04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10015362 S-TEC CORPORATION EASA.IM.A.S.00676 REV. 2 FAA STC SA09254AC-D PIPER PA-28-140
Installation of S-Tec System 20/30 Single and 1. Limitation according FAA STC SA09254AC-
11.09.2008
PIPER PA-28-150
Two Axis Automatic Flight Guidance Systems, D2. Compatibility of this modification with other
PIPER PA-28-160
Model ST-711-20/30According FAA-STC previously approved modifications must be
PIPER PA-28-180
SA09254AC-D
determined by the installer3. This STC is
PIPER PA-28-235
approved only for the product configuration as
defined in the approved design da
10015381 S-TEC CORPORATION EASA.IM.A.S.01066 REV. 1 FAA STC SA8896SW-D CESSNA 210L
CESSNA 210M
CESSNA 210N
CESSNA 210R
CESSNA T210L
CESSNA T210M
CESSNA T210N
CESSNA T210R
10015383 S-TEC CORPORATION EASA.IM.A.S.0107 REV. 1 CESSNA 177
CESSNA 177A
CESSNA 177B
10015397 S-TEC CORPORATION EASA.IM.A.S.01099 FAA STC SA09502AC-D AVIATION AIRCRAFT A-1
AVIATION AIRCRAFT A-1A
AVIATION AIRCRAFT A-1B
Installation of S-TEC System 55/55X Two Axis 1. As defined in the Limitations and Conditions
Automatic flight Guidance System, Model ST- section of FAA STC SA8896SW-D, latest
566, according to Bulletin No 666, Rev 2 dated approved revision2. Prior to installation of this
1-25-01 or later approved revisions
modification the installer must determine that
the interrelationship between this modification
andany other previously i
Installation of S-TEC Sysytem 20/30 Single
and Two-axis Automatic Flight Guidance
Systems.
Installation of S-TEC System 30 ALT Altitude
Hold System, Model ST-881
10015419 S-TEC CORPORATION EASA.IM.A.S.01142 REV. 1 FAA STC SA09130AC-D PILATUS PC 6 SERIES Installation of Meggitt Avionics S-TEC Autopilot
55/55X
1. Subject to compliance with the provisions
of Part 21 Subpart E, this STC and associated
data shall remain valid until surrendered,
withdrawn or otherwise terminated.2. If
transfer of this Certificate is requested under
Part 21A.116, the STC will b
1. 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.
1. Limited to PC-6/B1-H2; PC-6/B2-H2; PC-
6/B2-H4 and PC-6/B2-H4 when modified with
underwing fuel tanks2. If stabilizer electricaltrim
interrupt switch S043 is installed, the
optional trim wiring in accordance with detail
"A" on S-TEC drawing No 99213 Rev
10015441 S-TEC CORPORATION EASA.IM.A.S.01181 FAA STC SA09018AC-D CESSNA A185F Installation of S-TEC System 55/55X Two Axis Cessna Model A185F & Cessna Model A185F
Automatic Flight Guidance System, Model ST- when equipped with STC SA1441WE
596. Bulletin No.696 Revision 3 dated February (Robertson STOL) or STC SA968CE (Horton
2 2001 & Master Drawing List No. 92801 STOL) and/or STC SA2529WE (Internal Tip
Revision C dated February 2 2001 or later
approved revision (28 volt system). S-TE
Tanks)
10015442 S-TEC CORPORATION EASA.IM.A.S.01182 FAA STC SA09195AC-D COMMANDER 112, 112B, 112TC, Installation of S-TEC System 55/55X wo Axis This STC is approved only for the product
COMMANDER 112TCA, 114, Automatic Flight Guidance Ssytem. Model ST- configuration as defined in the approved design
114A
658, in accordance with FAA STC SA09195AC-data
referred to in the paragraph "Description".
D.
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
10015455 S-TEC CORPORATION EASA.IM.A.S.01201 FAA STC SA09283AC-D NAVION A (L-17B)
Installation of S-TEC System 20/30 Single and 1. This STC is approved only for the product
NAVION B
Two Axis Automatic Flight Guidance System configuration as defined in the approved design
NAVION G
Model ST-724-20/30 in accordance with FAA data referred to in the paragraph "Description".
NAVION H
STC SA09283AC-D
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
10015478 S-TEC CORPORATION EASA.IM.A.S.01232 REV. 1 FAA STC SA5112SW-D PIPER PA-30
Installation of S-TEC System 60 Two Axis 1. This STC is also eligible on the concerned
PIPER PA-39
Automatic Flight Guidance System Model ST- model when modified per STC SA727WE. 2.
127. FAA STC SA5112SW-D
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 aircra
10015555 S-TEC CORPORATION EASA.IM.A.S.01452 REV. 1 FAA STC SA09147AC-D CESSNA 152
CESSNA A152
10015556 S-TEC CORPORATION EASA.IM.A.S.01453 REV. 1 FAA STC SA09148AC-D CESSNA F152
CESSNA FA-152
Installation of S-TEC System 40/50 Single and
Two Axis Automatic Flight Guidance System,
Model ST-628, according to Bulletin No 728,
dated 3-29-96 or later approved revisions
Installation of S-TEC System 40/50 Single and
Two Axis Automatic Flight Guidance System,
Model ST-628, according to Bulletin No 728,
dated 3-29-96 or later approved revisions
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.
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.
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09.09.2008
10.09.2008
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10.09.2008
25.07.2005
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30.05.2005
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10.09.2008