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DA20 - Exterioir > AFM - Emergency Procedures > Flashcards

AFM - Emergency Procedures Flashcards

1
Q

Engine failure after take-off with flaps in T/O position

A

60 KIAS

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2
Q

MAX Maneuvering Speed

A

106 KIAS

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3
Q

Airspeed for best glide angle
Maximum Gross Weight– 1764 lbs (800 kg)
Wing Flaps in CRUISE position

A

73 KIAS

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4
Q

Precautionary Landing

with power and Wing Flaps in landing position

A

55 KIAS

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5
Q

Emergency landing with engine off

Wing Flaps in T/O position

A

60 KIAS

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6
Q

Emergency landing with engine off

Wing Flaps in LDG position

A

55 KIAS

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7
Q

Emergency landing with engine off (Wing Flaps CRUISE)

A

64 KIAS

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8
Q

Engine failiure during take-off run

A

(1) Throttle………………………………………… IDLE
(2) Brakes …………………………………………as required
(3) Flaps ……………………………………………CRUISE
(4) Mixture ………………………………………..IDLE CUT-OFF
(5) Ignition Switch …………………………….OFF
(6) GEN/BAT Master Switch …………….OFF

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9
Q

Engine Failure after Take-Off

A

INSUFFICIENT ENGINE POWER
(1) Airspeed …………………………………. 60 KIAS
(2) Throttle ……………………………………FULL
(3) Mixture ……………………………………FULL RICH
(4) Alternate Air …………………………………..OPEN
(5) Fuel Shut-off Valve ………………………………….OPEN
(6) Ignition Switch ………………………………….BOTH
(7) Fuel Pump ………………………………….ON
SHORTLY BEFORE LANDING

(8) Mixture ………………………………… IDLE CUTOFF
(9) Fuel Shut-off Valve ………………………………. CLOSED
(10)Ignition Switch ……………………………….. OFF
(11) Flaps ………………………………….as required
(12)GEN/BAT Master Switch ………………………. OFF
ENGINE INOPERATIVE
Perform emergency landing according to paragraph 3.3.3.

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10
Q

Engine Failure during Flight

A

ENGINE RUNNING ROUGHLY
(1) Mixture ………………………………………………. FULL RICH
(2) Alternate Air ……………………………………. OPEN
(3) Fuel Shut-off ……………………………………. OPEN
(4) Fuel Pump ……………………………………. ON
(5) Ignition Switch …………………………………….. cycle L - BOTH - R - BOTH
(6) Throttle ……………………………………… at present position
(7) No Improvement ………………………………….. reduce throttle to minimum
required power, land as soon
as possible

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11
Q

LOSS OF OIL PRESSURE

A

(1) Oil Temperature ………………………………….. check
(2) If Oil Pressure drops below …………………….land at the nearest suitable
Green Arc above 2100RPM. …………………..airport.
(3) If Oil Pressure drops below …………………….reduce throttle to minimum
Green Arc and oil temperature ………………..required power and land as
is rising ………………………………………………..soon as possible. Be prepared
…………………………………………………………..for engine failure and
…………………………………………………………..an emergency landing.

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12
Q

LOSS OF FUEL PRESSURE

A

(1) Fuel Pump …………………………………………. ON, and land at the nearest
suitable airport.
(2) If fuel pressure is not restored. ……………….Land at nearest suitable airport.
Be prepared for engine failure
and an emergency landing.

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13
Q

ENGING AIR START - PROP ROTATING

A

(1) Airspeed (VIAS) ………………………………….. 73 kts
(2) Mixture ………………………………………………. FULL RICH
(3) Fuel Shut-off Valve ………………………………. OPEN
(4) Ignition Switch …………………………………….. BOTH
(5) Fuel Pump ………………………………………….. ON
(6) Fuel Prime ………………………………………….. ON
(7) Throttle ………………………………………………. 3/4 in (2cm) forward
AFTER SUCCESSFUL RE-START:
(8) Oil Pressure ……………………………………….. check
(9) Oil Temperature ………………………………….. check
(10)Fuel Prime ………………………………………….. OFF
(11) Electrically Powered Equipment……………. ON if required

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14
Q

ENGING AIR START - PROP STOPPED

A

(1) Airspeed …………………………………………….. 73 kts.
(2) Electrically Powered Equipment ……………..OFF
(3) GEN/BAT Master Switch ………………………..ON
(4) Mixture ………………………………………………..FULL RICH
(5) Fuel shut off valve …………………………………OPEN
(6) Fuel Pump …………………………………………..ON
(7) Fuel Prime …………………………………………..ON
(8) Throttle ………………………………………………..3/4 in (2 cm) forward
(9) Ignition Switch ………………………………………START
(10)Ignition Switchwith Push-to-Start (Optional) START (TURN then PUSH)
AFTER SUCCESSFUL RE-START:
(11) Oil Pressure …………………………………………check
(12)Oil Temperature ……………………………………check
(13)Fuel Prime …………………………………………..OFF
(14)Electrically Powered Equipment……………..ON if required

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15
Q

Gliding

A

(a) Wing Flaps ………………………….CRUISE
(b) Airspeed at 1764 lbs (800 kg) ………………….73 KIAS
(c) Glide Ratio 11:1
Example: For every 1000 feet of altitude the aircraft can move forward 11,000
feet or 1.8 NM (3.4 km).

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16
Q

Emergency Landing

A

(1) Airspeed (Flaps in T/O position) ……………. 60 KIAS
(2) Airspeed (Flaps in LDG position) …………… 55 KIAS
(3) Airspeed (Flaps CRUISE) …………………….. 64 KIAS
(4) Fuel Shut-off Valve ………………………………. CLOSED
(5) Mixture ………………………………………………. IDLE CUTOFF
(6) Ignition Switch …………………………………….. OFF
(7) Safety Belts ………………………………………… secured
(8) Radio …………………………………………………. Transmit, 121.5 Mhz, giving
location and intentions
(9) Flaps …………………………………………………. as required
(10)GEN/BAT Master Switch ………………………. OFF
(11) After Touch – Down ……………………………… Apply brakes

17
Q

Precautionary Landing withEngine Power Available

A

(1) Search for a suitable place to land. Special attention must be given to wind
direction and obstacles in the approach path.
(2) Safety Belts ………………………………………….secured
(3) Initiate Descent
(4) Mixture ………………………………………………..FULL RICH
(5) Throttle ………………………………………………..as required
(6) Trim …………………………………………………….as required
(7) Wing Flaps …………………………………………..as required
(observe permissable speed)
(8) Over fly selected landing area (not below 500 ft / 150 m above ground)
to confirm suitability and that approach route is free of obstacles.
(9) Climb up to pattern altitude.
(10)Low pass over flight at a safe altitude to observe any possible obstacles,
such as cables, fences, ditches.
(11) Climb up to pattern altitude.
(12)Radio ………………………………………………….Transmit, giving location and
intentions.
NOTE
Page 3 - 11
Emergency Procedures DA20-C1 Flight Manual
DOC # DA202-C1
Revision 26
May 15, 2012
DOT Approved
(13)Final Approach:
(A) Mixture …………………………………………. FULL RICH
(B) Throttle ………………………………………… as required
(C) Fuel Pump ……………………………………. ON
(D) Wing Flaps …………………………………… LDG
(E) Airspeed ………………………………………. 55 KIAS
(14)Touch-down is to be made with minimum airspeed, nose wheel should be
kept above ground as long as possible.
(15)After Touch-down:
(A) Brake …………………………………………… as required
(B) Fuel Shut-off Valve ………………………… CLOSED
(C) Mixture …………………………………………. IDLE CUT-OFF
(D) Ignition Switch ………………………………. OFF
(E) GEN/BAT Master Switch………………… OFF

18
Q

Engine Fire during Engine-Start-Up on the Ground

A

(1) Fuel Shut-off Valve ………………………………. CLOSED
(2) Cabin Heat …………………………………………..CLOSED
(3) Mixture ………………………………………………..IDLE CUTOFF
(4) GEN/BAT Master Switch ………………………..OFF
(5) Ignition Switch ………………………………………OFF
(6) Evacuate Airplane immediately

19
Q

Engine Fire during Flight

A

(1) Fuel Shut-off Valve ………………………………. CLOSED
(2) Cabin Heat …………………………………………..CLOSED
(3) Airspeed ………………………………………………73 KIAS
(4) Fuel Pump …………………………………………..OFF
(5) Perform emergency landing with engine off according to paragraph 3.3.3.

20
Q

Electrical Fire including Smoke during Flight

A

(1) GEN/BAT Master Switch ………………………. OFF
(2) Cabin Air ……………………………………………. OPEN
(3) Fire Extinguisher …………………………………. use only if smoke development
continues.
IF FIRE EXTINGUISHER IS USED, THE CABIN MUST BE
VENTILATED.
In case the fire is extinguished and electric power is required for continuation of
the flight:
(4) Avionics Master Switch ………………………… OFF
(5) Electrically Powered Equipment ……………. OFF
(6) Circuit Breakers ………………………………….. Push all circuit breakers
(7) Circuit Breakers ………………………………….. Push BATTERY
(8) GEN/BAT Master Switch ………………………. ON BAT 1/2 only
(9) Circuit Breakers ………………………………….. Push GEN & GEN CONTROL
(10)GEN/BAT Master Switch ………………………. ON
(11) Circuit Breakers ………………………………….. Push AVIONICS and
AVIONICS MASTER
(12)Avionics Master Switch ………………………… ON
CAUTION
NOTE
Emergency Procedures DA20-C1 Flight Manual
Page 3 - 14 DOC # DA202-C1 May 15, 2012
Revision 26 DOT Approved
(13)Circuit Breakers ……………………………………Push to activate systems as
required.
(14)Radio ………………………………………………….ON
(15)Land as soon as possible.

21
Q

Cabin Fire during Flight

A

(1) GEN/BAT Master Switch ………………………. OFF
(2) Cabin Air ……………………………………………..OPEN
(3) Cabin Heat …………………………………………..CLOSED
(4) Fire Extinguisher …………………………………..discharge as required
(5) Land as soon as possible

22
Q

Electrical Fire including Smoke on the Ground

A

(1) GEN/BAT Master Switch ………………………. OFF
IF ENGINE IS RUNNING:
(2) Throttle ………………………………………..IDLE
(3) Mixture …………………………………………IDLE CUTOFF
(4) Fuel Shut-off Valve ………………………………..CLOSED
(5) Ignition Switch ………………………………………OFF
(6) Canopy ……………………………………….open
(7) Fire Extinguisher …………………………………..discharge as required

23
Q

Unintentional FlightInto Icing Area

A

(a) Leave icing area (through change of altitude or change of flight direction to
reach area with higheroutside air temp).
(b) Continue to move control surfaces to maintain their moveability.
(c) Alternate Air ………………………………………………..ON
(d) Increase RPM to avoid icing of propeller blades (observe maximum RPM).
(e) Cabin Heat …………………………………………………ON DEFROST

24
Q

Recovery from Unintentional Spin

A

(a) Throttle ………………………………………………………IDLE
(b) Rudder ………………………………………………………fully applied opposite to
direction of spin
(c) Control Stick ……………………………………………….ease forward
(d) Rudder ………………………………………………………neutral,after rotation has
stopped
(e) Wing Flaps …………………………………………………CRUISE
(f) Elevator ……………………………………………………..pull cautiously. Bring airplane
from descent into level flight
position. Do not exceed
maximum permissible speed
(VNE).

25
Q

Landing with Defective Tire on Main Landing Gear

A

(a) Final approach with wing flaps in landing position.
(b) Land airplane on the side of runway opposite to the side with the defective tire
to compensate for change indirection which is tobe expected during final
rolling.
(c) Land with wing slightly tipped in the direction of the non-defective tire. To
increase the maneuverability during rolling, the nose-wheel should be brought
to the ground as soon as possible after touch-down.
(d) To ease the load on the defective tire, the aileron should be fully applied in the
direction of the non-defective tire

26
Q

Total ElectricalPower Failure

A

(1) Battery Circuit Breaker …………………………. If tripped, reset
(2) GEN/BAT Master Switch ………………………. check ON
(3) Master Switch …………………………………….. OFF if power not restored
(4) If Unsuccessful ……………………………………. Land at nearest suitable airport

27
Q

Generator Failure

A

GEN. ANNUNCIATOR ILLUMINATED
(1) GEN/BAT Master Switch ………………………. Cycle Generator Master Switch
OFF - ON
(2) Generator Circuit Breaker …………………….. If tripped, reset
(3) Generator CONTROL Circuit Breaker ……. If tripped, reset
(4) If Generator can not be brought on-line ….. Switch OFF all non-flight
essential electrical consumers.
Monitor Ammeter and
Voltmeter. Land at nearest
suitable airport.

28
Q

Low Voltage Indication (needle in yellow Arc)

A

LOW VOLTAGE INDICATION (NEEDLE IN YELLOW ARC) WHILE AIRPLANE
IS ON THE GROUND
(1) Engine RPM ……………………………………….. Increase RPM until needle is in
the Green Arc. This should
occur before exceeding 1100
RPM.
(2) Non-flight essential electrical consumers ….Switch OFF consumers until
needle is in the Green Arc.
(3) If needle remains in the yellow arc …………..Discontinue any planned flight
and the ammeter is indicating to the activity
left of center (discharge).

29
Q

LOW VOLTAGE INDICATION (NEEDLE IN YELLOW ARC) DURING FLIGHT

A

(1) All non-flight essential electrical……………… Switch OFF
consumers
(2) If needle is remaining in the yellow arc…….Generator Failure
and the ammeter is indicating to the Refer to paragraph 3.3.8.C.
left of center (Discharge).

30
Q

Flap System Failure

A

Flap Position Indicator Failure
(a) Visual check of the flap position
(b) Select airspeed within the range of the white arc marked on the airspeed
indicator
(c) Check all positions of the flap toggle switch (flap stops are fail-safe)
(d) Modify approach and landing as follows:
(1) only CRUISE available: ………………………- raise approach speed by 10 kts
- throttle as required
- flat approach angle
(2) only T/O available: …………………………….- normal approach speed
- throttle as required
- flat approach angle
(3) only LDG available: ……………………………- normal landing

31
Q

Starter Relay Failure

A

(a) Throttle …………………………………………………..IDLE
(b) Mixture …………………………………………………..IDLE CUTOFF
(c) Ignition Switch ………………………………………..OFF
discontinue any planned flight.
Maintenance action is required.

32
Q

Avionics System Failure

A

TOTAL AVIONICS FAILURE:
(a) Check Avionics Master Circuit………………………..If popped, press and monitor
Breaker status. If it pops again, land at
the nearest suitable airport.
(b) Check Avionics Master Switch………………………Toggle avionics master switch,
if avionics system remains offline, pull avionics master
control circuit breaker. Land at
the nearest suitable airport if
operation is not restored.
RADIO SYSTEM OPERATIVE, NO RECEPTION:
(a) Microphone Key ………………………………………….check for stuck Microphone
Key on transceiver display.
(b) Headphones ……………………………………………….check, deactivate SQUELCH
for a few moments,
if SQUELCH not heard, check
headset connection.
RADIO SYSTEM OPERATIVE, TRANSMITTING NOT POSSIBLE:
(a) Selected Frequency …………………………………….check if correct
(b) Microphone ………………………………………………..Install handheld mike as
follows:
- Unplug and remove headset.
- Plug handheld mike in.
- Turn up speaker volume on
audio panel.
Check, if available use a
different headset.
Problem cannot be resolved: ……………….. - switch transponder(if available) to
“COMM FAILURE”
- code if required bythe situation and
permitted by applicable national
regulations

33
Q

Trim System Failure

A

STUCK TRIM:
(a) Circuit breaker …………………………………………….check, press if breaker is
tripped
(b) Rocker switch ……………………………………………..depress in both directions,
wait 5 minutes, try again

RUNAWAY OF TRIM:
(a) Control Stick ……………………………………………….Grip stick and maintain control
of the airplane.
(b) Trim motor circuit breaker …………………………….Pull circuit breaker.
(c) Rocker Switch …………………………………………….Check if depressed.
If the reason for the runaway condition is obvious and has been resolved, push in
(engage) the circuit breaker.

DA20 - Exterioir (14 decks)

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