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B1900MemoryItems > B1900MemoryItems > Flashcards

B1900MemoryItems Flashcards

1
Q

Electrical: Single Inverter or AC Bus Failure (L AC BUS or R AC BUS)

A

AC BUS Switch (failed side) - Off, then On

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2
Q

Electrical: Single Inverter Failure Followed by a Second Inverter or AC Bus Failure (L AC BUS or R AC BUS)

A

Illumination of Both Annunciators Simultaneously After a Single Inverter Failure Has Been Remedied (by placing one AC Bus Switch to TRANSFER) Indicates a Failure of the Second Inverter Selected ON, or a Failure of Either AC BUS.
Attitude/Heading Control - Use Standby Attitude Indicator and Compass

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3
Q

Electrical: Dual Inverter Failure (L AC BUS and R AC BUS)

A

Illumination of Both Annunciators Simultaneously (With Neither AC Bus Switch in Transfer), Indicated that a Failure in One Inverter is Affecting the Other Inverter.
Attitude/Heading Control - Use Standby Attitude Indicator and Compass

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4
Q

AP Malfunction - Elevator Trim Runaway

A

Control Wheel - HOLD FIRMLY
AP YD/DISC TRIM Switch - DEPRESS FULLY
Flight Controls/Power Levers - AS REQUIRED TO RECOVER THE AIRPLANE

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5
Q

Overspeed Warning Horn Sounds

A

Control Wheel - HOLD
AP - DISENGAGE
Airspeed - REDUCE

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6
Q

Unscheduled Electric Elevator Trim Runaway

A

Airplane Attitude - MAINTAIN

Control Wheel Disconnect Switch - DEPRESS FULLY

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7
Q

Unscheduled Rudder Boost Activation

A

Control Wheel Disconnect Switch - DEPRESS AND HOLD (1st Level)
Rudder Boost/Yaw Control Test Switch - OFF
If condition persists:
Rudder Boost Circuit Breaker - PULL

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8
Q

Use of Oxygen

A 
Oxygen Control - CONFIRM ON
Cabin Oxygen Control - PULL ON
Crew - DON MASK
Mask Selector Switch - SET
Headset - DON
MIC Selector Switches - OXYGEN MASK
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9
Q

CABIN ALT HI

A 
Oxygen Control - CONFIRM ON
Cabin Oxygen Control - PULL ON
Crew - DON MASK
Mask Selector Switch - SET
Headset - DON
MIC Selector Switches - OXYGEN MASK
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10
Q

GPWS Warning: PULL UP, PULL UP, TERRAIN TERRAIN PULL UP

A 
Wings - LEVEL
Airspeed - 122 Kts (Vx)
Power - MAX ALLOWABLE
Gear and Flaps - RETRACT
Continue climbing until warning stops
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11
Q

Spins

A

Control Column - FULL FORWARD, AILERONS NEUTRAL
Full Rudder - OPPOSITE THE DIRECTION OF SPIN
Power Levers - IDLE
Rudder - NEUTRALIZE WHEN ROTATION STOPS
Execute a smooth pullout.

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12
Q

Engine Fire on the Ground (FIRE PULL)

A 
Affected Engine:
Condition Levers - FUEL CUT-OFF
Firewall Fuel Valve - PULL CLOSED
Ignition and Engine Start Switch - STARTER ONLY
Fire Extinguisher, if required - ACTUATE
If condition persists:
Condition levers - BOTH FUEL CUTOFF
Propeller levers - BOTH FEATHER
Firewall fuel valve - BOTH PULL CLOSED
Gen ties - MAN. CLOSED
Flaps - 17 degrees
Cabin lights - ON
Avionics - ON
Evacuation - LP INITIATE
Mayday - CALL
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13
Q

Engine Failure During Take-off (at or above V1)

A

Vr Speed - ROTATE to APPROXIMATELY 8 DEGREES
Landing Gear - UP (When positive climb)
Airspeed - MAINTAIN V2 TO Acceleration Alt
Propeller (inop eng) - VERIFY FEATHERED

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14
Q

Bleed Air Line Failure (L BL AIR FAIL/R BL AIR FAIL)

A

Bleed Air Valve (Affected engine) - INSTR & ENVIR OFF

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15
Q

Glide

A

Landing Gear Control - UP
Flaps - UP
Propellers - FEATHERED
Airspeed - 140 KNOTS

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16
Q

Vxse

A

122kts

17
Q

Vyse (two engine)

A

138kts (Decrease 2kts/5000ft)

18
Q

Venr

A

123kts

19
Q

Vmca (Flaps up/17)

A

92kts

20
Q

Emergency Descent

A

180kts

21
Q

Max Range Glide

A

140kts

22
Q

Engine Failure (AP Engaged)

A 
AP - DISENGAGE
Engine Failure Procedure - COMPLETE
Trim Controls - RE-TRIM AIRPLANE
AP - RE-ENGAGE, IF DESIRED
Rudder Trim - MANUALLY ADJUST AFTER POWER AND CONFIG CHANGES
23
Q

Engine Fire of Failure in Flight (FIRE PULL)

A

Condition Lever - FUEL CUTOFF
Propeller Lever - FEATHER
Firewall Fuel Valve - PULL CLOSED
Fire Extinguisher, if required - ACTUATE

24
Q

Engine Failure During Take-off (At or below V1)

A

Power Levers - GROUND FINE

Brakes - MAXIMUM

25
Q

Engine Failure in Flight Below Vmca

A

Reduce power on operative engine to maintain control

Lower nose to Accelerate above Vmca

26
Q

L OIL PRESS LO / R OIL PRESS LO

A

Oil Pressure Gauge - Confirm Below 60PSI

If confirmed - SECURE ENGINE OR LAND AT NEAREST SUITABLE AIRPORT USING MINIMUM POWER REQUIRED TO SUSTAIN FLIGHT

27
Q

Propeller Collision During Ground Operation

A

If max braking and reverse not sufficient:
Power levers - GROUND FINE OR IDLE
Condition Levers - FUEL CUTOFF

28
Q

L FUEL PRESS LO / R FUEL PRESS LO

A

Standy pump (affected engine) - ON

29
Q

Electrical Smoke or Fire

A

Oxygen Control - CONFIRM ON
Crew - DON MASK AND GOGGLES
Headsets - DON
MIC Selector Switches - OXYGEN MASK

30
Q

Environmental Smoke or Fumes

A

Oxygen Control - CONFIRM ON
Crew - DON MASK AND GOGGLES
Headsets - DON
MIC Selector Switches - OXYGEN MASK

31
Q

CABIN DOOR / CARGO DOOR

A

All Occupants - SEATED WITH SEATBELTS SECURELY FASTENED

32
Q

Emergency Descent

A 
Power Levers - IDLE
Propeller Levers - SET 1700RPM
Flaps - 17
Landing Gear Control - DOWN
Airspeed - 180KTS
33
Q

L ENVIR FAIL / R ENVIR FAIL

A

Bleed Air Valve (affected engine) - CYCLE TO ENVIR OFF AND BACK TO OPEN
If Annunciator off, continue, If Illuminated:
Bleed Air Valve (affected engine) - ENVIR OFF

34
Q

CABIN DIFF HI

A

Bleed Air Valves - ENVIR OFF

35
Q

Dual Gen Failure L DC GEN + R DC GEN

A 
Instrument Emergency Lights - ON
Generators - RESET, THEN ON
If Either Gen Resets, Do Not Exceed 100% Load
If Neither Gen Resets:
Non-essential equipment - OFF
36
Q

Wind shear on rotation

A

Power levers - FULL AVAILABLE POWER
Attitude - INCREASE PITCH - WINGS LEVEL
Airspeed - STALL WARNING (min)
Configuration - MAINTAIN

37
Q

Wind shear on go-around

A

Power levers - FULL AVAILABLE POWER
Attitude - INCREASE PITCH - WINGS LEVEL
Airspeed - STALL WARNING (min)
Configuration - MAINTAIN

38
Q

Unexpected severe turbulence

A 
Seat belts - ADVISE PASSENGERS
Speed - REDUCE SMOOTHLY TO 170kts
Autopilot - DISENGAGE
Control - FLY ATTITUDE - DO NOT RETRIM
Auto ignition - ARM
39
Q

Vyse (single engine)

A

128kts (decreasing by 2kts every 5000ft)

B1900MemoryItems (3 decks)

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