Emergency Procedures Flashcards
ENGINE FAILURE/ TAKEOFF
A. Power levers idle
B. Brakes
INSUFFICIENT RUNWAY:
Condition levers CUTOFF
Fuel Firewall valves: CLOSED
Electrical Power: OFF-GANG BAR DOWN
ENGINE FAILURE TAKEOFF/AIRBORNE
A. Power: TAKE-OFF
B. Prop Levers: HIGH RPM
C. Speed: Maintain Vyse speed until clear obstacles
D. Gear: UP
A. Confirm inoperative engine: CAUTION, Auto feather system in use DO NOT retard the failed engine until the auto feather system has completely stopped prop rotation.
F. Inoperative Engine Prop Lever: FEATHER
G. Airspeed: VYSE
H. Clean-Up: INOPERATIVE ENGINE
-1. Condition lever: CUTOFF
-2.Bleed air valve-AS REQUIRED
-3.Auto Ignition-OFF
-4.Fuel Firewall valve-CLOSED
-5 Generator Switch-OFF
-6. Fuel Control Heat-OFF
-7 Autofeather-OFF
I. Electrical Load-MONITOR
Caution: if smoke or fumes enters cabin from failed engine, CLOSE PRESSURIZATION BLEED AIR VALVE
ENGINE FAIL or FIRE IN FLIGHT/CHIP DETECTOR LIGHT
AFFECTED ENGINE:
1. Power Lever: IDLE
2. Prop Lever: FEATHER
3. Condition Lever: CUTOFF
4. Fuel Firewall Valve: CLOSED
5. Bleed Air Valve: AS REQUIRED
6. Fire Extinguisher: ACTUATE
7.Clean Up Inoperative Engine:
a. Engine Auto Ignition: OFF
b. Generator Switch: OFF
c. Fuel Control Heat: OFF
d.Prop Sync: OFF
8. Electrical Load: MONITOR
ENGINE FLAMEOUT (2nd ENGINE)
- Power Lever: IDLE
- Prop: DO NOT FEATHER
3.Condition Lever: CUTOFF - Conduct Air Start Procedures: NOTE, The propeller will not unfeather without the engine operating.
ENGINE FAILURE IN FLIGHT BELOW MINIMUM SINGLE-ENGINE CONTROL SPEED
- Reduce power on operative engine as required
- Lower nose to accelerate above Vmc
- Power: AS REQUIRED
- Power Lever: IDLE INOP ENGINE
- Prop Lever: FEATHER
- CLEAN UP INOP ENGINE,
a. Condition Lever: CUTOFF
b. Engine Auto Ignition: OFF
c. Generator Switch: OFF
d. Fuel Control Heat: OFF
e. Prop Sync: OFF - Electrical Load: MONITOR
ENGINE FIRE (Ground)
Affected Engine:
1. Condition Lever: CUTOFF
2. Fuel Firewall Valve: CLOSED
3. Starter Switch: STARTER ONLY
4. Fire Extinguisher-ACTUATE as required
SINGLE ENGINE LANDING
Normal Landing Procedure with the following:
1. Prop Lever: operative engine, HIGH
2. Approach Speed: Vref+10
SINGLE ENGINE GO-AROUND
- Power: TAKEOFF
- Flaps: UP
- Landing Gear: UP
- Airspeed: Vyse
AIR START
STARTER ASSIST: Determine reason for failure, above FL200 starts are hotter, during engine acceleration you may need to move condition lever to CUTOFF to avoid exceeding MAX ITT.
1. Cabin temp mode: OFF
2. Vent Blower: AUTO
3. Radar: STANDBY or OFF
4. Windshield Heat: OFF
5. Power Lever: IDLE
6. Condition Lever: CUTOFF
7. Fuel Firewall Valve: OPEN
NOTE: if conditions permit, retard operative engine ITT to 700C or less to reduce the possibility of exceeding ITT limit.Reduce electrical load to minimum consistent with flight conditions.
8. Ignition and Engine Start Switch: ON
9. Check ignition light: ON
10. Condition Lever: LO-IDLE(8 sec after start switch is activated)
11. ITT and N1- MONITOR (1090c max)
12. Ignition and Engine Start Switch-OFF
13. Generator: ON
14. Prop Lever: As Required
15. Power Lever: As Required
16. Fuel Control Heat: ON
17. Electrical Equipment: As Required
WINDMILLING ENGINE AND PROP (NO STARTER)
- Cabin Temp Mode: OFF
- Vent Blower: AUTO
- Radar: STANDBY or OFF
- Windshield Heat: OFF
- Power Lever: IDLE
- Prop Lever: HIGH RPM
- Condition Lever: CUTOFF
- Fuel Firewall Valve: OPEN
- Generator Switch (Inoperative engine) : OFF
- Airspeed: 140kts
- Altitude: BELOW 20,000FT
- Auto Ignition: ARM
- Condition Lever: LO IDLE (8 secs after auto ignition is armed)
- Power: As required
- Generator: ON
- Auto Ignition: OFF
- Fuel Control Heat: ON
- Electrical Equipment: AS required
CROSSFEED (SINGLE ENGINE OPERATION)
LEFT ENGINE INOP:
1. Left standby pump: ON
2. Right Aux fuel transfer-OFF
3. Crossfeed: OPEN
4. FUEL CROSSFEED LIGHT: ON
5. Both FUEL PRESSURE LIGHTS-OUT
RIGHT ENGINE INOP
1. Right STBY Pump: ON
2. Left AUX fuel transfer: OFF
3. Crossfeed: OPEN
4. FUEL CROSSFEED LIGHT: ON
5. BOTH FUEL PRESSURE LIGHTS: OUT
Caution:
If the firewall valve is closed aux fuel supply will not be available and the fuel pressure light will remain illuminated on the side supplying.
TO DISCONTINUE CROSSFEED:
1. STBY pump OFF
2. CROSSFEED: CLOSED
3. Aux Fuel Transfer Switch: ON (If required)
BOOST PUMP FAILURE
- Standby Pump (failed side): ON
- Fuel Pressure Light: OFF
ELECTRICAL SYSTEM FAILURE
GENERATOR INOPERATIVE (Gen Out Annunciator light on)
1. Generator Switch: OFF, then ON to reset
IF Generator will not reset
2. Generator switch: OFF
3. Operating Generator: Do not Exceed 1.0 Load
Excessive Load Meter Indication, (over 1.0)
1. Battery Switch: OFF
If generator will not reset:
2. Generator Switch: OFF
3. Operating Generator: DO NOT EXCEED 1.0 LOAD
Excessive Loadmeter Indication (over 1.0)
1. Battery Switch: OFF (Monitor load meter)
If load meter still indicates above 1.0
2. Non-Essential Loads: OFF
3. Battery Switch: ON
Circuit Breaker Tripped
1. Non-Essential Circuit-DO NOT RESET IN FLIGHT
2. Essential Circuit: a. Circuit breaker, push to reset. b. If circuit breaker trips again, DO NOT RESET.
Subpanel Feeder Circuit Breaker Tripped
1. A short is indicated: DO NOT RESET IN FLIGHT
2. Depending on which circuit breaker is tripped, the following it’s may become inoperative:
a. Fuel quantity gauges
b. fuel pressure warning light.
c. Fuel Crossfeed
d. Aux Empty Light
e. Aux Fuel Transfer Valve
INVERTER INOPERATIVE
SELECT THE OTHER INVERTER
ELECTRICAL SMOKE OR FIRE
- Master switch off (Gang Bar down)
WARNING: Cabin will depressurize and Electrically driven flight instruments will become inoperative. - Oxygen control: ON
- Oxygen Mask: Insert Fittings, DON MASKS
NOTE: Cabin Pressurization dump valve and open storm window (if depressurized) will facilitate smoke and fume removal . - All Electrical Switches: OFF
- Batt and Gen switches: ON
- Essential Electrical Equipment: ON(isolate defective equipment)
- Oxygen: AS REQUIRED
