| SERVICE INFORMATION LIST |
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Doc. No. | Description | Rev. | Date | Downl. |
SI42NG-001/4
| Descriptions of DAI technical publication systems and handling of documents | 4 | 2024-03-21
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SI42NG-005
| Garmin Service Advisory No. 0922 Rev. A, VOR or LOC/ILS Approaches | - | 2009-07-08
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SI42NG-006
| Garmin Service Advisory No. 0929 Rev. A, Momentary failure indications (Red-X) can occur when deleting stored data | - | 2009-07-13
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SI42NG-007
| Garmin Software Service Bulletin No. 0945 Rev. A, G1000 System Software Version 0670.03 Update for G1000-equipped Diamond DA42NG Aircraft | - | 2009-11-04
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SI42NG-008 | Garmin Software Service Bulletin No. 0948 Rev. A, G1000 Synthetic Vision & Pathways Activation | - | 2009-12-03 |
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SI42NG-009
| Garmin Mandatory Service Bulletin No. 0823 Rev. C, GDU 104X CRS/BARO Knob Interference
| - | 2009-12-09
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SI42NG-010 | Garmin Service Alert No. 0824 Rev. C, GDU 104X CRS/BARO Knob Interference | - | 2009-12-09 |
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SI42NG-012 | AE Mandatory Service Bulletin MSB-E4-007, Replacement of Waste Gate Controller | - | 2010-04-07 |
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SI42NG-013 | AE Mandatory Service Bulletin MSB-E4-006, Repair of Sensor Cable for Camshaft Sensor of ECU B | - | 2010-04-07 |
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SI42NG-014 | AE Mandatory Service Bulletin MSB-E4-008, Exchange of oil separator hose between cylinder head cover and oil separator | - | 2010-06-08 |
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SI42NG-015/1 | AE Mandatory Service Bulletin MSB-E4-009, Replacement of the Engine High Pressure Pump | 1 | 2015-05-05 |
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SI42NG-016 | EASA-EAD 2010-0206-E: High Pressure Fuel Pump - Inspection/Replacement | - | 2010-10-12 | 
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SI42NG-017 | FAA-AD 2010-23-09: To prevent engine power loss or in-flight shutdowm | - | 2010-11-15 |
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SI42NG-018 | Removal and installation of passenger seat | - | 2011-03-30 |
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SI42NG-019/1 | EASA-AD 2010-0235R1: Rear passenger door retaining bracket - Replacement | 1 | 2014-03-04 |
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SI42NG-021 | Garmin Service Advisory No. 1051 Rev. A, 2010 IGRF (International Geomagnetic Reference Field) Magnetic Field Model | - | 2011-02-10 |
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SI42NG-022 | EASA-AD 2011-0039: High Pressure Fuel Pump - Inspection/Replacement | - | 2011-03-09 |
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SI42NG-023/1
| Installation and tightening torque of worm drive clamps in the charge-air and liquid cooling system
| 1 | 2013-01-18
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SI42NG-024 | FAA-AD 2011-10-13: To correct the rear passenger door locking mechanism | - | 2011-05-16 |
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SI42NG-025 | Garmin Service Advisory No. 1118 Rev. A, Momentary failure indications (Red-X) can occur when sorting stored flight plans
| - | 2011-05-17 |
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SI42NG-026
| Garmin Service Advisory No. 1129 Rev. A, Momentary loss of GRS 77/77H and GDC 74A/74B/74H functions
| - | 2011-05-31
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SI42NG-027 | EASA-AD 2011-0100: Wings - Upper Centre Wing Skin-to-Spar Adhesive Joint - Inspection / Repair
| - | 2011-05-31 |
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SI42NG-028 | Garmin Service Advisory No. 1029 Rev. D, European Geostationary Navigation Overlay System (EGNOS) Safety-of-Life (SoL) Service is Fully Operational
| - | 2011-06-20 |
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SI42NG-029 | Garmin Service Advisory No. 1141 Rev. A, Garmin SBAS-capable receivers may experience loss of LPV or LNAV/VNAV capability due to incoherent EGNOS satellite GEO ranging data | - | 2011-08-22 |
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SI42NG-030/1 | AE Mandatory Service Bulletin Revision MSB-E4-013/1, Gearbox oil inspection - Additional oil check for early debris indication | 1 | 2011-08-22 |
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SI42NG-031 | FAA-AD 2011-18-19: Replacement of the high pressure fuel pump | - | 2011-09-21 |
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SI42NG-032 | Measures that result from performing Austro Engine Mandatory Service Bulletin MSB-E4-013/1 | - | 2011-11-30 |
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SI42NG-033 | Austro Engine Mandatory Service Bulletin MSB-E4-014/1, Replacement of the Fuel Return Line and Banjo Fitting | - | 2012-04-23 |
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SI42NG-034 | Garmin Service Bulletin No. 1210 Rev. A, SafeTaxi® Availability In Europe | - | 2012-05-22 |
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SI42NG-035 | AE Mandatory Service Bulletin Revision MSB-E4-014/2, Replacement of the Fuel Injector Return Line and the Banjo Fitting | - | 2012-06-18 |
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SI42NG-036 | EASA-AD 2012-0174: Modification of the main landing gear damper | - | 2012-09-12 |
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SI42NG-037 | FAA-AD 2012-17-07: Inspection and if necessary the repair of the upper centre wing skin-to-spar adhesive joint | - | 2012-09-12 |
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SI42NG-038 | Garmin Service Alert No. 1228, SIDs and STARs non-JETs Limitation | - | 2012-11-06 |
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SI42NG-039/1 | Induction System - Abnormal/Emergency Procedures - Alternate Air when encountering Induction Filter Icing | 1 | 2013-01-14 |
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SI42NG-040 | Austro Engine Mandatory Service Bulletin No. MSB-E4-007/3, Replacement of Waste Gate Controller | - | 2012-12-11 |
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SI42NG-041 | EASA-AD 2012-0269: Revision of Normal and Abnormal Procedures of the Airplane Flight Manual in regards of Alternate Air usage | - | 2012-12-20 |
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SI42NG-042 | Identification of stainless steel control cables | - | 2013-02-08 |
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SI42NG-043/1 | EASA-AD 2013-0020R3: Inspection of the markings of the safety belts | 1 | 2014-04-08 |
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SI42NG-044 | MT-Propeller Service Bulletin No. 27, Inspection and modification of certain governor type- and serial numbers | - | 2013-02-28 |
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SI42NG-045 | Garmin Service Advisory No. 1309, Verification of displayed heading is not noticeable drifting prior Take-Off | - | 2013-03-04 |
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SI42NG-046 | EASA-AD 2013-0025: Replacement of certain Waste Gate Controller part numbers with an improved design at its E4 engines
| - | 2013-03-14 |
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SI42NG-047 | FAA-AD 2013-06-02: Revision of Normal and Abnormal Procedures of Airplane Flight Manual Doc. No 7.01.15-E and Doc. No. 7.01.16-E in regards of Alternate Air usage
| - | 2013-03-21 |
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SI42NG-048 | Garmin Service Advisory No. 1309 Rev. B, Verification of displayed heading is not noticeable drifting prior Take-Off
| - | 2013-04-12 |
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SI42NG-049 | FAA-AD 2013-06-02: Revision of Normal and Abnormal Procedures of Airplane Flight Manual Doc. No 7.01.15-E and Doc. No. 7.01.16-E in regards of Alternate Air usage
| - | 2013-03-21 |
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SI42NG-050 | EASA-AD 2013-0025R1: Alternative P/N waste gate controllers be installed as replacement parts, Austro Engine Mandatory Service Bulletin No. MSB-E4-007/4
| - | 2013-05-06 |
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SI42NG-051 | EASA-AD 2013-0121: Inspection to identify certain Nose Landing Gear Actuator P/N
| - | 2013-06-05 |
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SI42NG-052 | Proper draining of the fuel system
| - | 2013-06-19 |
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SI42NG-053 | FAA-AD 2013-14-08: Replacement of certain Waste Gate Controller part numbers with an improved design
| - | 2013-07-22 |
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SI42NG-054 | Garmin Service Advisory No. 1344 Rev. A, CDI / HSI scaling on a limited number of LPV and LNAV/VNAV approaches are incorrect
| - | 2013-08-21 |
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SI42NG-055 | Garmin Service Advisory No. 1348 Rev. A, Approach waypoints are not properly loaded or displayed when using a vector transition at certain approaches
| - | 2013-08-22 |
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SI42NG-056/1 | Austro Engine Mandatory Service Bulletin No. MSB-E4-007/6, Replacement of Waste Gate Controller
| - | 2013-09-20 |
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SI42NG-057/1 | Garmin Terrain Data Alert No. 1351 Rev. B, Anomalies when using Synthetic Vision Technology in Northwest Greenland
| - | 2015-03-03 |
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SI42NG-058 | EASA-AD 2013-0213: Austro Engine E4 Waste Gate Controller
| - | 2013-09-16 |
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SI42NG-059/1 | United Instruments Inc. Service Bulletin No. 12, Paint on dial may crack and separate from the surface
| - | 2013-10-31 |
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SI42NG-060 | EASA-AD 2013-0224: Installation of an additional alternator fail trigger
| - | 2013-09-20 |
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SI42NG-061 | Garmin Service Advisory No. 1352 Rev. A, Course deviation indicator (CDI) may deflect in the wrong direction in certain situations
| - | 2013-09-26 |
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SI42NG-062 | FAA-AD 2013-19-11: Inspection/modification of the Nose Landing Gear Actuator
| - | 2013-09-27 |
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SI42NG-063 | Main Landing Gear Extension/Retraction Mechanism
| - | 2013-11-19 |
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SI42NG-064 | Garmin Service Advisory No. 1363 Rev. A, User-modified terminal procedure stored in a Flight Plan may cause error condition
| - | 2013-11-21 |
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SI42NG-065 | Garmin Service Advisory No. 1344 Rev. B, LPV and LNAV/VNAV Approach Full Scale Deflection
| - | 2013-12-18 |
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SI42NG-066 | Garmin Service Advisory No. 1372 Rev. A, Unavailable RNAV (GPS) approaches due to lack of VDA
| - | 2013-12-18 |
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SI42NG-067 | EASA-AD 2013-0213R1: Austro Engine E4 Waste Gate Controller
| - | 2014-02-03 |
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SI42NG-068 | FAA-AD 2014-04-04: Alternator Fail Indication System
| - | 2014-03-05 |
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SI42NG-069 | FAA-AD 2014-08-10: Removing of certain Austro Engine part number (P/N) waste gate controllers from service
| - | 2014-05-07 |
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SI42NG-070 | Austro Engine Mandatory Service Bulletin No. MSB-E4-017, Check and if necessary replacement of the Timing Chain
| - | 2014-07-03 |
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SI42NG-071 | Garmin Service Advisory No. 1449 Rev. A, Unexpected flight paths may be displayed when sequencing to some vector transition approaches
| - | 2014-09-05 |
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SI42NG-072 | Garmin Service Advisory No. 1456 Rev. A, Published VNAV altitude constraint for the remaining final approach fix (FAF) waypoint is changed to a VNAV altitude constraint of zero foot
| - | 2014-10-17 |
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SI42NG-073/1 | Garmin Service Advisory No. 1514 Rev. B, Flight management system may provide erroneous lateral guidance
| - | 2015-03-27 |
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SI42NG-074 | Garmin Service Alert No. 1538 Rev. A, Operations with Altimeter Set to QFE (height above field elevation)
| - | 2015-08-12 |
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SI42NG-076 | Austro Engine MSB-E4-020, Inspection of Gearbox Housing
| - | 2016-03-04 |
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SI42NG-077 | 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 |
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SI42NG-078 | Garmin Service Advisory No. 1372 Rev. B, unavailable RNAV (GPS) approaches
| - | 2016-06-24 |
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SI42NG-079 | 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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SI42NG-080 | EASA-AD 2016-0190: Inspections of the auto pilot bridle clamps
| - | 2016-09-27 |
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SI42NG-081 | FAA-AD 2016-22-06: Inspections of the auto pilot bridle clamps in the pitch and roll control system
| - | 2016-11-02 |
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SI42NG-082 | 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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SI42NG-083 | 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
| - | 2017-03-02 |
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SI42NG-084/1 | EASA-AD 2017-0103R1: Amendment of the applicable AFM and updated requirement of timing chain replacement
| - | 2019-02-28 |
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SI42NG-085 | FAA-AD 2017-18-10: Mandating inspections and modification
of the flap control system, repetitive inspections of the flap bell crank
| - | 2017-10-30 |
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SI42NG-086/2 | Austro Engine MSB-E4-022/3, Replacement of certain batches of the Waste Gate Controller at E4 engines and the installation of waste gate control rod fail-safe bridges on all engines as terminating action
| - | 2018-05-17 |
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SI42NG-087 | Austro Engine MSB-E4-024/1, Replacement of the standard circlip at the Waste Gate Controller at E4 engines with a spring loaded circlip
| - | 2017-11-13 |
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SI42NG-088 | EASA-AD 2017-0250: Lifetime limit to waste gate controller and replacement of waste gate rod circlips to prevent unsafe condition due to disconnection
| - | 2017-12-18 |
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SI42NG-089 | FAA Special Airworthiness Information Bulletin (SAIB) NE-17-26, Display of intruder aircraft vertical trend indications
| - | 2017-10-30 |
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SI42NG-090 | FAA-AD 2018-07-16: MSB-E4-002 Rev. 2 introducing a lifetime limit to waste gate controller and replacement of waste gate rod circlips
| - | 2018-05-17 |
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SI42NG-091 | EASA-AD 2018-0125: Terminating action of MSBE4-022 Rev. 3, which leads to a lifetime limit change of the waste gate controller and waste gate rod circlips
| - | 2018-06-18 |
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SI42NG-092 | 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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SI42NG-093 | EASA-AD 2018-0214: Removal of the pilot (LH) side rudder pedal gust lock mounts in accordance with the MSB 42NG-077
| - | 2018-10-05 |
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SI42NG-094 | FAA-AD 2018-18-02: Amendment of the applicable AFM, and for engines operated under certain circumstances, the replacement of the engine timing chain
| - | 2018-11-23 |
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SI42NG-095 | Garmin Service Advisory No. 1905 Rev. A, GPS roll over
| - | 2019-01-14 |
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SI42NG-096 | EASA-AD 2019-0041: Airworthiness limitations and maintenance tasks for the Austro Engine E4 and E4P
| - | 2019-02-28 |
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SI42NG-097 | EASA-AD 2019-0066: Inspection of the nose landing gear assembly
| - | 2019-03-27 |
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SI42NG-098 | FAA-AD 2019-14-11: Removal of the pilot (LH) side rudder pedal gust lock mounts in accordance with the MSB 42NG-077
| - | 2019-08-07 |
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SI42NG-099 | EASA-AD 2019-0218: Rreplacement of Fuel Tank Connection Hoses
| - | 2019-09-06 |
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SI42NG-100 | 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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SI42NG-101 | 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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SI42NG-102 | DUPONT Product Discontinuation letter, KATHON FP 1.5 BIOCIDE
| - | 2020-03-30 |
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SI42NG-103 | FAA-AD 2020-15-05: Update of the Airplane Flight Manual with AFM TR-MÄM-42-973
| - | 2020-08-31 |
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SI42NG-104 | FAA-AD 2020-22-14: Replacement of the waste gate controller and control rod circlip
| - | 2020-12-16 |
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SI42NG-105/1 | Austro Engine MSB-E4-030 Rev. 3, Replacement of the oil pump
| - | 2021-03-19 |
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SI42NG-107/1 | EASA-AD 2021-0055R1: Replacement of the oil pump
| - | 2021-10-30 |
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SI42NG-108 | EASA-AD 2021-0094: Replacement of the oil pump
| - | 2021-03-31 |
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SI42NG-109 | FAA-AD 2021-09-04: Replacement of the oil pump
| - | 2021-04-26 |
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SI42NG-110 | Austro Engine MSB-E4-031/0, Replacement of certain engine oil pumps
| - | 2021-06-16 | |
SI42NG-111 | EASA-EAD 2021-0143-E: Replacement of certain engine oil pumps
| - | 2021-06-17 |
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SI42NG-112 | EASA-EAD 2021-0191-E: Replacement of certain engine oil pumps | - | 2021-08-19 |
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SI42NG-113 | FAA-AD 2021-17-01: Replacement of the oil pump | - | 2021-08-19 |
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SI42NG-114 | Austro Engine MSB-E4-034, Inspection and replacement of certain high pressure pump driving gears | - | 2021-08-20 |
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SI42NG-115 | Austro Engine MSB-E4-034 Rev. 1, Inspection and replacement of certain High Pressure Fuel Pump driving gear wheels | - | 2021-09-13 |
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SI42NG-116 | Austro Engine MSB-E4-035, Inspection of the High Pressure Fuel Pump driving gear wheel | - | 2021-09-13 |
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SI42NG-117 | EASA-EAD 2021-0203-E: Accomplishment with Austro Engine Service Bulletins MSB-E4-034/1 and MSB-E4-035 | - | 2021-09-13 |
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SI42NG-118 | EASA-AD 2021-0203R1: Accomplishment with Austro Engine Service Bulletins MSB-E4-034/1 and MSB-E4-035 | - | 2021-09-28 |
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SI42NG-119 | FAA-AD 2021-22-20: Accomplishment with Austro Engine MSB-E4-034/3 and MSB-E4-035/1 | - | 2021-11-09 |
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SI42NG-120 | FAA-AD 2021-24-10: Accomplishment with Austro Engine MSB-E4-030 Revision 4 | - | 2021-12-01 |
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SI42NG-121 | Austro Engine MSB-E4-036, Inspection and replacement of the High Pressure Pump Gear | - | 2021-12-01 |
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SI42NG-122 | EASA-EAD 2021-0274-E: Accomplishment with Austro Engine Service Bulletins MSB-E4-036 initial issue | - | 2021-12-09 |
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SI42NG-123 | FAA-AD 2021-22-03: Inspection of the Nose Landing Gear (NLG) actuator attachment | - | 2021-12-16 |
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SI42NG-124 | FAA-AD 2022-03-03: Accomplishment with Austro Engine Service Bulletin MSBE4-036/1 | - | 2022-02-01 |
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SI42NG-125 | 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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SI42NG-126 | SIRS Service Information Letter No. SIRS/SIL-CE2-A25-01 Rev.02, Magnetic compass illumination lamp | - | 2022-03-04 |
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SI42NG-127 | 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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SI42NG-128 | Austro Engine MSB-E4-039, Engine oil analysis and piston replacement | - | 2022-11-02 |
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SI42NG-129 | FAA-AD 2022-21-15: Installation of the T-yoke bolt D60-5320-00-32 | - | 2022-11-02 |
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SI42NG-130 | EASA-AD 2022-0240: Engine oil analysis and piston replacement | - | 2022-12-07 |
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SI42NG-131 | EASA-AD 2022-0240R1: Engine oil analysis and piston replacement | - | 2022-12-19 |
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SI42NG-132 | EASA-AD 2023-0013: Inspection and modification of the rudder steering bracket | - | 2023-01-19 |
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SI42NG-133 | 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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SI42NG-134 | United Instruments Service Note No. 5934-14, Replacement of nonconforming static port threads | - | 2023-04-17 |
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SI42NG-135 | EASA-AD 2023-0163: Engine oil analysis and piston replacement | - | 2023-09-06 |
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SI42NG-136 | FAA-AD 2023-20-03: Engine oil analysis and piston replacement | - | 2023-11-09 |
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SI42NG-138 | Austro Engine MSB-E4-042, crankshaft-bearing cap screws replacement on engine serial numbers listed in the MSB-E4-042 | - | 2024-02-01 |
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SI42NG-139 | EASA-EAD 2024-0037-E: Crankshaft-bearing cap screws replacement on Austro Engine E4 engines | - | 2024-02-02 |
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SI42NG-140 | EASA-AD 2024-0037R1: Crankshaft-bearing cap screws replacement on Austro Engine E4 engines | - | 2024-02-06 |
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SI42NG-141 | FAA-AD 2024-05-01: Crankshaft-bearing cap screws replacement on Austro Engine E4 engines | - | 2024-03-06 |
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SI42NG-142 | 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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SI42NG-143 | 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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SI42NG-144 | EASA-AD 2023-0013R1: Inspection and/or installation of the T-yoke bolt D60-5320-00-32 | - | 2024-04-29 |
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SI42NG-145 | Closing and latching the passenger door | - | 2024-08-22 |
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SI42NG-146 | Austro Engine MSB-E4-043, borescope inspection on engine serial numbers listed | - | 2024-08-28 |
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SI42NG-147 | EASA-EAD 2024-0172-E: Piston inspection or replacement, having the part number E4A-72-400-000 | - | 2024-08-29 |
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SI42NG-148 | FAA-AD 2024-19-10: Piston inspection or replacement, having the Part Number E4A-72-400-000 | - | 2024-09-25 |
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