Page 1 450 Pat Kennedy Way S.W. Olympia, WA 98501 PILOT’S OPERATING HANDBOOK SUPPLEMENT FAA APPROVED AIRPLANE FLIGHT MANUAL CESSNA T206H/206H SERIAL NO.: ___________________________ KIT 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.
Page 2 SOLOY TURBINE PAC POHS CESSNA T206H/206H CONGRATULATIONS ..Your airplane is SPECIAL! A Soloy Corporation Turbine Pac engine has been installed for those whose operation requires extra performance and greater utility than is available with the basic engine.
Page 3 SOLOY TURBINE PAC POHS CESSNA T206H/206H LOG OF EFFECTIVE PAGES This handbook supplement will be kept current with revisions distributed to the last known owner of each airplane equipped with a Soloy Turbine Pac engine. It is the responsibility of the owner to maintain this handbook in a current status when it is being used for operational purposes.
Page 4 SOLOY TURBINE PAC POHS CESSNA T206H/206H LOG OF EFFECTIVE PAGES (Continued) Page Revision Page Revision 3-10 3-11 3-12 3-13 3-14 3-15 3-16 2-10 3-17 3-18 2-11 3-19 2-12 3-20 2-13 2-14 3-21 2-15 3-22 2-16 2-17 2-18 2-19 2-20 2-21...
Page 5 SOLOY TURBINE PAC POHS CESSNA T206H/206H LOG OF EFFECTIVE PAGES (Continued) Page Revision Page Revision 4-21 5-23 4-22 5-24 5-25 4-23 4-24 5-26 4-25 5-27 4-26 5-28 4-27 5-29 4-28 5-30 4-29 4-30 4-31 4-32 5-10 5-11 5-12 5-13 5-14...
Page 6 SOLOY TURBINE PAC POHS CESSNA T206H/206H LOG OF EFFECTIVE PAGES (Continued) Page Revision Page Revision 7-19 7-20 7-21 7-22 7-23 7-24 7-25 7-26 8-10 8-11 8-12 8-13 Deleted 8-14 Deleted NOTE: Revised text is indicated by a revision bar in the margin.
Page 7 SOLOY TURBINE PAC POHS CESSNA T206H/206H LOG OF REVISIONS Revision Pages Comments FAA Approval Revised Date 5/23/03 Original Original of Manual. Jeffery A. Morfitt for Manager, Seattle Aircraft Certification Office, ANM-100S Renton, WA 98055- 4056 Date: May 23, 2003 11/14/14 Cover Removed prev.
Page 8 SOLOY TURBINE PAC POHS CESSNA T206H/206H Revision Pages Comments FAA Approval Revised Date 11/17/15 Cover Removed prev. revision signature and date. Corrected company name. i - viii Added Rev 2. for Manager, Seattle Table of Contents Aircraft Certification moved from pg. vii Office, ANM-100S to pg.
Page 9 SOLOY TURBINE PAC POHS CESSNA T206H/206H PERFORMANCE – SPECIFICATIONS RATE OF CLIMB AT SEA LEVEL (3600 LBS) 1,447 FPM APPROVED CEILING 20,000 FT. TAKEOFF PERFORMANCE: Ground Roll 570 FT. 1,063 FT. Total Distance Over a 50’ Obstacle LANDING PERFORMANCE: Ground Roll 553 FT.
Page 10 SOLOY TURBINE PAC POHS CESSNA T206H/206H TABLE OF CONTENTS SECTION GENERAL ................1 LIMITATIONS ................2 EMERGENCY PROCEDURES ..........3 NORMAL PROCEDURES ............4 PERFORMANCE ..............5 WEIGHT & BALANCE/EQUIPMENT LIST ....... 6 AIRPLANE & SYSTEMS DESCRIPTION ........ 7 AIRPLANE HANDLING, SERVICE & MAINTENANCE .... 8 SUPPLEMENTS (Optional Systems Description &...
Page 11: Table Of Contents
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL SECTION 1 GENERAL TABLE OF CONTENTS Page Three View - Normal Ground Attitude ............ 1-3 Introduction ................... 1-4 Descriptive Data ................... 1-4 Engine ....................1-4 Propeller .................... 1-4 Fuel ....................1-4 Oil ......................
Page 12 SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL This page left blank intentionally. F.A.A. Approved May 23, 2003...
Page 13 SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL Figure 1-1. Three View F.A.A. Approved May 23, 2003...
Page 14: Introduction
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL INTRODUCTION This handbook supplement contains nine sections and includes the material required to be furnished to the pilot by FAR Part 23. It also contains supplemental data. Section I provides basic data and information of general interest. It also contains definitions or explanations of symbols, abbreviations, and terminology commonly used.
Page 15: Oil
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL Oil Specifications: See handling, service and maintenance, Section 8 Oil Capacity: 9 U.S. Quarts, including oil filter. MAXIMUM CERTIFIED WEIGHTS Ramp Weight: 3,617 lbs. Takeoff: 3,600 lbs. Landing: 3,600 lbs. Weight in Baggage Compartment – Station 109 – 145: 180 lbs. maximum...
Page 16: Symbols, Abbreviations And Terminology
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL SYMBOLS, ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY & SYMBOLS Knots Calibrated Airspeed is indicated airspeed corrected for KCAS position and instrument error and expressed in knots. Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea level.
Page 17: Meteorological Terminology
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL METEOROLOGICAL TERMINOLOGY Outside Air Temperature is the free air static temperature. It is expressed in either degrees Celsius (formerly Centigrade) or degrees Fahrenheit. STANDARD Standard Temperature is 15C at sea level pressure TEMPERATURE altitude and decreases by 2C for each 1000 feet of...
Page 18: Engine Controls And Instruments
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL ENGINE POWER TERMINOLOGY (Continued) POWER TURBINE Determined by using the propeller RPM at a ratio of SPEED (N 18.1 RPM to 1% N speed. PROPELLER RPM Indicates the speed of the propeller in revolutions per minutes.
Page 19: Airplane Performance And Flight Planning Terminology
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL ENGINE CONTROLS AND INSTRUMENTS (Continued) PROPELLER Cockpit control to set propeller RPM. CONTROL PROPELLER A propeller gearbox mounted component which provides OVERSPEED overspeed protection in the event of a propeller GOVERNOR governor failure.
Page 20: Weight And Balance Terminology
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL WEIGHT AND BALANCE TERMINOLOGY Reference Datum is an imaginary vertical plane from REFERENCE DATUM which all horizontal distances are measured for balance purposes. Station is a location along the airplane fuselage given STATION in terms of the distance from the reference datum.
Page 21: Metric / Imperial / Us Conversion Charts
SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL WEIGHT AND BALANCE TERMINOLOGY (Continued) GROSS (LOADED) Gross (Loaded) Weight is the loaded weight of the WEIGHT airplane. Maximum Takeoff Weight is the maximum weight MAXIMUM TAKEOFF WEIGHT approved for the start of the takeoff run.
Page 22 SOLOY TURBINE PAC SECTION 1 POHS CESSNA T206H/206H GENERAL This page left blank intentionally. 1-12 F.A.A. Approved May 23, 2003...
Page 23 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS SECTION 2 LIMITATIONS TABLE OF CONTENTS PAGE Introduction ..................Airspeed Limitations ................Airspeed Indicator Markings ..............Powerplant Limitations ................ Propeller Limitations ................Powerplant Instrument Markings ............Weight Limits ..................Center of Gravity Limits ...............
Page 24 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS This page left blank intentionally. F.A.A. Approved May 23, 2003...
Page 25: Introduction
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS INTRODUCTION This Supplement contains the information required to be furnished to the pilot by FAR Part 23 and must be carried in the airplane during flight operations. It also provides additional information, which will assist in operating the airplane at its maximum efficiency.
Page 26: Airspeed Indicator Markings
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS AIRSPEED INDICATOR MARKINGS Airspeed indicator markings and their color code significance are shown in Figure 2-2. MARKING KIAS SIGNIFICANCE White Arc 40 – 96 Full flap operating range. Lower limit is Narrow 40 –...
Page 27 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS CONDITION ENGINE OPERATING LIMITS Power Setting TAKEOFF 101.4 Maximum 1810 50-130 0-107 40-60 (5 Min.) Max. Cont. 1810 50-130 0-107 40-60 Acceleration 1990 Starting Figure 2-3. Engine Operating Limits. NOTES: and oil pressure limits are noted by a step in their respective arcs.
Page 28: Propeller Limitations
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS Minimum starting N speeds are: 15% above 7C (45F); 13% at -18 to +7C (0 TO 40F); and 12% below -18C (-1F). Minimum starting oil temperature; MIL-L-7808G or later, -54C (-65F); MIL-L-23699, -40C (-40F).
Page 29: Powerplant Instrument Markings
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS POWERPLANT INSTRUMENT MARKINGS POWERPLANT INSTRUMENT MARKINGS INSTRUMENT LIMIT ------ 1630 1480 1810 1990 PROPELLER 1810 1630 (4)(5) 12%- 59%- ------ 105% 106% 105% TORQUE ------ 0-78 101.4 101.4 ------ 400 - 738...
Page 30: Weight Limits
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS MISCELLANEOUS INSTRUMENT MARKINGS SUCTION ------ 4.5-5.5 ------ ----- in. Hg. AMMETER 80-150 FUEL QTY. Figure 2-5. Miscellaneous Instrument Markings. NOTES : (1) N and oil pressure limits are noted by a step in their respective arcs.
Page 31: Center Of Gravity Limits
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS CENTER OF GRAVITY LIMITS Center of Gravity Range: Forward: 33.0 inches aft of datum at 2500 lbs. or less, with straight line variation to 42.5 inches aft of datum at 3600 lbs.
Page 32: Fuel Limitations
4.0 U.S. Gallons (2.0 gallons each tank) For Model 206H from S/N 20608174 & on, usable fuel is 87 gal. For Model T206H from S/N T20608362 & on, usable fuel is 87 gal. NOTE To ensure maximum fuel capacity and minimize cross-...
Page 33: Minimum Fuel
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS MINIMUM FUEL NOTE Fuel quantity gages and fuel low lights may be inaccurate during unlevel or uncoordinated flight maneuvers. CAUTION DUE TO THE POSSIBILITY OF FUEL STARVATION, TAKEOFF OR STEEP CLIMBS AT SPEEDS BELOW...
Page 34: Cold Weather Fuel Altitude Restrictions
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS COLD WEATHER FUEL ALTITUDE RESTRICTIONS When using any cold weather fuel the maximum flight altitude is restricted to: (A) 6,000 feet with a fuel temperature of 110ºF (43.3ºC) (B) 20,000 feet with a fuel temperature of 40ºF (4.4ºC) FUEL ADDITIVE For flight at ambient temperatures of 40F and below, the fuel used...
Page 35: Oil Specifications
SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS OIL SPECIFICATIONS The 250 series engines are certified and approved for use with only certain lubricating oils that comply with MIL-PRF-7808, MIL-PRF-23699, DOD-PRF- 85734, or SAE AS5780 specifications. Refer to the Rolls-Royce M250-C20 Series Operation and Maintenance Manual for current approved oils and limitations.
Page 36: Placards
DAY – NIGHT – VFR – IFR (2) On control lock: (Cessna placard) CONTROL LOCK – REMOVE BEFORE STARTING ENGINE (3) On aft baggage wall: (Cessna placard) EMERGENCY LOCATOR TRANSMITTER INSTALLED AFT OF THIS PARTITION. MUST BE SERVICED IN ACCORDANCE WITH FAR PART 91.207...
Page 37 OFF LEVEL FLIGHT ONLY NOTE For Model 206H from S/N 20608174 & on, usable fuel is 87 gal. For Model T206H from S/N T20608362 & on, usable fuel is 87 gal. (5) Forward of fuel tank filler cap: (Soloy placard) FUEL JET A SEE PILOT’S OPERATING HANDBOOK...
Page 38 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS (7) On the flap control indicator: (Soloy placard) 0° to 10° 137 KIAS (Partial flap range with blue color code; also, mechanical detent at 10°.) 10° to 40° 96 KIAS (White color code; also mechanical detent at 20°)
Page 39 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS (10) On firewall: (Soloy placard) WARNING FAILURE TO PROPERLY INSTALL, ALIGN AND TORQUE FUEL, OIL AND AIR TUBE FITTINGS COULD RESULT IN AN ENGINE FAILURE. REFER TO APPLICABLE MANUAL FOR PROPER INSTALLATION AND TORQUE PROCEDURES.
Page 40 LIMITATIONS (14) By ELT Switch (Cessna placard) RESET (15) On left hand instrument panel: (Cessna placard) WARNING ASSURE THAT SEAT IS LOCKED IN POSITION PRIOR TO TAXI, TAKEOFF AND LANDING. FAILURE TO PROPERLY LATCH SEAT AND HEED ALL SAFETY INSTRUCTIONS CAN RESULT IN BODILY INJURY OR DEATH.
Page 41 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS (17) On left hand instrument panel: (Cessna placard) WARNING ASSURE THAT ALL CONTAMINANTS, INCLUDING WATER, ARE REMOVED FROM FUEL AND FUEL SYSTEM BEFORE FLIGHT. FAILURE TO ASSURE CONTAMINANT FREE FUEL AND HEED ALL...
Page 42 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS (20) On forward cargo door: (Cessna placard) EMERGENCY EXIT OPERATION 1. ROTATE FORWARD CARGO DOOR HANDLE FULLFORWARD THEN FULL AFT. 2. OPEN FORWARD CARGO DOOR AS FAR POSSIBLE. 3. ROTATE RED LEVER IN REAR CARGO DOOR FORWARD.
Page 43 DO NOT TAKEOFF OR CLIMB BELOW V IF EITHER LOW FUEL INDICATOR LIGHTS ARE ILLUMINATED. (25) On each fuel tank filler cap: (Soloy placard) (26) On the upper right instrument panel: (Cessna placard) SMOKING PROHIBITED 2-21 F.A.A. Approved May 23, 2003...
Page 44 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS (27) On air oil shock strut: (Cessna placard) CESSNA AIR OIL SHOCK STRUT CESSNA AIRCRAFT COMPANY, WICHITA, KANSAS FILLING INSTRUCTIONS REMOVE VALVE CAP AND RELEASE ALL AIR. REMOVE VALVE HOUSING ASSEMBLY.
Page 45 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS (29) On forward pilot door: (Cessna placard) CLOSE OPEN LOCK (30) On seats: (Cessna placard) DO NOT INSTALL SEAT FACING AFT THIS SEAT IS CERTIFIED FOR FORWARD FACING ONLY. (31) By oxygen fill port: (Cessna placard)
Page 46 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS (34) On radio panel: (Cessna placard) N3754C SAMPLE NUMBER SHOWN (35) On control wheels: (Cessna placard) MAP LIGHT DIM ON PILOT CONTROL WHEEL (36) On control wheels: (Cessna placard) MAP LIGHT DIM...
Page 47 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS (40) On the oil filler cap: (Soloy placard) 2-25 F.A.A. Approved May 23, 2003...
Page 48 SOLOY TURBINE PAC SECTION 2 POHS CESSNA T206H/206H LIMITATIONS This page left blank intentionally. 2-26 F.A.A. Approved May 23, 2003...
Page 49 SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS PAGE Introduction ................3-3 AIRSPEEDS Airspeeds For Emergency Operation ........3-3 EMERGENCY PROCEDURES CHECKLIST Engine Failures ................ 3-3 Engine Failure During Takeoff Run ........3-3 Engine Failure Immediately After Takeoff ......
Page 50 SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES (Continued) ......... PAGE TABLE OF CONTENTS AMPLIFIED PROCEDURES Engine Failure ..............3-14 Maximum Glide, Chart 3.1 ..........3-15 Forced Landings ..............3-16 Landing Without Elevator Control ..........3-16 Fires ……………………………………………………………….. 3-16 Emergency Operation In Clouds ..........
Page 51: Introduction
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES INTRODUCTION Section 3 provides checklist and amplified procedures for coping with emergencies that may occur. Emergencies caused by airplane or engine malfunctions are extremely rare if proper preflight inspections and maintenance are practiced.
Page 52: Engine Failure Immediately After Takeoff
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF Airspeed – 80 KIAS Propeller Control – FEATHER (OUT) Fuel Cutoff Control – CUTOFF (OUT) Fuel Selector Valve – OFF (PRESS DOWN SAFETY SPRING TO ALLOW MOVEMENT TO OFF) Wing Flaps –...
Page 53: Forced Landings
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES NOTE As the propeller comes out of feather, there will be an oscillation of power until the propeller RPM stabilizes. 15. Apply power as required. WARNING DUE TO THERMAL CHANGES WITHIN...
Page 54: Ditching
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES Wing Flaps -- 20 Selected Field – FLY OVER NOTING TERRAIN & OBSTRUCTIONS Radio and Electrical Switches – OFF Wing Flaps -- 40 (recommended on final approach) Power control – As Required (FLIGHT IDLE minimum 14 psi torque) 10.
Page 55: Fires
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES FIRES DURING START ON GROUND CAUTION AN ENGINE FIRE (WITH THE RESULTANT FLAME EMANATING FROM THE TAILPIPE) CAN OCCUR DURING START IF THE COMBUSTION CHAMBER BECOMES OVER-LOADED WITH FUEL BEFORE IGNITION TAKES PLACE.
Page 56: Engine Fire In Flight
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES ENGINE FIRE IN-FLIGHT Fuel Cutoff Control – CUTOFF (OUT) Propeller Control – FEATHER (OUT) Fuel Selector – OFF Battery and Generator – OFF (except IFR) Cabin Heat and Air – OFF (except overhead vent) Airspeed –...
Page 57: Wing Fire
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES Fire Extinguisher – ACTIVATE (if available) WARNING AFTER THE FIRE IS EXTINGUISHED, IF AN OXYGEN SYSTEM IS AVAILABLE, OCCUPANTS SHOULD USE OXYGEN MASKS UNTIL SMOKE AND DISCHARGED DRY POWDER CLEARS.
Page 58 SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES These systems must be operated in the above mentioned conditions even if there is no visible sign of airframe ice and/or snow accumulation. Deactivation of the systems shall not be...
Page 59: Alternate Air Operation
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES 11. Missed approaches should be avoided whenever possible because of severely reduced climb capability. However, if a go- around is mandatory, make the decision much earlier in the approach than normal. Apply maximum power and maintain 95 KIAS while retracting the flaps slowly in 10°...
Page 60: Static Source Blockage (Erroneous Instrument Reading Suspected)
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES ALTERNATE AIR LIGHT ILLUMINATES IN FLIGHT: Check that the alternate air control is in the NORM position. Visually check that the ram inlet doors are raised and check for reverse operation.
Page 61: Electrical Power Supply System Malfunctions
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS AMMETER SHOWS DISCHARGE (Indicated by the GEN OFF BUS Warning Light and ammeter shows no amps.) Trip and reset the generator trip reset switch. If light remains on: Generator Switch –...
Page 62: Amplified Procedures
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES AMPLIFIED PROCEDURES ENGINE FAILURE If an engine failure occurs during the takeoff run, the most important thing to do is stop the airplane on the remaining runway. Those extra items on the checklist will provide added safety after a failure of this type.
Page 63 SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES FEATHERED PROPELLER FLAPS UP ZERO WIND BEST GLIDE SPEED WEIGHT (LBS) KIAS 3600 3200 2800 HEIGHT ABOVE TERRAIN IN FEET Figure 3-1, Maximum Glide. 3-15 F.A.A. Approved May 23, 2003...
Page 64: Forced Landings
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES FORCED LANDINGS If all attempts to restart the engine fail and a forced landing is imminent, select a suitable field and prepare for the landing as discussed under the Emergency Landing Without Engine Power checklist (See page 3-5).
Page 65: Emergency Operation In Clouds
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES EMERGENCY OPERATION IN CLOUDS VACUUM SYSTEM FAILURE In the event of a total vacuum system failure, loss of both vacuum pumps during flight, the directional indicator and attitude indicator will be disabled, and the pilot will have to rely on the turn coordinator or the turn and bank indicator if he inadvertently flies into clouds.
Page 66: Recover From A Spiral Dive
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES Before descending into the clouds, set up a stabilized let-down condition as follows: Reduce power to set up a 500 to 800 ft./min. rate of descent. Adjust the elevator and rudder trim control wheels for a stabilized descent at 95 KIAS.
Page 67: Alternate Air Light Does Not Illuminate
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES ALTERNATE AIR LIGHT DOES NOT ILLUMINATE Press to test the alternate air door light to check for a bad circuit. Then visually check that the ram inlet doors are in the ALT position (Raised).
Page 68: Rough Engine Operation Or Loss Of Power
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES NOTE If disorientation precludes a visual determination of the direction of rotation, the symbolic airplane in the turn coordinator or the needle of the turn and bank indicator may be referred to for this information.
Page 69: Oil Chip Detector
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES OIL CHIP DETECTOR The Oil Chip Detector light on the instrument panel illuminates to indicate possible internal deterioration of the engine or the propeller reduction gearbox (there are three chip detectors in the oil system). Land as soon as practicable if the light illuminates in flight.
Page 70: Insufficient Generator Output
SOLOY TURBINE PAC SECTION 3 POHS CESSNA T206H/206H EMERGENCY PROCEDURES INSUFFICIENT GENERATOR OUTPUT If the ammeter and VOLTS annunciator light indicate the generator is not supplying power to the system, it should be shut down. Circuit breakers should be checked and reset as required, the generator reset switch should be pressed and the generator restored.
Page 71 SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS PAGE Introduction .................. 4-3 Airspeeds for Normal Operation ............. 4-3 CHECKLIST PROCEDURES Preflight Inspection ..............4-4 Cabin ..................4-4 Empennage ................4-5 Right Wing, Trailing Edge ............4-5 Right Wing ................
Page 72 SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES AMPLIFIED PROCEDURES Preflight Inspection ..............4-15 Before Starting The Engine ............4-16 Starting Engine ................4-17 Taxiing ..................4-19 Before Takeoff ................4-20 Landing Lights ................4-21 Takeoff ..................4-21 Wing Flap Settings ..............
Page 73: Introduction
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES INTRODUCTION Section 4 provides checklist and amplified procedures for the conduct of normal operation. Normal procedures associated with optional systems can be found in Section 9. AIRSPEEDS FOR NORMAL OPERATION Unless otherwise noted, the following speeds are based on a maximum weight of 3600 pound and may be used for any lesser weight.
Page 74: Checklist Procedures
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES CHECKLIST PROCEDURES PREFLIGHT INSPECTION CABIN Pitot Tube cover -- REMOVE. Check for pitot blockage. Pilot's Operating Handbook and Soloy POH Supplement -- AVAILABLE IN THE AIRPLANE. Airplane Weight and Balance – CHECKED.
Page 75: Empennage
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES EMPENNAGE Rudder Gust Lock – REMOVE Tail Tie-Down – DISCONNECT Control Surfaces – CHECK freedom of movement and security. Trim Tab – CHECK Security Check cargo doors securely latched and locked (right side only).
Page 76: Nose
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES Fuel Tank Sump Quick Drain Valves -- DRAIN at least a cupful of fuel (using sampler cup) from each sump location to check for water, sediment, and proper fuel grade before each flight and after each refueling.
Page 77: Left Wing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES Landing and Taxi Lights – CHECK for condition and clean lenses 10. Nose Wheel Strut and Tire – CHECK for proper inflation 11. Optional Engine Oil Screen, Impending Filter bypass Indicator –...
Page 78: Before Starting Engine
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES BEFORE STARTING ENGINE Preflight Inspection – COMPLETE Passenger briefing - COMPLETE Cabin Doors and Windows – CLOSE and LOCK Seats, Belts, Shoulder Harnesses – ADJUST and LOCK. Ensure inertial wheel locking.
Page 79: Starting Engine (With External Power)
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES TOT and N – MONITOR TOT (810 to 927C), 10 seconds maximum and N for normal acceleration. Propeller (N ) – CHECK rotating by 25% N Transmission Oil Pressure – POSITIVE indication at completion of the start.
Page 80: Aborted Start Procedure
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES ABORTED START PROCEDURE Fuel Cutoff Control – CUTOFF (OUT) Start Motor Switch – MOTOR 10 to 30 seconds TOT – MONITOR Perform corrective maintenance action if required. BEFORE TAXIING Windows, vents and heater -- ADJUST as desired.
Page 81: Takeoff
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES 21. Wing Flaps – SET for take-off ( 0º TO 20º) 22. Ice Protection ( Alternate Air, Inlet Anti-ice)– AS REQUIRED 23. Annunciator Panel – CLEAR except alternate air, if in use.
Page 82: Enroute Climb
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES ENROUTE CLIMB NORMAL CLIMB Airspeed – 100 – 120 KIAS Ice Protection – AS REQUIRED Power Control – 78 PSI Torque or 738C TOT and 1810 propeller RPM Fuel Selector Valve - BOTH MAXIMUM PERFORMANCE CLIMB (V Airspeed –...
Page 83: Before Landing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES BEFORE LANDING Ice Protection – AS REQUIRED CAUTION SIGNIFICANT POWER LOSS WILL OCCUR WHILE OPERATING IN THE ALTERNATE AIR MODE. EXTREME CAUTION SHOULD BE USED TO MAINTAIN A MINIMUM OF 14 PSI TORQUE IN FLIGHT ON APPROACH TO LANDING.
Page 84: Balked Landing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES BALKED LANDING Power Control – ADVANCE for TAKEOFF POWER (101.4 PSI torque or 810C TOT limits). Airspeed – 60 KIAS Wing Flaps – RETRACT to 20 Airspeed – 70 – 80 KIAS after all obstacles are cleared.
Page 85: Amplified Procedures
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES AMPLIFIED PROCEDURES PREFLIGHT INSPECTION The preflight inspection, described in the abbreviated procedures part of this section, is recommended before flight. Baggage should be weighed, stowed, and tied down. The preflight should include a determination of the airplane’s operational status, a check that the necessary papers are on...
Page 86: Before Starting The Engine
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES To prevent loss of fuel in flight and to ensure equal flow, make sure the fuel tank filler caps are tightly sealed. The fuel tank vents on the lower surface of the tanks should also be inspected for obstructions.
Page 87: Starting Engine
Prior to starting the engine, make sure the propeller area is clear. Proper fuel and ignition management are the determining factors in obtaining a normal start of your Turbine Pac equipped Cessna. NOTE For the ultimate safety of all personnel who operate...
Page 88 SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES After advancing the fuel control cutoff, a delay of lightoff can occur under certain conditions. If this delay exceeds 3 seconds, return the fuel cutoff control to the CUTOFF (OUT) position to abort the start, but motor the engine for 10 seconds to clear the combustion chamber of residual fuel.
Page 89: Taxiing
OAT of 5C (41F) and below and anti-ice plus alternate air are required in visible moisture and an OAT of 1 C (34C) and below or while operating in falling or blowing snow. Refer to Figure 4-2 (Page 4-22) in the Cessna Pilot’s Operating Handbook for additional taxiing instructions. BEFORE TAKEOFF...
Page 90 SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES Prior to engine run-up, set parking brake ON. Check that all doors and windows are closed and that the passenger’s seat belts and shoulder harnesses are secure. Check fuel quantity and temperature. Refer to limitations section for restrictions.
Page 91: Landing Lights
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES NOTE The engine inlet anti-ice must be activated for flight or ground operation in visible moisture at an OAT of 5C (41F) and below (without alternate air on) or 1C (34C) and below (with alternate air on) and while operating in falling or blowing snow.
Page 92: Wing Flap Settings
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES LIMIT TIME LIMIT Up to 1810 RPM No Limit 1810 to 1990 RPM 15 Seconds Over 1990 RPM Not Allowed Maintain torque and TOT within limits. As the airplane accelerates, an increase in torque and TOT at a fixed power control position is normal.
Page 93: Enroute Climb
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES ENROUTE CLIMB Normally, maximum continuous power and a climb speed of 100 – 120 KIAS is maintained to cruise altitude. At lower altitudes, the torque limit of 78 PSI will be set until the TOT limit of 738C dictates the power available.
Page 94: Flight In Icing Conditions
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES FLIGHT IN ICING CONDITIONS Flight into icing conditions is prohibited. An inadvertent encounter with these conditions can best be handled using the checklist procedures in Section 3. The best procedure, of course, is to turn back or change altitude to escape icing conditions.
Page 95: Landings
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES LANDINGS NORMAL LANDING Landing should be made on the main wheels first to reduce the landing speed and subsequent need for braking in the landing roll. The power control can be moved to the GROUND IDLE position when the wheels have made firm contact with the runway surface.
Page 96: Balked Landing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES BALKED LANDING In a balked landing (go-around) climb, apply power as required and maintain torque and TOT within allowable limits. The flap setting should be reduced to 20. After all obstacles are cleared and a safe altitude and airspeed are obtained, the wing flaps should be retracted.
Page 97: Cold Weather Operation
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES When the airplane is not stored in a hangar, the air inlet should be covered to protect the induction system from birds and debris. Install the control locks, propeller bungee and exhaust covers.
Page 98: Hot Weather Operation
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES With a cold soaked engine, N may accelerate slowly through the 25-30% speed range. If the start is not completed within the time limits, abort the start and allow one minute for the heat to soak back into the engine and battery for the restart.
Page 99: Noise Abatement
SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES NOISE ABATEMENT Increased emphasis on improving the quality of our environment requires renewed effort on the part of all pilots to minimize the effect of airplane noise on the public.
Page 100 SOLOY TURBINE PAC SECTION 4 POHS CESSNA T206H/206H NORMAL PROCEDURES This page left blank intentionally. 4-30 F.A.A. Approved May 23, 2003...
Page 101 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE SECTION 5 PERFORMANCE TABLE OF CONTENTS ............ PAGE Introduction ................. 5-3 Figure 5-1: Airspeed Calibration ..........5-4 Figure 5-2: Temperature Conversion Chart ....... 5-5 Figure 5-3: Stall Speeds ............5-6 Figure 5-4: Minimum Engine Torque For Takeoff ......
Page 102 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE TABLE OF CONTENTS (Continued) PAGE Figure 5-11: Cruise Performance – Sea Level and 2,000 Feet ..5-20 Cruise Performance – 4,000 and 6,000 Feet ..... 5-21 Cruise Performance – 8,000 and 10,000 Feet ... 5-22 Cruise Performance –...
Page 103: Introduction
SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE INTRODUCTION Performance data charts on the following pages are presented so that you may know what to expect from the airplane under various conditions, and also, to facilitate the planning of flights in detail and with reasonable accuracy.
Page 104: Airspeed Calibration
SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE AIRSPEED CALIBRATION NORMAL STATIC SOURCE FLAPS UP KIAS KCAS FLAPS 20 KIAS KCAS FLAPS 40 KIAS KCAS ALTERNATE STATIC SOURCE VENTS AND WINDOWS CLOSED FLAPS UP KIAS KCAS FLAPS 20 KIAS KCAS FLAPS 40...
Page 105: Temperature Conversion Chart
SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE DEGREES CELSIUS Figure 5-2. Temperature Conversion Chart F.A.A. Approved May 23, 2003...
Page 106: Stall Speeds
SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE STALL SPEEDS CONDITIONS: Power Flight Idle NOTES: Maximum altitude loss during a stall recovery may be as much as 240 feet. KIAS values are approximate. Standard day. MOST REARWARD CENTER OF GRAVITY ANGLE OF BANK 0...
Page 107 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE MOST FORWARD CENTER OF GRAVITY ANGLE OF BANK 0 30 45 60 3600 0 3600 20 3600 40 Figure 5-3. Stall Speeds (Sheet 2 of 2) F.A.A. Approved May 23, 2003...
Page 108 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE MINIMUM ENGINE TORQUE FOR TAKEOFF CONDITIONS: Power – TAKEOFF Propeller – 1810 RPM Engine Air Induction System – NORM NOTES: The torque indicated below is the minimum value for which takeoff performance in this section can be obtained.
Page 109 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE F.A.A. Approved May 23, 2003...
Page 110 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE F.A.A. Approved 5-10 May 23, 2003...
Page 111 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE F.A.A. Approved 5-11 May 23, 2003...
Page 112 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE May 23, 2003 F.A.A. Approved 5-12...
Page 113 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE May 23, 2003 F.A.A. Approved 5-13...
Page 114 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE May 23, 2003 F.A.A. Approved 5-14...
Page 115 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE MAXIMUM RATE OF CLIMB CONDITIONS: Flaps Up 1810 RPM Maximum Continuous Power, 78 PSI or 738C TOT Inlet – Normal WEIGHT PRESS ALT CLIMB RATE OF CLIMB - FPM POUNDS FEET SPEED KIAS STD20C...
Page 116 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE MAXIMUM RATE OF CLIMB CONDITIONS: Flaps Up 1810 RPM Takeoff Power 101.4 PSI or 810C TOT Inlet – Normal PRESS CLIMB WEIGHT SPEED RATE OF CLIMB - FPM POUNDS FEET KIAS STD20C...
Page 117: Temperature - Standard
SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE TIME, FUEL AND DISTANCE TO CLIMB MAXIMUM RATE OF CLIMB CONDITIONS: NOTES: Flaps Up Add 20 lbs (3 gal.) of fuel for 1810 RPM engine start, taxi & takeoff. Maximum Continuous Power, 78 Distances shown are based on PSI or 738°C...
Page 118: Temperature - Standard +20°C
SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE TIME, FUEL AND DISTANCE TO CLIMB MAXIMUM RATE OF CLIMB CONDITIONS: NOTES: Flaps Up Add 20 lbs (3 gal.) of fuel for 1810 RPM engine start, taxi & takeoff. Maximum Continuous Power, 78 Distances shown are based on PSI or 738°C...
Page 119: Temperature - Standard -20°C
SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE TIME, FUEL AND DISTANCE TO CLIMB MAXIMUM RATE OF CLIMB CONDITIONS: NOTES: Flaps Up Add 20 lbs (3 gal.) of fuel for 1810 RPM engine start, taxi & takeoff. Maximum Continuous Power, 78 Distances shown are based on PSI or 738°C...
Page 120 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE CRUISE PERFORMANCE CONDITIONS: 3600 Pounds 1810 RPM Inlet – Normal PRESSURE ALTITUDE – SEA LEVEL STD -20C STD +20C (15C) (-5C) (35C) PRESSURE ALTITUDE – 2,000 STD -20C STD +20C (11C) (-9C)
Page 121 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE CRUISE PERFORMANCE CONDITIONS: 3600 Pounds 1810 RPM Inlet – Normal PRESSURE ALTITUDE – 4,000 STD -20C STD +20C (7C) (-13C) (27C) PRESSURE ALTITUDE – 6,000 STD -20C STD +20C (3C) (-17C) (23C)
Page 122 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE CRUISE PERFORMANCE CONDITIONS: 3600 Pounds 1810 RPM Inlet – Normal PRESSURE ALTITUDE – 8,000 STD -20C STD +20C (-1C) (-21C) (19C) PRESSURE ALTITUDE – 10,000 STD -20C STD +20C (-5C) (-25C) (15C)
Page 123 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE CRUISE PERFORMANCE CONDITIONS: 3600 Pounds 1810 RPM Inlet – Normal PRESSURE ALTITUDE – 12,000 STD -20C STD +20C (-9C) (-29C) (11C) PRESSURE ALTITUDE – 14,000 STD –20C STD +20C (-13C) (-33C) (7C)
Page 124 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE CRUISE PERFORMANCE CONDITIONS: 3600 Pounds 1810 RPM Inlet – Normal PRESSURE ALTITUDE – 16,000 STD -20C STD +20C (-17C) (-37C) (3C) PRESSURE ALTITUDE – 18,000 STD -20C STD +20C (-21C) (-41C) (-1C)
Page 125 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE CRUISE PERFORMANCE CONDITIONS: 3600 Pounds 1810 RPM Inlet – Normal PRESSURE ALTITUDE – 20,000 STD –20C STD +20C (-25C) (-45C) (-5C) Figure 5-11. Cruise Performance (Sheet 6 of 6) 5-25 F.A.A. Approved...
Page 126 45 Minute Reserve 88/87 Gallons Usable Fuel NOTE For Model 206H from S/N 20608174 & on, usable fuel is 87 gal. For Model T206H from S/N T20608362 & on, usable fuel is 87 gal. CONDITIONS: NOTE: 1810 RPM 100% N...
Page 127 45 Minute Reserve 88/87 Gallons Usable Fuel NOTE For Model 206H from S/N 20608174 & on, usable fuel is 87 gal. For Model T206H from S/N T20608362 & on, usable fuel is 87 gal. CONDITIONS: NOTE: 1810 RPM 100% N...
Page 128 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE F.A.A. Approved 5-28 May 23, 2003...
Page 129 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE May 23, 2003 F.A.A. Approved 5-29...
Page 130 SOLOY TURBINE PAC SECTION 5 POHS CESSNA T206H/206H PERFORMANCE This page intentionally left blank. 5-30 F.A.A. Approved May 23, 2003...
Page 131 SOLOY TURBINE PAC SECTION 6 POHS CESSNA T206H/206H WEIGHT & BALANCE/ EQUIPMENT LIST SECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST TABLE OF CONTENTS PAGE Introduction .................. 6-3 Airplane Weighing Procedures............6-3 Weight and Balance ..............6-3 Sample Loading Problem .............. 6-4 Loading Graph ................
Page 132 SOLOY TURBINE PAC SECTION 6 POHS CESSNA T206H/206H WEIGHT & BALANCE/ EQUIPMENT LIST This page left blank intentionally F.A.A. Approved May 23, 2003...
Page 133: Introduction
6.7 lbs./gal. Loading Arrangements (Figures 6-3, 6-4, 6-5 and 6-6) -- No Change NOTE Cessna Cargo Pod not approved for use with turbine powered Cessna 206. Sample Loading Problem – See Figure 6-7 See Loading Graph – See Figure 6-8 Center of Gravity Moment Envelope (Figure 6-9) –...
Page 134 SOLOY TURBINE PAC SECTION 6 POHS CESSNA T206H/206H WEIGHT & BALANCE/ EQUIPMENT LIST SAMPLE SAMPLE AIRPLANE YOUR AIRPLANE LOADING PROBLEM WEIGHT MOMENT WEIGHT MOMENT (LBS.) (LB.-INS. (LBS.) (LB.-INS. /1,000) /1,000) Basic empty weight (includes unusable fuel 2019 76.4 and full oil) Usable fuel (at 6.7...
Page 135: Loading Graph
SOLOY TURBINE PAC SECTION 6 POHS CESSNA T206H/206H WEIGHT & BALANCE/ EQUIPMENT LIST NOTE: Lines representing adjustable seats show the pilot or passenger center of gravity on adjustable seats positioned for an average occupant. Refer to Loading Arrangements diagram for forward and aft limits of occupant C.G. range.
Page 136: Comprehensive Equipment List
SOLOY TURBINE PAC SECTION 6 POHS CESSNA T206H/206H WEIGHT & BALANCE/ EQUIPMENT LIST –Add the Following COMPREHENSIVE EQUIPMENT LIST Changes: The equipment list description has been revised to delete certain Code R equipment and to install items as necessary for this modification.
Page 137 SOLOY TURBINE PAC SECTION 6 POHS CESSNA T206H/206H WEIGHT & BALANCE/ EQUIPMENT LIST 71 – Powerplant -27.0 71-01-R Filter, Induction Air 72 – Engines -17.5 72-01-R Engine, Lycoming TIO-540 509.0 -17.5 Engine, Lycoming TIO 540 72-02-R 73 – Engine Fuel & Control...
Page 138 SOLOY TURBINE PAC SECTION 6 POHS CESSNA T206H/206H WEIGHT & BALANCE/ EQUIPMENT LIST 30 – Ice & Rain Protection Electric Heated Boots, 30-01-O Propeller, (Anti-Ice 33 - Lights -44.0 33-07-A Cowl Landing Lights 34 – Navigation 34-01-R Indicator, Airspeed, Knots 16.9...
Page 139 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION SECTION 7 AIRPLANE & SYSTEMS DESCRIPTIONS TABLE OF CONTENTS ..............PAGE Introduction ..................7-3 Airframe .................... 7-3 Flight Controls .................. 7-3 Trim Systems ................7-3 Instrument Panel ................7-3 Pilot Panel Layout ..............
Page 140 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION TABLE OF CONTENTS (Continued) ........... PAGE Fuel System .................. 7-14 Fuel Distribution ..............7-14 Fuel Indicating System ............7-14 Fuel Flow Instrument Operating Details ........7-14 Limitations ................7-14 Auxiliary Fuel Pump Operation ..........
Page 141: Introduction
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION INTRODUCTION This section provides description and operation of the airplane and its systems. Some equipment described herein is optional and may not be installed in the airplane. Refer to Section 9, Supplements, for details of other optional systems and equipment.
Page 142 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION Transmission Oil Pressure Propeller Controls Suction Gage Power Control Fuel Quantity Rudder Trim Ammeter Engine Alternate Air Control Digital Clock and O.A.T. Alternate Static Air Control Fuel Flow and Temperature...
Page 143 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION FIGURE 7-1. INSTRUMENT PANEL (Sheet 2 of 2) F.A.A. Approved May 23, 2003...
Page 144: Center Panel Layout
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION CENTER PANEL LAYOUT The center panel contains the various avionics equipment arranged in a vertical rack. This arrangement allows each component to be removed without having to access the backside of the panel.
Page 145 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION Inlet air enters the engine through a plenum chamber formed around the compressor inlet bellmouth where it is directed to the compressor. The compressor consists of six axial compressor stages and one centrifugal stage, assembled as an integral unit.
Page 146: Engine Controls
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION ENGINE CONTROLS The propulsion system is operated by a set of three controls. They consist of the power control, propeller control, and fuel cutoff control. POWER CONTROL The power control in the cockpit is connected to the gas producer fuel control unit on the engine.
Page 147: Propeller Rpm Indicator
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION counterbalanced by oil from the lubrication system. The cylinder oil pressure is quoted to an external connection for use with a torque indicator that is calibrated in PSI of torque.
Page 148: New Engine Break-In And Operation
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION NEW ENGINE BREAK-IN AND OPERATION There are no specific break-in procedures required for the SOLOY TURBINE PAC turboprop engine. The engine may be safely operated through the normal ranges authorized by the manufacturer at the time of delivery of your airplane.
Page 149: Air Induction System
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION AIR INDUCTION SYSTEM The engine air induction system receives ram air through the engine air intakes located on the top of the cowling. The air is then routed to a plenum chamber where the compressor inlet bellmouth is located.
Page 150: Exhaust System
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION NOTE A drop in torque and a rise in TOT is normal with the actuation of the engine ice protection system. CAUTION SIGNIFICANT POWER LOSS WILL OCCUR WHILE OPERATING IN THE ALTERNATE AIR MODE.
Page 151 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION An auto feathering system provides for automatic reduction in propeller RPM in the event of the loss of engine power. This system is not a total feathering device. It is intended to reduce propeller drag due to an engine failure.
Page 152: Fuel System
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION FUEL SYSTEM The fuel system, see Figure 7-2, consists of left and right vented fuel tanks, two fuel reservoir tanks, a fuel selector valve, airframe mounted fuel filter, engine driven fuel pump, fuel system quantity and flow instrumentation.
Page 153 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION To determine the fuel used or fuel remaining, multiply the reading by the following factors. Fuel Used Multiplier Jet A, JP-5 1.02 Jet B, JP-4, or AVGAS/ PROCEDURES...
Page 154 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION available by pressing the appropriate buttons. Tanks Full Move the ADD/FULL toggle switch to the FULL position and hold. The maximum usable fuel figure will be displayed in the upper window.
Page 155: Auxiliary Fuel Pump Operation
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION Emergency A. In case of an electrical power failure in flight, the instrument will cease to function. After restoring the power, the lower window will resume accurate fuel flow reading, but the Time Remaining, Lb.
Page 156 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION Figure 7-2. Fuel System 7-18 F.A.A. Approved May 23, 2003...
Page 157: Fuel Return System
VOLTAGE FROM DAMAGING THE AVIONICS EQUIPMENT. ANNUNCIATOR PANELS In addition to the existing Cessna annunciator panel there is the turbine installation related annunciator panel located on the right hand instrument panel. Both panels provide caution (amber) and warning (red) messages for selected portions of the airframe systems.
Page 158 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION Inputs to the annunciator come from each fuel transmitter, low engine oil pressure switch, the vacuum pressure switches and the low voltage sensor. Highly reliable individual LED bulbs illuminate each message.
Page 159 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION The annunciator panel can be tested by turning the Battery Switch on and holding the annunciator panel switch in the TST position. All indicator messages will illuminate when the test switch is activated and until the switch is released.
Page 160 SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION Figure 7-4. Electrical Schematic 7-22 F.A.A. Approved May 23, 2003...
Page 161: Master Switch
LOW VOLTAGE ANNUNCIATION A low voltage warning annunciator is incorporated into the original Cessna annunciator panel and activates any time voltage falls below 25 volts. If low voltage is detected, the red annunciator VOLTS will flash for approximately 10 seconds before illuminating steadily.
Page 162: Circuit Breakers And Fuses
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION is off line. The generator may be reset by cycling the generator switch to the off position and back on. If the annunciator extinguishes, normal generator charging has resumed; however, if the annunciator illuminates again, a malfunction has occurred and the flight should be terminated as soon as practical.
Page 163: Lighting Systems
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION NOTE Before connecting an external power source confirm that the battery and avionics switches are in the off position. – No Change LIGHTING SYSTEMS CABIN HEATING, VENTILATING AND DEFROSTING –...
Page 164: Low Vacuum Annunciation
SOLOY TURBINE PAC SECTION 7 POHS CESSNA T206H/206H AIRPLANE & SYSTEMS DESCRIPTION feet, the desired vacuum is 4.5 to 5.5 inches of mercury. A vacuum reading out of this range at altitudes below 15,000 feet may indicate a system malfunction or improper adjustment, and in this case, the indicators should not be considered reliable.
Page 165 AIRPLANE HANDLING, SERVICE & MAINTENANCE TABLE OF CONTENTS PAGE Introduction ................... 8-3 Identification Plate ................ 8-3 Cessna Owner Advisories ............. 8-3 Publications ................8-3 Airplane File ................. 8-4 Airplane Inspection Periods ............8-4 Pilot Conducted Preventive Maintenance ........8-4 Alterations or Repairs ..............8-4 Ground Handling ................
Page 166 SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE This page left blank intentionally. F.A.A. Approved November 14, 2014...
Page 167: Introduction
– Add the Following Changes: IDENTIFICATION PLATE Adjacent to the basic Cessna identification plates can be found the SOLOY TURBINE PAC identification plate which contains the model number, serial number, supplemental type certificate (STC) and the date of the aircraft conversion.
Page 168: Airplane File
SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE -- No Change AIRPLANE FILE – No Change AIRPLANE INSPECTION PERIODS – PILOT CONDUCTED PREVENTIVE MAINTENANCE No Change – No Change ALTERATIONS OR REPAIRS GROUND HANDLING TOWING – Add the Following Changes:...
Page 169: Flyable Storage
SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE Install a surface control lock over the fin and rudder. Tie sufficiently strong ropes or chains to the wing and tail tie- down fittings and secure each rope or chain to a ramp tie- down.
Page 170: Servicing
SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE Accomplish fuel system preservation. If the engine will be stored for over 45 days, re-preserve at least each 90 days if stored and each 180 days if stored indoors.
Page 171: Oil Drain Period
SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE WARNING ALTHOUGH MIL-PRF-23699, AS5780, DOD-PRF-85734 OR MIL-PRF-7808G OIL IS ACCEPTABLE, DO NOT MIX THESE OILS. ONLY DISCRETIONARY MIXING OF OILS IS PERMITTED WITHOUT A TIME PENALTY. USE OF MIXED OILS FROM DIFFERENT SERIES IN...
Page 172: Oil Level Check
SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE CAUTION USE OF OILS THAT ARE NOT INCLUDED IN THE APPROVED OILS LISTING, OR FAILURE TO DRAIN OIL WITHIN THE PRESCRIBED INTERVAL WILL BE CONSIDERED AS MISUSE UNDER THE WARRANTY POLICY.
Page 173: Fuel Additives
SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE FUEL ADDITIVES For flight at ambient temperatures of 40F and below, the fuel used in this aircraft MUST have an anti-icing additive in compliance with MIL-L-27686D or E or Phillips PF A55MB, incorporated or added into the fuel during refueling in accordance with the additive manufacturer's instructions.
Page 174 SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE In order to obtain a lightoff when cold weather fuel is used, it may be necessary to: Preheat the engine, or Bleed the fuel system. Preheat the engine in the area of the fuel control.
Page 175: Oxygen Filling Pressures
SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE NOTE Anti-ice additive is needed for the jet fuel-AVGAS mixture. NOTE Prolonged and uninterrupted operation with only AVGAS mixture will induce lead buildup on turbine parts. This lead buildup can cause a gradual power reduction;...
Page 176: Cleaning And Care
SOLOY TURBINE PAC SECTION 8 POHS CESSNA T206H/206H HANDLING, SERVICE & MAINTENANCE CLEANING AND CARE WINDSHIELD-WINDOWS – No Change PAINTED SURFACES – No Change PROPELLER CARE – No Change ENGINE CARE The cleaning practices that are necessary for proper maintenance of the engine compressor are as follows: Water Rinse.
Page 177 SUPPLEMENTS SECTION 9 LOG OF APPROVED SUPPLEMENTS The following is a list of supplements from the Cessna Pilot Operating Handbook and FAA Approved Airplane Flight Manual and their status as when applied to the Turbine Cessna 206 airplane. Appropriate flight tests will be conducted to determine compatibility of those not listed as the need arises.
Page 178 SOLOY TURBINE PAC SECTION 9 POHS CESSNA T206H/206H SUPPLEMENTS Reserved No Change Bendix/King KAP 140 2 Axis Autopilot No Change with Altitude Preselect Cargo Pack Not Approved Propeller De-Ice Not Approved Century Horizontal Situation No Change Indicator (HIS) Bendix/King KLN 94 Global...
Page 179 SOLOY TURBINE PAC SECTION 9 POHS CESSNA T206H/206H SUPPLEMENTS INTRODUCTION It is the airplane owner’s responsibility to confirm compatibility any combination of Supplemental Type Certificate’s (STC) that are installed in conjunction with this modification. The following list consists of optional kits produced by Soloy Corporation for the Soloy Turbine powered Cessna 206 aircraft.
Page 180 SOLOY TURBINE PAC SECTION 9 POHS CESSNA T206H/206H SUPPLEMENTS This page left blank intentionally. F.A.A. Approved May 23, 2003...
Page 181 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 1 POHS CESSNA T206H/206H CONTINUOUS IGNITION SUPPLEMENT CONTINUOUS IGNITION KIT SECTION 1 GENERAL The installation of the Continuous Ignition Kit provides an added level of safety when operating in rain or snow. When the pilot closes the switch, it causes the ignition exciter to operate continuously providing re-ignition in case of a flame out.
Page 182 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 1 POHS CESSNA T206H/206H CONTINUOUS IGNITION SECTION 4 NORMAL PROCEDURES The Continuous Ignition switch should be on during flight in adverse weather conditions. CAUTION THE CONTINUOUS IGNITION SYSTEM SHOULD NOT BE USED IN LIEU OF ENGINE ANTI-ICE OR INLET ALTERNATE AIR.
Page 183 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 1 POHS CESSNA T206H/206H CONTINUOUS IGNITION SECTION 7 AIRPLANE & SYSTEMS DESCRIPTIONS IGNITION SYSTEM The modification consists of installing one circuit breaker in the circuit breaker/switch panel, and installing one lighted push button switch on the circuit breaker/switch or the instrument panel.
Page 184 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 1 POHS CESSNA T206H/206H CONTINUOUS IGNITION This page intentionally left blank. 4 of 4 F.A.A. Approved May 23, 2003...
Page 185 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 2 POHS CESSNA T206H/206H BLEED AIR HEATER SUPPLEMENT BLEED AIR HEATER KIT SECTION 1 GENERAL The installation of a bleed air cabin heater will assist the exhaust heat exchanger in cabin heating for extremely cold conditions. Compressor...
Page 186 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 2 POHS CESSNA T206H/206H BLEED AIR HEATER SECTION 3 EMERGENCY PROCEDURES ENGINE RESTART PROCEDURE DURING FLIGHT The bleed air heater must be turned off before attempting an in-flight restart. DISCHARGE AIR CONTAMINATION If there is any sign of contamination of the bleed air such as oil or oil vapor odor, turn off the bleed air heater valve and land as soon as practical.
Page 187 Cessna firewall heater valve. With the cabin heat control knob open, additional cabin heating will be attainable by rotating the bleed air heat control knob for the amount of heat desired.
Page 188 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 2 POHS CESSNA T206H/206H BLEED AIR HEATER SECTION 9 SUPPLEMENTS There is no change to the airplane Supplements Section when the bleed air heater is installed. 4 of 4 F.A.A. Approved May 23, 2003...
Page 189 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 3 POHS CESSNA T206H/206H COWL LANDING LIGHTS SUPPLEMENT NO. 3 COWL LANDING LIGHTS SECTION 1 GENERAL The airplane is equipped with both landing and taxi lights mounted on the left wing. These lights remain unchanged. This supplement addresses the installation of two additional landing lights mounted in the lower engine cowling.
Page 190 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 3 POHS CESSNA T206H/206H COWL LANDING LIGHTS SECTION 4 NORMAL PROCEDURES BEFORE STARTING Check operation of cowl landing lights. FLIGHT, LANDING, TAXI Use at pilots discretion as situation requires. SECTION 5 PERFORMANCE There are no changes to the Performance when the Cowl Light Kit is...
Page 191 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 3 POHS CESSNA T206H/206H COWL LANDING LIGHTS SECTION 8 HANDLING, SERVICE & MAINTENANCE There is no change to the airplane handling, service and maintenance procedures when the cowl landing light kit is installed. SECTION 9...
Page 192 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 3 POHS CESSNA T206H/206H COWL LANDING LIGHTS This page intentionally left blank 4 of 4 F.A.A. Approved May 23, 2003...

This manual is also suitable for:

206h

Cessna T206H Flight Manual

Table of Contents

This Page Left Blank Intentionally.

This Page Left Blank Intentionally.

Table of Contents

Page

This Page Intentionally Left Blank.

Table of Contents

Table of Contents

Quick Links

Chapters

Related Manuals for Cessna T206H

Summary of Contents for Cessna T206H

This manual is also suitable for:

Table of Contents