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Technify Motors TAE 125-02-114 Manual Supplement

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Approved Airplane Flight Manual Supplement
TAE 125-02-114 Engine Installation
SERIAL No.
REGISTER No.
This supplement must be attached to the EASA approved
Airplane Flight Manual when the TAE 125-02-114 engine has
been installed in accordance with EASA STC 10036328.
The information contained in this supplement supersedes or
adds to the EASA approved Airplane Flight Manual only as set
forth herein.
For limitations, procedures, performance and loading
information not contained in this supplement, consult the basic
EASA approved Airplane Flight Manual.
This Airplane Flight Manual Supplement is approved with EASA
STC 10036328.
Technify Motors GmbH
Platanenstraße 14
D - 09356 St. Egidien
for the
DA 40 D
Equipped with
Issue 2/0
_______________
_______________
Tel. +49-(0)37204/ 696-0
Fax +49-(0)37204/ 696-2912
www.continentaldiesel.de
support@ccontinentaldiesel.
Doc.-No.: 50-0310-50022
de

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  • Page 1 REGISTER No. _______________ This supplement must be attached to the EASA approved Airplane Flight Manual when the TAE 125-02-114 engine has been installed in accordance with EASA STC 10036328. The information contained in this supplement supersedes or adds to the EASA approved Airplane Flight Manual only as set forth herein.
  • Page 2 This page intentionally left blank...
  • Page 3 AFM Supplement DA 40 D LOG OF REVISIONS Approved Revision Chapter Description Date Endorsed Initial Issue 1 Sept. 01, EASA STC 10036328 2011 New fuel, March 16, new gearboxoil 2012 Change of Ownership Aug. 15, EASA STC 10036328, 2015 New gearbox oil Rev.
  • Page 4 AFM Supplement DA 40 D LIST OF EFFECTIVE CHAPTERS Issue/Revision Date Chapter Aug., 2015 Aug., 2015 Aug., 2015 Aug., 2015 Aug., 2015 Aug., 2015 Aug., 2015 Aug., 2015 Aug., 2015 Aug., 2015 Aug., 2015 APPROVAL The content of approved chapters is approved by EASA. All other content is approved by TAE under the authority of EASA DOA No.
  • Page 5 AFM Supplement DA 40 D TABLE OF CONTENTS CHAPTER 1..GENERAL (a non-approved chapter) CHAPTER 2..OPERATING LIMITATIONS (an approved chapter)) CHAPTER 3..EMERGENCY PROCEDURES (a non-approved chapter)) CHAPTER 4a..NORMAL OPERATING PROCEDURES (a non-approved chapter) CHAPTER 4b..ABNORMAL OPERATING PROCEDURES (a non-approved chapter)) CHAPTER 5..PERFORMANCE (a non-approved chapter)) CHAPTER 6..WEIGHT AND BALANCE / EQUIPMENT LIST...
  • Page 6 AFM Supplement DA 40 D This page is intentionally left blank Page vi Issue 2 Revision -, Aug. 2015...
  • Page 7 GENERAL 1.1 INTRODUCTION This supplement must be attached to the EASA approved Airplane Flight Manual when the TAE 125-02-114 engine has been installed in accordance with EASA STC 10036328. The information contained in this supplement supersedes or adds to the EASA approved Airplane Flight Manual only as set forth herein.
  • Page 8 AFM Supplement DA 40 D This page intentionally left blank Page 1-2 Issue 2 Revision -, Aug. 2015...
  • Page 9 AFM Supplement DA 40 D CHAPTER 2 OPERATING LIMITATIONS 2.4 POWERPLANT LIMITATIONS a) Engine manufacturer: ....... Technify Motors GmbH b) Engine designation: ........TAE 125-02-114 c) RPM limitations (shown as propeller PRM) Maximum: ..............2300 RPM Maximum overspeed:......2500 RPM (max 20 sec) d) Engine Power Max.
  • Page 10 AFM Supplement DA 40 D Manufacturer: ......MT Propeller Entwicklung GmbH k) Model: ............MTV-6-A/187-129 ................ MTV-6-A/190-69 l) Propellerdiameter:......1.87 m (MTV-6-A/187-129) ............1.90 m (MTV-6-A/190-69) m) Propeller pitch angle (0.75R): ......13.5° to 28° n) Oil Specification: .... AERO SHELL OIL DIESEL ULTRA ............SHELL HELIX ULTRA 5W-30 ............SHELL HELIX ULTRA 5W-40 ..........
  • Page 11 AFM Supplement DA 40 D ..........Shell Spirax GSX 75W-80 GL-4 ............Shell Spirax S6 ATF ZM ............Centurion Gearbox Oil N1  CAUTION: Use approved oil with exact designation only!  CAUTION: If the gearbox oil level is too low the reason must be determined and the problem must be corrected by authorized personnel.
  • Page 12 AFM Supplement DA 40 D Green Yellow Yellow arc/bar arc/bar arc/bar arc/bar arc/bar Indi-cation lower normal upper caution caution prohibited operating prohibited range range range range range Volt- below 11 11 to 12.5 12.6 to 14.9 15.0 to 15.5 above 15.5 meter Fuel qty.
  • Page 13 AFM Supplement DA 40 D 2.16 OTHER LIMITATIONS Fuel Temperature The fuel temperature limitations applicable for the TAE 125-02-99 engine are valid for the TAE 125-02-114. Refer to basic AFM. Page 2-5 Issue 2 Revision -, Aug. 2015...
  • Page 14 AFM Supplement DA 40 D CHAPTER 3 EMERGENCY PROCEDURES The emergency procedures included in this chapter supersede the procedures in the basic AFM. For emergency procedures not included in this chapter refer to basic AFM. Page 3-1 Issue 2 Revision -, Aug. 2015...
  • Page 15 AFM Supplement DA 40 D 3.2.4. RESTARTING THE ENGINE WITH WINDMILLING PROPELLER  Note: As long as an airspeed of at least 70 KIAS is maintained, and there is no major mechanical engine defect, the propeller will continue to windmill. After a complete stop the propeller starts to windmill at airspeeds above 115 KIAS.
  • Page 16 AFM Supplement DA 40 D (9) ENGINE MASTER ..........OFF - ON  Note: If it is not possible to start the engine: - adopt glide configuration - carry out emergency landing Refer to basic AFM  CAUTION: Engine restart following an engine fire should only be attempted if it is unlikely that a safe emergency landing can be made.
  • Page 17 AFM Supplement DA 40 D 3.2.5. RESTARTING THE ENGINE WITH STATIONARY PROPELLER  Note: Restarting the engine with stationary propeller is possible at altitudes below 14000 ft pressure altitude.  Note: Restarting the engine with windmilling propeller is possible at airspeeds between 70 and 110 KIAS and altitudes below 14000 ft.
  • Page 18 AFM Supplement DA 40 D (10) ELECTRIC MASTER ..........START (release when engine running)  Note: By increasing the airspeed above approximately 115KIAS, the propeller will begin to rotate due to windmilling and the engine can thus be started. For this, the ELECTRIC MASTER should be set to ON (see 3.2.4 - RESTARTING THE ENGINE WITH WINDMILLING PROPELLER of this...
  • Page 19 AFM Supplement DA 40 D This page intentionally left blank Page 3-6 Issue 2 Revision -, Aug. 2015...
  • Page 20 AFM Supplement DA 40 D CHAPTER 4A NORMAL OPERATING PROCEDURES 4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURES For take-off, climb, cruise climb and go-around the following airspeeds apply for the TAE 125-02-114 engine installation 980 kg 1000 kg 1150 kg Flight Mass (2160 lb)
  • Page 21 AFM Supplement DA 40 D This page intentionally left blank Page 4A-2 Issue 2 Revision -, Aug. 2015...
  • Page 22 AFM Supplement DA 40 D CHAPTER 4B ABNORMAL OPERATING PROCEDURES For abnormal operating procedures refer to basic AFM. Page 4B-1 Issue 2 Revision -, Aug. 2015...
  • Page 23 AFM Supplement DA 40 D This page intentionally left blank Page 4B-2 Issue 2 Revision -, Aug. 2015...
  • Page 24  Note: The chapter not relevant to the respective propeller can be omitted. 5.3 PERFORMANCE TABLES AND DIAGRAMS 5.3.2 Diagram for setting engine performance Not valid for TAE 125-02-114 engine installation. Page 5(a)-1 Issue 2 Revision -, Aug. 2015...
  • Page 25 AFM Supplement DA 40 D 5.3.7 Take-off distance Take-off distance at 1150 kg, 2535 lb Weight: 1150 kg / 2535 lb Flaps: T/O : 59 KIAS Power: MAX Airspeed for initial climb: 66 KIAS Runway: dry, level, paved ISA + 10°C ISA + 20°C ISA + 30°C (ft)
  • Page 26 AFM Supplement DA 40 D Take-off distance at 1150 kg, 2535 lb (continued) Weight: 1150 kg / 2535 lb Flaps: T/O : 59 KIAS Power: MAX Airspeed for initial climb: 66 KIAS Runway: dry, level, paved ISA + 18°F ISA + 36°F ISA + 54°F (ft) (ft)
  • Page 27 AFM Supplement DA 40 D Take-off distance at 1000 kg, 2205 lb Weight: 1000 kg / 2205 lb Flaps: T/O : 55 KIAS Power: MAX Airspeed for initial climb: 60 KIAS Runway: dry, level, paved ISA + 10°C ISA + 20°C ISA + 30°C (ft) 1000...
  • Page 28 AFM Supplement DA 40 D Take-off distance at 1000 kg, 2205 lb (continued) Weight: 1000 kg / 2205 lb Flaps: T/O : 55 KIAS Power: MAX Airspeed for initial climb: 60 KIAS Runway: dry, level, paved ISA + 18°F ISA + 36°F ISA + 54°F (ft) (ft)
  • Page 29 AFM Supplement DA 40 D Take-off distance at 980 kg, 2161 lb Weight: 980 kg / 2161 lb Flaps: T/O : 54 KIAS Power: MAX Airspeed for initial climb: 59 KIAS Runway: dry, level, paved ISA + 10°C ISA + 20°C ISA + 30°C (ft) 1000...
  • Page 30 AFM Supplement DA 40 D Take-off distance at 980 kg, 2161 lb (continued) Weight: 980 kg / 2161 lb Flaps: T/O : 54 KIAS Power: MAX Airspeed for initial climb: 59 KIAS Runway: dry, level, paved ISA + 18°F ISA + 36°F ISA + 54°F (ft) (ft)
  • Page 31 AFM Supplement DA 40 D 5.3.8 Climb Performance - Take-off climb Take-off at 1150 kg, 2535 lb Notes: For operation in air colder than provided, use coldest data For operation in air warmer than provided, use extreme caution Weight: 1150 kg / 2535 lb Flaps: T/O Airspeed for initial climb: 66 KIAS Power: MAX...
  • Page 32 AFM Supplement DA 40 D 5.3.9 Climb Performance - Cruise climb Cruise climb at 1150 kg, 2535 lb Notes: For operation in air colder than provided, use coldest data For operation in air warmer than provided, use extreme caution Weight: 1150 kg / 2535 lb Flaps: UP Airspeed for initial climb: 78 KIAS Power: MAX...
  • Page 33 AFM Supplement DA 40 D Cruise climb at 1000 kg, 2205 lb Notes: For operation in air colder than provided, use coldest data For operation in air warmer than provided, use extreme caution Weight: 1000 kg / 2205 lb Flaps: UP Airspeed for initial climb: 78 KIAS Power: MAX RATE OF CLIMB (feet per minute)
  • Page 34 AFM Supplement DA 40 D Cruise climb at 980 kg, 2161 lb Conditions: Notes: For operation in air colder than provided, use coldest data For operation in air warmer than provided, use extreme caution Weight: 980 kg / 2161 lb Flaps: UP Airspeed for initial climb: 78 KIAS Power: MAX...
  • Page 35 AFM Supplement DA 40 D 5.3.10 Cruise Performance Cruise performance, standard tanks Conditions: Weight ............1150 kg, 2535 lb Standard Tanks......106 l, 28 US gal usable fuel Flaps ..................UP Notes: Endurance information is based on standard tanks with 106 l (28 US gal) usable fuel.
  • Page 36 AFM Supplement DA 40 D Weight: 1150 kg / 2535 lb Flaps: Standard Tanks: 106 l (28 US gal) usable fuel Pres. Load KTAS Fuel Flow Range Endurance Alt. (ft) (kt) (l/h) (US gal/h) (NM) (hrs) 33.6 29.6 25.8 22.1 18.6 15.3 2000...
  • Page 37 AFM Supplement DA 40 D Weight: 1150 kg / 2535 lb Flaps: Standard Tanks: 106 l (28 US gal) usable fuel Pres. Load KTAS Fuel Flow Range Endurance Alt. (ft) (kt) (l/h) (US gal/h) (NM) (hrs) 10000 29.6 10000 25.8 10000 22.1 10000...
  • Page 38 AFM Supplement DA 40 D Cruise performance, long range tanks Conditions: Weight ............1150 kg, 2535 lb Long Range Tanks...... 147.6 l, 39 US gal usable fuel Flaps ..................UP Notes: Endurance information is based on long-range tanks with 147.6 l (39 US gal) usable fuel. Endurance time of this table is reduced by the time for startup and taxi, time, fuel and distance to climb and 45 min reserve.
  • Page 39 AFM Supplement DA 40 D Weight: 1150 kg / 2535 lb Flaps: Long Range Tanks: 147.6 l (39 US gal) usable fuel Pres. Load KTAS Fuel Flow Range Endurance Alt. (ft) (kt) (l/h) (US gal/h) (NM) (hrs) 33.6 29.6 25.8 22.1 18.6 15.3...
  • Page 40 AFM Supplement DA 40 D Weight: 1150 kg / 2535 lb Flaps: Long Range Tanks: 147.6 l (39 US gal) usable fuel Pres. Load KTAS Fuel Flow Range Endurance Alt. (ft) (kt) (l/h) (US gal/h) (NM) (hrs) 10000 29.6 10000 25.8 10000 22.1...
  • Page 41 AFM Supplement DA 40 D 5.3.15 Approved Noise Data With TAE 125-02-114 engine and Muffler LA50 Installed: ICAO Annex 16 Chapter X........69.6 dB(A) Page 5(a)-18 Issue 2 Revision -, Aug. 2015...
  • Page 42  Note: The chapter not relevant to the respective propeller can be omitted. 5.3 PERFORMANCE TABLES AND DIAGRAMS 5.3.2 Diagram for setting engine performance Not valid for TAE 125-02-114 engine installation. Page 5(b)-1 Issue 2 Revision -, Aug. 2015...
  • Page 43 AFM Supplement DA 40 D 5.3.7 Take-off distance Take-off distance at 1150 kg, 2535 lb 1150 kg / Weight: Flaps: T/O 2535 lb : 59 KIAS Power: MAX Airspeed for initial climb: 66 KIAS Runway: dry, level, paved ISA + 10°C ISA + 20°C ISA + 30°C ISA + 35°C...
  • Page 44 AFM Supplement DA 40 D Take-off distance at 1150 kg, 2535 lb (continued) 1150 kg / Weight: Flaps: T/O 2535 lb : 59 KIAS Power: MAX Airspeed for initial climb: 66 KIAS Runway: dry, level, paved ISA + 18°F ISA + 36°F ISA + 54°F ISA + 63°F (ft)
  • Page 45 AFM Supplement DA 40 D Take-off distance at 1050 kg, 2315 lb 1050 kg / Weight: Flaps: T/O 2315 lb : 55 KIAS Power: MAX Airspeed for initial climb: 60 KIAS Runway: dry, level, paved ISA + 10°C ISA + 20°C ISA + 30°C ISA + 35°C (ft)
  • Page 46 AFM Supplement DA 40 D Take-off distance at 1050 kg, 2315 lb (continued) 1050 kg / Weight: Flaps: T/O 2315 lb : 55 KIAS Power: MAX Airspeed for initial climb: 60 KIAS Runway: dry, level, paved ISA + 18°F ISA + 36°F ISA + 54°F ISA + 63°F (ft)
  • Page 47 AFM Supplement DA 40 D Take-off distance at 980 kg, 2161 lb Weight: 980 kg / 2161 lb Flaps: T/O : 54 KIAS Power: MAX Airspeed for initial climb: 59 KIAS Runway: dry, level, paved ISA + 10°C ISA + 20°C ISA + 30°C ISA + 35°C (ft)
  • Page 48 AFM Supplement DA 40 D Take-off distance at 980 kg, 2161 lb (continued) Weight: 980 kg / 2161 lb Flaps: T/O : 54 KIAS Power: MAX Airspeed for initial climb: 59 KIAS Runway: dry, level, paved ISA + 18°F ISA + 36°F ISA + 54°F ISA + 63°F (ft)
  • Page 49 AFM Supplement DA 40 D 5.3.8 Climb Performance - Take-off climb Take-off at 1150 kg, 2535 lb Notes: For operation in air colder than provided, use coldest data For operation in air warmer than provided, use extreme caution Weight: 1150 kg / 2535 lb Flaps: T/O Airspeed for initial climb: 66 KIAS Power: MAX...
  • Page 50 AFM Supplement DA 40 D 5.3.9 Climb Performance - Cruise climb Cruise climb at 1150 kg, 2535 lb Notes: For operation in air colder than provided, use coldest data For operation in air warmer than provided, use extreme caution Weight: 1150 kg / 2535 lb Flaps: UP Airspeed for initial climb: 78 KIAS Power: MAX...
  • Page 51 AFM Supplement DA 40 D Cruise climb at 1050 kg, 2315 lb Notes: For operation in air colder than provided, use coldest data For operation in air warmer than provided, use extreme caution Weight: 1050 kg / 2315 lb Flaps: UP Airspeed for initial climb: 78 KIAS Power: MAX RATE OF CLIMB (feet per minute)
  • Page 52 AFM Supplement DA 40 D Cruise climb at 980 kg, 2161 lb Notes: For operation in air colder than provided, use coldest data For operation in air warmer than provided, use extreme caution Weight: 980 kg / 2161 lb Flaps: UP Airspeed for initial climb: 78 KIAS Power: MAX RATE OF CLIMB (feet per minute)
  • Page 53 AFM Supplement DA 40 D 5.3.10 Cruise Performance Cruise performance, standard tanks Conditions: Weight ............1150 kg, 2535 lb Standard Tanks......106 l (28 US gal) usable fuel Flaps ..................UP Notes: Endurance information is based on standard tanks with 106 l (28 US gal) usable fuel. Endurance time of this table is reduced by the time for startup and taxi, time, fuel and distance to climb and 45 min reserve.
  • Page 54 AFM Supplement DA 40 D Weight: 1150 kg / 2535 lb Flaps: Standard Tanks: 106 l (28 US gal) usable fuel Pres. Load KTAS Fuel Flow Range Endurance Alt. (ft) (kt) (l/h) (US gal/h) (NM) (hrs) 33.6 29.6 25.8 22.1 18.6 15.3 2000...
  • Page 55 AFM Supplement DA 40 D Weight: 1150 kg / 2535 lb Flaps: Standard Tanks: 106 l (28 US gal) usable fuel Pres. Load KTAS Fuel Flow Range Endurance Alt. (ft) (kt) (l/h) (US gal/h) (NM) (hrs) 10000 29.6 10000 25.8 10000 22.1 10000...
  • Page 56 AFM Supplement DA 40 D Cruise performance, long range tanks Conditions: Weight ............1150 kg, 2535 lb Long Range Tanks.....147.6 l (39 US gal) usable fuel Flaps ..................UP Notes: Endurance information is based on long-range tanks with 147.6 l (39 US gal) usable fuel. Endurance time of this table is reduced by the time for startup and taxi, time, fuel and distance to climb and 45 min reserve.
  • Page 57 AFM Supplement DA 40 D Weight: 1150 kg / 2535 lb Flaps: Long Range Tanks: 147.6 l (39 US gal) usable fuel Pres. Load KTAS Fuel Flow Range Endurance Alt. (ft) (kt) (l/h) (US gal/h) (NM) (hrs) 33.6 29.6 25.8 22.1 18.6 15.3...
  • Page 58 AFM Supplement DA 40 D Weight: 1150 kg / 2535 lb Flaps: Long Range Tanks: 147.6 l (39 US gal) usable fuel Pres. Load KTAS Fuel Flow Range Endurance Alt. (ft) (kt) (l/h) (US gal/h) (NM) (hrs) 10000 29.6 29.6 10000 25.8 25.8...
  • Page 59 AFM Supplement DA 40 D 5.3.15 Approved Noise Data With TAE 125-02-114 engine and Muffler LA50 Installed: ICAO Annex 16 Chapter X........70.5 dB(A) Page 5(b)-18 Issue 2 Revision -, Aug. 2015...
  • Page 60 MASS AND BALANCE / EQUIPMENT LIST 6.3 MASS AND BALANCE REPORT After installation of the TAE 125-02-114 engine installation, the empty mass and empty mass moment must be established. Refer to the basic AFM and basic AMM for the DAI DA 40 D.
  • Page 61 AFM Supplement DA 40 D 6.5 EQUIPMENT LIST AND EQUIPMENT INVENTORY The following equipment is approved for the TAE 125-02-114 engine installation. Manu- Description Type Part No. facturer stalled ENGINE Engine TAE 125-02-114 Technify Motors GmbH Engine 05-7610-E0001 02 Technify...
  • Page 62 CHAPTER 7 DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS 7.9.1 ENGINE, GENERAL The TAE 125-02-114 engine has the same general characterics as the TAE 125-02-99 engine, except for the continuous and maximum power. Max. power: 114 kW (155 DIN-HP) at 2300 RPM, ISA, SL Max.
  • Page 63 Heat heat-exchanger is part of the liquid cooling system as well as a gearbox oil heat-exchanger. The gearbox oil heat- exchanger is part of the TAE 125-02-114 engine, but connected to the aircraft liquid cooling system. Refer to Figure 7-1 for a schematic.
  • Page 64 Alterations and repairs to the STC installation may be carried out only according to the supplement to the Airplane Maintenance Manual AMM-50-02 or i.a.w. a repair scheme which has been approved by Technify Motors GmbH or by the competent Airworthiness Authority. Page 8-1 Issue 2 Revision -, Aug.
  • Page 65 AFM Supplement DA 40 D This page intentionally left blank Page 8-2 Issue 2 Revision -, Aug. 2015...
  • Page 66 CHAPTER 9 SUPPLEMENTS 9.1 INTRODUCTION This chapter lists the supplements to the basic AFM that are affected by the TAE 125-02-114 engine istallation. For the affected supplements, a supplement has been created which adds or supersedes the affected supplements as described.
  • Page 67 AFM Supplement DA 40 D This page intentionally left blank Page 9-2 Issue 2 Revision -, Aug. 2015...
  • Page 68 TAE 125-02-114 Engine Installation This supplement must be attached to the EASA approved Airplane Flight Manual when the TAE 125-02-114 engine has been installed in accordance with EASA STC 10036328. The information contained in this supplement supersedes or adds to the EASA approved Airplane Flight Manual and supplement A31 only as set forth herein.
  • Page 69 AFM Supplement DA 40 D Supplement 1, Garmin G1000, VFR Approved Issue Pages Description Date Endorsed New Issue Aug. 15, EASA STC Change of Ownership 10036328, 2015 Rev. 3 Remark: The parts of the text which changed are marked with a vertical line on the margin of the page.
  • Page 70 Supplement 1, Garmin G1000, VFR 1. General This supplement contains the required information for operation of the airplane with a TAE 125-02-114 engine installation and the Garmin G1000 avionic system installed. This supplement must be used in conjunction with the basic DAI AFM incl.
  • Page 71 AFM Supplement DA 40 D Supplement 1, Garmin G1000, VFR 7. Description of the airplane and its systems No change. Refer to supplement A31 of the basic AFM. 8. Airplane Handling, Care and Maintenance No change. Refer to supplement A31 of the basic AFM. Page 9-1-4 Issue 2 Revision -, Aug.
  • Page 72 TAE 125-02-114 Engine Installation This supplement must be attached to the EASA approved Airplane Flight Manual when the TAE 125-02-114 engine has been installed in accordance with EASA STC 10036328. The information contained in this supplement supersedes or adds to the EASA approved Airplane Flight Manual and supplement A32 only as set forth herein.
  • Page 73 AFM Supplement DA 40 D Supplement 2, Garmin G1000, IFR Approved Issue Pages Description Date Endorsed New Issue Aug. 15, EASA STC Change of Ownership 10036328, 2015 Rev. 3 Remark: The parts of the text which changed are marked with a vertical line on the margin of the page.
  • Page 74 Supplement 2, Garmin G1000, IFR 1. General This supplement contains the required information for operation of the airplane with a TAE 125-02-114 engine installation and the Garmin G1000 avionic system installed. This supplement must be used in conjunction with the basic DAI AFM incl.
  • Page 75 AFM Supplement DA 40 D Supplement 2, Garmin G1000, IFR 7. Description of the airplane and its systems No change. Refer to supplement A32 of the basic AFM. 8. Airplane Handling, Care and Maintenance No change. Refer to supplement A32 of the basic AFM. Page 9-2-4 Issue 2 Revision -, Aug.

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