Tecnam P2008 User Manual

FLIGHT MANUAL
US-LSA
P2008
Manufacturer
COSTRUZIONI AERONAUTICHE TECNAM S.r.l.
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 14December 2007.
Ed2 rev2- 06/02/2014

Tecnam P2008 Specifications

General

Manufacturer	Tecnam
Model	P2008
Aircraft Type	Light Sport Aircraft
Engine Power	100 hp
Maximum Takeoff Weight	600 kg (1, 323 lb)
Seating Capacity	2
Stall Speed	65 km/h
Service Ceiling	4, 572 m
Fuel Capacity	100 L

Summary

Section 1 General

1.5 Weights

Maximum weights, standard weights, and specific loadings.

1.8 Powerplant

Detailed information on engine, propeller, and fuel systems.

Section 2 Operating Limitations

2.1.1 Airspeed Limitations

2.1.15 Weight Limitations

Maximum takeoff and landing weight limitations.

2.1.16 Center of Gravity Limits

Acceptable center of gravity range for safe flight.

Section 3 Weight & Balance

3.3 Weight and Balance

Section 4 Performance

4.4 Stall Speeds

4.6 Takeoff Performance

Data for calculating takeoff distance and run.

4.7 Landing Distance

Data for calculating landing distance.

4.8 Climb Rate Performance

Section 5 Emergency Procedures

5.1 Engine Failures

Procedures for engine failure on ground and in flight.

5.2 Smoke and Fire

Emergency procedures for smoke and fire incidents.

5.3 Landing Emergency

Procedures for forced landings and emergency landings.

5.4 Recovery from Unintentional Spin

Section 6 Normal Procedures

6.2 Checklist Procedures

Section 8 Placards & Markings

8.1.11 Fuel Selector Valve

8.1.21 Limitation Placards

Supplement S1 Page Replacement Instructions