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>4920 BAYO S.A.S. <strong>EASA</strong>.A.S.03167 CESSNA 177RG STC 42/2007 - Modification of radio electric 1. Aircraft must be equipped with HSI<br />
08.02.2008<br />
installation for B-RNAV certification with AP KI525A and S-TEC 60-2 autopilot;2. Prior to<br />
coupling.<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification and any other previously<br />
installed modification will<br />
10<strong>01</strong>5<strong>01</strong>0 BAYO S.A.S. <strong>EASA</strong>.A.S.03312 CESSNA 182J 54/2006 - IFR BRNAV certification extension of STC Bayo 27/2006 must be already<br />
the GNS430 without Autopilot coupling. installed.The Aircraft must be equipped with<br />
HSI KI525A.<br />
10<strong>01</strong>5098 BAYO S.A.S. <strong>EASA</strong>.A.S.03439 REV. 1 FAIRCHILD SWEARINGEN SA<br />
226-T<br />
10<strong>01</strong>5138 BAYO S.A.S. <strong>EASA</strong>.A.S.03491 FAIRCHILD SWEARINGEN SA<br />
226-T<br />
Modification of radio electrical Installation2 VHF The approvam is limited to MSN T-276 F-<br />
21A, 2VOR/ILS/MKR VIR 30A, 2 ATC TDR GLLOGPS use is forbidden for<br />
90, 1 RMI 30 removal2GNS 430 W, 2 MD 41, SID/STAR/ApproachesGPS/Auto Pilot<br />
2 A-30 ACK, 2GTX 330D, 1 KA-33, 1 ST3400 coupling is forbidden below 2000 ft.<br />
Installation<br />
Modification of radio electrical installation:<br />
replacement radar indicator by MFD Garmin<br />
GMX200 and/or Concord Batteries.<br />
1. The approval is limited to MSN T-276 F-<br />
GLLO;2. Use of GMX 200 limited to radar<br />
weather display function;3. Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification and any othe<br />
10<strong>01</strong>5179 BAYO S.A.S. <strong>EASA</strong>.A.S.03557 PIPER PA-25-235 Modification of radio electrical<br />
Limited to S/N 25-74-05726, 25-3109, 25- Prior to installation of this modification the 21.<strong>01</strong>.2009<br />
installation.Installation of AG-NAV2 GPS 37<strong>04</strong>, 25-3984, 25-4382, 25-3292,25-2400, 25- installer must determinethat the<br />
spreading guidance system not to be used for 4445.<br />
interrelationship between this modification<br />
navigation, in accordance with "Fiche<br />
and any otherpreviously installed<br />
d'approbation de conception d'une évolution<br />
modification will introduce no adverse<br />
No. 53/2007, rev.3 dated 12/12/08".<br />
effect uponthe airworthiness of the<br />
product. The installati<br />
10<strong>01</strong>5220 BAYO S.A.S. <strong>EASA</strong>.A.S.03635 BEECH 58 Modification of radio electrical installation for B- The applicability of this STC is limited to the<br />
14.11.2008<br />
RNAV certification with AP coupling<br />
Beech 58 S/N TH-488Navigation on SID and<br />
STARs prohibited in Terminal AreaUtilisation of<br />
GPS prohibited for approachesPrior to<br />
installation of this modification the installer must<br />
determine that the interrela<br />
10<strong>01</strong>7122 BAYO S.A.S. <strong>EASA</strong>.R.S.<strong>01</strong>209 EUROCOPTER FRANCE AS<br />
365N SERI<br />
10032968 BAYO S.A.S. STC 2<strong>01</strong>0-006 HR 100/200, HR100/200 B<br />
HR 100/210, HR 100/210 D<br />
HR 100/285 TIARA<br />
HR100/250 TR, HR 100/285 C<br />
10<strong>01</strong>5726 BAYSYS TECHNOLOGIES, LLC <strong>EASA</strong>.IM.A.S.<strong>01</strong>741 FAA STC ST<strong>01</strong>939LA AIRBUS A319-115<br />
AIRBUS A319-133<br />
BAYO avionics modification no. 16/2005: This STC can be installed only by BAYO<br />
installation of- two NAV/COM/GPS GNS 430 technical personal in accordance with BAYO<br />
for IFR B-RNAV operations, with their STC definition file n°16/2005-DEF, revision 0,<br />
associated MD 41 annunciators, A-30 ACK dated December 19th 2005 or later <strong>EASA</strong><br />
altitude encoders and KA 33cooling system,- a approved revision<br />
Garmin GTX 330 mode S transponder,- two<br />
Bendix-King<br />
Installation of single EFIS Aspen EFD1000 Pro<br />
for VFR navigation.<br />
Direct TV - Installation of a tailwind 55 Satellite<br />
direct TV receive system<br />
Approved software version for ACU and PFD<br />
units is 1.1.Navigation coupling to automatic<br />
pilot is limited to heading mode.<br />
1. Maximum Tekeoff Weight and Maximum<br />
Landing Weight shall be reduced as<br />
follows:Takeoff 350 lbs (159 Kg)Landing 410<br />
lbs (186 Kg)2. For airplane(s) modified by this<br />
STC, prior to the accumulation of 9,200 total<br />
flight cycles from the STC modification, the<br />
10<strong>01</strong>3982 BBJ DESIGN SERVICES LIMITED <strong>EASA</strong>.A.S.<strong>01</strong><strong>01</strong>4 AIRBUS A320-200 Reconfiguration of Passenger Cabin to 180<br />
Economy Class Passengers<br />
10<strong>01</strong>3985 BBJ DESIGN SERVICES LIMITED <strong>EASA</strong>.A.S.<strong>01</strong><strong>01</strong>7 REV. 1 BOEING 737-700<br />
Installation of 44 Passenger Seats, seats<br />
BOEING 737-800<br />
power supply and in seat power supply system<br />
on Boeing-BBJ128 Reynard J2000 double<br />
seats,safety equipment, carpet and new<br />
wardrobes. Installation of General Dynamics In<br />
Seat Power System.<br />
10<strong>01</strong>3986 BBJ DESIGN SERVICES LIMITED <strong>EASA</strong>.A.S.<strong>01</strong><strong>01</strong>8 Floor Structure rework. 1. This STC is restricted to Boeing 767-3Z9<br />
Registration G-VKNG, Serial Number 23765.2.<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other airc<br />
24.<strong>01</strong>.2008<br />
05.03.2008<br />
08.<strong>04</strong>.2008<br />
19.<strong>01</strong>.2006<br />
Prior to installation of this modification it 10.12.2<strong>01</strong>0<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.Install<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 110/<strong>462</strong><br />
23.11.2006<br />
17.<strong>01</strong>.2005<br />
24.10.2005<br />
08.06.2005