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Tecnam P92-JS-Checklist PRE-FLIGHT INSPECTIONS COCKPIT Flight Manual: Check that a copy is on board Weight and Balance: Check if within limits Parking brake: ON Engine throttle: Adjust friction lock Magnetos: OFF Fuel shutoff valves: Left / Right: ON Electric Fuel pump: OFF Radio and Avionics: OFF All Lights: OFF Master switch: ON Generator switch: ON, check generator light is illu Check acoustic operation Trim disconnect switch: ON Trim control: Activate control to full scale chec king travel limits and instrument indication. Navigation and Strobe Lights: Check operation and OFF Flaps control: Activate controls to full extension checking travel limits and instrument indication. Master and Generator switch: OFF LEFT WING Fuel level: check for obstructions. Pitot: Remove protection cap and check that is unobstructed. Left side leading and edge: Visual inspection Left aileron, Left Flap an d hinges: Visual inspection Left main Landing gear: Check inflation, tire condition and alignment. FUSELAGE AND EMPENNAGE Fuselage: Check skin condition Horizontal tail and Tab: Visual inspection Vertical tail and Rudder: Visual inspection Right main Landing gear: Check inflation, tire condition and alignment. Right aileron, Left Flap an d hinges: Visual inspection Right side leading and edge: Conditions: Weight: 550 kg - Engi ne: IDLE - No ground effect Lateral Banking 0º 30º 45º 60º KIAS KIAS KIAS KIAS 0º 44 47 52 63 15º 42 45 50 60 38º (Full) 39 42 47 56 CRUISE PERFORMANCE Conditions: Pressure Altitude 0 ft. OAT +15ºC Propeller RPM Speed KIAS Consumption Endurance (hours) Range (N. Miles) 55% 1900 96 15 lts/h 5.8 599 65% 2050 102 18 lts/h 4.9 495 Conditions: Pressure Alti tude 2000 ft. OAT +11ºC Propeller RPM Speed KIAS Consumption Endurance (hours) Range (N. Miles) 55% 1950 98 15 lts/h 5.8 571 65% 2070 106 18 lts/h 4.9 517 73% 2150 109 19 lts/h 4.6 501 Conditions: Pressure Altitude 4000 ft. OAT +7ºC Propeller RPM Speed KIAS Consumption Endurance (hours) Range (N. Miles) 55% 2020 101 15 lts/h 5.8 588 65% 2080 105 17 lts/h 5.1 540 70% 2150 110 18.5 lts/h 4.7 520 Conditions: Pressure Altitude 6000 ft. OAT +3ºC Propeller RPM Speed KIAS Consumption Endurance (hours) Range (N. Miles) 60% 2160 108 17 lts/h 5.1 556 Conditions: Pressure Altitude 8000 ft. OAT -0.8ºC Propeller RPM Speed KIAS Consumption Endurance (hours) Range (N. Miles) 55% 2120 99 15 lts/h 5.8 578 58% 2150 102 16 lts/h 5.4 556 Tecnam P92-JS-Checklist PRE-FLIGHT INSPECTIONS Right & Left side static port: Check for obstructions Nose wheel and tire: Check inflation, tire condition and condition of rubber shock absorber discs. Propeller and spinner: Check for nicks and security ENGINE Open engine cowling and perform the following: Check no foreign objects are present. Check the cooling circuits for losses, check coolan t reservoir level, insure radiator honeycomb is unobstructed. Check oil level by rotating the propeller in coun terclockwise until an audible sound is present. Check lubrication circuit for losses, check oil re servoir level and insure radiator honeycomb is unobstructed. Inspect fuel circuit for losses, check integrity of fireproof protection braids, drain circuit using the specific drainage valve located on the firewall. Drainage operation must be carried out with aircraft parked on level surface. Check connection and integrity of air intake system. Check integrity of silent-block suspensions. Check that all parts are secure or safe tied. Close engine cowling. BEFORE STARTING ENGINE Pre-Flight inspection: Complete Doors: Close and Secure Seat and seat belts: Adjust and Lock Circuit Breakers: Check In Parking brake: ON STARTING ENGINE Generator & Master switch: ON Electric fuel pump: ON Engine throttle: IDLE Choke: As needed Magnetos: ON Ignition key: Start Propeller RPM: Choke: OFF Instruments: Check oil pressure rise within 10 sec. (max. cold value 7 bar) Electric fuel pump: OFF and Check fuel pressure and then switch ON again. LANDING WITH FLAT TIRE Pre-landing checklist: Complete Flaps: Full Maintain aircraft nose high attitude as lo ng as possible FLAT MAIN TIRE: Approach: As usual Touchdown with good tire first and hold aircraft off flat tire as long as possible ELECTRICAL POWER SYSTEM MALFUNCTION Master and Generator switch: OFF if Generator light illuminates Master and Generator switch: ON Master and Generator switch: OFF if Generator light remain illuminates LOCKED CONTROL: Trim control: Check correct position Trim disconnect switch: OFF Speed: Adjust to control the aircraft without excessive stick force and land as soon as possible UNINTENTIONAL FLIGHT INTO ICING CONDITIONS Warmer external Temp: Locate and change attitude and direction of flight Flight controls: Move regularly Carburetor Heat: ON Propeller rpm: Increase to avoid ic e formation on the propeller blades Cabin Heat: ON RECOVERY FROM UNINTENTIONAL SPIN Engine throttle: IDLE Flight controls: Apply and hold full rudder opposite to the direction of spin. Move and hold stick forward until spin is halted. Neutralize rudder. Make a smooth recovery by pulling the stick back gently averting speeds in excess of V and maximum load factor. Engine throttle: Readjust to restore power REFERENCE SPEEDS 47 Kt Maneuver (550 Kg) VA: 93 Kt Lift off V 49 Kt Flaps extended V 68 Kt Obstacle T/O V OBS 56 Kt Normal operation V 106 Kt Obstancle Land V (0º / 38º): 58 / 48 Kt Stall (normal) V 44 Kt Max rate of climb V 73 Kt Stall (landing) V 39 Kt Never exceed V 134 Kt Glide 12.2:1 (550 Kg / 450 Kg): 66 / 60 Kt Tecnam P92-JS-Checklist BEFORE TAXIING Radio and Avionics: ON ON Trim control: Move to LH Trim position: Take-off (Center position) Fuel shutoff valves: Left / Right: ON Flaps: Up Request control to Tower: Authorization received TAXIING Brakes: Check Flight instruments: Check Directional gyro: Parking brake: ON Landing Light: ON Engine instruments: Check Oil Temp: 50-110ºC Temp: max135ºC Oil pressure: 2 – 5 bar Fuel pressure: 2.2 to 5.8 psi Take-Off - 15º Flight controls: Stick free and zero trim Request control to Tower: Authorization received TAKE-OFF AND CLIMB Traffic and Wind: Clear final and check Wind on runway Parking brake: OFF Carburetor Heat: OFF Transponder: Switch to ALT Engine Throttle: Full (Take-Off 2100 +/- 100 rpm Propeller) Rotation Speed: Vr = 47 kt Climb Speed: Vy = 73 Kt / Vx = 56 kt AT 500’ AGL Flaps: OFF Propeller rpm: Adjust to max 2050 rpm SMOKE & FIRE – WHILE PARKED OR DURING TAKE-OFF Fuel shutoff valves: OFF Electric Fuel pump: OFF Cabin Heat: OFF Take-Off: Abort if possible Engine running: OFF Warn bystanders to clear the area as fast as po ssible. Without removing the engine cowling use CO or a powder fire extinguisher to put out the flames directing spray towards cowling’s air intakes. ENGINE FIRE – DURING FLIGHT Fuel shutoff valves: OFF Electric Fuel pump: OFF Cabin Heat: OFF Engine throttle: All IN Magnetos: OFF Flaps: As needed Do not attempt Air Start. Carry out emergency procedure for “Forced Landing” CABIN FIRE DURING FLIGHT Master and Generator switch: OFF Cabin Heat: OFF Door vents: Open Direct fire extinguisher towards flame base. Ca rry out emergency procedure for “Forced Landing” FORCED LANDING WITHOUT ENGINE POWDER Speed: Landing area: Locate Fuel shutoff valves: OFF Electric Fuel pump: OFF Magnetos: OFF Seat and seat belts: Tighten, release door safety lock and unlatch doors. Flaps: Full Master and Generator switch: When certain to land: OFF POWER-ON FORCED LANDING Descend slope: Prompt Flaps: As needed Fuel shutoff valves: OFF Seat and seat belts: Tighten, release door safety lock and unlatch doors. Fuel shutoff valves: OFF Electric Fuel pump: OFF Flaps: Full Magnetos: OFF Master and Generator switch: OFF Tecnam P92-JS-Checklist ENGINE FAILURE DURING TAKE-OFF Engine throttle: IDLE Magnetos: OFF Flaps: Up Electric Fuel pump: OFF Fuel shutoff valves: OFF Call Tower: Declare Emergency Master and Generator switch: OFF ENGINE FAILURE AFTER TAKE-OFF Speed: Landing area: Locate Engine throttle: IDLE Electric Fuel pump: OFF Fuel shutoff valves: OFF Magnetos: OFF Flaps: As needed Call Tower: Declare Emergency Master and Generator switch: OFF ENGINE FAILURE DURING FLIGHT - IRREGULAR RPM Engine throttle: Check Carburetor Heat: ON Electric Fuel pump: ON Fuel shutoff valves: Left / Right: ON Irregular RPM condition persist: Land at the closest airport ENGINE FAILURE DURING FLIGHT – LOW FUEL PRESSURE (2.2 psi) Electric Fuel pump: ON Fuel shutoff valves: Left / Right: ON Low Fuel pressure condition persist: Land at the closest airport ENGINE FAILURE DURING FLIGHT – LOW OIL PRESSURE Oil Temp: If stable: Land at closest airport. If increasing: Engine throttle: 70 Kt Land at the closest airport and be alert for impeding engine fault. ENGINE AIR START Carburetor Heat: ON Fuel shutoff valves: Left / Right: ON Electric Fuel pump: ON Engine throttle: 50% Master and Generator switch: ON Ignition key: Start Engine instruments: Check readings and land at the closest airport CRUISE Propeller rpm: Engine instruments: Check Oil Temp: 90-110ºC s Temp: 90-135ºC Oil pressure: 2 –5 bar Fuel pressure: 2.2 to 5.8 psi Carburetor Heat: As required Fuel shutoff valves: Close Left shutoff valve as required Electric Fuel pump: ON Landing Light: ON Seat and seat belts: Adjust and Lock Carburetor Heat: As required Flaps: Extend gradually to Full flap position Fuel shutoff valves: Left / Right: ON Approach reference Speeds: 60 Kt - Full Flap 68 Kt – 15º Flap 70 Kt – 0º Flap 44 Kt – Touchdown / Full Flap BALKED LANDING Engine throttle: Full (Take-Off 2100 +/- 100 rpm Propeller) Flaps: Take-Off - 15º Carburetor Heat: As required Climb Speed: 60 Kt AFTER LANDING Flaps: Up Landing Light: OFF Transponder: Switch to Stand by Carburetor Heat: OFF Electric Fuel pump: OFF Parking brake: ON Propeller rpm: Keep engine runn ing at 1200 rpm for about 1 minute. Radio and Avionics: OFF Navigation Light: OFF Magnetos: OFF Strobe Light: OFF Master and Generator switch: OFF