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PC 12/47E > 3 - EMERGENCY PROCEDURES > Flashcards

3 - EMERGENCY PROCEDURES Flashcards

1
Q

Crew Alert System RED

A

WARNING messages which require IMMEDIATE CORRECTIVE action by the pilot.

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2
Q

Crew Alert System AMBER

A

CAUTION messages which require the pilots ATTENTION but not an immediate action

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3
Q

Crew Alert System CYAN

A

ADVISORY messages which indicate a system condition, which requires PILOT AWARENESS and may require ACTION

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4
Q

Crew Alert System WHITE

A

Status messages which are only shown on the ground and indicate a maintenance action is required

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5
Q

Flight Alerting System (FAS)

A

FAS messages are given when necessary on the PFD to warn of a condition that requires immediate action from the pilot. FAS messages are directly related to the operarion of the aircraft. All the FAS messages are accompanied by a voice callout and can only be cancelled by correting the aircraft condition

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6
Q

FAS MESSAGE - STALL

A

Reduce AOA

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7
Q

FAS MESSAGE - GEAR

A

Extend Landing Gear

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8
Q

FAS MESSAGE - CABIN

A

Check System MFD ENVIRONMENT window

If shows > 0.072 psi:
CPCS CABIN PRESSURE switch DUMP

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9
Q

FAS MESSAGE - NO TAKEOFF

A

Check aircraft configuration is correct for takeoff
Flaps: set 15° or 30º
CL: Set Flight Idle
Aileron, rudder, stabilizer trim: Set green range

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10
Q

FAS MESSAGE - OVERSPEED

A

Reduce airspeed

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11
Q

Operating Maneuvering Speed (Vo)

A

10450 lb - 166 kt
9921 lb - 161 kt
9480 lb - 158 kt
9039 lb - 154 kt
8380 lb - 148 kt
7940 lb - 144 kt
7500 lb - 140 kt
7060 lb - 136 kt
6610 lb - 132 kt
6170 lb - 127 kt
5730 lb - 123 kt

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12
Q

Best Glide (Propeller feathered)

A

10450 lb - 119 kt
9920 lb - 116 kt
9040 lb - 110 kt
8160 lb - 105 kt
7280 lb - 99 kt
6400 lb - 93 kt

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13
Q

Landing approach speed with ice accretion on the airframe - (AFTER FAILURE OF):

A
  • After failure of: - Minimum Approach speed:

Pneumatic Deice boots (flap limit 0°) - 130kt

AOA probe deice and/or Pitot static probe deice and/or pusher ice mode (flap position limit 15°) - 105kt

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14
Q

Balked landing (go around) (After failure of: Pneumatic Deice boots)

A

Pneumatic Deice boots (flap limit 0°)
(TO/Pwr, flaps 0°, LG down, Pusher ice Mode): 130 kt

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15
Q

REJECTED TAKEOFF (Not engine related)

A
  1. PCL - Idle
  2. Reverse - As required
  3. Braking - As required

If cannot be stopped on the reaming runway:

  1. PCL - Idle
  2. Condition Lever - CUT OFF/FEATHER
  3. FUEL EMERG shut off - Press latch down and pull lever up
  4. MASTER POWER switch - EMERGENCY OFF

After aircraft stopped

  1. AIRCRAFT - Evacuate

CAUTION: If any further taxing is required soft brake pedals and/or wheel fusible plugs release may occur, due to overheating.

CAUTION: A rejected takeoff may cause overheating of whell and brake assembly components. The main wheels and brakes should be inspected for damage in accordance with the respective componente manuals before the next flight.

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16
Q

ENGINE FAILURE BEFORE ROTATION

A
  1. PCL - Idle
  2. Braking - As required

If overrun or collision is likely

  1. CONDITION LEVER - CUT-OFF/FEATHER
  2. FUEL EMERG shut off - Press latch down and pull lever up
  3. MASTER POWER switch - EMERGENCY OFF
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17
Q

ENGINE FAILURE AFTER ROTATION - LANDING GEAR DOWN (Total power loss)

A
  1. Aircraft - Land straight ahead, turning only to avoid obstructions (max recomend bank angle 30º L/R)
  2. Flaps - 40º
  3. Final Approach Speed (10450 lb) - 88 kt - AOA centered
  4. PCL - Idle
  5. CONDITION LEVER - CUT-OFF/FEATHER
  6. FUEL EMERG shut off - press latch down and pul lever up

aft touchdown

  1. MASTER POWER switch - EMERGENCY OFF

aft acft stopped

  1. AIRCRAFT - Evacuate
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18
Q

ENGINE FAILURE AFTER ROTATION - LANDING GEAR UP (total power loss)

A
  1. LANDING GEAR - Down, if landing site allows, otherwise keep landing gear up
  2. Flaps - 40°
  3. Final approach speed (10450 lb)
    - 101 kt - flap 15
    - 91 kt - flap 30
    - 88 kt - flap 40
  4. PCL - Idle
  5. Condition Lever - CUT-OFF/FEATHER
  6. FUEL EMERG shut off - press lach down and pull lever up

aft touch down

  1. MASTER POWER switch - EMERGENCY OFF

when stopped

  1. Aircraft - Evacuate
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19
Q

ENGINE FAILURE IN FLIGHT - PARTIAL POWER LOSS

indications
- Un-commanded engine power reduction
- No response to PCL movement

note:
Below NG 58% the ACS will go off. At approx 35% both generator will go off line

A
  1. PCL - Idle
  2. Manual Override Lever (MOR) - Pull uptowards and move slowly forward until engine responds, wait and let engine stabilize

if engine compressor stalls and/or ITT exceeded

  1. Manual Override Lever (MOR) - Retard and move very slowly forward

if Ng falls below 50%

  1. Starter - Push momentarily
  2. Manual Override Lever - Move forward to required power (NG>80%)
  3. Aircraft - Land as soon as practical

In descent and until touch down

  1. Manual Override Lever - Maintain at least 75%

aft touch down

  1. Condition Lever - CUT-OFF/FEATHER

Note: When the starter is engaged both generator will go off-line and Main, AV2 Non Ess, Cab, GEN1 and GEN 2 busses go off. Upper MFD and copilots PFD will go blank 7.5 sec after NG is > 50% both generator will automatically come on-line and the ACS will come on at NG > 62%.

CAUTION
WHEN MOR IS IN OPERATION, DO NOT PERMITE NG FALL BELOW 75% AND OBSERVE ENGINE LIMITATIONS.

WARNING
DEPENDING ON AIRFIELD CONDITION AND AIRCRAFT WEIGHT AND CONFIGURATION, THE AVAILABLE POWER MIGHT NOT BE SUFFICENTE TO ENSURE A GO AROUND

WARNING
DO NOT MOVE PCL AFT OF IDLE DETENT

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20
Q

ENGINE FAILURE IN FLIGHT - TOTAL POWER LOSS

A
  1. Autopilot - Use SPD (best glide speed) and HDG/T or NAV mode
    - Best glide (propeller feathered)
    10450 lb - 119 kt
    9920 lb - 116 kt
    9040 lb - 110 kt
    8160 lb - 105 kt
    7280 lb - 99 kt
    6400 lb - 93 kt
  2. PCL - Idle
  3. Condition Lever - CUT-FF/FEATHER
  4. Aircraft - Proceed to nearest airfiel or landing site avoidin high terrain
  5. Reamaining fuel - check
  6. Aircraft - Carry out Air Start

If Cabin Altitude is above 10.000ft

  1. Aircraft - Make an Emergency descent
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21
Q

AIR START - WITH STARTER

A
  1. PCL - Idle
  2. CONDITION LEVER - CUT-OFF/FEATHER
  3. FUEL EMERG shut off - Full in
  4. BAT 1 and BAT 2 - ON
  5. Air start envelope - check
  6. IGNITION switch - ON
  7. STARTER - Push momentarily
  8. CONDITION LEVER (NG >13%) - FLIGHT IDLE
  9. ITT and NG - Monitor

when engine has relit NG>60%

  1. IGNITION switch - AUTO
  2. FUEL PUMP switches - AUTO
  3. GEN 1 and 2 - Check volts and amps
  4. Eletrical Equipment - As required

if air starts is unsuccessful

  1. Aircraft - Make a forced landing

WARNING
DOT NOT ATTEMPT MORE THAN ONE AIR START. REPEATED AIR START ATTEMPTS COULD DISCHARGE THE BATTERY TO A LEVEL THAT WOULD NO BE ABLE TO SUPPORT ESSENTIAL ELECTRICAL SERVICES.

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22
Q

PROPELLER - LOW PITCH

indidication: CAS Warning - Propeller Low Pitch, and voice callout “Propeller Low Pitch”

A
  1. PCL - Ensure forward of idle detent.

if it is not possible to maintain speed and height:

  1. CONDITION LEVER - CUT-OFF/FEATHER
  2. Aircraft - Emergency descent and landing procedures
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23
Q

ENGINE NP

indication: CAS warning or caution - Engine NP

A

A. ON GROUND IMMEDIATELY AFTER ENGINE START

  1. NP - Check NP RPM indication

if PROP RPM below 950

  1. Select as convenient either:

Condition Lever - FLIGHT IDLE
ELECTRICAL HEAT/COOL - INHIBIT
ACS BLEED AIR - INHIBT
PCL - Retard aft of idle detent until NP is ABOVE 950 rpm

B. ON GROUND

  1. NP - Check NP RPM indication

if propeller RPM is below 930:

  1. PCL - Retard aft of idle detent or increase power until NP is above 950 rpm.

if propeller rpm is above 1760

  1. PCL - Reduce power.

C. IN FLIGHT

  1. NP - Check NP RPM indication

if propeller RPM is below 1640

  1. PCL - Increase power
  2. Aircraft speed - Increase

if propeller RPM is above 1760

  1. PCL - Reduce power
  2. Aircraft speed - Reduce

if NP remains between 1760 and 1870 RPM

  1. Aircraft - Continue flight, at low aircraft apeed, using minimum possible power.

if NP is above 1870 RPM

  1. PCL - Reduce power (to idle if necessary)
  2. Aircraft speed - Reduce 120 kias or below
  3. Aircraft - Land as soon as possibel, using minimum power, If possible always retain glide capability, to the selected landing airfield, in case of total propeller failure.
24
Q

ENGINE NG

Indication: CAS warning or caution - Engine NG

A
  1. NG - Check NG% indication

if NG is above 103.5%

  1. PCL - Reduce power

if NG is above 104%

  1. PCL - Reduce power
  2. Aircraft speed - Reduce to 120 kt or below
  3. Aircraft - Land as soon as possible, using minimum power. If possible always retain lgide capability, to the selected landing airfield, in case of total engine failure

if NG is below 60%

A. ON GROUND IMMEDIATLEY AFTER ENGINE START

  1. Select as conveniente either

CONDITION LEVER - FLIGHT IDLE
or
ELECTRICAL HEAT/COOL - INHIBIT
or
ACS BLEED AIR - INHIBIT

B. IN FLIGHT
1. PCL - Increase power
2. Aircraft speed - Increase

if engine does not respond to PCL inputs:

  1. Aircraft - Carry out engine failure in flight partial power loss procedure
25
Q

ENGINE TORQUE

Indication: CAS warning or caution - Engine Torque

A
  1. TORQUE - Check indication

if torque above 44.2 psi

  1. PCL - Reduce power

if torque CAS warning or caution remains

  1. Aircraft - Land as soon as possible, using minimum power. If possible always retain glide capability, to the selected landing airfield, in case of total engine failure.
26
Q

ENGINE ITT

Indication: CAS warning or caution - Engine ITT

A
  1. ITT - Check ITT indication

if ITT above 850° C

  1. PCL - Reduce power

if ITT warning or caution remains

  1. Aircraft - Land as soon as possible, using minimum power. If possible always retain glide capability, to the selected landing airfiel, in case of total engine failure.
27
Q

ENGINE OIL PRESSURE

Indication: CAS warning or caution - Engine Oil Press

A
  1. Oil - Check OIL P PSI indication

if oil pressure warning or caution is confirmed

  1. NG - Check NG above 72%
  2. Torque - Reduce to below 24 PSI

if oil pressure warning or caution remains

  1. Aircraft - Land as soon as possible, using minimum power. If possible always retain glide capability, to the selected landing airfiel, in case of total engine failure.
28
Q

ENGINE OIL TEMPERATURE

Indication: CAS warning or caution - Engine Oil Temp

A

A. ON GROUND

  1. Oil - Check OIL T °C indication

if oil temperature is high

  1. Aircraft - Position into wind
  2. CONDITION LEVER - FLIGHT IDLE
  3. PCL - Increase power

of oil temperature does not return to normal

  1. ELECTRIAL HEAT/COOL switch - INHIBIT

if Engine Oil Temp warning or caution remains:

  1. Engine - Shut down engine. Maintenance required

if oil temperature is low (below -40º C);

  1. Engine - Dot not start. Preheating is required.

If oil temperature is -40°C or above

  1. PCL - Use low power settings until oil temperature is above 10ºC.

B. IN FLIGHT

  1. Oil - Check OIL T ºC indication

if oil temperature is high

  1. PCL - Reduce power

if oil temperature dos not returno to normal

  1. Landing gear - Extend

if Oil Temp warning or caution remains

  1. Aircraft - Land as soon as practical

after landing

  1. Engine - Shut down engine. Maintenance required.
29
Q

ENGINE STARTER ENGAGED

indication: CAS warning - Stater Engaged

A

A. ON GROUND (during an engine start)

  1. CONDITION LEVER - CUT-OFF/FEATHER
  2. START INTERRUPT switch - Push
  3. BAT 1 and BAT 2 switches - OFF
  4. EXT PWR (if available) - OFF
  5. Aircraft - Maintenance action required

B. IN FLIGHT (following an air start)

  1. BUS TIE Circuit Braker - Pull
  2. STARTER Circuit Breaker - Pull
  3. GEN 1 and GEN 2 switches - OFF

if Starter Engaged warning extinguished

  1. GEN 1 and GEN 2 swiches - OFF
  2. BUS TIE Circuit Breakes - Reset

if Starter Engaged warning remains

  1. BAT 2 switch - OFF
  2. GEN 1 switch - RESET then ON
  3. BAT 1 switch - Check, ON

NOTE
The CAS Starter Engaged warning will remain ON.

30
Q

ENGINE OIL CHIP

Indication: CAS caution - Engine Chip

A

A. ON GROUND: Before engine start

  1. Do not starg engine - Maintenance required

B. ON GROUND: After engine start or after landing

  1. Aircraft - Return to parking area
  2. Engine - Shut down

c. IN FLIGHT

  1. Aircraft - Check and monitor engine parameters
  2. PCL - Reduce power to minimun required for safe flight
  3. Aircraft - Land as soon as practical
31
Q

FIRE DETECT

Indication: CAS caution - Fire detector
Condition: A fault in the fire detection system has occurred

A

A. ON GROUND

  1. Engine - Do not start engine, shut down engine
  2. Engine Maintenance action required.

B. IN FLIGHT

  1. Engine - Check indication
  2. Aircraft - Land as soon as practical
32
Q

ENGINE FIRE

Indication: CAS warning - Engine fire and voice callout “fire”. Possible smoke and/or fumes

A

A. ON GROUND
1. PCL - Idle
2. CONDITION LEVER - CUT OFF/FEATHER
3. ACS EMER shut off - Pull
4. FUEL EMER shut off - Press latch down and pull lever up
5. RADIO - Emergency call
6. MASTER POWER switch - OFF
7. Parking brake - OFF (if possible)
8. Aircraft - Evacuate
9. Fire - Extinguish

B. IN FLIGHT
1. Engine Power - Reduce to minimum acceptable according to flight situation
2. ACS EMER shut off - Pull
3. Main OXYGEN lever - Confirm ON
4. Crew oxygen masks - ON (Follow precedure to don the masks)
5. Crew Oxygen - EMGCY
if smoke goggles worn
a. vent valve - OPEN
6. PASSENGER OXYGEN selector - ON
7. Systems MFD PAX OXY advisory - confirm ON
8. Passangers - Instructo to don masks
9. Aircraft - Check fire

if confirmed that fire exists
a. FUEL EMER shut off - press latch down and pull lever up
b. CONDITION LEVER - CUT-OFF/FEATHER

if smoke evatuation is required
a. ACS EMERG shut off - PULL
b. CABIN PRESSURE switch - DUMP

When cabin differential pressure is zero:
c. DV window - Open
d. FANS VENT switch - LOW

  1. Aircraft - Carry out emergency descente and landing.
33
Q

COCKPIT/CABIN FIRE, SMOKE OR FUME, SMOKE EVACUATION

A
  1. Main OXYGEN lever - Confirm ON
  2. Crew oxygen masks and smoke goggles - ON
    a. Remove the normal headset
    b. Put the oxygen mask on
    c. Put the smoke goggles on
    d. put the normal headset back on
    e. Set MEC SELECT switch on the rear left panel to MASK
  3. Crew Oxygen - EMGCY
  4. PASSENGER OXYGEN selector - ON
  5. Systems MFD PAX OXY adivisory - Confirm ON
  6. Passenger - Instruct to don masks
  7. Aircraft - Iniciate descent to below 10.000ft or MSA
  8. Aircraft - Proceed to nearest airfield

if smoke evacuation is required:
a. ACS EMER shut off - Pull
b. CABIN PRESSURE switch - DUMP
when cabin pressure differencia is zero
c. DV window - Open
d. VENT FANS - Low

  1. Fire Extinguisher - Use if required

as soon as time permites and source is know electrical:

  1. Associated electical equipment - OFF (CB’s)
  2. BUS TIE CB (overhead) - Pull
  3. GEN 2 switch - OFF
  4. BAT 2 switch - OFF
  5. CABIN HEATER CB - Pull

if smokes still persists with suspect electrial

  1. Aircraft - VMC condition (if possible)
  2. EPS switch - CHECK ARMED

commence flying wiht ESIS

  1. GEN 1 switch - OFF
  2. BAT 1 swithc - off

if smokes still persists with suspect electrial

  1. MASTER POWER switch - EMRGY OFF

Emergency landing gear procedures

34
Q

MAXIMUM RANGE DESCENT - AFTER ENGINE FAIL

A
  1. PCL - Idle
  2. CONDITION LEVER - CUT OFF/FEATHER
  3. Aircraft configuration - LG UP FLAPS 0
  4. Airspeed:
    119kt - 10450lb
    116kt - 9920lb
    110kt - 9040lb
    105kt - 8160lb
    99kt - 7280lb
    93kt - 6400lb

137kt - Icing conditions

  1. All occupants - Check seat belts
  2. Main OXYGEN lever - Confirm ON
  3. Crew oxygen masks - Prepare. Put before 10.000 cabin altitude
  4. PASSENGER OXYGEN - ON, calculate duration
  5. System MFD PAX OXY adivsory - ON
  6. Pax - Instruct to don masks
  7. Electrical load - Monitor bat amps
  8. Engine - Restart as soon as possible
    13 . Rate of descente - Adjust to achieve cabin altitude of 10.000ft before oxygen exhausted.

Below 10000ft

  1. ACS EMER shut off - Pull
    15 - Aircraft - Forced landing
35
Q

MAXIMUM RATE DESCENT

A
  1. PCL - IDLE
  2. Landing Gear - DOWN
  3. Aircraft speed - Mmo/Vmo
  4. All occupants - Check seatbelts
  5. Main OXYGEN lever - Confirm ON
  6. Crew oxygen masks - Prepare, put before 10.000 cabin altitude
  7. PASSENGER OXYGEN selector - ON, calculated duration
  8. Systems MFD PAX OXY adivisory - On
  9. Passangers - Masks

CAUTION
In turbulence reduce airspeed to 170 KT

36
Q

FORCED LANDING (engine cut-off/feather)

A
  1. PCL - Idle
  2. CONDITION LEVER - CUT-OFF/FEATHER
  3. FUEL EMENG - Pull
  4. Cabin Pressure - Dump
  5. Best glide speed:
    119kt - 10450lb
    116kt - 9920lb
    110kt - 9040lb
    99kt - 7280lb
    93kt - 6400lb
  6. Seat backs - upright
  7. Seat belts - fastened
  8. Pax - brief
  9. ELT - set ON
    if possible
    a. landing gear - DOWN
    if not suitable for gear
    a. LD UP
    b. flaps 40 - 88kt
  10. Final approach speed - 88kias (MTW)

aft touch down

  1. MASTER POWER switch - EMGCY OFF

after sttoped

  1. Aircraft - Evacuate
37
Q

LANDING WITH MAIN LANDING GEAR UNLOCKED

A
  1. Aircraft - Confirm landing gear position with tower or other aircraft

CAUTION
IF ONE MAIN LANDING GEAR IS NO DOWN, IT IS RECOMMENDED TO LAND WITH GEAR UP.

if failed gear is down but not locked

  1. Fuel weight - Reduce
  2. Passagers - Brief
  3. Flaps - 40
  4. Final approach speed - 88kt for MLW (aoa centered)
  5. Touchdown - gently, avoid sideslip during touchdown
  6. Landing - lower nose wheel immediately to maintain lateral control
  7. Rol Out - use full aileron during roll-out to lift the wing with the failed LG.
  8. PCL - idel
  9. Condition Lever - CUT-OFF/FEATHER
  10. MASTER POWER switch - EMGCY OFF
38
Q

LANDING WITH NOSE LANDING GEAR UNLOCKED

A
  1. PAX - brief
  2. Flaps - 40
  3. Final approach speed - 88 for MLW (aoa centered)
  4. Landing - Land on main wheels, keep nose high
  5. CONDITION LEVER - CUT-OFF/FEATHER
  6. MASTER POWER switch - EMRCY OFF
  7. Landing - Lower nose wheel slowly
  8. Aircraft - avoid braking
39
Q

LANDING WITH GEAR UP

A
  1. PAX - Brief
  2. Approachs - Standart
  3. Flaps - 40
  4. Final approach speed - 88kt for MLW (aoa centered)
  5. CABIN PRESSURE switch - DUMP

when runway is assured

  1. PCL - Idle
  2. CONDITION LEVER - CUT-OFF/FEATHER
  3. FUEL EMERG shut off - pull
  4. Aircraft - flare out

aft touch down

  1. MASTER POWER switch - EMERGCY OFF

aft the aircraft has stopped

  1. Acrft - Evacuate
39
Q

LANDING WITHOUT ELEVATOR CONTROL

A
  1. PAX - Brief
  2. Landing Gear - Down
  3. Flaps - 40
    4 . Final approach speed - 90kias
  4. Power - Set as necessary to maintain speed and 300 to 500 ft/mim rate of descent.
  5. Aircraft - Use stab trim to adjust pictch

when closing ground

  1. Aircraft - Reduce rate of descent by increasing pitch and/or power
  2. Power - Reduce pregressively
39
Q

LANDING WITH IMMOBILIZED HORIZONTAL STABILIZER

A
  1. Aircraft - Fly at indicated airspeed which reduces elevator forces to minimum
  2. Flaps - At a safe altitude select flap required for landing
  3. Landing - Land using normal procedures holding elevator forces
40
Q

DITCHING

A
  1. Landing Gear - UP

CAUTION
HEAVY SWELL WITH LIGHT WIND, DITCH PARALLEL TO THE SWELL, STRONG WIND, DITCH INTO THE WIND

  1. PAX - Brief
  2. ELT - ON
  3. FLAPS - 40
  4. Final approach speed - 88kias for mlw (aoa centered)
  5. CABIN PRESSURE switch - DUMP
  6. PCL - Idel
  7. CONDITION LEVER - CUT-OFF/FEATHER
  8. if time permits

a. CABIN PRESSURE - AUTO
b. CBCS SYSTEM MODE switch - MANUAL
c. MANUAL CONTROL - set and hold descente for 30 sec (to close OFV)

  1. FUEL EMERG shut off - latch down and pull up
  2. Ditching - Ditch with a low rate of descente
  3. MASTER POWER switch - EMERGCY OFF
  4. Aircraft - Evacuated with emergency exit only
41
Q

LG EMERGENCY EXTENSION

indication: Incorrect indication on LG indicatior lights and/or CAS caution HYDRAULICS is on. Red unlocked lights on and/or green lights not illuminated.

A
  1. LG Selector - DOWN
  2. Airspeed - 110 kt (power idle mementarily)

if 3 greens light not illuminated within 39 sec:

  1. Hand pump - Use full strokes, pump until 3 green lights are on. Complete lowering takes about 80 strokes.

if 3 green slights still not illuminated

  1. Aircraft - Yam the aircraft left and right to lock the main landing gear
  2. Airspeed - Reduce to minimum safe to improve nose gear locking

if not successful

carry out emergency landing

42
Q

STICK PUSHER FAILURE

indication: CAS caution - Pusher

A

A. ON GROUND
1. Pusher test - carry out

if caution persists
2. Aircraft - No flight permitted

B. IN FLIGHT
1. Pusher test - Carry out

if shaker 1 and 2 active and PUSHER caution extinguised
2. Aircraft - No further action

if shaker 1 or 2 not active or PUSHER cation persists

THE AIRCRAFT IS NOT STALL PROTECTED

43
Q

INADVERTENT PUSHER OPERATION

indication: Non-cammanded pusher operation, rapid nose pitch-down motion.

note: Control whell force to stop pusher operation is 60 to 65 pounds.

A
  1. Control whell - Hold against pusher action
  2. PUSHER INTR switch - Press and hold
  3. PUSHER SYS GND CB - Pull
  4. PUSHER SYS CB - Pull
  5. If shaker continues to operate - Carry out inadvertent shaker procedure

THE AIRCRAFT IS NOT STALL PROTECTED

  1. Airspeed not below 1.3 Vs

AOA MAY NOT BE RELIABLE

  1. Pusher test - Carry out to check shaker availability
44
Q

INADVERTENT SHAKER OPERATION

indication: Non-cammanded shaker operation.

A
  1. AOA - Decrease
  2. IAS - Increase

if shaker continues to operate

  1. STALL WARN 1 CB - Pull
  2. STALL WARN 2 CB - Puall

WARNING: THE AIRCRAFT IS NOT STALL PROTECTED

  1. Airspeed not below 1.3 Vs

CAUTION
AOA MAY NOT BE RELIABLE

45
Q

PITCH TRIM RUNAWAY

Indication: CAS warning - “Pitch trim runaway” and voice callout

A
  1. TRIM INTERRUPT switch - INTR
  2. PITCH TRIM CB - Pull
  3. TRIM INTERRUPT switch - NORM

if trim ranaway continues

  1. TRIM INTERRUPT switch - INTR
  2. PITCH TRIM ALTN CB - Pull
  3. PITCH TRIM CB - Close
  4. TRIM INTERRUPT switch - NORM

NOTE
Reduce speed if control forces are high

The autopilot will disconnect when Trim Interrupt is operated
If the pitch trim has failed the autopilot is not opeartive

if main stabilizer trim has failed
8. Pitch trim - Use ALTERNATE STAB TRIM

46
Q

TRIM RUNAWAY

Indication: Non-commanded trim operation, rapidly increasing out of trim forces

A
  1. TRIM INTERRUPUT switch - INTR
  2. CB of failed trim - Pull
    (PITCH TRIM, PITCH TRIM ALTN, AIL TRIM, RUD TRIM.
  3. TRIM INTERRUPT switch - NORM

NOTE
Reduce speed if control forces are high
The autopiloto will disconnect when TRIM INTERRUPT is operated.

47
Q

NO MAIN STABILIZER TRIM

A
  1. TRIM INTERRUPT - Check at NORM
  2. ALTERNATE STAB TRIM - Operate as required
48
Q

ELECTRICAL POWER LOSS

Indication: loss of electrical power

A
  1. MASTER POWER switch - Check ON and guarded
  2. BATT and GEN switches - Check ON

if indication remains:

  1. Aircraft - Land as soon as possible
49
Q

AVIONICS 2 BUS

Indication: CAS Caution - Avionics 2 Bus

Condition: Avionics 2 bus voltage below 22V

A
  1. AV 2 BUS switch - Confirm set to ON
  2. AV 2 CB - Confirm Set
  3. Aircraft - At the pilots discretion continue flying or not.
50
Q

AVIONICS 1 BUS

Indication: CAS CAUTION - Avionics 1 bus

Condition: Avionics 1 bus voltage below 22V

A
  1. AV 1 BUS switch - Confirm set ON
  2. AV 2 CB - Confirm set
  3. STBY BUS switch - Confirm set ON

note
The systems connected to the Standby bus on the left rear CB panel will be operative

  1. Aircraft - At the pilots discretion continue our not flying.
51
Q

ESSENTIAL BUS

Indication: CAS warning - Essential bus
Condition: Essential bus voltage is below 22V

A
  1. Overhead Panel - Confirm EPS switch is in ARMED position and EPS ON caption is on
  2. Pitch trim - Use ALTERNAT STAB TRIM
  3. Aircraft - At pilots discretion, continue flight without servies of failed bus or land as soon as possible. DO NOT FLY IN ICING CONDITIONS.
52
Q

BUS TIE

Indication: CAS Caution - Bus tie

Condition: BUS TIE in wrong state

A

if GEN 1 and GEN 2 switches are ON and volts/amps normal:

  1. BUS TIE CB - Pull

if a generator is off:

  1. BUS TIE CB - Check, if tripped
  2. BUS TIE CB - Reset (max 1 attempt)
  3. Aircraft - Land as soon as possible
53
Q

GENERATORS

Indication: CAS warning - Generator

Condition: GEN 1 and GEN 2 are off and engine running

A
  1. System MFD - ELECTRICAL - Confirm the failures
  2. GEN 1 and 2 switches - RESET then ON

if generator do not reset (warning remains on):

  1. System MFD-ELECTRICAL - Monitor BAT 1 and 2
  2. Aircraft - Land as soon as possible.

NOTE:
Two fully charged batteries will last for 33 minutes with the automatic load shedding.

54
Q

GENERATOR 1 OFF

Indication: CAS caution - Generator 1 Off

Condition: GEN 1 is OFF line and engine running

A
  1. Systems MFD-ELECTRICAL - Confirm the failure
  2. GEN 1 switch - RESET then ON

if doesnt reset

  1. Aircraft - At pilots discretion land or not
55
Q

BATTERY 1 OR 2 HOT OR BATTERY 1 + 2 HOT

A
  1. System MFD-ELECTRICAL - Check battery 1 and 2 charge currente

if charge current high

  1. BAT 1 or 2 switch - OFF (not ON again)

if charge currente normal

  1. BAT 1 OR 2 switch - OFF

if battery hot warning exringuishes, wait 5 min, then

  1. BAT 1 OR 2 switch - ON (ONCE ONLY)

if battery 1 and 2 hot

  1. BAT 1 AND 2 switches OFF
  2. Aircraft - LAND ASAP

PC 12/47E (5 decks)

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