Pag.1
EMERGENCY
CHECK LIST
EMERGENCY
CHECK LIST
P2002JF
P2002JF
Edizione 23/04/2015
ENGINE FAILURE IMMEDIATELY AFTER TAKE OFF
AIRPLANE EVACUATION
With the engine secured and propeller stopped (if practical):
1
FUEL SHUT OFF VALVE
OFF
2
ENGINE
SECURE
3
PARKING BRAKE
ON
4
RADIO
CALL MAYDAY
5
MASTER SWITCH
OFF
6
SEAT BELTS
UNSTRAP COMPLETELY
7
HEADPHONES
REMOVE
8
CANOPY
OPEN
9
IF CANOPY IS LOCKED OR
BREAK USING THE HAMMER
DOESN’T SLIDE
10
ESCAPE AWAY FROM FLAMES/ HOT ENGINE COMPARTMENT/
SPILLING FUEL TANKS.
ELECTRIC POWER SYSTEM MALFUNCTION
GENERATOR
LIGHT
ILLUMINATES
GENERATOR
LIGHT
MAY
ILLUMINATE FOR A FAULTY ALTERNATOR OR WHEN VOLTAGE IS
ABOVE 16V, IN THIS CASE THE OVER-VOLTAGE SENSOR
AUTOMATICALLY SHUTS DOWN THE ALTERNATOR .
ELECTRIC FUEL PUMP FAILURE
1
2
3
4
5
ELECTRICAL FUEL PUMP SWITCH
ELECTRICAL FUEL PUMP SWITCH
FUEL PRESSURE:
IF FUEL PRESSURE DOESN’T BUILD UP
LAND AS SOON AS POSSIBLE
FUEL PRESSURE
OFF
ON
1
WARNING
2
ENGINE FAILURE DURING TAKE OFF RUN
Following procedure is applicable to shut-down the engine in flight:
1
THROTTLE HAND CONTROL
IDLE
(rotate fully counter-clockwise)
OR
1
THROTTLE STANDARD CONTROL
IDLE
(fully out)
2
RUDDER
KEEP HEADING CONTROL
3
BRAKES
APPLY AS NEEDED
WHEN SAFELY STOPPED:
5
IGNITION KEY
OFF
6
FUEL SELECTOR VALVE
OFF
7
ELECTRIC FUEL PUMP
OFF
8
GENERATOR & MASTER SWITCHES
OFF
Stall speed increases with bank angle and
longitudinal load factor. Acoustic stall warning will
in any case provide a cor-rect anticipated clue of
incipient stall.
3
OR
THROTTLE STANDARD CONTROL
4
5
6
7
IGNITION KEY:
FUEL SELECTOR VALVE
ELECTRIC FUEL PUMP
GENERATOR & MASTER SWITCHES
WARNING
IDLE
(rotate fully counter-clockwise)
IDLE
OFF
OFF
OFF
OFF
A single engine aircraft take off should always be
preceded by a thorough take off emergency pilot
self-briefing. Decision to try an engine emergency
restart right after take off should be taken only if
environmental situation requires it: Pilot shall
never ignore the priority of attentively follow an
immediate emergency landing.
After possible mechanical engine seizure, fire or a
major propeller damage, engine restart attempt is
not recommended.
LOW FUEL PRESSURE
1
2
3
If the fuel pressure indicator falls below the 2.2 psi (0.15 bar):
ELECTRIC FUEL PUMP:
ON
FUEL SELECTOR VALVE:
CHANGE TANK
FUEL QUANTITY INDICATORS
CHECK
If fuel pressure doesn’t build up:
4
LAND AS SOON AS POSSIBLE MONITORING FUEL PRESSURE
4
If engine stops:
LAND AS SOON AS POSSIBLE
APPLY FORCED LANDING PROCEDURE
ENGINE SECURING
Following procedure is applicable to shut-down the engine in flight:
1
THROTTLE HAND CONTROL
IDLE
(rotate fully counter-clockwise)
OR
1
THROTTLE STANDARD CONTROL
IDLE
(fully out)
2
IGNITION KEY
OFF
3
FUEL SELECTOR
OFF
4
ELECTRICAL FUEL PUMP
OFF
5
GENERATOR SWITCH
OFF
AS NEEDED
THROTTLE HAND CONTROL
MONITOR
LAND AIRCRAFT AS SOON AS POSSIBLE
The immediate landing should be planned straight
ahead with only small changes in directions not
exceeding 45° to the left and 45° to the right.
3
TRIM SYSTEM FAILURE
3
MINIMUM 51 KIAS
FIND A SUITABLE PLACE TO LAND SAFELY
At, or right before touch down
FLAPS
WARNING
CHECK RISE
LOCKED CONTROL
Should trim control be inoperative, act as follows:
1
BREAKERS
CHECK
2
TRIM SWITCH LH/RH
CHECK CORRECT POSITION
3
SPEED: ADJUST TO CONTROL AIRCRAFT WITHOUT EXCESSIVE
STICK FORCE
4
LAND AIRCRAFT AS SOON AS POSSIBLE
RUNAWAY
In event of trim runaway, act as follows:
1
TRIM DISCONNECT SWITCH
OFF
2
SPEED: ADJUST TO CONTROL AIRCRAFT WITHOUT EXCESSIVE
STICK FORCE
SPEED
OIL PRESSURE LIMITS EXCEEDANCE
1
2
3
1
2
IF OIL PRESSURE EXCEEDS UPPER LIMIT (7 BAR):
REDUCE ENGINE POWER AS
PRACTICAL
OIL PRESS/OIL TEMP
CHECK WITHIN LIMITS
LAND AS SOON AS PRACTICAL
IF OIL PRESSURE IS UNDER THE LOWER LIMIT (0.8 BAR):
THROTTLE HAND CONTROL
REDUCE MINIMUM
(or STANDARD THROTTLE)
PRACTICAL
LAND AS SOON AS PRACTICAL
THROTTLE HAND CONTROL
(or STANDARD THROTTLE)
IF OIL PRESSURE CONTINUES TO DECREASE:
1
LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING
PROCEDURE
HIGH OIL TEMPERATURE
1
1
2
If oil pressure is low see Low Oil Pressure
If oil pressure is within limits:
THROTTLE HAND CONTROL
REDUCE MINIMUM
(or STANDARD THROTTLE)
PRACTICAL
IF OIL TEMPERATURE DOES NOT DECREASE:
AIRSPEED
INCREASE
LAND AS SOON AS PRACTICAL
IF ENGINE ROUGHNESS, VIBRATIONS, ERRATIC BEHAVIOUR, OR HIGH
CHT IS DETECTED:
1
LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING
PROCEDURE
Pag. 2
EMERGENCY
CHECK LIST
EMERGENCY
CHECK LIST
P2002JF
P2002JF
Edizione 23/04/2015
CHT LIMITS EXCEEDANCE
ENGINE FIRE IN FLIGHT
If CHT is above 135°C:
1
THROTTLE HAND CONTROL
REDUCE MINIMUM
(or STANDARD THROTTLE)
PRACTICAL
2
LAND AS SOON AS PRACTICAL
IF CHT CONTINUES TO RISE AND ENGINE SHOWS ROUGHNESS OR
POWER LOSS:
1
2
3
4
CABIN HEATING
FUEL SELECTOR VALVE
ELECTRIC FUEL PUMP
THROTTLE HAND CONTROL
1
4
THROTTLE STANDARD CONTROL
5
6
IGNITION KEY
CABIN VENT
LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING
PROCEDURE
IN FLIGHT ENGINE RESTART
After a mechanical engine seizure, fire or a
major propeller damage engine restart is not
recommended.
WARNING
1
2
3
4
5
6
7
CARBURETTOR HEAT - IF REQUIRED
ELECTRICAL FUEL PUMP
FUEL QUANTITY INDICATOR
FUEL SELECTOR
IGNITION KEY
IGNITION KEY
THROTTLE HAND CONTROL
(or STANDARD THROTTLE)
After engine restart, if practical, moderate
propeller rpm and throttle increase to allow OIL
and CHT temperatures for stabilizing in the
green arcs.
CAUTION
8
9
ON
ON
CHECK
CHANGE TANK
BOTH
START
SET AS
REQUIRED
IN CASE OF UNSUCCESSFUL ENGINE RESTART
ENGINE
WARNING
7
THROTTLE STANDARD CONTROL
5
6
7
8
CABIN HEAT OFF
GENERATOR & MASTER SWITCHES
PARKING BRAKE
AIRCRAFT EVACUATION
FULL POWER
(FULL IN)
OFF
OFF
SET
PERFORM IMMEDIATELY
ENGINE FIRE DURING TAKE OFF
1
BEFORE ROTATION: ABORT TAKE OFF
THROTTLE HAND CONTROL
IDLE
(ROTATE
COUNTER
CLOCKWISE)
OR
1
THROTTLE STANDARD CONTROL
2
3
RUDDER
BRAKES
4
5
6
7
8
9
10
With aircraft under control:
FUEL SELECTOR
ELECTRICAL FUEL PUMP
IGNITION KEY / CABIN HEAT
GENERATOR & MASTER SWITCHES
PARKING BRAKE
AIRCRAFT EVACUATION
Do not attempt engine restart
LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING
PROCEDURE
1
2
3
4
CABIN HEATING
CABIN VENTS
CANOPY
TRY TO CHOKE THE FIRE
OFF
OPEN
OPEN, IF NECESSARY
DIRECT THE FIRE EXTINGUISHER
TOWARDS FLAME BASE
IF SMOKE PERSISTS:
GENERATOR & MASTER SWITCHES
OFF
LAND AS SOON AS POSSIBLE AND EVACUATE THE AIRCRAFT
5
6
CAUTION
If the MASTER SWITCH is set to OFF, consider
that flaps extension and pitch trim operation
would be not possible.
ELECTRICAL SMOKE/FIRE IN THE CABIN ON
GROUND
FULL POWER
(ROTATE CLOCKWISE)
4
OFF
OPEN
ELECTRICAL SMOKE IN CABIN DURING FLIGHT
SECURE
OFF
OFF
OFF
OR
FULL POWER
(FULLY IN) UNTIL THE
ENGINE STOPS
CABIN FIRE/
LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING
PROCEDURE
FUEL SELECTOR
ELECTRICAL FUEL PUMP
IGNITION KEY
THROTTLE HAND CONTROL
FULL POWER UNTIL THE
ENGINE STOPS
OR
ENGINE FIRE ON THE GROUND
1
2
3
4
OFF
OFF
OFF
IDLE
(FULL OUT)
KEEP HEADING
AS REQUIRED
OFF
OFF
OFF
OFF
OFF
SET
PERFORM
1
2
GENERATOR SWITCH
THROTTLE HAND CONTROL
3
4
5
6
7
OR
THROTTLE STANDARD CONTROL
IGNITION KEY
FUEL SELECTOR VALVE
MASTER SWITCH
AIRCRAFT EVACUATION
OFF
IDLE (ROTATE FULLY
COUNTER-CLOCKWISE)
IDLE (FULLY OUT)
OFF
OFF
OFF
PERFORM
FORCED LANDING WITHOUT ENGINE POWER
1
FLAP/SPEED
UP/69 KIAS
FIND SUITABLE PLACE TO LAND SAFELY, APPROACH IT UPWIND
3
FUEL SELECTOR VALVE
OFF
4
ELECTRIC FUEL PUMP
OFF
5
IGNITION KEY
OFF
6
SAFETY BELTS
TIGHTEN
7
CANOPY LOCKS
CHECK LOCKED
When certain to land
8
FLAPS
AS REQUIRED
9
GENERATOR AND MASTER SWITCHES
OFF
Glide ratio:12.8 – With no wind every 1000ft AGL it is possible to cover ca. 2 NM
POWER ON FORCED LANDING
1
FLAP/ SPEED
UP/69 KIAS
FIND SUITABLE PLACE TO LAND SAFELY, APPROACH IT UPWIND
2
SAFETY BELTS
TIGHTEN
3
CANOPY LOCKS
CHECK LOCKED
When certain to land, right before touchdown
4
FLAP
AS REQUIRED
5
FUEL SELECTOR VALVE
OFF
6
ELECTRIC FUEL PUMP
OFF
7
IGNITION KEY
OFF
8
GENERATOR AND MASTER SWITCHES
OFF
Pag. 3
EMERGENCY
CHECK LIST
P2002JF
Edizione 23/04/2015
LANDING WITH A FLAT NOSE TYRE
1
2
3
4
5
PRE-LANDING CHECKLIST
COMPLETE
FLAPS
LAND
Land and maintain aircraft NOSE HIGH attitude as long as possible
As aircraft stops 4
ENGINE SECURING
PERFORM
AIRPLANE EVACUATION
PERFORM
LANDING WITH A FLAT MAIN TYRE
1
2
3
4
5
6
7
If it’s suspected a main tyre defect or it’s reported to be defective
PRE-LANDING CHECKLIST
FLAP
COMPLETE
LAND
Land aeroplane on side of runway opposite to defective tyre to compensate the change
in direction which is to be expected during final rolling
Touchdown with the GOOD TIRE FIRST and hold aircraft with the flat tyre off the
ground as long as possible by mean of aileron and rudder control.
As aircraft stops
ENGINE SECURING
AIRPLANE EVACUATIO
PERFORM
PERFORM
RECOVERY FRON UNINTENTIONAL SPIN
If unintentional spin occurs, the following recovery procedure should be used:
1
THROTTLE HAND CONTROL:
IDLE (rotate fully
counter-clockwise)
OR
THROTTLE STANDARD CONTROL
IDLE (fully out)
RUDDER
FULL OPPOSITE
STICK
CENTER/ NEUTRAL
As the spin stops
4
RUDDER
SET NEUTRAL
Smoothly recover avoiding to exceed VNE and maximum n=+3.8
5
THROTTLE HAND CONTROL
RESTORE ENGINE POWER
1
2
3
WARNING
Keep full rudder against rotation until spin has
stopped.
One complete turn and recovery takes around
500 feet.
UNINTENTIONALLY FLIGHT INTO ICING
CONDITIONS
Carburettor ice is possible when at low rpm in visible moisture (visibility < 5 km, near, mist,
clouds, rain, snow or hail) and OAT < 10°C. Airbox carburettor heater is designed to prevent
carburettor ice, less effectively functions as a de-icing system.
1
2
3
4
5
CARBURETTOR HEATING
ON
Immediately fly away from icing conditions ( changing altitude and direction
of flight, out of clouds, visible moisture, precipitations)
FLIGHT CONTROLS
Continue to move to maintain their movability
PROPELLER SPEED
CABIN HEAT
INCREASE RPM.
ON
In case of ice formation on wing leading edge, stall speed would increase
.
This Check List is compliant to Section 3 – Emergency Procedure of
the Aircraft Flight Manual Doc. No. 2002/028 3rdEdition – Rev. 3
issued by Costruzioni Aeronautiche TECNAM srl - Via Maiorise
CAPUA (CE) – Italy on the 28th February 2014.
AIRCRAFT MODEL:P2002-JF
EASA TYPE CERTIFICATE NO:A .006(DATED 2004,MAY27TH)
Sky Services Flight Academy
Head of Training
_______________________
EMERGENCY
CHECK LIST
P2002JF
Pag. 4
EMERGENCY
CHECK LIST
P2002JF
EMERGENCY
CHECK LIST
Edizione 23/04/2015
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P2002JF