Tecnam P92 Eaglet User Manual

P92 Eaglet
Flight Manual
Revision Date: 12-14-2007
Revision Number: 1.00
Doc n° 27-13-100-00
1
FLIGHT MANUAL
US-LSA
P92 Eaglet
Manufacturer
COSTRUZIONI AERONAUTICHE TECNAM S.r.l.
Type Certificate: ASTM SLSA
Serial number: ________________
Build year: ___________________
Registration:__________________
Introduction
This manual contains information to be furnished to the pilot as required by the FAA in addition to further information
supplied by the manufacturer.
This manual must always be present on board the aircraft.
The aircraft is to be operated in compliance with information and limitations contained herein. All sections follow the
ASTM guidelines as finalized 14 December 2007.

Tecnam P92 Eaglet Specifications

General

Manufacturer	Tecnam
Model	P92 Eaglet
Type	Light Sport Aircraft
Seats	2
Engine	Rotax 912
Max Takeoff Weight	550 kg (1, 213 lb)
Service Ceiling	4, 000 m (13, 123 ft)
Height	2.5 m
Empty Weight	300 kg
Cruise Speed	185 km/h (115 mph)
Stall Speed	65 km/h (40 mph)
Power	100 hp (75 kW)
Wingspan	8.6 m (28.2 ft)

Summary

SECTION 2 OPERATING LIMITATIONS

2.1.1 Airspeed Limitations

Airspeed limitations and their operational significance for the aircraft.

2.1.3 Powerplant Limitations

2.1.16 Center of Gravity Limits

SECTION 4 PERFORMANCE

4.4 Stall Speeds

Table showing stall speeds based on flap setting and bank angle.

4.6 Takeoff Performance

Chart for determining takeoff distances based on altitude, weight, and temperature.

4.7 Landing Distance

SECTION 5 EMERGENCY PROCEDURES

5.1 Engine Failures

Procedures for engine failures on ground and during flight.

5.3 Landing Emergency

Procedures for forced landings with or without engine power.

5.4 Recovery from Unintentional Spin

Step-by-step guide for recovering from an unintentional spin.