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FENIX B-200 > MANEUVERS > Flashcards

MANEUVERS Flashcards

1
Q

PREFLIGHT CHECK

ENGINE ANTI-ICE

A

SYS……………………………………………. ON

ENG ANTI ACT………………………….. STBY

ENGINE ANTI-ICE…………………….. OFF

ENG ANTI-ICE ACTUATORS…….. MAIN

ENG ANTI-ICE……………………………. ON

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2
Q

ENGINE START – [EXTERNAL POWER]

A

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

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3
Q

APPROACH TO STALL – TAKEOFF CONFIGURATION

A

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

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4
Q

APPROACH TO STALL – LANDING CONFIGURATION

A

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

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5
Q

APPROACH TO STALL – ENROUTE

A

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

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6
Q

CFIT

A

CFIT

POWER ………………………………………. MAX

ATTITUDE ………………………………….. WINGS LEVEL

PITCH …………………………………………. 15°

CONFIGURATION ……………………… LEAVE AS IS

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7
Q

CIRCLING

A

CIRCLING

*IAF*

TORQUE ……………….800 LBS

FLAPS ……………………APPROACH

*FAF*

TORQUE ……………….400 LBS

GEAR …………………….DOWN

*LEAVING MDA*

FLAPS ……………………FULL

PROPS …………………..FORWARD

YAW DAMP …………..OFF

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8
Q

FLOWS - AFTER START (SINGLE PILOT)

A

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

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9
Q

FLOWS - AFTER TAKEOFF (SINGLE PILOT)

A

FLOWS - AFTER TAKEOFF (SINGLE PILOT)

YAW DAMP………………………………..ON

PROPS………………………………………..1900

WINDSHIELD / ANTI-ICE…………..AS REQ

PRESSURIZATION…………………….CHECK

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10
Q

FLOWS - BEFORE TAKEOFF (SINGLE PILOT)

A

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

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11
Q

FLOWS - DESCENT

A

FLOWS - DESCENT

PRESSURIZATION ………….. SET

FUEL BALANCE ……………… CHECK

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12
Q

ILS - TWO ENGINE

A

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

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13
Q

FLOWS - PARKING

A

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

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14
Q

FLOWS - PREFLIGHT - (SINGLE PILOT)

A

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

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15
Q

FLOWS - STARTING

A

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

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16
Q

FLOWS - LANDING

A

FLOWS - LANDING

AUTOFEATHER………………….ARM

GEAR………………………………….DWN

FLAPS…………………………………SET

PROPS………………………………..FORWARD

A/P / YAW DAMP………………..OFF

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17
Q

ILS - SINGLE ENGINE

A

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

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18
Q

LANDING GEAR MANUAL EXTENSION

A

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.

19
Q

MISSED APPROACH - SINGLE ENGINE

A

MISSED APPROACH - SINGLE ENGINE

POWER ……………………. MAX ALLOWABLE

POS RATE / GEAR ….. UP

FLAPS ……………………… UP

AIRSPEED ……………….. VYSE

500’ AGL / POWER …. SET

PROP ……………………….. 1900 RPM

20
Q

MISSED APPROACH – TWO ENGINE

A

MISSED APPROACH – TWO ENGINE

POWER …………….FULL

FLAPS ………………UP

POS RATE…………GEAR UP

YAW DAMP ………ON

500’ ……………….…CLIMB PWR

PROPS ……………..1900 RPM

21
Q

NO FLAP LANDING

A

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

22
Q

NON PRECISION APPROACH - SINGLE ENGINE

A

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

23
Q

NON PRECISION APPROACH - TWO ENGINE

A

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

24
Q

PRE-FLIGHT

ALTITUDE ALERT CHECK

A

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.

25
Q

PREFLGHT CHECKS

FUEL SYSTEM

A

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

26
Q

PREFLIGHT

* AUTO-FEATHER CHECK

A

* 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

27
Q

PREFLIGHT

CHECKS AUTOPILOT CHECK

A

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

28
Q

PREFLIGHT

* BRAKE DEICE CHECK

A

BRAKE DEICE

BLEED AIR VALVES ………………………….. OPEN

BRAKE DEICE …………………………………… ON

BRAKE DEICE – (ILLUM)

BRAKE DEICE ………………………………….. OFF

BRAKE DEICE – (EXT)

29
Q

PREFLIGHT CHECK

ICE VANES

A

Eng anti-ice actuators…..STDBY

Eng anti-ice……………………OFF

Eng anti-ice Actuators…..MAIN

Eng Anti-ice……………………ON

30
Q

PREFLIGHT CHECKS

ELECTROTHERMAL PROP DEICE CHECK

A

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

31
Q

PREFLIGHT

ELEVATOR TRIM CHECK

A

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)

32
Q

PREFLIGHT

PRESSURIZATION CHECK

A

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

33
Q

PREFLIGHT CHECK

* PRIM GOV / OVERSPEED GOV / RUD BOOST CHECK

A

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

34
Q

PREFLIGHT CHECK

SURFACE DEICE SYSTEM CHECK

A

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

35
Q

PREFLIGHT CHECK

* VACUUM / PNEUMATIC PRESSURE CHECK

A

* VACUUM / PNEUMATIC PRESSURE CHECK

  1. Left Bleed Air Valve . INSTR & ENVIR OFF
    a. L BL AIR OFF . ILLUMINATED
    b. Gyro Suction Gauge and Pneumatic Pressure Gauge in Green
    Arc.
  2. 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
  3. 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.
  4. Right Bleed Air Valve. OPEN
    R BL AIR OFF - EXTINGUISHED
    RETURN TO PAGE N-15, BEFORE TAKEOFF (RUNUP), STEP 16
36
Q

PREFLIGHT CHECKS YAW DAMP CHECK

A

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

37
Q

PREFLIGHT CHECKS

WINDSHIELD ANTI-ICE CHECK

A

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

38
Q

PREFLIGHT CHECKS

* ENGINE ANTI-ICE

A

* 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)

39
Q

STEEP TURNS

A

STEEP TURNS

CONFIGURATION …….CLEAN

TORQUE ……………………1200 lbs.

PROPS ……………………….1700 RPM

AIRSPEED ………………….180 KTS

BANK …………………………45°

PITCH ………………………..+4°

AFTER 30° BANK

TORQUE ……………………1300 lbs.

40
Q

VISUAL APPROACH - SINGLE ENGINE

A

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

41
Q

VISUAL APPROACH – TWO ENGINE

A

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

42
Q

FLOWS - AFTER LANDING

A

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

43
Q

EMERGENCY

Simulated One-engine INOP

A

Propeller …………… 1600 RPM

Power Lever ……… 120 ft - lbs Torque

FENIX B-200 (5 decks)

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