B1900MemoryItems Flashcards
Electrical: Single Inverter or AC Bus Failure (L AC BUS or R AC BUS)
AC BUS Switch (failed side) - Off, then On
Electrical: Single Inverter Failure Followed by a Second Inverter or AC Bus Failure (L AC BUS or R AC BUS)
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
Electrical: Dual Inverter Failure (L AC BUS and R AC BUS)
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
AP Malfunction - Elevator Trim Runaway
Control Wheel - HOLD FIRMLY
AP YD/DISC TRIM Switch - DEPRESS FULLY
Flight Controls/Power Levers - AS REQUIRED TO RECOVER THE AIRPLANE
Overspeed Warning Horn Sounds
Control Wheel - HOLD
AP - DISENGAGE
Airspeed - REDUCE
Unscheduled Electric Elevator Trim Runaway
Airplane Attitude - MAINTAIN
Control Wheel Disconnect Switch - DEPRESS FULLY
Unscheduled Rudder Boost Activation
Control Wheel Disconnect Switch - DEPRESS AND HOLD (1st Level)
Rudder Boost/Yaw Control Test Switch - OFF
If condition persists:
Rudder Boost Circuit Breaker - PULL
Use of Oxygen
Oxygen Control - CONFIRM ON Cabin Oxygen Control - PULL ON Crew - DON MASK Mask Selector Switch - SET Headset - DON MIC Selector Switches - OXYGEN MASK
CABIN ALT HI
Oxygen Control - CONFIRM ON Cabin Oxygen Control - PULL ON Crew - DON MASK Mask Selector Switch - SET Headset - DON MIC Selector Switches - OXYGEN MASK
GPWS Warning: PULL UP, PULL UP, TERRAIN TERRAIN PULL UP
Wings - LEVEL Airspeed - 122 Kts (Vx) Power - MAX ALLOWABLE Gear and Flaps - RETRACT Continue climbing until warning stops
Spins
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.
Engine Fire on the Ground (FIRE PULL)
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
Engine Failure During Take-off (at or above V1)
Vr Speed - ROTATE to APPROXIMATELY 8 DEGREES
Landing Gear - UP (When positive climb)
Airspeed - MAINTAIN V2 TO Acceleration Alt
Propeller (inop eng) - VERIFY FEATHERED
Bleed Air Line Failure (L BL AIR FAIL/R BL AIR FAIL)
Bleed Air Valve (Affected engine) - INSTR & ENVIR OFF
Glide
Landing Gear Control - UP
Flaps - UP
Propellers - FEATHERED
Airspeed - 140 KNOTS
Vxse
122kts
Vyse (two engine)
138kts (Decrease 2kts/5000ft)
Venr
123kts
Vmca (Flaps up/17)
92kts
Emergency Descent
180kts
Max Range Glide
140kts
Engine Failure (AP Engaged)
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
Engine Fire of Failure in Flight (FIRE PULL)
Condition Lever - FUEL CUTOFF
Propeller Lever - FEATHER
Firewall Fuel Valve - PULL CLOSED
Fire Extinguisher, if required - ACTUATE
Engine Failure During Take-off (At or below V1)
Power Levers - GROUND FINE
Brakes - MAXIMUM
