Emergency Procedures (Non-Memory)

Question 1

Simulated engine failure shall not be initiated below either ______ or ________

Answer 1

Vsse or 200’ AGL

Question 2

Simulating a failed engine by moving the CONDITION lever to FUEL CUTOFF or feathering a propeller for emergency training shall not be practiced below ________

Answer 2

4000’ AGL

Question 3

During maneuvers requiring large rudder inputs (e.g. Vsse dynamic engine cut), ensure _____ _____ is not engaged

Answer 3

Yaw Damper

Question 4

Training that shall be conducted in daylight VMC only? (8)

Answer 4

1. Stalls or Approaches to Stalls
2. Ditching Drills
3. Emergency Shutdown
4. Air Starts
5. V1 Cuts
6. Landing Gear Manual Extension
7. Simulated In-Flight Fires
8. Emergency Descents

Question 5

_______ will be lost if either bleed air valve switch is placed in the INST & ENVIR OFF position.

Answer 5

Rudder boost

Question 6

CABIN DOOR warning?

Answer 6

Do not attempt to close door or check for security until the cabin is depressurized and the aircraft is on the ground.

Question 7

FUEL PRESS L/R considerations?

Answer 7

CAUTION - Engine driven fuel pump operations without boost pump fuel pressure is limited to 10 hours. Operation is limited to 20,000’ MSL when operating on aviation gasoline with one standby boost pump inoperative.

Question 8

HYD FLUID LOW

Answer 8

Hydraulic fluid low in the power pack and manual extension of the landing gear may be required.

Question 9

Hot Brakes

Answer 9

Usually caused by excessive or heavy braking action. If hot brakes are suspected, stop the aircraft and allow the brakes to cool.

CAUTION - Do not set parking brake if hot brakes are known or suspected

Question 10

Brake Failure

Answer 10

In the event of wheel brake failure, proceed as follows:
1. Maintain directional control with rudder and asymmetric power
2. Try the other crewmember’s brakes.
3. Stop the aircraft using propeller reversing.

Question 11

Continued flight with engine failure considerations? (6)

Answer 11

1. The nature of the malfunction and the possible mechanical difficulties that may occur if flight is continued.
2. The altitude, weight, and usable fuel at the time of engine stoppage.
3. The terrain and weather conditions en route and at suitable landing points.
4. Possible air traffic congestion at suitable landing points.
5. Pilot familiarity with the airport to be used.
6. Power on remaining engine is sufficient for en route conditions and available landing sites.

Question 12

Engine Failure on the second engine

Answer 12

Perform the appropriate Airstart Checklist. Do not feather both propellers if a windmilling airstart is to be attempted. Should all attempts to restart either engine fail, transition to the maximum glide range airspeed (140 KIAS, gear up, flaps up, both props feathered), which will result in a zero-wind glide distance of approximately 2 NM per 1000 feet.

Question 13

A drop in 1. ______, 2. ______, and 3. ______ indicates a flameout condition.

Answer 13

1. ITT
2. Torque
3. Turbine RPM (N1)

Question 14

Oil pressure considerations?

Answer 14

Pressure below 85 PSI (above 21,000’) and 100 PSI (below 21,000’) is undesirable and should be tolerated only for the completion of flight at a reduced power not to exceed 1,100 ft-lbs.

Oil pressure below 60 PSI and/or oil temperature that exceeds 99 C is unsafe and requires that either the engine be shut down or a landing be made as soon as possible using minimum power to sustain flight.

Question 15

Electrical systems that may cause a ignition hazard to leaking fuel? (5)

Answer 15

1. Navigation Lights
2. Recognition Lights
3. Strobe Lights
4. Fuel Vent Heaters
5. Stall Warning Sensor Heater

Question 16

Fuel Siphoning

Answer 16

Airspeed to 140 KIAS, land as soon as practical.

NOTE: Extreme nose-low attitudes will aggravate the fuel siphoning condition (maybe don’t use an aggressive emergency descent, depending on fuel state)

Question 17

The auxiliary battery will power (5 things) for _____ minutes.

Answer 17

1. Pilot Audio
2. RTU
3. U/VHF
4. NAV 1
5. ESIS

“PRUNE”

30 minutes

Question 18

What two circuit breakers should be reset?

Non essential circuit breaker trips?

Essential circuit breaker?

Answer 18

Tripped standby fuel pump and fuel quantity indicator.

Do not reset in flight.

Reset once, if it trips again, do not reset.

Question 19

Consideration for a same side current limiter failure with opposite side generator failure?

Answer 19

The battery cannot be recharged and should be conserved for necessary operation.

Question 20

Loose or unlatched cowling?

Answer 20

1. POWER lever (affected engine) - Reduced
2. Airspeed - Reduced.
3. Land as soon as possible

NOTE: Extending the corresponding ice vane may create a vacuum that will draw the cowling closed.