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PC12 > PC12 phase 1s > Flashcards

PC12 phase 1s Flashcards

1
Q

Oxygen Donning Procedure

A
  1. Remove Headset
  2. Put oxygen mask on, smoke goggles if required
  3. headset back on
  4. Mic switch - MASK
  5. Pax oxygen selector - Auto or ON
  6. Main Oxygen lever - confirm ON
  7. systems MFD PAX OXY advisory - confirm ON
  8. Pax - instruct to don masks
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2
Q

Emergency Descent

A
  1. Power Lever - idle
  2. Airspeed < 180KIAS
  3. gear - down
  4. cabin secure and seatbelts fastened
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3
Q

Cabin Altitude

A
  1. Oxygen donning procedure
  2. CPCS - Manual
  3. CPCS MANUAL CONTROL switch - push DESCENT intermittently
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4
Q

Cabin Pressure
- differential > 6.35psi exceeded

A
  1. CABIN PRESSURE switch - DUMP
  2. ACS EMERG shut off - Pull
  3. Oxygen donning Procedure - commence
  4. Aircraft - carry out emergency descent
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5
Q

Pax door/Cargo door/ Pax + cargo door open in flight

A
  1. cabin secure seatbelts fastened
  2. Aircraft speed - reduce IAS to practical minimum
  3. Aircraft - slow descent to 10,000ft
  4. CPCS system mode - Auto
  5. Aircraft - land ASAP
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6
Q

Engine Fire - ground

A
  1. PCL - idle
  2. condition lever - cut-off/feather
  3. ACS EMERG shut off - pull
  4. FUEL EMERG shut off - press latch down and pull lever up
  5. radio - emergency call
  6. MASTER power - off
  7. Park brake - OFF if possible
  8. Aircraft - evcuate
  9. Fire - Extinguish
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7
Q

Engine Fire - in flight

A
  1. Engine Power - reduce to min acceptable
  2. ACS EMERG cutoff - pull
  3. Oxygen donning procedure - commence
    - crew oxygen - 100%
    - if smoke goggles worn
    * vent valve - OPEN
  4. Aircraft - check for fire
    if fire
  5. FUEL EMERG shutoff - press latch down and pull lever up
  6. condition lever - cut-off/feather
  7. BAT 2 - OFF
    if smoke evacuation is required
  8. ACS EMERG shut-off pull
  9. CABIN PRESSURE switch - DUMP
    when cabin pressure diff = 0
  10. DV window - OPEN
  11. VENT FANS - LOW
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8
Q

ENGINE ITT

A
  1. check ITT indication
    if ITT above 850
  2. PCL - reduce power
    if ITT warning remains
  3. aircraft - land ASAP min power
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9
Q

Engine NG - on ground AND/OR immediately after engine start

A
  1. check Ng indication
    if above 103.5%
  2. PCL - reduce power
    if NG is below 60%, select either
  3. condition lever - flight idle or
  4. ELECTRICAL HEAT/COOL - INHIBIT or
  5. ACS BLEED AIR - INHIBIT
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10
Q

Engine NG - in flight - overspeed

A
  1. check Ng
    if above 103.5%
  2. reduce power
    if above 104%
  3. PCL - reduce power
  4. Speed - reduce to 120KIAS or below
  5. aircraft - land ASAP using min power
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11
Q

Engine Ng - in flight - underspeed

A
  1. check Ng indication
    if below 60%
  2. PCL - increase power
  3. speed - increase
    if engine does not respond
  4. Engine Failure in flight - partial power loss
  5. PCL - idle
  6. MOR lever - unstow and move forwards until engine responds
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12
Q

Engine Np - on ground

A

immediately after start
1. check Np indication
if below 950 select either
2. condition lever - flight idle or
3. electrical HEAT/.COOL - INHIBIT or
4. ACS BLEED air - INHIBIT or
5. PCL - retard aft of idle detent until Np above 950

on ground
1. check indication
if below 930
2. PCL - retard aft of idle detentor increase power until above 950
if prop RPM is above 1760
2. PCL - reduce power

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13
Q

Engine Np - in flight

A
  1. check indication
    if below 1640
  2. PCL - increase power
  3. airspeed - increase
    if above 1760
  4. PCL - reduce power
  5. airspeed - reduce
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14
Q

Engine oil - on ground

A
  1. engine - dont start, maintenance required
  2. engine - fill with oil
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15
Q

Engine oil Pressure

A
  1. check indication
    if confirmed
  2. Ng - check Ng above 72%
  3. Torque - reduce to below 24psi
    if warning remains
  4. aircraft - land ASAP using min power
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16
Q

Engine oil temp - on ground

A
  1. check indication
    if temperature is too high
  2. aircraft - position into wind
  3. condition lever - flight idle
  4. PCL - increase power
    if does not return to normal
  5. ELETRICAL HEAT/COOL -inhibit
    if warning remains
  6. shut down engine, maintenance required
17
Q

Engine oil temp - in flight

A
  1. check indication
    if oil temp too high
  2. PCL - reduce power
    if does not return to normal
  3. landing gear - extend
    if warning remains
  4. land as soon as practical
18
Q

Engine Torque

A
  1. check indication
    if torque above 44.3PSI
  2. PCL - reduce power
    if warning remains
  3. land ASAP using min power
19
Q

ESS bus - below 22V

A
  1. Overhead panel - confirm EPS switch ARMED and EPS ON caption is on
  2. pitch trim - use ALTERNATE STAB TRIM
  3. aircraft - land or continue at pilot discretion, without failed bus services, do not fly in icing conditions
20
Q

Generators - GEN 1 and GEN 2 off and engine running

A
  1. confirm failures in systems MFD
  2. GEN 1 switch - reset then on
  3. GEN 2 switch - reset then on
    if generators do not reset and warning remains
  4. monitor BAT 1 and BAT 2
  5. aircraft - land asap do not fly in icing conditions
21
Q

Pitch trim runaway

A
  1. TRIM INTERRUPT SWITCH - INTR
  2. reduce aircraft speed if control forces high
  3. PITCH TRIM cb (LA1) - PULL
  4. TRIM INTERRUPT switch - NORM
    if stopped
  5. PITCH TRIM - use alternate stab trim
    if not stopped
  6. TRIM INTERRUPT switch - INTR
  7. PITCH TRIM ALTN cb (RA1) - PULL
  8. PITCH TRIM cb (LA1) - CLOSE
  9. TRIM INTERRUPT switch - NORM
22
Q

Propeller Pitch

A
  1. PCL - ensure forward of the idle detent
    if not possible to maintain speed and height
  2. Condition lever - cut-off/feather
23
Q

starter engaged - on ground

A
  1. condition lever - cut-off/feather
  2. START INTERRUPT switch - push
  3. BAT 1 and BAT 2 switch - OFF
  4. EXT PWR (if available) - OFF
  5. aircraft - maintenance action required
24
Q

starter engaged - in flight - following airstart

A
  1. BUS TIE CB - pull
  2. STARTER CB LL1 - PULL
  3. GEN 1 and GEN 2 switches - OFF
25
Q

AP HOLD LH (RH) DN / AP hold nose up (DN)

A
  1. aircraft control wheel and rudder pedals - grasp and position feet to gain control
  2. autopilot disengage switch - press and disengage AP
  3. aircraft - retrim manually as necessary
    if no AFCS associated CAS messages
  4. aircraft - attempt to re-engage AP once
26
Q

IMC glide procedure

A

Aviate - control aircraft
- glide established - 110KTS@4100kg - 119kts@MTOW
- phase 1s completed, engine shut down and feathered
- mayday call and “standby”
Navigate
- MFD swap, altsel to 0
- NRST - divert to most suitable airfield, confirm within reach - 2nm/1,000ft
- use AP to track
- 3nm final point @1,500ft
*systems
- consider o2 requirements
- consider reduction of electrical load
Communicate
- advise med staff - PIEMAN
- ELT ON and transponder to 7700
- update ATC

PC12 (3 decks)

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