Page 1 450 Pat Kennedy Way S.W. Olympia, WA 98501 PILOT’S OPERATING HANDBOOK SUPPLEMENT FAA APPROVED AIRPLANE FLIGHT MANUAL 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.: ____________________...
Page 2 SOLOY TURBINE PAC CONGRATULATIONS POHS CESSNA U/TU 206G CONGRATULATIONS ..Your airplane is SPECIAL! A Soloy, LLC 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 U/TU 206G 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 U/TU 206G LOG OF EFFECTIVE PAGES (Continued) Page Revision Page Revision 1-10 3-10 3-11 3-12 3-13 3-14 3-15 3-16 3-17 3-18 2-10 3-19 3-20 2-11 2-12 2-13 2-14 2-15 2-16 2-17 2-18 2-19 2-20 2-21...
Page 5 SOLOY TURBINE PAC POHS CESSNA U/TU 206G LOG OF EFFECTIVE PAGES (Continued) Page Revision Page Revision 5-23 4-17 5-24 4-18 4-19 5-25 4-20 5-26 5-27 4-21 4-22 5-28 4-23 4-24 4-25 4-26 6-10 5-10 5-11 5-12 5-13 5-14 5-15 5-16...
Page 6 SOLOY TURBINE PAC POHS CESSNA U/TU 206G LOG OF EFFECTIVE PAGES (Continued) Page Revision Page Revision 7-17 7-18 7-19 7-20 7-21 7-22 7-23 7-24 7-25 7-26 7-27 7-28 7-29 7-30 8-10 8-11 8-12 8-13 8-14 NOTE: Revised text is indicated by a revision bar in the margin.
Page 7 SOLOY TURBINE PAC POHS CESSNA U/TU 206G LOG OF REVISIONS Revision Pages Revised Comments FAA Approval Date 1/4/85 Original Original of Manual. Lester H. Berven for Manager, Seattle Aircraft Certification Office, ANM-100S Renton, WA 98055- 4056 Date: 1/4/85 1/11/85 i, ii, iii, iii(a), Added Log of Lester H.
Page 8 SOLOY TURBINE PAC POHS CESSNA U/TU 206G LOG OF REVISIONS (Continued) Revision Pages Revised Comments F.A.A. Approval Date 1/27/86 i, ii, iii, iii(a), Added 5.00-5, 6- Lester H. Berven 2-10, 8-11 Ply Nose Wheel for Manager, Seattle Size Aircraft Certification...
Page 9 SOLOY TURBINE PAC POHS CESSNA U/TU 206G LOG OF REVISIONS (Continued) Revision Pages Revised Comments F.A.A. Approved Date 3/30/90 I, ii, iii(a), 9- Added Donald B. Wilson Cessna for Manager, Seattle Skydiving Kit Aircraft Certification Office, ANM-100S Supplements, Renton, WA 98055-...
Page 10 SOLOY TURBINE PAC POHS CESSNA U/TU 206G LOG OF REVISIONS (Continued) Revision Pages Revised Comments F.A.A. Approved Date 7/30/92 I, ii, iii, iii(a), Addition to Richard A. Paul iii(b), 2-8, 2- Fuel Low for Manager, Seattle 11, 3-4, 3- Warning...
Page 11 SOLOY TURBINE PAC POHS CESSNA U/TU 206G LOG OF REVISIONS (Continued) Revision Pages Revised Comments F.A.A. Approved Date 10/4/05 All pages Re-issuance of T.E.A. complete POHS in for Manager, Seattle digital format. Aircraft Certification Changed all Office, ANM-100S references to Soloy...
Page 12 SOLOY TURBINE PAC POHS CESSNA U/TU 206G LOG OF REVISIONS (Continued) Revision Pages Revised Comments F.A.A. Approved Date 11/17/15 Cover Removed prev. revision signature and date. i-iv, x-xii Added Rev 17. Table of Contents moved from pg. x to pg. xi. Added page for Manager, Seattle xii.
Page 13 SOLOY TURBINE PAC POHS CESSNA U/TU 206G 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 &...
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Page 15: Table Of Contents
SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G GENERAL SECTION 1 GENERAL TABLE OF CONTENTS Page Introduction ................... 1-4 Descriptive Data ................... 1-4 Engine ....................1-4 Propeller .................... 1-4 Fuel ....................1-4 Oil ...................... 1-4 Maximum Certified Weights ............... 1-5 Standard Airplane Weights ..............
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Page 17 SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G GENERAL Figure 1-1. Three View F.A.A. Approved November 14, 2014...
Page 18: Introduction
SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G GENERAL INTRODUCTION This handbook supplement contains nine sections and includes the material required to be furnished to the pilot by CAR Part 3. 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 19: Maximum Certified Weights
SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G GENERAL MAXIMUM CERTIFIED WEIGHTS Takeoff: 3,600 lbs. Landing: 3,600 lbs. Weight in Baggage Compartment – Station 109 – 145: S/Ns U20602589 & U20603522 thru U20604649 – 120 lbs. maximum S/Ns U20604650 thru U20606847 and on – 180 lbs. maximum...
Page 20: Symbols, Abbreviations And Terminology
SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G 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 21: Meteorological Terminology
SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G 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 22: Engine Controls And Instruments
SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G GENERAL ENGINE POWER TERMINOLOGY (Continued) Revolutions per minute. Shaft horsepower is the power delivered at the propeller shaft. STAGNATED Slow acceleration during an engine start, possibly START deteriorating to total stoppage of acceleration even though combustion is still occurring in the combustion section.
Page 23: Airplane Performance And Flight Planning Terminology
SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G GENERAL ENGINE CONTROLS AND INSTRUMENTS (Continued) TORQUE METER An instrument that indicates power output of the engine in psi of torque where 1 psi is equal to 4.12 shp. Standard temperature as defined in meteorological terminology.
Page 24 SOLOY TURBINE PAC SECTION 1 POHS CESSNA U/TU 206G GENERAL WEIGHT AND BALANCE TERMINOLOGY (Continued) Moment is the product of the weight of an item MOMENT multiplied by its arm. (Moment divided by the constant 1000 is used in this handbook to simplify balance calculations by reducing the number of digits.)
Page 25 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS SECTION 2 LIMITATIONS TABLE OF CONTENTS PAGE Introduction ..................Airspeed Limitations ................Airspeed Indicator Markings ..............Powerplant Limitations ................ Engine Operating Limits ............... Propeller Limitations ................Powerplant Instrument Markings ............
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Page 27: Introduction
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS – No change except: INTRODUCTION This Supplement contains the information required to be furnished to the pilot by CAR Part 3 and must be carried in the airplane during flight operations.
Page 28: Airspeed Indicator Markings
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G 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 29: Engine Operating Limits
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G 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 30: Propeller Limitations
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G 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);...
Page 31: Powerplant Instrument Markings
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS POWERPLANT INSTRUMENT MARKINGS POWERPLANT INSTRUMENT MARKINGS INSTRUMENT LIMIT ------ 1630 1480 1810 1990 PROPELLER 1810 1630 (4)(5) 59%- ------ 105% 106% 105% TORQUE ------ 0-78 101.4 101.4 ------ 150C 400 - 738...
Page 32: Miscellaneous Instrument Markings
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS MISCELLANEOUS INSTRUMENT MARKINGS SUCTION ------ 4.6-5.4 ------ ------ in. Hg. AMMETER 80-150 FUEL QTY. E to Figure 2-5. Miscellaneous Instrument Markings. NOTES : (1) N and oil pressure limits are noted by a step in their respective arcs.
Page 33: Weight Limits
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS WEIGHT LIMITS Maximum Takeoff Weight: 3600 lbs. Maximum Landing Weight: 3600 lbs. Maximum Weight in Baggage Compartment – Station 109 to 145: S/Ns U20602589, U20603522 thru U20604649: 120 lbs. S/Ns U20604650 thru U20606847 and on: 180 lbs.
Page 34: Kinds Of Operation Limits
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS KINDS OF OPERATION LIMITS Flight into known icing conditions is prohibited. The engine alternate air must be activated for flight or ground operation in the following conditions: In visible moisture at an OAT of 5C (41F) and below.
Page 35: Minimum Fuel
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS MINIMUM FUEL Due to the possibility of fuel starvation, takeoff or steep climbs at speeds below V (86 KIAS at sea level) with either fuel quantity gauge indicating in the yellow arc (1/8 fuel quantity), or if installed FUEL LOW lights are on, are prohibited.
Page 36: Oil Specifications
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS CAUTION PROPER MIXING OF THE ANTI-ICING ADDITIVE WITH FUEL IS EXTREMELY IMPORTANT BECAUSE CON- CENTRATION IN EXCESS OF THAT RECOMMENDED (0.15% BY VOLUME) WILL RESULT IN DETRIMENTAL EFFECTS TO THE FUEL TANKS. ASSURE THAT THE FUEL ADDITIVE IS DIRECTED INTO AND BLENDING WITH FLOWING FUEL FROM THE FUELING NOZZLE.
Page 37: Landing Gear Limitations
SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS LANDING GEAR LIMITATIONS Nose Wheel Size: 6.00-6 5.00-5 (Limited to 6.00-6 main wheel size only with 5.00-5 nose wheel) Main Wheel Size: 6.00-6 8.00-6 8.50-6 MAXIMUM OPERATING ALTITUDE LIMITS Maximum Operating Altitude: 20,000 feet.
Page 38 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS (1) In full view of the pilot: (The “DAY-NIGHT-VFR-IFR” entry, shown on the example below, will vary as the airplane is equipped.) For S/Ns U20603522 thru U20604649 This airplane must be operated as a normal category...
Page 39 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS (3) On fuel selector plate: For S/Ns: U20603522 thru U20604649 TWO-POSITION SELECTOR VALVE USABLE FUEL 76 U.S. GAL. FUEL SELECTOR “ON” “OFF” FOUR-POSITION SELECTOR VALVE 2-15 F.A.A. Approved November 14, 2014...
Page 40 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS (3) On fuel selector plate: For S/Ns: U20602589, U20604650 thru U20606847 and on TWO-POSITION SELECTOR VALVE USABLE FUEL 88 U.S. GAL. FUEL SELECTOR “ON” “OFF” FOUR-POSITION SELECTOR VALVE 2-16 F.A.A. Approved...
Page 41 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS (4) Forward of fuel tank filler cap: For S/Ns: U20602589, U20603522 thru U20606847 and on FUEL JET A SEE PILOT’S OPERATING HANDBOOK FOR ANTI-ICE ADDITIVE REQUIREMENT AND ALTERNATE FUELS. (5) On oil filler cap:...
Page 42 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS (7) On the flap control indicator: For S/Ns: U20602589, U20603522 thru U20606847 and on (8) On the warning lights dimmer switch: For S/Ns: U20602589, U20603522 thru U20606847 and on WARNING...
Page 43 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS (10) Next to the propeller control: For S/Ns: U20602589, U20603522 thru U20606847 and on PROP PULL FTHR (11) Next to the fuel cutoff control: For S/Ns: U20602589, U20603522 thru U20606847 and on...
Page 44 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS (13) On aft cargo door: For S/N U20602589, U20603522 thru U20604649: BAGGAGE NET 120 LBS MAX CAPACITY. REFER TO WEIGHT AND BALANCE DATA FOR BAGGAGE AND CARGO LOADING. For S/Ns U20604650 thru U20606847 and on: BAGGAGE NET 180 LBS MAX CAPACITY.
Page 45 SOLOY TURBINE PAC SECTION 2 POHS CESSNA U/TU 206G LIMITATIONS (15) Next to the fuel totalizer: For S/Ns: U20602589, U20603522 thru U20606847 and on MAXIMUM ALTITUDE 8,000 FEET WHEN USING COLD WEATHER FUEL AT FUELTEMPERATURES ABOVE 4°C. (16) Near airspeed indicator:...
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Page 47 SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS PAGE Introduction ................3-3 Airspeeds For Emergency Operation ........3-3 OPERATIONAL CHECKLIST Engine Failures ................ 3-3 Engine Failure During Takeoff Run ........3-3 Engine Failure Immediately After Takeoff ......
Page 48 SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES (Continued) ......... PAGE TABLE OF CONTENTS AMPLIFIED PROCEDURES Engine Failure ..............3-13 Forced Landings ..............3-14 Landing Without Elevator Control ..........3-14 Fires ……………………………………………………………….. 3-14 Emergency Operation In Clouds ..........3-15 Vacuum System Failure ..........
Page 49: Introduction
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G 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 50: Engine Failure Immediately After Takeoff
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES NOTE An internal engine fire (recognized by a rapid increase in TOT) can occur during shutdown if fuel cutoff is not complete. If a shutdown fire occurs, immediately engage the starter and motor the engine to minimize the temperature encountered.
Page 51: Forced Landings
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES TOT 150 or lower and N 15% below 15,000 FT. MSL. maximum obtainable above 15,000 FT. MSL. Start Motor Switch – START and hold Fuel Cutoff Control – RUN (IN) TOT and N –...
Page 52: Precautionary Landing With Engine Power
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES PRECAUTIONARY LANDING WITH ENGINE POWER Airspeed – 80 KIAS Wing Flaps -- 20 Selected Field – FLY OVER NOTING TERRAIN & OBSTRUCTIONS Radio and Electrical Switches – OFF Wing Flaps -- 40 (recommended on final approach) Power Control –...
Page 53: Engine Fire In Flight
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES Fuel Cutoff Control – CUTOFF (OUT) Start Motor Switch – MOTOR to extinguish the fire. Fuel Selector – OFF Monitor – TOT Fire Extinguisher – OBTAIN (have ground attendants obtain if not installed).
Page 54: Cabin Fire
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES If fire appears out and electrical power is necessary for continuance of the flight: Battery and Generator – ON Monitor electrical load Circuit Breakers – CHECK for faulty circuit, do not reset.
Page 55: Icing
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES ICING INADVERTENT ICING ENCOUNTER NOTE The engine alternate air must be activated for flight or ground operation in visible mois- ture at an OAT of 5C (41F) and below or while operating in falling or blowing snow regardless of ambient temperature.
Page 56: Engine Alternate Air Failure
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES Use a 10º to 20º landing flap setting for ice accumulations of 1 inch or less. With heavier ice accumulations, approach with flaps retracted to ensure adequate elevator effectiveness in the approach and landing.
Page 57: Static Source Blockage (Erroneous Instrument Reading Suspected)
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES STATIC SOURCE BLOCKAGE (Erroneous Instrument Reading Suspected) Vents and Windows – CLOSED Alternate Static Source Valve – PULL ON Airspeed – Consult Calibration Table in Section 5. LANDING WITH A FLAT MAIN TIRE Wing Flaps –...
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Page 59: Amplified Procedures
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G 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 60: Forced Landings
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G 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.
Page 61: Emergency Operation In Clouds
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES EMERGENCY OPERATION IN CLOUDS VACUUM SYSTEM FAILURE In the event of a vacuum system failure 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 62: Recovery From A Spiral Dive
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G 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 63: Alternate Air Light Does Not Illuminate
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G 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 64: Rough Engine Operation Or Loss Of Power
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES SIMULTANEOUSLY APPLY AND HOLD FULL RUDDER OPPOSITE TO THE DIRECTION OF ROTATION AND MOVE THE CONTROL WHEEL BRISKLY FORWARD FAR ENOUGH TO BREAK THE STALL. Full down elevator may be required at aft center of gravity loadings to assure optimum recoveries.
Page 65: Low Engine Oil Pressure And/Or Low Transmission Pressure
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES LOW ENGINE OIL PRESSURE AND/OR LOW TRANSMISSION OIL PRESSURE The combined engine and transmission oil pressure warning light illuminates when the engine oil or the propeller reduction gearbox pressure is lower than normal. Should the light illuminate in flight, confirm the loss of oil pressure with the oil pressure gauges and land as soon as practicable.
Page 66: Insufficient Generator Output
SOLOY TURBINE PAC SECTION 3 POHS CESSNA U/TU206G EMERGENCY PROCEDURES If the problem no longer exists, normal generator charging will resume and the warning light will go off and the system should be checked at the completion of the flight.
Page 67 SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS PAGE Introduction ..................Speeds for Normal Operation ............CHECKLIST PROCEDURES Preflight Inspection ................Cabin ..................... Empennage ................... Right Wing, Trailing Edge ..............
Page 68 SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES AMPLIFIED PROCEDURES Preflight Inspection ................4-13 Before Starting The Engine ..............4-14 Starting Engine .................. 4-15 Taxiing ....................4-17 Before Takeoff ................... 4-18 Takeoff ....................4-19 Wing Flap Settings................. 4-20 Crosswind Takeoff .................
Page 69: Introduction
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G 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. SPEEDS 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 70: Checklist Procedures
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES CHECKLIST PROCEDURES PREFLIGHT INSPECTION CABIN Control Wheel Lock – REMOVE. Battery Switch – ON. Fuel Quantity Indicators – CHECK QUANTITY Wing Flaps – DOWN Battery Switch -- OFF Fuel Selector Valve – ON (BOTH if fuel low warning system...
Page 71: Right Wing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES RIGHT WING Wing Tie-Down – DISCONNECT Fuel Tank Vent – CHECK for stoppage Main Wheel Tire – CHECK for proper inflation Fuel Tank Sump Quick-Drain Valve – DRAIN at least a cupful of...
Page 72: Left Wing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES LEFT WING Main Wheel Tire – CHECK for proper inflation. Fuel Tank Sump Quick Drain Valves -- DRAIN at least a cupful of fuel (using sampler cup) to check for water, sediment and proper fuel grade before each flight of the day and after each refueling.
Page 73: Starting Engine
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES STARTING ENGINE Propeller – CLEAR TOT 150C or Lower NOTE TOT can readily be reduced to 150°C by motoring the starter. Start Motor Switch – MOTOR and HOLD to 12 – 15% N based on temperatures listed below.
Page 74: Before Takeoff
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES BEFORE TAKEOFF Parking Brake – SET Cabin Doors and Windows – CLOSE and LOCK Seat Belts and Shoulder Harnesses – SECURE Engine Instruments -- CHECK Flight Controls – FREE and CORRECT Elevator and Rudder Trim --- TAKEOFF setting Propeller Control –...
Page 75: Takeoff
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES TAKEOFF NORMAL TAKEOFF Wing Flaps – 0 to 20 Power Control – FLIGHT IDLE and stabilize at 1810 N RPM, then TAKEOFF POWER (101.4 PSI torque or 810C TOT limits).
Page 76: Cruise
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES WARNING WITH 1/8 FUEL TANK QUANTITY OR LESS, OR IF THE INSTALLED FUEL LOW LIGHTS ARE ON, CLIMBS AT SPEEDS BELOW V ARE PROHIBITED. CRUISE Ice Protection – AS REQUIRED Propeller Speed –...
Page 77: Short Field Landing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES SHORT FIELD LANDING Airspeed – 75 – 85 KIAS (flaps UP) Wing Flaps -- 40 (below 96 KIAS) Airspeed – MAINTAIN 63 KIAS Elevator Trim -- ADJUST Power Control – REDUCE TO FLIGHT IDLE (14 PSI torque minimum) as obstacle is cleared.
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Page 79: Amplified Procedures
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES AMPLIFIED PROCEDURES PREFLIGHT INSPECTION The preflight inspection, described in the abbreviated procedures part of this section, is recommended before flight. The preflight should include a determination of the airplane’s operational status, a check that the necessary papers are on board and in order, and a computation of weight and C.G.
Page 80: Before Starting The Engine
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G 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 81: 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 82 SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES CAUTION DURING A START, THE FUEL CUTOFF CONTROL MUST NEVER BE ADVANCED FROM THE CUTOFF POSITION UNTIL AFTER THE STARTER AND IGNITION EXCITER HAVE BEEN ENERGIZED AND THE DESIRED CRANKING SPEED HAS BEEN ATTAINED.
Page 83: Taxiing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES If a stagnated start is experienced, or if it appears that the TOT will exceed the starting limits, abort the start by putting the fuel cutoff control to the CUTOFF (OUT) position and motor the engine for ten seconds to clear the combustion chamber of residual fuel.
Page 84: Before Takeoff
Alternate engine air is required when the aircraft is in visible moisture and an OAT of 5C (41F) and below or while operating in falling or blowing snow. Refer to Figure 4-2 in the Cessna Pilot’s Operating Handbook for additional taxiing instructions. BEFORE TAKEOFF...
Page 85: Takeoff
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES Check and set flight instruments and radios as desired. Be sure that the autopilot is OFF for takeoff. Check that the normal static source is selected. Check that necessary lights and electrical systems are ON, including ice protection systems if weather conditions warrant.
Page 86: Wing Flap Settings
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES LIMIT TIME LIMIT Up to 1900 RPM No Limit 1900 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 87: Enroute Climb
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G 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 88: Flight In Icing Conditions
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G 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 89: Short Field Landing
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES SHORT FIELD LANDING For short field landings, make a power approach at 63 KIAS with full flaps. After all approach obstacles are cleared, progressively reduce power. Maintain 63 KIAS approach speed by lowering the nose of the airplane.
Page 90: Cold Weather Operation
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES CAUTION AN AFTERFIRE (RECOGNIZED BY A RAPID INCREASE IN TOT) CAN OCCUR DURING SHUTDOWN IF FUEL CUTOFF IS NOT COMPLETE. IF A SHUTDOWN FIRE OCCURS, IMMEDIATELY ENGAGE THE STARTER AND MOTOR THE ENGINE WITHOUT IGNITION TO EXTINGUISH THE FIRE.
Page 91 SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES NOTE Variations in jet fuels can affect engine lightoff in cold ambient conditions. The engine may experience a short delay before lightoff after the Fuel Cutoff Control is moved to the RUN position. This delay should be less than three seconds regardless of the type of fuel used.
Page 92: Hot Weather Operation
SOLOY TURBINE PAC SECTION 4 POHS CESSNA U/TU 206G NORMAL PROCEDURES HOT WEATHER OPERATION On a hot day, takeoff power will be limited by TOT. There is a lag in the TOT gauge; therefore, it should be monitored during the takeoff run.
Page 93 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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 94 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G PERFORMANCE This Page Left Blank Intentionally F.A.A. Approved October 4, 2005...
Page 95: Introduction
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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 96: Airspeed Calibration
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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...
Page 97: Temperature Conversion Chart
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G PERFORMANCE DEGREES CELSIUS Figure 5-2. Temperature Conversion Chart F.A.A. Approved October 4, 2005...
Page 98: Stall Speeds
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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. MOST REARWARD CENTER OF GRAVITY ANGLE OF BANK 0...
Page 99 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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 October 4, 2005...
Page 100 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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 101 TAKEOFF DISTANCE, SHORT FIELD 3600 LBS PRESS FEET -20°C -10°C 0°C 10°C 20°C 30°C 40°C TOTAL TOTAL TOTAL TOTAL TOTAL TOTAL TOTAL GRND GRND GRND GRND GRND GRND GRND TO CLR TO CLR TO CLR TO CLR TO CLR TO CLR TO CLR ROLL ROLL...
Page 102 TAKEOFF DISTANCE, SHORT FIELD 3300 LBS PRESS FEET -20°C -10°C 0°C 10°C 20°C 30°C 40°C TOTAL TOTAL TOTAL TOTAL TOTAL TOTAL TOTAL GRND GRND GRND GRND GRND GRND GRND TO CLR TO CLR TO CLR TO CLR TO CLR TO CLR TO CLR ROLL ROLL...
Page 103 TAKEOFF DISTANCE, SHORT FIELD 3000 LBS PRESS FEET -20°C -10°C 0°C 10°C 20°C 30°C 40°C TOTAL TOTAL TOTAL TOTAL TOTAL TOTAL TOTAL GRND GRND GRND GRND GRND GRND GRND TO CLR TO CLR TO CLR TO CLR TO CLR TO CLR TO CLR ROLL ROLL...
Page 104 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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...
Page 105 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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 106: Temperature - Standard
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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 107: Temperature - Standard +20°C
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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 108: Temperature - Standard -20°C
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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 109 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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)
Page 110 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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)
Page 111 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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)
Page 112 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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)
Page 113 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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)
Page 114 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G 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) 5-22 F.A.A.
Page 115 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G PERFORMANCE RANGE PROFILE 45 Minute Reserve 76 Gallons Usable Fuel CONDITIONS: NOTE: 1810 RPM 100% N THIS CHART ALLOWS FOR FUEL 3600 LB AT ENGINE START USED IN START, TAXI, AND CLIMB...
Page 116: Range Profile - 88 Gallons Fuel
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G PERFORMANCE RANGE PROFILE 45 Minute Reserve 88 Gallons Usable Fuel CONDITIONS: NOTE: 1810 RPM 100% N THIS CHART ALLOWS FOR FUEL 3600 LB AT ENGINE START USED IN START, TAXI, AND CLIMB...
Page 117 SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G PERFORMANCE ENDURANCE PROFILE 45 Minute Reserve 76 Gallons Usable Fuel CONDITIONS: NOTE: 1810 RPM 100% N THIS CHART ALLOWS FOR FUEL 3600 LB AT ENGINE START USED IN START, TAXI, AND CLIMB...
Page 118: Endurance Profile - 88 Gallons Fuel
SOLOY TURBINE PAC SECTION 5 POHS CESSNA U/TU 206G PERFORMANCE ENDURANCE PROFILE 45 Minute Reserve 88 Gallons Usable Fuel CONDITIONS: NOTE: 1810 RPM 100% N THIS CHART ALLOWS FOR FUEL 3600 LB AT ENGINE START USED IN START, TAXI, AND CLIMB...
Page 119 LANDING DISTANCE, SHORT FIELD 3600 LB PRESS FEET -20°C -10°C 0°C 10°C 20°C 30°C 40°C TOTAL TOTAL TOTAL TOTAL TOTAL TOTAL TOTAL GRND GRND GRND GRND GRND GRND GRND TO CLR TO CLR TO CLR TO CLR TO CLR TO CLR TO CLR ROLL ROLL...
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Page 121 SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G WEIGHT & BALANCE/ EQUIPMENT LIST SECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST TABLE OF CONTENTS PAGE Introduction .................. 6-3 Airplane Weighing Procedures ............6-3 Sample Weight & Balance Forms ..........6-3 Weight and Balance ............... 6-3 Equipment List ................
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Page 123: Introduction
SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G WEIGHT & BALANCE/ EQUIPMENT LIST INTRODUCTION This section supplies supplemental information for establishing the basic empty weight and moment of the airplane. Supplemental information for calculating the weight and moments for various operations is also provided.
Page 124: Equipment List
SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G 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 2079 73.2 and full oil) Usable fuel (at 6.7...
Page 125 SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G 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 126 SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G 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.
Page 127 SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G 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.
Page 128 SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G WEIGHT & BALANCE/ EQUIPMENT LIST EQUIPMENT LIST EQUIPMENT LIST ITEM NO. DESCRIPTION (lbs) (ins) EQUIPMENT REMOVED Powerplant and Accessories -17.0 A01-R Engine, Continental IO-520F 450.0 -9.5 A05-R Filter, Induction Air -6.0...
Page 129 SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G WEIGHT & BALANCE/ EQUIPMENT LIST EQUIPMENT LIST ITEM NO. DESCRIPTION (lbs) (ins) TURBINE PAC ADDITIONS Powerplant and Accessories -32.7 Engine, Soloy Turbine Pac 320.0 Propeller HC-C3YN-5A/ -58.2 95.0 FC9587D-2 -40.8 Governor, Propeller -62.0...
Page 130 SOLOY TURBINE PAC SECTION 6 POHS CESSNA U/TU 206G WEIGHT & BALANCE/ EQUIPMENT LIST This page left blank intentionally 6-10 F.A.A. Approved October 4, 2005...
Page 131 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION SECTION 7 AIRPLANE & SYSTEMS DESCRIPTIONS TABLE OF CONTENTS ..............PAGE Introduction ..................7-9 Airframe .................... 7-9 Flight Controls .................. 7-9 Trim Systems ................7-9 Instrument Panel ................7-9 Optional 2”...
Page 132 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION TABLE OF CONTENTS (Continued) ........... PAGE Fuel System .................. 7-22 Fuel Tanks ................7-22 Fuel Indicating System ............7-22 Fuel Required For Flight ............7-23 Fuel Totalizer ............... 7-24 Operating Details ..............
Page 133 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION Figure 7-1. Instrument Panel (Sheet 1 of 2) For Aircraft S/Ns U20602589 thru U20606439 F.A.A. Approved October 4, 2005...
Page 134 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION Suction Gauge 25. Cabin Heat Control Ammeter 26. Flap Control & Indicator Clock 27. Propeller Control Annunciator Dimmer 28. Power Control Spare 29. Engine Alternate Air Control Turn Coordinator 30.
Page 135 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION Clock 26. N1 Tachometer Aux Mic & Headset Jacks 27. Maps Compartment Marker Beacon 28. Defrost Control Turn Coordinator 29. Aux Cabin Air Control Airspeed Indiciator 30. Cabin Air Control 31.
Page 136 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION Ammeter 30. Fuel Filter (Light) Spare 31. Gen Off Buss (Light) Clock 32. Defrost Control Suction Gauge 33. Map Compartment Spare 34. Aux Cabin Air Control Turn Coordinator 35.
Page 137 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION For Aircraft S/Ns U20606440 and on Figure 7-3. Instrument Panel (Sheet 1 of 2) 2” Instruments F.A.A. Approved October 4, 2005...
Page 138 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION For Aircraft S/Ns U20603522 thru U20606439 Figure 7-3. Instrument Panel (Sheet 2 of 2) 2” Instruments For Aircraft S/Ns U20606440 and on F.A.A. Approved October 4, 2005...
Page 139: Introduction
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G 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 140: Optional 2" Engine Instruments
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION contains the elevator and rudder trim control wheels, engine alternate air control lever, microphone bracket and the fuel selector valve handle. A parking brake handle is mounted under the switch and control panel in front of the pilot.
Page 141: Ground Control
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION The amber AUTO FEATHER light advises that the overspeed governor and the auto feather solenoid are operating. Also, before starting the engine, it advises that the pressure sensor is providing power for the auto feather system.
Page 142: Shoulder Harnesses
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION SHOULDER HARNESSES – No Change INTEGRATED SEAT BELT/SHOULDER HARNESSES WITH INERTIA REELS – No Change – No ENTRANCE DOORS AND CABIN WINDOWS Change – No Change CONTROL LOCKS...
Page 143: Engine Controls
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION A two-stage helical gear set in the engine power and accessory gearbox reduces rotational speed from 33,290 RPM at 100% N power turbine speed to 6016 RPM at the output drive spline. A flex coupled...
Page 144: Propeller Control
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION PROPELLER CONTROL The vernier propeller control in the cockpit is connected to the propeller governor mounted on the Soloy propeller reduction gearbox. The propeller control controls propeller governor settings from the maximum RPM position (1810 RPM) to a minimum flight position (1450 RPM) to full feather.
Page 145: N 1 Percent Rpm Indicator
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION PERCENT RPM INDICATOR The N RPM indicator indicates the percent of the gas producer RPM based on a figure of 105% N at 53,519 RPM. ENGINE OIL PRESSURE INDICATOR Oil pressure is displayed in pounds per square inch.
Page 146: Ignition System
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION Oil from the cooler is then circulated back to the integral tank. The propeller reduction gearbox oil is routed from the tank to the gearbox oil pump then through a filter in the gearbox. The oil is retrieved from the gearbox by a scavenge pump, and passes by an oil chip detector through a filter and back into the integral tank.
Page 147: Exhaust System
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION During normal operation of the engine air system, the movable ram inlet doors are retracted out of the direct ram air inlet. For cold weather operation (5C or below) in visible moisture, or while operating in falling or blowing snow, the doors should be raised to block the ram air inlet.
Page 148: Propeller
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION PROPELLER The airplane is equipped with an all-metal, three-bladed, constant speed, full feathering, governor regulated propeller. A setting introduced into the governor with the propeller control establishes the propeller speed, and thus, the engine power turbine speed to be maintained.
Page 149 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION Figure 7-6. Fuel System 7-19 F.A.A. Approved October 4, 2005...
Page 150 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION Figure 7-6A. Fuel System 7-20 F.A.A. Approved October 4, 2005...
Page 151 SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION Figure 7-6B. Fuel System 7-21 F.A.A. Approved October 4, 2005...
Page 152: Fuel System
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION FUEL SYSTEM The fuel system, see Figure 7-6, consists of left and right vented fuel tanks, two fuel reservoir tanks, a fuel selector valve, engine fuel filter, fuel system quantity and flow instrumentation.
Page 153: Fuel Required For Flight
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION accurate readings during skids, slips, climbs, descents, or unusual attitudes. If both indicator pointers should rapidly move to a zero reading, check the circuit breaker for an electrical malfunction.
Page 154: Fuel Totalizer
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION FUEL TOTALIZER A fuel totalizer system is also installed. The totalizer displays a continuous readout of total fuel flow in pounds per hour, time remaining in hours and minutes and fuel temperature in degrees F.
Page 155: If No Extra Fuel Is Needed
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION NOTE Using the test function while engine is running causes the computer to lose 13 seconds of fuel count. Time remaining shows no display at the upper display window.
Page 156: If Extra Fuel Is Needed
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION If Extra Fuel is Needed, (less than total usable lb.) On paper, add the amount of fuel remaining displayed to the amount of fuel from the refueling truck meter using 6.71 lb/gal.
Page 157: Electrical System
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION ELECTRICAL SYSTEM Electrical power for the aircraft is supplied by a 24 volt direct current negative ground electrical system A single 19 amp hour, 24 volt lead...
Page 158: Circuit Breakers And Fuses
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION CIRCUIT BREAKERS AND FUSES The circuit breakers and fuses remains the same with the following exceptions: The APU circuit fuse and clock circuit fuse are mounted adjacent to the electrical component housing on the left side of the firewall.
Page 159: Stall Warning System
SOLOY TURBINE PAC SECTION 7 POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS DESCRIPTION STALL WARNING SYSTEM – No Change AVIONICS SUPPORT EQUIPMENT – No Change AUDIO CONTROL PANEL – No Change MICROPHONE HEADSET – No Change STATIC DISCHARGERS – No Change 7-29 F.A.A.
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Page 161 SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE SECTION 8 AIRPLANE HANDLING, SERVICE & MAINTENANCE TABLE OF CONTENTS PAGE Introduction ................... 8-3 Identification Plate ................ 8-3 Owner Follow-Up System ............. 8-3 Publications ................8-3 Airplane File ................. 8-4 Airplane Inspection Periods ............
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Page 163: Introduction
– No Changes Except: OWNER FOLLOW-UP SYSTEM In addition to the Cessna system, Soloy, LLC offers a support system consisting of technical publications and service information. PUBLICATIONS -- No Change Except: In addition to the Cessna publications, Soloy, LLC furnishes various publications with the airplane at the time of delivery.
Page 164: Airplane File
SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE The following additional publications are supplied with your new engine from Rolls Royce: 250-C20 Series Operations & Maintenance Manual Parts Catalog Distributor Directory Service Instructions applicable to accessory items installed.
Page 165: Flyable Storage
SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE Set the parking brake and install the control wheel lock. CAUTION DO NOT SET PARKING BRAKE WHEN THE BRAKES ARE OVERHEATED OR DURING COLD WEATHER WHEN ACCUMULATED MOISTURE MAY...
Page 166: Servicing
SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE Re-preserve at least each thirty days if the aircraft is stored outdoors and each ninety days if stored indoors. Install covers on the compressor inlet and the exhaust collector stacks.
Page 167 SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE TABLE I RECOMMENDED OILS AT SPECIFIC AMBIENT TEMPERATURES Temperature Rating Specification MIL-PRF-23699, SAE AS5780, -40°C (-40°F) and above MIL-PRF-7808, DOD-PRF-85734 -40°C (-40°F) and below MIL-PRF-7808 NOTE Because of availability, decreased coking...
Page 168: Oil Drain Period
SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE OIL DRAIN PERIOD It is recommended that the oil be changed every 200 hours or six months, whichever comes first. CAUTION USE OF OILS THAT ARE NOT...
Page 169: Cold Weather Fuels
SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE COLD WEATHER FUELS To assure consistent starts below 4ºC (40ºF), the following fuels may be necessary: MIL-T-5624, Grade JP-4 ASTM D-6615, Jet B AVGAS/JET A, JET A1, or JP-5 Mixtures.
Page 170 SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE CAUTION THERE IS NO LIMIT FOR ENGINE OPERATION USING THE AVGAS-JET FUEL MIXTURE AS LONG AS 80/87 GRADE AVGAS IS USED AND THE 1:VOLUME RATIO IS OBSERVED. USE...
Page 171: Fuel Additives
SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE WARNING HANDLING LEAD RESIDUE COATED PARTS CAN BE EXTREMELY DANGEROUS. 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...
Page 172: Landing Gear
SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE LANDING GEAR Nose Wheel Tire Pressure -- 29 PSI on 6.00-6, 4-Ply Rated Tire 49 PSI on 5.00-5, 6-Ply Rated Tire Main Wheel Tire Pressure -- 42 PSI on 6.00-6, 6-Ply Rated Tire 35 PSI on 8.00-6, 6-Ply Rated Tire...
Page 173 SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE starter generator and the bleed air system. Refer to the Airplane Maintenance and the Engine Operation and Maintenance Manuals for proper lubrication of controls and components after engine cleaning.
Page 174 SOLOY TURBINE PAC SECTION 8 POHS CESSNA U/TU 206G HANDLING, SERVICE & MAINTENANCE This page left blank intentionally. 8-14 F.A.A. Approved November 14, 2014...
Page 175 Cessna 400 DME (Type R-476A) Cessna 400 Marker Beacon Type R-402A Cessna 400 Nav/Com (720 Channel Type RT-485A) With or Without Cessna 400 Area Navigation System (Type RM- 478A) Cessna 400 Nav/Com (720 Channel Type RT-485B) With or Without Cessna 400 Area Navigation System (Type RN-...
Page 176 SOLOY TURBINE PAC SECTION 9 POHS CESSNA U/TU 206G SUPPLEMENTS INTRODUCTION This section consists of a series of Soloy Turbine Pac supplements, each covering a single optional system that may be installed in the airplane. Each supplement contains a brief description and, when applicable, supplement to Sections 2 through 8.
Page 177 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 1 POHS CESSNA U/TU 206G EXHAUST HEAT EXCHANGER KIT SUPPLEMENT NO. 1 BLEED AIR HEATER KIT SECTION 1 GENERAL The installation of an exhaust heat exchanger kit will provide cabin heater air. Outside air enters from an inlet in the cowl, through a heat exchanger mounted within the left hand engine exhaust duct and enters the existing aircraft manifold through the existing firewall heater valve.
Page 178 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 1 POHS CESSNA U/TU 206G EXHAUST HEAT EXCHANGER KIT SECTION 4 NORMAL PROCEDURES There are no changes to the normal procedures when the heater kit is installed. SECTION 5 PERFORMANCE The installation of the heat exchanger in the exhaust duct reduces the available horsepower when operating at TOT limits.
Page 179 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 1 POHS CESSNA U/TU 206G EXHAUST HEAT EXCHANGER KIT CABIN HEATING, VENTILATING AND DEFROSTING SYSTEM The temperature and volume of airflow into the cabin can be regulated by manipulation of the push-pull CABIN HEAT and CABIN AIR control knobs.
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Page 181 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 2 POHS CESSNA U/TU 206G ENGINE INLET ANTI-ICE KIT SUPPLEMENT NO. 2 ENGINE INLET ANTI-ICE KIT SECTION 1 GENERAL INTRODUCTION The basic Soloy Turbine Pac 206 is equipped with an alternate air system to provide anti-ice protection to the engine inlet in visible moisture at an OAT of 5ºC (41ºF) and below and while operating in falling or blowing...
Page 182 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 2 POHS CESSNA U/TU 206G ENGINE INLET ANTI-ICE KIT SECTION 2 LIMITATIONS The following information must be presented in the form of a placard attached to the central pedestal: Near alternate air control: ALTERNATE AIR...
Page 183 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 2 POHS CESSNA U/TU 206G ENGINE INLET ANTI-ICE KIT NOTE The engine alternate air must be activated for flight or ground operation in visible moisture at an OAT of 1ºC (34ºF) and below or while operating in falling or blowing snow regardless of ambient temperature.
Page 184 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 2 POHS CESSNA U/TU 206G ENGINE INLET ANTI-ICE KIT Power Control – FLIGHT IDLE Start Motor Switch – MOTOR TOT 150 degrees or lower and N 15% below 15,000 FT. MSL. maximum obtainable above 15,000 FT. MSL 10.
Page 185 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 3 POHS CESSNA T206H/206H COWL LANDING LIGHTS SUPPLEMENT NO. 3 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 186 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 3 POHS CESSNA T206H/206H COWL LANDING LIGHTS 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 187 SOLOY TURBINE PAC SOLOY SUPPLEMENT NO. 3 POHS CESSNA T206H/206H COWL LANDING LIGHTS 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.
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