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General| Brand | Diamond Aircraft |
|---|---|
| Model | DA 50 C |
| Category | Aircrafts |
| Language | English |
Details the certification basis for the DA 50 C aircraft, including EASA and FAA approvals.
Lists incorporated changes and revisions to the Airplane Flight Manual.
Provides an introduction to the Airplane Flight Manual and its purpose.
Explains the meaning of WARNING, CAUTION, and NOTE terms used in the manual.
Details the overall dimensions, wings, flaps, ailerons, and stabilizers of the DA 50 C.
Defines common acronyms related to airspeeds and meteorological terms.
Provides conversion factors between SI units and US units for various dimensions.
Presents a three-view drawing of the DA 50 C airplane with key dimensions.
Describes the Garmin G1000 NXi integrated avionics system and its capabilities.
Introduces operating limitations and emphasizes adherence for safe operation.
Specifies airspeed limitations for various flight conditions and configurations.
Explains the significance of markings on the airspeed indicator.
Details limitations for the engine, propeller, oil pressure, and temperatures.
Describes engine instrument markings and their corresponding color code significance.
Specifies the maximum and minimum mass limits for safe operation.
Defines the Datum Plane and flight CG position limits with a graphical range.
Lists approved maneuvers and flight conditions, emphasizing limitations.
Details maneuvering load factors for positive and negative G-loads at various speeds.
States the maximum operating altitude and mentions potential altitude restrictions.
Specifies the minimum crew requirement and maximum number of occupants.
Lists approved kinds of operation (VFR, IFR, day/night) and minimum equipment.
Shows relevant limitation placards for the DA 50 C airplane.
Specifies approved fuel designations, quantities, and additives.
Defines temperature limits for airplane operation and pre-heating requirements.
Outlines requirements for battery charge, especially for night or IFR flights.
Specifies that doors must not be blocked by the key lock during operation.
Prohibits the use of Portable Electronic Devices (PED) during low visibility approaches.
States that smoking in the airplane is not permitted.
Describes the Garmin G1000 NXi system's operational capabilities and navigation requirements.
Details limitations for GPS navigation, including RAIM and database requirements.
Outlines autopilot limitations, disengagement procedures, and system checks.
Provides general guidance on handling emergencies, prioritizing flight control.
Lists critical airspeeds for emergency situations like gliding and gear extension.
Describes how to tune the emergency frequency (121.500 MHz) on the G1000.
Lists CAS warning messages and their corresponding causes and corrective actions.
Procedure for high load or high current on alternators.
Procedure for failure of both engine alternators, emphasizing electrical load reduction.
Procedure for high coolant temperature, including actions for COOLANT LVL caution.
Procedure for high engine oil temperature, with actions based on oil pressure.
Procedure for low or high fuel pressure warnings.
Procedure for high gearbox oil temperature.
Procedures for dealing with unlocked doors, including rear door warnings.
Procedure for high fuel temperature in left or right fuel tanks.
Procedure for low or high engine oil pressure indications.
Procedure for starter malfunction, including actions for disengaged starter.
Procedure for high engine air intake temperature.
Procedures for engine failure during take-off, with and without sufficient runway.
Procedures for engine failures occurring while the aircraft is on the ground.
Procedure for engine failure during flight, including icing conditions.
Procedure for attempting to restart the engine in flight.
Procedure for defective RPM regulating system, covering oscillating RPM and overspeed.
Procedure for a defective cowl flap indicator light.
Troubleshooting steps for engine issues encountered in flight.
Procedure for manually extending the landing gear in an emergency.
Procedure for landing with a defective tire on the main landing gear.
Recommendations for landing with defective brakes.
Describes the landing gear unsafe warning light and actions to take.
Procedure for landing with the landing gear retracted (gear up).
Procedure for a complete failure of the electrical system.
Procedure for handling an engine fire while the aircraft is on the ground.
Procedure for electrical fire with smoke occurring on the ground.
Procedure for smoke or fire during take-off that can be aborted.
Procedure for smoke or fire during take-off that cannot be aborted.
Procedure for handling an engine fire during flight.
Procedure for electrical fire with smoke occurring in flight.
Procedure for unintentional flight into icing conditions.
Procedure for suspected carbon monoxide contamination in the cabin.
Step-by-step procedure for recovering from an aircraft spin.
Procedure for gliding the aircraft, including airspeed and flap settings.
Procedure for executing an emergency descent.
Information on the location and operation of the emergency exit.
Procedure for performing an emergency landing with the engine off.
Procedure for autopilot or electric trim malfunctions and failures.
Lists CAS caution messages related to the G1000 and their corrective actions.
Procedure for a failure of alternator 1.
Procedure for a failure of alternator 2.
Procedure for the CHECK GEAR caution message.
Procedure for a low coolant level caution.
Procedure for an Engine Control Unit A failure.
Procedure for an Engine Control Unit B failure.
Procedure for a low fuel quantity caution message.
Procedure for pitot heat failure or being switched off.
Procedure for stall warning heat failure or being switched off.
Procedure for essential bus voltage being low.
Procedure for stall warning system failure.
Procedure for high engine air intake temperature.
Procedure for failure in the electrical rudder trim system indication or function.
Procedure for failure in the flap operating system indication or function.
Procedure for starting the engine with external power.
Procedure for starting the engine with external power.
Instructions to follow after a lightning strike.
Procedure for a defective fuel transfer system.
Procedure for autopilot disconnect, indicated by yellow AP flashing on PFD.
Procedure for autopilot overspeed recovery.
Procedure for loss of navigation information (VOR, VAPP, GPS or LOC flashing).
Procedure for autopilot out of trim conditions.
Describes flashing yellow mode annunciations and system reversion.
Details effects of G1000 NXi system losses on autopilot operation.
Introduces the chapter containing checklists and procedures for normal operation.
Describes the flight characteristics and handling of the DA 50 C.
Provides essential airspeeds for normal operation across different flight masses.
Outlines the daily checks to be performed before the first flight of the day.
Details the pre-flight inspection steps for the cabin and its equipment.
Provides a detailed walk-around check procedure for the aircraft's exterior.
Checklist for procedures before starting the engine.
Procedure for starting the aircraft engine, including cautions and notes.
Checklist for procedures to be followed before taxiing.
Procedure and cautions for taxiing the aircraft.
Checklist for procedures to be completed before take-off.
Normal operating procedure for take-off, including speeds and conditions.
Procedure for climbing the aircraft, with cautions for oil/coolant temperature.
Describes autopilot operation during climb using VS and FLC modes.
Procedure for maintaining cruise flight, including power settings and fuel transfer.
Describes autopilot operation during cruise using VS, FLC, and Altitude Hold modes.
Procedure for descending the aircraft, including PEDs usage.
Describes autopilot operation during descent using VS and FLC modes.
Procedure for approach and landing, including backrest position and speeds.
Describes autopilot operation during approach and landing for VOR, ILS, and GPS.
Procedure for executing a go-around maneuver.
Describes autopilot operation during a go-around.
Post-operation procedures after landing.
Procedure for shutting down the engine.
Procedure for exiting the airplane after parking.
Procedure for post-flight inspection and recording issues.
Procedures for parking the airplane, including gust lock usage.
Operating considerations for flight in rain, snow, or visible moisture.
Procedures and precautions for refueling the aircraft.
Considerations for flight at high altitudes, including oxygen provision.
Introduction to performance tables and diagrams and their conditions.
Guidance on using performance data tables and diagrams for flight planning.
Provides calibrated airspeeds corresponding to indicated airspeeds for flaps TO/LDG and UP.
Presents the International Standard Atmosphere chart for reference.
Lists stalling speeds at various flight masses and bank angles.
Provides a chart for determining wind components.
Details factors affecting take-off distance and provides warnings.
Provides SI units take-off distances for 1999 kg at various conditions.
Provides SI units take-off distances for 1800 kg at various conditions.
Provides SI units take-off distances for 1600 kg at various conditions.
Describes climb performance during take-off climb and provides gradient formula.
Provides climb rates for 1999 kg at various altitudes and temperatures.
Provides climb rates for 1800 kg at various altitudes and temperatures.
Provides climb rates for 1600 kg at various altitudes and temperatures.
Describes climb performance during cruise climb and provides gradient formula.
Provides cruise climb rates for 1999 kg at various conditions.
Provides cruise climb rates for 1800 kg at various conditions.
Provides cruise climb rates for 1600 kg at various conditions.
Provides time, fuel, and distance data for climbing at 1999 kg.
Provides time, fuel, and distance data for climbing at 1800 kg.
Provides time, fuel, and distance data for climbing at 1600 kg.
Describes cruise performance conditions.
Provides cruise performance data for 1999 kg at various conditions.
Details factors affecting landing distance and provides warnings.
Provides SI units landing distances for 1999 kg at various conditions.
Provides imperial units landing distances for 1800 kg at various conditions.
Provides SI units landing distances for 1600 kg at various conditions.
Provides SI units landing distances for 1999 kg with abnormal flap positions.
Provides imperial units landing distances for 1800 kg with abnormal flap positions.
Provides SI units landing distances for 1600 kg with abnormal flap positions.
Describes go-around climb performance and provides gradient formula.
Provides go-around climb rates for 1999 kg at various conditions.
Provides go-around climb rates for 1800 kg at various conditions.
Provides go-around climb rates for 1600 kg at various conditions.
Provides glide ratio and maximum horizontal distance per 1000 ft altitude loss.
States the maximum flight mass and ICAO/CS-36 noise levels.
Introduction to mass and balance, pilot responsibility, and CG range.
Defines the Datum Plane (DP) and its location relative to the airplane.
Details conditions for establishing empty mass and recording changes.
Enables operation within mass and balance limits, requiring tables and diagrams.
Lists important lever arms aft of the Datum Plane for various items.
Presents a loading diagram illustrating mass, fuel quantity, and load moment.
Guides on calculating loading conditions and verifying CG positions.
Shows the permissible center of gravity range graphically.
Presents the permissible moment range graphically.
Lists approved equipment for installation and the equipment inventory.
Describes the construction of the fuselage, wings, and empennage.
Explains the operation of ailerons, elevator, flaps, and rudder.
Details the construction and operation of the ailerons.
Describes the two-piece flap construction, operation, and position indicator.
Details the construction and operation of the rudder.
Describes the construction and operation of the elevator.
Explains the elevator trim control and its take-off position indication.
Describes the rudder trim control and its indication on the G1000 NXi MFD.
Details the electrical pedal adjustment and locking mechanism.
Lists major instruments and controls on the instrument panel.
Provides an overview of the landing gear system, including its functions and operation.
Illustrates the hydraulic gear extension system's operating modes and conditions.
Describes the wheel brakes and the parking brake system.
Details the construction and adjustment of the crew seats and safety harnesses.
Describes the operation and locking of the left and right pilot doors.
Describes the operation and locking of the passenger door.
Details the emergency exit window integration and activation process.
Information on the location and use of the egress hammer for emergency exits.
Describes the functions and operation of the heating and ventilation system.
Provides general information and key specifications for the Centurion 3.0 engine.
Describes the variable pitch three-bladed propeller and its construction.
Explains the propeller pitch control system and its relationship with the FADEC.
Details the operation of the power lever and FADEC system.
Lists engine instruments displayed on the Garmin G1000 NXi.
Describes the liquid cooling system, including short, external, and bypass circuits.
Explains the turbo-charger system, including exhaust gases, FADEC control, and intercooler.
Describes the FADEC system's role in electronic engine management.
Details the fuel system's operation, including low and high pressure circuits.
Describes the feeder pumps, main pump, and emergency pump operation.
Explains the location and operation of the fuel valve with its three positions.
Describes the main and auxiliary fuel tanks, their capacity, and components.
Details the alternate means for fuel quantity indication for ground use.
Describes the electrical system, power generation, storage, and distribution.
Describes the Mid Continent MD302 Standby Attitude Module.
Explains the crew alerting system levels (Warning, Caution, Advisory) and alert display.
Describes the integrated avionics system and its components.
Details the PFD display format, controls, and crew alerting system integration.
Describes the MFD display functions, including engine data and maps.
Describes the audio panel's functions, including intercom and marker beacon system.
Explains the AHRS system for determining attitude, slip, and heading.
Describes the ADC's function in providing airspeed, altitude, and temperature data.
Details the optional PFD/MFD control unit for data entry and tuning.
Describes the GFC 700 autopilot system features and disconnection means.
Explains the pitot-static system, including pressure measurement and alternate static source.
Describes the stall warning system, its location, and activation.
Details the baggage compartment areas, mass limits, and securing methods.
Explains the installation and adjustment of trim weights for CG adjustment.
Contains manufacturer recommended procedures for ground handling and servicing.
Outlines scheduled and unscheduled maintenance inspection requirements.
Specifies that alterations or repairs must follow the Airplane Maintenance Manual.
Provides detailed procedures and safety precautions for refueling the aircraft.
Step-by-step procedure for checking the engine oil level.
Procedure for checking the gearbox oil level.
Procedure for checking and correcting tire inflation pressures.
Provides guidance on moving the airplane on the ground and towing procedures.
Procedures for parking the airplane, including gust lock installation and removal.
Describes mooring points for securing the airplane to the ground.
Information on the locations for jacking the airplane.
Provides procedures for cleaning painted surfaces, doors, propeller, and interior.
Lists approved fluids and procedures for cleaning ice and snow from the aircraft.
Lists additional optional equipment and their corresponding AFM supplements.
