Supplemental Type Certificate

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.) USA N34626 9/26/17 Nationality and Registration Mark Date Removed an ARC RT359A transponder. Installed the following equipment: Garmin GTX345 ADS-B in/out transponder at STA68.75 IAW STC# SA01714WI. The GTX345 interfaces to the audio panels unswitched input (PMA8000), GTN650 to display weather, traffic and to receive gps position information, to the transponder antenna(AV74) and encoder (SSD120). The ADS-B out system was shown to meet the equipment performance requirements of 14 CFR part 91.227. Attached is the Instructions for continued airworthiness for the GTX345 document number 190-00734-11 Rev. 5. _END_ ✓ Additional Sheets Are Attached FAA Form 337 (10-06) United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate Number SA01714WI This certificate issued to Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062 certifies that the change in the typo design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of Part 23* of the Federal Aviation Regulations. Original Product Type Certificate Number: Mbuke: Abodek * See attached Approved Model List (AML) No. ·SA01714WI dated May 1, 2013 or later FAA- approved revision for list of approved aircraft models and applicable airworthiness regulations. Description of Type Design Change: Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Data Required: (1) Garmin Master Drawing List (MDL) 005-00734-04, Revision 1, dated May 1, 2013 or later FAA-approved revision. (2) Garmin Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual (AFMS), 190-00734-15, Revision 1, dated May 1, 2013 or later FAA-approved revision. Bimitations and Conditions: (1) Compatibility of this design change with previously approved modifications must be determined by the installer. (2) Aircraft installations involving the Garmin transponder GTX 33/33D/330/330D models require the previous installation of an approved ADS-B position source. Refer to the design data specified in the Master Drawing List (MDL) listed above for specific hardware and software requirements. (3) Aircraft installations involving the Garmin transponder GTX 335/335R/345/345R models without an optional internal GPS require the previous installation of an approved ADS-B position source. Refer to the design data specified in the Master Drawing List (MDL) listed above for specific hardware and software requirements. This certificate and the supporting data which is the basis for approval skall remain in effect until surrendered, suspended, revoked or a termination duto is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: August 7, 2012 Lute of issuance. May 1, 2013 Date reissued: Date amended: April 29, 2014, March 8, 2016 By direction of the i Administrator FEDERAL * AVIATION OMINISTRATION ignature) Michael Warren ODA STC Unit Administrator ODA-240087-CE Garmin International, Inc. (Title) 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 8110-2 (10-68) PAGE 1 of 3 PAGES This certificate may be transferred in accordance with FAR 21.47. FAA Approved Model List (AML) STC SA01714WI Table I: Approved Aircraft WITHOUT GX000 Equipped Flight Deck System for installation of GTX 33/330 or GTX 335/345 Transponders Airplane Make (TCDS Holder) Airplane Model Designation Type Certificate Number * TC Certification Master Drawing List Revision AML Revision/Date [common name or previous make] Basis (005-00734-04) 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, CAR 3 A4CE FAR 23 Original 5/1/2013 TU206G, 206H, T206H 337, 337A (USAF 02B), 337B, T337B, 337C, 337E, T337E, T337C, 337D, T337D, M337B (USAF 02A), 337F, CAR 3 Original A6CE 1 FAR 23 5/1/2013 T337F, 337G, T337G, 337H, P337H, T337H, T337H-SP (continued) Textron Aviation Inc. (Textron Aviation Inc.) [Cessna Aircraft Company] 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425 Original A7CE CAR 3 177, 177A, 177B 207, 207A, T207, T207A 177RG 404, 406 501 551 5/1/2013 Original A13CE FAR 23 5/1/2013 Original A16CE FAR 23 5/1/2013 Original A20CE FAR 23 5/1/2013 Original A25CE FAR 23 1 5/1/2013 Original A27CE FAR 23 1 5/1/2013 Original Issued: May 1, 2013 Revised: 21-July-2016 441 A28CE FAR 23 T303 A34CE FAR 23 5/1/2013 Original 5/1/2013 21 of 27 Notes GARMIN. March 8, 2016 Subject: 1200 East 151st Street Olathe, KS 66062 P: 913-397-8200 F: 913-397-8282 STC Permission to use STC SA01714WI for Garmin GTX 330, 330D, 33, 33D, 335, and 335R with ADS-B Out (see AML); Garmin GTX 345 and 345R with ADS-B In and Out (see AML) Consistent with FAA Order 8110.4( ) and Advisory Circular (AC) 21-40( ), Garmin International grants permission to Garmin dealers, installers, and owners of the Garmin GTX 330, 330D, 33, 33D, 335, 335R, 345, and 345R to use STC SA01714WI and deliverable data associated with it, for the sole and express purpose of installation and approval of the installation of the Garmin GTX 330, 330D, 33, 33D, 335, 335R, 345, and 345R and associated interfaces to other previously approved equipment. Emnett Seffit Emmett Griffith Director of Engineering Garmin AT, Inc. 20160308eg01 Page 1 of 1 MAJOR REPAIR AND ALTERATION Form Approved OMB NO 2120-0020 2/28/2011 Electronic Fracking Nurnber For FAA Use Only US Department of Transportation Federal Aviation Administration (Airframe, Powerplant, Propeller, or Appliance) 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)) Serial No. Nationality and Registration Mark USA N34626 1. Aircraft 2. Owner Make Cessna Name (As shown on registration certificate) Robertson, Jason 17701907 Model Series 177 Address (As shown on registration certificate) Address 5998 Wyndemere. Dr. City Erie State PA Zip 16505 Country USA 3. For FAA Use Only 4. Type Repair Alteration 5. Unit Identification Unit Make ☑ AIRFRAME POWERPLANT PROPELLER Type APPLIANCE Manufacturer A. Agency's Name and Address Name Dunkirk Avionics LLC Address 3163 Airport Drive City Jamestown Zip 14701 Country USA 0 Model Serial No. (As described in Item 1 above) 6. Conformity Statement B. Kind of Agency State New York ✓ U. S Certificated Mechanic Foreign Certificated Mechanic Certificated Repair Station. Certificated Maintenance Organization Manufacturer C. Certificate No. DKZR372X 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 per 14 CFR Part 43 App. B Signature/Date of Authorized Individual 7. Approval 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 FAA Fit. Standards Inspector BY Manufacturer Repair Station Rejected Persons Approved by Canadian Department of Transport ☐ Approved Maintenance Organization Other (Specify) Inspection Authorization FAA Designee Certificate or Designation No. DKZR372X FAA Form 337 (10-06) Signature/Date of Authorized Individual F 10/23/14 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 mark and date work completed.) USA N34626 10/23/2014 Nationality and Registration Mark Date 1.) Removed a JP Instruments FS450 fuel flow gauge. Installed the following equipment: JP Instruments EDM800 engine analyzer IAW STC# SA2586NM. JP Instruments fuel flow option IAW STC# SA00432SE. 2.) The EDM800 interfaces to the EGT, CHT, oil temperature, oil pressure, outside air temperature and RPM sensors. The fuel flow interfaces to the gps(gtn650. Refer to the appropriate installation manual for interconnect information. 16.) When the ICA needs to be revised a letter will be submitted to the local FSDO with a copy of the revised FAA Form 337 and revised ICA. END Additional Sheets Are Attached FAA Form 337 (10-06) United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate This Certificate issued to Number SA2586NM J. P. INSTRUMENTS PO Box 7033 Huntington Beach, CA 92646 certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereen meets the airworthiness requirements of Part 3 of the Civil Aviation Regulations, including respective Amendments as specified in the attacked Approved. Model List. Original Product Type Certificate Number: Abake: * *See attached FAA Approved J.P. Instruments * Master Eligibility List No. SA2586NM for list Abodel: * of approved aircraft models and applicable TCDS Description of Type Design Change: Installation of J. P. Instruments temperature monitoring systems in accordance with FAA Approved J. P. Instruments Drawing List Report No. 100, Revision D, dated December 19, 1996, or later FAA approved revisions. FAA Approved Airplane/Rotorcraft Flight Manual Supplement No. 1 for EGT-701 temperature indicator, Revision A, dated December 13, 1996, or later FAA approved revisions. Limitations and Conditions: The approval of the change in type design applies to the basic airplane of the specific models that are otherwise unmodified. 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 installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of that airplane. 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. (See continuation sheet) This certificate and the supporting data which is the basis for approval shall remain in effect, until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application December 31, 1984 Date of issuance : .. FEDERAL August 14, 1985 AVIATION TOMINISTRATION Date reissued: Date amended: July 13, 1987, November 13, 1992, December 19, 1996, May 15, 1998, June 17, 1999 By direction of the Administrator Jon (Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title) 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 8110-2 (10-68) Page 1 of 3 This certificate may be transferred in accordance with FAR 21.47. United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA2586NM Limitations and Conditions - continued Cylinder head, oil, turbine inlet and/or exhaust gas temperature, fuel flow equipment, tachometer instruments, and manifold pressure instruments required by the original type design, or if required by other FAA approval, must remain installed and operable. Aircraft listed on the FAA approved Master Eligibility List SA2586NM and that have been previously modified with a fuel flow indication system that utilizes the Flowscan fuel flow transducer (P/N: 201-A, 201-B, 201-C, or 231 or equivalent as listed on page 4 of the FAA Approved Installation Instructions, Drawing 103) are eligible for installation of the EGT-701 fuel flow option. This certificate does not constitute installation approval of the fuel flow transducer. EGT-701 temperature indicator with tachometer (rpm) and manifold pressure options are eligible for the 4 cylinder and 6 cylinder engines listed on the Master Eligibility List (MEL) SA2586NM only. FAA Approved Airplane/Rotorcraft Flight Manual Supplement No. 1, Revision A, dated December 13, 1996 or later FAA approved revision, is required with the installation of the EGT-70 system. Eligible dash numbers for the EGT-701 are listed on MEL SA2586NM. A copy of this certificate must be maintained as part of the permanent records of the modified aircraft. -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 0110-2(10-68) Page 3 of 3 This certificate may be transferred in accordance with FAR 21.47.