04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10033951 S.E.A.M. FR182 STC 3005/10 rev 0 - Modification d'installation Limitation to Cessna FR182 equipped with Prior to installation of this modification it 22.02.2<strong>01</strong>1<br />
des équipements radio etBRNAV avec ASPEN EFD 1000 and NAVOMATIC300A. must be determined thatthe<br />
couplage au pilote automatique.<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 />
10035923 S.E.A.M. C90 Installation of a passenger information display,<br />
a Sigma-Tek 5000B-36attitude indicator, a<br />
Garmin GMA 340 audio panel, a Collins ADF-<br />
60Anavigation system, a Garmin GTX 330<br />
transponder, a Garmin G600 primaryand<br />
navigation system with coupling to automatic p<br />
10036296 S.E.A.M. P-<strong>EASA</strong>.A.S.03809 F90 STC 2465/08 Rev 5GNS530W TAWS -<br />
GNS530W - Radar GWX 68 - TAS KTA 870<br />
Installation.<br />
10036367 S.E.A.M. P-<strong>EASA</strong>.A.S.03923 F90 STC 2589/09 Rev 4Dual EFIS G600<br />
installation<br />
100373<strong>04</strong> S.E.A.M. P-<strong>EASA</strong>.A.S.03890 PA-44-180 Avionics upgrade including Aspen Electronic<br />
Flight Display (EFD) 1000Pro system and<br />
Garmin GNS 430 W with coupling to S-TEC<br />
55X automaticpilot<br />
100378<strong>04</strong> S.E.A.M. 1900, 1900C, 1900D, 200, 200C Installation of Garmin 500 Series system with<br />
coupling to autopilotRockwell-Collins FCS 80,<br />
according to SEAM modification file n.<br />
3541/11.<br />
10038255 S.E.A.M. F177RG Installation of a Garmin GNS 400 series<br />
system, a Garmin GA 35 or GA 56GPS<br />
antenna, a Mid Continent MD41 annunciator<br />
and a Garmin GTX 330transponder.<br />
10038454 S.E.A.M. BN-2 Installation of Garmin GNS 400 series system,<br />
GA 35 GPS antenna, GMX 200multifunction<br />
display, GMA 347 audio box, SL30 NAV/COM<br />
system, GTX 330transponder, Mld Continent<br />
MD 41 annunciator, Collins ALT<br />
50radioaltimeter and Indigo One Tracking<br />
system, accordi<br />
10038702 S.E.A.M. DR 400/180 STC 3725/11 rev. 0 dated <strong>04</strong>/<strong>01</strong>/2<strong>01</strong>2 -<br />
Amélioration équipements radionavB-RNAV<br />
This STC is limited to airplane s/n LJ-972.RNP<br />
APCH-VNAV and LPV Approach operations<br />
are not authorised.A third radionavigation or<br />
radiocommunication system independent<br />
fromGNS 430 W units must be<br />
installed.Mechanical instruments must be<br />
installed to back-<br />
Prior to installation of this modification it 27.07.2<strong>01</strong>1<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 />
Limitation to Beech F90 equipped with SPZ200 Prior to installation of this modification it 29.08.2<strong>01</strong>1<br />
autopilot and modifiedaccording SEAM STC must be determined thatthe<br />
2589/09 Dual G600 Installation.<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 />
Limitation to Beech F90 equipped with SPZ200 Prior to installation of this modification it 02.09.2<strong>01</strong>1<br />
autopilot and modifiedaccording SEAM STC must be determined thatthe<br />
2465/08 avionics installation.<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 />
1) This avionics installation if limited to aircraft Prior to installation of this modification it 17.11.2<strong>01</strong>1<br />
S/N 44-8095025 andit is approved for BRNAV, must be determined thatthe<br />
PRNAV and RNP Approach LNAV<br />
interrelationship between this modification<br />
operations.2) The only authorized mode for and any other previouslyinstalled<br />
GPS coupling to the S-TEC 55X automaticpilot modification and/ or repair will introduce<br />
(AP) is the NAV GPSS mode of the AP (activa no adverse effectupon the airworthiness<br />
of the product.<br />
Installation of this design change must be<br />
performed by SEAM technicalpersonnel. If the<br />
GNS 500 Series system is installed whereas<br />
another Garmin GNSsystem is already<br />
installed on the airplane, a third<br />
independentradiocommunication or<br />
radionavigation syst<br />
Installation of this design change must be<br />
performed by authorised SEAMtechnical<br />
personnel.The aircraft must be equipped with<br />
at least one radionavigation<br />
orradiocommunication mean not similar to the<br />
GNS 400 series unit.This installation is<br />
approved for us<br />
This design change must be installed by SEAM<br />
technical personnel.This installation as<br />
approved for use in BRNAV<br />
operations.Coupling of GNS system to<br />
autopilot is authorised only for CENTURY<br />
2000autopilot.Installation of software updates<br />
must be approved.In<br />
Prior to the installation of this modification<br />
it must be determinedthat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification and/or repair will introduce<br />
noadverse effect upon the airworthiness<br />
of the product.<br />
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 />
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 />
22.12.2<strong>01</strong>1<br />
<strong>01</strong>.02.2<strong>01</strong>2<br />
17.02.2<strong>01</strong>2<br />
S/N 2105 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.Install<br />
09.03.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 386/<strong>462</strong>
Change language