GLA Emergency Procedures

Question 0

PROPELLER COLLISIONS DURING GROUND OPERATIONS

Answer 0

Power Levers …………………………… GROUND FINE or IDLE
Condition Levers ………………………. FUEL CUTOFF

Question 1

ENGINE FIRE ON GROUND

Answer 1

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

Question 2

ENGINE FAILURE DURING TAKEOFF, ABORTED TAKEOFF

Answer 2

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)

Question 3

ENGINE FIRE OR FAILURE IN FLIGHT

Answer 3

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)

Question 4

ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (Vmca)

Answer 4

Reduce power on operative engine as required to maintain control
Lower nose to achieve airspeed above Vmca

Question 5

OIL PRESSURE LOW (L or R OIL PRES LO ANNUNCIATOR)

Answer 5

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

Question 6

ELECTRICAL SMOKE OR FIRE

Answer 6

Oxygen Mask and goggles ……. Don
Purge Valves …………. Open
Crew …….. Establish Communications

Question 7

Environmental Systems Smoke or Fumes

Answer 7

Oxygen Masks and Goggles ……. Don
Purge Valves ……… Open
Crew ……… Establish Communications

Question 8

Cabin Door or Cargo Door Unlocked (Cabin or Cargo Door Annunciator)

Answer 8

All Occupants ……… Confirm Seated with seatbelts securely fastened

Question 9

Emergency Descent

Answer 9

Power levers............... Idle
Prop levers .......... Full forward (set 1700 rpm)
Flaps ..........       17 degrees
Landing Gear ........  Down
Airspeed ........... 180 Knots

Question 10

Glide

Answer 10

Landing Gear - Up
Flaps - Up
Prop levers - feather
Airspeed - 140 Knots

Question 11

Single Inverter or AC Bus Failure (L or R AC Bus ANNUNCIATOR)

Answer 11

AC Bus Switch (Failed Side) - Cycle Off, than on (AC Bus Annunciator - Extinguished)

Question 12

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

Answer 12

Attitude/Heading Control …… Use standby attitude indicator and compass

Question 13

Dual Inverter Failure (L and R AC Bus Annunciator)

Answer 13

attitude/heading control …… use standby attitude indicator and compass

Question 14

Dual Generator Failure (L and R DC GEN Annuniactors)

Answer 14

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

Question 15

High Differential Pressure (CAB DIFF HI) Annunciator

Answer 15

Bleed Air Valves………. ENVIR OFF

Question 16

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

Answer 16

Bleed Air Valve (affected engine) …….. INST & ENVIR OFF

ENVIR OFF annunciator Illuminated

Question 17

Unscheduled Rudder Boost Activation

Answer 17

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)

Question 18

Use of Oxygen

Answer 18

Oxygen Masks …… DON
Cabin Oxygen Control …… PULL ON
Crew ……… ESTABLISH COMMUNICATIONS

Question 19

Rapid Loss of Pressurization/Explosive Decompression

Answer 19

Oxygen Masks ……. DON
Cabin Oxygen Control ……. PULL ON
Crew ……….. ESTABLISH COMMUNICATIONS

Question 20

In-Flight Activation of GPWS Warning (In IMC or at NIGHT)

Answer 20

Wings ................. Level
Airspeed ............. 122 Knots
Power .................. Max Allowable
Gear and Flaps .... Retract
Continue Climb at 122 KIAS until all visual and Aural Warnings Cease

Question 21

In-Flight Activation of GPWS warning (in DAY VMC)

Answer 21

Evaluate Flight Path with Respect to Terrain

Take Action as Necessary to Recover Safe Terrain Clearance

Question 22

SPINS

Answer 22

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

Question 23

Environmental Failure (L or R ENVIR FAIL annunciator)

Answer 23

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)

Question 24

Fuel Pressure Low (L or R Fuel Pressure Lo Annunciator)

Answer 24

Standby pump (failed side) ….. ON

Question 25

Unscheduled Electric Elevator Trim (if installed)

Answer 25

Airplane Attitude ……… MAINTAIN (USING ELEVATOR CONTROL)
Control wheel disconnect switch ….. DEPRESS FULLY (PITCH TRIM) Annunciator illuminated
Manually re-trim the airplane