04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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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>01</strong>5753 TRIAD INTERNATIONAL MAINTENANCE <strong>EASA</strong>.IM.A.S.<strong>01</strong>786 FAA STC ST03200AT BOEING 737-800 Complete interior reconfiguration in accordance<br />
with TIMCO Aviation Services, Inc MDL, report<br />
<strong>04</strong>T1<strong>01</strong>L500, revision “D”, dated December 08,<br />
2005, or later <strong>EASA</strong> approved revision<br />
20.07.2006<br />
10029274 TRIUMPH INSTRUMENTS BURBANK Inc. <strong>EASA</strong>.IM.A.S.03255 REV. 1 FAA STC ST02236LA CL-600-2B19, CL-600-2C10<br />
CL-600-2D15, CL-600-2D24<br />
Triumph Replacement Hydraulic Accumulators. None. 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 />
17.03.2<strong>01</strong>0<br />
10034472 TRIUMPH INSULATION SYSTEMS, L.L.C. REV. 1 FAA STC ST02<strong>01</strong>3LA B767-200 Insulation Blanket Installation None 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 />
11.<strong>04</strong>.2<strong>01</strong>1<br />
10026913 TROLLTUNE CORPORATION P-<br />
<strong>EASA</strong>.IM.A.S.03179<br />
FAA STC SA03608AT 182P AND 182Q (SEE<br />
ATTACHMENT)<br />
Increased Maximum Gross Takeoff Weight<br />
(MGTOW). This STC allows a 150 lbIncrease<br />
in MGTOW from 2950 to 3100 lbs. There is no<br />
change to themaximum landing weight of 2950<br />
lbs.<br />
10<strong>01</strong>3953 TROYES AVIATION <strong>EASA</strong>.A.S.0<strong>04</strong>93 REV. 2 CESSNA F177-RG Installation of sliding panel on the front left and<br />
right door windows amd rear right<br />
window.Addition of new S/N 087 F-BURU on<br />
None. 1. Prior to installation of this modification 21.08.2009<br />
the installer mustdetermine that the<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product.2. The insta<br />
Limited to F177RG S/N <strong>01</strong>12, 0065 and S/N<br />
087 F-BURU.<br />
10<strong>01</strong>3954 TROYES AVIATION <strong>EASA</strong>.A.S.0<strong>04</strong>94 REV. 3 CESSNA F177RG<br />
STC <strong>EASA</strong>.A.S.0<strong>04</strong>93.<br />
Installation of a camera sight door under the Applicability F177RG S/N <strong>01</strong>12, 0065, 103, The approval holder shall fulfil the 29.03.2<strong>01</strong>0<br />
fuselage.Addition of new aircraft to STC<br />
<strong>EASA</strong>.A.S.0<strong>04</strong>94 Revision 2.<br />
087 F-BURU and S/N 51 F-HBAG.<br />
obligations of Part 21,Paragraph21.A109.<br />
10<strong>01</strong>4266 TROYES AVIATION <strong>EASA</strong>.A.S.<strong>01</strong>495 REV. 3 REIMS CESSNA F177-RG Provisions for three attachments in the right Limited to: F177RG S/N <strong>01</strong>12, 0065, 103, 153 1) Prior to installation of this modification 06.10.2009<br />
side of the instrumentpanel in accordance with and 087 F-BURU; S/N 051D-EMEN<br />
the installer mustdetermine that the<br />
the STC <strong>EASA</strong>.A.S.<strong>01</strong>495R1: adjunction of a<br />
interrelationship between this modification<br />
newserial number "S/N 051"<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product. 2) The inst<br />
10<strong>01</strong>4285 TROYES AVIATION <strong>EASA</strong>.A.S.<strong>01</strong>522 CESSNA 340A FAM n° 47 - Limitation of MTOW to 2699 kg s/n 340A-<strong>04</strong>51 23.02.2006<br />
10<strong>01</strong>4642 TSA TRANSAIRCO S.A. <strong>EASA</strong>.A.S.02792 PILATUS PC-12<br />
PILATUS PC-12/45<br />
PILATUS PC-12/47<br />
AFT Refreshment Galley and OvenRefer to<br />
master certification documents list TS PC12-<br />
25.30.02MCL<br />
10<strong>01</strong>5718 TTF AEROSPACE, LLC <strong>EASA</strong>.IM.A.S.<strong>01</strong>716 FAA STC ST00231BO BOEING 737-800 Installation of Yokohama forward Lavatory E<br />
and Yokohama aft lavatory K and attendant<br />
seat in accordance with TTF Aerospace MDL<br />
TTF-05T026-<strong>01</strong> Rev B, dated February 24,<br />
2006<br />
1. Limited to serial number 321 and later;2.<br />
Galley power and microwave oven use is not<br />
approved during take-off and landing phases of<br />
flight and during emergency or abnormal<br />
procedures;3. When aft refreshment galley is<br />
installed, the luggage area<br />
Limited to installation on Boeing 737-800 S/N<br />
28325, 3<strong>04</strong>70, 32277 and 32278<br />
only.Installation of FAA STC <strong>01</strong>533LA<br />
requiredInstruction for airworthiness 9ICA, TTF<br />
Aerospace Document TTF-05T026-18 revision<br />
new, dated February 13, 2006 or later FAA<br />
accepted re<br />
10<strong>01</strong>6453 TTF AEROSPACE, LLC <strong>EASA</strong>.IM.A.S.02799 FAA STC ST<strong>01</strong>195SE BOMBARDIER DHC-8-100<br />
SERIES<br />
BOMBARDIER DHC-8-200<br />
SERIES<br />
BOMBARDIER DHC-8-300<br />
SERIES<br />
Installation of a Reinforced Flight Deck Door. 16.06.2008<br />
10<strong>01</strong>5250 TUIFLY GmbH <strong>EASA</strong>.A.S.03692 B737-800 Cabin Configuration Change to 52BC plus 6YC Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
05.11.2008<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 452/<strong>462</strong><br />
28.02.2008<br />
21.11.2006<br />
06.<strong>04</strong>.2006