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 10015557 S-TEC CORPORATION EASA.IM.A.S.01454 REV. 1 FAA STC SA5302SW-D CESSNA 210 Installation of S-TEC System 40/50 Single and 1. As defined in the Limitations and Conditions 09.09.2008 Two Axis Automatic Flight Guidance System, section of FAA STC SA5302SW-D, latest Model ST-212-40/50, according to Bulletin No approved revision2. Prior to installation of this 312, dated 3-21-88 or later approved revisions modification the installer must determine that the interrelationship between this modification andany other previously i 10015558 S-TEC CORPORATION EASA.IM.A.S.01455 REV 1 FAA STC SA09628AC TWIN COMMANDER AIRCRAFT 690C TWIN COMMANDER AIRCRAFT 690D TWIN COMMANDER AIRCRAFT 695 TWIN COMMANDER AIRCRAFT 10015559 S-TEC CORPORATION EASA.IM.A.S.01456 FAA STC SA5242SW-D 695A AERMACCHI F 260 B AERMACCHI F 260 C AERMACCHI F 260 D Installation of S-TEC/Meggitt MAGIC 01298-07- 01-005 Digital Flight Control SystemFAA STC SA09628AC 10015588 S-TEC CORPORATION EASA.IM.A.S.01499 FAA STC SA09239AC-D CESSNA F172-N Installation of S-TEC System 20/30 Single and tow Axis Automatic Flight Guidance Systems 10015604 S-TEC CORPORATION EASA.IM.A.S.01540 REV. 1 FAA STC SA7209SW-D CESSNA 337D CESSNA 337E CESSNA 337F CESSNA 337G CESSNA 337H CESSNA P337H CESSNA T337D CESSNA T337E CESSNA T337F CESSNA T337G CESSNA T337H CESSNA T337H-SP 10015606 S-TEC CORPORATION EASA.IM.A.S.01541 REV. 1 FAA STC SA7210SW-D REIMS AVIATION F-337E REIMS AVIATION F-337F REIMS AVIATION F-337G REIMS AVIATION F-337H REIMS AVIATION FT-337E REIMS AVIATION FT-337F REIMS AVIATION FT-337GP REIMS AVIATION FT-337HP 10015633 S-TEC CORPORATION EASA.IM.A.S.01589 FAA STC SA7805SW-D PIPER PA-28R-180 PIPER PA-28R-200 PIPER PA-28R-201 PIPER PA-28R-201T 10015634 S-TEC CORPORATION EASA.IM.A.S.01590 FAA STC SA7815SW-D PIPER PA-23 PIPER PA-23-160 10015669 S-TEC CORPORATION EASA.IM.A.S.01645 REV 1 FAA STC SA09214AC-D CESSNA 172R CESSNA 172S 10015783 S-TEC CORPORATION EASA.IM.A.S.01839 FAA STC SA09522AC-D BEECH 95 BEECH B95A BEECH D95A BEECH E95 Airplane with S-TEC/Meggit 01298-07-01-005 Digital Flight Control System is prohibited from flight into known icing condition. STC SA01627CH, Meggit EFIS installation is required for this modification. Compatibility of this design with previously approved Installation of S-TEC System 40/50, Single and 1. Only eligible on model F260B when Two Axis Automatic Flight Guidance Systems equipped with Aileron Assemblies P/N SF260- Model ST-235-40/50FAA STC SA5242SW-D 02-05-01 (L.H.) and P/N SF260-02-05-02 (R.H.)2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragrap Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System with Optional Autotrim System, Model ST-314, according toBulletin No 414, dated 3-14-90 or later approved revision Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System with Optional Autotrim System, Model ST-314, according toBulletin No 414, dated 3-14-90 or later approved revisions. Installation of S-TEC Manual Trim System (field installation) i.a.w. MDL 92549 Rev A STC SA7815SW-D, Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-486 Installation of S-TEC System 30 ALT Altitude Hold Sytem, Model ST-673, according to Bulletin No 773, Revision 4 dated 9-22-98 or later approved revision Also eligible on the above models when modified by 180 HP Engine conversion. EASA approval of this STC must be ckecked.This STC is issued as result of the validation of the S-TEC Corporation STC No SA09239AC-D approved by the FAA on June 26, 1997. 1. Eligble when above models are modified per FAA STC SA1627WE (Robertson STOL Conversion)2. Eligible when the above models are modified per FAA STC SA937CE (Horton STOL Craft Conversion)3. It is the operator's responsibility to ensure the above mentioned 1. Eligible when the above models are modified per FAA STC SA1627WE (Robertson STOL Conversion).2. Eligible when the above models are modified per FAA STC SA937CE (Horten STOL Craft Conversion).3. It is the operators responsibility to ensure the a Limited to Installations without the trim monitor system 1. Eligible on models modified per STC SA504WE and/or STC SA824WE.2. Eligible on models modified per STC SA461SW, SA636SW, SA671SW and 899SW3. Instructions for continued airworthiness acc. Doc. P/n 81431 5. Maintenance Instructions 2.- 4. must be performed This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. Installation of S-TEC System 55/55X Two Axis FAA/DAS Approved Pilot’s Operating Automatic Flight Guidance System, Model ST- Handbook and / or FAA Approved Airplane 898. Flight Manual Supplement P/N 892113 dated 2- 18-02 or later approved revision, is required for Beech models 95 and B95.FAA/DAS Approved Pilot’s Operating Handbook and / or FAA Approv 04/01/2013 Page 428/462 17.10.2006 13.03.2006 04.08.2005 12.09.2008 09.09.2008 30.01.2006 17.02.2006 10.09.2008 17.10.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015784 S-TEC CORPORATION EASA.IM.A.S.01840 FAA STC SA8908SW-D CESSNA 335 Installation of S-TEC System 55/55X Two Axis Eligible to be used on aircraft 340 and 340A 26.09.2006 CESSNA 340 Automatic Flight Guidance System, Model ST- when modified per FAA STC SE4327SW CESSNA 340A 575 (RAM Engine Conversion only if this STC has been EASA approved. 10015786 S-TEC CORPORATION EASA.IM.A.S.01842 REV 1 FAA STC SA09000AC-D VULCANAIR P68 B Installation of S-TEC System 55 two axis 1. Also eligible on the above models with 10.09.2008 VULCANAIR P68 C automatic flight guidance system, model ST- Camera Port2. This STC is approved only for VULCANAIR P68 C-TC 585, in accordance with FAA STC SA the product configuration as defined in the 09000AC-D approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations 10015801 S-TEC CORPORATION EASA.IM.A.S.01866 FAA STC SA09527AC-D TWIN COMMANDER AIRCRAFT Installation of S-TEC Digital Flight Control If airplane is modified by STC SA236CH 20.10.2006 690 System (autopilot) Part Numbers 01284 or (Garrett TPE 331-10T-515 engines), STC TWIN COMMANDER AIRCRAFT 01298-01-01-002 or 01-304-04-01-008, SA3861NM ("Q" tip propellers), or STC 690A (MAGIC 2100) (ST-902) in Twin Commander SA1359GL (winglets), installer must check TWIN COMMANDER AIRCRAFT 690, 690A and 690B, also if modified by any of availability of EASA-approval. 690B the following STC’s: STC SA236CH (Garrett TPE 10015802 S-TEC CORPORATION EASA.IM.A.S.01867 REV. 1 FAA STC SA09007AC-D CESSNA 182P Installation of S-TEC System 55/55X Two Axis This STC is approved only for the product 10.09.2008 CESSNA 182Q Automatic Flight Guidance System Model ST- configuration as defined in the approved design 587. data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10015804 S-TEC CORPORATION EASA.IM.A.S.01869 FAA STC SA09008AC-D CESSNA F182-P Installation of S-TEC System 55/55X Two Axis 26.04.2006 CESSNA F182-Q Automatic Flight Guidance System Model ST- 587. 10015827 S-TEC CORPORATION EASA.IM.A.S.01916 FAA STC SA5125SW-D PIPER PA-28R-180 Installation of S-TEC System 60 Two Axis 1. FAA Approved Supplement to Pilot’s 11.10.2006 PIPER PA-28R-200 Automatic Flight Guidance System, Model ST- Operating Handbook and / or FAA Approved PIPER PA-28R-201 137, with Optional Autotrim System. Airplane Flight Manual, P/N 89176-1, dated 06- PIPER PA-28R-201T 21-90,or later approved revision, is required for Piper Models PA-28R-201 and PA-28R- 201T.2. FAA Approved Supplement to Pilot’s Ope 10015901 S-TEC CORPORATION EASA.IM.A.S.02027 FAA STC SA9232AC-D CESSNA 210G Installation of S-TEC System 20/30 Single and 1. Also eligible on Models T210G, T210H and 27.06.2006 CESSNA 210H Two Axis Automatic Flight Guidance System, T210J when modified per FAA STC CESSNA 210J Model ST-687-20/30 SA2689SW (RAM Modification)2. FAA/DAS CESSNA T210G Approved Suppllemental Flight Maual, P/N CESSNA T210J 891412, dated 30 May 1997, is required for Cessna Models 210G, T210G, 210H, T210H, 210J and T210J and 10015902 S-TEC CORPORATION EASA.IM.A.S.02028 FAA STC SA09237AC-D CESSNA 172M Installation of S-TEC System 20/30 Single and 1) Also eligible on the above models when 26.06.2006 CESSNA 172N Two Axis Automatic Flight Guidance Systems, modified by 180 H.P. Engine Conversion.2) Model ST-674-20/30 FAA/DAS Approved Supplemental Flight Manual, P/N 891423, dated 16 June 1997 is required for S-TEC System 20 for Cessna Model 172M and the above model when modified by 180 H 10015905 S-TEC CORPORATION EASA.IM.A.S.02031 FAA STC SA09313AC-D BEECH A35 Installation of S-TEC System 20/30 Single and Also eligible on Model 35 when modified per 12.06.2006 BEECH B35 Two Axis Automatic Flight Guidance Systems, STC SA1-460 (Auxiliary Wing Tip Fuel BEECH C35 Model ST-757-20/30 Tanks).FAA/DAS approved supplemental flight BEECH D35 manual, P/N 89160, dated 12-05-97 is required BEECH E35 for Beech model 35 and this model when BEECH F35 modified per STC SA1-460 (Auxiliary Wing Tip BEECH G35 F 10015922 S-TEC CORPORATION EASA.IM.A.S.02055 FAA STC SA09009AC-D CESSNA 182E Installation of S-TEC System 55/55X Two Axis FAA/DAS Approved Supplemental Flight 19.10.2006 CESSNA 182F Automatic Flight Guidance System, Model ST- Manual, Part No. 891174, Rev. 2, dated 6-11- CESSNA 182G 588 in Cessna 182E, 182F, 182G, 182H, 01, or later approved revisions, is required for CESSNA 182H 182J,182K, 182L, 182M, and 182N, also when Cessna Models 182E, 182F, and CESSNA 182J modified per STC SA1382WE (Robertson 182G.FAA/DAS Approved Supplemental Flight CESSNA 182K STOL) Manual, Part No. 891175, Rev. 2, dated 6-11- CESSNA 182L CESSNA 182M CESSNA 182N 01, or lat 10015927 S-TEC CORPORATION EASA.IM.A.S.02063 REV. 1 FAA STC SA7199SW-D BEECH 100 Installation of S-TEC Yaw Damper System, 1. Also eligible on Models 100 and B1000 17.10.2006 BEECH A100 Model ST-302 when modified per STC SA3823NM (Lower Aft BEECH B100 Fuselage Strakes).2. Also eligible on Model A1000 when modified per STC SA3828NM (Lower Aft Fuselage Strakes) with or without STC SA16779SO (750 S.H.P. Engines).3. Flight Ma 04/01/2013 Page 429/462
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04/01/2013 Page 1/462 - EASA

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