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Aviation > Dash 7 EPs > Flashcards

Dash 7 EPs Flashcards

1
Q

EMERGENCY SHUTDOWN

A
  1. POWER lever – FLT IDLE.
  2. Condition lever – FUEL SHUTOFF.
  3. PULL FUEL OFF handle – Pull.
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2
Q

SMOKE & FUMES ACTIONS

A
  1. Crew oxygen masks & goggles – 100% and On.
  2. ICS switch – MASK, establish communications.
    = 3. DOME light switch – ON.
    = 4. EMER LTS switch – ON.
    = 5. FASTEN BELT switch – ON.
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3
Q

ENGINE MALFUNCTION BEFORE V1

A
  1. POWER levers (4) – DISC.
  2. Braking – As required.
  3. Reverse – As required.
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4
Q

ENGINE MALFUNCTION AT OR AFTER V1

A

= 1. POWER levers (4) – Maximum available.
= 2. LANDING GEAR (after positive rate of climb) – UP.
3. Airspeed – Climb at V2.
= 4. Confirm – Autofeather, no fire.

If engine failure, no feather.

= 5. Condition lever (failed engine) – FUEL SHUT OFF.

After commencement of third segment, Minimum 400’ AGL.

  1. Airspeed – Accelerate to Vclimb.
    = 7. FLAPS (On Profile) – Select Up.
    = 8. EMERGENCY SHUTDOWN (affected engine) – Complete.
    = 9. EXTG switch – (if required) FWD BTL. (Wait 30 seconds – if fire persists – EXTG switch – AFT BTL.)
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5
Q

ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT

A

= 1. SYNCHROPHASE switch – OFF.
2. Power – As required.
= 3. Affected Engine – Identify.
= 4. EMERGENCY SHUTDOWN (affected eng) – Complete.

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6
Q

TWO ENGINES MALFUNCTION OPERATIONS

A
  1. Condition levers (FWD 3) – MAX RPM.
  2. Power – Maximum Available.
    = 3. Complete appropriate memory items / checklist for second engine malfunction
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7
Q

TWO ENGINE GO-AROUND OR MISSED APPROACH PROCEDURE

A
  1. POWER levers (4) – Maximum available.
  2. LANDING GEAR – UP.
    = 3. FLAPS – Up.
    = 4. Airspeed – 118 KIAS.
  3. Bank angle – 30 degrees maximum.
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8
Q

ALL ENGINES INOPERATIVE

A
  1. Airspeed – 1.3 Vs
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9
Q

OVER TEMPERATURE (OTHER THAN STARTING)

A

If T5 exceeds 800 degrees C and cannot be controlled by reducing the power lever:

ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT checklist – Complete.

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10
Q

ENGINE NG OVERSPEED

A

= 1. SYNCHROPHASE switch – OFF.
= 2. POWER lever (affected engine) – FLT IDLE.

If there is no response to power lever movement:

= 3. PULL FUEL OFF handle – Pull.

Below 1,500 FT/LB Torque:

= 4. Condition lever (affected engine) – FUEL SHUT OFF.

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11
Q

ABNORMAL OIL PRESSURE

A

If Engine OIL PRESS is confirmed below 75 PSI:

= 1. Complete ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT or land as soon as practicable using minimum power on that engine.

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12
Q

PROPELLER OVERSPEED

A

= 1. SYNCHROPHASE switch – OFF.
2. POWER lever (affected engine) – FLT IDLE.
3. Airspeed – Reduce.
= 4. Condition lever (affected engine) – START & FEATHER.

If prop does not feather:

= 5. Condition lever (affected engine) - FUEL SHUT OFF

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13
Q

ENGINE FIRE OR SEVERE ENGINE DAMAGE ON GROUND

A
  1. POWER levers (4) - FLT IDLE.
  2. Condition levers (4) – FUEL SHUTOFF.
  3. PULL FUEL OFF handle (Illuminated) – Pull.
  4. EXTG switch – FWD BTL (wait 5 sec.), AFT BTL.
  5. APU STOP switch – Press for 1 second (if applicable).
  6. Notify ATC and crew of impending evacuation.
  7. Master BATTERY switch – OFF.
  8. DC EXT PWR switch – OFF (If applicable).
  9. Evacuate aircraft.
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14
Q

ENGINE FIRE OR SEVERE ENGINE DAMAGE IN FLIGHT

A

= 1. SYNCHROPHASE switch – OFF.
2. Power – As required.
= 3. Affected engine – Identify.
= 4. EMERGENCY SHUTDOWN(affected engine) – Complete.
= 5. EXTG switch – FWD BTL, (wait 30 seconds) if fire persists – AFT BTL.

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15
Q

APU FIRE OR SEVERE ENGINE DAMAGE

A
  1. APU FIRE PUSH switch light – Press for 1 second and release.
  2. APU ON indicator – Not illuminated.

If APU FIRE PUSH indicator is still illuminated:

  1. APU FIRE BOTTLE switch – Activate.
  2. Master BATTERY switch – OFF.
  3. DC EXT PWR switch – OFF.
  4. APU DC GEN ON switch – OFF.
  5. Evacuate Aircraft.
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16
Q

ABNORMAL OIL TEMPERATURE

A

If Engine OIL TEMP remains above 99 degrees for more than 15 minutes:

= 1. Complete ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT checklist or land as soon as practicable using minimum power on that engine.

17
Q

FIRE DETECTION SYSTEM FAILURE

A

= 1. DETECTOR LOOP switch – Select Non-Illuminated Loop Position
= 2. Fire Warning Test – Conduct.

** CHECK FIRE DET caution light and either LOOP A or B advisory light illuminates indicates a fault.

18
Q

FIRE IN AFT BAGGAGE COMPARTMENT, FLIGHT COMPARTMENT, IN CABIN, UNKNOWN SOURCE OF SMOKE, or ELECTRICAL SYSTEM SMOKE OR FIRE IN FLIGHT

A
  1. SMOKE & FUMES ACTIONS checklist – Complete.
19
Q

RIGHT DC BUS FAULT

A

= 1. DOME light switch – DOME.
= 2. PANEL LIGHTING circuit breakers (8), center ovhd panel – Pull.

**DC BUS followed by: SEC INV, AUX INV, R STALL WARN, #3 DC GEN, #4 DC GEN, PITOT HEAT caution lights on.

20
Q

PRIMARY INVERTER FAILED

A

= 1. 115V BUS TIE circuit breaker (2nd row right ovhd panel) – Pull.

21
Q

SECONDARY INVERTER FAILED

A

= 1. INV SEL switch – R BUS.

= 2. 115V BUS TIE circuit breaker (2nd row right ovhd panel ) – Pull.

22
Q

AUXILIARY INVERTER FAILED

A

= 1. 115V BUS TIE circuit breaker (2nd row right ovhd panel ) – Pull.

23
Q

TWO INVERTERS FAILED

A

= 1. DOME light switch – DOME.

= 2. PANEL LIGHTING circuit breakers (8), Center ovhd – Pull.

24
Q

ROLL AXIS JAM OR MALFUNCTION -

CONTROL WHEEL IMMOVABLE

A
  1. Autopilot – Disengage.
  2. Call out “ROLL JAM”.
  3. ROLL DISC T handle – Pull and rotate 90 degrees. Pilot with unjammed wheel has control.
25
Q

AIRCRAFT ROLLS WITH NO CONTROL WHEEL INPUT

A
  1. Autopilot – Disengage.
26
Q

ROLL SPLR SWITCH LIGHT IS ON

A
  1. Autopilot – Disengage.

2. ROLL SPLR switch light – Push.

27
Q

ELEVATOR CONTROL JAM IN FLIGHT

A
  1. Autopilot – Disengage.
  2. Control column – Apply pressure, call out “PITCH JAM HELP”.
  3. Airspeed and flap setting – Maintain.
    = 4. Control column – Apply pressure against jam.

If jam persists, relax control column force momentarily.

  1. PITCH DISC T handle – Pull and rotate 90 degrees.
  2. Pilot with free control column flies aircraft.
28
Q

EMERGENCY DESCENT: NO STRUCTURAL DAMAGE INVOLVED

A

= 1. SYNCHROPHASE switch – OFF.

  1. POWER levers – FLT IDLE.
  2. Condition levers – MAX RPM.
  3. Airspeed – Vmo.
29
Q

EMERGENCY DESCENT: STRUCTURAL DAMAGE INVOLVED

A

= 1. SYNCHROPHASE switch – OFF.
2. POWER levers – FLT IDLE.
3. Condition levers – MAX RPM.
4. Airspeed – 124 KIAS.
= 5. FLAP selector – Select 15 ( Below 147 KIAS).
= 6. LANDING GEAR handle – DN (Below 147 KIAS).
= 7. FLAP selector – Select 25 (Below 124 KIAS).

30
Q

FAILURE OF ANY ONE TRAILING FLAP SEGMENT TO RETRACT FROM 45 degree TO 25 degree POSITION

A
  1. Airspeed on go-around – 98 KIAS maximum.
31
Q

AILERON TRIM TAB RUNAWAY

A
  1. Autopilot – Disengage.
32
Q

RUD 1 or RUD 2 SWITCH LIGHT ILLUMINATION

A
  1. Autopilot – Disengage.
33
Q

RUDDER TRIM ACTUATOR RUNAWAY

A
  1. Autopilot – Disengage.
34
Q

CABIN PRESSURIZATION LOST WHEN OPERATING ABOVE 10,000 FEET

A

If CABIN PRESS caution light is on:

  1. Crew oxygen masks – 100% and On, Establish communications.

Aviation (2 decks)

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