| | | SERVICE INFORMATION LIST |
| | | | | | |
Doc. No. | | | Description | Rev. | Date | Downl. |
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 | | | EASA-AD 2010-0235: Rear passenger door retaining bracket - Replacement | - | 2010 -11-22 | 
|
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 | NEW
|