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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />

10<strong>04</strong>0972 TIMCO AEROSYSTEMS FAA STC NO. ST03928AT-D 777-300 Audio/Video On-Demand & In-seat Power none JADE/JAMCO STC ST02107SE-D must 10.08.2<strong>01</strong>2<br />

System Installation.<br />

be installed to or concurrently withthis<br />

STC.Prior to installation of this<br />

modification it must be determined<br />

thatthe interrelationship between this<br />

modification and any other<br />

previouslyinstalled modification and/ or<br />

repair<br />

10<strong>01</strong>5495 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>257 REV. 1 FAA STC ST03068AT-D BOEING 767-300 Cabin Standardization in accordance with This approval should not be extended to other<br />

<strong>01</strong>.12.2006<br />

TIMCO Master Data List 03T<strong>01</strong>2L0<strong>01</strong>, revision aircraft of this model on which other previoulsy<br />

D, dated November 30th, 2006, or later FAA approved modifications are incorporated<br />

approved revision.<br />

unless it is determined by the installer that the<br />

interrelationship between this change and any<br />

of those other previously<br />

10<strong>01</strong>5545 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>433 FAA STC ST03197AT BOEING 737-800 Complete interior reconfiguration in accordance 1. Compatibility of this design change with<br />

with TIMCO Aviation Services, Inc MDL, report other previously approved modifications must<br />

17.07.2006<br />

<strong>04</strong>T1<strong>01</strong>L0<strong>01</strong>, revision "C", dated December be determined by the installer.2. This STC is<br />

07, 2005, or later <strong>EASA</strong> approved revision approved only for the product configuration as<br />

defined in the approved design data referred to<br />

in the paragraph "De<br />

10<strong>01</strong>56<strong>01</strong> TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>537 FAA STC ST03107AT-D BOEING 767-300 Interior Reconfiguration 15.12.2005<br />

10<strong>01</strong>5636 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>592 FAA STC ST<strong>01</strong>929AT-D BOMBARDIER DHC-8-100<br />

SERIES<br />

BOMBARDIER DHC-8-200<br />

SERIES<br />

BOMBARDIER DHC-8-300<br />

SERIES<br />

Installation of Flight Data Recorder Expanded<br />

Parameters with a Plessey FDAU<br />

Limited to: 99T037C002 for DHC-8-<br />

100/20000T029C009 for DHC-8-<br />

300Maintenance required: pitch, roll and yaw<br />

position transducers and strings have to be<br />

detailed visually inspected and checked for<br />

smooth operation acc. MRB interval 2C<br />

10<strong>01</strong>5637 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>593 FAA STC ST03135AT-D BOEING 767-300 Installation of Rockwell Collins ACARS CMU-<br />

900<br />

28.11.2005<br />

10<strong>01</strong>5831 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>922 REV 1 FAA STC ST03372AT BOEING 767-300 Installation of Lower Lobe Crew Rest Module 1. This approval should not be extended to<br />

16.<strong>01</strong>.2008<br />

(CRM) and Main DeckVestibule in in<br />

other Aircraft of this model on which other<br />

accordance with Timco Master data List previously approved modifications are<br />

<strong>04</strong>T1<strong>04</strong>L0<strong>01</strong>, Rev H, dated December 7, 2007 incorporated unless it is determined by the<br />

or later approved revisions approved by <strong>EASA</strong> installer that the interrelationship between this<br />

in accordance with <strong>EASA</strong> ED Decision<br />

20<strong>04</strong>/<strong>04</strong>/CF (or<br />

change and any other previously ap<br />

10<strong>01</strong>5910 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.02037 FAA STC ST03107AT-D BOEING 767-300 Interior Reconfiguration 16.08.2006<br />

10<strong>01</strong>5974 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.02125 FAA STC ST03300AT-D AIRBUS A321 Installation of a doghouse (storage container) in Limitations and Conditions specified in FAA<br />

18.<strong>01</strong>.2007<br />

the bulk cargo compartment.<br />

STC ST03300AT-D remain applicable.<br />

10<strong>01</strong>5998 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.02155 FAA STC ST03342AT-D BOEING DC-9-87 (MD-87) Installation of a Door Safety Strap 1. TIMCO’s Instructions For Continued<br />

24.10.2006<br />

BOEING MD-88<br />

Airworthiness 06T005R<strong>01</strong>4, Rev. IR dated<br />

June 8, 2006, is a required part of this STC.2.<br />

This STC is approved only for the product<br />

configuration as defined in the approved design<br />

data referred to in the paragraph<br />

10<strong>01</strong>6002 TIMCO AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.02163 FAA STC ST<strong>01</strong>216AT-D AIRBUS A300 Installation of Airshow 210 System -- 08.10.2006<br />

10027196 TIMCO AVIATION SERVICES INC. FAA STC ST00696AT-D B747-400 Installation of Collins SAT-906 SatCom System None Prior to installation of this modification it 14.09.2009<br />

with Ball Antenna's inaccordance with Timco<br />

must be determined thatthe<br />

Master Data List MDL-<strong>01</strong>068, Revision M,<br />

interrelationship between this modification<br />

datedOctober 27, 1999 or later approved<br />

and any other previouslyinstalled<br />

revision.<br />

modification and/ or repair will introduce<br />

no adverse effectupon the airworthiness<br />

of the product.<br />

1003<strong>04</strong>07 TIMCO AVIATION SERVICES INC. FAA STC ST03820AT-D B767-300 Interior reconfiguration, B767-300Validation of<br />

FAA STC ST03820AT-D The aircraft will have<br />

the seating configuration changed to<br />

addadditional coach (Y) class seating,<br />

additional seat track installationwith associated<br />

structural modifications, removal of a<br />

10<strong>01</strong>4179 TMC AERO <strong>EASA</strong>.A.S.<strong>01</strong>316 AIRBUS A330-243 This STC deals with the installation of a TMC The approval of this modification is limited to<br />

stretcher. All documents related to this STC are the Airbus A330-243. the lmitations and<br />

listed in the STC form A330-25-23. The conditions defined in the <strong>EASA</strong> Datasheet are<br />

associated "Fiche de Modification" from<br />

Corsair is referenced 25-137 Rev. 1 ( or later<br />

<strong>EASA</strong>-approved revision )<br />

applicable.<br />

19.07.2006<br />

As per FAA STC ST03820AT-D Prior to installation of this modification it<br />

must be determined thatthe<br />

interrelationship between this modification<br />

and any other previouslyinstalled<br />

modification and/ or repair will introduce<br />

no adverse effectupon the airworthiness<br />

of the product.<br />

15.06.2<strong>01</strong>0<br />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 450/<strong>462</strong><br />

02.06.2005

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