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PC-12 AB > NEW Emergency Procedures > Flashcards

NEW Emergency Procedures Flashcards

1
Q

Partial power loss in flight:

A

CAUSE check: move PCL, fuel pumps, ignition

  1. PCL —————————- IDLE
  2. MOR ————————– ADVANCE SLOWLY
    if a compressor stall occurs and/or ITT exceeded:
  3. MOR ————————– RETARD
    if engine falls below 50% Ng:
  4. STARTER ——————– 2 SECONDS
    (when starter is pressed, A/P disengages and EFIS goes dark)
  5. MOR ————————– ADVANCE TO >80% Ng
  6. LAND ————————- ASAP
    Do not permit anything less than 65% Ng, maintain 75% until touchdown

NOTE: Go-around may not be an option, total landing distance increased by a factor of 2, do NOT use MOR on ground for taxi

CONFIRM CHECKLIST WITH FO!

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2
Q

Engine failure before rotation:

A
  1. PCL —————————— IDLE
  2. BRAKING ———————- MAX
    If runway overrun imminent:
  3. CONDITION LEVER ——– IDLE/CUTOFF
  4. FUEL EMERG. —————- OUT AND UP
  5. GANGBAR ——————– OFF
    EVACUATE
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3
Q

Engine failure after rotation (gear down):

A

if altitude is not sufficient to land straight ahead, turn only to avoid obstacles

  1. FLAPS —————————- 40
  2. FINAL REF ———————- 84KTS
  3. PCL ——————————- IDLE
  4. CONDIITON LEVER ——— IDLE/CUTOFF
  5. FUEL EMERG. —————– OUT AND UP
    after touchdown:
  6. GANGBAR ——————— OFF
    EVACUATE
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4
Q

Engine failure after rotation (gear up):

A
  1. LANDING GEAR ———————– DOWN
  2. N ESNTL BUS OVRD —————– OVRD ON
  3. FLAPS ———————————— 40
  4. FINAL REF —————————— 84KTS OR 98 FLAPS 15
  5. PCL —————————————- IDLE
  6. CONDITION LEVER —————— IDLE/CUTOFF
  7. FUEL EMERG. ————————- OUT AND UP

After touchdown:
8. GANGBAR —————————– OFF

Be sure to abide by your takeoff brief; FO to get gear, flaps, N ESNTL for you and advice ATC!

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5
Q

Total power loss:

A

Initially, check fuel amount, fuel flow, select fuel pumps and ignition to ON

  1. PCL ———————————- IDLE
  2. CONDITION LEVER ————- IDLE/CUTOFF
  3. REMAINING FUEL ————— CHECK
  4. AIR START ————————– CONDUCT
    transfer controls to FO, 114kts, carry out air start checks
  5. IF >13,500’ ————————- EMERGENCY DESCENT
  6. IF AIR START UNSUCESSFUL, FORCED LANDING

AIR START:
1. PCL ———————————IDLE
2. CONDITION LEVER ———— IDLE/CUTOFF
3. FUEL EMERG. ——————- FULL IN
4. ELECTRICAL LOAD ———— REDUCE/SHED
(lights, cabin heat, recircs, anti-ice IF WEATHER PERMITS)
5. ECS ——————————— OFF
6. GEN 2, GEN 1 ——————- OFF
7. BAT 1(and 2) ——————– ON
8. AIR START ENVELOPE ——- CHECK
(not possible above 20,000ft, make emergency descent)
9. STARTER ————————- ON
10. IGNITION ———————- ON
11. CONIDITON LEVER ——— GI ABOVE 13% Ng
12. ITT & NG ———————– MONITOR
When stable above 60% Ng:
13. IGNITON ———————– AUTO
14. CONDITION LEVER ——— FI
15. GEN2, GEN 1 —————– ON
16. ELECTRICAL ——————- AS REQ’D
17. ECS —————————— AUTO

1:15
Multiply altitude by 2.5 to get distance

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6
Q

Air start:

A

Do NOT attempt more than 1 air start, it discharges battery to a critical endurance

  1. PCL ———————————IDLE
  2. CONDITION LEVER ———— IDLE/CUTOFF
  3. FUEL EMERG. ——————- FULL IN
  4. ELECTRICAL LOAD ———— REDUCE/SHED
    (lights, cabin heat, recircs, probes IF WEATHER PERMITS)
  5. ECS ——————————— OFF
  6. GEN 2, GEN 1 ——————- OFF
  7. BAT 1(and 2) ——————– ON
  8. AIR START ENVELOPE ——- CHECK
    (not possible above 20,000ft, make emergency descent)
  9. STARTER ————————- ON
  10. IGNITION ———————- ON
  11. CONIDITON LEVER ——— GI ABOVE 13% Ng
  12. ITT & NG ———————– MONITOR
    When stable above 60% Ng:
  13. IGNITON ———————– AUTO
  14. CONDITION LEVER ——— FI
  15. GEN2, GEN 1 —————– ON
  16. ELECTRICAL ——————- AS REQ’D
  17. ECS —————————— AUTO

NOTE: with single battery, an air start causes a transient DC BAT voltage drop causing A/P and EFIS/AHRS to go offline. Aircraft should be straight and level during this phase.

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7
Q

Engine fire on ground:

A
  1. PCL ———————————— IDLE
  2. CONDITION LEVER ————– IDLE/CUTOFF
  3. ECS EMERG. ———————— OUT AND UP
  4. FUEL EMERG. ———————- OUT AND UP
  5. RADIO ——————————– EMERG. CALL
  6. GANGBAR ————————— OFF
  7. PARKING BRAKE —————— ON
    EVACUATE, FIRE EXTINGUISHER
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8
Q

Engine fire in flight:

A

After identifying fire and carrying out final checks, ask FO to plug in nearest, advise ATC to descend, and read aloud checklist

  1. PCL ——————————– REDUCE TO MINIMUM
    (reduce to minimum to maintain level flight)
  2. ECS EMERG. ——————– OUT AND UP
  3. OXYGEN MASKS ————– ON,
  4. CREW OXYGEN ————— ON
    only if cabin pressure is lost:
  5. PAX OXYGEN —————— ON
  6. FIRE ——————————- CONFIRM IT EXISTS
  7. FUEL EMERG. —————– OUT AND UP
  8. CONDITON LEVER ——— IDLE/CUTOFF
  9. EMERGENCY DESCENT/ FORCED LANDING
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9
Q

Cockpit/cabin fire, smoke or fumes:

A

After doing initial steps, give FO control to proceed direct nearest, a descent below 10,000’, and prepare checklist

  1. OXYGEN MASKS ——————— ON
  2. CREW OXYGEN ———————– ON
  3. PAX OXYGEN ————————– ON
  4. PASSENGERS ————————– INSTRUCT TO DON MASKS
  5. AIRCRAFT —————————— DESCEND BELOW 10,000’
  6. GPS ————————————— PROCEED DCT AIRPORT
    if a smoke evacuation is required:
  7. ECS EMERG. —————————- OUT AND UP
  8. ECS —————————————- DUMP
  9. DV PORT ——————————– OPEN
  10. FANS ———————————– ON HIGH
  11. FIRE EXTINGUISHER ————— USE
    if source is known, pull respective CCB. if not:
  12. BUS TIE CB ————————— OUT (overhead)
  13. GEN 2 TIE CB ———————— OUT (overhead)
  14. GEN 1(BAT 2) ———————– OFF
    if smoke persists:
  15. GEN 1 ——————————— ON
  16. GEN 2 ——————————— OFF
    if smoke STILL persists:
  17. GEN 2 ————————————– ON
  18. BAT 1 ————————————— OFF
    if smoke STILL AGAIN persists:
  19. All electrical equipment off.

NOTE: in any case, do NOT pull CABIN FAN or U/F FAN associated with the aux. cabin heating system

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10
Q

Oil pressure 60 - 90 PSI:

A

EIS master caution blinking!

  1. Ng ————- Above 72%
  2. Torque —— Reduce below 23.9
  3. Aircraft —— Land as soon as practical
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11
Q

Oil pressure below 60 PSI or above 135 PSI:

A

Land as son as possible using minimum torque.

Retain glide capability, i.e. follow donut

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12
Q

Oil temp above 105:

A
  1. PCL ———————– REDUCE POWER
    if oil temperature does not reduce to normal:
  2. LANDING GEAR ——- LOWER
  3. LAND AS SOON AS PRACTICAL
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13
Q

CHIP CAWS on ground/in flight:

A

Before engine start on ground:
DO NOT START

After engine start on ground:
- RETURN TO PARKING
- SHUT DOWN ENGINE
- INSPECT CHIP DETECTOR AND ENGINE IF REQ’D

In flight:
MONITOR ENGINE PARAMITERS
REDUCE POWER TO MINIMUM FOR SAFE FLIGHT
LAND AS SOON AS PRACTICAL

After landing:
INSPECT CHIP DETECTOR AND ENGINE IS REQ’D

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14
Q

When does OIL QTY CAWS light illuminate?

A

1 minute after shutdown or 1 minute before start with battery running

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15
Q

Propeller overspeed:

A
  1. PCL —————– REDUCE
  2. SPEED ————- REDUCE
    if Np remains between 1760 and 1870:
  3. PCL —————– REDUCE TO IDLE IF NEEDED
  4. SPEED ————- REDUCE TO BELOW 120kts
  5. LAND ASAP

NOTE: retain best glide just in case engine fails. In the event of heavy vibration or speed runaway, be prepared to shut engine down

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16
Q

Propeller low pitch (PROP LOW P):

A

PROP LOW P CAWS light!

  1. PCL ————— ENSURE FORWARD OF IDLE
    if not able to maintain speed and altitude:
  2. CONDITION LEVER ————– IDLE/CUTOFF
  3. EMERGENCY LANDING ——– CARRY OUT
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17
Q

Propeller underspeed:

A

When prop is indicating below 1640 RPM, EIS will blink

In flight:
1. PCL —————— INCREASE POWER
2. SPEED ————– INCREASE

On ground:
1. Retard PCL aft of idle OR increase power until above 950 RPM

Minimum GI RPM range is 650-950 RPM. EIS will blink for this

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18
Q

What are the two types of emergency descents?

A

Engine failure, flown for max range
and
Engine running, flown for max descent rate

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19
Q

Maximum range descent (single battery):

A

1.PCL ———————————— IDLE
2. CONDITION LEVER ————– IDLE/CUTOFF
3. A/C CONFIG. ———————– GEAR UP, FLAPS 0
4. SPEED ——————————– 114kts (or ride donut)
5. OXYGEN MASKS —————— ON if cab. alt. >10,000’
6. PAX OXYGEN ———————- ON if cab. alt. >10,000’
7. PAX ———————————– BRIEFED
(Seats upright, seatbelts on, stow objects)
8. ELECTRICAL LOAD ————— SHED LOAD
9. AIR START ————————– CONDUCT
if air start unsuccessful:
10. DESCENT RATE —————— INCREASE to below 10,000’
11. WINDSHIELD HEAT ———— HEAVY, draws less!
12. ECS EMERG. ———————- OUT AND UP

NOTE: When retracting flaps and/or gear, AHRS and EFIS could go offline and severe battery draw will occur. However, when in clean, it significantly increases gliding distance. OIL QTY CAWS may appear while in a long extended glide with no power. Disregard this for engine air start.

20
Q

When time permits, what CBs can we pull to reduce the electrical load?

A

AHRS 2 —————— on AV1 BUS and AV2 BUS
EFIS 2 ——————– on AV1 BUS
RMI 1 ——————– on AV1 BUS
RMI 2 ——————– on AV2 BUS
EFIS EADI ————— on AV2 BUS
LH PITOT DE ICE —– on GEN 1 BUS

21
Q

What are switches we can turn off in the cockpit (excluding CCBs) to reduce electrical loads?

A
  1. External lights
  2. Internal lights
  3. De-icing systems, ALL besides probe heat
  4. Nav/Comm2
  5. ADF
  6. Transponder
  7. WX Radar
22
Q

Maximum range descent (dual battery):

A
  1. PCL ——————————- IDLE
  2. CONDITION LEVER ———- IDLE/CUTOFF
  3. A/C CONFIG. ——————- GEAR UP/ FLAPS UP
  4. SPEED —————————- 114kts (or ride donut)
  5. AUTOPILOT ——————– ENGAGE IAS, and NAV when direct nearest airport
  6. OXYGEN MASKS ————– ON if cab. alt. >10,000’
  7. PAX OXYGEN —————— ON if cab. alt. >10,000’
  8. PAX ——————————- BRIEFED
  9. ELECTRICAL LOAD ———- SHED LOAD
    as follows: external lights, de-ice systems, internal lights, LH PITOT DEICE on GEN 1 BUS out

CAUTION:
Monitor BAT 1 & BAT 2 AMPS. If one is positive, switch off that battery (its feeding the other one, possible overcharge). After 5 minutes the battery can be switched on again. if it happens again shut that battery off.

NOTE: When retracting flaps and/or gear, AHRS and EFIS could go offline and severe battery draw will occur. However, when in clean, it significantly increases gliding distance.

23
Q

Maximum rate descent:

A
  1. PCL ————————- IDLE
  2. LDG GEAR —————- EXTEND BELOW 177KTS
  3. SPEED ———————- Mmo/Vmo
  4. OXYGEN MASKS ——– PREPARE
  5. PAX OXGYEN ————- ON and calculate oxygen duration and check flow to pax
  6. WINDSHIELD HEAT —- AS REQ’D

CAUTION: In turbulence reduce speed to 170kts

24
Q

A fully charged battery will last as follows:

A

60 AMPS = 20mins
50 AMPS = 30mins

25
Q

Two fully charged batteries will last as follows:

A

60 AMPS = 40mins
50 AMPS = 60mins

26
Q

Forced landing:

A
  1. PCL —————————– IDLE
  2. CONDITION LEVER ——- IDLE/CUTOFF
  3. FUEL EMERG. ————– OUT AND UP
  4. ELECTRICAL LOAD ——- REDUCE
  5. ECS —————————- DUMP
  6. BEST GLIDE —————– 114kts or donut

For yourself and pax, seats upright, seatbelts on, loose items stowed

if landing site allows:
7a) LANDING GEAR ———— DOWN by using hand pump

if landing site not suitable:
7b) LDG GEAR ——————– UP
7c) FLAPS ————————– 40
(to silence aural flap warning, pull audio circuit breaker)

  1. REF SPEED ———————– 84kts
    after touchdown:
  2. GANGBAR ———————– OFF
  3. EVACUATE

Hand pump, takes about 80 pumps for gear to lower. Do this if after 30 seconds and no 3 green. Recommended below 110kts!

27
Q

Wheel brake failure:

A

Use max reverse and nose wheel steering to maintain directional control

28
Q

What are possible conditions on ground where AIR/GND disagree CAWS would illuminate?

A

On ground:
-Stick shaker could be going off
- Pressurization could be trying to set at cruise altitude
- Landing gear handle in the up position
- Transponder can transmit on ground

29
Q

What systems could be affected when AIR/GND CAWS is illuminated in flight?

A

Initially, could be fixed by cycling the gear down and up again, ONLY ONCE.

If no effect:

  • Stick pusher becomes inoperative
  • Landing gear handle solenoid goes to locked; gear can be lowered but not retracted
  • Transponder set to ON or ALT
  • Hydraulic pump not active if engine not on
  • ECS; if aircraft goes to GI, cabin could depressurize
  • Prop deice not operative with engine off

Along with this, CAB PRESS, PROP LOW P, STAB TRIM, CHIP, HYDR could be giving false indications

30
Q

What is an indication of flap asymmetry in flight?

A

FLAP CAWS illumination, followed by PUSHER CAWS meaning flap system has failed and stick pusher in “safe” mode

31
Q

Inadvertent pusher/shaker operation:

A
  1. CONTROL WHEEL ————– HOLD AGAINST PRESSURE
  2. PUSHER INTR ——————– PRESS AND HOLD
  3. PUSHER SYS CCB ————— PULL on BAT BUS
  4. AIRSPEED ————————- NOT BELOW 1.3 Vs
    (your ref speeds per flap setting essentially)

NOTE: AOA may not be reliable

32
Q

Inadvertent shaker:

A
  1. AOA —————- Decrease
  2. Airspeed ——— Increase
    If shaker continues:
  3. STALL WARN UNIT 1 CCB ———- PULL (BAT BUS)
  4. STALL WARN UNIT 2 CCB ———- PULL (GEN1 BUS)

WARNING: Aircraft is not stall protected

33
Q

Trim runaway:

A
  1. Trim interrupt ———- INTR
    if CAWS A/P TRIM blue advisory and/or A/P triple light
    indicator is on:

2a) A/P CCB —————– OUT (AV2 BUS)
2b) Trim interrupt ——– NORM
reduce airspeed if control forces are high

if CAWS A/P TRIM and A/P triple indicator is NOT on:

2a) CB of failed trim —– OUT
2b) Trim interrupt ——– NORM
reduce airspeed if control forces are high

if main stabilizer trim has failed:

Pitch trim ——————– ALTERNATE STAB

Rule out autopilot then main trim then use alternate trim.

34
Q

What does an ESTL BUS CAWS light indicate?

A

Voltage below 18V on BAT, GEN1 or GEN2.

35
Q

In any case when you have a BUS failure, what should you avoid?

A

Avoid icing conditions. for GEN 1 and BAT BUS failure, consider EFIS to CMPST.

36
Q

If BAT is OFF what is not possible?

A

Engine start!

37
Q

What does AV BUS CAWS light indicate?

A

Avionics BUS 1 or 2 voltage below 18V.

38
Q

Cabin pressurization failure CAWS indication:

A

Tow different indications!

if cabin diff. >5.75 PSI

  1. CABIN ALTITUDE SELECTOR ——– CHECK CORRECT SETTING
  2. MANUAL CONTORL VALVE ———- USE TO REDUCE DIFF.
    if unsuccessful:
  3. ECS ——————————————- OFF
  4. ECS EMERG. ——————————- OUT AND UP
  5. OXYGEN MASKS ————————- ON
  6. PAX OXYGEN VALVE ——————- ON
  7. PAX —————————————— INSTRUCT TO DON
  8. EMERGENCY DESCENT

if cabin alt. >10,000’

  1. OXYGEN MASKS ————————- ON
  2. PAX OXYGEN VALVE ——————– ON
  3. PAX —————————————— INSTRUCT TO DON
  4. ECS —————————————— CHECK AUTO
  5. ECS PRESS. SWITCH ——————– CHECK AUTO
  6. MANUAL CONTROL VALVE ———- CHECK CLOSED
    if unsuccessful:
  7. Limit cabin altitude <10,000’
  8. If necessary, carry out emergency descent
39
Q

ECS Failure CAWS indication:

A
  1. ECS CCB ———————– RESET IF TRIPPED
    if problem remains:
  2. ECS —————————— OFF
  3. ECS —————————— AUTO
    if unsuccessful:
  4. AICRAFT ———————— LIMIT TO 10,000’ CABIN ALT
  5. ECS ——————————- OFF
  6. ECS SMERG. ——————- OUT AND UP
    if aircraft above 10,000’:
  7. OXYGEN MASKS ————- ON
  8. PAX OXYGEN VALVE ——– ON
  9. If necessary, carry out emergency descent
40
Q

Dry motoring run:

A
  1. CONDITION LEVER ———– IDLE/CUTOFF
  2. PCL ——————————– IDLE
  3. IGNITION CCB —————— PULL
  4. BAT/GPU POWER ————- ON
  5. FUEL PUMPS ——————- ON
  6. STARTER ————————- ENGAGE
    monitor engine oil increase. After 15 seconds, if a fire appears, fuel shutoff OUT & UP and continue to dry motor for another 15 seconds.
  7. STARTER ————————– RESET
  8. FUEL PUMPS ——————– AUTO
  9. IGNITION CCB —————— RESET
  10. BAT/EXT POWER ————- OFF
    observe starter cooling limits, then attempt another start
41
Q

A/P CONTROL - TRIM failure:

(aircraft begins making abrupt changes in attitude)

A
  1. CONTROL WHEEL ——————– GRASP
  2. A/P —————————————- DISENGAGE
  3. AIRCRAFT ——————————- RE-TRIM
  4. A/P CCB ——————————— PULL

Do not attempt to use A/P

42
Q

No start/wet start:

A

No increase of Ng or ITT after 10 seconds GI is introduced No Ng no ITT

1.CONDITION LEVER ——————– IDLE/CUTOFF
2. IGNITION ——————————— AUTO
3. STARTER ———————————- RESET
4. FUEL PUMP —————————— L & R ON
5. Dry motoring

5a. CONDITION LEVER ———– IDLE/CUTOFF
5b. PCL ——————————– IDLE
5c. IGNITION CCB —————— PULL
5d. BAT/GPU POWER ————- ON
5e. FUEL PUMPS ——————- ON
5f. STARTER ————————- ENGAGE
monitor engine oil increase. After 15 seconds, if a fire appears, fuel shutoff OUT & UP and continue to dry motor for another 15 seconds.
5g. STARTER ————————– RESET
5h. FUEL PUMPS ——————– AUTO
5i. IGNITION CCB —————— RESET
5j. BAT/EXT POWER ————- OFF

  1. observe starter cooling limits, then attempt another start
43
Q

Hung start:

A

Rise in ITT with no rise in Ng >13% after GI is introduced

  1. CONDITION LEVER —————– IDLE/CUTOFF
  2. IGNITION —————————— AUTO
  3. STARTER ——————————- RESET
  4. FUEL PUMPS ————————- AUTO
  5. Monitor engine during deceleration
  6. Let fuel drain for 30 seconds after engine has stopped
  7. Dry motoring

7a. CONDITION LEVER ———– IDLE/CUTOFF
7b. PCL ——————————– IDLE
7c. IGNITION CCB —————— PULL
7d. BAT/GPU POWER ————- ON
7e. FUEL PUMPS ——————- ON
7f. STARTER ————————- ENGAGE
monitor engine oil increase. After 15 seconds, if a fire appears, fuel shutoff OUT & UP and continue to dry motor for another 15 seconds.
7g. STARTER ————————– RESET
7h. FUEL PUMPS ——————– AUTO
7i. IGNITION CCB —————— RESET
7j. BAT/EXT POWER ————- OFF

  1. observe starter cooling limits, then attempt another start

Remember 30sec 60sec, 30sec 60sec, 30sec 30mins

44
Q

Hot start:

A

If, after ignition during an engine start, there is a fast increase in ITT towards 1000°C, do the
following procedure:

  1. CONDITION LEVER ————————- IDLE/CUTOFF
  2. IGNITION ————————————– AUTO
  3. FUEL PUMPS ——————————— AUTO
    continue to operate starter for 20 seconds
  4. STARTER —————————————- RESET
  5. Monitor engine during deceleration
  6. Let fuel drain for 30 seconds after engine stops
    if ITT exceeded starter limits (temp AND time), do not fly
    if ITT was less than starter limits, do dry motoring of engine

Make sure battery or external power supply was correct

Attempt another start.

45
Q

Engine fire during start:

A
  1. CONDITION LEVER ——————— IDLE/CUTOFF
  2. IGNITION ———————————- AUTO
  3. FUEL PUMPS —————————– AUTO
  4. FUEL SHUTOFF ————————– OUT AND UP
  5. EVACUATE

PC-12 AB (16 decks)

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