GLA Emergency Procedures Flashcards
PROPELLER COLLISIONS DURING GROUND OPERATIONS
Power Levers …………………………… GROUND FINE or IDLE
Condition Levers ………………………. FUEL CUTOFF
ENGINE FIRE ON GROUND
Condition levers ……………….. FUEL CUTOFF
Firewall Fuel Valves …………… PULL CLOSED
Ignition and Start Switch ……. STARTER ONLY
Fire Extinguisher ……………….. ACTUATE (if required)
Thence…
Parking Brake …………………… SET
Condition Levers ………………. FUEL CUTOFF
Prop Levers ……………………… FEATHER
Firewall Fuel Valves …………… PULL CLOSED
Fire Extinguishers ……………… ACTUATE (if required)
Master Switch …………………… GANGBAR OFF
ENGINE FAILURE DURING TAKEOFF, ABORTED TAKEOFF
at or below V1
Power Levers ……………………… GROUND FINE or IDLE
WARNING: DO NOT USE REVERSE THRUST WITH ONE ENGINE INOPERATIVE
CARE MUST BE EXERCISED WHEN USING SINGLE ENGINE GROUND FINE ON SURFACES WITH REDUCED FRICTION
BRAKES …………………………. MAXIMUM (or as required to achieve stopping distance)
ENGINE FIRE OR FAILURE IN FLIGHT
SET MAX POWER
WARNING: DO NOT INCREASE POWER ON A BURNING ENGINE
Props ………….. FULL FORWARD
Confirm …………….. GEAR UP/FLAPS UP
Verify which engine has failed …………… REFERENCE ENG. INSTRUMENTS
Affected Engine
Condition Lever ……………………. FUEL CUTOFF
Prop Lever …………………………… FEATHER
Firewall Fuel Valve ………………… PULL CLOSED
Fire Extinguisher …………………… ACTUATE (if required)
ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (Vmca)
Reduce power on operative engine as required to maintain control
Lower nose to achieve airspeed above Vmca
OIL PRESSURE LOW (L or R OIL PRES LO ANNUNCIATOR)
Oil Pressure Gage……. CONFIRM BELOW 60 PSI
If confirmed……….. SECURE ENGINE OR LAND AT THE NEAREST SUITABLE AIRPORT USING THE MINIMUM POWER REQUIRED TO SUSTAIN FLIGHT
ELECTRICAL SMOKE OR FIRE
Oxygen Mask and goggles ……. Don
Purge Valves …………. Open
Crew …….. Establish Communications
Environmental Systems Smoke or Fumes
Oxygen Masks and Goggles ……. Don
Purge Valves ……… Open
Crew ……… Establish Communications
Cabin Door or Cargo Door Unlocked (Cabin or Cargo Door Annunciator)
All Occupants ……… Confirm Seated with seatbelts securely fastened
Emergency Descent
Power levers............... Idle Prop levers .......... Full forward (set 1700 rpm) Flaps .......... 17 degrees Landing Gear ........ Down Airspeed ........... 180 Knots
Glide
Landing Gear - Up
Flaps - Up
Prop levers - feather
Airspeed - 140 Knots
Single Inverter or AC Bus Failure (L or R AC Bus ANNUNCIATOR)
AC Bus Switch (Failed Side) - Cycle Off, than on (AC Bus Annunciator - Extinguished)
Single Inverter Failure Followed by a Second Inverter Failure or AC Bus Failure (L or R AC BUS ANNUNCIATOR)
Attitude/Heading Control …… Use standby attitude indicator and compass
Dual Inverter Failure (L and R AC Bus Annunciator)
attitude/heading control …… use standby attitude indicator and compass
Dual Generator Failure (L and R DC GEN Annuniactors)
Instrument emergency lights (if required) - ON
Generators ……… RESET, then ON
(if either generator will reset)
Do not exceed 100% on operating generator
(if neither generator will reset):
non-essential equipment …… OFF
High Differential Pressure (CAB DIFF HI) Annunciator
Bleed Air Valves………. ENVIR OFF
Bleed Air Line Failure (L or R BL AIR FAIL annunciator)
Bleed Air Valve (affected engine) …….. INST & ENVIR OFF
ENVIR OFF annunciator Illuminated
Unscheduled Rudder Boost Activation
Control wheel Disconnect Switch ……. Depress and Hold (1st level)
Rudder Boost/Yaw control test switch …. OFF
if conditions persist:
Rudder Boost Circuit Breaker ….. PULL (main CB panel - 2nd row u, 7th CB in from lower right corner)
Use of Oxygen
Oxygen Masks …… DON
Cabin Oxygen Control …… PULL ON
Crew ……… ESTABLISH COMMUNICATIONS
Rapid Loss of Pressurization/Explosive Decompression
Oxygen Masks ……. DON
Cabin Oxygen Control ……. PULL ON
Crew ……….. ESTABLISH COMMUNICATIONS
In-Flight Activation of GPWS Warning (In IMC or at NIGHT)
Wings ................. Level Airspeed ............. 122 Knots Power .................. Max Allowable Gear and Flaps .... Retract Continue Climb at 122 KIAS until all visual and Aural Warnings Cease
In-Flight Activation of GPWS warning (in DAY VMC)
Evaluate Flight Path with Respect to Terrain
Take Action as Necessary to Recover Safe Terrain Clearance
SPINS
If a Spin is Entered Inadvertently
Control Column ………….. Full Forward, Ailerons Neutral
Full Rudder ………………… Opposite Direction of Spin
Power Levers ……………… IDLE
Controls …………………….. Neutralize when Rotation Stops
Execute a smooth pullout
Environmental Failure (L or R ENVIR FAIL annunciator)
Bleed air valve (affected side) - CYCLE TO ENVIR OFF AND BACK OPEN
If ENVIR FAIL annunciator extinguishes, continue operation, if annunciator remains
Bleed air valve (affected side) - ENVIR OFF (ENVIR off annunciator - extinguished)
Fuel Pressure Low (L or R Fuel Pressure Lo Annunciator)
Standby pump (failed side) ….. ON
Unscheduled Electric Elevator Trim (if installed)
Airplane Attitude ……… MAINTAIN (USING ELEVATOR CONTROL)
Control wheel disconnect switch ….. DEPRESS FULLY (PITCH TRIM) Annunciator illuminated
Manually re-trim the airplane
