release). Avidyne Primary Flight Display, p/n 700-00006-( ), loaded with Release 8.0.4 software (or later FAA approved release) with Modification 55 installed. ForDFCIOO Avidyne Integrated Flight Display, p/n 700-00083-() loaded with Release 9.2.1 software (or later FAA approved release). S. Compatibility of this design with previously approved modifications must be detennined by the installer. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Cirrus Design Corporation SR20 and SR22 aircraft is as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A00009CH. (Certification Basis continued on Page 4 of 4) Any alte.raUon cf this c:e:tJ.!.i.cate i·;· punish.!ble by a fine of :1ot exceeding $1,000, or 1111p.ri.solll!l('nt not dl..Ct>ed11117 J years, er both. FAA Fcna Bll0-2-1 (10-69) Pa9e 3 of 4 Thi.G cert.i.t.l.cate 111.1y be in with F'J!R 21. 47. ©f c_America of 'mranspodation - Jlf weral J\&iation J\bministratinu 'IDupt artrtifh:ab ( ClIDtttittua:tion SA00296BO June 27, 2013 (continued from Page 3 of 4) b. The certification for parts changed or affected by the change since the reference amendment date, June 27, 2013, is based upon part 23 as amended by Amendment 23-57 as follows: Regulations at the latest amendment 23-0 through 23-57 23.301, 23.303, 23.305, 23.307(a), 23.337(a)(l)(b)(l), 23.34l(a), 23.473(d)(g), 23.56l(a)(b)(3)(e), 23.601 - 23.613, 23.77l(a), 23.773(a)(2), 23.777(a)(b), 23.867(b), 23.1301, 23.1308(c), 23.1309(a)(l)(2)(b)(e), 23.l 31 l(a)(2)(3)(4)(6), 23.1322, 23 .1329, 23.1335, 23.135 l(a)( l )(2)(i)(b)( 1)(e)(f), 23. l 357(a)(2)(b)(c)(d), 23.1359(c), 23.136S(a)(b)(d)(e)(t), 23.1367, 23.138l(a)(b), 23.143l(a)(b)(c), 23.1501, 23.1523, 23.1525, 23.1529, 23.l541(a), 23.1549(a), 23.lSSS(a)(b), 23.158 l(a)(b)(2)(3)(f), 23.1583(m), 23.15850) Regulations at an intermediate amendment None Regulations at the amendment level in TCDS A00009CH None If the holder agrees to pennit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that pennission. Any •lt&rac.ion of thls c:..:rU.tic:aLe is by;; fine cf not. !l,ODIJ, er iir,pr.isol\lllent not excel!'ctiuo J yeac1', or FAA Form BJ 10-2-1 !10-69! Paqr. 4 01' 4 • Form Approved 1Electronic Tracking Number OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION 212812011 US Department For FAA Use Only of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9, Part 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty for each such violation. (49 U.S.C. §46301 (a)) Nationality and Registration Mark Serial No. 1. Aircraft USA N8AE 2999 Make Model ISeries CIRRUS DESIGN CORP SR22 Name (As shown on registration certificate) Address (As shown on registration certificate) Address jQjfl AS EI 2. Owner. City WINTER State FL REISS LEASING LLC Zip 32708 Country USA 3. For FAA Use Onlv 4.Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. D [Z] AIRFRAME (As described in Item 1 above) D D POWERPLANT D D PROPELLER Type D D APPLIANCE Manufacturer 6. Confonnlty Statement A. Agency's Name and Address B. Kind of Agency Name SABASOIA U. S. Certificated Mechanic I Manufadurer Address 6530 TamQa Executive Aimort Road #125-A Foreign Certificated Mechanic C. Certificate No. City Iampa State El ./ Certificated Repair Station Zip 34285 Countiy USA Certificated Maintenance Organization QVOD957X D. I certify that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. - Extended range fuel SignahJre/Oate of per 14 CFR Part 43 D 3/9/16 /Jn App.B . 7. Annroval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is [ll Approved 0 Rejected FAA Flt. Standards Manufacturer Maintenance Organization I Persons Approved by Canadian Inspector Department of Transport BY Other (Specify) FAA Designee ./ Repair Station Inspection Authorization Certificate or ;p;:/ lndMdual Designation No. QVOD957X FAA Fonn 337 (10-06) I ·' NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable aitworlhiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) jusA N8AE Ie.__'9_11_6 ___ __, Nationality and Registration Mark Date Reference Material: Avidyne DFC 90 Installation Manual 600-00251-000 Rev: 09 Avidyne System Interface Cirrus 2X - System 20/30/55(X) 700-00170-000 Avidyne Post Installation Configuration and Testing 700-00170-XXX Rev: 01 Removed 55x (SN:0810-13366). Installed DFC-90 (SN: M153571994). Removed S-TEC 55X autopilot (SN: 0810-13366) and installed Avidyne DFC-90 (SN: M153571994) autopilot IAW Avidyne installation manual PN: 600-00251-000 rev 09 per STC SA00296BO and Cirrus Maintenance Manual PN: 13773-001 rev. 85. Updated equipment list, weight and balance negligible. See document PN: 700-00170-XXX Rev: 01 for Instructions for Continued Airworthiness. END----------------------- [lJ Additional Sheets Are Attached FAA Fonn 337 (10-06) ft) Form Approved )I Electronic Tracking Number OMB No 2120·0020 MAJOR REPAIR AND AL TERATION 11 /:!0/2007 U.S. Department Fo r FAA Use Only of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Adminis·tration INST RUCTI ONS : Print or type all entries. See Title 14 CFR §43 .9 , Part 43 A ppendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions a nd disposition of this form . This report is requ ired by law (49 U.S.C. §44701 ). Failure to report can result in a civil penalty for each such violation. (49 U .S . C. §46301 (a)) National ity and Regi stration Mark Ser ial No. USA NSAE 2999 1. Aircra ft Make Mod el ISeries CI RRUS SR22 Name (As shown on registration certificate) Address (As shown on registration certificate) FCPS LLC 58 STAT E STREET STE 2 2. Own er PORTSMO UTH , NH 0380 1- 3824 USA 3. Fo r F AA U se O nly 4. Typ e 5. Unit Id e ntific a tion Re pair Alteration Unit Make Model Serial N o. D IXl AIRFRAME (As de scribed in Item 1 ab ove) D D POW ER PLAN T D D PR OPEL LER Type D D APPLIANCE Manufacturer 6. Conformity State me nt A. Age ncy's Name a nd Address B. Kind of Agency Nex.Ai r A vion i cs LL C U. S. Certificated Mechan ic I Ma nufacturer 265 FRUIT STRE ET Foreign Certificat ed Mechanic C. Certificate No. MANSFIELD, MA x Certificated Repair Station N40R0878 020 48 USA Certificated Maintenance Organi zation D. I certify that the repa ir and/or alteration made to th e unit(s) identified in item 5 above and described on the rever se or attach ments hereto have been made in accordance with the requirements of Part 43 of the U. S. Federal Av iation Regulations and that the information furnished herei n is true and co rrect to the best knowledge.:..? Extended ra nge fuel D AND R EW O' SH EA per 14 CFR Part 43 App . 8 0 5-May-2017 7 . A ppro va l for Re turn to Se rvi ce P ursuant to the autho ri ty given persons specified be low, the unit i de ntified in item 5 was inspected in the manner pr esc ribed by the Administrator of the Federal Aviation Adm inistration and is gg Approved D Rejected FAA Flt. Stand ards Manufacturer Maintenan ce Organization I Pe rsons Approved by Canadian In spector Department of Tran sport BY FAA Des igne e x Repair Statio n I nspection Authorization Oth er (Specify) Certificate or ____.:::- MI C HAEL REARICK Designation No. N40R08 7B _..,.- 05-May-2017 FAA Fo rm 337 (10-06) ... NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration marlc and date worlc completed.) May-03-2017 Nationality and Registration Mark Date GENERAL: ALL WORK PERFORMED CONFORMS TO THE PARAMETERS SET FORTH IN THE FARS AND THE RECOMMENDATIONS AND GUIDELINES SET FORTH IN AC43.13-1 BAND AC43.13-2B. FAA ADVISORY CIRCULAR 43.13-1 B, CHAPTER 10, WEIGHT AND BALANCE FAA ADVISORY CIRCULAR 43.13-1 B, CHAPTER 11, AIRCRAFT ELECTRICAL SYSTEMS FAA ADVISORY CIRCULAR 43.13-1 B, CHAPTER 12, AIRCRAFT AVIONICS SYSTEMS FAA ADVISORY CIRCULAR 43.13-2B, CHAPTER 1, PARA. 100 THROUGH 114, STRUCTURAL DATA FAA ADVISORY CIRCULAR 43.13-2B, CHAPTER 2, PARA. 200 THROUGH 210, RADIO INSTALLATIONS FAA ADVISORY CIRCULAR 43.13-2B, CHAPTER 3, PARA. 300 THROUGH 312, ANTENNA INSTALLATIONS REMOVED THE FOLLOWING: INSTALLED THE FOLLOWING: 1. AEROSPACE LOGIC CIRRUS FUEL INDICATOR FOR CIES INC SENDERS FOR TWO TANKS (FL202G) PER MANUFACTURER'S INSTALLATION MANUAL, S200-FL202G-001REV1.1 DATED DEC 2014. FOR REGULATORY COMPLIANCE PLEASE REFERENCE AEROSPACE LOGIC AML STC # SA02825NY AND THE FOLLOWING TSO APPROVALS: II FAA TSO-CSSA (QUALIFIED SENDERS) 2. GARMIN FLIGHT STREAM 210 REMOTE BLUETOOTH SYSTEM PER MANUFACTURER'S INSTALLATION MANUAL, 190-01007-A3, REV 10 DATED AUG 2016 AND GARMIN AML STC # SA02019SE-D. FOR REGULATORY COMPLIANCE PLEASE REFERENCE THE TSO MANUAL 190-01700-00 REV B DATED OCT 2014 AND THE FOLLOWING TSO APPROVALS: II FAA TSO-C157 (XM wx DATA) NEW COMPONENTS WERE INSTALLED IN THE ORIGINAL LOCATIONS. NO STRUCTURAL MODIFICATIONS WERE NEEDED. PERFORMED MAINTENANCE OPERATION CHECK (MOC). PERFORMED FLIGHT TEST PERFORMED EMI TESTING IN ACCORDANCE WITH AC 43.13-1 B PARA. 11-107, INTERFERENCE TESTS UPDATED AIRCRAFT WEIGHT AND BALANCE POWER ASSESSMENT DONE IN ACCORDANCE WITH FAR REQUIREMENTS. POWER LOAD DOES NOT EXCEED 80% OF THE AIRCRAFT SYSTEM CAPACITY, DETERMINED BY CALCULATION NOTES: LOGBOOK ENTRIES MADE PER FAR REQUIREMENTS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: AEROSPACE LOGIC CIRRUS FUEL INDICATOR FOR CIES INC SENDERS FOR TWO TANKS (FL202G), P/N S200-FL202G-001 (LATEST REV). --·UUAUUUAUU NOTHING FOLLOWS ******"AUUUUUUUUU- 0 ADDITIONAL SHEETS ARE ATTACHED FAA Fonn 337 (10-06) } t i t i t r $ n l A l t flrpartmriit nf Sraneportation — .Jftbrrnl JKbtntinn Abmhiioirntinn ^uppUmental ®gp^ Qli^rtiftcatcI M P O R T . 4 ^ * 4 ^ S A 0 2 8 2 5 N Y /iJ»Vfr AeiXM|MC« i^gjc IlK. 180 James Sbnxt South, 205 liamitton. Ontario C a n a d a L 8 r 4 V I f r r / t / t r i M n / A i r r X i r / t y ^ M > i m M d h C f x4nr/lvr «rj J^frr/trt/4fr*fM Amr/i Mf Mtrtrrv^tMt^ t*fm>rstmt/} r/Mr tt//itr4ri/¥W AMI, * .Set anactml FAA Appiovctl M(h1<;! LHt dated (>7/38^010 or Utter FAA approved rcvuions for tlte list of approved airptnne m t x i f b i . (A*xrtjfMvr r/.^ytr Iitslallicion t>t'Aero«{»cc lx»gic Alrcrnll Instrument, ktcnlillcd in doctmtcni No. S200-CPI,, Rev. 1.0. doled 12/02/2009 »ir later Transport Canada appinved revisicMi!^ as priniaiy w secondary, new or rcptKcmcnt initniinenti. Insnllztiun nnm be in acctudance with Aetospoix l^ic Documem No. S200-CIL Rev. 1.0. doled I2/D2/200V, Transpun Canadaappivvcd 12/14/2009, ur later TrnnspontCuoaibappruvcda'visicnt'i. (2i<v CVtnlmualion .Slisot 2 nt2) ■ r r f f f y f r w A t n t t / A ( f t A t / i r < * ^ ^ 4 / i / J r 4 i n j ^ t r / y t r r t ^ / m t t t t m i n n r u A f v u i m r / m t • 4 ^ f ' J / j f / X r . fy^t/yrArwA^,- Jtttnury 15. J0)0 r/AHr»M*r Joly 2tl. 2(H0 ^ j / w A V , . ^ 5 . u V AittiMiny SivetjK M3nai;cr t X i f f t t s t t m ) \ N t v t Yo r t i A i r c i d i t C ' c fl i r i c i t r a t i O f r t i : l l n i t r f t p ( A t o r r t r a ^(pnrtuirnt of tSrnnapnrtiiHiin — ,3ffftrral Atiinlion .A&miuislrntion Supplemental ®upe Certificate (Qlmtthuwttiini ^l^cct) S A 0 2 8 2 5 N Y tJxIc i>f Lviueicc. Iu)> 38.2010 1, Operalidn of instrwiwnts titili/ing an mtensity control module muM he in accoi dance with Aerospace I j>gic • Doeiawnl S200-FM8. Rev tO. dated I2/02.'200'J, rronHWift Canada appfow-d 12/14/2009, w later I ranspott Canada revisions 2. Instnliaitim limitalions must he observed in aeeordanee with Aerospaee Kogie InMallation Litnhationt Saateroew - Doeunient No, S200-IIS. Kev, 1.0. dated 11^2/2009. Transp«n Canada approved I2M4.<20Q9, or later Transport Canada approved revisiooi. ITw products are to be installed in existing panel holes and ate to replace existing insinimcitt,Mio« As primaiy repbcemem products h is retonmtended Mtd preferred tltm they be plaeed in the iiatne panel locattim as the original equipment, "fheir visihlli^' and placetnent rcUtive to other htstrunteots are to be the satne or similar to Uie exliihtg insmmients. Wlterc they are in a dilTcrent loeation, tt is the r«)>p«»sibiltty of the installer to ensure tlistt they anj visible to tlte pihrt tinder all conditions. -X. M.tintcnsnce mujt be in accordance with Aeiospace l-ogie Initructioits fur Continued Airworthiness - l>)«ttmcm No. S200.ICA, Rev. 1.2, dated 5.O4/20I0 or later I rann'ort Cuiada accepted rcvijions. 4. Tlie installer must dciermint; wliether this dcsii;n cliaiigc 14 cvinpotibie with previously approved m o d i r i e a t i o n s . 5 irthe holder niirecs to permit •mother person to u«c ihin certiffewe to atler u product, the holder must give the other person WTrtlen evideiKC of that permission