Phoenix S-LSA Glider 02/U15 User Manual

Phoenix S-LSA Glider
02/U15
Aircraft Operating
Instructions

Phoenix S-LSA Glider 02/U15 Specifications

General

Wing Area	13.6 m2 (146 sq ft)
Aspect Ratio	16.5
Wingspan	15.00 m
Max Takeoff Weight	472.5 kg (1, 042 lb)
MTOW	472.5 kg (1, 042 lb)

Summary

Aircraft and Systems Descriptions

Operating Weights and Loading

Details on minimum load, maximum weights, and takeoff/landing weights.

Fuel and Fuel Capacity

Engine Specifications and Parameters

Information on engine manufacturer, model, power, RPM, temps, and pressures.

Operating Limitations

Stalling Speeds and Flap Extended Range

Stalling speeds (Vs1, Vs0) and speed range (Vs0, VFE) with flaps extended.

Speed Limitations (VA, VNE, VT, VLO)

Covers maneuvering, never exceed, aerotow, and landing gear speeds.

Crosswind, Wind, and Load Factor Limitations

Weight and Balance Information

Center of Gravity (CG) Range and Determination

Details the procedure and calculation for determining the aircraft's CG.

Performance

Glider and Powered Glider Performance Metrics

Wind Limitations for Takeoff/Landing

Emergency Procedures

Engine Failure Management

Covers engine failure during takeoff run, after takeoff, and in flight.

In-Flight Engine Start and Fire Procedures

Procedure for in-flight start, and handling fire on ground, takeoff, or in flight.

Landing Emergencies

Procedures for emergency, precautionary, and forced landings.

Recovery from Unintentional Spin

Other Emergencies: Vibration and Icing

Normal Procedures

Pre-flight Check Procedure

Detailed procedure for a thorough pre-flight inspection of the aircraft.

Powered Glider Ground Operations

In-flight Operations: Cruise, Approach, and Landing

Airplane Ground Handling and Servicing

Servicing Fuel, Oil, and Coolant

Required Placards and Markings

Airspeed Indicator Markings and Limitations

Weight, Crew, and Luggage Limitations Placards