EPs

Question 1

One-engine-inoperative

Best angle of climb (VXSE) _______
Best rate of climb (VYSE) _______
Enroute climb _______

Answer 1

Best angle of climb (VXSE) 125 knots
Best rate of climb (VYSE) 125 knots
Enroute climb 125 knots

Question 2

Air Minimum Control Speeds (VMCA)

Flaps Up _______
Flaps Approach _______

Answer 2

Flaps Up 94 knots

Flaps Approach 93 knots

Question 3

Airspeed
Emergency Descent _______
Maximum Range Glide _______

Answer 3

Emergency Descent 184 knots

Maximum Range Glide 135 knots

Question 4

ENGINE FIRE OR FAILURE IN FLIGHT

Answer 4

Affected Engine:
Condition Lever ………………………….. FUEL CUTOFF
Prop Lever …………………………………… FEATHER
Firewall Fuel Valve ……………………...CLOSE
Fire extinguisher (if fire warning persists)…. ACTUATE

Question 5

ENGINE FIRE ON GROUND

Answer 5

Affected Engine:
Condition Lever ……………………………………FUEL CUTOFF
Firewall Fuel Valve ………………………………CLOSE
Starter Switch …………………………………….STARTER ONLY
Fire Extinguisher (if fire warning persists) ………. ACTUATE

Question 6

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

Answer 6

Condition Levers ………………………………. FUEL CUTOFF
Prop Levers ……………………………………….. FEATHER
Firewall Fuel Valves ………………………….. CLOSE
Master Switch (gang bar) …………………. OFF
Battery Bus ……………………………………….. EMERG OFF
ESIS Power ………………………………………. OFF

Question 7

ENGINE FAILURE DURING TAKEOFF

(AT OR BELOW V1) – TAKEOFF ABORTED

Answer 7

Power Levers …………………………………. GROUND FINE

Brakes ……………………………………………… MAXIMUM

Question 8

ENGINE FAILURE DURING TAKEOFF

(AT OR ABOVE V1) – TAKEOFF CONTINUED

Answer 8

VR Speed …………….ROTATE TO APPROX 10° PITCH ATTITUDE
Landing Gear (when positive climb est.) …………… UP
Airspeed …………………… MAINTAIN V2 TO 400 FT AGL
Propeller (inoperative engine) ……………….. VERIFY FEATHERED

Question 9

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

Answer 9

Power …………… REDUCE AS REQ’D TO MAINTAIN CONTROL

Nose …………….. LOWER TO ACCELERATE ABOVE VMCA

Question 10

ELECTRICAL SMOKE OR FIRE

Answer 10

Oxygen Mask(s) …………………………………………….. DON
Mask Selector Switch …………………………………… EMERG
Mic Switch(es) ………………………………………………. OXY

Question 11

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

Answer 11

Oxygen Mask(s) …………………………………………….. DON
Mask Selector Switch ………………………………….. EMERG
Mic Switch(es) ………………………………………………. OXY

Question 12

AIRSTAIR DOOR/CARGO DOOR UNLOCKED

Answer 12

All Occupants ………………….. SEATED WITH SEAT BELTS SECURELY FASTENED

Question 13

EMERGENCY DESCENT

Answer 13

Power Levers ………………………………………. IDLE
Prop Levers ………………………………………… FULL FORWARD
Flaps (202 kts max) …………………………… APPROACH
Landing Gear (184 kts max) ………………… DOWN
Airspeed ……………………………………………. 184 KNOTS MAX

Question 14

GLIDE

Answer 14

Landing Gear ……………………………………………. UP
Flaps ……………………………………………………… UP
Prop Levers ……………………………………………… FEATHERED
Airspeed …………………………………………………. 135 KNOTS

Question 15

DUAL GENERATOR FAILURE

Answer 15

Instrument Emergency Lights (if req’d) …………. ON
Generators ………………………………………… RESET, THEN ON
If either generator will reset:
Operating Generator Load meter …………………. MONITOR

Question 16

DUAL GENERATOR FAILURE
(continued)
If neither Generator will reset

Answer 16

ECS Mode ……………………………………………………… OFF
Cockpit/Cabin Blower ………………………………………… AUTO
Non-essential Equipment ……………………………………. OFF

Question 17

USE OF OXYGEN

Answer 17

Oxygen Mask(s) …………………………………………………. DON
Mic Switch(es) …………………………………………………… OXY

Question 18

PRESSURIZATION LOSS

Answer 18

Oxygen Mask(s) ……………………………………….. DON
Mic Switch(es) …………………………………………. OXY
Passenger Manual Drop Out ………………………… PULL ON
Descend ……………………………………………….. AS REQUIRED

Question 19

HIGH DIFFERENTIAL PRESSURE

Answer 19

Bleed Air Valves …………………………………….. ENVIR OFF
Oxygen (crew and passengers) …………………… AS REQUIRED
Descend ……………………………………………… AS REQUIRED

Question 20

AUTO DEPLOYMENT OXYGEN SYSTEM FAILURE

Answer 20

Passenger Manual Drop Out ………………………… PULL ON

Question 21

BLEED AIR FAIL

Answer 21

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

Question 22

SPINS

Answer 22

Control Column …. FULL FORWARD, AILERONS NEUTRAL
Full Rudder ……… OPPOSITE DIRECTION OF SPIN
Power Levers …… IDLE
Rudder …………… NEUTRALIZE WHEN ROTATION STOPS
Execute a smooth pullout

Question 23

UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION

Answer 23

Airplane Attitude ……… MAINTAIN USING ELEVATOR CONTROL

AP/Trim Disconnect ….. DEPRESS AND FULLY HOLD

Question 24

UNSCHEDULED RUDDER BOOST ACTIVATION

Answer 24

AP/Trim Disconnect …… DEPRESS TO 1ST LEVEL AND HOLD
Rudder Boost ………….. OFF
If Condition Persists:
YD/AP Disc (on FGP) … PULL DOWN

Question 25

AUTOPILOT FAILURE, AUTOPILOT MISTRIM [E] OR [A] | If a mistrim indication continues for more than a few seconds

Answer 25

Flight controls ………………………………….. HOLD FIRMLY | AP ………………………………………………. DISENGAGE

Question 26

AUTOPILOT TRIM FAIL [TRIM]

Answer 26

Flight controls ………………………………….. HOLD FIRMLY | AP ………………………………………………. DISENGAGE

Question 27

AUTOPILOT AUTOMATIC DISENGAGEMENT

Answer 27

Maintain airplane control | AP/TRIM Disconnect ……. DEPRESS TO 1ST LEVEL TO CANCEL HORN

Question 28

ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) | In IMC or at Night

Answer 28

Wings ……………………………………………… LEVEL Power ……………………………………………… MAX ALLOWABLE Pitch ……………………………………………….. INCREASE Promptly and smoothly increase pitch towards an initial pitch attitude of 20° to 25° Adjust as required to avoid continuous buffeting and/or stall warning Adjust to maintain 125 KIAS 4. Gear and Flaps ………………………………………………….. UP

Question 29

MISSION EQUIPMENT ITEMS | Electrical Fire or Smoke

Answer 29

Mission Power Switch ……………………………………... OFF Door Power Switch ………………………………………… OFF Mission and Door Power Circuit Breakers ……………… PULL OUT

Question 30

MISSION EQUIPMENT ITEMS | Cabin Depressurization

Answer 30

Mission Power Switch ……………………………………... OFF Cloaking Door …….………………………………………… CLOSE Door Power Switch ………………………………………… OFF