P.O.BOX. 7033
11
EASA European Aviation Safety Agency SUPPLEMENTAL TYPE CERTIFICATE 10051939 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 Description of Design Change: Installation of J P Instruments (JPI) 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 Head of G neral Aviation and Remotely Piloted Aircraft Systems (RPAS) Note; The following numbers are listed on the certificate: EASA current Project Number: 0010033200-001 SUPPLEMENTAL TYPE CERTIFICATE - 10051939 - J.P. INSTRUMENTS, INC TE.STC.00091-003 - Copyright European Aviation Safety Agency. AN rights reserved. 1/2
Transcript of P.O.BOX. 7033
EASAEuropean Aviation Safety Agency
SUPPLEMENTAL TYPE CERTIFICATE
10051939
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 thirdcountries that participate in the activities of EASA under Article 66 of that Regulation and inaccordance with Commission Regulation (EU) No. 748/2012 to
J.P. INSTRUMENTS, INC
P.O.BOX. 7033HUNTINGTON BEACH CA 92646
USA
and certifies that the change in the type design for the product listed below with the limitations andconditions specified meets the applicable Type Certification Basis and environmental protectionrequirements when operated within the conditions and limitations specified below:
Original Type Certificate Number: SEE EASA APPROVED MODEL LISTType Certificate Holder : SEE EASA APPROVED MODEL LIST
Type Design - Model : SEE EASA APPROVED MODEL LIST
Description of Design Change:Installation of J P Instruments (JPI) 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 emissionslevels 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
Head of G neral Aviation andRemotely Piloted Aircraft Systems (RPAS)
Note;The following numbers are listed on the certificate:EASA current Project Number: 0010033200-001
SUPPLEMENTAL TYPE CERTIFICATE - 10051939 - J.P. INSTRUMENTS, INC
TE.STC.00091-003 - Copyright European Aviation Safety Agency. AN rights reserved.
1/2
EASAEuropean Aviation Safety Agency
Associated Technical Documentation:Installation in accordance with JPI Installation Manual for the EDM 900/930, Report 908, datedSeptember 9, 2004.Operation in accordance with JPI Flight Manual Supplement ref EDM-900 and EDM-930, PrimaryEngine Data Management System, dated December 10,2004, Document Numbers 900-0001 and930-0001 Rev C respectively.or later revisions of the above listed documents approved by EASA in accordance with EASA EDDecision 2004/04/CF (or subsequent revisions of this decision)” and! or the TechnicalImplementation Procedures of EU! USA Bilateral Agreement.
Limitations!Conditions:Prior to installation of this design change it must be determined that the interrelationship between thisdesign change and any other previously installed design change and! or repair will introduce noadverse effect upon the airworthiness of the product.
- end -
Note:The following numbers are listed on the certificate:EASA current Project Number: 0010033200-001
SUPPLEMENTAL TYPE CERTIFICATE - 10051939- J.P. INSTRUMENTS, INC
TE.STC.00091-003 - Copyright European Aviation Safety Agency. All tights reserved.
2/2
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0519
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