EPS Flashcards

1
Q

Engine Failure Before V1 (Abort)

A

Power levers- Ground FINE

Braking- As required

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2
Q

Engine Failure After V1

A

Power- Max allowable
Landing Gear Control- Up (positive rate of climb confirmed)
Airspeed- Maintain V2 until 400 ft AGL and clear of obstacles
Propellar- Verfiy Feathered. if propeller does not autofeather, perform manual feather.
Flaps (after VYSE)- UP

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3
Q

Engine Failure in Flight below Vmca

A

Power- reduce as required to maintain control

Pitch attitude- Lower to accelerate above Vmca

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4
Q

Engine Failure During Flight

A

AP/YD- disengage
Power- As Required
Failed Engine- identify
Propeller- Verify Feathered

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5
Q

Engine Failure during Final Approach

A

Power- As Required

Landing Gear- Confirm Down

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6
Q

Engine Failure (Second Engine)

A

Airspeed- As required
Power Lever- IDLE
PROP Lever- As Required

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7
Q

Maximum Glide

A

Landing Gear Control Handle- UP
Flaps- UP
Prop Levers- FEATHERED
Airspeed- 135 KIAS

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8
Q

Single Engine Go- Around

A

Power- Max Allowable
Landing Gear Control Handle- UP
Flaps- UP
Airspeed- VYSE

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9
Q

Primary Governor and Overspeed Governors Failed (Above 1768 RPMS)

A
Power Lever (affected Engine)- IDLE
Prop lever (affected Engine)- FEATHER
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10
Q

L or R Bleed Air Fail Annunciator Illuminated

A

Bleed Air Valves switch (affected engine)- PNEU and ENVIR OFF

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11
Q

EXCESSIVE Differential Pressure (Cabin DIFF HI Annunciator Illuminated)

A
Bleed Air Valves switches- ENVIR OFF
Crew Oxygen Mask- EMER and Don
Mic Switches- OXY
Passenger Manual DROP OUT handle- PULL ON
Descend- AS REQUIRED
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12
Q

LOSS of Pressurization (Cabin Altitude and/or Cabin ALT HI annunciator illuminated)

A

Crew Oxygen Mask- EMER and Don
MIC Switches- OXY
Passenger Manual Drop Out handle- Pull ON
Descend- As required

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13
Q

Door Unlocked Warning Annunciator Illuminated

A

All occupants- seated with seatbelts securely fastened.

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14
Q

Engine/ Nacelle Fire during start or ground operations

A
prop levers- feathered
condition levers- fuel cutoff
f/w valve push switch- push to close (CLOSED annunciator illuminated)
extinguisher push switch- push
master switch- off
bat bus- emer off
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15
Q

engine fire in flight (identified)

A
power lever (affected engine)- idle
prop lever (affected engine)- feather
condition lever (affected engine- fuel cutoff
f/w valve push switch- push to close (Closed annunciator illuminated)
extinguisher push switch- push
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16
Q

fuselage fire

A

fight the fire

land as soon as possible if fire continues

17
Q

wing fire

A

perform engine shutdown on the affected side

land as soon as possible

18
Q

electrical smoke or fire

A

crew oxygen masks- emer and don

mic switches- oxy

19
Q

environmental system smoke

A

crew oxygen masks- emer and don

mic switches- oxy

20
Q

emergency descent

A
power levers- idle
prop levers- high rpm
flaps (202 KIAS Max)- approach
ldg gear control handle (182 KIAS Max) - down
airspeed- 182 kias maximum
21
Q

both dc gen lights illuminated

A
mission power- off
instrument emergency lights- on (if required)
generators- gen reset, then on
if either generator will reset
operation generator load meter- monitor (100% max)
if neither genertaor will reset
ecs mode- off
cockpit/cabin blower- auto
non-essential equipment- 0ff
22
Q

unscheduled rudder boost activation

A

ap/trim master switch- press to first detent and hold
rudder boost switch- off
ap/trim master switch- release
if condition persists
YD/AP disc switch (on flight guidance panel) - pull down

23
Q

unscheduled electric elevator trim

A

airplane attitude- maintain using elevator control

AP/TRIM master switch- depress fully and hold

24
Q

Autopilot mistrim E or A

A

flight controls- hold firmly. control forces may exceed 25 pounds.
autopilot- disengage

25
Q

Autopilot Mistrim (TRIM)

A

flight controls- hold firmly

Autopilot- disengage

26
Q

Cracked Cabin Window

A

Crew oxyegen masks- ON

mic switches- OXY

27
Q

Spins

A

Autopilot and yaw damper- disengage
control column- full forward, ailerons neutral
full rudder- opposite the direction of spin
power levers- idle
rudder- neutralize when rudder stops
execute a smooth pullout.

28
Q

unexpected autopilot disengagement

A

aircraft control - Maintain

Autopilot/ trim disconnect switch- press to first level to cancel horn.

29
Q

stalls (departure from controlled flight)

A
autopilot and yaw damper- disengage
aircraft pitch- apply controls to reduce angle of attack
aircraft bank- wings level
power- as required
execute a smooth recovery.