P92-JS Flight Manual

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. WARNING CAUTION NOTE FLIGHT MANUAL Date: Issue 3: 25th May2010 1-3 P92-JS S E C T I O N 1 GENERAL THREE-VIEW DRAWING Dimensions shown refer to aircraft weight of 550kg (and 600 kg) and normal operating tire pressure. Propeller ground clearance 320mm Propeller ground clearance with deflated front tire and nosewheel shock absorber compressed by 102mm Minimum ground steering radius 5.5m NOTE FLIGHT MANUAL Date: Issue 3: 25th May2010 1-4 P92-JS S E C T I O N 1 GENERAL DESCRIPTIVE DATA WING For 550 kg MTOW For 600 kg MTOW Wing span: 8.7 m 8.7 m Wing chord 1.4 m 1.4 m Wing surface 12 m2 12 m2 Wing loading 45.8 kg/m2 50.0 kg/m2 Aspect ratio 6.31 6.31 Taper ratio 1.0 1.0 Dihedral 1.5° 1.5° FUSELAGE Overall length 6.400 m 6.400 m Overall width 1.100 m 1.100 m Overall height 2.500 m 2.500 m EMPENNAGE Stabilator span 2.900 m 2.900 m Vertical tail span 1.230 m 1.230 m LANDING GEAR Wheel track: 1.800 m 1.800 m Wheel base: 1.600 m 1.600 m Main gear tires: Air Trac; Cleveland wheel hub and brakes kit: 5.00-5 199-102 5.00-5 199-102 Nose gear tire: Sava 4.00-6 4.00-6 CONTROL SURFACES TRAVEL LIMITS Ailerons Up 20° down 15 ° 2° Stabilator Up 18° down 3° 1° Trim-Tab 2° ; 12° 1° Rudder RH 25° LH 25° 1° Flaps 0° -38° 1° FLIGHT MANUAL Date: Issue 3: 25th May2010 1-5 P92-JS S E C T I O N 1 GENERAL ENGINE Manufacturer: Bombardier-Rotax GmbH Model 912 S2 Certification basis FAR 33 Amendment 15 Austrian Type- Certification No. n° TW 9-ACG of 27 Nov. 1998 Type: 4 cylinder horizontally-opposed twins with overall displacement of 1352 c.c., mixed cooling, (water-cooled heads and air- cooled cylinders), twin carburettors, integrated reduction gear with torque damper. Maximum power: 73.5 kW (98.6 hp) @ 5800 rpm (max.5 min.) 69.0 kW (92.5 hp) @ 5500 rpm (continuous) PROPELLER Manufacturer: HOFFMANN Propeller Certification basis: CAR Part 14 Type-Certification No.: SO/E 30 of 10/12/1999 Model: HO17GHM A 174 177C Number of blades: 2 Diameter: 1740 mm (no reduction permitted) Type: Fixed pitch - wood FLIGHT MANUAL P92-JS S E C T I O N 1 GENERAL Date: Issue 3rev2: 16th June 2015 1-6 FUEL Fuel grade: EN 228 Premium EN 228 Premium plus AVGAS 100LL (see Section 2.9) Fuel tanks: 2 wing tanks integrated within the wing's leading edge with fuel strainer located in engine cowling. Capacity of each wing tank 35 liters (optional 45 liters) Total capacity: 70 liters (optional 90 liters) Total usable fuel 66.8 liters. (86.8 liters) OIL SYSTEM Oil system type: Forced, with external oil reservoir Oil: Automotive grade API "SF" or "SG" type oil preferably synthetic or semi-synthetic Oil Capacity: 3.0 liters COOLING Cooling system: Mixed air and liquid pressurized closed circuit system Coolant: Antifreeze and water liquid mixture Capacity 3 liters FLIGHT MANUAL P92-JS S E C T I O N 1 GENERAL Date: Issue 3: 25th May2010 1-7 MAXIMUM CERTIFIED WEIGHTS Maximum take-off weight: 550 kg 600 kg Maximum landing weight: 550 kg 600 kg Maximum baggage weight 20 kg 20 kg STANDARD WEIGHTS Standard Empty Weight 325 kg 325 kg Maximum Useful Load 225 kg 275 kg SPECIFIC LOADINGS Wing Loading 45.8 kg/m2 50 kg/m2 Power Loading 5.6 kg/hp 6.1 kg/hp FLIGHT MANUAL P92-JS S E C T I O N 1 GENERAL Date: Issue 3: 25th May 2010 1-8 ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS Knots Calibrated Airspeed is indicated airspeed corrected for position and instrument error and expressed in knots. KIAS Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots. KTAS Knots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitude and temperature. VFE Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. VNO Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air, then only with caution. VNE Never Exceed Speed is the speed limit that may not be exceeded at any time. VS Stalling Speed. VS0 Stalling speed in landing configuration VS1 Stalling speed in clean configuration (flap 0°) VX Best Angle-of-Climb Speed is the speed which results in the greatest gain of altitude in 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 takeoff VLO Lift off speed: is the speed at which the aircraft generally lifts off from the ground. Vobs Obstacle speed: is the speed at which the aircraft flies over a 15m obstacle during takeoff or landing FLIGHT MANUAL P92-JS S E C T I O N 1 GENERAL Date: Issue 3: 25th May2010 1-9 METEOROLOGICAL TERMINOLOGY OAT Outside Air Temperature is the free air static temperature expressed in degrees Celsius (°C). TS Standard Temperature is 15°C at sea level pressure altitude and decreased by 2°C 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. ENGINE POWER TERMINOLOGY RPM Revolutions Per Minute: is the number of revolutions per minute of the propeller, multiplied by 2.4286 yields engine RPM. AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplane during takeoff and landing is guaranteed. Usable fuel is the fuel available for flight planning. Unusable fuel is the quantity of fuel that cannot be safely used in flight.. g is the acceleration of gravity. TOR is the takeoff distance measured from actual start to wheel liftoff point TOD is total takeoff distance measured from start to 15m obstacle clearing GR is the distance measured during landing from actual touchdown to stop point LD is the distance measured during landing, from 15m obstacle clearing to actual stop. S/R is specific range, that is, the distance (in nautical miles) which can be expected at a specific power setting and/or flight configuration per kilo of fuel used. FLIGHT MANUAL P92-JS S E C T I O N 1 GENERAL Date: Issue 3: 25th May 2010 1-10 WEIGHT AND BALANCE TERMINOLOGY Datum is an imaginary vertical plane from which all horizontal distances are measured for balance purposes. Arm is the horizontal distance from the reference datum to the center of gravity (C.G.) of an item. 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 airplane. Standard Empty Weight Standard Empty Weight is the weight of a standard airplane, including unusable fuel, full operating fuels and full engine oil. Basic Empty Weight is the standard empty weight plus the weight of optional equipment. Useful Load is the difference between takeoff weight and the basic empty weight. Maximum Weight is the maximum certified weight of the aircraft. Maximum Takeoff Weight is the maximum weight approved for the start of the takeoff run. Maximum Landing Weight is the maximum weight approved for the landing touch down. Tare is the weight of chocks, blocks, stands, etc. used when weighing an airplane, and is included in the scale readings. Tare is deducted from the scale reading to obtain the actual (net) airplane weight. FLIGHT MANUAL P92-JS S E C T I O N 1 GENERAL Date: Issue 3: 25th May2010 1-11 UNIT CONVERSION CHART MULTIPLYING BY YIELDS TEMPERATURE Fahrenheit [°F] Celsius [°C] Celsius [°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 second. [m/s] Knots [kts] 1.853 Kilometers / hour [km/h] Kilometers / hour [km/h] 0.5396 Knots [kts] PRESSURE Atmosphere [atm] 14.7 Pounds / sq. in [psi] Pounds / sq. in [psi] 0.068 Atmosphere [atm] LENGTH Kilometers [km] 0.5396 Nautical miles [nm] Nautical miles [nm] 1.853 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 Liters [l] 0.2642 U.S. Gallons [US Gal] U.S. Gallons [US Gal] 3.785 Liters [l] AREA Square meters [m2] 10.76 Square feet [sq ft] Square feet [sq ft] 0.0929 Square meters [m2] FLIGHT MANUAL P92-JS S E C T I O N 1 GENERAL Date: Issue 3: 25th May 2010 1-12 INTENTIONALLY LEFT BLANK