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General| Manufacturer | Tecnam |
|---|---|
| Model | P2008 JC |
| Engine Type | Rotax 912 S2 |
| Horsepower | 100 hp |
| Maximum Takeoff Weight | 600 kg (1, 323 lb) |
| Seating Capacity | 2 |
| Fuel Capacity | 100 l (26.4 US gal) |
| Cruise Speed | 120 knots |
| Service Ceiling | 14, 000 ft |
Details changes made to the manual.
Lists all effective pages in the manual.
Introduces the manual and its purpose.
Lists the main sections of the manual.
Purpose of Section 1.
Aircraft type approval and airworthiness category.
Definitions for safety-related terms.
Aircraft physical characteristics and dimensions.
Description of the aircraft engine.
Description of the propeller.
Movement limits of flight control surfaces.
Information on wing and power loading.
Glossary of terms and acronyms used.
Purpose of Section 2.
Critical airspeed limits for operation.
Color codes and explanations on the airspeed indicator.
Operating limits for the engine and propeller.
Fuel capacity and approved types.
Recommended engine lubricant.
Type of coolant used.
Requirements for aircraft painting.
Propeller specifications.
The highest altitude the aircraft can safely operate.
Operating temperature range for the aircraft.
Markings on powerplant instruments.
Markings on other aircraft instruments.
Maximum takeoff and landing weights.
Acceptable center of gravity limits.
List of flight maneuvers approved for the aircraft.
Limits for load factors during maneuvers.
Safe crosswind limits demonstrated.
Minimum crew and occupant limits.
Required equipment for different operations.
Placards indicating operational limitations.
Other placards found in the aircraft.
Purpose of Section 3.
Colors and meanings of alert lights.
Procedure for alternator failure.
Procedure for pitot heat system failure.
Procedures for G3X display failures.
Steps for evacuating the aircraft.
Procedure to shut down the engine in flight.
Procedures for engine failure scenarios.
Procedure for attempting engine restart in flight.
Procedures for cabin and engine fire incidents.
Procedures for emergency landings.
Procedure for recovering from an unintentional spin.
Procedures for other emergency situations.
Purpose of Section 4.
Significant airspeeds for normal flight operations.
Cabin and external checks before flight.
Checklists for various phases of normal operation.
Purpose of Section 5.
Guidance on interpreting performance data charts.
Graph showing calibrated vs. indicated airspeed.
Chart detailing standard atmospheric conditions.
Stall speeds in various configurations.
Maximum demonstrated crosswind limits.
Takeoff distances at various conditions.
Climb performance after takeoff.
Climb performance during en-route flight.
Data for cruise flight conditions.
Landing distances at various conditions.
Performance data for go-around.
Aircraft noise level information.
Purpose of Section 6.
Steps for weighing the aircraft.
Loading charts for weight and balance calculations.
Guidelines for loading baggage.
Comprehensive list of aircraft equipment.
Purpose of Section 7.
Description of the aircraft airframe.
Description of flight control systems.
Layout and components of the instrument panel.
Description of seats and harnesses.
Description of aircraft doors.
Description of engine and propeller.
Description of the aircraft's fuel system.
Description of the aircraft's electrical systems.
Description of the stall warning system.
Description of the aircraft's avionics systems.
Procedure for using external power.
Description of the pitot-static system.
Description of the aircraft's brake system.
Purpose of Section 8.
Requirements for aircraft inspections.
Procedures for aircraft modifications and repairs.
Routine maintenance tasks.
Procedure for checking engine cowlings.
Procedures for handling the aircraft on the ground.
Procedures for cleaning and caring for the aircraft.
Procedure for removing ice from the aircraft.
Purpose of Section 9.
List of available AFM supplements.
Revision history for Supplement S1.
Lists effective pages for Supplement S1.
Index for Supplement S1.
Purpose of Supplement S1.
Purpose of this Section 2.
Critical airspeed limits for VFR Night operation.
Markings on the airspeed indicator.
Operating limits for the powerplant.
Fuel specifications for VFR Night.
Lubricant recommendations.
Coolant type.
Painting requirements.
Propeller specifications.
Highest safe operating altitude.
Operating temperature range.
Markings on powerplant instruments.
Markings on other instruments.
Weight limitations.
Acceptable CG limits.
Permitted flight maneuvers.
Load factor limits during maneuvers.
Safe crosswind limits demonstrated.
Minimum crew and occupant limits.
Required equipment for VFR Day and Night.
Placards indicating operational limitations.
Other placards in the aircraft.
Purpose of this Section 3.
Colors and meanings of alert lights.
Procedure for alternator failure.
Procedure for pitot heat system failure.
Procedures for G3X display failures.
Steps for evacuating the aircraft.
Procedure to shut down the engine in flight.
Procedures for engine failure scenarios.
Procedure for attempting engine restart in flight.
Procedures for cabin and engine fire incidents.
Procedures for emergency landings.
Procedure for recovering from an unintentional spin.
Procedures for other emergency situations.
Purpose of this Section 4.
Significant airspeeds for normal flight operations.
Cabin and external checks before flight.
Checklists for various phases of normal operation.
