JODEL D.112 INFORMATION MANUAL C-FVOF

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1 JODEL D.112 INFORMATION MANUAL C-FVOF

2 Table of Contents I General Description...4 Dimensions:...4 Powertrain:...4 Landing gear:...4 Control travel:...4 II Limitations...5 Speed limits:...5 Airpeed indicator marking:...5 Maximum total allowable weight:...5 Design Load Factor:...5 Limits of centering:...5 Lever arm:...5 Engine limitations:...6 Marking of engine instruments:...6 Minimum crew:...6 Operating Manual:...6 III Emergency procedures...7 In-flight engine shut down:...7 Carburetor icing:...7 Forced Landing:...7 Stall:...7 IV Normal Procedures Check List...8 Before the flight:...8 WALK AROUND INSPECTION: CABIN EMPENNAGE RIGHT WING NOSE LEFT WING...8 Starting:...9 After Engine Start...9 Taxi:...9 Before Take Off:...9 Flight Instruments:...9 Take Off:...10 Climb :...10 Cruise:...10 Descent:...10 Go Around:...10 Landing:...10 Shut Down:...10 Property of C-FVOF Flying Club Page 2 of 12

3 V Weight and balance calculation...11 Before the flight: check the loading...11 VI Performance...12 Stall speed:...12 Practical ceiling:...12 Cruise:...12 Demonstrated cross-wind:...12 Property of C-FVOF Flying Club Page 3 of 12

4 I General Description Single-engine 65-hp two-seater low wing side-by-side. Dimensions: Wingspan: (8.2 m) Length: 20 4 (6.2 m) Height: 6 11 (2.1 m) Surface Area: ft² (12.75 m²) Maximum gross weight: 1168 lbs (530 kg) Powertrain: Engine: Continental A65 65 hp Oil: crankcase capacity: 4 liters Summer: Aéro D100 Winter: Aéro D80 Gasoline: 100 LL; Mogas Fuel capacity: 60 l in fuselage; gauge type is float and rod. Fuel shut-off valve and sump drain: located under fuel tank. Propeller: Sensenich 72 X 42 Landing gear: Main: rubber shock absorber pneumatic tires 600 X 6 inflation pressure 15 psi Tail: solid rubber tire 6X2 Control travel: Elevators: 30 upwards 25 downwards Rudder: Ailerons: 25 left and right 25 upwards and downwards Property of C-FVOF Flying Club Page 4 of 12

5 II Limitations Speed limits: Never exceed speed: Vne: 155 mph (250 km/h) Maximum structural cruising speed: Vno: 124 mph (200 km/h) Maximum design turbulent air penetration speed: 105 mph (175 km/h) Stall speed: Vs: 35 mph (55 km/h) Airpeed indicator marking: Green arc (normal operating range): 44 to 124 mph (70 to 200 km/h) Yellow arc (operation conducted with caution and only in smooth air): 124 to 155 mph (200 to 250 km/h) Red radial line (maximum for all operations): 155 mph (250 km/h) Maximum total allowable weight: 1168 lbs (530 kg) Design Load Factor: Positive: + 4.4g Negative: g Limits of centering: Front limit: 16% [10.6 (+ 0.27m)] Rear limit: 32% [9.3 (+ 0.54m)] Reference datum: Leading edge rectangular part of the wing [chord length (1.71m)] Lever arm: Empty airplane: Crew: Luggage: Gasoline: see weighing report (0.58m) (1.15m) -8.3 (0.21m) Property of C-FVOF Flying Club Page 5 of 12

6 Engine limitations: Continuous static max: 2100 RPM Continuous take-off and max: 2500 RPM In-flight oil pressure: 29 to 40 psi (2 to 2.8) bar Reduced engine oil pressure: 10 psi (0.7 bar) Oil temperature: Min: 30 C Max: 104 C Marking of engine instruments: Tachometer: Green arc from 600 RPM to 2300 RPM Red radial line at 2300 RPM Oil pressure gauge: Green arc from 10 to 37 psi (0.7 to 2.6 bar) Oil thermometer: Green bow from 30 C to 104 C Red radial line at 104 C Minimum crew: 1 pilot Operating Manual: This aircraft shall be operated in the normal category in accordance with the approved flight manual PROHIBITED ANY ACROBATIC MANOUVER OR INTENTIONAL SPIN IS PROHIBITED Property of C-FVOF Flying Club Page 6 of 12

7 III Emergency procedures In-flight engine shut down: Fuel off. When engine quits - Ignition off Dead Stick landing Carburetor icing: If the engine RPM drops without the other parameters varying, it may be icing: pull carb heat full on, the speed should increases as soon as the Ice melts. If the icing is severe (continued RPM reduction, vibrations). Leave heat on and set full throttle. Forced Landing: Seat belts on Fuel shutoff off Glide Speed - 60 mph Shut off electrical equipment before landing Stall: Engine power to idle Maintain level flight to bleed off airspeed To recover: lower nose and apply power Property of C-FVOF Flying Club Page 7 of 12

8 IV Normal Procedures Check List Before the flight: check C of G. WALK AROUND INSPECTION: 1 CABIN Ignition off Fuel on Throttle closed Flight controls free. Neutral trim 2 EMPENNAGE Check general condition of the aircraft structure Elevators and rudder - locks removed and freedom of movement Tail wheel secure Check elevator trim secure 3 RIGHT WING Aileron - locks removed and freedom of movement Right main landing gear (brake & wheel) secure 4 NOSE Fuel: cap closed; check and confirm fuel quantity Engine clean (check for bird nests in spring) Carburetor air inlet filter- secure and clean Exhaust secure Check fuel tank sump for water, sediment and proper fuel grade Check oil level Check condition of the propeller is satisfactory Fuel cap closed Cowls and access panels closed and secure 5 LEFT WING Pitot tube: remove cover; check dynamic vent clear Left main landing gear (brake & wheel) - secure Aileron - locks removed and freedom of movement Property of C-FVOF Flying Club Page 8 of 12

9 Starting: Brakes on Stick full nose up Fuel on Prime when necessary - Throttle cracked Mags on Contact Person swinging the propeller will confirm the above commands and when ready will advise the pilot with the expression - Contact The pilot will confirm Contact After Engine Start Oil pressure must be established within 30 seconds otherwise cut off engine Avoid prolonged operation below 1,000 RPM Engine warm up at 1200 RPM Taxi: Use minimum power low speed minimum braking Before Take Off: No loose objects in cockpit Harness-on Fuel On Flight Instruments: check - Altimeter set. L & R Magneto check: 1500 RPM (maximum mag drop 75 RPM) set idle at 1,000 RPM carb heat on: check RPM for drop close throttle: check engine idles smoothly with heat on Carb heat off: set idle at 1,000 RPM Flight Controls: check free and full operating range. Property of C-FVOF Flying Club Page 9 of 12

10 Take Off: When clear, taxi to position and line up Open throttle smoothly rpm greater than 2,000 continue to accelerate. 40 mph rotate aircraft lift-off Keep aircraft close to the ground accelerating to 60 mph climb out Climb : Optimum speed: 60 mph Use full throttle. Cruise: Normal cruise: 2100 RPM Descent: Carb heat on before reducing power In prolonged descents, increase the engine speed from time to time normal glide speed 60 mph Minimum approach speed 56 mph Go Around: apply Full Throttle gently but firmly Carb Heat off Accelerate to and climb at 60 mph Landing: 3 point Use of the brakes: as necessary Shut Down: Throttle idle mag switch Left off then on right off then on then both off Property of C-FVOF Flying Club Page 10 of 12

11 V Weight and balance calculation Before the flight: check the loading The total weight must not be more than 530 kg The center of gravity must be between 0.27 m and 0.54 m aft of the reference datum (leading edge of wing at root) Example of loading: Weight (kg) x Lever Arm (m) = Moment (m-kg) Empty aircraft 340 x = Crew 150 x = +87 Gasoline 30 x = -6.3 Luggage 10 x +1,150 = Sum Hence: x = m kg / 530 kg = m The center of gravity is m aft of the reference datum Total weight does not exceed 530 kg: therefore the aircraft is properly loaded. Property of C-FVOF Flying Club Page 11 of 12

12 VI Performance Stall speed: In straight and level flight at a weight of 530 kg: Vs = 35 mph Practical ceiling: At the weight of 530 kg, practical ceiling in standard atmosphere is 11,480 ft (3500 m) reached in 60 min. Cruise: Normal cruise: 2100 RPM, Airspeed 85 mph Average consumption: 15 l / h Eco Cruise: 1800 RPM Average consumption: 12 l / h Demonstrated cross-wind: 15 kt Property of C-FVOF Flying Club Page 12 of 12

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