EASA - J.P. Instruments

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EASAEuropean Aviation Safety Agency SUPPLEMENTAL TYPE CERTIFICATE 10051935 This Supplemental Type Certificate is issued by EASA, acting in accordance with Regulation (EC) No. 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation and in accordance with Commission Regulation (EU) No. 748/2012 to J.P. INSTRUMENTS, INC P.O.BOX. 7033 HUNTINGTON BEACH CA 92646 USA and certifies that the change in the type design for the product listed below with the limitations and conditions specified meets the applicable Type Certification Basis and environmental protection requirements when operated within the conditions and limitations specified below: Original Type Certificate Number: SEE EASA APPROVED MODEL LIST Type Certificate Holder : SEE EASA APPROVED MODEL LIST Type Design - Model : SEE EASA APPROVED MODEL LIST Original STC Number : FAA STC SAOI828SE Description of Design Change: Installation of J P Instruments (JPI) EDM-960 Primary Engine Data Management System. EASA Certification Basis: The Certification Basis (CB) for the original product remains applicable to this certificate! approval. The requirements for environmental protection and the associated certified noise and! or emissions levels of the original product are unchanged and remain applicable to this certificate! approval. See Continuation Sheet(s) For the European Aviation Safety Agency, Date of issue: 19 January 2015 Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033315-001 SUPPLEMENTAL TYPE CERTIFICATE - 10051935 - J.P. INSTRUMENTS, INC TE.STC.00091-003 - Copyright European Aviation Safety Agency. All rights reserved. 1/2 RIER Head of General Aviation and Remotely Piloted Aircraft Systems (RPAS) EASAEuropean Aviation Safety Agency Associated Technical Documentation: Installation in accordance with JPI Installation Manual for EDM-960, Report No 909, Revision NC, dated February 22,2009. Operate in accordance with JPI FAA approved Flight Manual Supplement No 960-001, dated March 27, 2009. or later revisions of the above listed documents approved by EASA in accordance with EASA ED Decision 2004/04/CF (or subsequent revisions of this decision)” and! or the Technical Implementation Procedures of EU! USA Bilateral Agreement. LimitationslConditions: Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and! or repair will introduce no adverse effect upon the airworthiness of the product. - end - Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033315-001 SUPPLEMENTAL TYPE CERTIFICATE - 10051935- J.P. INSTRUMENTS, INC TE.STC.00091-003 - copyright European Aviation Safety Agency. All tights reserved. 2/2 For the European Aviation Safety Agency, Date of Issue: 19 January 2015 Head of General Aviation Remotely Piloted Aircraft system (RPAS) J.P. INSTRUMENTS, INC — EASA Approved Model List (AML) Note: The following numbers are listed on the certificate: EASA current Project Number: 0060034291-001 STC APPROVAL — 10051935— JR INSTRUMENTS, INC 3,3 TYPE CERTIFICATION 1. AIRCRAFT MAKE AIRCRAFT MODEL CERTIFICATE BASIS FOR TEM NUMBER CHANGE PA-34-200, PA-34-200T, PA-34-220T 21. Piper Aircraft, Inc. EASA.IM.A.090 CAR 3 \lso PA-34-200T, PA-34-220T with STC SAI694NM 22. Piper Aircraft, Inc. PA-44-180, PA-44-180T EASA.IM.A.232 FAR 23 23. SOCATA, SA. GA-7 FR TCDS 190 FAR 23 500, 500-A, 500-B, 500-5, 500-U 24. Twin Commander 6A1 CAR 3 Also 500-S, 500-U with STC SA5969NM. Also 500-B, 500-S, 500-U with STC SAOII42SE or SAOI2I2SE or SAOOI69SE 25. Twin Commander 680FL, 685 2A4 CAR 3 26. Vulcanair S.p.A P68 Observer, P68 Observer 2, P680 EASA.A.385 FAR 23 J.P. INSTRUMENTS, INC — EASA Approved Model List (AML) Note: The following numbers are listed on the certificate: EASA current Project Number: 0060034291-001 STC APPROVAL — 10051935— J.P. INSTRUMENTS, INC ¶1 TYPE CERTIFICATION 1. AIRCRAFT MAKE AIRCRAFT MODEL CERTIFICATE BASIS FOR TEM NUMBER CHANGE 10. CESSNA T303 A34CE FAR 23 310, 3101, 310J, 310J-1, E31OJ, 310K, 310L, 3100, 310R, T31OP, T3OQ, T31OR 11. CESSNA Also 310G, 310H, 3101, 310J, 310K, 310L, 310N, 310P, 3100 with STC SA4I2SO. 3A10 CAR 3 Also T31OP, T31OQ, T31OR with STC SA275OSW. Also 310R, T3JOP, T31OQ, T31OR with STC SA2207S0 337, 337A, 3378, 337C, 337G, 337H, T337C, T337E, T337F, T337G, T337H, P337H 12. CESSNA Also T337G with STC SA45O4NM or SA0008OLA. Also 337G, 337H, T337H with A6CE FAR 23 STC SAO36I8AT. Also P337H with STC SA0008OLA. 335, 340, 340A 13 CESSNA 340 with SIC SA2346SW-D or SA3485 WE. Also 340A with STC SA7365SW-D or 3A25 CAR 3 . SA4241SW. Also 340, 340A with STC SA86O4SWor SA09574SC-D or SA8989SW-D or SA8O55SW-D or SA7975SW 14. CESSNA 404 A25CE FAR 23 401, 401A, 401 B, 4028, 402C, 414, 414A, 421, 421A, 421 B, 421C 15 CESSNA Also 414A with STC SAO9IO5SCorSA7633SWorSA82O4SW-DorSA8727SW-D A7CE CAR 3 . or SA8728SW-D or SA8I25SWor SA4546SW-D or SA4956NM or SA4943SW-D. Also 421C with STC SA5878SW Also 414 with STC SA09469SC-D or SA8424SW- D or SA8054$W..D or SA43T9SW-D or SA757OSW-D 16. DIAMOND DA42, DA42 NG, DA42 M-NG EASA.A.005 FAR 21.29 PA-23-235, PA-23-250 17. Piper Aircraft, Inc. 1AIO CAR 3 PA-30, PA-39, PA-40 18. Piper Aircraft, Inc. AIEA CAR 3 Also PA-30, PA-39 with STC SAI239SW PA-31, PA-31-325, PA-31-350 CAR 3 19. Piper Aircraft, Inc. A2OSO FAR 23 Also PA-31, PA-31-325 with STC SA97OSO 20. Piper Aircraft,