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B1900 Complete frankenstein Deck > Memory Items > Flashcards

Memory Items Flashcards

1
Q

Engine Failure in Flight

A 
Affected Engine
Condition Lever - Cut Off
Propeller Lever - Feather
Firewall Fuel Valve - Pull Closed
Fire Extinguisher - Actuate
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2
Q

In- Flight Activation of GPWS Warning (GPWS Annunciator and Continuous “Pull UP, Pull UP” Voice Message)

A 
In IMC or at night
Wings - Level
Airspeed - 122 KIAS
Power - Max Allowable
Gear and Flaps - Retract
Continue climb at 122 KIAS until all visual and aural warnings cease

In Day VMC
Evaluate Flight path with respect to terrain
Take action as necessary to recover safe terrain clearance

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3
Q

Electrical Smoke or Fire

A 
Oxygen Control - Confirm ON
Crew - Don Mask and Goggles
-Mask Selector Switch - Emergency
- Purge Valve - Open
Headsets - Don
Mic Selector Switches - Oxygen Mask
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4
Q

Engine Failure during Take off at or below V1

A

Power Lever - Ground Fine
(Do not use reverse thrust with one engine inoperative)
Brakes - Maximum or as required to achieve stopping distance

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5
Q

Spins

A

Intentional Spins are prohibited. If an unintentional spin is encountered perform the following procedure immediately - the longer the delay, the more difficult recovery will become. Steps 1 through 3 should be done AGGRESSIVELY and SIMULTANEOUSLY. The full forward position of the control column may be reduced slightly, if required to prevent the airplane for exceeding the 90 degree nose down (inverted) attitude
Control Column - Full Forward, Ailerons Neutral
Full Rudder - Opposite the direction of spin
Power Levers - IDLE
Rudder - Neutralize when rotation stops
Execute smooth pullout

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6
Q

Dual Generator Failure (L and R DC GEN Annunciators)

A 
Instruments Emergency lights - ON
Generators - Reset, then ON
If either Generator will reset
Do not exceed 100% Load on operating Generator
If neither generator will reset
Non-Essential Equipment - OFF
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7
Q

Use of Oxygen

A 
Oxygen Control - Confirm ON
Cabin Oxygen Control - Pull ON
Crew - Don Mask
Mask Selector Switch - SET
 - Inflatable type harness - Normal
 - Strap Type Harness - Normal (100% at cabin altitudes above 20,000 ft)
Headsets - DON
Mic Selector Switch - Oxygen Mask
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8
Q

Oil Pressure low (L or R OIL PRESS LO Annunciator)

A

Oil Pressure Gauge -
60-90PSI is undesirable. Do not exceed 2000Ft-lbs Torque for completion of flight.
Confirm below 60 PSI
if Confirmed - Secure engine or land at nearest suitable airport using minimum power required to sustain flight

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9
Q

Vmca

A

92

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10
Q

Vyse

A

128

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11
Q

Bleed Air Line Failure (L or R BL AIR FAIL Annunciator)

A

Bleed Air Valve (Affected Engine) INST & ENVIR OFF

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12
Q

Cabin Door or Cargo door Annuciator

A

All Occupants - Seated with seat belts securely fastened

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13
Q

Glide

A

Landing Gear Control - Up
Flaps - Up
Propellers - Feathered
Airspeed 140 Knots

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14
Q

Single Inverter Failure followed by a second Inverter or AC bus Failure (L or R AC BUS Failure)

A

Attitude/Heading Control - Use standby attitude indicator and Compass

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15
Q

Environmental System Smoke or Fumes

A 
Oxygen Control - Confirm ON
Crew - Don Mask and Goggles
-Mask Selector Switch - Emergency
- Purge Valve - Open
Headsets - Don
Mic Selector Switches - Oxygen Mask
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16
Q

Fuel Press Low (L or R FUEL PRESS LOW Annunciator)

A

Standby Pump (Failed Side) - ON

17
Q

Environmental Failure (L or R ENVIR FAIL Annunciator)

A

Bleed Air Valve (Affected Side) - Cycle to ENVIR OFF and back to OPEN
if ENVIR FAIL Annunciator Extinguishes, Continue Operation. If Annunciator remains Illuminated
Bleed Air Valve (affected side) - ENVIR OFF

18
Q

Engine Fire on Ground

A

Affected Engine - Fuel Cut off
Firewall Fuel valve - Pull Closed
Ignition and Engine Start Switch - Starter only
Fire Extinguisher, if required - Actuate

19
Q

Propeller Collision during ground operation

A

If maximum braking and maximum reverse are insufficient and collision is imminent
Power Levers - Ground Fine or Idle
Condition Levers - Fuel Cut off

20
Q

Emergency Descent

A

180

21
Q

Venr

A

123

22
Q

Cabin Decompression (CAB ALT HI Annuciator)

A 
Oxygen Control - Confirm ON
Cabin Oxygen Control - Pull ON
Crew - Don Mask
Mask Selector Switch - SET
 - Inflatable type harness - Normal
 - Strap Type Harness - Normal (100% at cabin altitudes above 20,000 ft)
Headsets - DON
Mic Selector Switch - Oxygen Mask
23
Q

High Pressure Differential (CAB DIFF HI Annunciator)

A

Bleed Air Valves - ENVIR OFF

24
Q

Engine Failure at or above V1 Take off continued

A

Vr Speed (Rotate to approximately 8 degrees
Landing Gear (when positive climb established) - Up
Airspeed - Maintain V2 to 400ft AGL
Propeller (inoperative engine) Verify Feathered\
Do not retard the failed engine power lever until the Auto feather system has completely stopped propeller rotation.
Airspeed @ 400 ft AGL….Accelerate to VENR Climb speed
Flaps….UP
Power Reduce to MCP
Bleed Valve (Operative engine) ….OFF
Climb to 1500 ft and accomplish checklist

25
Q

Emergency Descent

A 
Power Levers - Idle
Propeller Levers Set 1700 RPM
Flaps - 17 Degrees
Landing Gear Control - Down
Airspeed - 180 Knots
26
Q

Dual Inverter Failure (L and R AC BUS Annunciator)

A

Attitude/Heading Control - Use Standby Attitude Indicator and Compass

27
Q

Vxse

A

122

28
Q

Max Glide Range

A

140

29
Q

Engine Failure in flight below Vmca

A

Reduce power on operative engine to maintain control

Lower Nose to accelerate above Vmca

30
Q

Unscheduled Electric Elevator Trim

A

Airplane Attitude - Maintain (Using Elevator Control)

Control Wheel Disconnect Switch (Depress Fully, Pitch Trim OFF Annunciator - Illuminated)

31
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

32
Q

Single Inverter or AC Bus Failure (L or R Bus Annunciators

A

AC BUS Switch (Failed Side) - OFF, then ON

(AC Bus Annunciator - Extinguished) if not checklist

B1900 Complete frankenstein Deck (8 decks)

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