04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015928 S-TEC CORPORATION EASA.IM.A.S.02064 REV. 1 FAA STC SA7198W-D BEECH 100 Installation of S-TEC Systems 65 Two Axis 1. Also eligible on Models 100, A100 and 17.10.2006 BEECH A100 Automatic Flight Guidance System, Model ST- B1000 when modified per STC SA3828NM BEECH B100 301 (Lower Aft Fuselage Strakes).2. Also eligible on Model A100 when modified per STC SA1679SO (750 S.H.P. Engines).3. Airplane Flight Manual Supplement, P/N 89827S, dated 9-29-89 is 10015996 S-TEC CORPORATION EASA.IM.A.S.02152 FAA STC SA09124AC-D PIPER PA-60-601P Installation of S-TEC 55/55X two axis 1. According to AFMS, Section 2 Operating 29.08.2006 PIPER PA-60-602P automatic flight control system in Aerostar Limitation2. Instructions for continued models airworthiness acc. Doc. P/N 81319 Rev. 23. Maintenance Instructions 2.-4. must be performed every 100 flight hours or once every calender year, whichever comes first 10016052 S-TEC CORPORATION EASA.IM.A.S.02224 FAA STC SA09262AC-D CESSNA 182Q CESSNA 182R CESSNA 182T Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance System, Model ST-718-20/30 in Cessna 182Q, 182R and T182, also when modified per STC SA1382WE (Robertson STOL) For 182Q the maximum aft c.g. is limited to 46.0 inches aft of datum when autopilot is installedInstaller must check availability of EASA-approval for Robertson STOL STC No. when aeroplane is modified per that STC 10016053 S-TEC CORPORATION EASA.IM.A.S.02225 FAA STC SA09218AC-D GRUMMAN GA-7 Installation of S-TEC System 55/55X Two Axis -- Automatic Flight Guidance System, Model ST- 661 in Grumman American GA-7 14.12.2006 10016054 S-TEC CORPORATION EASA.IM.A.S.02226 FAA STC SA09316AC-D CESSNA R182 Installation of S-TEC System 20/30 Single and This STC is approved only for the product 18.12.2006 CESSNA TR182 Two Axis Automatic Flight Guidance System, configuration as defined in the approved design Model ST-759-20/30 in Cessna R182, and data referred to in the paragraph "Description". TR182. Compatibility with other aircraft/engine configurations shall be determined by the installer. 10016080 S-TEC CORPORATION EASA.IM.A.S.02264 FAA STC SA09201AC-D CESSNA 172R Installation of S-TEC System 55/55X Two Axis This STC is approved only for the product 16.01.2007 CESSNA 172S Automatic Flight Guidance System, Model ST- configuration as defined in the approved design 563 in Cessna 172R and 172S data referred to in the paragraphs "Description" and “Associated Technical Documentation”. Compatibility with other aircraft/engine configurations shall be determined 10016103 S-TEC CORPORATION EASA.IM.A.S.02293 FAA STC SA09160AC-D PIPER PA-32-260 PIPER PA-32-300 PIPER PA-32R-300 10016146 S-TEC CORPORATION EASA.IM.A.S.02347 FAA STC SA09397CA-D PIPER PA-31 PIPER PA-31-300 PIPER PA-31-325 PIPER PA-31-350 Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST- 640 Installation of S-TEC System 65 Two Axis Automatic Flight Guidance System with Autotrim, Model ST-849, and with Optional Flight Director/Steering Horizon. 10016175 S-TEC CORPORATION EASA.IM.A.S.02403 FAA STC SA09139AC-D PIPER PA-44-180 Installation of S-TEC Manual Electric Trim System, Model ST-619, in above mentioned airplane Type / Variant 10016194 S-TEC CORPORATION EASA.IM.A.S.02431 FAA STC SA8886SW-D CESSNA 206 CESSNA P206 CESSNA P206A CESSNA P206D CESSNA P206E CESSNA TP206C CESSNA TP206D CESSNA TU206B CESSNA TU206C CESSNA TU206D CESSNA TU206E CESSNA TU206G CESSNA U206 CESSNA U206B CESSNA U206C CESSNA U206D CESSNA U206E CESSNA U206F CESSNA U206G This STC is also eligible on:- PA-31 and PA- 31-300 when modified per STC SA970SO,- PA-31-325 when modified per STC SA00048SE,- PA-31-350 when modified per STC SA1151SO and / or any of STC SA5796NW, STC SA00192SE, STC SA00039SE, STC SA00126SE.I Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.The installa Installation of S-TEC System 55/55X Two Axis This STC is also eligible on variants 206, P206, Automatic Flight Guidance System, Model ST- U206, P206A, TP206A, U206A, TU206A, 556 in above mentioned airplane Types / P206B, TP206B, U206B, TU206B, P206C, Variants, also when modified per STC as listed TP206C, U206C, TU206C, P206D, TP206D, in 3.5 (Limitations and Conditions) U206D, TU206D, P206E, TP206E, U206E, TU206E, U206F, and TU206F when converted to 28 Volt electri 04/01/2013 Page 430/462 14.12.2006 28.02.2007 23.02.2007 15.06.2007 05.07.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016196 S-TEC CORPORATION EASA.IM.A.S.02434 FAA STC SA09352AC-D Installation of S-TEC System, Model 20/30 This STC is eligible on variants M-5-210C, M-5- 03.07.2007 Single and Two Axis Automatic Flight Guidance 235C, M-6-235, MX-7-180, M-7-235, M-7- Systems, Model ST-810 235A, M-7-235B, M-7-235C and MX-7-235 in landplane, floatplane, or amphibian configuration.This STC is eligible on variants MX-7-180A, MX-7-180B, MX-7-180C, MXT-7- 180, MXT 10016203 S-TEC CORPORATION EASA.IM.A.S.02445 FAA STC SA09287AC-D PIPER 31 AND SERIES Installation of S-TEC System, Model 20/30 Prior to installation of this modification the 26.07.2007 PIPER PA-28R-180 Single and Two Axis Automatic Flight Guidance installer must determine that the PIPER PA-28R-200 Systems, Model ST-729 interrelationship between this modification and PIPER PA-28R-201T any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10016278 S-TEC CORPORATION EASA.IM.A.S.02567 FAA STC SA09251AC-D PIPER PA-28-161 PIPER PA-28-181 PIPER PA-28-236 10016317 S-TEC CORPORATION EASA.IM.A.S.02623 REV. 1 FAA STC SA09001AC-D CESSNA 310I CESSNA 310J CESSNA 310K CESSNA 310L CESSNA 310N CESSNA 310P CESSNA 310Q CESSNA 310R CESSNA T310P CESSNA T310Q CESSNA T310R 10016405 S-TEC CORPORATION EASA.IM.A.S.02734 FAA STC SA09298AC-D PIPER PA-31 PIPER PA-31-325 10016425 S-TEC CORPORATION EASA.IM.A.S.02763 FAA STC SA09132AC-D CESSNA 172M CESSNA 172N 10016442 S-TEC CORPORATION EASA.IM.A.S.02787 FAA STC SA09233AC-D PIPER PA-28-161 PIPER PA-28-181 PIPER PA-28-236 10016604 S-TEC CORPORATION EASA.IM.A.S.03019 FAA STC SA09257AC-D PIPER PA-28-140 PIPER PA-28-150 PIPER PA-28-160 PIPER PA-28-180 PIPER PA-28-235 10028097 S-TEC CORPORATION P- EASA.IM.A.S.03269 FAA STC SA5357SW-D PA-28-151, PA-28-161, PA-28-181, PA-28-236, PA-28-201T 10028331 S-TEC CORPORATION FAA STC SA09401AC-D (ST-853) 401, 401A, 401B 402A, 402B, 402C Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-703-20/30. This STC is also eligible on: - PA-28-151 when modified per STC SA2969SW (180 HP Engine Conversion)If airplane is modified per the above mentioned STC, installer must check availability of EASA-approval. Installation of S-TEC System 55/55X Two Axis This STC is also eligible on variants 310K, Automatic Flight Guidance System, Model ST- 310L, and 310N when modified per STC 594, also when modified per FAA STC as SA412SO (300 H.P. Colemill Conversion).This listed in 3.5 (Limitations and Conditions). STC is also eligible on variants T310P, and T310Q when modified per STC SA2750SW (RAM Modification.Installer must check availab Installation of S-TEC SYSTEM 55/55X Two This STC is also eligible on Models PA-31 Axis Automatic Flight Guidance System, Model when modified per STC SA970SO (350 hp ST-751, also when modified per FAA STC as Colemill Conversion)This STC is also eligible listed in 3.5 (Limitations and Conditions). on Model PA-31-325 when modified per STC SA00048SE (Vortex Generators System).Prior to installation of this modification the insta Installation of S-TEC System 55/55X Two Axis Prior to installation of this modification the Automatic Flight Guidance System, Model ST- installer must determine that the 612 in Cessna 172M and 172N. interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install Installation of S-TEC System 30 ALT Altitude Hold System, Model ST 684 (28 Volt System) Installation of S-TEC System 30 ALT Altitude Hold System, Model ST-712 (14 Volt System) Installation of S-TEC Manual Electric Trim System, Model ST-156 (14 VoltSystem) Installation of S-TEC System 55/55X Two Axis Automatic Flight GuidanceSystem, Model ST- 853 (28 Volt System) The approval holder shall fulfil the obligations of Part 21, Paragraph 21.A109 1 Prior to installation of this modification the installer must verify the availability of EASA approval for one or more mentioned STC(s) when the product is modified per that/those STC(s).1 Prior to installation of this modification the installer mu Compatibility of this modification with other previously approvedmodifications must be determined by the installer. The Approval of the installation of this system is not applicable tospecific aircraft having other previously approved modifications, unless Compatibility of this modification with other previously approvedmodifications must be determined by the installer.The Approval of the installation of this system is not applicable tospecific aircraft having other previously approved modifications, unlessi 22.10.2007 22.11.2007 22.05.2008 08.05.2008 13.05.2008 14.01.2009 Prior to installation of this modification it 01.12.2009 must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and / or repair will introduce no adverse effectupon the airworthiness of the product. Prior to installation of this modification it 17.12.2009 must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 04/01/2013 Page 431/462
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04/01/2013 Page 1/462 - EASA

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