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Cessna U206G STATIONAIR User Manual

Cessna U206G STATIONAIR
188 pages
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SOLOY, LLC
450 Pat Kennedy Way S.W.
Olympia, WA 98501
PILOT’S OPERATING HANDBOOK
SUPPLEMENT
AND
FAA APPROVED AIRPLANE FLIGHT MANUAL
FOR
CESSNA U206G & TU206G STATIONAIR
SERIAL NOS. U20602589, U20603522 TO U20606846
1985 SERIAL NOS. U20606847 TO U20606920
1986 SERIAL NOS. U20606921 TO U20607020
SERIAL NO.: ___________________________
REGISTRATION NO.: ____________________
This Supplement must be attached to the Pilot’s Operating Handbook (POH) when a
Soloy, LLC Turbine Pac engine is installed in accordance with S.T.C. SA2353NM.
Information contained herein supplements or supersedes the basic POH only in those
areas listed herein. For limitations, procedures and performance information not
contained in this Supplement, consult the basic POH.
F.A.A. Approved __________________________________________
Manager, Seattle Aircraft Certification Office
Date:
Publication Number: S1016A
UNCONTROLLED
COPY

Table of Contents

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Cessna U206G STATIONAIR Specifications

General IconGeneral
BrandCessna
ModelU206G STATIONAIR
CategoryAircrafts
LanguageEnglish

Summary

SECTION 1 GENERAL

INTRODUCTION

Provides an overview of the section's content and purpose.

DESCRIPTIVE DATA

Details about the aircraft's engine, propeller, fuel, and oil systems.

MAXIMUM CERTIFIED WEIGHTS

Specifies the maximum takeoff and landing weights for the aircraft.

SYMBOLS, ABBREVIATIONS AND TERMINOLOGY

Defines common terms, symbols, and abbreviations used in the manual.

ENGINE CONTROLS AND INSTRUMENTS

Describes the operation of engine controls and the function of instruments.

WEIGHT AND BALANCE TERMINOLOGY

Defines terms related to aircraft weight and balance calculations.

SECTION 2 LIMITATIONS

AIRSPEED LIMITATIONS

Defines aircraft speed restrictions for safe operation.

POWERPLANT LIMITATIONS

Lists operational restrictions for the engine and propeller systems.

ENGINE OPERATING LIMITS

Details acceptable limits for engine parameters like torque and temperature.

WEIGHT LIMITS

Specifies the maximum allowable weights for takeoff and landing.

CENTER OF GRAVITY LIMITS

Defines the forward and aft limits for the aircraft's center of gravity.

FUEL LIMITATIONS

Lists restrictions and requirements for fuel usage.

PLACARDS

Describes required aircraft placards and their locations.

SECTION 3 EMERGENCY PROCEDURES

AIRSPEEDS FOR EMERGENCY OPERATION

Lists recommended airspeeds for various emergency flight conditions.

ENGINE FAILURES

Details procedures for handling engine failures during different flight phases.

FORCED LANDINGS

Outlines procedures for making forced landings with and without engine power.

FIRES

Provides procedures for dealing with engine, electrical, cabin, and wing fires.

ICING

Details procedures for handling inadvertent encounters with icing conditions.

ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS

Describes procedures for addressing electrical system failures.

SECTION 4 NORMAL PROCEDURES

SPEEDS FOR NORMAL OPERATION

Lists recommended airspeeds for normal flight phases.

PREFLIGHT INSPECTION

Outlines the comprehensive preflight inspection checklist.

STARTING ENGINE

Describes the step-by-step engine starting sequence.

TAKEOFF

Details normal and short field takeoff procedures.

LANDINGS

Describes normal and short field landing procedures.

SECURING AIRPLANE

Outlines procedures for properly securing the aircraft after flight.

SECTION 5 PERFORMANCE

INTRODUCTION

Explains the purpose and use of performance data charts.

AIRSPEED CALIBRATION

Provides data for correcting airspeed readings under different conditions.

STALL SPEEDS

Lists stall speeds for various flap settings and bank angles.

TAKEOFF DISTANCE, SHORT FIELD 3600 LBS

Provides takeoff distance data for short field operations at 3600 lbs.

MAXIMUM RATE OF CLIMB

Lists maximum climb rates at different altitudes and weights.

CRUISE PERFORMANCE

Details cruise performance data like torque, speed, and fuel flow.

LANDING DISTANCE, SHORT FIELD 3600 LB

Provides landing distance data for short field operations at 3600 lbs.

SECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST

INTRODUCTION

Explains the purpose of weight and balance data and equipment lists.

SAMPLE WEIGHT AND BALANCE FORMS

Provides example forms for calculating aircraft weight and balance.

EQUIPMENT LIST

Lists installed aircraft equipment, including weights and arms.

SECTION 7 AIRPLANE & SYSTEMS DESCRIPTION

INSTRUMENT PANEL

Describes the layout and function of the aircraft's instrument panel.

ENGINE

Provides a description of the Soloy Turbine Pac engine and its components.

ENGINE CONTROLS

Describes the operation of the power, propeller, and fuel cutoff controls.

ENGINE INSTRUMENTS

Lists and describes the function of various engine instruments.

FUEL SYSTEM

Describes the aircraft's fuel system, including tanks and indicators.

ELECTRICAL SYSTEM

Describes the aircraft's electrical power supply system.

SECTION 8 HANDLING, SERVICE & MAINTENANCE

INTRODUCTION

Explains the purpose of the section regarding ground handling and servicing.

GROUND HANDLING

Provides procedures and cautions for ground handling the aircraft.

TIE-DOWN

Outlines procedures for properly securing the aircraft for tie-down.

ENGINE OIL

Provides information on engine oil specifications and levels.

FUEL

Details fuel types, additives, and handling procedures.

LANDING GEAR

Provides information on landing gear tire pressures and strut maintenance.

SECTION 9 SUPPLEMENTS

INTRODUCTION

Explains the purpose of the supplements section.

SOLOY SUPPLEMENT NO. 1 BLEED AIR HEATER KIT

Describes the bleed air heater kit, its installation, and operation.

SOLOY SUPPLEMENT NO. 2 ENGINE INLET ANTI-ICE KIT

Describes the engine inlet anti-ice kit and its operational procedures.

SOLOY SUPPLEMENT NO. 3 CONTINUOUS IGNITION KIT

Describes the continuous ignition kit and its safety features.

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