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Pilatus PC-21 > PC21 Boldface > Flashcards

PC21 Boldface Flashcards

1
Q

EMERGENCY EGRESS ON THE GROUND

A
  1. SEAT PIN - IN
  2. LEG RESTRAINTS - RELEASE
  3. SEAT HARNESS - RELEASE
  4. OXYGEN MASK HOSE - DISCONNECT
  5. MIC-TEL - DISCONNECT
  6. PSP - DISCONNECT
  7. CANOPY - OPEN
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2
Q

EMERGENCY LANDING CHECKS

A
  1. AIRSPEED - BELOW 180 KIAS
  2. LANDING GEAR HANDLE - DOWN
  3. EMERGENCY LDG GR HANDLE - PULL
  4. FLAPS - AS REQUIRED
    when aircraft has stopped
  5. BATT 1 AND BATT 2 - OFF
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3
Q

ENGINE FIRE OR SMOKE AND FUMES - ON THE GROUND

A
  1. ACS SHUT OFF - PULL
  2. PCL - FUEL OFF
  3. FUEL HYD CUTOFF - PULL
  4. BATTS AND GENS - OFF
  5. BRAKES - AS REQUIRED
  6. EMERGENCY EGRESS ON THE GROUND
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4
Q

ENGINE FIRE - IN FLIGHT

A
  1. EO2 - PULL
  2. ACS SHUT OFF - PULL
  3. PCL - MINIMUM PRACTICAL
  4. PMS - MANUAL
  5. CHECK FOR FIRE
    if fire is not confirmed
  6. LAND AS SOON AS POSSIBLE
    if fire confirmed
  7. PCL - FUEL OFF
  8. FUEL HYD CUTOFF - PULL
  9. BATT 1 - OFF
  10. GEN 1 AND GEN 2 - OFF
    if fire persists
  11. EJECT
    if fire goes out - non-boldface continues
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5
Q

SMOKE AND FUMES IN COCKPIT - IN FLIGHT

A
  1. EO2 - PULL
  2. ACS SHUT OFF - PULL
  3. CABIN PRESSURE - RAM
    if fumes continue
  4. GEN 1 AND GEN 2 - OFF
    if fumes still continue - non-boldface
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6
Q

ABORTED TAKE-OFF

A
  1. PCL - IDLE
  2. BRAKES - AS REQUIRED
    if aborting due to engine fire
  3. ENGINE FIRE OR SMOKE AND FUMES - ON THE GROUND
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7
Q

ENGINE FAILURE AFTER TAKE-OFF

A
  1. PCL - OFF
    if suitable runway available
  2. FUEL HYD CUTOFF - PULL
  3. EMERGENCY LANDING CHECKS
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8
Q

ENGINE MECHANICAL FAILURE

A
  1. PCL - FUEL OFF
  2. FUEL HYD CUTOFF - PULL
  3. EO2 - PULL IF ABOVE 10,000FT
    continue non-boldface
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9
Q

ENGINE FLAMEOUT

A
  1. PCL - IDLE
  2. IGNITERS - ON
    continue non-boldface
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10
Q

ENGINE SURGE

A
  1. PCL - IDLE
  2. LAND AS SOON AS POSSIBLE
    continue non-boldface
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11
Q

PMS FAILURE (PMS MANUAL)

A
  1. PCL - CONTROL ENGINE LIMITS MANUALLY

when at a safe height continue non-boldface

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12
Q

ENGINE TORQUE

A
  1. PCL - MINIMUM PRACTICAL
    if warning/caution remains
  2. LAND AS SOON AS POSSIBLE
    continue non-boldface
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13
Q

PROPELLER SPEED

A

A. OVERSPEED - NP ABOVE 2200RPM (WARNING)

  1. PCL - MINIMUM PRACTICAL
  2. AIRSPEED - REDUCE
  3. LAND AS SOON AS POSSIBLE

B. OVERSPEED - NP ABOVE 2080RPM (CAUTION)
non-boldface

C. UNDERSPEED - NP BELOW 1900RPM (CAUTION)
non-boldface

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14
Q

ENGINE TEMPERATURE - ON GROUND

A

if ITT rapidly increases towards & exceeds 750oC in ground idle:
1. PCL - FUEL OFF
continue non-boldface
if ITT slowly increases towards & exceeds 750oC in ground idle:
non-boldface
3. PCL - advance above 65% NG
continue non-boldface

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15
Q

ENGINE TEMPERATURE - IN FLIGHT

A

A. ITT ABOVE 860oC

  1. PCL - MINIMUM PRACTICAL
  2. LAND AS SON AS POSSIBLE

B. ITT BELOW 350oC (possible flameout)
continue non-boldface

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16
Q

ENGINE SPEED

A

A. NG BELOW 50.7% (CAUTION)
1. IGNITERS - ON
2. PCL - SLOWLY INCREASE POWER
if no engine response continue non-boldface

B. NG ABOVE 104% (CAUTION 2 SECS, THEN WARNING)
1. PCL - MINIMUM PRACTICAL
if warning remains
2. LAND AS SOON AS POSSIBLE
or continue non-boldface
17
Q

OIL PRESSURE OUT OF LIMITS

A 
if warning or caution remains indicated
1. PCL - MINIMU PRACTICAL
if warning indicated
2. LAND AS SOON AS POSSIBLE
or continue non-boldface
18
Q

OIL TEMPERATURE HIGH - ON GROUND

A

A. OIL TEMP WARNING
1. PCL - FUEL OFF
continue non-boldface

B. OIL TEMP CAUTION
continue non-boldface

19
Q

OIL TEMPERATURE HIGH - IN FLIGHT

A

A. OIL TEMP WARNING
1. PCL - MINIMUM PRACTICAL
2. LAND AS SOON AS POSSIBLE
continue non-boldface

B. OIL TEMP CAUTION
non-boldface

20
Q

METAL PARTICLES DETECTED IN GEARBOX

A
  1. PCL - MINIMUM PRACTICAL

2. LAND AS SOON AS POSSIBLE

21
Q

UNCOMMANDED POWER CHANGES

A
  1. PCL - IDLE
  2. PMS - MANUAL
  3. PCL - AS REQUIRED
    continue non-boldface
22
Q

OXYGEN SYSTEM OFF (BOTH COCKPITS)

A
  1. OXYGEN - ON, CHECK FLOW, CONNECTIONS, MASK
    if above 10,000ft
  2. EO2 - PULL
  3. DESCEND BELOW 10,000FT CABIN ALTITUDE
    AT OR BELOW 10,000FT CONTINUE NON-BOLDFACE
23
Q

OBOGS COMPUTER BIT FAILURE

A
  1. OXYGEN SYSTEM OFF (BOTH COCKPITS) CHECKLIST
24
Q

OBOGS FAILURE

A
  1. OXYGEN - OFF (BOTH COCKPITS)
    if above 10,000ft cabin altitude
  2. EO2 - PULL
  3. DESCEND BELOW 10,000FT CABIN ALTITUDE
25
Q

OXYGEN PRESSURE OR CONCENTRATION LOW

A
  1. OXYGEN - ON, CHECK FLOW, CONNECTIONS, MASK
  2. PCL - INCREASE IF POSSIBLE
    if above 10,000ft cabin altitude
  3. EO2 - PULL
  4. DESCEND BELOW 10,000FT CABIN ALTITUDE
    continue non-boldface
26
Q

OXY FLOW WARNING

A
  1. OXYGEN - ON, CHECK FLOW, CONNECTIONS, MASK
    if rear cockpit afffected
  2. INSTRUCTOR SWITCH - FRONT OR REAR SELECTED
    if above 10,000ft cabin altitude & problem remains
  3. EO2 AFFECTED COCKPIT - PULL
  4. DESCEND BELOW 10,000FT CABIN ALTITUDE
    continue non-boldface
27
Q

CABIN ALTITUDE ABOVE 25,000ft

A
  1. DESCEND TO 25,000ft CABIN ALTITUDE OR BELOW

continue non-boldface

28
Q

AIRCRAFT ALTITUDE ABOVE 26,000ft

A
  1. DESCEND TO 25,000ft CABIN ALTITUDE OR BELOW

continue non-boldface

29
Q

CABIN OVERPRESSURE WARNING

A
  1. CABIN PRESS - PRESS DUMP
  2. PCL - MINIMUM PRACTICAL
    continue non-boldface
30
Q

FUEL PRESSURE LOW

A
  1. FUEL PUMPS - ON
  2. PCL - MINIMUM PRACTICAL
    if warning remains
  3. LAND AS SOON AS POSSIBLE
    or continue non-boldface
31
Q

TRIM RUNAWAY

A
  1. TRIM/AIL PWR - OFF

continue non-boldface

32
Q

AILERON CONTROL SYSTEM MALFUNCTION

A
  1. TRIM/AIL PWR - OFF

continue non-boldface

33
Q

FLAP FAILURE

A
  1. AIRSPEED - BELOW 180kts

continue non-boldface

34
Q

GEAR RETRACTION FAILURE

A
  1. AIRSPEED - BELOW 180kts

continue non-boldface

35
Q

GEAR LOWERING FAILURE

A
  1. AIRSPEED - BELOW 180kts

continue non-boldface

Pilatus PC-21 (1 decks)

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