DA 42 AFM Rev. 4 DA42_Diamond Twin_Flight Manual DA42 Diamond Twin Flight
User Manual: DA42_Diamond-Twin_FlightManual
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- FRONT MATTER
- 1 GENERAL
- 2 OPERATING LIMITATIONS
- 2.1 Introduction
- 2.2 Airspeed
- 2.3 Airspeed Indicator Markings
- 2.4 Power-Plant Limitations
- 2.5 Engine Instrument Markings
- 2.6 Warning, Caution and Advisory Alerts
- 2.7 Mass (Weight)
- 2.8 Center of Gravity
- 2.9 Approved Maneuvers
- 2.10 Maneuvering Load Factors
- 2.11 Operating Altitude
- 2.12 Flight Crew
- 2.13 Kinds of Operation
- 2.14 Fuel
- 2.15 Limitation Placards
- 2.16 Other Limitations
- 3 EMERGENCY PROCEDURES
- 3.1 Introduction
- 3.2 Airplane-Related G1000 Warnings
- 3.3 G1000 System Warnings
- 3.4 G1000 Failures
- 3.5 One Engine Inoperative Procedures
- 3.5.1 Detecting the Inoperative Engine
- 3.5.2 Engine Troubleshooting
- 3.5.3 Engine Securing (Feathering) Procedure
- 3.5.4 Unfeathering & Restarting the Engine in Flight
- 3.5.5 Engine Failure During Take-off
- 3.5.6 Engine Failures in Flight
- 3.5.7 Landing with one Engine Inoperative
- 3.5.8 Go-around / Balked Landing with one Engine Inpoerative
- 3.5.9 Flight with One Engine Inoperative
- 3.6 Landing Gear System Failures
- 3.7 Failures in the Electrical System
- 3.8 Smoke and Fire
- 3.9 Other Emergencies
- 4A NORMAL OPERATING PROCEDURES
- 4A.1 Introduction
- 4A.3 Advisory Alerts on the G1000
- 4A.4 Flight Characteristics
- 4A.5 Daily Check
- 4A.6 Checklists for Normal Operating Procedures
- 4A.6.1 Pre-Flight Inspection
- 4A.6.2 Before Starting Engine
- 4A.6.3 Starting Engine
- 4A.6.4 Before Taxiing
- 4A.6.5 Taxiing
- 4A.6.6 Before Take-off
- 4A.6.7 Take-off
- 4A.6.8 Climb
- 4A.6.9 Cruise
- 4A.6.10 Descent
- 4A.6.11 Approach & Landing
- 4A.6.12 Go-around
- 4A.6.13 After Landing
- 4A.6.14 Shut-down
- 4A.6.15 Parking
- 4A.6.16 Exit Airplane
- 4A.6.17 Post Flight Inspection
- 4A.6.18 Flight in Rain
- 4A.6.19 Refueling
- 4A.6.20 Flight at High Altitude
- 4B ABNORMAL OPERATING PROCEDURES
- 4B.1 Precautionary Landing
- 4B.2 Canopy in Cooling Gap Position
- 4B.3 Engine Instrument Indications outside of Green Range on the G1000
- 4B.4 Caution-Alerts on the G1000
- 4B.4.1 Cautions/General
- 4B.4.2 L/R ECU A FAIL
- 4B.4.3 L/R ECU B FAIL
- 4B.4.4 L/R FUEL LOW
- 4B.4.5 Low Voltage Caution (LOW VOLTS)
- 4B.4.6 L/R ALTN FAIL
- 4B.4.7 L/R COOL LVL
- 4B.4.8 PITOT FAIL / HT OFF
- 4B.4.9 STALL HT FAIL / OFF
- 4B.4.10 L/R Fuel Transfer Fail (if Aux. Tanks Are Installed)
- 4B.4.11 L/R Auxiliary Fuel Tank Empty (if Aux. Tanks Installed)
- 4B.4.12 STICK LIMIT
- 4B.4.13 RAIM UNAVAIL
- 4B.4.14 AHRS ALIGNING - Keep Wings Level
- 4B.5 Failures in Flap Operating System
- 4B.6 Failures in Hydraulic System
- 4B.7 Starting Engine with External Power
- 5 PERFORMANCE
- 5.1 Introduction
- 5.2 Use of the Performance Tables and Diagrams
- 5.3 Performance Tables and Diagrams
- 5.3.1 Airspeed Calibration
- 5.3.2 Fuel Flow Diagram
- 5.3.3 International Standard Atmosphere
- 5.3.4 Stalling Speeds
- 5.3.5 Wind Components
- 5.3.6 Take-off Distance
- 5.3.7 Climb Performance - Take-off Climb
- 5.3.8 Climb Performance - Cruise Climb
- 5.3.9 One Engine Inoperative Climb Performance
- 5.3.10 Cruising (True Airspeed TAS)
- 5.3.11 Landing Distance
- 5.3.12 Gradient of Climb on Go-around
- 5.3.13 Approved Noise Data
- 6 MASS AND BALANCE
- 7 DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS
- 7.1 Introduction
- 7.2 Airframe
- 7.3 Flight Controls
- 7.4 Instrument Panel
- 7.5 Landing Gear
- 7.6 Seats and Safety Harnesses
- 7.7 Baggage Compartment
- 7.8 Canopy, Rear Door, and Cabin Interior
- 7.9 Power Plant
- 7.10 Electrical System
- 7.11 Pitot-Static System
- 7.12 Stall Warning System
- 7.13 Garmin G1000 Integrated Avionics System
- 8 AIRPLANE HANDLING, CARE AND MAINTENANCE
- 9 SUPPLEMENTS