SERVICE DOCUMENTS

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Warning: The airplane pilot and owner are fully and solely responsible for choosing and considering the correct documents, complete and applicable for the explicit aircraft. If you have doubts, please contact your nearest authorized distributor or customer.care@flightdesign.com.
Safety Alerts
Download Date Subject Affected Manual Compliance
SA-ASTM-CT_-01-en 15-10-2008 Engine Mount Bolts s/n up to 05-05-01 (including) n/a n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-ASTM-CT__-03 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction Aircraft witd Garmin SL30 or SL40 & aircraft production date before AUG 2010 (excluded), or retrofitted witd SL 30/40 produced before to OCT 2010 (excluded) mandatory, w/o time limit n/a
SB-ASTM-CT_-01-en 15-10-2008 Landing Gear Inspection All s/n n/a n/a
SB-ASTM-CT_-02-en 15-10-2008 Inspection of Neuform 3-Bladed Variable Pitch Propeller Installation All aircrafts equipped witd Neuform 3-blade Variable Pitch Propeller before tde next flight n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-ASTM-CT_-01-en 15-10-2008 Rohacell ® foam core All s/n n/a n/a
SN-ASTM-CT_-02-en 15-10-2008 Engine coolant All s/n n/a n/a
SN-ASTM-CT_-03-en 15-10-2008 Coolant hose chafing up to 02-06-04-25 (including) n/a n/a
SN-ASTM-CT_-04-en 15-10-2008 Upper rudder hinge All s/n n/a n/a
SN-ASTM-CT_-05-en 15-10-2008 Aileron Bracket up to 04-04-01 n/a n/a
SN-ASTM-CT_-06-en 22-09-2008 Information on Usage of Etdanol Blended Fuel All s/n n/a n/a

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-LTUL-CT__-05 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. up to x-12-05-02 must be conducted prior to next flight n/a
SA-LTUL-CT__-04 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL All s/n must be conducted prior to next flight n/a
SA-LTUL-CT__-03 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914. all s/n up to D-11-07-08, F-11-07-06 and E-11-06-01 (incl.) Required before next flight, but at latest before 01 January 2012 n/a
SA-LTUL-CT_-02-en 15-10-2008 Engine Mount Bolts all s/n up to 05-05-01 n/a n/a
SA-LTUL-CT_-01-en 15-10-2008 Securing of control system bolts All s/n n/a n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-LTUL-CT__-04 08-10-2010 Garmin SL30 and SL40
Comm Radio Spurious Emissions Correction
All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded),or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-LTUL-CT__-03 06-05-2010 Fuel Filter Exchange All serial numbers prior to D-09-02-10 or F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) n/a CT Parts and Maintenance Manual,
CT Aircraft Maintenance Manual
SB-LTUL-CT_-01-en 15-10-2008 Landing Gear Inspection All s/n n/a n/a
SB-LTUL-CT_-02-en 15-10-2008 Inspection of Neuform 3-Bladed Variable Pitch Propeller Installation All aircrafts equipped with Neuform 3-blade Variable Pitch Propeller before the next flight n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-LTUL-CT__-10 13-04-2016 Spare Parts Availability not limited n/a n/a
SN-LTUL-CT_-01-en 15-10-2008 Rohacell® foam core All s/n n/a n/a
SN-LTUL-CT_-02-en 15-10-2008 Engine coolant All s/n n/a n/a
SN-LTUL-CT_-03-en 15-10-2008 Coolant hose chafing All s/n n/a n/a
SN-LTUL-CT_-04-en 15-10-2008 Upper rudder hinge All s/n n/a n/a
SN-LTUL-CT_-08-en 15-10-2008 Aileron Bracket up to 04-04-01 n/a n/a
SN-LTUL-CT_-06-en 15-10-2008 Recovery System Shoot Out Opening Check All s/n n/a n/a
SN-LTUL-CT_-07-en 15-10-2008 Detection of Damages from Hard Landings All s/n n/a n/a
SN-LTUL-CT_-09-en 22-09-2008 Information on Usage of Ethanol Blended Fuel All s/n n/a n/a

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-SECS-CT_-02-en 28-11-2011 Engine Mount Bolts all s/n up to D-11-07-08, F-11-07-06 and E-11-06-01 (incl.) n/a n/a
SA-SECS-CT_-01-en 15-10-2008 Securing of control system bolts All s/n before the next flight n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-SECS-CT__-03 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded) or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-SECS-CT__-02 06-05-2010 Fuel Filter Exchange All serial numbers prior to D-09-02-10 or F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) n/a CT Parts and Maintenance Manual, CT Aircraft Maintenance Manual
SB-SECS-CT_-01-en 15-10-2008 Landing Gear Inspection All s/n n/a n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-SECS-CT_-01-en 15-10-2008 Rohacell ® foam core All s/n n/a n/a
SN-SECS-CT_-02-en 15-10-2008 Engine coolant All s/n n/a n/a
SN-SECS-CT_-03-en 15-10-2008 Coolant hose chafing All s/n n/a n/a
SN-SECS-CT_-04-en 15-10-2008 Upper rudder hinge All s/n n/a n/a
SN-SECS-CT_-06-en 15-10-2008 Aileron Bracket up to 04-04-01 n/a n/a
SN-SECS-CT_-05-en 15-10-2008 Detection of Damages from Hard Landings All s/n n/a n/a
SN-SECS-CT_-07-en 22-09-2008 Information on Usage of Ethanol Blended Fuel All s/n n/a n/a

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-ASTM-CT2K-04 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. aircraft serial number earlier than x 12 05 02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. before the next flight n/a
SA-ASTM-CT2K- 03 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL all s/n before the next flight n/a
SA-ASTM-CT2K-02 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914 all s/n before the next flight, but at latest before 01 January 2012 n/a
SA-ASTM-CT2k-01-en 15-10-2008 Engine Mount Bolts up to 05-05-01 (incl.) n/a Maintenance and Inspection Procedures Manual
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-ASTM-CT2k-05 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-ASTM-CT2k-04 06-05-2010 Fuel Filter Exchange All serial numbers prior to D-09-02-10 or F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and Maintenance Manual, CT Aircraft Maintenance Manual
SB-ASTM-CT2k-01-en 15-10-2008 Radiator Isolator Mounts from 03-04-03-16 to 05-06-03 before the next flight Maintenance and Inspection Procedures Manual
SB-ASTM-CT2k-02-en 15-10-2008 Landing Gear Inspection all s/n n/a Maintenance and Inspection Procedures Manual
SB-ASTM-CT2k-03-en 15-10-2008 Inspection of Neuform 3-Bladed Variable Pitch Propeller Installation All aircrafts equipped with Neuform 3-blade Variable Pitch Propeller before the next flight n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-ASTM-CT2k-09 13-04-2016 Spare Parts Availability not limited n/a Flight and Maintenance Manual
SN-ASTM-CT2k-01-en 15-10-2008 Rohacell ® foam core all s/n n/a n/a
SN-ASTM-CT2k-02-en 15-10-2008 Engine coolant all s/n n/a n/a
SN-ASTM-CT2k-03-en 15-10-2008 Coolant hose chafing up to 01-04-01-12 (not incl.) n/a n/a
SN-ASTM-CT2k-04-en 15-10-2008 Coolant hose chafing up to 02-06-04-25 (incl.) n/a n/a
SN-ASTM-CT2k-05-en 15-10-2008 Upper rudder hinge all s/n n/a n/a
SN-ASTM-CT2k-06-en 15-10-2008 Aileron Bracket up to 04-04-01 n/a n/a
SN-ASTM-CT2k-07-en 15-10-2008 Maintenance Inspection Intervals all s/n n/a Maintenance and Inspection Procedures Manual, Rotax engine Maintenance Manual
SN-ASTM-CT2k-08-en 22-09-2008 Information on Usage of Ethanol Blended Fuel all s/n n/a n/a

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-LTUL-CT2K-05 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. aircraft serial number earlier than x 12 05-02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory before the next flight n/a
SA-LTUL-CT2K-04 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL. all s/n before the next flight n/a
SA-LTUL-CT2K-03 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914. all s/n before the next flight, but at latest before 01 January 2012 n/a
SA-LTUL-CT2k-02-en 15-10-2008 Engine Mount Bolts up to 05-05-01 (incl.) n/a Maintenance and Inspection Procedures Manual
SA-LTUL-CT2k-01-en 15-10-2008 Securing of control system bolts all s/n before the next flight n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-LTUL-CT2k-06 28-03-2014 Airspeed Markings all s/n latest at the next annual inspection Flight and Maintenance Manual
SB-LTUL-CT2k-05 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-LTUL-CT2k-04 06-05-2010 Fuel Filter Exchange All serial numbers prior to D-09-02-10 or F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and Maintenance Manual, CT Aircraft Maintenance Manual
SB-LTUL-CT2k-01-en 15-10-2008 Radiator Isolator Mounts from 03-04-03-16 to 05-06-03 before the next flight Maintenance and Inspection Procedures Manual
SB-LTUL-CT2k-02-en 15-10-2008 Landing Gear Inspection all s/n n/a Maintenance and Inspection Procedures Manual
SB-LTUL-CT2k-03-en 15-10-2008 Inspection of Neuform 3-Bladed Variable Pitch Propeller Installation All aircrafts equipped with Neuform 3-blade Variable Pitch Propeller before the next flight n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-LTUL-CT2k-12 13-04-2016 Spare Parts Availability not limited n/a Flight and Maintenance Manual
SN-LTUL-CT2k-06-en_1 19-12-2009 CT and CT2k MTOW increase for German Certification all s/n n/a n/a
SN-LTUL-CT2k-01-en 15-10-2008 Rohacell® foam core all s/n n/a n/a
SN-LTUL-CT2k-02-en 15-10-2008 Engine coolant all s/n n/a n/a
SN-LTUL-CT2k-04-en 15-10-2008 Coolant hose chafing all s/n n/a n/a
SN-LTUL-CT2k-03-en 15-10-2008 Coolant hose cracking all s/n n/a n/a
SN-LTUL-CT2k-05-en 15-10-2008 Upper rudder hinge all s/n n/a n/a
SN-LTUL-CT2k-09-en 15-10-2008 Aileron Bracket up to 04-04-01 n/a n/a
SN-LTUL-CT2k-10-en 15-10-2008 Maintenance Inspection Intervals all s/n n/a Maintenance and Inspection Procedures Manual, Rotax engine Maintenance Manual
SN-LTUL-CT2k-07-en 15-10-2008 Recovery System Shoot Out Opening Check all s/n n/a n/a
SN-LTUL-CT2k-08-en 15-10-2008 Detection of Damages from Hard Landings all s/n n/a n/a
SN-LTUL-CT2k-11-en 22-09-2008 Information on Usage of Ethanol Blended Fuel all s/n n/a n/a

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-SECS-CT2K-05 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. aircraft serial number earlier than x-12-05-02 (excluded, with (x) being the identifier of the relevant model, (when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. before the next flight n/a
SA-SECS-CT2K-04 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL all s/n before the next flight n/a
SA-SECS-CT2K-03 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914 all s/n before the next flight, but at latest before 01 January 2012 n/a
SA-SECS-CT2k-02-en 15-10-2008 Engine Mount Bolts up to 05-05-01 n/a n/a
SA-SECS-CT2k-01-en 15-10-2008 Securing of control system bolts all s/n before the next flight n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-SECS-CT2k-04 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without timace limit n/a
SB-SECS-CT2k-03 06-05-2010 Fuel Filter Exchange All serial numbers prior to D-09-02-10 or F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and Maintenance Manual, CT Aircraft Maintenance Manual
SB-SECS-CT2k-01-en 15-10-2008 Radiator Isolator Mounts from 03-04-03-16 to 05-06-03 before the next flight Maintenance and Inspection Procedures Manual
SB-SECS-CT2k-02-en 15-10-2008 Landing Gear Inspection all s/n n/a Maintenance and Inspection Procedures Manual
Service Notifications
Download Date Subject Affected Manual Compliance
SN-SECS-CT2k-10 13-04-2016 Spare Parts Availability not limited n/a Flight and Maintenance Manual
SN-SECS-CT2k-01-en 15-10-2008 Rohacell ® foam core all s/n n/a n/a
SN-SECS-CT2k-02-en 15-10-2008 Engine coolant all s/n n/a n/a
SN-SECS-CT2k-03-en 15-10-2008 Coolant hose chafing all s/n n/a n/a
SN-SECS-CT2k-04-en 15-10-2008 Coolant hose chafing all s/n n/a n/a
SN-SECS-CT2k-05-en 15-10-2008 Upper rudder hinge all s/n n/a n/a
SN-SECS-CT2k-07-en 15-10-2008 Aileron Bracket up to 04-04-01 n/a n/a
SN-SECS-CT2k-08-en 15-10-2008 Maintenance Inspection Intervals all s/n n/a Maintenance and Inspection Procedures Manual, Rotax engine Maintenance Manual
SN-SECS-CT2k-06-en 15-10-2008 Detection of Damages from Hard Landings all s/n n/a n/a
SN-SECS-CT2k-09-en 22-09-2008 Information on Usage of Ethanol Blended Fuel all s/n n/a n/a

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-ASTM- CTSW-06 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. All CTSW aircrafts with aircraft serial number earlier than x 12 05 02 (excluded, with (x) being the identifier of the relevant model, when applicable),where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory before the next flight n/a
SA-ASTM- CTSW- 05 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL all s/n before the next flight n/a
SA-ASTM-CTSW-04 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914 All S/N up to S/N D-11-07-08 (inclusive) before next flight, but at latest before 01 January 2012 n/a
SA-ASTM-CTSW-01-en 15-10-2008 Engine Mount Bolts all s/n up to 05-05-01 (incl.) n/a Maintenance and Inspection Procedures Manual
SA-ASTM-CTSW-02-en 15-10-2008 Servo Tab Spring from 05-11-09 up to 06-09-05 within the next 25 hours, or at the next maintenance interval, whichever occurs first Maintenance Manual
SA-ASTM-CTSW-03-en_1 15-10-2008 Trim Tab Reinforcement CTSW 2006-2007 from 06-07-15 up to 07-05-18 before the next flight 070625 Trim Tab Reinforcement Procedure; Maintenance Manual
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-ASTM-CTSW-16 23-12-2019 Repair procedure to additional wires protection E-18-10-55, D-19-05-03 immediate action (within the next 10 hours) n/a
SB-ASTM-CTSW-99 15-10-2019 Equipment Manufacturer Notification n/a n/a n/a
SB-ASTM-CTSW-14 26-08-2019 Dynon Autopilot Servo SV42T Inspection and Replacement of Linear Actuator Servo Pulley in case of alteration of autopilot servo system to SV42T servo or auto pilot installation retrofits before the next flight n/a
SB-ASTM-CTSW-13 02-10-2015 Verification of Rescue System Cover Installation all s/n latest within 3 months following the issue date of this Notification, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB-ASTM-CTSW-12 11-11-2014 Inspection of BRS Handle Bracket All aircrafts with Airframe Emergency Parachute System BRS 1050 or 1350 installed, from S/N D-05-01-01 onwards. as part of every regular 100 hrs inspection n/a
SB-ASTM-CTSW-10 30-07-2012 Inspection of the Rescue System Rear Harness connection from 06-01-07(included) to 06-11-13(included); only those with installed BRS1350 HS Airframe Emergency Parachute System before the next flight PARACHUTE INSTALLATION MANUAL (PIM) BRS 1350 HS Flight Design GmbH
SB-ASTM-CTSW-09 23-12-2010 Correction of Gross Weight Metric Conversion to Pounds All serial numbers with applicable Aircraft Operating Instructions (AOI) revision 5, 5a, 5b, 6, 7, 8. before 30 days after the issuance of this notice AU 010 01000 Flight Design CTSW Aircraft Operating Instructions (AOI)
SB-ASTM-CTSW-08 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-ASTM-CTSW-06 06-05-2010 Fuel Filter Exchange All serial numbers prior to D-09-02-10 or F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and Maintenance Manual, CT Aircraft Maintenance Manual
SB-ASTM-CTSW-07 30-11-2009 Stabilizer rear wall stiffening S/N range 06-09-01 to 07-05-03, when equipped with full span trim tab, plus aircraft that do have trim tab balancing weights but do not have pre-formed stiffeners supporting each individual trim tab hinge point. at the next annual inspection. In cases where the next annual inspection comes within three months from issuing of this document it is permissible to extend compliance to the time limit of three moths from issuing of this document. CTSW Parts Catalog, CTSW-LSA Maintenance and Inspections Procedures Manual
SB-ASTM-CTSW-01-en 15-10-2008 Radiator Isolator Mounts all s/n from 03-04-03-16 to 05-06-03 before the next flight Maintenance and Inspection Procedures Manual
SB-ASTM-CTSW-02-en 15-10-2008 Landing Gear Inspection all s/n every 300 hours, at the annual inspection, or after a hard landing, whichever occurs first. Maintenance and Inspection Procedures Manual
SB-ASTM-CTSW-03-en 15-10-2008 Servo Tab Hinge Enhancement 05-12-01, 05-12-02, 05-12-03, 05-12-05, 05-12-06, 05-12-07, 05-12-08, 06-01-07, 06-01-08, 06-01-09, 06-01-10, 06-01-11, 06-01-12, 06-02-05, 06-02-06 n/a n/a
SB-ASTM-CTSW-05-en 15-10-2008 Inspection of Neuform 3-Bladed Variable Pitch Propeller Installation All aircrafts equipped with Neuform 3-blade Variable Pitch Propeller before the next flight n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-ASTM-CTSW-06 13-04-2016 Spare Parts Availability not limited n/a n/a
SN-ASTM-CTSW-01-en 15-10-2008 Rohacell ® foam core all s/n n/a Maintenance and Inspection Procedures Manual
SN-ASTM-CTSW-02-en 15-10-2008 Engine coolant all s/n n/a Rotax engine manual
SN-ASTM-CTSW-03-en 15-10-2008 Upper rudder hinge all s/n n/a Maintenance and Inspection Procedures Manual
SN-ASTM-CTSW-04-en 15-10-2008 Maintenance Inspection Intervals all s/n n/a Maintenance and Inspection Procedures Manual; Rotax Maintenance Manual
SN-ASTM-CTSW-05-en 22-09-2008 Information on Usage of Ethanol Blended Fuel all s/n n/a Aircraft Operation Instructions; Rotax engine Operators Manual

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-LTUL- CTSW-08 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. All CT type aircrafts with aircraft serial number earlier than x 12 05-02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. before the next flight n/a
SA-LTUL-CTSW-07 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL. all s/n before the next flight n/a
SA-ASTM- CTSW-06 16-05-2012 Trim Tab Retrofit CTSW All aircraft equipped with stabilizer built using Aramid fibers for the stabilizer skin (includes all Ultralight certified aircraft), and equipped with long (full span) Trimtab attached to the Stabilizer. before the next flight Flight- and Maintenance Manual CTSW 2006
SA-LTUL-CTSW-05 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914. All S/N up to S/N D-11-07-08 (inclusive) before next flight, but at latest before 01 January 2012 n/a
SA-LTUL-CTSW-04 11-08-2010 Temporary Airspeed Limitation CTSW All aircraft equipped with stabilizer built using Aramide fibers for the stabilizer skin (includes all Ultralight certified aircraft), and equipped with long (full span) Trimtab attached to the Stabilizer. before the next flight Flight- and Maintenance Manual CTSW 2006
SA-LTUL-CTSW-01-en 15-10-2008 Engine Mount Bolts all s/n up to 05-05-01 in the next 20 hours n/a
SA-LTUL-CTSW-02-en 15-10-2008 Servo Tab Spring CTSW 2006 from 05-11-09 to 06-09-05 within the next 25 hours, or at the next maintenance interval, whichever occurs first Maintenance Manual
SA-LTUL-CTSW-03-en 15-10-2008 Trim Tab Reinforcement CTSW 2006 model year 2006 and 2007 s/n from 06-07-15 to 07-05-18 (incl.) when equipped with full span trim tab. before the next flight 070625 Trim Tab Reinforcement Procedure; Maintenance Manual
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-LTUL-CTSW-99 15-10-2019 Equipment Manufacturer Notification n/a n/a n/a
SB-LTUL-CTSW-13 02-10-2015 Verification of Rescue System Cover Installation. up to serial number D-11-07-08 (including) latest within 3 months following the issue date of this Notification, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB-LTUL-CTSW-13 02-10-2015 Inspection Horizontal Tail. Aircraft S/N that have a horizontal tail produced of Aramid fabric installed each 100 hrs inspection n/a
SB-LTUL-CTSW-12 11-11-2014 Inspection of BRS Handle Bracket All aircrafts with Airframe Emergency Parachute System BRS 1050 or 1350 installed, from S/N D-05-01-01 onwards. as part of every regular 100 hrs inspection n/a
SB-LTUL-CTSW-09 19-05-2011 Tow Bar Markings and Operation D-10-07-02 before the next flight CTSW Flight and Maintenance Manual; AZ 0430 0004 Supplement Tow Bar Interface and Operation to the Flight and Maintenance Manual
SB-LTUL-CTSW-08 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-LTUL-CTSW-06 06-05-2010 Fuel Filter Exchange All serial numbers prior to D-09-02-10 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and Maintenance Manual CT Aircraft Maintenance Manual
SB-LTUL-CTSW-07 30-11-2009 Stabilizer rear wall stiffening S/N range 06-09-01 to 07-05-03, when equipped with full span trim tab, plus aircraft that do have trim tab balancing weights but do not have pre-formed stiffeners supporting each individual trim tab hinge point. at the next annual inspection. In cases where the next annual inspection comes within three months from issuing of this document it is permissible to extend compliance to the time limit of three moths from issuing of this document. CTSW Parts Catalog
SB-LTUL-CTSW-01-en 15-10-2008 Radiator Isolator Mounts all s/n from 03-04-03-16 to 05-06-03 before the next flight Maintenance and Inspection Procedures Manual
SB-LTUL-CTSW-02-en 15-10-2008 Landing Gear Inspection all s/n every 300 hours, at the annual inspection, or after a hard landing, whichever occurs first. Maintenance and Inspection Procedures Manual
SB-LTUL-CTSW-05-en 15-10-2008 Inspection of Neuform 3-Bladed Variable Pitch Propeller Installation All aircrafts equipped with Neuform 3-blade Variable Pitch Propeller before the next flight n/a
SB-LTUL-CTSW-04-en 15-10-2008 BRS Recovery System Handle Inspection from 05-06-01 (incl.) up to 07-03-07 (excl.) immediate inspection n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-LTUL-CTSW-06 13-04-2016 Spare Parts Availability not limited n/a n/a
SN-LTUL-CTSW-01-en 15-10-2008 Rohacell® foam core all s/n n/a n/a
SN-LTUL-CTSW-02-en 15-10-2008 Engine coolant all s/n n/a n/a
SN-LTUL-CTSW-03-en 15-10-2008 Upper rudder hinge all s/n n/a n/a
SN-LTUL-CTSW-04-en 15-10-2008 Maintenance Inspection Intervals all s/n n/a Maintenance and Inspection Procedures Manual; Rotax Maintenance Manual
SN-LTUL-CTSW-05-en 22-09-2008 Information on Usage of Ethanol Blended Fuel all s/n n/a Aircraft Operation Instructions; Rotax engine Operators Manual

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-SECS-CTSW-06 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. All above listed CT type aircraft models with aircraft serial number earlier than x 12 05 02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. before the next flight n/a
SA-SECS-CTSW-05 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL All CTSW up to S/N 11-07-08 before the next flight n/a
SA-SECS-CTSW-04 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914 All S/N up to S/N D-11-07-08 (inclusive) before next flight, but at latest before 01 January 2012 n/a
SA-SECS-CTSW-01-en 15-10-2008 Engine Mount Bolts all s/n up to 05-05-01 in the next 20 hours n/a
SA-SECS-CTSW-02-en 15-10-2008 Servo Tab Spring CTSW 2006 from 05-11-09 to 06-09-05 within the next 25 hours, or at the next maintenance interval, whichever occurs first Maintenance Manual
SA-SECS-CTSW-03-en 15-10-2008 Trim Tab Reinforcement CTSW 2006 model year 2006 and 2007 s/n from 06-07-15 to 07-05-18 (incl.) when equipped with full span trim tab (assembled before September 1st 2007) before the next flight 070625 Trim Tab Reinforcement Procedure; Maintenance Manual
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-SECS-CTSW-99 15-10-2019 Equipment Manufacturer Notification n/a n/a n/a
SB-SECS-CTSW-08 02-10-2015 Verification of Rescue System Cover Installation. up to serial number D-11-07-08 (including) latest within 3 months following the issue date of this Notification, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB-SECS-CTSW-09 02-10-2015 Inspection Horizontal Tail. Aircraft S/N that have a horizontal tail produced of Aramid fabric installed each 100 hrs inspection n/a
SB-SECS-CTSW-06 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-SECS-CTSW-04 06-05-2010 Fuel Filter Exchange All serial numbers prior to D-09-02-10 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and Maintenance Manual CT Aircraft Maintenance Manual
SB-SECS-CTSW-05 30-11-2009 Stabilizer rear wall stiffening S/N range 06-09-01 to 07-05-03, when equipped with full span trim tab, plus aircraft that do have trim tab balancing weights but do not have pre-formed stiffeners supporting each individual trim tab hinge point. at the next annual inspection. In cases where the next annual inspection comes within three months from issuing of this document it is permissible to extend compliance to the time limit of three moths from issuing of this document. CTSW Parts Catalog
SB-SECS-CTSW-01-en 15-10-2008 Radiator Isolator Mounts all s/n from 03-04-03-16 to 05-06-03 before the next flight Maintenance and Inspection Procedures Manual
SB-SECS-CTSW-02-en 15-10-2008 Landing Gear Inspection all s/n every 300 hours, at the annual inspection, or after a hard landing, whichever occurs first. Maintenance and Inspection Procedures Manual
Service Notifications
Download Date Subject Affected Manual Compliance
SN-SECS-CTSW-06 13-04-2016 Spare Parts Availability not limited n/a n/a
SN-SECS-CTSW-01-en 15-10-2008 Rohaceall ® foam core all s/n n/a n/a
SN-SECS-CTSW-02-en 15-10-2008 Engine coolant all s/n n/a n/a
SN-SECS-CTSW-03-en 15-10-2008 Upper rudder hinge all s/n n/a n/a
SN-SECS-CTSW-04-en 15-10-2008 Maintenance Inspection Intervals all s/n n/a Maintenance and Inspection Procedures Manual; Rotax Maintenance Manual
SN-SECS-CTSW-05-en 22-09-2008 Information on Usage of Ethanol Blended Fuel all s/n n/a Aircraft Operation Instructions; Rotax engine Operators Manual

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-ASTM-CTHL-03 04-11-2014 Installation verification of BRS Pickup Collar All aircrafts with Airframe Emergency Parachute System BRS 1350 HS installed, and with S/N up to C-11-11-02, included. Aircraft with higher S/N are not affected. prior to next flight n/a
SA-ASTM-CTHL-02 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. All CT and MC type aircrafts with aircraft serial number earlier than x 12 05 02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. prior to next flight n/a
SA-ASTM-CTHL-01 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914 All S/N up to S/N C-11-02-01 (inclusive) before next flight, but at latest before 01 January 2012 n/a

Not applicable.

Not applicable.

Not applicable

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-LTUL- CTSL-03 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. All CT type with s/n earlier than x 12 05-02 (excluded, with (x) -the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. prior to next flight n/a
SA-LTUL-CTSL-02 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL. up to S/N E-12-02-08 prior to next flight n/a
SA-LTUL-CTSL-01 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914. All S/N up to S/N E-11-06-01 (inclusive). before next flight, but at latest before 01 January 2012 n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB- LTUL –CT Supralight-99 15-10-2019 Equipment Manufacturer Notification n/a n/a n/a
SB-LTUL-CTSL-06 26-08-2019 Dynon Autopilot Servo SV42T Inspection and Replacement of Linear Actuator Servo Pulley aircraft equipped with DYNON autopilot before the next flight n/a
SB-LTUL-CT Supralight-04 02-10-2015 Verification of Rescue System Cover Installation. up to s/n E-14-02-03 (including) latest within 3 months following the issue date of this Notification, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB- LTUL –CT Supralight-05 02-10-2015 Inspection Horizontal Tail. Aircraft S/N that have a horizontal tail produced of Aramid fabric installed with each 100 hrs inspection n/a
SB-LTUL- CTSL-03 11-11-2014 Inspection of BRS Handle Bracket. All aircraft with Airframe Emergency Parachute System BRS 1050 or 1350 installed, from S/N E-09-02-11 onwards.  inspection is required at every regular 100 hrs inspection. Initial inspection of the bracket: within the next 6 weeks on aircraft with >1.000 hrs operation. If cracks are detected, the part must be exchanged before the next flight. n/a
SB-LTUL–CT Supralight-02 19-05-2011 Tow Bar Markings and Operation E-10-06-07; E-10-06-08; E-10-08-02; E-10-08-15; E-10-11-03; E-10-11-04 Iftow bar interface is used: The inspection is mandatory before the next flight. When the tow bar interface is never used: The inspection is mandatory latest 30 days following the issue date of this SB. Flight Design CT Supralight Flight and Maintenance Manual, AZ 0430 0004 Supplement Tow Bar Interface and Operation to the Flight and Maintenance Manual
SB-LTUL–CT Supralight-01 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-LTUL-CT Supralight-03 13-04-2016 Spare Parts Availability not limited n/a n/a
SN-LTUL-CT Supralight-02 15-05-2015 Supporting Information to Engine Start-Up of Rotax 912 iS on Flight Design Aircraft All aircraft with any version of engine Rotax 912 iS series installed n/a Supplement to the Aircraft Operating Instructions with Rotax 912 iS engine – relevant document and version applicable to the individual aircraft
Service Letters
Download Date Subject Affected Manual Compliance
SL-LTUL-CTSL-01 24-09-2020 Drain Holes in Air Filter Box all s/n prior to next flight n/a

Service Bulletins
Download Date Subject Affected Manual Compliance
SB- SECS –CT Supralight-99 15-10-2019 Equipment Manufacturer Notification n/a n/a n/a
SB- SECS –CT Supralight-02 02-10-2015 Verification of Rescue System Cover Installation. up to s/n E-14-02-03 (including) latest within 3 months following the issue date of this Notification, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB- SECS –CT Supralight-03 02-10-2015 Inspection Horizontal Tail. Aircraft S/N that have a horizontal tail produced of Aramid fabric installed with each 100 hrs inspection n/a
Service Notifications
Download Date Subject Affected Manual Compliance
SN-SECS-CT Supralight-01 13-04-2016 Spare Parts Availability not limited n/a n/a

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-ASTM–MC_-04 04-11-2014 Installation verification of BRS Pickup Collar All aircrafts with Airframe Emergency Parachute System BRS 1350 HS installed, and with S/N up to A-12-04-33, included. Aircraft with higher S/N are not affected. prior to next flight n/a
SA-ASTM- MC_-03 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1,
ASB-912-062R1 / ASB-914-044R1.
All CT and MC type aircrafts with aircraft serial number earlier than x 12 05 02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. prior to next flight n/a
SA-ASTM- MC_- 02 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL up to S/N A-11-07-31 prior to next flight n/a
SA-ASTM-MC_-01 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914 All S/N up to S/N A-11-01-31 (inclusive) before next flight, but at latest before 01 January 2012 n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-ASTM–MC_-04 23-12-2019 Repair procedure to additional wires protection A-19-01-06 within the next 10 hours n/a
SB-ASTM-MC_-99 15-10-2019 Equipment Manufacturer Notification n/a at each annual inspection n/a
SB-ASTM-MC_-02 19-05-2011 Tow Bar Markings and Operation A-09-01-31; A-10-01-32; A-10-04-31;
A-10-07-31; A-10-10-31
When the tow bar interface has been used: The inspection is mandatory before the next flight. Flight Design MC Maintenance and Inspection Procedures Manual,
AZ 0430 0003 Supplement Tow Bar Interface and Operation to the Aircraft Operating Instructions (AOI)
SB-ASTM-MC_-01 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded),
or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded)
mandatory, but without time limit n/a

Not applicable

Not applicable

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-ASTM-CTLS-04 25-11-2014 CTLSi Engine Installation Redundancy Diagnosis / ASB-914-044R1. All CT type aircrafts with aircraft serial number earlier than x 12 05-02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. prior to next flight AF 0480 0011_00 – Supplement S3 to the
Airplane Maintenance Manual (AMM)
CTLS-LSA with ROTAX 912 iS
SA-ASTM-CTLS-05 04-11-2014 Installation verification of BRS Pickup Collar All aircrafts with Airframe Emergency Parachute System BRS 1350 HS installed, and with S/N up to F-13-09-04, included. Aircraft with higher S/N are not affected. prior to next flight n/a
SA-ASTM- CTLS-03 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. All CT type aircrafts with aircraft serial number earlier than x 12 05-02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. prior to next flight n/a
SA-ASTM- CTLS- 02 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL CTLS up to S/N F-12-02-10 prior to next flight n/a
SA-ASTM-CTLS-01 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914 All S/N up to S/N F-11-07-06 (inclusive) before next flight, but at latest before 01 January 2012 n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-ASTM-CTLS-17 23-12-2019 Repair procedure to additional wires protection F-18-10-52, F-18-10-54, F-18-11-03, F-18-11-04, F-19-03-01, F-19-04-51, F-19-04-55, F-19-05-01, F-19-05-02, F-19-05-05, F-19-05-06, F-19-08-52, F-19-11-01, F-19-11-02, F-19-11-04 within the next 10 hours n/a
SB-ASTM-CTLS-16 22-11-2019 Installation of Starter Solenoid on CTLS with Large SLA Battery F-10-01-01, F-10-01-02, F-10-01-03, F-10-02-07, F-10-02-08, F-10-06-04, F-10-07-05, F-10-07-06, F-10-07-07; F-10-08-05, F-10-08-06, F-10-08-11, F-10-08-12, F-10-11-07, F-10-12-03, F-11-04-05, F-11-04-11, F-11-04-13, F-11-05-02, F-11-05-11, F-11-07-03- F-11-07-06, F-11-09-04, F-11-09-12, F-11-10-01, F-11-10-03, F-11-10-06, F-11-10-07, F-12-02-09, F-12-02-10, F-12-02-10, F-12-04-09, F-13-04-08, F-14-04-03, F-14-04-06, F-16-06-46 before the next flight n/a
SB-ASTM-CTLS-99 15-10-2019 Equipment Manufacturer Notification n/a n/a n/a
SB-ASTM-CTLS-15 26-08-2019 Dynon Autopilot Servo SV42T Inspection and Replacement of Linear Actuator Servo Pulley F-19-02-54, F-18-03-01, F-18-08-52, F-18-07-03, F-18-07-02, F-18-08-51, F-18-09-01, F-18-10-50, F-18-09-05, F-18-10-52, F-19-04-51, F-19-04-55, F-18-11-05, F-17-07-03, F-17-07-04, F-16-05-52, F-16-05-53, F-16-05-54, F-16-06-03, F-16-07-01, F-16-07-02, F-16-09-46, F-15-04-50, F-14-06-04. Other aircraft may affected in case of alteration of autopilot servo system to SV42T servo or auto pilot installation retrofits. before the next flight n/a
SB-ASTM-CTLS-14 20-03-2019 Installation of Reinforcement Plates on 4 Point Harnesses for CTLS Series not limited latest within 6 months following the issue date of this Bulletin, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB-ASTM-CTLS-13 04-08-2016 Verification of Stabilator Mounting Pivot all s/n prior to next flight AC 0480 0002, Rev.00,
CT / CTLS-HL Airplane
Maintenance Manual (AMM)
SB-ASTM-CTLS-12 02-12-2015 in the level of a Service Directive USA Data Plate Replacement F-12-04-01; F-12-05-04; F-12-05-05; F-12-07-04; F-12-07-05; F-13-01-06; F-13-01-07; F-13-01-08; F-13-02-01; F-13-02-02; F-13-02-03; F-13-03-07; F-13-03-08; F-13-03-09; F-13-04-03; F-13-04-06; F-13-06-01; F-13-06-02; F-13-06-05; F-13-12-09; F-13-12-10; F-14-06-03; F-14-06-04; F-14-06-06; F-14-07-08; F-14-07-10; F-14-07-11; F-14-07-12; F-14-07-13; F-15-04-50 latest at the next annual inspection of the aircraft n/a
SB-ASTM-CTLS-11 02-10-2015 Verification of Rescue System Cover Installation All CTLS-LSA prior to serial number F-15-04-50 (including). latest within 3 months following the issue date of this Notification, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB-ASTM-CTLS -08 09-09-2014 Replacement of regulator A and regulator B for ROTAX engine type 912iS. Aircraft that have fuse boxes installed, as identified in concurrent Rotax SB-912 i-004iS. As minimum, the following aircraft S/N are affected on the basis of the equipment installed when delivered ex-factory: F-11-10-09; F-12-11-08; F-12-11-06; F-12-10-05; F-12-08-05; F-12-08-04; F-12-07-05; F-12-07-04; F-12-06-06; F-12-06-01; F-12-05-05; F-12-05-04; F-12-04-01; F-12-04-06; F-12-03-12; F-12-03-11; F-12-03-10; F-12-03-09; F-13-12-10; F-13-12-09;F-13-09-04; F-13-06-05; F-13-04-03; F-13-03-08; F-13-02-03; F-13-02-02; F-13-02-01; F-13-01-08; F-13-01-07; F-13-01-06; F-13-01-05. Aircraft later than S/N F-14-01-03 are not affected At the initial 25 hrs inspection or within the next 100 hrs inspection MMH-912i_Maintenance Manual
Heavy for ROTAX 912 i Series,
MML-912i_Maintenance Manual (Line)
ROTAX 912 i Series
SB-ASTM-CTLS-06 19-05-2011 Tow Bar Markings and Operation F-10-01-01; F-10-01-02; F-10-01-03; F-10-01-05; F-10-01-16; F-10-01-17; F-10-02-05; F-10-02-06; F-10-02-07; F-10-02-08; F-10-02-10; F-10-03-01; F-10-03-11; F-10-04-03; F-10-04-04; F-10-05-06; F-10-05-10; F-10-05-11; F-10-06-02; F-10-06-03; F-10-06-04; F-10-06-10; F-10-07-05; F-10-07-06; F-10-07-07; F-10-07-10; F-10-07-12; F-10-08-05; F-10-08-06; F-10-08-07; F-10-08-11; F-10-08-12; F-10-09-04; F-10-09-05; F-10-09-06; F-10-10-10; F-10-10-11; F-10-11-07; F-10-12-03; F-10-12-12; F-10-12-13; F-10-12-14; F-11-01-07 When the tow bar interface has been used: The inspection is mandatory before the next flight. When the tow bar interface has never been used: The inspection is mandatory latest 30 days following the issue date of this SB. Flight Design CTLS Maintenance and
Inspection Procedures Manual,
AZ 0430 0003 Supplement Tow Bar
Interface and Operation
to the Aircraft Operating
Instructions (AOI)
SB-ASTM-CTLS-05 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit. n/a
SB-ASTM-CTLS-01 06-05-2010 Fuel Filter Exchange All serial numbers prior to F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and
Maintenance Manual,
CT Aircraft Maintenance
Manual
SB-ASTM-CTLS-02 30-11-2009 Rudder Centring Fork-Control Stop Replacement. F-08-04-09, F-08-04-10, F-08-04-11, F-08-04-12, F-08-04-13, F-08-04-14, F-08-04-15, F-08-04-16, F-08-04-17, F-08-05-08, F-08-05-09, F-08-05-10, F-08-05-11, F-08-05-12, F-08-05-13, F-08-05-14, F-08-05-16, F-08-06-10, F-08-06-11, F-08-06-12, F-08-06-13, F-08-07-04, F-08-07-05, F-08-07-06, F-08-07-07, F-08-07-08, F-08-07-09, F-08-07-10, F-08-07-11, F-08-08-05, F-08-08-06, F-08-08-23, F-08-08-24, F-08-09-03, F-08-09-12, F-08-09-13, F-08-10-19, F-08-10-20, F-08-11-21, F-08-11-22 before the next flight CTLS Maintenance and Inspections
Procedures Manual
SB-ASTM-CTLS-03 30-11-2009 Rudder Centring Fork-Control Stop Replacement. F-08-10-21, F-08-11-20, F-08-11-28, F-08-12-17, F-09-01-08, F-09-01-09, F-09-01-10, F-09-02-10, F-09-02-12, F-09-02-13, F-09-02-16, F-09-03-12, F-09-03-13, F-09-03-14, F-09-03-15, F-09-04-01, F-09-04-06, F-09-04-07, F-09-04-08, F-09-04-09, F-09-04-10, F-09-05-08, F-09-05-09, F-09-06-03, F-09-06-04, F-09-06-16, F-09-07-11, F-09-08-02, F-09-08-05, F-09-08-06, F-09-08-07, F-09-08-15, F-09-08-16, F-09-09-08 before the next flight CTLS Maintenance and
Inspections Procedures
Manual
Service Notifications
Download Date Subject Affected Manual Compliance
SN-ASTM-CTLS-06 02-05-2017 CTLE-LSA Compliance as a Light-Sport Aircraft not limited n/a n/a
SN-ASTM-CTLS-05 13-04-2016 Spare Parts Availability not limited n/a n/a
SN-ASTM-CTLS-04 15-05-2015 Supporting Information to Engine Start-Up of Rotax 912 iS on Flight Design Aircraft All aircraft with any version of engine Rotax 912 iS series installed n/a Supplement to the Aircraft
Operating Instructions
with Rotax 912 iS engine –
relevant document and
version applicable to the
individual aircraft
SN-ASTM-CTLS-02 28-03-2011 Elimination of Noise in Radio from Dynon SkyView SV-D1000 F-09-10-14; F-10-02-06; F-10-02-07; F-10-02-08; F-10-05-11; F-10-06-02; F-10-06-03; F-10-07-05; F-10-07-06; F-10-07-07; F-10-08-06; F-10-08-11; F-10-08-12; F-10-09-04; F-10-10-10; F-10-10-11; F-10-11-07; F-10-12-03; F-10-09-05; F-10-09-06 on condition only, when noise is present n/a
SB-ASTM-CTLS-06 19-05-2011 Tow Bar Markings and Operation F-10-01-01; F-10-01-02; F-10-01-03; F-10-01-05; F-10-01-16; F-10-01-17; F-10-02-05; F-10-02-06; F-10-02-07; F-10-02-08; F-10-02-10; F-10-03-01; F-10-03-11; F-10-04-03; F-10-04-04; F-10-05-06; F-10-05-10; F-10-05-11; F-10-06-02; F-10-06-03; F-10-06-04; F-10-06-10; F-10-07-05; F-10-07-06; F-10-07-07; F-10-07-10; F-10-07-12; F-10-08-05; F-10-08-06; F-10-08-07; F-10-08-11; F-10-08-12; F-10-09-04; F-10-09-05; F-10-09-06; F-10-10-10; F-10-10-11; F-10-11-07; F-10-12-03; F-10-12-12; F-10-12-13; F-10-12-14; F-11-01-07 When the tow bar interface has been used: The inspection is mandatory before the next flight. When the tow bar interface has never been used: The inspection is mandatory latest 30 days following the issue date of this SB. Flight Design CTLS Maintenance and
Inspection Procedures Manual,
AZ 0430 0003 Supplement Tow Bar
Interface and Operation
to the Aircraft Operating
Instructions (AOI)
SB-ASTM-CTLS-05 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-ASTM-CTLS-01 06-05-2010 Fuel Filter Exchange All serial numbers prior to F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and Maintenance
Manual, CT Aircraft Maintenance
Manual
SB-ASTM-CTLS-02 30-11-2009 Rudder Centring Fork-Control Stop Replacement. F-08-04-09, F-08-04-10, F-08-04-11, F-08-04-12, F-08-04-13, F-08-04-14, F-08-04-15, F-08-04-16, F-08-04-17, F-08-05-08, F-08-05-09, F-08-05-10, F-08-05-11, F-08-05-12, F-08-05-13, F-08-05-14, F-08-05-16, F-08-06-10, F-08-06-11, F-08-06-12, F-08-06-13, F-08-07-04, F-08-07-05, F-08-07-06, F-08-07-07, F-08-07-08, F-08-07-09, F-08-07-10, F-08-07-11, F-08-08-05, F-08-08-06, F-08-08-23, F-08-08-24, F-08-09-03, F-08-09-12, F-08-09-13, F-08-10-19, F-08-10-20, F-08-11-21, F-08-11-22 before the next flight CTLS Maintenance and
Inspections Procedures
Manual
SB-ASTM-CTLS-03 30-11-2009 Rudder Centring Fork-Control Stop Replacement. F-08-10-21, F-08-11-20, F-08-11-28, F-08-12-17, F-09-01-08, F-09-01-09, F-09-01-10, F-09-02-10, F-09-02-12, F-09-02-13, F-09-02-16, F-09-03-12, F-09-03-13, F-09-03-14, F-09-03-15, F-09-04-01, F-09-04-06, F-09-04-07, F-09-04-08, F-09-04-09, F-09-04-10, F-09-05-08, F-09-05-09, F-09-06-03, F-09-06-04, F-09-06-16, F-09-07-11, F-09-08-02, F-09-08-05, F-09-08-06, F-09-08-07, F-09-08-15, F-09-08-16, F-09-09-08 before the next flight CTLS Maintenance and
Inspections Procedures
Manual
SN-ASTM-CTLS-01-en 22-09-2008 Information on Usage of Ethanol Blended Fuel all s/n n/a Aircraft Operation
Instructions; Rotax engine
Operators Manual
Service Letters
Download Date Subject Affected Manual Compliance
SL-ASTM-CTLS-02 24-09-2020 Drain Holes in Air Filter Box all s/n prior to next flight n/a

Safety Alerts
Download Date Subject Affected Manual Compliance
SA-LTUL-CTLS-04 19-12-2013 CTLSi Rotax Redundancy Diagnosis All aircrafts with Rotax 912iS installation prior to next flight AF 0430 0030_00 – Supplement S1 to the Flight and Maintenance Manual (FMM) CTLSi with ROTAX 912 iS
SA-LTUL- CTLS-03 07-03-2013 Inspection for applicability of Rotax ASB-912-062UL R1 / ASB-914-044UL R1, ASB-912-062R1 / ASB-914-044R1. All CT type aircrafts with aircraft serial number earlier than x 12 05-02 (excluded, with (x) being the identifier of the relevant model, when applicable), where in addition the engine has been exchanged on aircraft after delivery of the aircraft from the factory. prior to next flight n/a
SA-LTUL-CTLS-02 30-05-2012 Inspection for applicability of Rotax ASB-912-061 / ASB-912-061UL CTLS up to S/N F-12-02-10 prior to next flight n/a
SA-LTUL-CTLS-01 28-11-2011 Checking of the Crankshaft Journal for ROTAX Engine Type 912 and 914 All S/N up to S/N F-11-07-06 (inclusive) before next flight, but at latest before 01 January 2012 n/a
Service Bulletins
Download Date Subject Affected Manual Compliance
SB-LTUL-CTLS-16 30-07-2020 Technische Mitteilung Auflastung CTLS/CTLSi auf 600kg maximales Abfluggewicht alle Maschinen, die dem Kennblatt 61151.4 entsprechen (Seriennummer F-xx-xx-xx) execute by optional n/a
SB-LTUL-CTLS-15 23-12-2019 Repair procedure to additional wires protection F-18-10-52, F-18-10-54, F-18-11-03, F-18-11-04, F-19-03-01, F-19-04-51, F-19-04-55, F-19-05-01, F-19-05-02, F-19-05-05, F-19-05-06, F-19-08-52, F-19-11-01, F-19-11-02, F-19-11-04 within the next 10 hours n/a
SB-LTUL-CTLS-99 15-10-2019 Equipment Manufacturer Notification n/a n/a n/a
SB-LTUL-CTLS-14 26-08-2019 Dynon Autopilot Servo SV42T Inspection and Replacement of Linear Actuator Servo Pulley aircraft equipped with DYNON autopilot before the next flight n/a
SB-LTUL-CTLS-13 06-05-2019 Installation of Reinforcement Plates on 4 Point Harnesses for CTLS Series not limited latest within 6 months following the issue date of this Bulletin, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB-LTUL-CTLS-11 02-10-2015 Verification of Rescue System Cover Installation. CTLS up to serial number F-13-11-02 (including) latest within 3 months following the issue date of this Notification, or at the next annual inspection of the aircraft, whichever comes first. n/a
SB-LTUL-CTLS-12 02-10-2015 Inspection Horizontal Tail. Aircraft S/N that have a horizontal tail produced of Aramid fabric installed with each 10ac0 hrs inspection n/a
SB-LTUL-CTLS-12 02-10-2015 Inspection Horizontal Tail. Aircraft S/N that have a horizontal tail produced of Aramid fabric installed with each 10ac0 hrs inspection n/a
SB-LTUL-CTLS-08 19-05-2011 Tow Bar Markings and Operation F-10-02-01; F-10-02-02; F-10-02-09; F-10-03-10; F-10-05-07; F-10-05-08; F-10-05-09; F-10-06-05; F-10-06-06; F-10-06-09; F-10-07-01; F-10-07-04; F-10-07-08; F-10-08-04; F-10-09-02; F-10-09-03; F-10-09-08; F-10-10-09; F-10-10-12; F-10-12-04; F-10-12-05; F-10-12-06; F-11-01-01; F-11-01-04; F-11-01-15; F-11-01-16; F-11-01-17; F-11-02-02 When the tow bar interface has been used: The inspection is mandatory before the next flight. When the tow bar interface has never been used: The inspection is mandatory latest 30 days following the issue date of this SB. Flight Design CTLS Flight and Maintenance Manual, AZ 0430 0004 Supplement Tow Bar Interface and Operation to the Flight and Maintenance Manual
SB-LTUL-CTLS-07 08-10-2010 Garmin SL30 and SL40 Comm Radio Spurious Emissions Correction All aircraft with Garmin SL30 Garmin SL40 units installed and with aircraft production date earlier than August 2010 (excluded), or when retrofitted with named Garmin units that have been produced by Garmin prior to October 2010 (excluded) mandatory, but without time limit n/a
SB-LTUL-CTLS-03 06-05-2010 Fuel Filter Exchange All serial numbers prior to F-09-02-01 (usage of letters at beginning of S/N started in 2008, therefore all S/N beginning without a letter are affected) before the next flight CT Parts and Maintenance Manual, CT Aircraft Maintenance Manual
SB-LTUL-CTLS-04 30-11-2009 Rudder Centring Fork-Control Stop Replacement. F-08-04-02, F-08-04-03, F-08-04-04, F-08-05-04, F-08-05-07, F-08-05-17, F-08-05-18, F-08-05-19, F-08-06-01, F-08-06-02, F-08-06-03, F-08-06-04, F-08-06-05, F-08-06-17, F-08-06-20, F-08-06-22, F-08-07-01, F-08-07-02, F-08-07-14, F-08-07-19, F-08-07-20, F-08-07-21, F-08-07-22, F-08-07-24, F-08-07-25, F-08-08-01, F-08-08-03, F-08-08-16, F-08-08-25, F-08-09-07, F-08-09-19, F-08-09-23, F-08-09-24, F-08-10-25 before the next flight n/a
SB-LTUL-CTLS-05 30-11-2009 Stopper device of rudder centring device exchange. F-08-10-26, F-08-10-28, F-08-11-17, F-08-11-18, F-08-11-19, F-09-01-12, F-09-01-13, F-09-02-09, F-09-02-14, F-09-03-02, F-09-03-05, F-09-03-06, F-09-03-07, F-09-03-08, F-09-03-16, F-09-04-02, F-09-04-03, F-09-05-02, F-09-05-03, F-09-05-16, F-09-06-01, F-09-07-03, F-09-07-08, F-09-07-09, F-09-07-12, F-09-09-03, F-09-09-04, F-09-09-05, F-09-09-07 before the next flight n/a
SB-LTUL-CTLS-01-en 15-10-2008 Inspection of Neuform 3-Bladed Variable Pitch Propeller Installation All aircrafts equipped with Neuform 3-blade Variable Pitch Propeller before the next flight n/a
SB-LTUL-CTLS-02-en 15-10-2008 Enhancement of Permissible Speed for CTLS 07-11-12, 07-11-14, 07-11-25, 07-12-01, 07-12-02, 07-12-17, 07-12-18, 08-01-20, 08-01-21, 08-01-22, 08-01-23 no time limits CTLS Flight and Maintenance Manual
Service Notifications
Download Date Subject Affected Manual Compliance
SN-LTUL-CTLS-05 13-04-2016 Spare Parts Availability not limited n/a n/a
SN-LTUL-CTLS-04 15-05-2015 Supporting Information to Engine Start-Up of Rotax 912 iS on Flight Design Aircraft All aircraft with any version of engine Rotax 912 iS series installed n/a Supplement to the Aircraft Operating Instructions with Rotax 912 iS engine – relevant document and version applicable to the individual aircraft
SN-LTUL-CTLS-02 28-03-2011 Elimination of Noise in Radio from Dynon SkyView SV-D1000 F-10-05-09; F-10-06-06; F-10-07-04; F-10-07-08; F-10-09-02; F-10-09-03; F-10-09-08; F-10-10-12; F-11-01-04; on condition only, when noise is present n/a
SN-LTUL-CTLS-01-en 22-09-2008 Information on Usage of Ethanol Blended Fuel all s/n n/a Aircraft Operation Instructions; Rotax engine Operators Manual
Service Letters
Download Date Subject Affected Manual Compliance
SL-LTUL-CTLS-02 24-09-2020 Drain Holes in Air Filter Box all s/n prior to next flight n/a

Not applicable

Safety Alerts
Download Date Subject Affected Manual Compliance
SB-CTLS-ELA-001 23-12-2019 Repair procedure to additional wires protection F-18-08-51, F-18-08-52, F-18-11-05, F-19-08-51, F-18-09-01 within the next 10 hours n/a