DA40 NEW GENERATION LIST OF APPLICABLE DIAMOND PUBLICATIONS last update:

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1 E E AIRPLANE FLIGHT MANUAL (english) - BASIC MANUAL Airplane Flight Manual (AFM) Complete Revision AIRPLANE FLIGHT MANUAL (english) - SUPPLEMENTS Supplement A01, Garmin G1000 Avionics System Supplement A02, Intercom System PM 1000 II, PS Engineering Inc Supplement A05, Conventional Cockpit DA 40 NG Club Supplement A13, Autopilot System KAP 140, Bendix/King Supplement A29, DA 40 NG Garmin Transponder GT Supplement A30, DA 40 NG Garmin COM/NAV, SL Supplement A33, Garmin G1000 SBAS and P-RNAV Operation Supplement E7, Operation with Ventilation Inlet Baffle Supplement N017, Operation in CIS Supplement N048, Operation in the Ukraine Supplement O01, Use of the DA 40 NG as Tow-Plane Supplement O02, Landing Gear with Large Tyres and 1280 kg Maximum Landing Mass Supplement O03, Cold Weather Operation Supplement O04, Diesel Operation Supplement S04, 406MHz Emergency Locator Transmitter Artex ME Supplement S06, G1000 Synthetic Vision Technology Supplement S07, Recirculating Air - Cabin Cooling E AIRPLANE FLIGHT MANUAL (english) - VALID TEMPORARY REVISIONS TR-MÄM , Garmin G1000 Avionics System TR-MÄM , Coolant Temperature Upper Caution Range 100 C-105 C TR-MÄM , Removal of High Current Procedure TR-OÄM , Front Seats with Adjustable Backrest - Hydrolok TR-OÄM , Transponder GT33ES E AIRPLANE FLIGHT MANUAL (english) - OBSOLETE TEMPORARY REVISIONS TR-MÄM , Stall Horn Classification obsolete with Rev. 1 - TR-MÄM /a, Maximum Zero Fuel Mass 1265 kg obsolete with Rev. 3 - TR-MÄM , Operation Without Wheel Fairings obsolete with Rev. 1 - TR-MÄM & OÄM , Exhaust Pipe with Muffler obsolete with Rev. 2 - TR-MÄM , Safety Harnesses obsolete with Rev. 1 - TR-MÄM , CG - Range Diagram obsolete with Rev. 1 - TR-MÄM , TS-1 Fuel obsolete with Rev. 2 - TR-MÄM , Pitot Static Tube obsolete with Rev. 1 - TR-MÄM , High Pressure Pump Procedure obsolete with Rev. 1 - TR-MÄM , Additional Fuel Grades obsolete with Rev. 3 - TR-MÄM , Brake Assembly Part Number obsolete with Rev. 1 - TR-MÄM , Additional Brake Assembly obsolete with Rev. 3 - TR-MÄM , Additional Gearbox Oil obsolete with Rev. 3 - TR-MÄM , Alternator Regulator E4A obsolete with Rev. 3 - TR-MÄM , Engine Start Procedure obsolete with Rev. 3 - TR-MÄM , Additional Engine Oils obsolete with Rev. 3 - Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 1 of 11

2 TR-MÄM , New GFC 700 Autopilot Hardware obsolete with Rev. 3 - TR-MÄM , GIA 63 W new Part Number obsolete with Rev. 3 - TR-MÄM , GMU 44 New Part Number obsolete with Rev. 3 - TR-MÄM , Maximum Landing Mass 1280 kg obsolete with Rev. 3 - TR-MÄM /a & TR-OÄM /b, Airspeed Indicator Markings obsolete with Rev. 3 - TR-MÄM , Shorter NLG Damper obsolete with Rev. 3 - TR-MÄM , New AE 300 Gearbox obsolete with Rev. 3 - TR-MÄM , Cold Weather Operation obsolete with Rev. 3 - TR-MÄM , High Oil Pressure Procedure obsolete with Rev. 3 - TR-MÄM , Engine Oils and Fuel Additives obsolete with Rev. 3 - TR-MÄM /a, ECU Caution Clearing Procedure obsolete with Rev. 3 - TR-MÄM , GT 33 P/N obsolete with Rev. 3 - TR-MÄM , New Exhaust Attachments obsolete with Rev. 3 - TR-MÄM , Alternative Fuel Pump - Weldon B obsolete with Rev. 3 - TR-MÄM , Cold Weather Power Check Information obsolete with Rev. 3 - TR-MÄM , Alternator Part No. E4A obsolete with Rev. 3 - TR-MÄM , Entering and Exiting the Airplane obsolete with Rev. 3 - TR-MÄM /a, Starting the Engine with External Power obsolete with Rev. 3 - TR-OÄM , Winter Baffle Fresh Air Inlet obsolete with Rev. 3 - TR-OÄM , Installation of Approved Fire Extinguishers obsolete with Rev. 3 - TR-OÄM , Front Seats with Adjustable Backrest obsolete with Rev. 3 - TR-OÄM , HID - Lights obsolete with Rev. 3 - TR-OÄM , W-500 Installation obsolete with Rev. 1 - TR-OÄM , Tow-Plane Operation obsolete with Rev. 3 - TR-OÄM , ADF Installation obsolete with Rev. 1 - TR-OÄM /a & OÄM /a, Additional Alternator & Recirculating obsolete with Rev. 1 - Air - Cabin Cooling TR-OÄM /d & OÄM /d, Additional Alternator & Recirculating obsolete with Rev. 3 - Air - Cabin Cooling TR-OÄM /a, Conventional Cockpit DA 40 NG Equipment List obsolete with Rev. 2 - TR-OÄM , Emergency Axe obsolete with Rev. 1 - TR-OÄM /a, Emergency Axe obsolete with Rev. 3 - TR-OÄM , Sun Visors for Tall Canopy obsolete with Rev. 1 - TR-OÄM , Austro Engine E4 Retrofit, Garmin G1000 with Autopilot obsolete with Rev. 1 - KAP 140 TR-OÄM , Austro Engine E4 Retrofit, Garmin G1000 without obsolete with Rev. 1 - Autopilot GFC 700 TR-OÄM , Short Baggage Extension obsolete with Rev. 1 - TR-OÄM , DA 40 NG without Autopilot GFC obsolete with Rev. 1 - TR-OÄM /a, Landing Gear with Large Tyres and 1280 kg Maximum obsolete with Rev. 3 - Landing Mass TR-OÄM /a, Garmin G1000 SBAS and P-RNAV Operation obsolete with Rev. 3 - TR-OÄM , Avidyne/Ryan TAS 600 Series obsolete with Rev. 3 - TR-OÄM , Whelen LED Position Lights obsolete with Rev. 3 - TR-OÄM , LED Landing- and Taxi Lights obsolete with Rev. 3 - TR-OÄM , Whelen LED Position / Anti Collision Lights obsolete with Rev. 3 - TR-OÄM , Diesel Operation obsolete with Rev. 3 - TR-OÄM , Comant COM Antennas obsolete with Rev. 3 - TR-OÄM , Engine Master Switch Guard obsolete with Rev. 3 - Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 2 of 11

3 TR-OÄM , Additional Chronometer obsolete with Rev. 3 - Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 3 of 11

4 AIRPLANE MAINTENANCE MANUAL (english) - BASIC MANUAL Airplane Maintenance Manual (AMM) Complete Revision AIRPLANE MAINTENANCE MANUAL (english) - VALID TEMPORARY REVISIONS The temporary revisions (TR's) listed below are valid in conjunction with the latest revision of the AMM until these TR's have been incorporated into the AMM, even though on the title page of one of these TR's the validity is limited to a certain revision of the AMM. AMM-TR-MÄM , New GFC 700 Autopilot Hardware AMM-TR-MÄM , Adjust Taxi Light Procedure AMM-TR-MÄM , Cold Weather Operation AMM-TR-MÄM , Engine Oil Quick Drain AMM-TR-MÄM , Fuel Filter Element Check Valve AMM-TR-MÄM , Trouble Shooting Fuel System AMM-TR-MÄM /a, Governor Nut Torque AMM-TR-MÄM , Coolant Tank Pressure Relief Valve Test AMM-TR-MÄM , Coolant System Pressure Test AMM-TR-MÄM , Removal of Checklist Items AMM-TR-MÄM , Stall Warning System AMM-TR-MÄM , Lubrication Schedule AMM-TR-MÄM , Protective Pads for Charged Air Hoses AMM-TR-MÄM , Replacement of Passenger Door Hinges AMM-TR-MÄM , Additional Elevator Mass AMM-TR-MÄM , Silicate Cartridge AMM-TR-MÄM , Inspection of NLG Elastomer Pack Center Tube AMM-TR-OÄM , HID - Lights AMM-TR-OÄM , Towing Device AMM-TR-OÄM /f, Additional Alternator AMM-TR-OÄM /b, Recirculating Air - Cabin Cooling (RACC) AMM-TR-OÄM , Provisions for Tablet Mount AMM-TR-OÄM , Seat Belt Holder AMM-TR-OÄM , Headset Hanger AMM-TR-OÄM , Battery Heating System AMM-TR-OÄM , Whelen LED Position / Anti Collision Lights AMM-TR-OÄM , Diesel Operation AMM-TR-OÄM , Front Seats with Adjustable Backrest - Hydrolok AMM-TR-OÄM , Bilstein NLG - Damper AIRPLANE MAINTENANCE MANUAL (english) - OBSOLETE TEMPORARY REVISIONS AMM-TR-MÄM /b & 549, Cowling Redesign obsolete with Rev. 1 - AMM-TR-MÄM , Shock Mount Installation Torques obsolete with Rev. 1 - AMM-TR-MÄM , Safety Harnesses obsolete with Rev. 1 - AMM-TR-MÄM , New Governor Speed Settings obsolete with Rev. 1 - AMM-TR-MÄM , Fuel Pulsation Damper obsolete with Rev. 1 - AMM-TR-MÄM , Safety Walk Adhesive Strips obsolete with Rev. 1 - AMM-TR-MÄM /a & 506/a, Replacement of Charged Air Hose with Tube obsolete with Rev. 2 - Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 4 of 11

5 AMM-TR-MÄM , Firewall Reinforcements on Engine Mount Holes obsolete with Rev. 2 - AMM-TR-MÄM & 520, Breather Line with Additional Outlet obsolete with Rev. 2 - AMM-TR-MÄM , Maintenance Program Phase obsolete with Rev. 1 - AMM-TR-MÄM , Maintenance Interval GFC obsolete with Rev. 1 - AMM-TR-MÄM , Landing Gear Special Torque Values and obsolete with Rev. 1 - Corrections AMM-TR-MÄM , Propeller Shipping Plug Removal obsolete with Rev. 2 - AMM-TR-MÄM , Gearbox Oil Inspection obsolete with Rev. 1 - AMM-TR-MÄM , Fuel Drain Valve Mounting Torque obsolete with Rev. 2 - AMM-TR-MÄM , Alternator Regulator E4A obsolete with Rev. 2 - AMM-TR-MÄM /a, Alternative Engine Shock Mount obsolete with Rev. 2 - AMM-TR-MÄM /a & OÄM /b & MÄM , 1280 kg obsolete with Rev. 2 - Maximum Landing Mass and / or Landing Gear with Large Tires AMM-TR-MÄM /a, Adaptation of Engine Time Limits obsolete with Rev. 2 - AMM-TR-MÄM , Rudder Control Cable Installation obsolete with Rev. 2 - AMM-TR-MÄM , Turbo Connector and Worm Drive Clamps obsolete with Rev. 2 - AMM-TR-MÄM , New AE 300 Gearbox obsolete with Rev. 2 - AMM-TR-MÄM , Snow and Ice Removal obsolete with Rev. 2 - AMM-TR-MÄM , Additional Greases obsolete with Rev. 2 - AMM-TR-MÄM , Charged Air Hoses SG obsolete with Rev. 2 - AMM-TR-OÄM , Front Seats with Adjustable Backrest obsolete with AMM-TR-OÄM AMM-TR-OÄM , Exhaust Muffler obsolete with Rev. 1 - AMM-TR-OÄM /e, Additional Alternator obsolete with Rev. 2 - AMM-TR-OÄM , Recirculating Air - Cabin Cooling (RACC) obsolete with Rev. 1 - AMM-TR-OÄM /a, Recirculating Air - Cabin Cooling (RACC) obsolete with Rev. 2 - AMM-TR-OÄM , Coated Safety Walk obsolete with Rev. 1 - AMM-TR-OÄM , Conventional Cockpit DA 40 NG Club obsolete with Rev. 1 - AMM-TR-OÄM /a, Emergency Axe obsolete with Rev. 1 - AMM-TR-OÄM , Sun Visors for Tall Canopy obsolete with Rev. 1 - AMM-TR-OÄM , DA 40 NG Retrofit, G1000 with Autopilot KAP obsolete with Rev. 1 - AMM-TR-OÄM , DA 40 NG Retrofit, G1000 without Autopilot GFC obsolete with Rev AMM-TR-OÄM , Short Baggage Extension obsolete with Rev. 1 - AMM-TR-OÄM , DA 40 NG without Autopilot GFC obsolete with Rev. 1 - AMM-TR-OÄM , Landing Gear with Large Tires and 1280 kg Maximum Landing Mass obsolete with AMM-TR-MÄM & OÄM /a - AMM-TR-OÄM , Foot Step Rear Option obsolete with Rev. 2 - AMM-TR-OÄM , Avidyne/Ryan TAS 600 Series obsolete with Rev. 2 - AMM-TR-OÄM , Whelen LED Position Lights obsolete with Rev. 2 - Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 5 of 11

6 ILLUSTRATED PARTS CATALOGUE (english) - BASIC MANUAL Illustrated Parts Catalogue (IPC) current (N/A) online available Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 6 of 11

7 SERVICE BULLETIN LIST SB40NG-001 not issued yet - MSB40NG-002/8 Software for E4-A (AE300) Engine, approved versions DA 40 NG S/N , , 40.N001 and subsequent All DA 40 NG converted using OSB D4-080 MSB40NG-003/7 Software for Garmin G1000; approved software systems, manifests and DA 40 NG S/N D4.111, D4.365, 40.N001 and configurations subsequent All DA 40 NG converted using OSB D4-080 OSB40NG-004 Installation of a coated safety walk DA 40 NG S/N 40.N001 and subsequent SB40NG-005 not issued yet - OSB40NG-006 Import Requirements to CIS DA 40 NG all S/N, in which NÄM 'Operation in the CIS' has not been carried out OSB40NG-007/1 Installation of a fuel pressure pulsation damper DA 40 NG S/N 40.N001 through 40.N014, D4.301, D4.326 SB40NG-008 not issued yet - SB40NG-009 not issued yet - RSB40NG-010 Installation of check valves on fuel pumps DA 40 NG S/N 40.N001 through 40.N039, D4.197, D4.213, D4.301, D4.326 RSB40NG-011 REVOKED Exchange of charged air elbow DA 40 NG S/N 40.N001 through 40.N032, 40.N035 through 40.N044 Airplanes converted to DA 40 NG with WI-OSB up to Rev. 3 MSB40NG-012/2 Replacement of aft engine shock mounts DA 40 NG S/N 40.N001 through 40.N050, 40.N052 through 40.N054, D4.197, D4.213, D4.263, D4.301, D4.326 RSB40NG-013 Replacement of air conditioning system DA 40 NG S/N 40.N011, 40.N012, 40.N015, 40.N016, 40.N035, 40.N065 SB40NG-014 not issued yet - MSB40NG-015/1 Installation of a rudder cable guard DA 40 NG S/N 40.N001 through 40.N070 Airplanes converted to DA 40 NG via OSB D4-080 MSB40NG-016/2 Correction of Airspeed Indicator (ASI) markings DA 40 NG S/N 40.N001 through 40.N087 Airplanes converted to DA 40 NG via OSB D4-080 using WI-OSB-D4-080 up to Revision 6 OSB40NG-017 CG adjustment DA 40 NG S/N 40.N001 and subsequent MSB40NG-018/1 Exchange of charged air tubing; incl. WI Rev DA 40 NG S/N 40.N001 through 40.N084 Airplanes converted to DA 40 NG with WI-OSB up to Rev. 6 RSB40NG-019 Replacement of the Charged Air Hoses with glass fiber reinforced silicone hoses DA 40 NG S/N 40.N001 though 40.N091 DA 40 D airplanes converted to DA 40 NG via OSB D4-080 using WI-OSB D4-080 up to revision 7 REVOKED MSB40NG-020/4 Inspection of the nose landing gear (NLG) pivot of NLG-legs installed under DA 40 NG all S/N with OÄM (landing gear OÄM (landing gear with large tires) for cracks with large tires) installed OSB40-NG-021 Installation of alternator regulator, Austro Engine P/N E4A DA 40 NG S/N 40.N001 through 40.N062 All DA 40 NG converted via OSB using WI- OSB up to and including revision 7 Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 7 of 11

8 OSB40NG-022 Installation of an engine oil quick drain-valve DA 40 NG S/N 40.N001 through 40.N151 Airplanes converted to DA 40 NG via OSB D4-080 OSB40NG-023 Installation of a radiator baffle DA 40 NG all S/N OSB40NG-024 Installation of Battery Heaters DA 40 NG all S/N OSB40NG-025 Installation of an engine master switch guard DA 40 NG S/N 40.N001 and subsequent OSB40NG-026 Installation of LED Taxi and Landing Lights DA 40 NG S/N 40.N001 and subsequent Airplanes converted to DA 40 NG SB40NG-027 not issued yet - OSB40NG-028 Installation of Sun visors DA 40 NG S/N 40.N001 and subsequent SB40NG-029 not issued yet - OSB40NG-030 Installation of Provisions for Operation with Diesel fuel DA 40 NG S/N 40.N001 and subsequent Airplanes converted to DA 40 NG RSB40NG-031 Installation of permanent maintenance access holes in wings DA 40 NG S/N 40.N001 and subsequent OSB40NG-032 Installation provisions for a safety mesh to protect the fuel vent covers into DA 40 NG S/N 40.N001 and subsequent the wings SB40NG-033 not issued yet - SB40NG-034 not issued yet - OSB40NG-035 Installation of a hydraulic NLG damper DA 40 NG S/N 40.N001 and subsequent Only airplanes with Large Tires (OÄM ) installed OSB40-NG-036 Installation of the Coolant Level Sensor D4D DA 40 NG S/N 40.N001 through 40.N229 Airplanes converted to DA 40 NG SB40NG-037 not issued yet - OSB40NG-038 Improvement of powerplant cooling DA 40 NG S/N 40.N029, 40.N033, 40.N034, 40.N038 and subsequent Airplanes converted to DA 40 NG via OSB D4-080 using WI-OSB D4-080 Revision 4 or later OSB40NG-039 Replacement of nose landing gear strut DA 40 NG S/N 40.N088 and subsequent Note: This Service Bulletin is only applicable, if OÄM is NOT installed OSB40NG-040/1 Installation of the nose landing gear fairings for the lowered nose landing gear (MÄM /OSB 40NG-039) DA 40 NG S/N 40.N088 and subsequent Note: This Service Bulletin is only applicable to airplanes with MÄM or OSB 40NG-039 and OÄM installed. Note: This Service Bulletin is only applicable, if OÄM is NOT installed. RSB40NG-041 Inspection of NLG elastomer pack center tube DA 40 NG All airplanes with more than 1000 flight hours Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 8 of 11

9 SERVICE INFORMATION LIST SI40NG-001 Descriptions of DAI technical publication systems and handling of DA 40 NG all S/N documents SI40NG-002/1 AE Mandatory Service Bulletin MSB-E4-009/2, Possible exchange of the engine high pressure pump all DA 40 NG airplanes SI40NG-003 EASA-EAD: High Pressure Fuel Pump - Inspection/Replacement all DA 40 NG airplanes EASA-EAD: E SI40NG-004 not issued yet - SI40NG-005 Garmin Service Advisory No Rev. A, 2010 IGRF (International all DA 40 NG Geomagnetic Reference Field) Magnetic Field Model SI40NG-006 EASA-AD: High Pressure Fuel Pump - Inspection/Replacement all DA 40 NG airplanes EASA-AD: SI40NG-007/1 Installation and tightening torque of worm drive clamps in the charge-air and all DA 40 NG airplanes liquid cooling system SI40NG-008 Garmin Service Advisory No Rev. A, Momentary failure indications (Red-) can occur when sorting stored flight plans All DA 40 NG airplanes equipped with Garmin G1000 System SI40NG-009 Garmin Service Advisory No Rev. A, Momentary loss of GRS 77/77H All DA 40 NG aircraft equipped with Garmin G1000 and GDC 74A/74B/74H functions System SI40NG-010 Garmin Service Advisory No Rev. D, European Geostationary Navigation Overlay System (EGNOS) Safety-of-Life (SoL) Service is Fully Operational All DA 40 NG airplanes equipped with GARMIN G1000 System SI40NG-011 SI40NG-012/1 SI40NG-013 SI40NG-014 Garmin Service Advisory No Rev. A, Garmin SBAS-capable receivers may experience loss of LPV or LNAV/VNAV capability due to incoherent EGNOS satellite GEO ranging data AE Mandatory Service Bulletin Revision MSB-E4-013/1, Gearbox oil inspection - Additional oil check for early debris indication Measures that result from performing Austro Engine Mandatory Service Bulletin MSB-E4-013/1 Austro Engine Mandatory Service Bulletin MSB-E4-014/1, Replacement of the Fuel Return Line and Banjo Fitting All DA 40 NG airplanes equipped with GARMIN G1000 System All DA 40 NG airplanes All DA 40 NG airplanes All DA 40 NG airplanes SI40NG-015 Garmin Service Bulletin No Rev. A, SafeTaxi Availability In Europe All DA 40 NG airplanes equipped with Garmin G1000 system SI40NG-016 AE Mandatory Service Bulletin Revision MSB-E4-014/2, Replacement of the All DA 40 NG airplanes Fuel Injector Return Line and the Banjo Fitting SI40NG-017 EASA-AD: Installation of a temporary placard in the cockpit DA 40 NG airplanes S/N 40.N001 through 40.N087 EASA-AD: inclusive, and any DA 40 D aeroplane modified in-service to DA 40 NG through application of Optional Service Bulletin OSB D4-080 by using Work Instruction WI- OSB D4-080 up to Revision 6 MSB 40NG-016 SI40NG-018 Garmin Service Alert No. 1228, SIDs and STARs non-jets Limitation All DA 40 NG airplanes equipped with GARMIN G1000 System SI40NG-019 Austro Engine Mandatory Service Bulletin No. MSB-E4-007/3, Replacement All DA 40 NG airplanes of Waste Gate Controller SI40NG-020 EASA-AD: Inspection, and replacement if necessary, of the charged air tubing from the turbocharger to the intercooler for chafing marks DA 40 NG airplanes S/N 40.N001 through 40.N084 inclusive, and any DA 40 D aeroplane modified in-service to DA 40 NG through application of Optional Service Bulletin OSB D4-080 by using Work Instruction WI- OSB D4-080 up to Revision 6 EASA-AD: SI40NG-021/1 EASA-AD: Inspection of the markings of the safety belts All DA 40 NG airplanes EASA-AD: R3 Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 9 of 11

10 SI40NG-022 MT-Propeller Service Bulletin No. 27, Inspection and modification of certain All DA 40 D airplanes equipped with MT-Propeller governor type- and serial numbers governors SI40NG-023 Garmin Service Advisory No. 1309, Verification of displayed heading is not noticeable drifting prior Take-Off All DA 40 D aircraft equipped with GARMIN G1000 SI40NG-024 EASA-AD: Replacement of certain Waste Gate Controller part numbers with All DA 40 NG airplanes EASA-AD: an improved design at its E4 engines SI40NG-025 Proper draining of the fuel system All DA 40 NG airplanes SI40NG-026 Garmin Service Advisory No Rev. B, Verification of displayed heading All DA 40 NG airplanes equipped with Garmin G1000 is not noticeable drifting prior Take-Off SI40NG-027 EASA-AD: Alternative P/N waste gate controllers be installed as All DA 40 NG airplanes EASA-AD: R1 replacement parts, Austro Engine Mandatory Service Bulletin No. MSB-E4-007/4 SI40NG-028 FAA-AD: Inspection and replacement if necessary of the charged air tubing DA 40 NG airplanes S/N 40.N001 through 40.N084 FAA-AD: from the turbocharger to the intercooler for chafing marks inclusive and any DA 40 D aeroplane modified inservice to DA 40 NG SI40NG-029 Identification of stainless steel control cables All DA 40 NG airplanes SI40NG-030 FAA-AD: Replacement of certain Waste Gate Controller part numbers with All DA 40 NG airplanes FAA-AD: an improved design SI40NG-031 Garmin Service Advisory No Rev. A, CDI / HSI scaling on a limited All DA 40 NG airplanes number of LPV and LNAV/VNAV approaches are incorrect SI40NG-032 Garmin Service Advisory No Rev. A, Approach waypoints are not properly loaded or displayed when using a vector transition at certain approaches All DA 40 NG airplanes SI40NG-033/1 Austro Engine Mandatory Service Bulletin No. MSB-E4-007/6, Replacement All DA 40 NG airplanes of Waste Gate Controller SI40NG-034/1 Garmin Terrain Data Alert No Rev. B, Anomalies when using Synthetic Vision Technology in Northwest Greenland All DA 40 NG airplanes SI40NG-035 EASA-AD: Austro Engine E4 Waste Gate Controller All DA 40 NG airplanes EASA-AD: SI40NG-036/1 United Instruments Inc. Service Bulletin No. 12, Paint on dial may crack and All DA 40 NG airplanes separate from the surface SI40NG-037 Garmin Service Advisory No Rev. A, Course deviation indicator (CDI) All DA 40 NG airplanes may deflect in the wrong direction in certain situations SI40NG-038 Garmin Service Advisory No Rev. A, User-modified terminal procedure stored in a Flight Plan may cause error condition All DA 40 NG airplanes SI40NG-039 Garmin Service Advisory No Rev. B, LPV and LNAV/VNAV Approach All DA 40 NG airplanes Full Scale Deflection SI40NG-040 Garmin Service Advisory No Rev. A, Unavailable RNAV (GPS) All DA 40 NG airplanes approaches due to lack of VDA SI40NG-041 EASA-AD: Austro Engine E4 Waste Gate Controller All DA 40 NG airplanes EASA-AD: R1 SI40NG-042/1 Andair GAS375 Gascolator Filters All DA 40 NG airplanes SI40NG-043 FAA-AD: Removing of certain Austro Engine part number (P/N) waste gate All DA 40 NG airplanes FAA-AD: controllers from service SI40NG-044 Austro Engine Mandatory Service Bulletin No. MSB-E4-017, Check and if All DA 40 NG airplanes necessary replacement of the Timing Chain SI40NG-045 Garmin Service Advisory No Rev. A, Unexpected flight paths may be displayed when sequencing to some vector transition approaches All DA 40 NG airplanes Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 10 of 11

11 SI40NG-046 Installation of charged air hose P/N D _ All DA 40 NG airplanes with serial number 40.N091 and subsequent, or with RSB 40NG-019 carried out SI40NG-047 SI40NG-048 Garmin Service Alert No Rev. A, Operations with Altimeter Set to QFE (height above field elevation) Andair Service Alert: Certain fuel valve systems with extension may have a possible lack of engagement between the universal joint assembly and the top of the valve assembly All DA 40 NG airplanes equipped with Garmin G All DA 40 NG airplanes NEW Copyright Diamond Aircraft Industries Tel.: Fax: support@diamond-air.at Page 11 of 11