| SERVICE INFORMATION LIST |
| | | | |
Doc. No. | Description | Rev. | Date | Downl. |
SI42-001/4 | Descriptions of DAI technical publication systems and handling of documents
| 4 | 2024-03-21
| 
|
SI42-002/5
| Software for Garmin G1000
| 5
| 2005-04-20
| N/A |
SI42-003/1
| Software for TAE engine
| 1
| 2005-04-06
| N/A |
SI42-004 | TAE SB 125-0011, Rev. 1, Exchange of the clutch disk | - | 2005-06-10 |
|
SI42-005 | TAE SB 125-0003, Rev. 5, Oil pressure sensor | - | 2005-06-10 |
|
SI42-006 | TAE SB 125-0011, Rev. 2, Exchange of the clutch disk | - | 2005-06-13 |
|
SI42-007 | TAE SB 125-0011, Rev. 3, Exchange of the clutch disk | - | 2005-06-14 |
|
SI42-008 | TAE SB 125-0003, Rev. 6, Oil pressure sensor | - | 2005-06-17 |
|
SI42-009 | New TAE Operation & Maintenance Manual OM-02-01 Version 3/0 | - | 2005-07-07 |
|
SI42-010 | Garmin Service Alert - Direct-To waypoint selection | - | 2005-08-01 |
|
SI42-011 | Garmin SB 0522 Rev. B - G1000 Covers on GIA 63 units | - | 2005-08-24 |
|
SI42-012 | TAE SB 125-0007, Coolant exchange interval not applicable | - | 2005-09-12 |
|
SI42-014 | New 2005 IGRF Magnetic Field Model for G1000, Garmin MSB 0533 | - | 2005-11-30 |
|
SI42-015 | Exchange of safety walk | - | 2005-11-08 |
|
SI42-016 | Garmin G1000 System Software Version Update | - | 2005-11-17 |
|
SI42-018 | Garmin G1000 System Software Version Update | - | 2005-12-22 |
|
SI42-020 | EASA AD 2006-0044 - TAE | - | 2006-02-27 |
|
SI42-021 | Clarification of use of AFM-TR-MÄM-42-103 resp. AFM-TR-MÄM-42-111/a (One Engine Inoperative Climb Performance) | - | 2006-03-17 |
|
SI42-023 | Garmin SA: GDC 74A Pitot Static Test | - | 2006-05-04 |
|
SI42-024 | Various TAE publications | - | 2006-05-04 |
|
SI42-025 | Garmin G1000 System Software Version Update | - | 2006-05-10 |
|
SI42-026 | Various TAE publications | - | 2006-05-11 |
|
SI42-028 | Thielert TM TAE 125-0015 Rev. 1 | - | 2006-05-19 |
|
SI42-029 | Thielert TM TAE 125-0015 Rev. 2 | - | 2006-05-31 |
|
SI42-031 | EASA AD: Engine - Propeller System Check Valve Bracket Installation | - | 2006-09-06 |
|
SI42-032 | Thielert TM TAE 125-0016 Rev 0; Adaptor Catch Tank | - | 2006-10-05 |
|
SI42-033 | Various TAE Publications | - | 2006-12-07 |
|
SI42-034 | Garmin SA 0701, Multiple Initial Approach Fixes in the Transition List | - | 2007-01-22 |
|
SI42-035 | Electronic Checklist | - | 2007-01-29 |
|
SI42-036 | EASA-AD: Auxiliary Fuel Tank Venting - Inspection/Modification | - | 2007-02-26 |
|
SI42-037 | Garmin Service Alert 070227-00 | - | 2007-03-02 |
|
SI42-038 | MSB42-039 Retrofit Breather Line | - | 2007-04-17 |
|
SI42-039 | Various TAE Publications | - | 2007-07-06 |
|
SI42-040 | Starting Engine With External Power | - | 2007-03-09 |
|
SI42-041 | Garmin SB Nr. 0710 Rev. A, GTX 33/33D units - Mod Level Change | - | 2007-05-29 |
|
SI42-042 | Thielert SB-TM-TAE 125-1001 Priority 1, Exchanging the Chain Tensioner | - | 2007-06-15 |
|
SI42-043 | Thielert TM TAE 125-0016 Rev 1; Adaptor Catch Tank | - | 2007-06-18 |
|
SI42-044 | EASA-AD: ECU Backup Batteries Installation (TAE125-01 and TAE125-02-99 engines) | - | 2007-07-04 |
|
SI42-045 | EASA-AD: ECU Backup Batteries Installation (DA42) | - | 2007-07-04 |
|
SI42-046 | Garmin Service Advisory 070816-00, GRS 77 | - | 2007-08-17 |
|
SI42-047 | EASA-AD Rev.: ECU Backup Batteries Installation (DA42) | - | 2007-08-30 |
|
SI42-048 | Garmin Service Bulletin No. 0735, GRS 77 | - | 2007-09-10 |
|
SI42-049 | Garmin Service Bulletin No. 0736, G1000 System ID Tool | - | 2007-09-13 |
|
SI42-050 | Thielert SB-TM-TAE 125-1003 Priority 1, Exchanging the Mounting Brackets of the Injectors | - | 2007-09-17 |
|
SI42-051 | Thielert SB-TM-TAE 125-1004 Priority 1, Removing the Small O-Ring of the Oil Filter Module | - | 2007-09-17 |
|
SI42-052 | EASA-AD: Catch Tank (Sump) Filter Adaptor Installation | - | 2007-09-26 |
|
SI42-053 | EASA Service Information Notice 2007-34; Use of Non-Approved Gearbox Oil in TAE 125 Series Engines | - | 2007-10-11 |
|
SI42-054 | Transponder Airborne Status | - | 2007-10-25 |
|
SI42-055 | EASA-AD Rev.: Engine Control Unit Back-up Batteries Installation | - | 2007-11-07 |
|
SI42-057 | Miscellaneous TAE Publications | - | 2007-12-18 |
|
SI42-058 | Thielert SB-TM-TAE 125-0017; Piston Cooling Nozzle Inspection, Rev. 0 | - | 2007-12-17 |
|
SI42-059 | Thielert SB-TM-TAE 125-0017; Piston Cooling Nozzle Inspection, Rev. 1 | - | 2008-01-07 |
|
SI42-060 | EASA-AD 2008-0016: Piston Cooling Nozzles - Inspection | - | 2008-01-22 |
|
SI42-061 | Thielert SB-TM-TAE 125-1003 Priority 1; Exchanging the Mounting Brackets of the Injectors | - | 2008-01-24 |
|
SI42-062 | Garmin Service Alert No. 0801, Supplemental Data Cards | - | 2008-02-11 |
|
SI42-063/1 | EASA Emergency AD: Thielert SB-TM-TAE 125-1005 Priority 1 Rev.1; Installation of Bracket High-Pressure Fuel Line | - | 2008-02-13 |
|
SI42-064 | Thielert SB-TM-TAE 125-0017; Piston Cooling Nozzle Inspection, Rev. 2 | - | 2008-02-25 |
|
SI42-065 | EASA-AD 2008-0016 R1: Piston Cooling Nozzles - Inspection | - | 2008-02-25 |
|
SI42-066 | Thielert SB-TM-TAE 125-1005 Priority 1 Rev.2; Installation of Bracket High-Pressure Fuel Line | - | 2008-03-06 |
|
SI42-067 | EASA Emergency AD: Thielert SB-TM-TAE 125-1005 Priority 1 Rev.2; Installation of Bracket High-Pressure Fuel Line | - | 2008-03-07 |
|
SI42-068 | Garmin Service Advisory 0806 Rev. A, G1000 Transponder Flight Identification Operation | - | 2008-03-18 |
|
SI42-069 | EASA Emergency AD 2008-0056R1-E: Thielert SB-TM-TAE 125-1005 Priority 1 Rev.2; Installation of Bracket High-Pressure Fuel Line | - | 2008-03-19 |
|
SI42-070 | Garmin Service Advisory 0806 Rev. B, G1000 Transponder Flight Identification Operation | - | 2008-03-20 |
|
SI42-071 | FADEC Test sequence | - | 2008-03-28 |
|
SI42-072 | EASA-AD 2008-0086, Exchange of the Aileron Bellcrank and Bent Rod Ends, MSB42-043/1 | - | 2008-05-13 |
|
SI42-073 | FAA-AD 2008-02-06, Garmin Service Bulletin No. 0713 Rev. D, GSB 85 Inspection Procedure | - | 2008-05-14 |
|
SI42-074 | Thielert SB-TM-TAE 125-1006 Priority 1; Clutch Inspection | - | 2008-05-23 |
|
SI42-075 | EASA Emergency AD 2008-0100-E: Thielert SB-TM-TAE 125-1006 Priority 1; Clutch Assembly, Inspection/Replacement | - | 2008-05-26 |
|
SI42-076/1 | Thielert SB-TM-TAE 125-1006 Priority 1, Rev. 1; Replace Clutch | 1 | 2008-05-30 |
|
SI42-077 | EASA Emergency AD 2008-0106-E: Thielert SB-TM-TAE 125-1006 Priority 1, Rev. 1; Clutch Assembly, Replacement | - | 2008-05-30 |
|
SI42-078/1 | Honeywell Service Bulletin KAP 140-22-102, Reduce the possibility of intermittent failures because of top cover on KC 140 | 1 | 2008-10-27 |
|
SI42-079/1 | Honeywell Service Bulletin KC 140-22-102, Replace top cover to make sure connector pins engage correctly | 1 | 2008-10-27 |
|
SI42-080 | Thielert SB-TM-TAE 125-0018, Proportional pressure reducing valve | - | 2008-06-20 |
|
SI42-081 | EASA-AD 2008-0128, Operation & Maintenance Manual OM-02-01 for TAE 125-01 engine | - | 2008-07-28 |
|
SI42-082 | Garmin Service Bulletin No. 0823, GDU 104X CRS/BARO Knob Interference | - | 2008-07-17 |
|
SI42-083 | Garmin Service Alert No. 0824, GDU 104X CRS/BARO Knob Interference | - | 2008-07-17 |
|
SI42-084 | Thielert SB-TM-TAE 125-0018, Proportional pressure reducing valve | - | 2008-07-14 |
|
SI42-085 | EASA-AD 2008-0130, Replacement of the propeller control valve | - | 2008-07-15 |
|
SI42-086 | EASA-AD 2008-0136, Lightning strike procedure in the DA 42 and DA 42 M Airplane Flight Manual | - | 2008-07-25 |
|
SI42-087 | Garmin Service Bulletin No. 0823 Rev. B, GDU 104X CRS/BARO Knob Interference | - | 2008-08-05 |
|
SI42-088 | Garmin Service Alert No. 0824 Rev. B, GDU 104X CRS/BARO Knob Interference | - | 2008-08-05 |
|
SI42-089 | EASA-AD 2008-0139, Repetitive inspection and further on the replacement of the rear engine support bracket mounting bolts | - | 2008-07-25 |
|
SI42-090 | EASA-AD 2008-0145, Replacement of the propeller control valve | - | 2008-08-26 |
|
SI42-091 | EASA-AD 2008-0136R1, Lightning strike procedure in the DA 42 and DA 42 M Airplane Flight Manual | - | 2008-10-27 |
|
SI42-092 | Thielert SB-TM-TAE 125-1008 Priority 1, Replacing the Rail Pressure Control Valve and Modifying th VRail Plug | - | 2008-09-25 |
|
SI42-093 | Thielert SB-TM-TAE 125-1008 Priority 1 Rev. 1, Replacing the Rail Pressure Control Valve and Modifying th VRail Plug | - | 2008-09-30 |
|
SI42-094 | Garmin Software Service Bulletin No. 0836 Rev. A, G1000 System Software Version Update | - | 2008-10-17 |
|
SI42-095 | Garmin Service Advisory 0806 Rev. C, Transponder Flight Identification Operation | - | 2008-10-24 |
|
SI42-096 | Honeywell-SB KS 270C-22-09, Exchange of the tach generator | - | 2008-10-27 |
|
SI42-097 | Honeywell-SB KS 271C-22-10, Exchange of the tach generator | - | 2008-10-27 |
|
SI42-098 | Engine failures caused by improper draining of the fuel system during the pre flight inspection | - | 2008-10-30 |
|
SI42-099 | Thielert SB-TM-TAE 125-0018 Rev. 1, Proportional pressure reducing valve (Propeller control valve) | - | 2008-11-17 |
|
SI42-100 | Thielert SB-TM-TAE 125-1007 Priority 1 Rev. 1, Proportional pressure reducing valve (Propeller control valve) | - | 2008-11-17 |
|
SI42-101 | Garmin Software Service Bulletin No. 0849 Rev. A, G1000 System Software Version Update | - | 2009-01-23 |
|
SI42-102 | Garmin Service Advisory No. 0908 Rev. A, Garmin Integrated Flight Deck Systems Equipped with the Honeywell Model KN63 DME | - | 2009-03-16 |
|
SI42-103 | Garmin Software Service Bulletin No. 0849 Rev. B, G1000 System Software Version Update | - | 2009-04-21 |
|
SI42-105 | Garmin Service Advisory No. 0914 Rev. A, Possible temporary loss of heading/attitude information
| - | 2009-05-08
|
|
SI42-106 | Garmin Service Advisory No. 0915 Rev. A, Navigation suspending during non-precision approaches | - | 2009-05-11 |
|
SI42-107 | Thielert SB-TM-TAE 125-1007 Priority 1 Rev. 2, Proportional pressure reducing valve (Propeller control valve) | - | 2009-05-26 |
|
SI42-108 | Garmin Software Service Bulletin No. 0849 Rev. C, G1000 System Software Version Update | - | 2009-06-26 |
|
SI42-109 | Garmin Service Advisory No. 0922 Rev. A, VOR or LOC/ILS Approaches | - | 2009-07-08 |
|
SI42-110 | EASA-AD 2009-0151, Thielert SB-TM-TAE 125-1009 Priority 1, Propeller Control - Constant Speed Unit - Vibration Isolator | - | 2009-07-13 |
|
SI42-111 | Garmin Service Advisory No. 0929 Rev. A, Momentary failure indications (Red-X) can occur when deleting stored data | - | 2009-07-13 |
|
SI42-112 | EASA-AD 2009-0145R1 , Replacement of the propeller control valve | - | 2009-07-24 |
|
SI42-113
| Thielert SB-TM-TAE 125-1009 Priority 1 Rev. 1, Constant Speed Unit - Vibration Isolator | - | 2009-08-18
|
|
SI42-114
| EASA-AD 2008-0215 , Replacement of Rail Pressure Control Valve - Modification of VRail Plug | - | 2009-08-19
|
|
SI42-115 | Thielert SB-TM-TAE 125-0020, Constant Speed Unit - Vibration Isolator | - | 2009-08-24 |
|
SI42-116 | EASA-AD 2009-0193 , Constant Speed Unit - Vibration Isolator | - | 2009-08-28 |
|
SI42-117 | Thielert SB-TM-TAE 125-1009 Priority 1 Rev. 2, Constant Speed Unit - Vibration Isolator | - | 2009-09-02 | |
SI42-118
| Illustrated Parts Catalogue (IPC) - Change of the available media
| - | 2009-10-05 |
|
SI42-119 | Thielert SB-TM-TAE 125-1009 Priority 1 Rev. 3, Constant Speed Unit - Vibration Isolator | - | 2009-10-16 | |
SI42-120 | Thielert TM TAE Various Documents
| - | 2010-02-22
|
|
SI42-121 | EASA-AD, Constant Speed Unit - Vibration Isolator | - | 2009-1 1-03 | |
SI42-122
| Garmin Mandatory Service Bulletin No. 0823 Rev. C, GDU 104X CRS/BARO Knob Interference
| - | 2009-1 2-09 |
|
SI42-123
| Garmin Service Alert No. 0824 Rev. C, GDU 104X CRS/BARO Knob Interference
| - | 2009-1 2-09 |
|
SI42-124 | Thielert SB-TM-TAE 125-0020 Rev. 1, Constant Speed Unit - Vibration Is | - | 2009-1 2-01 |
|
SI42-125
| EASA-AD 2009-0193R1, Constant Speed Unit - Vibration Isolator
| - | 2009-1 2-11 |
|
SI42-126
| FAA-AD 2009-24-10, To prevent engine in-flight shutdown
| - | 2009-1 2-09 |
|
SI42-127 | Airplane Maintenance Manual Chapter 12-30: Conservation of Exterior Parts | - | 2009 -1 2-11 |
|
SI42-128 | Thielert SB-TM-TAE 125-0017 Rev. 3, Piston Cooling Nozzles | - | 2010 -03 -08
|
|
SI42-129 | FAA-AD 2010-04-06: To prevent engine in-flight shutdown | - | 2010 -03 -15 |
|
SI42-130 | Thielert SB-TM-TAE 125-1010 P1 Initial Issue, Replace timing Chain | - | 2010 -04 -12 |
|
SI42-132 | FAA-AD 2010-06-12: To prevent engine in-flight shutdown | - | 2010 -07 -06 |
|
SI42-133 | Thielert SB-TM-TAE 125-1010 P1 Rev. 2, Replace timing Chain | - | 2010 -06 -08 |
|
SI42-134 | Thielert SB-TM-TAE 125-1011-P1 Initial Issue & SB-TM-TAE 125-0021 Initial Issue, Replacement Clutch | - | 2010 -06 -10 |
|
SI42-135 | EASA-EAD 2010-0111-E: Thielert SB-TM-TAE 125-1011-P1 Initial Issue & SB-TM-TAE 125-0021 Initial Issue, Replacement Clutch | - | 2010 -06 -10 |
|
SI42-136 | EASA-EAD 2010-0111-E [Corrected 11 June 2010]: Thielert SB-TM-TAE 125-1011-P1 Initial Issue & SB-TM-TAE 125-0021 Initial Issue, Replacement Clutch | - | 2010 -06 -14 |
|
SI42-137 | FAA-AD 2010-11-09: To prevent engine in-flight shutdown | - | 2010 -06 -14 |
|
SI42-138 | EASA-AD 2010-0136: Engine - Timing Chain - Replacement | - | 2010 -07 -06 |
|
SI42-139 | EASA-AD 2010-0137: ReplacEngine - FADEC Software - Modification | - | 2010 -07 -06 |
|
SI42-140 | EASA-AD 2010-0155: Main Landing Gear Damper-to-Trailing Arm Joints - Inspection/Replacement | - | 2010 -08 -09 |
|
SI42-141 | Garmin Service Bulletin Nr. 1031 Rev. A, G1000 System Software Version 0370.22 Update | - | 2010 -08 -25 |
|
SI42-142 | Garmin Service Bulletin Nr. 1032 Rev. A, G1000 Synthetic Vision & Pathways Activation | - | 2010 -08 -25 |
|
SI42-143 | FAA-AD 2010-18-02: To prevent engine in-flight shutdown leading to loss of control of the airplane | - | 2010 -08 -26 |
|
SI42-144 | EASA-AD 2010-0155R1: Main Landing Gear Damper-to-Trailing Arm Joints - Inspection/Replacement | - | 2010 -09 -14 | 
|
SI42-145 | Update of TAE Repair Manual RM-02-01 Issue 4 Revision 7 | - | 2010 -11-08 |
|
SI42-146 | Thielert SB-TM-TAE 125-1009 P1 Rev. 4, Constant Speed Unit - Vibration Isolator | - | 2010 -11-08 |
|
SI42-147 | Removal and installation of passenger seat | - | 2011 -03-30 |
|
SI42-148/1 | EASA-AD 2010-0235R1: Rear passenger door retaining bracket - Replacement | 1 | 2014-03-04 |
|
SI42-150 | EASA-AD 2010-0020: Main Landing Gear Damper-to-Trailing Arm Joints - Inspection/Replacement | - | 2011-07-02 |
|
SI42-151 | Garmin Service Advisory No. 1051 Rev. A, 2010 IGRF (International Geomagnetic Reference Field) Magnetic Field Model | - | 2011-02-10 |
|
SI42-152 | FAA-AD 2011-05-06: To prevent engine in-flight shutdown leading to loss of control of the airplane | - | 2011-02-24 |
|
SI42-153 | FAA-AD 2011-07-09: FADEC Software, to prevent engine in-flight shutdown or power loss | - | 2011-05-02 |
|
SI42-154 | EASA-EAD 2011-0087-E: Thielert SB-TM-TAE 125-1013-P1 Initial Issue, Friction Disc
| - | 2011-05-13 |
|
SI42-155 | FAA-AD 2011-10-13: To correct the rear passenger door locking mechanism | - | 2011-05-16 |
|
SI42-156 | Garmin Service Advisory No. 1118 Rev. A, Momentary failure indications (Red-X) can occur when sorting stored flight plans
| - | 2011-05-17 |
|
SI42-157 | Garmin Service Advisory No. 1129 Rev. A, Momentary loss of GRS 77/77H and GDC 74A/74B/74H functions | - | 2011-05-31 |
|
SI42-158 | EASA-AD 2011-0100: Wings - Upper Centre Wing Skin-to-Spar Adhesive Joint - Inspection / Repair
| - | 2011-05-31 |
|
SI42-159 | FAA-AD 2011-11-07: To prevent failure of the joint and subsequent damage or malfunction of the MLG
| - | 2011-06-17 |
|
SI42-160 | EASA-AD 2011-0152-E: Engine - Clutch Assembly - Identification / Replacement
| - | 2011-08-19 |
|
SI42-161 | Thielert SB-TM-TAE 000-0004 Rev. 124, TAE-Manuals in effect
| - | 2011-09-21 |
|
SI42-162 | FAA-AD 2011-23-01: Engine - Clutch Assembly - Identification / Replacement
| - | 2011-11-14 |
|
SI42-163 | Thielert SB-TM-TAE 000-0004 Rev. 126, TAE-Manuals in effect
| - | 2011-11-18 |
|
SI42-164 | FAA-AD 2010-06-12R1: Replacement of the existing rail pressure control valve with an improved rail pressure control valve | - | 2012-01-09 |
|
SI42-165 | FAA-AD 2012-02-05: Inspection and replacement of the friction disc | - | 2012-01-31 |
|
SI42-166 | Thielert SB-TM-TAE 125-1014 P1 Initial Issue, Connecting Pin Waste Gate Lever | - | 2012-02-27 |
|
SI42-167 | EASA-AD 2011-0020R2: Main Landing Gear Damper-to-Trailing Arm Joints - Inspection/Replacement | - | 2012-03-01 |
|
SI42-168 | FAA-AD 2010-11-09R1: Exchange of the proportional pressure reducing valves also known as propeller control valves | - | 2012-03-08 |
|
SI42-169 | Thielert SB-TM-TAE 125-1015 P1 Initial Issue, Gearbox Oil Filling Plug | - | 2012-05-02 |
|
SI42-170 | Garmin Service Bulletin No. 1210 Rev. A, SafeTaxi® Availability In Europe | - | 2012-05-22 |
|
SI42-171 | EASA-AD 2012-0112: One-Time Inspection of the Gearbox Oil Filling Plug at certain gearbox serial numbers | | 2012-06-26 |
|
SI42-172 | EASA-AD 2012-0116: FADEC Software Modification | - | 2012-07-09 |
|
SI42-173 | Thielert SB-TM-TAE 125-0022 Initial Issue, sealing of an assembly opening in the crankcase | - | 2012-08-21 |
|
SI42-174 | EASA-AD 2012-0174: Modification of the main landing gear damper | - | 2012-09-12 |
|
SI42-175 | FAA-AD 2012-17-07: Inspection and if necessary the repair of the upper centre wing skin-to-spar adhesive joint | - | 2012-09-12 |
|
SI42-176 | Garmin Service Alert No. 1228, SIDs and STARs non-JETs Limitation | - | 2012-11-06 |
|
SI42-177 | FAA-AD 2012-26-12: One-Time Inspection of the Gearbox Oil Filling Plug vent hole | - | 2013-01-11 |
|
SI42-178 | FAA-AD 2012-26-13: Full Authority Digital Engine Control Software Modification | - | 2013-01-11 |
|
SI42-179 | Identification of stainless steel control cables | - | 2013-02-08 |
|
SI42-180/1 | EASA-AD 2013-0020R3: Inspection of the markings of the safety belts | 1 | 2014-04-08 |
|
SI42-181 | MT-Propeller Service Bulletin No. 27, Inspection and modification of certain governor type- and serial numbers | - | 2013-02-28 |
|
SI42-182 | Garmin Service Advisory No. 1309, Verification of displayed heading is not noticeable drifting prior Take-Off | - | 2013-03-04 |
|
SI42-183 | Thielert SB-TM-TAE 125-1017 P1 Initial Issue, Replacement of the High Pressure Pump with an improved design for engines operated in certain countries | - | 2013-04-17 |
|
SI42-184 | Garmin Service Advisory No. 1309 Rev. B, Verification of displayed heading is not noticeable drifting prior Take-Off | - | 2013-04-12 |
|
SI42-185 | FAA-AD 2013-07-01: Modification of the main landing gear damper | - | 2013-04-17 |
|
SI42-186 | EASA-AD 2013-0109: Sealing of the crankcase assembly opening located under the coolant tank | - | 2013-05-24 |
|
SI42-187 | EASA-AD 2013-0121: Inspection to identify certain Nose Landing Gear Actuator P/N | - | 2013-06-05 |
|
SI42-188/1 | Garmin Terrain Data Alert No. 1351 Rev. B, Anomalies when using Synthetic Vision Technology in Northwest Greenland | 1 | 2015-03-03 |
|
SI42-189 | Garmin Service Advisory No. 1352 Rev. A, Course deviation indicator (CDI) may deflect in the wrong direction in certain situations | - | 2013-09-26 |
|
SI42-190 | FAA-AD 2013-19-11: Inspection/modification of the Nose Landing Gear Actuator | - | 2013-09-27 |
|
SI42-191 | United Instruments Inc. Service Bulletin No. 12, Paint on dial may crack and separate from the surface | - | 2013-10-31 |
|
SI42-192 | Main Landing Gear Extension/Retraction Mechanism | - | 2013-11-19 |
|
SI42-193 | Garmin Service Advisory No. 1363 Rev. A, User-modified terminal procedure stored in a Flight Plan may cause error condition | - | 2013-11-21 |
|
SI42-194 | FAA-AD 2013-24-06: Requires applying sealant to close the engine clutch housing (crankcase assembly) opening | - | 2013-12-05 |
|
SI42-195 | EASA-AD 2013-0279: Replacement of the high pressure fuel pump with an improved design | - | 2013-12-05 |
|
SI42-196 | Garmin Service Advisory No. 1372 Rev. A, Unavailable RNAV (GPS) approaches due to lack of VDA | - | 2013-12-18 |
|
SI42-197 | FAA-AD 2014-17-03: Replacement of the high pressure fuel pump with an improved design | - | 2014-09-05 |
|
SI42-198 | EASA-AD 2014-0232: Engine - Clutch Assembly - Identification / Replacement | - | 2014-11-06 |
|
SI42-199 | FAA-AD 2015-02-01: Replacement of certain P/N and S/N clutch assemblies
| - | 2015-02-09 |
|
SI42-200 | EASA-AD 2015-0055: Starting – Software Mapping / Start Phase Monitoring System
| - | 2015-04-01 |
|
SI42-201 | Garmin Service Alert No. 1538 Rev. A, Operations with Altimeter Set to QFE (height above field elevation)
| - | 2015-08-12 |
|
SI42-202 | EASA-AD 2015-0189: Reduced inspection interval of certain fuel feed pump part numbers | - | 2015-09-22 |
|
SI42-203 | Technify Motors SB Nr. 125-1019 P1, Replacement of certain Integral Exhaust Manifold part numbers at specific engine serial numbers
| - | 2015-09-24 |
|
SI42-204 | FAA-AD 2015-21-01: Start phase monitoring system
| - | 2016-01-12 |
|
SI42-205 | Technify Motors SB No. TMG 125-1020 P1, Replacement of the clutch by a dual mass flywheel, inspection and, if necessary the replacement, of the gearbox for oil leakage and moisture
| - | 2016-02-01 |
|
SI42-206 | FAA-AD 2016-07-19: Replacement of certain fuel feed pump part numbers at TAE 125-02 engines
| - | 2016-04-07 |
|
SI42-207 | United Instruments Inc. SB No. 13, Specific 5934 Series Altimeters manufactured between January 2015 and February 2016 are susceptible to develop a slow diaphragm leak which would affect the accuracy of the altimeters
| - | 2016-04-29 |
|
SI42-208 | Garmin Service Advisory No. 1372 Rev. B, unavailable RNAV (GPS) approaches
| - | 2016-06-24 |
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SI42-209 | Garmin Service Advisory No. 1612 Rev. A, Update of the IGRF (International Geomagnetic Reference Field) Magnetic Field Model from base year 2010 to 2015
| - | 2016-07-15 |
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SI42-210/1 | EASA-AD 2016-0156R1: Modification if certain exhaust pipe part numbers are installed
| 1 | 2016-11-25 |
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SI42-211 | Technify Motors SB No. TMG 125-1021 P1, Fixing the wastegate lever bushing
| - | 2016-11-04 |
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SI42-212 | Garmin Software SB No. 0533 Rev. C, update of the IGRF (International Geomagnetic Reference Field) Magnetic Field Model
| - | 2016-11-17 |
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SI42-213 | FAA-AD 2017-01-12: Modification if certain exhaust pipe part numbers are installed
| | 2017-02-01 |
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SI42-214/1 | EASA-AD 2017-0034R1: Inspection and, if necessary, replacement of certain gearbox serial numbers
| 1 | 2018-03-05 |
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SI42-215 | FAA-AD 2017-04-06: Certain altimeters displaying higher than actual altitude due to a slow diaphragm leak which were examined in United Instruments SB No. 13
| - | 2017-03-24 |
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SI42-216 | EASA-AD 2017-0074: Inspections and modification of the flap control system, repetitive inspections of the flap bell crank, and, depending on the findings, replacement of the flap bell crank with an improved design
| - | 2017-05-02 |
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SI42-217 | EASA-AD 2017-0090: Additional repetitive inspections of the engine exhaust pipe
| - | 2017-05-23 |
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SI42-218/1 | FAA-AD 2017-11-08: Additional repetitive inspections of the engine exhaust pipe
| 1 | 2017-06-19 |
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SI42-219 | EASA-AD 2017-0120: Additional repetitive inspections of the engine exhaust pipe
| - | 2017-07-13 |
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SI42-220 | FAA-AD 2017-15-09: Additional repetitive inspections of the engine exhaust pipe
| - | 2017-10-20 |
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SI42-221 | FAA-AD 2017-18-10: Inspections and modification of the flap control system, repetitive inspections of the flap bell crank
| - | 2017-10-30 |
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SI42-222 | FAA-AD 2017-19-15: Replacement of the clutch by a dual mass flywheel, inspection and, if necessary the replacement, of the gearbox for oil leakage and moisture at certain gearbox Serial numbers
| - | 2017-10-31 |
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SI42-223 | FAA Special Airworthiness Information Bulletin (SAIB) NE-17-26, Display of intruder aircraft vertical trend indications | - | 2017-10-30 |
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SI42-224 | EASA-AD 2017-0254: Modification and/or inspection of the engine exhaust pipe | - | 2018-01-25 |
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SI42-225 | Technify Motors issued Priority 1 - Safety SB No. TMG 125-1022 P1, Replacement of rail pressure regulating valve | - | 2018-03-05 |
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SI42-226 | FAA-AD 2018-10-10: Modification and/or inspection of the engine exhaust pipe | - | 2018-06-25 |
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SI42-227 | In the aircraft assembly line residue from manufacturing of the air filter was found in the charged air system | - | 2018-09-20 |
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SI42-228 | Garmin Service Advisory No. 1905 Rev. A, GPS roll over | - | 2019-01-14 |
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SI42-229 | EASA-AD 2019-0066: Inspection of the nose landing gear assembly | - | 2019-03-27 |
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SI42-230 | EASA-AD 2019-0218: Rreplacement of Fuel Tank Connection Hoses | - | 2019-08-07 |
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SI42-231 | EASA-AD 2019-0235: Inspection, modification or replacement of the Emergency Locator Transmitter (ELT) C406 | - | 2019-11-06 |
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SI42-232 | EASA-AD 2019-0302: Repetitive inspections for correct installation of the self-locking nut to the Rudder T-yoke axle bolt | - | 2019-12-16 |
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SI42-233 | EASA-AD 2020-0008: Repetitive inspections of the flap bell crank assembly and if necessary replacement with an improved part | - | 2020-01-21 |
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SI42-234 | CAT Priority 1 Safety SB CG 125-1026 P1, Replacement of timing chain for TAE 125-02-114 version 01 engines | - | 2020-11-20 |
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SI42-235 | CAT Priority 1 Safety SB CG 125-1027 P1, Replacement of the main bearing studs | - | 2020-12-18 |
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SI42-236 | EASA-AD 2021-0022: Replacement of the main bearing studs | - | 2021-01-19 |
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SI42-237 | CAT Priority 1 Safety SB CG 125-1027 P1 Rev. 1, Replacement of the main bearing studs | - | 2021-08-19 |
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SI42-239 | CAT Priority 1 Safety SB CG 125-1028 P1, Inspection of the cylinder head side cover sealing | - | 2021-09-23 |
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SI42-240 | FAA-AD 2021-22-03: Inspection of the Nose Landing Gear (NLG) actuator attachment | - | 2021-12-16 |
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SI42-241 | FAA-AD 2022-03-01: Replacement of Fuel Tank Connection Hoses from certain delivery batches according MSB 42-138 and MSB 42NG-080 | - | 2022-02-14 |
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SI42-242 | SIRS Service Information Letter No. SIRS/SIL-CE2-A25-01 Rev.02, Magnetic compass illumination lamp | - | 2022-03-04 |
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SI42-243 | FAA-AD 2022-06-08: Repetitive inspections of the flap bell crank assembly and if necessary replacement with an improved part | - | 2022-04-06 |
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SI42-244 | FAA-AD 2022-21-15: Installation of the T-yoke bolt D60-5320-00-32 | - | 2022-11-02 |
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SI42-245 | EASA-AD 2023-0013: Inspection and modification of the rudder steering bracket | - | 2023-01-19 |
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SI42-246 | FAA-AD 2023-01-08: Replacement of the main bearing studs | - | 2023-02-03 |
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SI42-247 | Garmin SB No. 22117 Rev. B, Replacement of the cable retention pins at the GSM 86 servo gearbox assembly | - | 2023-03-20 |
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SI42-248 | United Instruments Service Note No. 5934-14, Replacement of nonconforming static port threads | - | 2023-04-17 |
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SI42-249 | Garmin SB No. 0736 Rev. C, G1000 System ID Tool to change the G1000 System ID to a valid System ID | - | 2024-03-08 |
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SI42-250 | FAA-AD 2024-06-13: Inspection and/or installation of the T-yoke bolt D60-5320-00-32 | - | 2024-04-23 |
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SI42-251 | EASA-AD 2023-0013R1: Inspection and/or installation of the T-yoke bolt D60-5320-00-32 | - | 2024-04-29 |
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SI42-252 | Closing and latching the passenger door | - | 2024-08-22 |
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SI42-253 | EASA-AD 2024-0235: Inspection of the passenger door latching mechanism and modification of the airplane | - | 2024-12-09 |
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SI42-254 | Safe Flight Instrument LLC Doc. No. R-4065, Troubleshooting Guide for the Stall Warning System on the DA 42 Aircraft | - | 2025-01-22 |
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SI42-255 | Gas Spring of the passenger door latching mechanism | - | 2025-10-01 | NEW |
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