Cessna 208B/TPE331-12JR Landplane Airplane Flight Manual Supplement

performance. Performance for other operational conditions can be derived by reference to operational data in other sections of this handbook. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 General Information Rev. 5 iv November 7, 2019 FAA Approved CONTENTS SECTION GENERAL ………………………………………… 1 LIMITATIONS …………………………………….. 2 EMERGENCY PROCEDURES ………………… 3 NORMAL PROCEDURES ………………………. 4 PERFORMANCE ………………………………….5 WEIGHT & BALANCE/EQUIPMENT LIST ……. 6 AIRPLANE & SYSTEMS DESCRIPTIONS …….7 AIRPLANE HANDING, SERVICE & MAINTENANCE ………………………………….. 8 SUPPLEMENTS (Optional Systems Description & Operating Procedures) …………………9 Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 General Information Rev. 5 v November 7, 2019 FAA Approved SAFETY Your safety when operating this airplane is dependent on the airplane and you. Supervan Systems, Ltd. is committed to flight safety. The goal of the Supervan Systems team has been to design and build a safe, reliable engine modification for the Cessna Caravan that features excellent performance, efficiency, and capability. Although, the aircraft performs better in many areas, you should still respect all WARNINGS, CAUTIONS, and NOTES contained in both the original Cessna Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual, and those contained in this Airplane Flight Manual Supplement. You have the obligation to maintain and operate the airplane in a safe, professional, and conservative manner in accordance with Cessna approved Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual, approved Airplane Flight Manual Supplement, Maintenance Manual, Maintenance Manual Supplement, and company issued service information from either Cessna or Supervan Systems, Ltd. This will assure that the high level of safety we are both striving for is attained. WARNINGS, CAUTIONS, AND NOTES The following definitions apply to WARNINGS, CAUTIONS, and NOTES found throughout this supplement. WARNING OPERATING PROCEDURES, TECHNIQUES, OR ETC., WHICH MAY RESULT IN PERSONAL INJURY OR LOSS OF LIFE IF NOT CAREFULLY FOLLOWED. CAUTION OPERATION PROCEDURES, TECHNIQUES, OR ETC., WHICH MAY RESULT IN DAMAGE TO EQUIPMENT IF NOT CAREFULLY FOLLOWED. NOTE An operation procedure, technique, etc., which is considered essential to emphasize. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 1: General Rev. 5 1-1 November 7, 2019 FAA Approved SECTION 1: GENERAL Table of Contents Page Three View ................................................................................................... 1-2 Introduction .................................................................................................. 1-3 Descriptive Data ........................................................................................... 1-4 Engine .............................................................................................. 1-4 Propeller ............................................................................................ 1-4 Fuel ................................................................................................... 1-4 Oil ...................................................................................................... 1-6 Maximum Certificated Weights .......................................................... 1-6 Standard Airplane Weights ................................................................ 1-6 Cabin, Entry, Cargo Door and Compartment Dimensions ................. 1-7 Specific Loadings .............................................................................. 1-7 Symbols, Abbreviations and Terminology .................................................... 1-7 General Airspeed Terminology and Symbols .................................... 1-7 Meteorological Terminology............................................................... 1-7 Engine Power Terminology................................................................ 1-7 Airplane Performance and Flight Planning Terminology .................... 1-8 Weight and Balance Terminology ...................................................... 1-8 Autopilot/Flight Director Terminology ................................................. 1-8 Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 1: General Rev. 5 1-2 November 7, 2019 FAA Approved Figure 1-1, Three View Sheet (Sheet 1of 2) 12 3/8” 3 5/8” 15 7/8” 7” 109.5” Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 1: General Rev. 5 1-3 November 7, 2019 FAA Approved INTRODUCTION This handbook contains 9 sections, and includes the material required to be furnished to the pilot by Federal Aviation Regulations and additional information provided by Supervan Systems, Ltd. This handbook constitutes the FAA Approved Airplane Flight Manual Supplement to the Cessna Model 208B Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual (Cessna POH/AFM) when the aircraft is modified in accordance with STC SA10841SC. WARNING  THIS HANDBOOK IS NOT INTENDED TO BE A GUIDE FOR BASIC FLIGHT INSTRUCTION OR A FLIGHT TRAINING MANUAL AND SHOULD NOT BE USED AS ONE. IT IS NOT A SUBSTITUTE FOR ADEQUATE AND COMPETENT FLIGHT INSTRUCTION, PILOT SKILL, AND PILOT KNOWLEDGE OF CURRENT AIRWORTHINESS DIRECTIVES, APPLICABLE FEDERAL AVIATION REGULATIONS AND/OR ADVISORY CIRCULARS.  ASSURING THE AIRWORTHINESS OF THE AIRPLANE IS THE RESPONSIBILITY OF THE AIRPLANE OWNER OR OPERATOR. DETERMINING IF THE AIRPLANE IS SAFE FOR FLIGHT IS THE RESPONSIBILITY OF THE PILOT IN COMMAND. THE PILOT IS ALSO RESPONSIBLE FOR ADHERING TO THE OPERATION LIMITATIONS SET FORTH BY INSTRUMENT MARKINGS, PLACARDS, AND THE CESSNA POH/AFM. Generally, information in this handbook is applicable to both cargo and passenger versions of the Model 208B. Some equipment differences exist between these versions, and specific versions are identified through use of the terms “Cargo Version” and “Passenger Version”. When one of these terms appears in text or on an illustration, the information applies only to that group of airplanes. If no term appears, the information applies to all airplanes. Section 1 provides basic data and information of general interest. It also contains definitions or explanations of symbols, abbreviations, and terminology commonly used. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 1: General Rev. 5 1-4 November 7, 2019 FAA Approved DESCRIPTIVE DATA ENGINE Number of Engines: 1 Engine Manufacturer: Honeywell International, Inc. Engine Model Number: TPE331-12JR Engine Type: Direct drive, single-shaft engine utilizing two centrifugal compressors, an annular reverse- flow combustion chamber, three axial turbines, and a single exhaust. The engine drives the propeller through 26.2:1 reduction gearbox at the front of the engine. Horsepower: Flat rated at 900 shaft horsepower. PROPELLER Propeller Manufacturer: Hartzell Propeller, Inc Propeller Model Number: HC-B4TN-5QL/LT10890NK (de-ice), or HC-B4TN-5NL/LT10890N (non de-ice), or HC-B4TN-5QL/LT10891NK (de-ice), or HC-B4TN-5NL/LT10891N (non de-ice) Number of Blades: 4 Propeller Diameter Maximum: 109.5 inches. Minimum: 107.5 inches. Propeller Type: Constant-speed, full feathering, reversible, hydraulically-actuated aluminum-bladed propeller, with a feathered blade angle of +81.2º, a flight idle blade angle of +5.0º (±1.0º), and a maximum reverse blade angle of -12º (42-inch station). FUEL Table 1-1, Approved Fuel Types Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 1: General Rev. 5 1-5 November 7, 2019 FAA Approved Alternate/Emergency Fuels Aviation Fuel (All grades of military and commercial aviation gasoline). CAUTION Aviation gasoline (ASTM D910, Grade 80/87) is restricted to emergency use and shall not be used in excess of 1000 gallons per 100 hours of operation Aviation gasoline (ASTM D910, Grade 100/130 low lead or grade 100LL PPS EMS53122) is restricted to emergency use and shall not be used in excess of 250 gallons per 100 hours of operation. Total usage must be limited to 7000 gallons during any 3000-hour period. When mixing the above aviation gasolines, use this formula to set proportions of each grade during any overhaul period: Amount of Grade 100LL or 100/130 (gal) + Amount of Grade 80/87 (gal) < 1 7000 (gal) 30,000 (gal) If 25 percent or more Avgas is used at any time, one quart of aviation grade mineral oil must be added to the mixture per 100 gallons of Avgas. Whenever any of the above fuels or combinations of the above fuels is changed, make engine speed and power checks prior to flight. Refer to the Honeywell TPE331-12JR maintenance manual for fuel trim, which may be needed to restore speed settings and/or maximum power. Approved Fuel Additives: Fuels without icing inhibitors may have MIL-I-27686E Fuel System Icing Inhibitor, or an equivalent inhibitor, added, but not in excess of 0.15 percent by volume. CAUTION JP-4 and JP-5 fuel per MIL-T-5624 contain the correct premixed quantity of an approved type of anti-icing fuel additive and no additional anti-ice compounds should be added. If additional anti-static protection is desired, the following additives are approved for use: Shell ASA3 (up to 300 conductivity units, but the additive should not exceed 1ppm) If additional biocidal protection is desired, the following additive is permitted for use in certain conditions. Sohio Biobor JF (270ppm maximum {20 ppm of elemental boron} may be used) Fuel Capacity (S/N 20800001 thru 20800130 Not Modified With SK208-52): Total Capacity: 335 U.S. gallons. Total Capacity Each Tank: 167.5 U.S. gallons. Total Usable: 331 U.S. gallons. Fuel Capacity (S/N 20800001 thru 20800130 Modified With SK208-52 and S/N 20800131 and higher): Total Capacity: 335.6 U.S. gallons. Total Capacity Each Tank: 167.8 U.S. gallons. Total Usable: 331 U.S. gallons. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 1: General Rev. 5 1-6 November 7, 2019 FAA Approved OIL Approved Lubricants Type Oil Mil- Specification Brand Name Type II Only MIL-L-23699 Mobil Jet Oil II BP (Exxon) 2380 Turbo Oil Chevron Jet Engine Oil No. 5 Stauffer Jet II Cal Tech RPM Jet Engine Oil No. 5 Castrol 205 Castrol 5000 Aeroshell/Royco Turbine Oil 500 Aeroshell/Royco Turbine Oil 560 Mobil 254 Table 1-2, Approved Engine Lubricants Oil Grade (Specification): Oil conforming to table 1-2 must be used. Total Oil Capacity: 10 U.S. quarts (including oil in filter, cooler and hoses). Drain and Refill Quantity: Approximately 8 U.S. quarts. Oil Quantity Operating Range: Fill to between FULL or ADD on dipstick. It takes approximately 1 U.S. quart from the ADD to FULL marks on the dipstick. To get an accurate reading, it is recommended to check the level with hot oil. WARNING ENSURE OIL FILLER CAP IS SECURELY INSTALLED. OPERATING THE ENGINE WITH THE FILLER CAP LOOSE WILL RESULT IN EXCESSIVE OIL LOSS AND EVENTUAL ENGINE STOPPAGE. MAXIMUM CERTIFICATED WEIGHTS No changes to type certificated weights. Compatibility with this engine modification and the APE I gross weight increase STC SA00188SE to 8950 lbs and the APE II gross weight increase STC SA00392SE to 9062 lbs has been shown. If the aircraft has one of these STC kits installed, the aircraft can be operated at the associated gross weight under that STC, except for flight in known icing conditions. Refer to Supplement 1, Known Icing Equipment, SSL- KIS-208B-12JR, for weight limits during flight in known icing conditions. STANDARD AIRPLANE WEIGHTS Refer to new weight and balance accomplished during engine modification or later revision. Aircraft empty weights increase by approximately 90 lbs. Maximum useful loads decrease by approximately 90 lbs. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 1: General Rev. 5 1-7 November 7, 2019 FAA Approved CABIN, ENTRY, CARGO DOOR AND COMPARTMENT DIMENSIONS No changes SPECIFIC LOADINGS Wing Loading: 31.3 lbs/sq. ft. Power Loading: 9.72 lbs/shp SYMBOLS, ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS See Cessna POH/AFM METEOROLOGICAL TERMINOLOGY See Cessna POH/AFM ENGINE POWER TERMINOLOGY This section only references terms that are different from the OEM engine installation. Please reference the Cessna POH/AFM for any terms not included here. Beta Mode Beta Mode is the engine operational mode in which propeller blade pitch is controlled by the power lever. A beta light can illuminate during landing under some conditions, but is not normally used during flight. Operation below the flight idle gate is prohibited in flight. GCP GCP is the Generator Control Panel FCM FCM is the Function Control Module Hot Start Hot Start is an engine start, or attempted start, which results in an EGT exceeding 770ºC. EGT EGT signifies Exhaust Gas Temperature Max Climb Power Max Climb Power, Max Continuous Power, and Max Cruise Power Max Continuous Power all utilize the same power setting on the Honeywell TPE331-12JR Max Cruise Power as installed in the Caravan. These all equate to either 100% torque, or 650ºC EGT (SRL ON), whichever is reached first at 100% engine rpm. For SRL “off” temperatures, see Section 2, page 2-5. SRL SRL is Single Red Line relating to the maximum exhaust gas temperature for takeoff and continuous operations with the SRL system operating, which is 650ºC. Takeoff Power Takeoff Power is the same as Maximum Continuous Power in this installation. It equates to either 100% torque, or 650ºC EGT (SRL ON), whichever is reached first at 100% engine rpm and has no time limit. For SRL “off” temperatures, see Section 2, page 2-5. TTL TTL stands for Torque and Temperature Limiter Computer Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 1: General Rev. 5 1-8 November 7, 2019 FAA Approved AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY See Cessna POH/AFM WEIGHT AND BALANCE TERMINOLOGY See Cessna POH/AFM AUTOPILOT/FLIGHT DIRECTOR TERMINOLOGY See Cessna POH/AFM Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-1 November 7, 2019 FAA Approved SECTION 2: LIMITATIONS TABLE OF CONTENTS PAGE Introduction .................................................................................................. 2-2 Airspeed Limitations ..................................................................................... 2-2 Airspeed Indicator Markings ......................................................................... 2-2 Power Plant Limitations ................................................................................ 2-2 Engine Operating Limits ............................................................................... 2-4 Maximum Exhaust Gas Temperature Limits (Manual Mode) ....................... 2-5 Power Plant Instrument Markings ................................................................ 2-6 Miscellaneous Instrument Markings ............................................................. 2-6 Preflight ........................................................................................................ 2-6 Visual and Tactile Check .............................................................................. 2-6 Ignition Unit Duty Cycle ................................................................................ 2-7 Electrical Limits ............................................................................................ 2-7 Weight Limits ................................................................................................ 2-7 Center of Gravity Limits ................................................................................ 2-7 Maneuver Limits ........................................................................................... 2-7 Flight Load Factor Limits .............................................................................. 2-7 Flight Crew Limits ......................................................................................... 2-7 Kinds of Operation Limits ............................................................................. 2-7 Required Equipment..................................................................................... 2-7 Day VFR ............................................................................................ 2-7 Night VFR .......................................................................................... 2-7 IFR..................................................................................................... 2-8 Flight into Known Icing ...................................................................... 2-8 Cold Weather Operations .................................................................. 2-8 Fuel Limitations ............................................................................................ 2-8 Maximum Operating Altitude ........................................................................ 2-10 Outside Air Temperature Limits .................................................................... 2-10 Maximum Passenger Seating Limits ............................................................ 2-10 Other Limitations .......................................................................................... 2-10 Flap Limitations ................................................................................. 2-10 Type II, Type III, or Type IV Anti-ice Fluid Takeoff Limitations ..................... 2-10 Flight in Known Icing Visual Cues ................................................................ 2-10 Placards ....................................................................................................... 2-11 Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-2 November 7, 2019 FAA Approved INTRODUCTION Section 2 includes the operating limitations, instrument markings, and basic placards necessary for the safe operation of the airplane, its engine, standard systems and standard equipment. WARNING THE LIMITATIONS INCLUDED IN THIS SECTION AND IN SECTION 9 HAVE BEEN APPROVED BY THE FEDERAL AVIATION ADMINISTRATION. OBSERVATION OF THESE OPERATING LIMITATIONS IS REQUIRED BY FEDERAL AVIATION REGULATIONS. NOTE Operation in countries other than the United States may require the observance of other limitations, procedures, or performance data. Refer to Section 9 of this Airplane Flight Manual Supplement for amended operating limitations, procedures, performance data and other necessary information for supplemental systems. AIRSPEED LIMITATIONS No changes AIRSPEED INDICATOR MARKINGS No changes POWER PLANT LIMITATIONS Engine Manufacturer: Honeywell International, Inc. Engine Model Number: TPE331-12JR Engine Operating Limits: Refer to Table 2-1 Fuel Grade and Approved Fuel Additives: Refer to Fuel Limitations Oil Grade (Specification): Oil conforming to Honeywell International requirements must be used. Refer to Section 1 or 8 for a listing of approved oils. When adding oil, service the engine with the same type and brand which is currently being used in the engine. CAUTION DO NOT MIX TYPES OR BRANDS OF OIL. Propeller Manufacturer: Hartzell Propeller, Inc. Propeller Model Numbers: HC-B4TN-5QL/LT10890NK with de-ice HC-B4TN-5NL/LT10890N without de-ice HC-B4TN-5QL/LT10891NK with de-ice HC-B4TN-5NL/LT10891N without de-ice Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-3 November 7, 2019 FAA Approved Propeller Diameter: Maximum: 109.5” Minimum: 107.5” Propeller Blade Angle @ 42” station, Feathered: +81.2º Flight Idle Blade Angle: 5º ± 1.0º Reverse: -12º Propeller System Operating Limits: An overspeed fuel governor check should be made for the following reasons;  Normally, every 300 flight hours.  Prior to each flight when air starts are to be intentionally made.  Any indication of an overspeed governor malfunction.  When any maintenance or adjustments involving the engine control system have been performed. See Section 4 for instructions on conducting the overspeed governor check. Engine Control Operating Limits: Flight operation with the power lever retarded below the FLIGHT IDLE position is prohibited and may lead to loss of airplane control. Engine Starting Cycle Limits: Using airplane batteries only: 60 seconds ON- 60 seconds OFF 60 seconds ON- 60 seconds OFF 60 seconds ON- 30 minutes OFF Using airplane batteries with external power: 45 seconds ON- 120 seconds OFF 45 seconds ON- 120 seconds OFF 45 seconds ON- 60 minutes OFF CAUTION DUE TO THE POSSIBILITY OF EXCESSIVELY HIGH CURRENT SURGE DURING ENGINE START, IT IS RECOMMENDED THAT THE MAXIMUM STARTING CURRENT FROM AN EXTERNAL POWER SOURCE BE LIMITED TO 1700 AMPERES. CAUTION IT IS RECOMMENDED THAT THE START MODE SWITCH BE IN THE PARALLEL POSITION FOR ALL STARTS USING EXTERNAL POWER DUE TO THE HIGH CURRENT. DAMAGE TO THE AIRCRAFT BATTERIES CAN OCCUR USING THE PARALLEL-SERIES MODE WITH EXTERNAL POWER. NOTE The specified starter ON times assumes no ignition of fuel, but does include engine clearing time. Starter ON times may be extended if ignition of fuel occurs, but procedures listed under Battery Start in Section 4 should be observed. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-4 November 7, 2019 FAA Approved ENGINE OPERATING LIMITS Operating Condition SHP Torque (%) Max EGT (degrees C) RPM (%) Oil Press. (psig) Oil Temp. (degrees C) Fuel Pressure (psi) Starting --- --- 770 (1 sec) --- --- -40 (min) 8 Ground Idle --- --- 770 (1 sec) 68 (min) 40 (min) 127 8-20 Takeoff 900 100 650 (1) 101.0 (7) 70-120 (3) 55-110 (4) 20-80 Maximum Continuous 900 100 650 (1) 101.0 (7) 70-120 (3) 55-110 (4) 20-80 Climb 900 100 650 (1) 101.0 (7) 70-120 (3) 55-110 (4) 20-80 Cruise 900 100 650 (1) 96 to 101.0 (7) 70-120 (3) 55-110 (4) 20-80 Landing --- --- --- 93.0 (min) 70-120 (3) 55-110 (4) 20-80 Maximum Reverse --- --- 565 (1) 101.0 (7) 70-120 (3) 55-110 (4) 20-80 Transient --- 104 (5 min) 770 (1 sec) 104 (2) (6) 127 (5) 80-90 Note 1: This temperature is based on the Single Red Line (SRL) control system “ON”. With the SRL system “OFF” the maximum permissible temperatures vary as a function of ambient temperature, altitude, and other operating conditions. Refer to EGT table 2-2, Section 2, page 2-5. Note 2: Transient operation of propeller output shaft speed above 104 percent, to a maximum of 106 percent, is allowable for fuel control overspeed governor test when propeller is on the start locks. DO NOT allow the engine to windmill between 18% and 28 %. Note 3: Normal operating range above 23,000 ft.: 50-120 psig. Note 4: Oil temperature limits are for Type II oil only Note 5: The TPE331-12JR has an oil temperature limit between 110ºC and 127ºC for a maximum of 10 minutes. The normal continuous limit is 110ºC. If the 10 minute limit is exceeded, a SOAP sample is required within 25 flight hours. When at ground idle, oil temperature limit is 127ºC without a time limitation. Note 6: Transients above 120 psig can occur during cold weather starting Note 7: 101% to 101.5% for 5 minutes, 101.5% to 105.5% for 30 seconds. 105.5% to 106% for 5 seconds. If RPM time limits are exceeded, conduct power checks to determine satisfactory engine performance. Record the time in excess of time limits in engine logbook. If 5 second time limit or 106% is exceeded, remove engine. Table 2-1, Engine Operating Limits Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-5 November 7, 2019 FAA Approved Honeywell TPE331-12JR Manual Mode (SRL “OFF” or INOP) EGT Table OAT (ºC) SRL “OFF” EGT @ 100%RPM (ºC) SRL “OFF” EGT @ 96%RPM (ºC) -60 556 535 -55 558 537 -50 559 539 -45 561 540 -40 563 542 -35 564 544 -30 566 546 -25 568 547 -20 569 549 -15 574 551 -10 578 552 -5 582 554 0 587 556 5 591 557 10 595 561 15 600 565 20 604 569 25 608 574 30 613 578 35 617 582 40 622 587 45 626 591 50 630 596 55 635 600 60 639 605 Table 2-2, Maximum Exhaust Gas Temperature Limits (Manual Mode) Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-6 November 7, 2019 FAA Approved POWER PLANT INSTRUMENT MARKINGS Instrument Red Line Green Arc Yellow Arc Red Line Minimum Limit Normal Operating Caution Range Maximum Limit Torque Indicator --- 0-100% --- 100% Exhaust Gas Temperature (EGT) Indicator (2) --- --- --- 650ºC (1) Engine % RPM Indicator --- 68-85% 92-100% 85-92% 100-101% 101% Oil Pressure Indicator 40 psi 70-120 psi 40-70 psi (4) 120 psi Oil Temperature Indicator -40ºC 55-110ºC -40-55ºC 110-127ºC 127ºC Fuel Pressure 8 psi Narrow 8-20 psi (3) Wide 20-80 psi 80-90 psi 90 psi 1) This temperature is based on the Single Red Line (SRL) control system “ON”. With the SRL system “OFF” the maximum permissible temperatures vary as a function of ambient temperature, altitude, and other operating conditions. Refer to EGT table 2-2, Section 2, page 2-5. 2) The EGT indicator incorporates a red triangle at 770ºC and the letters “SL” to indicate the start limit of the engine. 3) The fuel pressure indicator has a narrow green band between 8-20 psi and a white line from 8-20 psi in the outer ring with the letters “GI” to signify that those pressures are only allowed during ground idle operation. The minimum in flight is 20 psi. 4) The oil pressure indicator has a white line from 40-70 psi in the outer ring with the letters “GI” to signify that those pressures are only allowed during ground idle operation. Figure 2-1, Power Plant Instrument Markings MISCELLANEOUS INSTRUMENT MARKINGS Instrument Red Line Green Arc Yellow Arc Red Line Minimum Limit Normal Operating Caution Range Maximum Limit Propeller Anti-ice Ammeter --- 24-28 amps --- --- Figure 2-2, Power Plant Instrument Markings PREFLIGHT No changes. VISUAL AND TACTILE CHECK No changes Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-7 November 7, 2019 FAA Approved IGNITION UNIT DUTY CYCLE The ignition unit can be used continuously with no limitation. ELECTRICAL LIMITS The Unison 300SG119Q starter/generator is limited to a continuous load of 200 amps on the ground and 225 amps from sea level to FL180. From FL180 to FL250, the maximum continuous load is limited to 200 amps. The Goodrich 23079-000-1 starter/generator is limited to a continuous load of 200 amps on the ground and 300 amps from sea level to FL180. From FL180 to FL250, the maximum continuous load is limited to 250 amps. WEIGHT LIMITS Maximum Ramp Weight: 8785 lbs* Maximum Ramp Weight: 8750 lbs* Maximum Landing Weight: 8500 lbs Maximum Weight for Flight into Known Icing Conditions: Cargo Pod ON: 8550 lbs Cargo Pod OFF: 8750 lbs * Compatibility with this engine modification and the APE I gross weight increase STC SA00188SE to 8950 lbs and the APE II gross weight increase STC SA00392SE to 9062 lbs has been shown. If the aircraft has one of the gross weight STC kits installed, the aircraft can be operated at the associated gross weight under that STC. CENTER OF GRAVITY LIMITS, MANEUVER LIMITS, FLIGHT LOAD FACTOR LIMITS & FLIGHT CREW LIMITS No changes. KINDS OF OPERATION LIMITS This airplane is equipped for day VFR, and may be equipped for night VFR and/or IFR operations and for flight into known icing conditions. The operating limitations placard reflects the limits applicable at the time of Airworthiness Certificate issuance. The following equipment list identifies the systems and equipment that are required instead/or beyond those required in the Cessna POH/AFM. REQUIRED EQUIPMENT The following equipment is required in place of the required OEM equipment. All other equipment listed in the OEM flight manual is still required. DAY VFR:  Operational engine inlet anti-ice system in place of the OEM inertial separator system  EGT indicator in place of the OEM ITT indicator  Engine % RPM indicator in place of the OEM Ng% RPM and Propeller RPM Indicator NIGHT VFR: No changes. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-8 November 7, 2019 FAA Approved IFR: No changes. FLIGHT INTO KNOWN ICING: Same required equipment as for unmodified Cessna 208B with addition of heated engine inlet anti-ice system. The aircraft is limited to a maximum of 10 degrees flaps in icing conditions or when ice remains on the aircraft after encountering icing conditions. Refer to Supplement S1, Known Icing Equipment, SSL-KIS-208B-12JR, for other limitations and differences for the modified Cessna 208B. COLD WEATHER OPERATIONS: No changes. FUEL LIMITATIONS Two Standard Tanks: Total Fuel, Both Tanks: 335.6 U.S. gallons Each Tank: 167.8 U.S. gallons Usable Fuel, Both Tanks On: 331 U.S. gallons Single Tank On: 164 U.S. gallons per tank Unusable Fuel Both Tanks On: 4.7 U.S. gallons Single Tank On: 3.9 U.S. gallons per tank NOTE To achieve full capacity, fill the fuel tank to the top of the filler neck. Filling fuel tanks to the bottom of the fuel filler collar (level with the flapper valve) allows space for thermal expansion and results in a decrease in fuel capacity of four gallons per side (eight gallons total). With low fuel reserves (FUEL LOW annunciator(s) ON), continuous uncoordinated flight with the turn and bank “ball” more than one-quarter ball out of center position is prohibited. Unusable fuel quantity increases when more severe sideslip is maintained. Due to possible fuel starvation, maximum full rudder sideslip duration time is two minutes. Maximum fuel imbalance in flight is 200 lbs. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-9 November 7, 2019 FAA Approved Approved Fuel Grade (Specification) and Fuel Additives: FUEL GRADE SPEC (1) MIN FUEL TEMP FOR TAKEOFF(2) MAXIMUM OPERATING ALT. (No boost pump unless specified) JET A JET A-1 JET B JP-4 JP-5 JP-8 AVIATION GASOLINE -ALL GRADES (3) ASTM-D1655 ASTM-D1655 ASTM-D1655 MIL-T-5624 MIL-T-5624 MIL-T-83133A 80/87 100/130 -35ºC -40ºC -45ºC -54ºC -40ºC -40ºC -54ºC -54ºC 25,000 FT 25,000 FT 9,500 FT 9,500 FT 25,000 FT 25,000 FT 9,000 FT (see note 3) 9,000 FT (see note 3) 1) Fuels without icing inhibitors may have MIL-I-27686E Fuel System Icing Inhibitor, or an equivalent inhibitor, added, but not in excess of 0.15 percent by volume. CAUTION JP-4 AND JP-5 FUEL PER MIL-T-5624 AND JP-8 FUEL PER MIL-T-83133A CONTAIN THE CORRECT PREMIXED QUANTITY OF AN APPROVED TYPE OF ANTI-ICING FUEL ADDITIVE AND NO ADDITIONAL ANTI-ICE COMPOUNDS SHOULD BE ADDED. 2) Minimum starting temperature is that given or the minimum allowable oil temperature (-40ºC), whichever is warmer. NOTE Starts may be attempted with fuel at lower temperatures providing other specified engine limitations are not exceeded. 3) When using aviation gasoline, the maximum fuel and ambient temperature for takeoff is 29ºC (85ºF) and the maximum operating altitude is 9000 feet. The boost pump must be ON for all flight operations. Table 2-4, Approved Fuel Grade and Fuel Additives Alternate/Emergency Fuels Aviation Fuel (All grades of military and commercial aviation gasoline). CAUTION AVIATION GASOLINE (ASTM D910, GRADE 80/87) IS RESTRICTED TO EMERGENCY USE AND SHALL NOT BE USED IN EXCESS OF 1000 GALLONS PER 100 HOURS OF OPERATION. AVIATION GASOLINE (ASTM D910, GRADE 100/130 LOW LEAD OR GRADE 100LL PPS EMS53122) IS RESTRICTED TO EMERGENCY USE AND SHALL NOT BE USED IN EXCESS OF 250 GALLONS PER 100 HOURS OF OPERATION. TOTAL USAGE MUST BE LIMITED TO 7000 GALLONS DURING ANY 3000-HOUR PERIOD. WHEN MIXING THE ABOVE AVIATION GASOLINES, USE THIS FORMULA TO SET PROPORTIONS OF EACH GRADE DURING ANY OVERHAUL PERIOD: AMOUNT OF GRADE 100LL OR 100/130 (GAL) + AMOUNT OF GRADE 80/87 (GAL) < 1 7000 (GAL) 30,000 (GAL) IF 25 PERCENT OR MORE AVGAS IS USED AT ANY TIME, ONE QUART OF AVIATION GRADE MINERAL OIL MUST BE ADDED TO THE MIXTURE PER 100 GALLONS OF AVGAS. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-10 November 7, 2019 FAA Approved WHENEVER ANY OF THE ABOVE FUELS OR COMBINATIONS OF THE ABOVE FUELS IS CHANGED, MAKE ENGINE SPEED AND POWER CHECKS PRIOR TO FLIGHT. REFER TO THE HONEYWELL TPE331-12JR MAINTENANCE MANUAL FOR FUEL TRIM, WHICH MAY BE NEEDED TO RESTORE SPEED SETTINGS AND/OR MAXIMUM POWER. Other Approved Fuel Additives: If additional anti-static protection is desired, the following additives are approved for use: Shell ASA3 (up to 300 conductivity units, but shall the additive should not exceed 1ppm) If additional biocidal protection is desired, the following additive is permitted for use in certain conditions. Sohio Biobor JF (270ppm maximum {20 ppm of elemental boron} may be used) MAXIMUM OPERATING ALTITUDE No changes. OUTSIDE AIR TEMPERATURE LIMITS No changes. MAXIMUM PASSENGER SEATING LIMITS No changes. OTHER LIMITATIONS FLAP LIMITATIONS Approved flap range in icing conditions ......................................... 0º to 10º TYPE II, TYPE III, OR TYPE IV ANTI-ICE FLUID TAKEOFF LIMITATIONS No changes. FLIGHT IN KNOWN ICING VISUAL CUES (As Required by AD 96-09-15, Paragraph (a) (1)) No changes. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 2: Limitations Rev. 5 2-11 November 7, 2019 FAA Approved PLACARDS- In addition to OEM placards 1. On the electrical junction box next to the external power plug: 2. On the instrument panel next to the torque gauge: 3. On the oil tank next to the filler cap: Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-1 November 7, 2019 FAA Approved SECTION 3: EMERGENCY PROCEDURES TABLE OF CONTENTS Page Introduction .................................................................................................. 3-3 Airspeeds for Emergency Operation ........................................................... 3-3 OPERATIONAL CHECKLISTS Engine Failures ............................................................................................ 3-4 Engine Failure during Takeoff Roll........................................................................... 3-4 Engine Failure Immediately After Takeoff ................................................................ 3-4 Engine Failure during Flight ..................................................................................... 3-4 Engine Flameout during Flight ................................................................................. 3-5 Airstart .................................................................................................... 3-5 Airstart from Feather or Wind-milling below 60% .................................................... 3-5 Forced Landings .......................................................................................... 3-7 Emergency Landing without Engine Power ............................................................. 3-7 Precautionary Landing with Engine Power .............................................................. 3-7 Ditching .................................................................................................................... 3-7 Smoke and Fire ............................................................................................ 3-8 Engine Fire In Flight ................................................................................................. 3-8 Electrical Fire in Flight .............................................................................................. 3-8 Cabin Fire ................................................................................................................. 3-9 Wing Fire .................................................................................................................. 3-9 Cabin Fire during Ground Operations ...................................................................... 3-10 Engine Fire during Start On Ground ........................................................................ 3-10 Icing .......................................................................................................... 3-11 Weather Conditions Conducive to Severe In-Flight Icing ........................................ 3-11 Procedures for Exiting the Severe Icing Environment ............................................. 3-11 Inadvertent Icing Encounter ..................................................................................... 3-11 Static Source Blockage ............................................................................................ 3-12 Engine Malfunctions ..................................................................................... 3-13 Loss of Oil Pressure ................................................................................................. 3-13 Fuel Control Malfunction .......................................................................................... 3-13 Engine Inlet Anti-Ice and Continuous Ignition ......................................................... 3-13 Non-Responsive Power Lever ................................................................................. 3-13 Gear Box Contamination .......................................................................................... 3-13 Fuel System Malfunction/Inadvertent Fuel Flow Interruption Procedures .... 3-14 Loss of Fuel Pressure .............................................................................................. 3-14 Fuel Flow Interruption to Fuel Reservoir .................................................................. 3-14 Fuel Tank Selector Off During Engine Start ............................................................ 3-14 Fuel Level Low with Single Tank Selected .............................................................. 3-14 Flap System Malfunction Procedures ........................................................... 3-15 Asymmetric Flap Extension or Sudden Flap Retraction On One Side .................... 3-15 Flaps Fail To Extend or Retract ............................................................................... 3-15 Landing Gear Malfunction Procedures ......................................................... 3-16 Landing with Flat Main Tire ...................................................................................... 3-16 Landing with Flat Nose Tire ..................................................................................... 3-16 Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-2 November 7, 2019 FAA Approved Electrical Power Supply System Malfunctions .............................................. 3-16 Generator Failure ..................................................................................................... 3-16 Inverter Failure ......................................................................................................... 3-17 Starter Contactor Does Not Disengage After Engine Start ...................................... 3-17 Emergency Descent Procedures .................................................................. 3-18 Rough Air ................................................................................................................. 3-18 Smooth Air ............................................................................................................... 3-18 Inadvertent Opening of Airplane Doors in Flight ........................................... 3-18 Upper Half of Cargo Door or Upper Half of Passenger Airstair Door Open ............ 3-18 Lower Half of Passenger Airstair Door Open ........................................................... 3-18 Right or Left Crew Doors Open ................................................................................ 3-18 Cargo Pod Door(s) Open ......................................................................................... 3-18 AMPLIFIED PROCEDURES Engine Failure .............................................................................................. 3-19 Maximum Glide Distance Chart .................................................................... 3-20 Forced Landings .......................................................................................... 3-21 Landing Without Elevator Control ................................................................. 3-22 Smoke And Fire ........................................................................................... 3-22 Emergency Operation in Clouds .................................................................. 3-23 Inadvertent Flight into Icing Conditions ........................................................ 3-23 Static Source Blocked ....................................................................... 3-23 Spins .................................................................................................... 3-23 Engine Malfunctions ..................................................................................... 3-24 Loss of Oil Pressure ................................................................................................. 3-24 Fuel Control Unit Malfunction ................................................................................... 3-24 Non-Responsive Power Lever …………………………………………………………. 3-24 Propeller Control Malfunction…………………………………………………………… 3-24 Gear Box Contamination .......................................................................................... 3-24 Fuel System Malfunction/Inadvertent Fuel Flow Interruption Procedures .... 3-25 Electrical Power Supply System Malfunctions .............................................. 3-25 Generator or Main Bus Malfunctions ....................................................................... 3-25 Loss of Electrical Power ........................................................................................... 3-26 Partial Avionics Power Failure ................................................................................. 3-26 Standby Electrical System Malfunctions .................................................................. 3-26 Inadvertent Opening of Airplane Doors in Flight ........................................... 3-27 Emergency Exits .......................................................................................... 3-27 Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-3 November 7, 2019 FAA Approved 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. Enroute weather emergencies can be minimized or eliminated by careful flight planning and good judgment when unexpected weather is encountered. However, should an emergency arise, the basic procedures described in this section should be considered and applied as necessary to correct the problem. Emergency procedures associated with ELT and other supplemental systems can be found in Section 9 of the Cessna POH/AFM. Emergency procedures relating to Known Icing Equipment and the Standby Alternator System can be found in Section 9 of this airplane flight manual supplement. WARNING THERE IS NO SUBSTITUTE FOR PROPER AND COMPLETE PREFLIGHT PLANNING HABITS AND THEIR CONTINUAL REVIEW IN MINIMIZING EMERGENCIES. BE THOROUGHLY KNOWLEDGEABLE OF HAZARDS AND CONDITIONS WHICH REPRESENT POTENTIAL DANGERS, AND BE AWARE OF THE CAPABILITIES AND LIMITATIONS OF THE AIRPLANE. AIRSPEEDS FOR EMERGENCY OPERATION Engine Failure after Takeoff: Wing Flaps Up……………………………………………………………..100 KIAS Wing Flaps Down…………………………………………………………. 80 KIAS Maneuvering Speed: 8750 Pounds…………………………………………………………….....148 KIAS 7500 Pounds…………………………………………………………….....137 KIAS 6250 Pounds…………………………………………………………….....125 KIAS 5000 Pounds………………………………………………………….........112 KIAS Maximum Glide: With Cargo Pod Without Cargo Pod 9062 Pounds………………………..96 KIAS……………………………98 KIAS 8750 Pounds………………………. 95 KIAS……………………………97 KIAS 7500 Pounds………………………..87 KIAS……………………………90 KIAS 6250 Pounds………………………..79 KIAS……………………………82 KIAS 5000 Pounds………………………..71 KIAS……………………………74 KIAS Precautionary Landing with Engine Power, Flaps Down……………………….80 KIAS Landing Without Engine Power: Wing Flaps Up……………………………………………………………...100 KIAS Wing Flaps Down…………………………………………………………...80 KIAS NOTE This section contains all emergency procedures that are in the basic airplane flight manual. These procedures are revised as necessary or expanded to reflect aircraft changes resulting from this modification. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-4 November 7, 2019 FAA Approved OPERATIONAL CHECKLISTS Procedures in the Operational Checklists portion of this section shown in bold-faced type are immediate- action items which should be committed to memory ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF ROLL 1. Power Lever – BETA range. 2. Brakes – APPLY. 3. Wing Flaps – RETRACT. If airplane cannot be stopped on remaining runway: 4. Fuel Shutoff/Feather Lever – SHUTOFF/FEATHER. 5. Ignition Switch- OFF. 6. Fuel Valve Switch – OFF. 7. Fuel Shutoff – OFF (pull out). 8. Fuel Tank Selectors – OFF (warning horn will sound). 9. Battery Switch – OFF. ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF 1. Airspeed – 85 KIAS with 20º flaps. 2. Fuel Shutoff/Feather Lever – SHUTOFF/FEATHER. 3. Ignition Switch- OFF. 4. Wing Flaps – FULL DOWN. 5. Fuel Valve Switch – OFF. 6. Fuel Shutoff – OFF (pull out). 7. Fuel Tank Selectors – OFF (warning horn will sound). 8. Battery – OFF. ENGINE FAILURE DURING FLIGHT (No re-start will be attempted) 1. Airspeed – 95 KIAS 2. Fuel Shutoff/Feather Lever – SHUTOFF/FEATHER. 3. Wing Flaps – UP 4. Fuel Boost Switch – OFF. 5. Fuel Shutoff – OFF (pull out). 6. Ignition Switch – OFF 7. Standby Power Switch (if installed) – OFF 8. Electrical Load – REDUCE as follows: A. Avionics Bus 2 Switch – OFF. B. Flashing Beacon – OFF. C. Strobe Lights – OFF. D. Ice Protection (if installed) – CONSIDER (if pitot heat is required, pull the RIGHT PITOT HEAT circuit breaker and turn pitot heat switch ON). E. Vent Fans – OFF. F. GEN FIELD circuit breaker – PULL (top row, last breaker on forward end). G. Autopilot Circuit Breaker – PULL (third row from bottom, second from forward end). 9. Landing – Refer to Emergency Landing Without Engine Power checklist in the Forced Landings section. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-5 November 7, 2019 FAA Approved ENGINE FLAMEOUT DURING FLIGHT 1. If Engine RPM Is Above 60%: a) Power Lever – ½ inch forward of FLIGHT IDLE b) Ignition Switch – CONT c) Power Lever – AS DESIRED after satisfactory relight as evidenced by normal EGT and RPM. d) Ignition Switch – AUTO if cause of flameout has been corrected. 2. If Engine RPM is Below 60%: a) Fuel Valve Switch – OFF b) Refer to Airstart checklists for engine restart. AIRSTART WARNING IF AN ENGINE HAS BEEN SHUT DOWN BECAUSE OF AN OBVIOUS FAILURE, AS INDICATED BY THE ENGINE INSTRUMENTS OR EXCESSIVE VIBRATION, AN AIRSTART SHOULD NOT BE ATTEMPTED. AN AIRSTART FROM FEATHER SHOULD NOT BE ATTEMPTED BELOW 1000 FEET ABOVE GROUND LEVEL (AGL) DUE TO THE TIME AND ALTITUDE REQUIRED FOR RESTART. PILOT SHOULD PREPARE FOR EMERGENCY LANDING WITHOUT ENGINE POWER. CAUTION DO NOT ENGAGE THE STARTER DURING AN AIR START BECAUSE THE HIGH TORQUE REQUIREMENTS OF A FEATHERED PROPELLER MAY DAMAGE THE STARTER. DO NOT ATTEMPT AN AIRSTART FROM FEATHER WITH THE FUEL SHUTOFF/FEATHER LEVER IN THE SHUTOFF/FEATHER POSITION AS ALL THE OIL FROM THE TANK WILL BE PUMPED INTO THE ENGINE SUMP MAKING AN AIRSTART IMPOSSIBLE. AIRSTART FROM FEATHER or WIND-MILLING below 60% 1. Ground/Air Switch- AIR. 2. Standby Power Switch (if installed) – OFF. 3. Avionics Power Switches – OFF. 4. SRL Switch – ON (or OFF for manual airstart or if SRL INOP). NOTE Engine will not automatically re-light during the airstart if the SRL computer speed switch has failed or the SRL switch is in the “OFF” position. 5. Air Conditioner (if installed) – OFF. 6. Bleed Air Heat Switch – OFF. 7. Engine Inlet Anti-ice Switch – OFF. 8. Power Lever – ½ inch forward of FLIGHT IDLE. 9. Speed Lever – MIN RPM (approx. 96%). 10. Fuel Shutoff/Feather Lever – NORM. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-6 November 7, 2019 FAA Approved AIRSTART (continued) AIRSTART FROM FEATHER or WIND-MILLING below 60% (continued) 11. Fuel Shutoff – ON (push in). 12. Fuel Tank Selectors – LEFT ON, RIGHT ON. 13. Battery Switch – ON. 14. Fuel Boost Switch – ON (check AUX FUEL PUMP ON annunciator ON, FUEL PRESS LOW annunciator OFF). 15. Fuel Valve Switch – RUN. 16. Altitude – 20,000 feet maximum. 17. Airspeed – 90 KIAS minimum. 18. Start Switch- START. 19. RPM Indicator – RISING. NOTE The propeller unfeathering pump will begin unfeathering the propeller and engine rpm should begin to rise. At 10% rpm, ignition, fuel flow, and light-off should occur automatically with SRL “ON”. If no fuel flow occurs at 10% (or conducting a manual air-start), move the FUEL VALVE switch to the “ON/ENRICH” position momentarily and check for fuel flow, ignition, and light off. Modulate FUEL VALVE to the “ON/ENRICH” position if necessary to help accelerate the engine during manual starts. Monitor EGT. When rpm reaches 10%: 20. Fuel Valve Switch- ON/ENRICH momentarily (Automatic with SRL-“ON”). a) EGT – MONITOR (770ºC maximum for one second). b) RPM – Increasing at least 1% per second to propeller governor setting. When rpm reaches 60% 21. Start Switch – OFF. When rpm reaches approx 96% rpm on propeller governor 22. Speed Lever - AS REQUIRED. 23. Power Lever - AS REQUIRED. 24. Ignition Switch – AUTO unless conditions warrant use of CONT. WARNING IF CONDITIONS EXIST, SUCH AS HEAVY PRECIPITATION OR NEARLY EMPTY FUEL TANKS, TURN THE IGNITION SWITCH TO CONT. 25. Fuel Boost Switch – NORM (unless it cycles on and off, then leave ON). 26. Generator Switch – ON. 27. Standby Power Switch (if installed) – ON. 28. Engine Inlet Anti-ice Switch – AS REQUIRED. 29. Electrical and Avionics Equipment – AS REQUIRED. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-7 November 7, 2019 FAA Approved FORCED LANDINGS EMERGENCY LANDING WITHOUT ENGINE POWER 1. Seats, Seat Belts, Shoulder Harnesses – SECURE. 2. Airspeed – 100 KIAS (flaps UP). 80 KIAS (flaps DOWN). 3. Fuel Shutoff/Feather Lever – SHUTOFF/FEATHER. 4. Fuel Valve – OFF. 5. Fuel Boost Switch – OFF. 6. Ignition Switch – OFF. 7. Standby Power Switch (if installed) – OFF. 8. Non-essential Equipment (if installed) – OFF. 9. Fuel Shutoff – OFF (pull out). 10. Fuel Tanks Selectors – OFF (warning horn will sound). 11. Crew Doors – UNLATCH PRIOR TO TOUCHDOWN. 12. Battery Switch – OFF when landing is assured. 13. Touchdown – SLIGHTLY TAIL LOW. 14. Brakes – APPLY HEAVILY. PRECAUTIONARY LANDING WITH ENGINE POWER 1. Seats, Seat Belts, Shoulder Harnesses – SECURE. 2. Wing Flaps - 10º. 3. Airspeed – 90 KIAS. 4. Selected Field – FLY OVER, noting terrain and obstructions. 5. All Electrical Switches (except Battery and Generator) – OFF. 6. Wing Flaps- FULL DOWN (on final approach). 7. Airspeed – 80 KIAS. 8. Crew Doors – UNLATCH PRIOR TO TOUCHDOWN. 9. Generator Switch – OFF. 10. Battery Switch – OFF. 11. Touchdown – SLIGHTLY TAIL LOW. 12. Fuel Shutoff/Feather Lever – SHUTOFF/FEATHER. 13. Brakes – APPLY HEAVILY. DITCHING NO CHANGES FROM CESSNA RECOMMENDED PROCEDURES. WARNING THE AIRPLANE HAS NOT BEEN FLIGHT TESTED IN ACTUAL DITCHINGS, THUS THE ABOVE RECOMMENDED PROCEDURE IS BASED ENTIRELY ON THE BEST JUDGMENT OF SUPERVAN SYSTEMS LTD. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-8 November 7, 2019 FAA Approved SMOKE AND FIRE ENGINE FIRE IN FLIGHT (Red ENGINE FIRE Annunciator ON or OFF) 1. Power Lever – IDLE. 2. Fuel Valve Switch – OFF. 3. Fuel Shutoff/Feather Lever – SHUTOFF/FEATHER. 4. Fuel Shutoff – OFF. 5. Cabin Heat Firewall Shutoff Control – PULL OFF. 6. Forward Side Vents – CLOSE. 7. Overhead Vents – OPEN. 8. Ventilation Fans (if installed) – ON. 9. Wing Flaps - 20º- 30º. 10. Airspeed – 80-85 KIAS. 11. Forced landing – EXECUTE (as described in Emergency Landing Without Engine Power). ELECTRICAL FIRE IN FLIGHT 1. Battery Switch – OFF. 2. Generator Switch – OFF. 3. Standby Power Switch (if installed) – OFF. WARNING WITHOUT ELECTRICAL POWER, ALL ELECTRICALLY-OPERATED GYROS AND ENGINE INSTRUMENTS, SRL COMPUTER, TORQUE/TEMPERATURE LIMITER, FUEL BOOST PUMP, ANNUNCIATOR LIGHTS, WING FLAPS AND ALL AVIONICS WILL BE INOPERATIVE. VACUUM-DRIVEN GYROS WILL STILL BE OPERATIVE. (FOR AIRPLANES WITH A KFC-150 AUTOPILOT OR KFC-225 AUTOPILOT, VACUUM-DRIVEN GYROS ARE THE PILOT’S HORIZON GYRO AND RIGHT-HAND DIRECTIONAL GYRO. FOR AIRPLANES WITH A KFC-250 AUTOPILOT, VACUUM-DRIVEN GYROS ARE THE RIGHT-HAND HORIZON AND DIRECTIONAL GYROS.) 4. Vents – CLOSED (to avoid drafts). 5. Bleed Air Heat Switch – OFF. 6. Hand Fire Extinguisher – ACTIVATE. WARNING OCCUPANTS SHOULD USE OXYGEN MASKS (IF INSTALLED) UNTIL SMOKE CLEARS. AFTER DISCHARGING AN EXTINGUISHER WITHIN A CLOSED CABIN, VENTILATE THE CABIN. 7. Avionics Power Switches – OFF. 8. All Other Electrical Switches – OFF. WARNING LAND THE AIRPLANE AS SOON AS POSSIBLE. DO NOT ATTEMPT TO TROUBLE-SHOOT ELECTRICAL PROBLEMS IN FLIGHT. If fire appears out and electrical power is absolutely necessary for continuance of flight, only restore power to equipment essential for flight: 9. Bus 1 Pwr and Bus 2 Pwr Circuit Breakers – PULL (6 total- first circuit breaker on each row) 10. Battery Switch and Standby Power Switch (if installed) – ON. 11. Generator Switch – ON. 12. Circuit Breakers – CHECK for faulty circuit (open circuit breaker); DO NOT reset. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-9 November 7, 2019 FAA Approved SMOKE AND FIRE (continued) ELECTRICAL FIRE IN FLIGHT (continued) 13. Bus 1 Pwr and Bus 2 Pwr Circuit Breakers- PUSH one at time with delay after each until short circuit is localized. Leave that Bus Pwr circuit breaker PULLED if necessary. 14. Inverter Switch (if installed) – 1 or 2. 15. Radio Switches – OFF. 16. Avionics Power Switches – ON. 17. Radio and Electrical Switches – ON one at a time, with delay after each until short circuit is localized. 18. Vents – OPEN when it is ascertained that fire is completely extinguished. 19. Bleed Air Heat – ON if necessary. 20. Land the airplane as soon as possible. CABIN FIRE 1. Battery Switch – OFF. 2. Generator Switch – OFF. WARNING WITHOUT ELECTRICAL POWER, ALL ELECTRICALLY-OPERATED GYROS AND ENGINE INSTRUMENTS, SRL COMPUTER, TORQUE/TEMPERATURE LIMITER, FUEL BOOST PUMP, ANNUNCIATOR LIGHTS, WING FLAPS AND ALL AVIONICS WILL BE INOPERATIVE. VACUUM-DRIVEN GYROS WILL STILL BE OPERATIVE. (FOR AIRPLANES WITH A KFC-150 AUTOPILOT VACUUM-DRIVEN GYROS ARE THE PILOT’S HORIZON GYRO AND RIGHT-HAND DIRECTIONAL GYRO. FOR AIRPLANES WITH A KFC- 250 AUTOPILOT, VACUUM-DRIVEN GYROS ARE THE RIGHT-HAND HORIZON AND DIRECTIONAL GYROS.) 3. Standby Power Switch (if installed) – OFF. 4. Vents – CLOSED (to avoid drafts). 5. Bleed Air Heat Switch – OFF. 6. Hand Fire Extinguisher – ACTIVATE. WARNING OCCUPANTS SHOULD USE OXYGEN MASKS (IF INSTALLED) UNTIL SMOKE CLEARS. AFTER DISCHARGING AN EXTINGUISHER WITHIN A CLOSED CABIN, VENTILATE THE CABIN. 7. Land the airplane as soon as possible. WING FIRE 1. Pitot/Static Heat Switch – OFF. 2. Stall Heat Switch – OFF. 3. Strobe Lights Switch – OFF. 4. Navigation Lights Switch – OFF. 5. Landing and Taxi Light Switches – OFF. 6. Radar (if installed) – OFF. 7. Ventilation Fans (if installed) – OFF. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-10 November 7, 2019 FAA Approved SMOKE AND FIRE (continued) WING FIRE (continued) WARNING PERFORM A SIDESLIP AS REQUIRED TO KEEP FLAMES AWAY FROM THE FUEL TANK AND CABIN. LAND THE AIRPLANE. CABIN FIRE DURING GROUND OPERATIONS 1. Power Lever – IDLE. 2. Brakes – AS REQUIRED. 3. Fuel Valve Switch – OFF. 4. Fuel Shutoff/Feather Lever – SHUTOFF/FEATHER. 5. Battery Switch – OFF. 6. Airplane – EVACUATE. 7. Fire – EXTINGUISH. ENGINE FIRE DURING START ON GROUND (Red ENGINE FIRE Annunciator ON or OFF) 1. Fuel Valve Switch –OFF. 2. Fuel Shutoff/Feather Lever – SHUTOFF/FEATHER. 3. Fuel Boost Switch – OFF. 4. Starter Mode Switch – MOTOR. CAUTION  DO NOT EXCEED THE STARTING CYCLE LIMITATIONS; REFER TO SECTION 2  SHOULD THE FIRE PERSIST, AS INDICATED BY SUSTAINED EXHAUST GAS TEMPERATURE, IMMEDIATELY CLOSE THE FIREWALL FUEL SHUTOFF AND CONTINUE MOTORING. 5. Fuel Shutoff – OFF (pull out). 6. Starter Switch – OFF. 7. Battery Switch – OFF. 8. Airplane – EVACUATE. 9. Fire – EXTINGUISH. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-11 November 7, 2019 FAA Approved ICING THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN-FLIGHT ICING (Required by AD 96-09-15, Paragraph (a) (2)): 1. Visible rain at temperatures below 0 degrees Celsius ambient air temperature. 2. Droplets that splash or splatter on impact at temperatures below 0 degrees Celsius ambient air temperature. PROCEDURES FOR EXITING THE SEVERE ICING ENVIROMENT (Required by AD 96-09-15, Paragraph (a) (2)): These procedures are applicable to all flight phases from takeoff to landing. Monitor the ambient air temperature. While severe icing may form at temperatures as cold as -18 degrees Celsius, increased vigilance is warranted at temperatures around freezing with visible moisture present. If the visual cues specified in Section 2 Limitations for identifying severe icing conditions are observed, accomplish the following: 1. Immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the severe icing conditions in order to avoid extended exposure to flight conditions more severe than those for which the airplane has been certificated. 2. Avoid abrupt and excessive maneuvering that may exacerbate control difficulties. 3. Do not engage the autopilot 4. If the autopilot is engaged, hold the control wheel firmly and disengage the autopilot. 5. If an unusual roll response or uncommanded roll control movement is observed, reduce the angle-of-attack. 6. If the flaps are extended, do not retract them until the airframe is clear of ice. 7. Report these weather conditions to Air Traffic Control. INADVERTENT ICING ENCOUNTER 1. Ignition Switch – CONT. 2. Engine Inlet Anti-ice Switch – ON. 3. PITOT/STATIC, STALL, WINDSHIELD, PROP ANTI-ICE – ON. 4. If above 20,000 feet: a) Airspeed – 160 KIAS Maximum. b) Altitude – DESCEND to 20,000 feet or below as soon as practical. 5. Turn back or change altitude to obtain an outside air temperature that is less conducive to icing. 6. Ignition Switch – AUTO after 5 minutes operations. 7. Bleed Air Heat Switch and Temp Control – ON and ADJUST 8. Push Fwd Cabin Heat control full in and pull Defrost control full out to obtain maximum windshield defroster effectiveness. 9. Speed Lever – INCREASE to 100% RPM to minimize ice build-up. CAUTION IF EXCESSIVE VIBRATION IS NOTED, MOMENTARILY REDUCE PROPELLER RPM TO 96% WITH THE SPEED LEVER, THEN RAPIDLY MOVE THE CONTROL FULL FORWARD. CYCLING THE RPM FLEXES THE PROPELLER BLADES AND HIGH RPM INCREASES CENTRIFUGAL FORCE, CAUSING ICE TO SHED MORE READILY. 10. If icing conditions are unavoidable, plan a landing at the nearest airport. With an extremely rapid ice build-up, select a suitable “off airport” landing site. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-12 November 7, 2019 FAA Approved ICING (continued) INADVERTENT ICING ENCOUNTER (continued) 11. With an ice accumulation of ¼ inch or more on the wing leading edges, be prepared for a significantly higher power requirement, approach speed, stall speed, and longer landing roll. 12. If necessary, set up a forward slip for visibility through the left portion of the windshield during the landing approach. 13. Use a minimum approach speed of 110 KIAS, select the minimum flap setting required, and maintain extra airspeed consistent with available field length. With ice suspected on the airframe, or operating at 5ºC (41ºF) or less in visible moisture, Do Not Extend Flaps Beyond 10º for Landing. WARNING WITH HEAVY ICE ACCUMULATIONS ON THE HORIZONTAL STABILIZER LEADING EDGE, DO NOT EXTEND FLAPS WHILE ENROUTE OR HOLDING. WHEN LANDING IS ASSURED, SELECT THE MINIMUM FLAP SETTING REQUIRED, NOT TO EXCEED 10º, AND MAINTAIN EXTRA AIRSPEED CONSISTENT WITH AVAILABLE FIELD LENGTH. DO NOT RETRACT THE FLAPS ONCE THEY HAVE BEEN EXTENDED, UNLESS REQUIRED FOR GO-AROUND. THEN RETRACT FLAPS IN INCREMENTS WHILE MAINTAINING 5 TO 10 KNOTS EXTRA AIRSPEED. 14. Land on the main wheels first, avoiding a slow and high flare-out. 15. 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 takeoff power and maintain a minimum of 110 KIAS while retracting the flaps slowly in small increments. STATIC SOURCE BLOCKAGE (Erroneous Instrument Reading Suspected) 1. Static Pressure Alternate Source Valve – PULL FULL ON. NOTE The alternate static source is connected to the left-hand flight panel instruments only. 2. Refer to Section 5 of the Cessna POH/AFM for airspeed and altimeter corrections. 3. Autopilot – DISENGAGE altitude hold mode. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-13 November 7, 2019 FAA Approved ENGINE MALFUNCTIONS LOSS OF OIL PRESSURE (Red OIL PRESS LOW Annunciator ON) Oil Pressure Gage – CHECK oil pressure indication. If oil pressure gage confirms annunciator warning, proceed in accordance with Engine Failures checklists or at the discretion of the pilot and consistent with safety, continue engine operation in preparation for an emergency landing as soon as possible. FUEL CONTROL MALFUNCTION If there is an indication of improper operation of the fuel control, when possible, check the handling of the aircraft by a simulated landing flare at a safe altitude before trying to land. If unusual drag is noted that cannot be eliminated by increasing the power, it may be necessary to feather the propeller when the pilot has the runway made. ENGINE INLET ANTI-ICE AND CONTINUOUS IGNITION Engine inlet anti-ice (inlet heat) should be used during all flight in potential icing conditions. These conditions exist when flying in precipitation or visible moisture (including clouds or fog), with OAT of 5ºC (41ºF) or less. Select Ignition Switch to CONT as below: 1. During takeoff or approach, before operation in icing conditions. 2. When ice is observed shedding from the propeller and/or spinner. 3. Before applying inlet heat, when ice has accumulated. 4. Immediately, any time engine flameout occurs as a possible result of ice ingestion. NON-RESPONSIVE POWER LEVER If a lack of response to the power lever is observed: 1. Ignition switch – CONT. 2. Engine Inlet Anti-ice Switch - ON. After the engine has cleared and normal operation is observed, which occurs in approximately three minutes: 3. Engine Inlet Anti-ice – OFF. 4. Ignition Switch - AUTO. GEAR BOX CONTAMINATION (Amber CHIP DETECTOR Annunciator ON) 1. Engine Gages – CAREFULLY MONITOR engine gages for abnormal oil pressure, oil temperature or power indications. 2. If engine gages are normal, proceed to destination and determine cause of chip detector annunciator warning prior to next flight. 3. If engine gages confirm chip detector annunciator warning, proceed in accordance with Engine Failures checklists or at the discretion of pilot and consistent with safety, continue engine operation in preparation for an emergency landing as soon as possible. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-14 November 7, 2019 FAA Approved FUELS SYSTEM MALFUNCTION/INADVERTENT FUEL FLOW INTERRUPTION PROCEDURES LOSS OF FUEL PRESSURE (Amber FUEL PRESS LOW Annunciator On) 1. Fuel Boost Switch – ON 2. If FUEL PRESS LOW annunciator extinguishes: a) Carefully monitor fuel quantity and cabin odor for evidence of a fuel leak. b) Land as soon as practical and determine cause for low fuel pressure before next flight. 3. If FUEL PRESS LOW annunciator and AUX FUEL PUMP ON annunciator are illuminated: a) Carefully monitor engine gages for sign of fuel starvation. b) Land as soon as possible. FUEL FLOW INTERRUPTION TO FUEL RESERVOIR (Red RESERVOIR FUEL LOW Annunciator On) 1. Fuel Tank Selectors – LEFT ON, RIGHT ON 2. Ignition Switch – AUTO or CONT 3. Fuel Boost Switch – ON 4. If RESERVOIR FUEL LOW annunciator remains illuminated and there is usable fuel in the wing tanks: a) Carefully monitor engine gages and FUEL PRESS LOW annunciator for signs of fuel starvation. b) Land as soon as possible and determine cause of RESERVOIR FUEL LOW warning. WARNING IF THERE ARE SIGNS OF FUEL STARVATION, PREPARE FOR A FORCED LANDING (AS DESCRIBED IN EMERGENCY LANDING WITHOUT ENGINE POWER). FUEL TANK SELECTOR OFF DURING ENGINE START (Red FUEL SELECT OFF Annunciator On and Both Fuel Selector Warning Horns Activated) 1. Left and Right Fuel Tank Selectors – ON. FUEL LEVEL LOW WITH SINGLE TANK SELECTED (Red FUEL SELECT OFF And Amber LEFT Or RIGHT FUEL LOW Annunciators On and Fuel Selector Warning Horn Activated) 1. Left and Right Fuel Tank Selectors – ON (turning both fuel tank selectors ON will extinguish the red FUEL SELECT OFF annunciator and silence the warning horn). Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-15 November 7, 2019 FAA Approved FLAP SYSTEM MALFUNCTION PROCEDURES ASYMMETRIC FLAP EXTENSION OR SUDDEN FLAP RETRACTION ON ONE SIDE 1. Apply aileron and rudder to stop the roll. 2. Flap Selector – UP 3. Airspeed – SLOW to 100 KIAS or less. 4. If both flaps retract to a symmetrical setting: a) Plan a flaps up landing. b) Refer to Section 5 of the Cessna POH/AFM (notes above landing performance tables) for increase in approach speed and landing distance. 5. If both flaps cannot be retracted to a symmetrical setting: a) Land as soon as practical. b) Maintain a minimum airspeed of 90 KIAS on the approach and avoid a nose high flare on landing. FLAPS FAIL TO EXTEND OR RETRACT 1. Flap Motor and STBY Flap Motor Circuit Breakers – CHECK IN. 2. If flaps still fail to extend or retract: a) Guarded and Safetied Standby Flap Motor Switch (Overhead) – MOVE GUARD, breaking safety wire, and POSITON SWITCH TO STBY. b) Guarded and Safetied Standby Flap Motor Up/Down Switch (Overhead) – MOVE GUARD, breaking safety wire, and position switch UP or DOWN (hold switch until flaps reach desired position, except release switch before flaps reach full up or down travel). CAUTION WITH THE STANDBY FLAP SYSTEM IN USE, LIMIT SWITCHES, WHICH NORMALLY SHUT OFF THE PRIMARY FLAP MOTOR WHEN REACHING THE FLAP TRAVEL LIMITS, ARE ELECTRICALLY INACTIVATED. THEREFORE, THE PILOT MUST RELEASE THE STANDBY FLAP MOTOR UP/DOWN SWITCH BEFORE THE FLAPS REACH THEIR TRAVEL LIMIT TO PREVENT OVERLOADING AND DAMAGE TO THE FLAP SYSTEM. 3. Guarded Standby Flap Motor Switch – Leave in STBY position until after landing when maintenance action can be accomplished Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-16 November 7, 2019 FAA Approved LANDING GEAR MALFUNCTION PROCEDURES LANDING WITH FLAT MAIN TIRE 1. Airplane – FLY as desired to lighten fuel load. 2. Fuel Selectors – POSITION ONE SIDE OFF TO LIGHTEN LOAD ON SIDE OF FLAT TIRE (maximum fuel imbalance of 200 pounds). 3. Approach – NORMAL (flaps FULL). 4. Touchdown – INFLATED TIRE FIRST. Hold airplane off flat tire as long as possible with aileron control. 5. Directional Control – MAINTAIN using brake on wheel with inflated tire as required. LANDING WITH FLAT NOSE TIRE 1. Passengers and Baggage – MOVE AFT if practical (remain within approved C.G. envelope). 2. Approach – NORMAL with full flaps. 3. Touchdown – NOSE HIGH. Hold nose wheel off as long as possible during roll. 4. Brakes – MINIMUM necessary. ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS GENERATOR FAILURE (Red VOLTAGE LOW and/or Red GENERATOR OFF Annunciators On) 1. Volt/Ammeter Selector Switch – VOLTS. If voltage is near normal of 28.5 volts, assume fault in VOLTAGE LOW annunciator circuit and continue flight to destination monitoring voltage and generator output. CAUTION A RED VOLTAGE LOW WARNING FOLLOWED BY A BUS 1 OR BUS 2 CIRCUIT BREAKER OPENING MAY BE A FEEDER FAULT THAT HAS ISOLATED ITSELF. DO NOT RESET THE BREAKER. THE VOLTAGE LOW WARNING SHOULD EXTINGUISH. If voltage is less than 24.5 volts: 2. Volt/Ammeter Selector Switch – GEN and monitor ammeter. 3. If generator output is zero: A. GEN FIELD Circuit Breaker – PUSH IN. B. Generator Switch – OFF then GEN. 4. If generator output is still zero: A. Generator Switch – OFF. B. Electrical Load – REDUCE as follows: a) Avionics Bus 2 Switch – OFF b) Flashing Beacon – OFF c) Strobe Lights – OFF d) Ice Protection (if installed)– CONSIDER (if pitot heat is required, pull RIGHT PITOT HEAT circuit breaker and turn pitot heat switch on). e) Vent Fans – OFF f) Air Conditioner (if installed) – OFF g) GEN FIELD Circuit Breaker – PULL (top row, last breaker on forward end). With KFC-150 or KFC-225 Autopilot System Installed: h) A/P CONT Circuit Breaker – PULL Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-17 November 7, 2019 FAA Approved ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS (continued) GENERATOR FAILURE (Red VOLTAGE LOW and/or Red GENERATOR OFF Annunciators On) (continued) With KFC-250 Autopilot System Installed: i) A/P FD Circuit Breaker – PULL. (third row from bottom, second breaker from forward end.) To reactivate the avionics fan and the disabled section of the audio amplifier if desired: (i) Pull all AVIONICS BUS 2 circuit breakers except AVIONICS FAN and AUDIO AMP breakers (second row from bottom, last two breakers on forward end). (ii) Avionics Bus 2 Switch – On C. Flight – TERMINATE as soon as practical. NOTE If the optional Standby Electrical System is installed, the flight may be continued to destination with the GENERATOR OFF annunciator illuminated. Refer to emergency procedures of Standby Electrical System supplement in Section 9. 5. If generator output resumes: A. Volt/Ammeter Selector Switch – VOLTS and monitor voltmeter. If voltage increases past 29 volts, expect the generator to trip off again. If this occurs, turn off the nonessential radio and electrical equipment and land as soon as practical. INVERTER FAILURE (Amber INVERTER INOP Annunciator ON) (Airplanes Equipped with KFC-250 Autopilot Only) 1. Inverter Switch – SELECT other inverter. 2. Failed Inverter – REPAIR before next flight. If INVERTER INOP annunciator remains on: 3. Inverter 1 and 2 Circuit Breakers – CHECK IN. 4. If the left-hand gyros are flagged, the INVERTER INOP annunciator is correct. 5. Disregard left-hand gyros, land as soon as practical, and repair inverters. STARTER CONTACTOR DOES NOT DISENGAGE AFTER ENGINE START (Amber STARTER ENERGIZED Annunciator ON) 1. SRL Power Switch – OFF. If amber STARTER ENERGIZED light is no longer illuminated, perform normal engine shutdown and repair SRL box. If amber STARTER ENERGIZED light is still illuminated, proceed as follows: 2. Fuel Valve Switch – OFF. 3. Battery Switch – OFF 4. Auxiliary Power Unit – OFF, then DISENGAGE 5. Engine Shutdown – COMPLETE Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-18 November 7, 2019 FAA Approved EMERGENCY DESCENT PROCEDURES ROUGH AIR 1. Seats, Seat Belts, Shoulder Harnesses – SECURE 2. Power Lever – IDLE 3. Propeller Control Lever – MAX (full forward) 4. Wing Flaps – UP 5. Maneuvering speed for various weights: 8750 Pounds – 148 KIAS 7500 Pounds – 137 KIAS 6250 Pounds – 125 KIAS 5000 Pounds – 112 KIAS SMOOTH AIR 1. Seats, Seat Belts, Shoulder Harnesses – SECURE. 2. Power Lever – IDLE. 3. Propeller Control Lever – MAX (full forward). 4. Wing Flaps -- 10º. 5. Airspeed – 175 KIAS INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT UPPER HALF OF CARGO DOOR OR UPPER HALF OF PASSENGER AIRSTAIR DOOR OPEN (Red DOOR WARNING Annunciator On) 1. Airspeed – MAINTAIN LESS THAN 100 KIAS 2. Wing Flaps – FULL (wing downwash with the flaps extended will move the doors near their normally closed position). 3. If available or practical, have a second crew member go aft to close and latch door. 4. If landing is required with door open perform a normal approach and landing LOWER HALF OF PASSENGER AIRSTAIR DOOR OPEN 1. Airspeed – MAINTAIN 100 KIAS 2. Flight Controls – MANEUVER for return for landing 3. Wing Flaps – FULL. 4. Approach – NORMAL 5. Landing – SLIGHTLY TAIL LOW; avoid nose high flare RIGHT OR LEFT CREW DOORS OPEN 1. Airspeed – MAINTAIN LESS THAN 125 KIAS 2. Door – PULL CLOSED and LATCH CARGO POD DOOR(s) OPEN 1. Airspeed – MAINTAIN LESS THAN 125 KIAS 2. Land – AS SOON AS PRACTICAL a. Approach – NORMAL b. Landing – AVOID A NOSE HIGH FLARE Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-19 November 7, 2019 FAA Approved AMPLIFIED PROCEDURES The following Amplified Procedures elaborate upon information contained in the Operational Checklists portion of this section. These procedures also include information not readily adaptable to a checklist format, and material to which a pilot could not be expected to refer in resolution of a specific emergency. NOTE If a red or non-dimmable amber annunciator illuminates at night and becomes an unacceptable distraction to the pilot because of its brightness level, it may be extinguished for the remainder of the flight by pushing in on the face of the light assembly and allowing it to pop out. To reactivate the annunciator, pull the light assembly out slightly and push back in. For further details, refer to Section 7, Annunciator Panel. ENGINE FAILURE If an engine failure occurs during the takeoff roll, 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. Prompt lowering of the nose to maintain airspeed and establish a glide attitude is the first response to an engine failure after takeoff. Feathering the propeller substantially reduces drag, thereby providing increased glide distance. In most cases, the landing should be planned straight ahead with only small changes in direction to avoid obstructions. Altitude and airspeed are seldom sufficient to execute a 180º gliding turn necessary to return to the runway. The checklist procedures assume that adequate time exists to secure the fuel and electrical systems prior to touchdown. After an engine failure in flight, the best glide speed as shown in Figure 3-1 should be established as quickly as possible. Propeller feathering is dependent on existing circumstances and is at the discretion of the pilot. Maximum RPM selection will provide increased engine wind milling speed for emergency restarts. On the other hand, to obtain the maximum glide, the propeller must be feathered. While gliding toward a suitable landing area, an effort should be made to identify the cause of the power loss. An engine failure might be identified by abnormal temperatures, mechanical noises or high vibration levels in conjunction with the power loss. A flameout will be noticed by a drop in EGT, torque, and RPM. CAUTION DO NOT ATTEMPT TO RESTART AN ENGINE THAT IS DEFINITELY KNOWN TO HAVE HAD A MECANICAL FAILURE. A flameout may result from the engine running out of fuel, or possibly may be caused by unstable engine operation. Once the fuel supply has been restored to the engine or cause of unstable engine operation eliminated, the engine may be restarted. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-20 November 7, 2019 FAA Approved Figure 3-1, Maximum Glide BEST GLIDE SPEED WEIGHT (LBS) KIAS (WITH CARGO POD) KIAS (WITHOUT CARGO POD) 9062 8750 7500 6250 5000 96 95 87 79 71 98 97 90 82 74 The best airstart technique is to initiate the relight procedure immediately after a flameout occurs, provided the pilot is certain that the flameout was not the result of some malfunction that might make it hazardous to attempt a relight. Regardless of airspeed or altitude, there is always the possibility that the engine may light up successfully just as soon as the ignition is turned on. In an emergency, turn on the ignition just as soon as possible after a flameout, provided the engine speed has not dropped below 60%. Under these circumstances, it is not necessary to shut off the fuel or feather the propeller. The power lever, however, should be retarded to IDLE position. If a flameout has occurred and the engine speed has dropped below 60%, the fuel valve switch should be moved to the OFF position before an airstart is attempted. CAUTION THE PILOT SHOULD DETERMINE THE REASON FOR POWER LOSS BEFORE ATTEMPTING AN AIRSTART. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-21 November 7, 2019 FAA Approved Propeller feathering is dependent on circumstances and is at the discretion of the pilot. However, if engine oil pressure drops below 40 psi, the engine should be shut down and the propeller should be feathered unless a greater emergency exists. Typically, as oil pressure decreases, propeller control may become an issue necessitating engine shutdown. If an airstart is to be attempted, follow the checklist procedures. Wind-milling air starts utilizing the propeller unfeathering pump are the only type of airstart available. Attempting a starter-assisted airstart can shear the starter shaft due to the high torque loads of a feathered propeller. Successful air starts may be achieved at all airspeeds above 90 kts from sea level up to an altitude of 20,000 feet. However, start temperatures tend to be higher at slower airspeeds. CAUTION IF A RISE IN RPM AND EGT ARE NOT INDICATED WITHIN 10 SECONDS, PLACE FUEL VALVE SWITCH TO OFF AND ABORT START. REFER TO ENGINE FAILURE DURING FLIGHT AND EMERGENCY LANDING WITHOUT POWER CHECKLISTS. CAUTION EMERGENCY AIRSTARTS MAY BE ATTEMPTED BELOW 10% RPM AND OUTSIDE THE NORMAL AIRSPEED ENVELOPE, BUT EGT SHOULD BE CLOSELY MONITORED. A MANUAL AIRSTART (SRL “OFF”) WITHOUT THE USE OF FUEL ENRICHMENT CAN BE PERFORMED IF START TEMPERATURES ARE TOO HIGH WITH THE SRL SYSTEM ON. REFER TO THE AIRSTART CHECKLIST 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 in the Emergency Landing Without Engine Power checklist. Before attempting an “off airport” landing with engine power available, one should fly over the landing area at a safe, but low altitude to inspect the terrain for obstructions and surface conditions, proceeding as discussed in the Precautionary Landing With Engine Power checklist. NOTE The overhead fuel tank selectors control shutoff valves at the wing fuel tank outlets. To minimize the possibility of a fire, these selectors can be set to the OFF position during the final stage of an approach to an “off airport” landing. With the selectors turned OFF, there is adequate fuel in the fuel reservoir tank for 2.5 minutes of maximum continuous power operation or approximately 9 minutes idle power operation. A warning horn will sound with both fuel selectors turned OFF. If it is objectionable, it may be silenced by pulling the START CONT circuit breaker. WARNING IF THE PRECAUTIONARY LANDING IS ABORTED, TURN THE FUEL TANK SELECTORS TO THE “ON” POSITION AFTER INITIATING THE BALKED LANDING. Prepare for ditching by securing or jettisoning heavy objects located in the baggage area and collect folded coats for protection of occupants’ face at touchdown. Transmit Mayday message on 121.5 MHz giving location and intentions and squawk 7700 if a transponder is installed. Avoid a landing flare because of difficulty in judging height over a water surface. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-22 November 7, 2019 FAA Approved LANDING WITHOUT ELEVATOR CONTROL Using power lever and elevator trim control, trim for approximately 500 fpm descent with 20º flaps at 85 KIAS. Then control the glide angle by adjusting power. If required, make small trim changes to maintain approximately 85 KIAS as power is adjusted during the approach. The landing flare can be accomplished by a gentle power reduction accompanied by nose up trim. At forward C.G. loadings, it may be necessary to make a small power increase in the final flare stage to bring the nose up and prevent touchdown on the nose first. After touchdown, move the power lever to idle. SMOKE AND FIRE In the event a fire is encountered, the following information will be helpful in dealing with the emergency as quickly and safely as possible. The preflight checklist in Section 4 is provided to aid the pilot in detecting conditions which could contribute to an airplane fire. As a fire requires a combustible material, oxygen and a source of ignition, close preflight inspection should be given to the engine compartment and the underside of the wing and fuselage. Leaks in the fuel or oil systems can lead to a ground or in-flight fire. WARNING FLIGHT SHOULD NOT BE ATTEMPTED WITH KNOWN FUEL OR OIL LEAKS. THE PRESENCE OF FUEL OR UNUSUAL OIL STAINS MAY BE AN INDICATION OF SYSTEM LEAKS AND SHOULD BE CORRECTED PRIOR TO FLIGHT. Probable causes of an engine fire are a malfunction of the fuel control unit and improper starting procedures. Improper procedures, such as introducing fuel into the engine when the engine RPM is below 10% RPM, will cause a hot start which may result in an engine fire. In the event that this occurs, proceed in accordance with the Engine Fire During Start On Ground checklist. If an airplane fire is discovered on the ground or during takeoff, but prior to committed flight, the airplane should be stopped and evacuated as soon as practical. Engine fires originating in flight must be controlled as quickly as possible in an attempt to prevent major structural damage. Immediately shut off all fuel to the engine and shut down the engine. Close the cabin heat firewall shutoff control and forward side vents. To avoid drawing fire into the cabin, open the overhead vents, extend 20º to 30º flaps and slow down to 80-85 KIAS. This provides a positive cabin pressure in relation to the engine compartment. An engine restart should not be attempted. An open foul weather window produces a low pressure in the cabin. To avoid drawing the fire into the cabin, the foul weather window should be kept closed. A fire or smoke in the cabin should be controlled by identifying and shutting down the faulty system. Smoke may be removed by opening the cabin ventilation controls. When the smoke is intense, the pilot may choose to expel the smoke through the foul weather window. The foul weather window should be closed immediately if the fire becomes more intense when the window is opened. The initial indication of an electrical fire is usually the odor of burning insulation. The checklist for this problem should result in elimination of the fire. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-23 November 7, 2019 FAA Approved EMERGENCY OPERATION IN CLOUDS No changes from the OEM procedures found in the Cessna POH/AFM. INADVERTENT FLIGHT INTO ICING CONDITIONS Intentional flight into known icing conditions is prohibited unless the complete flight into known icing equipment package is installed and operative and the airplane weight is 8750 pounds or less (cargo pod off) or 8550 pounds or less (cargo pod on). During instrument flights, however, icing conditions may be encountered inadvertently and, if the known icing equipment package is not completely functional, some corrective action will be required as shown in the checklist. Initiation of a climb is usually the best ice avoidance action to take; however, alternatives are descent to warmer air or course reversal. STATIC SOURCE BLOCKED If erroneous instrument readings are suspected due to water, ice, or other foreign matter in the pressure lines going to the left flight panel’s external static pressure source, the alternate static source valve should be pulled full on. A chart in Section 5 provides a correction which may be applied to the indicated airspeeds and altitudes resulting from inaccuracies in the alternate static source pressures. NOTE The altitude hold mode of the autopilot should be disengaged before actuating the alternate static source valve. SPINS Intentional Spins are prohibited in this airplane. Should an inadvertent spin occur, the following technique may be used: 1. RETARD THE POWER LEVER TO IDLE POSITION. 2. PLACE AILERONS IN NEUTRAL POSITION. 3. 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. 4. HOLD THESE CONTROL INPUTS UNTIL ROTATION STOPS. Premature relaxation of the control inputs may extend the recovery. 5. AS ROTATION STOPS, NEUTRALIZE RUDDER AND MAKE A SMOOTH RECOVERY FROM THE RESULTING DIVE. NOTE If disorientation precludes a visual determination of the direction of rotation, the needle of the turn and bank indicator may be referred to for this information. NOTE Airspeed during the recovery of the airplane may exceed the respective flap setting VFE. When able, it is recommended that flaps be retracted during recovery to prevent this type of occurrence. Supervan Systems, Ltd. Cessna 208B/TPE331-12JR Landplane 10699 Private Road 5117 Airplane Flight Manual Supplement Celina, Texas 75009 SSL-FMS-208B-12JR (972) 382-2500 Section 3: Emergency Procedures Rev. 5 3-24 November 7, 2019 FAA Approved ENGINE MALFUNCTIONS LOSS OF OIL PRESSURE The complete loss of oil pressure, as evidenced by the low oil pressure annunciator being illuminated and confirmed by the oil pressure gage reading, implies that the pilot will eventually lose control of the propeller as the propeller springs and counterweights attempt to drive the propeller blades into feather. Also, the engine will eventually seize. Therefore, if the pilot elects to continue to operate the engine after loss of oil pressure, engine and propeller operation should be closely monitored for indication of the onset of propeller feathering or engine seizure and the engine failure checklist should be completed at that time. Operation of the engine at a reduced power setting (preferably at the minimum power required for the desired flight regime) will generally prolong the time to loss of engine/propeller thrust. Operation of the engine with the oil pressure in the yellow arc is not considered critical, but is a cause for concern and should be tolerated only for the completion of the flight. Continued monitoring of the oil pressure gage will provide an early indication of dropping oil pressure due to insufficient oil supply or a malfunctioning oil pump, and will give the pilot additional time to divert to a suitable emergency landing area with the engine operating. FUEL CONTROL UNIT MALFUNCTION If there is an indication of improper operation of the fuel control, when possible, check the handling of the aircraft by a simulated landing flare at a safe altitude before trying to land. If unusual drag is noted that cannot be eliminated by increasing power, it might be necessary to feather the engine and perform an Emergency Landing Without Engine Power. NON-RESPONSIVE POWER LEVER If during flight the power lever becomes unresponsive, it may be due to a frozen P2T2 sensor. The power lever response can be restored by utilizing the engine inlet anti-ice heat, which also heats the sensor. It is recommended to turn on the engine ignition during this operation to prevent an engine flameout. It may take several minutes for the power lever response to