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General| Engine | Lycoming IO-360-L2A |
|---|---|
| Service Ceiling | 13, 500 ft |
| Length | 27 ft 2 in |
| Wingspan | 36 ft 1 in |
| Height | 8 ft 11 in |
| Fuel Capacity | 56 gallons |
| Max Cruise Speed | 124 knots |
| Range | 696 nm |
| Avionics | Garmin G1000 |
Lists maximum and cruise speeds for the aircraft.
Details ground roll and obstacle clearance distances for takeoff.
Details ground roll and obstacle clearance distances for landing.
Lists stall speeds with flaps up/down and power off.
Specifies ramp, takeoff, and landing weights.
Defines the maximum load the airplane can carry.
Details the engine manufacturer, model, type, and power rating.
Provides basic data on the airplane's engine and propeller.
Details fuel capacity and grade specifications.
Lists maximum weights for ramp, takeoff, and landing.
Defines terms used in weight and balance calculations.
Details airspeed limitations and their significance.
Lists limitations for the engine and propeller.
Specifies maximum weights for normal and utility categories.
Outlines limits for normal and utility category maneuvers.
Lists critical airspeeds for various emergency scenarios.
Provides immediate action items for engine failures.
Details procedures for engine failure during takeoff roll and after takeoff.
Outlines procedures for emergency landing without engine power.
Provides procedures for fires during start and in flight.
Details procedures for inadvertent icing encounters.
Addresses high volts and low volts annunciator conditions.
Lists normal operating airspeeds for takeoff, climb, and landing.
Outlines preflight inspection procedures and checks.
Details the walk-around inspection and cabin checks.
Lists steps for preparing to start the engine.
Provides step-by-step instructions for starting the engine using the battery.
Provides instructions for starting the engine using external power.
Details pre-takeoff checks and configurations.
Outlines procedures for normal and short field takeoffs.
Details normal cruise power settings and procedures.
Lists steps to prepare for landing.
Covers normal and short field landing procedures.
Provides detailed information on starting the engine.
Procedure for checking magneto operation.
Procedure for checking alternator and electrical system.
Procedure for checking engine operation at full throttle.
Describes stall characteristics and warning systems.
Covers procedures for holding, procedure turns, and missed approaches.
Details takeoff distance calculations, including wind correction.
Discusses selecting cruising altitude and power settings.
Estimates total fuel needed for the flight, including reserve.
Describes estimating landing distance.
Lists stall speeds at maximum weight and various bank angles.
Details takeoff distances for short fields at max weight.
Details takeoff distances for short fields at 2400 lbs.
Details takeoff distances for short fields at 2200 lbs.
Provides rate of climb data at max weight.
Presents cruise performance data for various altitudes and powers.
Details landing distances for short fields at max weight.
Details steps for weighing the airplane.
Explains how to use loading data for weight and balance.
Graphical representation of CG limits.
Specifies CG limits for normal and utility categories.
Describes the airplane's construction, wings, and control surfaces.
Explains the flight control system operation.
Describes the construction and components of the instrument panel.
Explains primary flight instruments on the GDU 1040 PFD.
Provides an overview of the engine specifications and accessories.
Explains throttle and mixture control operations.
Describes the Engine Indicating System (EIS) displays.
Explains the fuel injection system components and operation.
Outlines the components of the airplane fuel system.
Specifies correct FUEL SELECTOR valve positions for various operations.
Details the hydraulic brake system and operation.
Describes the DC electrical system components.
Explains voltmeter and ammeter indications.
Describes the LOW VOLTS annunciation and causes.
Details the pitot-static system and its instruments.
Describes the vacuum system and its instruments.
Introduces the Garmin G1000 avionics system.
Explains the ELT installation and operation.
Details the cabin fire extinguisher and its operation.
Outlines FAA required inspection schedules.
Details annual and 100-hour inspection requirements.
Covers oil specifications and viscosity recommendations.
Lists approved fuel grades and capacity.
Describes causes and detection of fuel contamination.
Information for Pointer ELT installation and operation.
Operating information for the Bendix/King KAP 140 Autopilot.
Information for Artex C406-N ELT installation and operation.
Operating information for the Bendix/King KR87 ADF.
