TECNAM P2010tdi - Aircraft Flight Manual

LIST OF EFFECTIVE PAGES P2010tdi – Aircraft Flight Manual Page LoEP-1 4. LIST OF EFFECTIVE PAGES The List of Effective Pages (LOEP), applicable to manuals of every operator, lists all the basic AFM pages: each manual could contain either basic pages or one variant of these pages when the pages of some Supplements are embodied. Should supplements be embodied in accordance with approved instructions, make reference to the LOEP addressed on Supplements themselves. Edition 2, Rev 0 .....................31 May , 2021 Edition 2, Rev 1 .....................19 Jan , 2022 Edition 2, Rev 2 .....................22 Feb , 2022 Edition 2, Rev 3 .....................01 June 2022 Edition 2, Rev 4 ………………21 November 2022 2nd Edition - Rev. 4 Aircraft Flight Manual LIST OF EFFECTIVE PAGES P2010tdi – Aircraft Flight Manual Page LoEP-2 Section Pages Revision Section 0 i, ii, iii, iv; RoR-1 Rev. 0 LoEP-4 Rev. 3 RoR-2, LoEP-1 thru 3 Rev. 4 Section 1 1 thru 5, 7 thru 14 Rev. 0 6 Rev. 4 Section 2 1 thru 6, 8, 10 thru 12, 15 thru 20, 24 thru 29 Rev. 0 13, 14, 21 thru 23, 30 Rev. 1 7, 9, 30 Rev. 4 Section 3 1 thru 5, 8 thru 21, 23 thru 26, 28, 29, 31, 32, 34 thru 46 Rev. 0 9, 22, 33 Rev. 1 6, 7, 27, 30 Rev. 4 Section 4 1 thru 10, 15, 16, 18 thru 19, 20, 21, 23, 24 Rev. 0 10, 17, 22 Rev. 1 11, 12 Rev. 3 13, 14 Rev. 4 Section 5 1 thru 4, 6 thru 8, 11 thru 15, 18 thru 22 Rev. 0 5, 9, 10, 16, 17 Rev. 1 2nd Edition - Rev. 4 Aircraft Flight Manual LIST OF EFFECTIVE PAGES P2010tdi – Aircraft Flight Manual Page LoEP-3 Section 6 1 thru 4, 7, 12 ,13 Rev. 0 5, 6, 8 thru 11 Rev. 1 14, 15, 16 Rev. 3 Section 7 1 thru 6, 8, 10, 13 thru 21, 23 thru 26, 28, 29, 32, 34 thru 41, 43 thru 55, 57 thru 61, 63, 64, 65, 67, 69, 70, 72 Rev. 0 7, 9, 11, 22, 27, 30, 56, 71 Rev. 1 42 Rev. 2 12, 31, 33, 62, 66, 68, 73, 74 Rev. 3 Section 8 All Rev. 0 Section 9 1 thru 4, 6 Rev. 0 5 Rev. 4 Supplements LoEP: make reference to the Supplements LoEP Pages. 2nd Edition - Rev. 3 Aircraft Flight Manual LIST OF EFFECTIVE PAGES P2010tdi – Aircraft Flight Manual Page LoEP-4 Intentionally left blank 2nd Edition - Rev. 0 Section 1 - GENERAL P2010tdi – Aircraft Flight Manual Page 1 - 0 SECTION 1 GENERAL 2nd Edition - Rev. 0 Section 1 – GENERAL INDEX P2010tdi – Aircraft Flight Manual Page 1 - 1 INDEX 1. INTRODUCTION ...................................................................................3 2. WARNING – CAUTION – NOTE............................................................3 3. THREE VIEW AND DIMENSIONS .........................................................4 3.1. Dimensions .......................................................................................5 4. ENGINE .................................................................................................6 5. PROPELLER .........................................................................................6 6. MAXIMUM WEIGHTS AND SPECIFIC LOADINGS...............................7 6.1. Maximum Weights.............................................................................7 6.2. Specific Loadings ..............................................................................7 7. FUEL, LUBRICANT AND COOLANT ....................................................8 7.1. Fuel ...................................................................................................8 7.2. Lubricant ...........................................................................................8 7.3. Coolant .............................................................................................8 8. ACRONYMS AND TERMINOLOGY ......................................................9 8.1. Velocity terminology ..........................................................................9 8.2. Meteorological terminology..............................................................10 8.3. Avionics System Acronyms .............................................................10 8.4. Aircraft performance and flight planning terminology .......................11 8.5. Weight and balance terminology .....................................................12 9. UNIT CONVERSION CHART ..............................................................13 10. LITRES / US GALLONS CONVERSION CHART ................................14 2nd Edition - Rev. 0 Section 1 – GENERAL INDEX P2010tdi – Aircraft Flight Manual Page 1 - 2 Intentionally left blank 2nd Edition - Rev. 0 Section 1 – GENERAL INTRODUCTION P2010tdi – Aircraft Flight Manual Page 1 - 3 1. Introduction The Aircraft Flight Manual has been prepared to provide pilots and instructors with information for the safe and efficient operation of this aeroplane. This manual also contains supplemental data supplied by the aeroplane manufacturer. 2. Warning – Caution – Note Following definitions apply to warnings, cautions and notes used in the Aircraft Flight Manual. Means that the non-observation of the corresponding procedure leads to an immediate or important degradation of the flight safety. Means that the non-observation of the corresponding procedure leads to a minor or to a more or less long term degradation of the flight safety Draws the attention to any special item not directly related to safety but which is important or unusual 2nd Edition - Rev. 0 Section 1 – GENERAL THREE VIEW AND DIMENSIONS P2010tdi – Aircraft Flight Manual Page 1 - 4 3. Three view and Dimensions Figure 1-1 - General View 2nd Edition - Rev. 0 Section 1 – GENERAL THREE VIEW AND DIMENSIONS P2010tdi – Aircraft Flight Manual Page 1 - 5 3.1. Dimensions Overall dimensions Wing Span…………………………………… 10.30m / 33.79ft Overall Length………………………………. 7.91m / 25.95ft Overall Height……………………………….. 2.84m / 9.32ft Stabilator span……………………………… 3.35m / 10.99ft Wing Wing surface………………………………… 13.9 m2 / 149.6 ft2 Mean Geometric Chord…………………….. 1.349m / 4.426ft Dihedral………………………………………. 1° Aspect ratio………………………………….. 7.63 Fuselage Cabin width…………………………………... 1.14m / 3.74ft Cabin length…………………………………. 2.3m / 7.55 ft Landing Gear Wheels Track………………………………... 2.1m / 6.89ft Wheels base…………………………………. 2.15m / 7.05 Main Gear Tire………………………………. 6.00-6 Nose Gear Tire……………………………… 5.00-5 2nd Edition - Rev. 4 Section 1 – GENERAL GENERAL FEATURES P2010tdi – Aircraft Flight Manual Page 1 - 6 4. Engine Manufacturer.…………………….… Continental Aerospace Technologies GmbH Model……….………………………. TAE 125-02-125 Type Certificate.………………….... EASA.E.055 Engine type.…...…………………… Liquid cooled 4 cylinder in-line four-stroke diesel engine with DOHC (double overhead camshaft), turbo charged, engine equipped with an electric starter and one alternator and optional auxiliary drive. Max. take-off power (max. 5 min) ……….. 125 kW / 168 hp (100%) @2300 rpm Max. continuous power …………………… 114 kW / 153 hp (91%) @2250 rpm 5. Propeller Manufacturer.…………………….… MT Propeller Model……….………………………. MTV-6-R/190-69 Type Certificate.………………….... EASA.P.094 Blades.…...…………………………. 3 laminated wood composite Diameter……….……………...……. 1900mm / 6 ft 2.8 in Type…………………………...……. Variable pitch propeller at constant speed 2nd Edition - Rev. 0 Section 1 – GENERAL ACRONYMS AND TERMINOLOGY P2010tdi – Aircraft Flight Manual Page 1 - 7 6. Maximum Weights and Specific Loadings 6.1. Maximum Weights Maximum Take-Off Weight…………... 1160 kg (2557 lb) Maximum Landing Weight…………... 1160 kg (2557 lb) For Aircraft embodying MOD2010/207: Maximum Take-Off Weight…………... 1200 kg (2645 lb) Maximum Landing Weight…………... 1200 kg (2645 lb) 6.2. Specific Loadings Wing Loading…………........................ 83.45 kg/m2 (17.09 lb/ft2) Power Loading…………...................... 6.90 kg/hp (15.22 lb/hp) For Aircraft embodying MOD2010/207: Wing Loading…………........................ 86.33 kg/m2 (17.68 lb/ft2) Power Loading…………...................... 7.14 kg/hp (15.74 lb/hp) 2nd Edition - Rev. 0 Section 1 – GENERAL ACRONYMS AND TERMINOLOGY P2010tdi – Aircraft Flight Manual Page 1 - 8 7. Fuel, Lubricant and Coolant 7.1. Fuel Fuel Specification.............................................. JET A-1 (ASTM D 1655) Diesel (EN 590) 7.2. Lubricant Engine Oil Specification.................................... Aero Shell Oil Diesel Ultra Shell Helix Ultra 5W-30 Gearbox Oil Specification………………….…… Centurion Gearbox Oil N1 7.3. Coolant Coolant Specification.................................. Water / radiator protection in a ratio of 50:50 Radiator Protection………………………...… BASF Glysantin Protect Plus / G48 2nd Edition - Rev. 0 Section 1 – GENERAL ACRONYMS AND TERMINOLOGY P2010tdi – Aircraft Flight Manual Page 1 - 9 8. Acronyms and Terminology 8.1. Velocity terminology KCAS Calibrated Airspeed is the indicated airspeed expressed in knots, corrected taking into account the errors related to the instrument itself and its installation. KIAS Indicated Airspeed is the speed shown on the airspeed indicator and it is expressed in knots. KTAS True Airspeed is the KCAS airspeed corrected taking into account altitude and temperature. VA Design Manoeuvring speed is the speed above the which it is not allowed to make full or abrupt control movement. VFE Maximum Flap Extended speed is the highest speed permissible with flaps extended. VNO Maximum Structural Cruising Speed is the speed that should not be exceeded, except in smooth air and only with caution. VNE Never Exceed Speed is the speed limit that may not be exceeded at any time. VO Operating Manoeuvring speed is the speed above the which it is not allowed to make full or abrupt control movement. Operating at or below manoeuvring speed does not provide structural protection against multiple full control inputs in one axis or full control inputs in more than one axis at the same time. VS Stall Speed is the minimum steady flight speed for a specific flaps configuration and power setting. VS0 Stall Speed in landing configuration (flaps fully extended). VX Best Angle-of-Climb Speed is the speed which results in the greatest gain of altitude with respect to a given horizontal distance. VY Best Rate-of-Climb Speed is the speed which results in the greatest gain in altitude in a given time. VR Rotation speed: is the speed at which the aircraft rotates about the pitch axis during take-off. VREF Reference Speed is the reference speed for the approach during landing phase. V50ft Obstacle speed (screen speed, V50ft): is the speed at which the aircraft flies over a 15m (50 ft) obstacle during take-off or landing. VGLIDE Glide speed: is the speed of maximum efficiency (to fly the longest distance per unit of altitude lost) 2nd Edition - Rev. 0 Section 1 – GENERAL ACRONYMS AND TERMINOLOGY P2010tdi – Aircraft Flight Manual Page 1 - 10 8.2. Meteorological terminology ISA International Standard Atmosphere: is the air atmospheric standard condition at sea level, at 15°C (59°F) and at 1013.25hPa (29.92 inHg). QFE Official atmospheric pressure at airport level: it indicates the aircraft absolute altitude with respect to the official airport level. QNH Theoretical atmospheric pressure at sea level: is the atmospheric pressure reported at the medium sea level, through the standard air pressure-altitude relationship, starting from the airport QFE. OAT Outside Air Temperature is the air static temperature expressed in degrees Celsius (°C) / Fahrenheit (°F). TS Standard Temperature is 15°C (59°F) at sea level pressure altitude and decreased by about 2°C (3.5°F) for each 1000 ft of altitude. HP Pressure Altitude is the altitude read from an altimeter when the barometric subscale has been set to 1013 mb (29.92 inHg). 8.3. Avionics System Acronyms XPDR Transponder 2nd Edition - Rev. 0 Section 1 – GENERAL ACRONYMS AND TERMINOLOGY P2010tdi – Aircraft Flight Manual Page 1 - 11 8.4. Aircraft performance and flight planning terminology Crosswind Velocity is the velocity of the crosswind component for the which adequate control of the airplane during take-off and landing is assured. Usable fuel is the total fuel minus unusable fuel. Unusable fuel is the quantity of fuel that cannot be safely used in flight. G is the acceleration of gravity. TOR (Take-off Ground Roll) is the take-off distance measured from actual start to MLG (main landing gear) wheel lift-off point. TOD (Take-off Distance) is total take-off distance measured from start to 15m (50 ft) obstacle clearing. LR is the distance measured during landing from actual touchdown to stop point. LD is the distance measured during landing, from 15m (50 ft) obstacle clearing to actual stop. 2nd Edition - Rev. 0 Section 1 – GENERAL ACRONYMS AND TERMINOLOGY P2010tdi – Aircraft Flight Manual Page 1 - 12 8.5. Weight and balance terminology Datum “Reference datum” is an imaginary vertical plane from which all horizontal distances are measured for balance purposes. Arm is the horizontal distance of an item measured from the reference datum. Moment is the product of the weight of an item multiplied by its arm. C.G. Center of Gravity is the point at which the airplane, or equipment, would balance if suspended. Its distance from the reference datum is found by dividing the total moment by the total weight of the aircraft. Standard Empty Weight is the weight of the aircraft with engine fluids and oil at operating levels. Basic Empty Weight (BEW) is the standard empty weight to which it is added the optional equipment weight. Useful Load is the difference between maximum take-off weight and the basic empty weight. Maximum Take-off Weight (MTOW) is the maximum weight approved to perform the take-off. Maximum Landing Weight (MLW) is the maximum weight approved for the landing touchdown. 2nd Edition - Rev. 0 Section 1 – GENERAL ACRONYMS AND TERMINOLOGY P2010tdi – Aircraft Flight Manual Page 1 - 13 9. Unit Conversion Chart Table 1-1 - Unit Conversion Chart MOLTIPLYING BY  YIELDS TEMPERATURE Fahrenheit [°F] ( ) 5 9 32 ⋅ − F Celsius [°C] Celsius [°C] 9 5 32 ⋅       + C Fahrenheit [°F] FORCES Kilograms [kg] 2.205 Pounds [lbs] Pounds [lbs] 0.4536 Kilograms [kg] SPEED Meters per second [m/s] 196.86 Feet per minute [ft/min] Feet per minute [ft/min] 0.00508 Meters per [m/s] Knots [kts] 1.852 Kilometers/hour [km/h] Kilometers/hour [km/h] 0.5399 Knots [kts] PRESSURE Atmosphere [atm] 14.7 Pounds / sq. in [psi] Pounds / sq. in [psi] 0.068 Atmosphere [atm] LENGTH Kilometers [km] 0.5399 Nautical miles [nm] Nautical miles [nm] 1.852 Kilometers [km] Meters [m] 3.281 Feet [ft] Feet [ft] 0.3048 Meters [m] Centimeters [cm] 0.3937 Inches [in] Inches [in] 2.540 Centimeters [cm] VOLUME Litres [l] 0.2642 U.S. Gallons [US U.S. Gallons [US Gal] 3.785 Litres [l] AREA Square meters [m2] 10.76 Square feet [sq ft] Square feet [sq ft] 0.0929 Square meters [m2] 2nd Edition - Rev. 0 Section 1 – GENERAL ACRONYMS AND TERMINOLOGY P2010tdi – Aircraft Flight Manual Page 1 - 14 10. Litres / US Gallons Conversion Chart Table 1-2 - Litres/US Gallons Conversion Chart Litres US Gallons US Gallons Litres 5 1.3 1 3.8 10 2.6 2 7.6 15 4.0 3 11.4 20 5.3 4 15.1 25 6.6 6 22.7 30 7.9 8 30.3 35 9.2 10 37.9 40 10.6 12 45.4 45 11.9 14 53.0 50 13.2 16 60.6 60 15.9 18 68.1 70 18.5 20 75.7 80 21.1 22 83.3 90 23.8 24 90.9 100 26.4 26 98.4 110 29.1 28 106.0 120 31.7 30 113.6 130 34.3 32 121.1 140 37.7 34 128.7 150 39.6 36 136.3 160 42.3 38 143.8 170 44.9 40 151.4 180 47.6 42 159 190 50.2 45 170.3 200 52.8 47 177.9 210 55.5 50 189.3 220 58.1 55 208.2 230 60.7 60 227.1 240 63.4 63 238.4 2nd Edition - Rev. 0 Section 2 - LIMITATIONS P2010tdi – Aircraft Flight Manual Page 2 - 0 SECTION 2 LIMITATIONS 2nd Edition - Rev. 0 Section 2 – LIMITATIONS INDEX P2010tdi – Aircraft Flight Manual Page 2 - 1 INDEX 1. INTRODUCTION ........................................................................................3 2. SPEED .......................................................................................................4 2.1. Speed limitations ...............................................................................4 2.2. Airspeed Indicator Markings ..............................................................6 3. POWERPLANT ..........................................................................................7 3.1. Engine...............................................................................................7 3.2. Propeller ...........................................................................................7 3.3. Powerplant Limitations ......................................................................7 4. INSTRUMENTATION MARKINGS ...........................................................10 5. FUEL ........................................................................................................11 6. OIL ...........................................................................................................11 7. COOLANT ................................................................................................11 8. OPERATIVE AND ADDITIONAL LIMITATIONS ......................................12 8.1. Maximum Operating Altitude ...........................................................12 8.2. Flight Crew ......................................................................................12 8.3. Smoking ..........................................................................................12 8.4. Types of surface..............................................................................12 8.5. Paint ...............................................................................................12 9. WEIGHTS AND CENTER OF GRAVITY LIMITS ......................................13 10. MANEUVERS AND LOAD FACTOR LIMITS ......................................15 10.1. Load Factor Limits ......................................................................15 10.2. Approved Maneuvers .................................................................15 11. SEATS AND BAGGAGE .....................................................................16 11.1. Maximum Passenger Seating Configuration ...............................16 11.2. Baggage Loading Limit ...............................................................16 12. LIMITATION PLACARDS ....................................................................17 12.1. Speed limitations ........................................................................17 12.2. Operating and autopilot limitations ..............................................17 12.3. No smoking placard ....................................................................17 2nd Edition - Rev. 0 Section 2 – LIMITATIONS INDEX P2010tdi – Aircraft Flight Manual Page 2 - 2 12.4. Baggage compartment placard ...................................................17 13. KINDS OF OPERATION ......................................................................18 14. PBN (RNAV & RNP) OPERATIONAL CAPABILITY ...........................24 14.1. General GNSS Navigation Equipment Approvals .......................24 15. AVIONIC SYSTEM LIMITATIONS .......................................................25 15.1. General ......................................................................................25 15.2. G1000Nxi GNSS (GPS/SBAS) Navigation System Limitations ...27 16. AUTOPILOT SYSTEM LIMITATIONS .................................................30 2nd Edition - Rev. 0 Section 2 – LIMITATIONS INTRODUCTION EASA Approved P2010tdi – Aircraft Flight Manual Page 2 - 3 1. Introduction Section 2 includes operating limitations instrument markings and basic placards necessary for safe operation of P2010tdi aircraft, its engines, standard systems and equipment. 2nd Edition - Rev. 0 Section 2 – LIMITATIONS SPEED EASA Approved P2010tdi – Aircraft Flight Manual Page 2 - 4 2. Speed 2.1. Speed limitations The following table addresses the airspeed limitations and their operational significance: Table 2-1 - Speeds Limitations SPEED KCAS KIAS REMARKS VNE Never exceed Speed 164 163 Do not exceed this speed in any operation. VNO Maximum Structural Cruising Speed 130 130 Do not exceed this speed except in smooth air and only with caution. VA Design Manoeuvring Speed 119 119 Do not make full or abrupt control movement above this speed, because under certain conditions the aircraft may be overstressed by full control movement. VO Operating Manoeuvring Speed 119 119 VFE Maximum Speed flap extended (flap TO) 101 100 Do not exceed this speed for indicated flaps setting. Maximum Speed flap extended (flap LAND) 92 90 2nd Edition - Rev. 0 Section 2 – LIMITATIONS SPEED EASA Approved P2010tdi – Aircraft Flight Manual Page 2 - 5 For Aircraft embodying MOD2010/207: Table 2-2a - Speeds Limitations (MOD 2010/207) SPEED KCAS KIAS REMARKS VNE Never exceed Speed 164 163 Do not exceed this speed in any operation. VNO Maximum Structural Cruising Speed 130 130 Do not exceed this speed except in smooth air and only with caution. VA Design Manoeuvring Speed 121 121 Do not make full or abrupt control movement above this speed, because under certain conditions the aircraft may be overstressed by full control movement. VO Operating Manoeuvring Speed 121 121 VFE Maximum Speed flap extended (flap TO) 103 102 Do not exceed this speed for indicated flaps setting. Maximum Speed flap extended (flap LAND) 93 92 2nd Edition - Rev. 0 Section 2 – LIMITATIONS SPEED EASA Approved P2010tdi – Aircraft Flight Manual Page 2 - 6 2.2. Airspeed Indicator Markings Table 2-3 - Airspeed Indicator Markings MARKING KIAS EXPLANATION White arc 48-90 Positive Flap Operating Range (lower limit is VSO, at specified maximum weight and upper limit is the maximum speed permissible with landing flaps extension). Green arc 61-130 Normal Operating Range (lower limit is VS1 at specified maximum weight and most forward e.g. with flaps retracted and upper limit is maximum structural speed VNO). Yellow arc 130-163 Manoeuvres must be conducted with caution and only in smooth air. Red line 163 Maximum speed for all operations. For Aircraft embodying MOD2010/207: Table 2-4 - Airspeed Indicator Markings(MOD 2010/207) MARKING KIAS EXPLANATION White arc 49-92 Positive Flap Operating Range (lower limit is VSO, at specified maximum weight and upper limit is the maximum speed permissible with landing flaps extension). Green arc 62-130 Normal Operating Range (lower limit is VS1 at specified maximum weight and most forward e.g. with flaps retracted and upper limit is maximum structural speed VNO). Yellow arc 130-163 Manoeuvres must be conducted with caution and only in smooth air. Red line 163 Maximum speed for all operations. 2nd Edition - Rev. 4 Section 2 – LIMITATIONS POWERPLANT P2010tdi – Aircraft Flight Manual Page 2 - 7 EASA Approved 3. Powerplant 3.1. Engine MANUFACTURER………………………... Continental Aerospace Technologies GmbH MODEL……………………………………... TAE 125-02-125 TYPE………………………………………... Liquid cooled 4 cylinder in-line four-stroke diesel engine with DOHC (double overhead camshaft), turbo charged, engine equipped with an electric starter and one alternator and optional auxiliary drive. 3.2. Propeller MANUFACTURER………………………….. MT Propeller MODEL………………………………………. MTV-6-R/190-69 TYPE…………………………………………. Laminated wood composite, variable pitch propeller at constant speed, 3 blades DIAMETER…………………………………... 1900 mm (75 in) 3.3. Powerplant Limitations Following list reports the operating limitations for installed engines: Power  Max. take-off power (max. 5 min) ……….. 125 kW / 168 hp (100%) @2300 rpm  Max. continuous power …………………… 114 kW / 153 hp (91%) @2250 rpm Oil pressure  Normal operating pressure ……………….. 2.3 – 6 bar min. 1.0 bar max. 6.5 bar 2nd Edition - Rev. 0 Section 2 – LIMITATIONS POWERPLANT EASA Approved P2010tdi – Aircraft Flight Manual Page 2 - 8 Oil temperature  Operating temperature………..… min. 50°C (122°F) max. 120°C (248°F) Coolant temperature  Operating temperature………..… min. 60°C (140°F) max. 105°C (221°F) Gearbox temperature  Operating temperature………..… min. 0°C (32°F) max. 120°C (248°F) Fuel temperature*  Operating temperature ………...................  Engine start up temperature (JET A-1)……  Opening-up* temperature (JET A-1)…… max. 75°C (167 °F) min. -25°C (-13 °F) min. -30°C (-22 °F) *) Opening-up is the minimum temperature to increase power setting of the engine. Diesel Fuel, Blends of Diesel Fuel with Jet Fuel, or unknown fuel grade:  Engine starting fuel temperature . . . . . . . ….. . min. -5 °C (+23 °F)  Opening-up fuel temperature . . . . . . . . . . . . . . min. -5 °C (+23 °F) ** *) Temperature refers to temperature of the fuel in the tank. **) The take-off with Diesel fuel is not permitted, if the temperature of the fuel in the tank is below -5°C (-10°C if Liqui Moly "Diesel Fliess-Fit" is added at appropriate ratio). Refer to additive specification for proper usage. Engine operation Time limit for engine operation with negative g-force values………… -0.2 g for 5 seconds -0.3 g for 4 seconds -0.4 g for 3 seconds -0.5 g for 2 seconds Additional temperature limitations must be observed if the airplane is operated with Diesel Fuel or blends of Diesel Fuel with Jet Fuel. If you do not know what fuel grade is in the tank, always assume it is additive-free Diesel. 2nd Edition - Rev. 4 Section 2 – LIMITATIONS POWERPLANT EASA Approved P2010tdi – Aircraft Flight Manual Page 2 - 9 Cold Weather Operation* P2010tdi is equipped with a sensor monitoring intercooler temperature. In case of both intercooler temperature equal or lower than 15°C (59°F) and altitude/Outside Air Temperature envelope within red area, a CAS message (“INTRCLR TEMP LO”) alerts the pilot. In this case, leave immediately this condition and manage the engine to restore allowed conditions (Refer to Par. 7.8.1 in Section 3).engine to restore allowed conditions (Refer to Par. 7.8.1 in Section 3). If continuous monitoring of intercooler temperature in-flight is not possible, engine operation in the red area should be avoided, due to the risk of an engine flame out. *) applicable for aircraft NOT embodying MOD 2010/240 - CD-170 upgrade for MAT limitation removal (Engine P/N 05-7200-K040301). 2nd Edition - Rev. 0 Section 2 – LIMITATIONS INSTRUMENTATION MARKINGS EASA Approved P2010tdi – Aircraft Flight Manual Page 2 - 10 4. Instrumentation Markings Table 2-5 – Avionics System Instrument Markings INSTRUMENT RED ARC/LINE Minimum limit WHITE ARC Advisory GREEN ARC Safe operation YELLOW ARC Caution RED ARC Maximum limit PROPELLER RPM / / 0 -> 2250 2251 -> 2300 2301 -> 2500 POWER % Power / / 0 -> 91 92 -> 100 / OIL PRESS bar 0 -> 0.9 1.0 -> 2.2 2.3 -> 6.0 6.1 -> 6.5 6.6 -> 7 OIL TEMP. °C / 0 -> 49 50 -> 120 / 121 -> 125 Coolant Temperature °C / 0 -> 59 60 -> 105 / 106 -> 110 Gearbox Temperature °C / / 0 -> 120 / 121 -> 125 Fuel Temperature °C -35 -> -31 / -5 -> 65 66 -> 75 -30 -> -6 76 -> 80 Fuel Flow l/hr / 0 -> 50 / / / gal/hr / 0 -> 13.2 / / / FUEL QTY litres 0 / 0 -> 115 / / gal 0 -> 30.4 Alternator Ammeter A / / 1 -> 70 0 -> 1 / Main Battery Ammeter A / / 0 -> 100 / / Main Bus /Essential Bus Voltage V 20 / 24 -> 29 21 -> 23 30 -> 31 Backup Battery Voltage V 20 – 21 / 24 – 30 21 – 23 30 - 31