1FTS PC-21 Boldface

Ejection Checks

If time critical:


1. SEAT FIRING HANDLE - PULL

Emergency Egress on the Ground

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
8. EXIT THE COCKPIT

Emergency Landing Checks

1. AIRSPEED - BELOW 180 KIAS
2. LANDING GEAR HANDLE - DOWN
3. EMERGENCY LANDING GEAR HANDLE - PULL
4. FLAPS - AS REQUIRED

When aircraft has stopped:
5\. BATT 1 AND BATT 2 - OFF

Engine Fire - In Flight

1. PCL - MINIMUM PRACTICAL
2. EO2 - PULL
3. ACS SHUT OFF - PULL
4. CHECK FOR FIRE

If fire confirmed:
5\. PCL - FUEL OFF
6\. FUEL HYD CUTOFF - PULL
7\. BATT 1 - OFF
8\. GEN 1 AND GEN 2 - OFF

If fire continues:
9\. EJECT

If fire extinguishes:

10\. FUEL PUMPS - OFF

11\. CABIN PRESS - PRESS DUMP

12\. Execute GLIDING CHECKS procedure

If fire not confirmed or FIRE warnings go out:
13\. PMS - MANUAL

Smoke or Fumes in the Cockpit - In Flight

1. EO2 - PULL
2. DESCEND BELOW 10 000 FT AIRCRAFT ALTITUDE
3. OXYGEN - OFF (BOTH COCKPITS)
4. ACS SHUT OFF - PULL
5. CABIN PRESS - RAM

If fumes continue:
6: GEN 1 AND GEN 2 - OFF

Engine Fire or Smoke and Fumes - On Ground

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

Aborted Takeoff

1. PCL - IDLE
2. BRAKES - AS REQUIRED

Engine Failure After Takeoff

1. PCL - FUEL OFF

If suitable runway is available:
2. FUEL HYD CUTOFF - PULL
3. EMERGENCY LANDING CHECKS

Engine Mechanical Failure

1. PCL - FUEL OFF
2. FUEL HYD CUTOFF - PULL
3. EO2 - PULL IF ABOVE 10 000 FT

Engine Flameout

1. PCL - IDLE

Engine Surge

1. PCL - IDLE

PMS Failure (PMS Manual)

1. PCL - CONTROL ENGINE LIMITS MANUALLY

Engine Torque

1. PCL - MINIMUM PRACTICAL

Propeller Speed

A. Overspeed - NP above 2200RPM (warning) or NP above 2080RMP (caution):


1. PCL - MINIMUM PRACTICAL
2. AIRSPEED - REDUCE

Engine Temperature - In Flight

ITT above 860ºC:


1. PCL - MINIMUM PRACTICAL

Engine Temperature - On Ground

If ITT rapidly increases towards and exceeds 750C in ground idle with warning displayed:
1. PCL - FUEL OFF

Engine Speed

A. NG below 50.7% (caution):


1. IGNITERS - ON
2. PCL - SLOWLY INCREASE POWER

B. NG above 104% (caution for 2 seconds, then warning):


1. PCL - MINIMUM PRACTICAL

Oil Pressure Out of Limits

If warning or caution remains indicated:


1. PCL - MINIMUM PRACTICAL

Oil Temperature High - In Flight (Warning)

A. OIL TEMP warning:


1. PCL - MINIMUM PRACTICAL

Oil Temperature High - On Ground (Warning)

A. OIL TEMP warning:


1. PCL - FUEL OFF

Metal Particles Detected In Gearbox

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

Uncommanded Power Changes

1. PCL - IDLE
2. PMS - MANUAL
3. PCL - AS REQUIRED

Oxygen System Off (Both Cockpits)

If above 10 000ft cabin altitude:
1. EO2 - PULL
2. DESCEND BELOW 10 000FT CABIN ALTITUDE

MFD OXY WARNING

If above 10 000ft cabin altitude:


1. EO2 - PULL
2. DESCEND BELOW 10 000FT CABIN ALTITUDE

Oxy Flow Warning

1. OXYGEN - ON. CHECK FLOW, CONNECTIONS, MASK
2. INSTRUCTOR SWITCH - CHECK FOR CORRECT SELECTION

If above 10 000ft cabin altitude and problem remains:


3. EO2 - PULL (AFFECTED COCKPIT)
4. DESCEND BELOW 10 000FT CABIN ALTITUDE

Oxygen Overpressure

If experiencing uncommanded oxygen system overpressure symptoms and difficulty in breathing:


1. OXYGEN - OFF (AFFECTED COCKPIT)

If above 10 000ft cabin altitude:
2\. EO2 - PULL
3\. DESCEND BELOW 10 000FT CABIN ALTITUDE

Physiological Episode and Hypoxia

1. EO2 - PULL (both cockpits)
2. DESCEND BELOW 10000FT AIRCRAFT ALTITUDE
3. OXYGEN - OFF (BOTH COCKPITS)

When at or below 10000 ft aircraft altitude:

4\. ACS SHUTOFF - PULL

5\. CABIN PRESSURE - RAM

6\. Control rate and depth of breathing

7\. Land as soon as possible

8\. EO2 Reset

If symptoms persist:
9\. EJECT

Cabin Overpressure Warning

1. CABIN PRESS - PRESS DUMP
2. PCL - MINIMUM PRACTICAL

Fuel Pressure Low

1. FUEL PUMPS - PUMP L AND PUMP R
2. PCL - MINIMUM PRACTICAL

If warning remains:
3. LAND AS SOON AS POSSIBLE

Brake Failure

1. BRAKES - RELEASE
3. SERVICEABLE BRAKES - GRADUALLY RE-APPLY

Trim Runaway

1. TRIM/AIL PWR - OFF

Aileron Control System Malfunction

1. TRIM/AIL PWR - OFF

Flap Failure

1. AIRSPEED - BELOW 180 KIAS

Gear Retraction Failure

Lights not extinguished after up selection:
1. AIRSPEED - BELOW 180 KIAS

Gear Lowering Failure

1. AIRSPEED - BELOW 180 KIAS