MANEUVERS Flashcards
PREFLIGHT CHECK
ENGINE ANTI-ICE
SYS……………………………………………. ON
ENG ANTI ACT………………………….. STBY
ENGINE ANTI-ICE…………………….. OFF
ENG ANTI-ICE ACTUATORS…….. MAIN
ENG ANTI-ICE……………………………. ON
ENGINE START – [EXTERNAL POWER]
ENGINE START – [EXTERNAL POWER]
[CAUTION]: Never connect EXT PWR source to airplane unless battery indicating at least 20v.
If battery voltage less than 20v, battery must be recharged or replaced before connecting EXT PWR.
NOTE: When EXT PWR source used it must be set at 28.0 – 28.4 volts and be capable of producing 1,000 amps momentarily and 300 amps continuously.
The battery should be on to absorb transients present in some EXT PWR sources, EXT PWR ANNUN is provided to alert crew when an EXT DC PWR plug is connected to airplane.]
AVIONICS MASTER ……………………… OFF
L / R GEN ………………………………………. OFF
BATT ……………………………………………… ON
EXT PWR SOURCE ………………………. OFF, THEN CONCT
EXTERNAL POWER SOURCE ……… ON
VOLTMETER …………………………………. 28.0 – 28.4 VOLTS
[NOTE: If the battery partially discharged, the BATT CHG ANNUC will ILLUM approx 6 secs after the EXT PWR is on line.
If ANNUN does not ext w/i 5 mins, refer to BATT CHRGE RATE]
PROP LEVER…………………………………. FEATHER
RH IGN ………………………………………… ON
R IGN ON (ILLUM) / R FUEL PRESS (EXT)
RH COND LVR (12% N1 OR ABV …. LOW IDLE
RH ITT / N1 ……………………………………. (1000°C MAX)
RH OIL PRESS ……………………………… CHECK
RH IGN (50% N1 OR ABOVE) ……… OFF
LH IGN / ENG START …………………… ON
[L IGN ON (ILLUM) / L FUEL PRESS (EXT)
LH COND LVR (12% N1, OR ABV) … LOW IDLE
LH ITT AND N1 ……………………………… (1000°C MAX)
LH OIL PRESS ………………………………. CHECK
LH IGN (50% N1 OR ABOVE ……….. OFF
EXT PWR SOURCE ……………………… DISC
L / R GEN ……………………………………… RESET, THEN ON
PROP LEVERS ……………………………….FULL FORWARD
APPROACH TO STALL – TAKEOFF CONFIGURATION
APPROACH TO STALL – TAKEOFF CONFIGURATION
TORQUE ………………………….. 600 LBS
FLAPS ……………………………… APPROACH
GEAR ………………………………. DOWN
BANK ………………………………. 15° - 30°
AIRSPEED ………………………. 90 KTS
APPROX PITCH ……………… 8°
*RECOVERY*
POWER ………………………….. AS NEEDED
ATTITUDE …………………….. REDUCE ANGLE OF ATTACH
POS RATE / GEAR ………… UP
AIRSPEED ……………………… VYSE
FLAPS ……………………………. UP
APPROACH TO STALL – LANDING CONFIGURATION
APPROACH TO STALL – LANDING CONFIGURATION
TORQUE ……………………….. 200 LBS
FLAPS …………………………… APPROACH
GEAR ……………………………. DOWN
FLAPS ………………………….. FULL
PROPS …………………………… 1900 RPM
ALTITUDE …………………….. DESCEND (500 fpm)
AIRSPEED ……………………. 80 KTS
PITCH …………………………… 8°
*RECOVERY*
POWER ………………………… AS NEEDED
ATTITUDE ……………………. BREAK ANGLE OF ATTACK
AIRSPEED ……………………. 100 KTS
POS RATE / GEAR ………. UP
FLAPS ………………………….. UP
APPROACH TO STALL – ENROUTE
APPROACH TO STALL – ENROUTE
TORQUE ………………………… 200 LBS
PITCH ……………………………. 10°
AIRSPEED …………………….. REDUCE (100 KTS APPROX)
*RECOVERY*
POWER …………………………. AS NEEDED
ATTITUDE …………………….. REDUCE ANGLE OF ATTACH
AIRSPEED ……………………. INCREASE
CFIT
CFIT
POWER ………………………………………. MAX
ATTITUDE ………………………………….. WINGS LEVEL
PITCH …………………………………………. 15°
CONFIGURATION ……………………… LEAVE AS IS
CIRCLING
CIRCLING
*IAF*
TORQUE ……………….800 LBS
FLAPS ……………………APPROACH
*FAF*
TORQUE ……………….400 LBS
GEAR …………………….DOWN
*LEAVING MDA*
FLAPS ……………………FULL
PROPS …………………..FORWARD
YAW DAMP …………..OFF
FLOWS - AFTER START (SINGLE PILOT)
FLOWS - AFTER START (SINGLE PILOT)
INVERTERS……………………………CHECK 1 / 2 (105-120 V) LOADMETERS……………………….PARALLEL
AVIONICS MASTER………………ON
BLEED AIR VALVES………………SET
ENV SYSTEMS CONTROLS…SET
BRAKE DEICE………………………..AS REQ
FLAPS…………………………………….SET
FLIGHT CONTROLS………………CHECK
ENGINE ANTI-ICE…………………..SET
TRIMS……………………………………..0°/0°/TAKEOFF
FLOWS - AFTER TAKEOFF (SINGLE PILOT)
FLOWS - AFTER TAKEOFF (SINGLE PILOT)
YAW DAMP………………………………..ON
PROPS………………………………………..1900
WINDSHIELD / ANTI-ICE…………..AS REQ
PRESSURIZATION…………………….CHECK
FLOWS - BEFORE TAKEOFF (SINGLE PILOT)
FLOWS - BEFORE TAKEOFF (SINGLE PILOT)
PRESSURIZATION…………………………….. CHECK / SET
ELEV TRIM / AUTOPILOT / YD…………. CHECK / SET
* VAC PNEUMATIC PRESS……………….. CHECK
* ALTITUDE ALERT……………………………. CHECK
PROP SYNC……………………………………… ON
INSTRUMENTS…………………………………. CHECK
* GOVENORS / RUDDER BOOST……. CHK (1 at a time)
* AUTOFEATHER……………………………… CHK (2 at a time) / ARM
PROP LEVERS………………………………….. FORWARD
* ENGINE ANTI-ICE …………………………. CHECK / OFF
AUTO IGNITION……………………………….. CHECK / ON
ICE PROTECTION…………………………….. AS REQ
LIGHTS……………………………………………… SET
GENERATOR LOAD………………………….. PARALLEL
ANNUNCIATORS……………………………… OUT
TAKEOFF BRIEFING…………………………. COMPLETE
HOT 5s……………………………………………… ON
X-PNDER…………………………………………… SET
FLOWS - DESCENT
FLOWS - DESCENT
PRESSURIZATION ………….. SET
FUEL BALANCE ……………… CHECK
ILS - TWO ENGINE
ILS - TWO ENGINE
*2 MI. PRIOR FAF*
TORQUE ……………… 800 LBS
FLAPS ………………….. APPROACH
AIRSPEED …………… 135 KTS
*GLIDESLOPE INT*
TORQUE …………….. 800 LBS
GEAR ………………….. DOWN
FLAPS ………………… DOWN
PROPS …………….…. FORWARD
YAW DAMP ………… OFF
FLOWS - PARKING
FLOWS - PARKING
AVIONICS MASTER……………OFF
INVERTER ………………………….OFF
BATTERY…………………………….CHARGED
ITT……………………………………….STABILIZE
CONDITION LEVERS…………FUEL CUTOFF
PROPS………………………………..FEATHER
DC VOLT / LOADMETERS…CHECK
OVRHD PANEL………………….OFF
OXY SYSTEM READY……….OFF
FLOWS - PREFLIGHT - (SINGLE PILOT)
FLOWS - PREFLIGHT - (SINGLE PILOT)
FIRE EXTINGUISHER …………………….. COPILOT SEAT
COPILOT CIRCUIT BREAKERS ……… CHECK
ALTERNATE STATIC AIR SOURCE … NORMAL
OXYGEN SUPPLY FIRE SYSTEM ….. TEST
CABIN TEMP MODE CONTROL …… OFF
ELEC HEAT …………………………………….. OFF
AFT BLOWER …………………………………. OFF
STALL WARNING …………………………… TEST
BLEED AIR VALVES ……………………….. ENVIRON OFF
VENT BLOWER ………………………………. OFF
CONDITION LEVERS …………………….. CUTOFF
PROP LEVERS ……………………………….. FORWARD
POWER LEVERS ……………………………. IDLE
OXY MANUAL OVERRIDE ……………. IN
OXY SYSTEM HANDLE ………………… PULL
OXY ……………………………………………….. CHECK
TRIMS ……………………………………………. ZERO
CABIN PRESSURE ……………………….. PRESS
RUDDER BOOST …………………………. ON
ELEC TRIM …………………………………… ON
PRESS CONTROLLER ………………… 1000’ ABOVE CRUISE
PILOT OXY MASK ………………………. CHECK
ANNUNC PANEL ………………………… TEST
HYD FLUID SENSOR ………………….. TEST
LDG GEAR HANDLE …………………… TEST
BEACON ……………………………………… ON
ICE PROTECTION ………………………. OFF
PROP SYN ………………………………….. ON
ICE VANES …………………………………. CHECK
BATTERY ……………………………………. ON
FUEL SYSTEM …………………………… CHECK
PILOT CIRCUIT BREAKERS ………. CHECK
FLOWS - STARTING
FLOWS - STARTING
ENGINE START – [BAT] VOLT …………. (23v MIN)
RH IGN AND ENG START ………………… ON
[R FUEL PRESS] - (EXT)
RH CONDITION LEVER …………………… (12% N1)
LOW IDLE RH ITT AND N1 ………………. (1000c MAX)
RH OIL PRESSURE …………………………… Check
[NOTE: If no ITT rise observed W/I 10 secs after moving CND LVR to LOW IDLE, move to CUTOFF. Allow 60 secs.]
RH IGN AND ENG START ……………….. 50% N1 – OFF
RH COND LVR …………………………………. HIGH IDLE
RH GEN ……………………………………………. RESET / ON.
In order to turn the GEN ON, the GEN switch must be held in spring loaded RESET position for a min of 1 sec, then released to ON.
BATTERY …………………………………………. CHARGE [LOAD-50% OR LESS.
The BATTERY CHARGE ANNUN will ILLUM approx 6 seconds after the generator is on line.
If the ANNUN does not EXT w/i 5 mins, refer to OTHER NORMAL PROCEDURES.]
RH GEN………………………………………….. OFF
LH IGN / ENG START ……………………. ON
[L FUEL PRESS] - (EXT)
LH COND LVR ………………………………. (12% N1) LOW IDLE
RH GEN…………………………………………. ON
LH ITT / N1 …………………………………….. (1000c MAX)
LH OIL PRESSURE ……………………….. CHECK
LH IGN / ENG START …………………… OFF - 50% N1 – OFF
DC VOLT / LOADMETERS ……………. (27.5 – 29.0 V)
LH GEN………………………………………….. RESET / ON
RH COND LVR ……………………………… LOW IDLE
FLOWS - LANDING
FLOWS - LANDING
AUTOFEATHER………………….ARM
GEAR………………………………….DWN
FLAPS…………………………………SET
PROPS………………………………..FORWARD
A/P / YAW DAMP………………..OFF
ILS - SINGLE ENGINE
ILS - SINGLE ENGINE
*2 MI. PRIOR FAF*
TORQUE …………………………. 1600 LBS.
FLAPS ……………………………… APPROACH
AIRSPEED ……………………….. 135 KTS
*GLIDESLOPE INT*
TORQUE ………………………….. 1400 LBS
GEAR ……………………………….. DOWN
PROPS ……………………………… FORWARD
YAW DAMP ………………………. OFF
AIRSPEED …………………………. VREF +10
LANDING GEAR MANUAL EXTENSION
LANDING GEAR MANUAL EXTENSION
AIRSPEED ……………………………………………… < 181 KTS
LDG GR CB (Pilot’s Subpanel) ……………… PULL
LANDING GEAR CONTROL …………………. DWN
ALTERNATE EXT HANDLE …………………… PUMP UP / DWN
(Until L / R / NOSE illum / further resistance felt)
ALTERNATE EXT HANDLE ………………….. STOW
NOTE: Ensure ALT EXT handle is in the full DWN position prior to placing it in the securing clip.
MISSED APPROACH - SINGLE ENGINE
MISSED APPROACH - SINGLE ENGINE
POWER ……………………. MAX ALLOWABLE
POS RATE / GEAR ….. UP
FLAPS ……………………… UP
AIRSPEED ……………….. VYSE
500’ AGL / POWER …. SET
PROP ……………………….. 1900 RPM
MISSED APPROACH – TWO ENGINE
MISSED APPROACH – TWO ENGINE
POWER …………….FULL
FLAPS ………………UP
POS RATE…………GEAR UP
YAW DAMP ………ON
500’ ……………….…CLIMB PWR
PROPS ……………..1900 RPM
NO FLAP LANDING
NO FLAP LANDING
*DOWNWIND*
TORQUE …………………800 LBS
PROPS …………………….1700 RPM
AIRSPEED ……………….150 KTS
*ABEAM*
GEAR ……………………….DOWN
PROPS ……………………. FORWARD
AIRSPEED ………………..135 KTS
*BASE*
TORQUE …………………..500LBS
AIRSPEED …………………VREF +10
Y/D ……………………………OFF
*FINAL*
AIRSPEED ………………….VREF
VSI ……………………………..500-600 FPM
NON PRECISION APPROACH - SINGLE ENGINE
NON PRECISION APPROACH - SINGLE ENGINE
*IAF*
TORQUE ……………………………. 1600 LBS
AIRSPEED ………………………….. 150 KTS
FLAPS ………………………………… APPROACH
*FAF*
GEAR ………………………………….. DOWN
TORQUE …………………………….. 1400 LBS
PROPS ………………………………… FULL
YAW DAMP …………………………. OFF
NON PRECISION APPROACH - TWO ENGINE
NON PRECISION APPROACH - TWO ENGINE
*IAF*
TORQUE …………………………….. 800 LBS
AIRSPEED ………………………….. 150 KTS
FLAPS ………………………………… APPROACH
*FAF*
TORQUE ……………………………. 400 LBS
GEAR …………………………………. DOWN
FLAPS ………………………………… DOWN
PROPS ……………………………….. FULL
YAW DAMP ……………………….. OFF
PRE-FLIGHT
ALTITUDE ALERT CHECK
PRE-FLIGHT
PILOT’S BARO……………… ADJUST - NEAREST 100’
ALT ALT ALERTER ………. MATCH ALTIMETER READING
PILOT’S BARO …………….. INC / DEC ALT 200’ FROM INITIAL ALT
[Aural warning horn - 2 seconds]
ALT ALERT ANNUN on pilot’s / co-pilot’s instrument panel and ALT pre-selector panel (illuminate)
PILOT’S BARO……………… ADJUST TO FIELD ELEV
ALT ALERT ANNUN …….(EXT) at 200’ from alert panel setting.
PREFLGHT CHECKS
FUEL SYSTEM
PREFLGHT CHECKS
SHUTOFF VALVES ………… CLOSE
STDBY PUMPS ………………. ON - (1 at a time. Listen for ops)
L / R FUEL PRESS (ILLUM)
SHUTOFF VALVES ………… OPEN - L / R FUEL PRESS (EXT)
STANDBY PUMPS …………. OFF - L / R FUEL PRESS (ILLUM)
X-FEED …………………………….ALT LH / RH X-FEED (ILLUM)
L / R FUEL PRESS (EXT)
X-FEED ……………………………. OFF
AUX TANK TRANSFER …… AUTO
NO TRANSFER LIGHT…….. PUSH TO TEST
PREFLIGHT
* AUTO-FEATHER CHECK
* AUTO-FEATHER CHECK
POWER LEVERS …………………………. 500 LBS TORQUE
AUTO-FEATHER SWITCH ………….. HOLD TO TEST
POWER LEVERS …………………………. RETARD INDIVID
- 410 LBS – OPPOSITE AUTO-FEATHER (EXT)
- 260 LBS – BOTH AUTO-FEATH (EXT) /
PROP FEATHERS RETURN TO 500 LBS AFTER TEST
POWER LEVERS ………………………… IDLE (EXT)]
AUTO-FEATHER SWITCH……………. RELEASE
PREFLIGHT
CHECKS AUTOPILOT CHECK
PREFLIGHT
ELEV TRIM ………………………. TAKEOFF POSITION
ELEC ELEV TRIM …………….. ON
ELEVATOR ……………………….. FORWARD
AUTOPILOT ……………………… ENGAGE YAW / AP – (ILLUM)
ELEC ELEV TRIM ……………… OPERATE BOTH DIRECT A/P disengages / YD remains engaged
ELEVATOR ……………………….. CENTERED
AUTOPILOT ……………………… ENGAGE
Pull back on elevator -Pitch trim moves nose down
Push forward on elevator – Pitch trim moves nose up
AUTOPILOT / TRIM DISC ….. DEPRESS – (1ST LEVEL) YAW DISC / AP DIS – (ILLUM) FLASHING, THEN (EXT)
REPEAT FOR CO-PILOT’S SIDE
PREFLIGHT
* BRAKE DEICE CHECK
BRAKE DEICE
BLEED AIR VALVES ………………………….. OPEN
BRAKE DEICE …………………………………… ON
BRAKE DEICE – (ILLUM)
BRAKE DEICE ………………………………….. OFF
BRAKE DEICE – (EXT)
PREFLIGHT CHECK
ICE VANES
Eng anti-ice actuators…..STDBY
Eng anti-ice……………………OFF
Eng anti-ice Actuators…..MAIN
Eng Anti-ice……………………ON
PREFLIGHT CHECKS
ELECTROTHERMAL PROP DEICE CHECK
ELECTROTHERMAL PROP DEICE CHECK
(CAUTION – Do no operate prop deice when props are static)
AUTOMATIC PROP DEICE ………………. AUTO
DEICE AMMETER …………………………….. 18-24 AMPS
(Monitor 90 secs to ensure automatic timer operation)
MANUAL PROP DEICE ……………………. HOLD IN MANUAL
Small deflection on both loadmeters indicates manual system is operating.
Deice Ammeter ……………………………….. 0 Amps
Manual Prop Deice …………………………. RELEASE
Deice Ammeter ………………………………. 18-24 AMPS
Automatic Prop Deice ……………………. OFF
PREFLIGHT
ELEVATOR TRIM CHECK
PREFLIGHT
ELEC ELEVATOR TRIM ………………………ON
PILOT / CO-PILOT TRIM SWITCHES …CHECK
Move each switch fore and aft – verify trim INOP
Move both switches for and aft – verify trim OPERATES
Ensure pilot’s trim switch overrides copilot’s trim switch
A/P TRIM DISC ………………………………….. PRESS (2ND LEVEL)
ELEC TRIM OFF – (ILLUM)
ELECTRIC ELEVATOR TRIM ……….. OFF, THEN ON
ELEC TRIM OFF – (EXT)
PREFLIGHT
PRESSURIZATION CHECK
PREFLIGHT
BLEED AIR VALVES …………….. OPEN
PRESS CONTROLLER …………. SET (1000’ BLW FLD ELEV)
RATE KNOB…………………………….12:00 POS
CABIN PRESS SWITCH ……….. HLD IN TEST POS
CABIN ALT / VSI………………….. CHK FOR DESC IND
CABIN PRESS SWITCH ……….. REL TO PRESS POS
PRESS CONTR …………………….. SET
PREFLIGHT CHECK
* PRIM GOV / OVERSPEED GOV / RUD BOOST CHECK
PREFLIGHT CHECK
* PRIM GOV / OVERSPEED GOV / RUD BOOST CHECK
BLEEDS ………………………………… ON
RUDDER BOOST …………………. ON
PROP GOV TEST SWITCH ….. HOLD TO TEST
PWR LVRS (Indiv) …………………. INC UNTIL STABLE (1800-1910 RPM)
PROP LEVER ……………………….. RET TO DET, THEN FULL FRWRD
(CHECKS PRIMARY GOV)
POWER LEVER ……………………. INC UNTIL RUD MOVEMENT
POWER LEVER ……………………. IDLE
• REPEAT STEPS 3-6 FOR OPPOSITE ENGINE
PREFLIGHT CHECK
SURFACE DEICE SYSTEM CHECK
SURFACE DEICE SYSTEM CHECK
CONDITION LEVERS ……………………….HIGH IDLE
PNEUMATIC PRESSURE ………………… CHECK
SURFACE DEICE SWITCH ……………… SINGLE / RELEASE
[Pneum Press – Decrease momentarily chk boots.
Inflation time - 6 secs - wings, 4 secs - horiz stabilizer]
SURFACE DEICE SWITCH ……………… MANUAL / HOLD
[Pneum Press – Decrease, chk boots - inflation]
SURFACE DEICE SWITCH ……………….RELEASE, chk boots
CONDITION LEVERS ………………………. LOW IDLE
STALL WARNING HEAT ………………….. CHECK
PITOT HEAT ………………………………………CHECK
PREFLIGHT CHECK
* VACUUM / PNEUMATIC PRESSURE CHECK
* VACUUM / PNEUMATIC PRESSURE CHECK
- Left Bleed Air Valve . INSTR & ENVIR OFF
a. L BL AIR OFF . ILLUMINATED
b. Gyro Suction Gauge and Pneumatic Pressure Gauge in Green
Arc. - Right Bleed Air Valve. INSTR & ENVIR OFF
a. R BL AIR OFF , L BL AIR FAIL &
R BL AIR FAIL . ILLUMINATED
b. Gyro Suction Gauge and Pneumatic Pressure Gauge . ZERO - Left Bleed Air Valve . OPEN
a. L BL AIR OFF , L BL AIR FAIL &
R BL AIR FAIL . EXTINGUISHED
b. Gyro Suction Gauge and Pneumatic Pressure Gauge in Green
Arc. - Right Bleed Air Valve. OPEN
R BL AIR OFF - EXTINGUISHED
RETURN TO PAGE N-15, BEFORE TAKEOFF (RUNUP), STEP 16
PREFLIGHT CHECKS YAW DAMP CHECK
PREFLIGHT CHECKS YAW DAMP CHECK
YAW DAMP …………………. ON YAW (ILLUM)
RUDDER PEDALS ………. CHECK ADDED RES
AP / TRIM DISC ………….. DEPRESS (1ST LEVEL)
YAW DIS (ILLUM) FLASHING, THEN (EXT)
• REPEAT FOR CO-PILOT’S SIDE
PREFLIGHT CHECKS
WINDSHIELD ANTI-ICE CHECK
PREFLIGHT CHECKS
(CHECK PILOT / CO-PILOT ONE AT A TIME)
WINDSHIELD ANTI-ICE …………….. HI
(Observe increase on LH / RH loadmeters)
WINDSHIELD ANTI-ICE …………….. OFF, THEN NORMAL
(Observe increase on LH / RH loadmeters)
WINDSHIELD ANTI-ICE …………….. OFF
PREFLIGHT CHECKS
* ENGINE ANTI-ICE
* ENGINE ANTI-ICE
ENGINE ANTI-ICE ACTUATORS ……………. STDBY
ENGINE ANTI-ICE ………………………………….. OFF
L / R ENG ANTI-ICE – (EXT)
ENGINE ANTI-ICE ACTUATORS …………… MAIN
ENGINE ANTI-ICE …………………………………. ON L / R
ENG ANTI-ICE - (ILLUM)
STEEP TURNS
STEEP TURNS
CONFIGURATION …….CLEAN
TORQUE ……………………1200 lbs.
PROPS ……………………….1700 RPM
AIRSPEED ………………….180 KTS
BANK …………………………45°
PITCH ………………………..+4°
AFTER 30° BANK
TORQUE ……………………1300 lbs.
VISUAL APPROACH - SINGLE ENGINE
VISUAL APPROACH - SINGLE ENGINE
*DOWNWIND*
TORQUE ……………………………………………………. 1600 LBS.
AIRSPEED ……………………….140 KTS FLAPS
APPROACH AIRSPEED ….130 KTS
*ABEAM*
GEAR ………………………………DOWN
*BASE*
AIRSPEED ……………………….130 KTS
PROPS …………………………….FORWARD
YAW DAMP ……………………..OFF
CHECKLIST …………………………..COMPLETE
FINAL AIRSPEED …………………..VREF + 10
VISUAL APPROACH – TWO ENGINE
VISUAL APPROACH – TWO ENGINE
*DOWNWIND*
TORQUE ………………800 lbs.
AIRSPEED …………….150 KTS
FLAPS …………………..APPROACH
AIRSPEED …………….135 KTS
*ABEAM*
GEAR ……………………DOWN
*BASE*
FLAPS …………………..DOWN
PROPS ………………….FORWARD
YAW DAMP …………. OFF
CHECKLIST …………..COMPLETE
FLOWS - AFTER LANDING
FLOWS - AFTER LANDING
LIGHTS……………………………….OFF
FLAPS…………………………………UP
TEMP/CTRLLR……………………OFF
VENT BLOWER………………….OFF
BLEED AIR VALVES……………ENV OFF
XPNDER……………………………..SET
PRESS DIFF………………………..0
TRIMS…………………………………0/0/TAKEOFF
ENG ANTI-ICE…………………….SET
AUTO IGNITION…………………OFF
AUTO-FEATHER…………………OFF
EMERGENCY
Simulated One-engine INOP
Propeller …………… 1600 RPM
Power Lever ……… 120 ft - lbs Torque
