A319 EASA STC 10052076_CERT_REV_0_20150129

Feb 2, 20151 like867 views

The European Aviation Safety Agency (EASA) issued Supplemental Type Certificate 10052076 to Tempus Jet Centers II, LLC. This certificate approves the installation of a VIP interior modification for the Airbus A379-115 aircraft, originally certified under EASA.A.064. The certification basis and environmental requirements for the original aircraft remain applicable. The approval is subject to prior installation of EASA STC EASA.A.S.00375 and limitations specified in the associated technical documentation.

EASAEuropean Aviation Safety Agency
SUPPLEMENTAL TYPE CERTIFICATE
10052076
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
TEMPUS JET CENTERS II, LLC.
133 WALLER MILL ROAD
WILIAMSBURG VA 23185
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 : EASA.A.064
Type Certificate Holder : AIRBUS
Type Design - Model : A379-115
Original STC Number : FAA STC ST02481 LA
Description of Design Change:
Installation of a VIP Interior Modification
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: 29 January 2015
Note:
The following numbers are listed on the certificate:
EASA current Project Number: 0010033376-001
SUPPLEMENTAL TYPE CERTIFICATE - 10052076- TEMPUS JET CENTERS II, LLc.
TE.STC.00091-003-Copynght European Aviation Safety Agency. All rights reserved.
1/2
Alain LEROY
Head of Large Aeroplanes Department

EASAEuropean Aviation Safety Agency
Associated Technical Documentation:
FAA Supplemental Type Certificate ST02481 LA issued on July 17,2014
Master Data List 8425ED-MDL Rev. F, dated June 25, 2014
Airplane Flight Manual Supplement 8245-EM-AFMS Rev. A, dated June 25, 2014
Instructions for Continued Airworthiness 8425-ICA Rev. lR, dated August 4, 2013
FAA Part 25 I EASA CS 25 Compliance Assessment, dated November 20, 2014
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.
Limitations/Conditions:
EASA STC EASA.A.S.00375 must be installed prior to installation of the present airworthiness
approval
- end -
Note:
The following numbers are listed on the certificate:
EASA current Project Number: 0010033376-001
SUPPLEMENTAL TYPE CERTIFICATE - 10052076- TEMPUS JET CENTERS II, LLC.
TE.STC.00091-003 - Copyright European Aviation Safety Agency. All rights reserved.
2/2

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A319 EASA STC 10052076_CERT_REV_0_20150129

1. EASAEuropean Aviation Safety Agency SUPPLEMENTAL TYPE CERTIFICATE 10052076 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 TEMPUS JET CENTERS II, LLC. 133 WALLER MILL ROAD WILIAMSBURG VA 23185 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 : EASA.A.064 Type Certificate Holder : AIRBUS Type Design - Model : A379-115 Original STC Number : FAA STC ST02481 LA Description of Design Change: Installation of a VIP Interior Modification 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: 29 January 2015 Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033376-001 SUPPLEMENTAL TYPE CERTIFICATE - 10052076- TEMPUS JET CENTERS II, LLc. TE.STC.00091-003-Copynght European Aviation Safety Agency. All rights reserved. 1/2 Alain LEROY Head of Large Aeroplanes Department

2. EASAEuropean Aviation Safety Agency Associated Technical Documentation: FAA Supplemental Type Certificate ST02481 LA issued on July 17,2014 Master Data List 8425ED-MDL Rev. F, dated June 25, 2014 Airplane Flight Manual Supplement 8245-EM-AFMS Rev. A, dated June 25, 2014 Instructions for Continued Airworthiness 8425-ICA Rev. lR, dated August 4, 2013 FAA Part 25 I EASA CS 25 Compliance Assessment, dated November 20, 2014 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. Limitations/Conditions: EASA STC EASA.A.S.00375 must be installed prior to installation of the present airworthiness approval - end - Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033376-001 SUPPLEMENTAL TYPE CERTIFICATE - 10052076- TEMPUS JET CENTERS II, LLC. TE.STC.00091-003 - Copyright European Aviation Safety Agency. All rights reserved. 2/2

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A319 EASA STC 10052076_CERT_REV_0_20150129

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