e50p normal procedures

NORMAL PROCEDURESPHENOM 100

This is a document only for Carenado PHENOM 100. Do not attempt a real flight based on this document. You should always use certified and official documents for performing real flights.

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DETAILED NORMAL PROCEDURESThe normal procedures are to be used by a trained flight crew to ensure that the airplane is in

the proper condition and correctly configured for each phase of flight, resulting in a safe and

efficient operation.

The normal procedures are broken down into the following phases:

COCKPIT/CABIN SAFETY INSPECTION

Phase Callout/Challenge: Action/Response:

PHENOM 100 NORMAL PROCEDURES

Arriving at theAirplane

Evaluate if there is room for the taxi-out or push-back maneuver. See if the airplane looks good, leveland normal. Look for fluid spots onthe ground, unexpected things attached to the airplane, bent or unaligned airframe components, etc.If icing is an issue, examine theairplane’s external surface to determine the exact nature and extent of the airplane icing. A close inspection of critical areas such as the wing upper surface is recommended, since clear ice, although critical, is not always visible at a distance.Make sure that the airplane has thewheel chocks and landing gearsafety pins on as required.

2


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PHENOM 100

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3

COCKPIT/CABIN SAFETY INSPECTION (Continued)


Cockpit/CabinSafetyInspection

EmergencyDoor LockingPin

EmergencyDoor

Water Barrier

Documents,Manuals andCharts

MaintenanceStatus

EmergencyEquipment

CHECKVerify Fire Extinguisher, Flashlight(work properly), First Aid Kit, andthe following optional items, ifinstalled:Protective Breathing Equipment(PBE), Smoke Goggles, OverwaterLife Vest and Survival Kit.

REMOVE

SECURED AND LOCKED

AS REQUIREDIt must be installed for single pilotoperation or if the flight is going tobe conducted over water.

CHECK ON BOARDCheck for regulations in countriesintended to fly in, an approvedAirplane Flight Manual, an approved MEL, navigation and approach charts, QRH, runway analyses and driftdown analyses (if applicable).Check documents, such as Certificate of Airworthiness, copy ofthe Insurance Policy and Airplaneweighing document.

CHECK


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PHENOM 100

4




OXYGENSUPPLYHandle

SUPPLYCONTROLKnob

Oxygen MaskRegulator

ELECTRICALPanel

CircuitBreakers

FUEL PUMP 1& 2 Switches

FUEL XFRButton

ELT Switch

PUSH TO RESTORE

PAX AUTO

CHECK 100%

CHECKCheck GEN 1 & 2 Switches andBUS TIE Knob in the AUTOposition, set GPU Button asrequired and check BATT 1 & 2Switches in the OFF position.

CHECKVerify all circuit breakers IN at thepanels adjacent to the left and rightseats.

AUTO

PUSHED OUT

PUSHERCUTOUTButtonHYD PUMPKnob

Gust Lock Pin

PUSHED OUT

AUTO

REMOVE

ARMED


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PHENOM 100

5


Phase Callout/Challenge: Action/Response:Cockpit/CabinSafetyInspection

Rudder GustLock

HEATINGPanel

AIR CONDITIONINGPanel

RELEASENOTE: A light actuation of the pedalmay be required to unlockthe Rudder Gust Lock.

CHECKCheck WSHLD 1 & 2 Switches inthe OFF position and ADS/AOAKnob in the AUTO position.

ICEPROTECTIONPanel

CHECKCheck ENG 1 & 2 Switches,WINGSTAB and INSP LIGHTSwitches in the OFF position.

LDG GEARLever

DN

PRESSURIZATIONPanel

AIR CONDITIONINGPanel

CHECKCheck PRESSURIZATION MODESwitch in the AUTO position,BLEED Knob in the BOTH positionand DUMP Button pushed out.

AS REQUIRED

ENG FIREEXTINGUISHERPanel

ENGSTART/STOPKnobs

CHECKCheck both SHUTOFF Buttonspushed out and BOTTLE SwitchOFF.

STOP

AS REQUIRED


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PHENOM 100

6


EXTERNAL INSPECTION




Prior to ExternalSafetyInspection

ExternalSafetyInspection

CheckExternal Lights

Flap Lever

Seats andBelts

VERIFY ZERO

Set the Emergency/Parking Brake.

Check external lights and turn the lights and batteries OFFimmediately after checking them to avoid batteries discharge.

Perform External Safety Inspection as indicated on RecommendedWalk-Around Sequence.

CONDITION


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PHENOM 100

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AOA Vane CHECK FREEAOA Vane Drain NO OBSTRUCTIONPitot Tube and Static Ports CONDITION, NO

OBSTRUCTION

Oxygen Discharge Indicator GREEN DISK INPLACE

Antennas CONDITIONRed Beacon Light CONDITIONNLG Doors, Wheel and Tire CONDITIONNLG Torque Link CONNECTED

AND SECUREDNLG Safety Pin REMOVEDForward Baggage Compartment Door REMOVEDRadome CONDITION


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PHENOM 100

NOOBSTRUCTION

NOOBSTRUCTION

NOOBSTRUCTION

NOOBSTRUCTIONCLEAR

DRAIN ANDCHECK FORCONTAMINATION

CONDITION

SECURED

CONDITION, NOOBSTRUCTION

CONDITION,

CHECK FREE

Air Inlet.

Access Door

Pitot Tube and Static Ports.

AOA Vane

AOA Vane Drain

LDG/Taxi Lights

Fuselage Air Inlet

Engine Fan

Engine Air Inlet

Starter/Generator Air Inlets.

* Fuel Drains

8

Fuel Drains and Dump Valves................................................................ NO LEAKS

Right Wing De-Ice Boot ......................................................................... CONDITION

MLG Doors, Wheels, Brakes and Tires.................................................. CONDITION

MLG Safety Pin....................................................................................... REMOVED

Fuel Cap ................................................................................................ CLOSED AND LOCKED

Fuel Tank Air Inlet................................................................................... NO OBSTRUCTION

Navigation/Strobe Lights ........................................................................ CONDITION

Right Aileron ......................................................................................... ECK FREE

NOTE: Using an inadequate tool to accomplish the fuel drainage maycause damage to the drain valve.


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PHENOM 100

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Right Aileron Static Dischargers ........................................................... NUMBER (3) AND CONDITION

Right Flaps............................................................................................ CONDITION

Right Spoiler (if applicable)................................................................... CONDITION

Battery Access Door ............................................................................. SECURED

Cowlings................................................................................................ LATCHED

Engine Exhaust..................................................................................... CLEAR

Drain Masts........................................................................................... CONDITION

Oil Level ................................................................................................ CHECK

Oil Filter Impending Bypass Indicator ................................................... NOT EXTENDED

Heat Exchanger Air Exhaust................................................................. CLEAR

Pylon ..................................................................................................... CONDITION

Vertical Stabilizer .................................................................................. CONDITION

Rudder .................................................................................................. CONDITION

Rudder Static Dischargers.................................................................... NUMBER (2) AND CONDITION

Yaw Trim Tab........................................................................................ CONDITION

Horizontal Stabilizer .............................................................................. CONDITION

Horizontal Stabilizer De-Ice Boot.......................................................... CONDITION

Elevator ................................................................................................. CONDITION

Pitch Trim Tab....................................................................................... CONDITION

Elevator Static Dischargers .................................................................. NUMBER (2) AND CONDITION

Antennas............................................................................................... CONDITION

Air Exhaust............................................................................................ NO OBSTRUCTION

Aft Baggage Compartment Door .......................................................... SECURE

Pylon ..................................................................................................... CONDITION

Cowlings................................................................................................ LATCHED


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Engine Exhaust....................................................................................... CLEAR

Drain Masts............................................................................................. CONDITION

Oil Level.................................................................................................. CHECK

Oil Filter Differential Indicator ................................................................. NOT EXTENDED

DC Power Receptacle ............................................................................ CHECK

Left Spoiler (if applicable) ...................................................................... CONDITION

Left Flaps................................................................................................ CONDITION

Left Aileron.............................................................................................. CHECK FREE

Left Aileron Static Dischargers ............................................................... NUMBER (3) AND CONDITION

Roll Trim Tab ......................................................................................... CONDITION

Navigation/Strobe Lights ........................................................................ CONDITION

Left Wing De-Ice Boot ............................................................................ CONDITION

Fuel Cap ................................................................................................. CLOSED AND LOCKED

NOTE: Make sure that the fuel cap is properly closed and locked.

Fuel Tank Air Inlet................................................................................... NO OBSTRUCTION

MLG Doors, Wheels, Brakes and Tires................................................... CONDITION

MLG Safety Pin....................................................................................... REMOVED

LDG/Taxi Lights...................................................................................... CONDITION

Wing Inspection Light ............................................................................ CONDITION

Fuselage Air Inlet.................................................................................... NO OBSTRUCTION

Engine Fan ............................................................................................. CONDITION

Engine Air Inlet ....................................................................................... NO OBSTRUCTION

Starter/Generator Air Inlets..................................................................... CLEAR


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PHENOM 100

11

POWER-UP

Phase Callout/Challenge: Action/Response:Power-Up BATT 1 & 2

SwitchesONIf the battery has been cold soakedfor 2 hours or longer at ambientsurface temperature of -18°C (0°F)or lower, it must be preheated toabove -18°C (0°F) prior to enginestart.

GPU Button(if applicable)

AS REQUIREDVerify AVAIL light illuminatedbefore pushing the GPU Button in.If GPU is not available, maintainGPU Button pushed out.

CVDR Panel(if operative)

CHECKSet the toggle Switch to TESTHOLD 5 SEC position and hold for5 seconds. Verify no fail indicationon CVDR panel annunciators.


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12

BEFORE STARTING

Phase Callout/Challenge: Action/Response:BeforeStarting

Oxygen MaskFlow andMicrophone

CHECKSet MASK MIC Switch to the ONposition and press TEST/RESETButton, then set MASK MIC Switchto the OFF position.

SIGNS/OUTLETSwitch

BELTS/ON

BatteriesVoltage

CHECKEach battery voltage must be atleast 24 V.NOTE: Check GPU switch OFFbefore check batteries voltage.

External Lights AS REQUIRED

Fuel Quantityand Balance

OxygenPressure

CHECK

VERIFY


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PHENOM 100

13

BEFORE STARTING (Continued)

Phase Callout/Challenge: Action/Response:BeforeStarting

TEST Panel

Thrust Levers

TEST- Press the ANNUNCIATOR button(All pushbuttons illuminate).- Press the FIRE Button (Message“FIRE, FIRE” sounds. FIREmessage shows on ITT dials.ENG 1 and ENG 2 SHUTOFFpushbuttons red and white lightsilluminate. E1 and E2 FIRE CASMessages are displayed).- Pull the control wheel out andpress and hold the STALL PROTButton for 4 seconds (Message“STALL, STALL” sounds threetimes and the stick pusheractuates).

IDLE

Parking Brake

Doors

SET

CLOSEDCheck Doors status inMFD/SYSTEM/STATUS.

ENGIGNITIONSwitches

AUTO


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PHENOM 100

14

ENGINE STARTING

Phase Callout/Challenge: Action/Response:EngineStarting

StartingNumber 2

StartingNumber 1

Rotate ENG START/STOPmomentarily to START, then toRUN.Observe N2 increasing, Fuel Flowincreasing, ignition A or B ON, ITTincreasing and Oil Pressureincreasing.Observe start cycle end atapproximately 54% N2, whenIgnition A or B annunciationdisappears and the ITT limitdecreases.

Repeat the sequence above.

NOTE: - Avoid starting the engine with tailwinds speeds higher than 10 kt. It may lead to engine surge, ITT Exceedances and Exhaust Burns. - If any starting limit is exceeded, do not attempt further starts and report to the maintenance personnel. - If a hung or no start occurs, accomplish the Dry Motoring Procedure before attempting another start to reduce hot starts occurrence.


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PHENOM 100

15

AFTER STARTING

Phase Callout/Challenge: Action/Response:ELEC EMERButton

Battery 1 & 2Voltage

ELEC EMERButton

External Lights

AFCS ControlUnit

PUSH IN

CHECKEACH BATTERY VOLTAGE MUSTBE AT LEAST 23.8 V.NOTE: - Wait at least 10 secondsbetween batteries voltagecheck.- If battery voltage does notreach 23.8 V, push theELEC EMER Button out,in order to recharge thebattery at least10 minutes, and thenperform the after startingcheck again.The parking brake must be appliedand the main brake must bereleased for battery voltage check.

PUSH OUT

AS REQUIRED

SET

Altimeters(pilots, IESI)

Transponder

TakeoffSpeeds

SET & X-CHECK

SETSet CODE and verify GND mode.

SETSet V1, VR, V2 and VFS on theINSET PFD as per the runwayanalysis.


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PHENOM 100

16

AFTER STARTING (Continued)

Phase Callout/Challenge: Action/Response:After Starting Takeoff Data

N1 Target

LFE

SETSelect the ENG TDS SET page onMFD and set the data below:OAT…SETATR…ON or OFF

CHECK

SET

Flight Controls CHECK FREE

Flaps

CHECK/SETVerify that Roll, Yaw and Pitch(NORM and BKP) trims areoperating properly both ways.Adjust Yaw and Roll trims to theneutral position and Pitch trim toTakeoff (green band) according tothe CG position.

SET FOR TAKEOFFSet Flaps 1 or 2 for takeoffaccording to runway analysis.

Ice Protection AS REQUIREDIf icing conditions exist or areforecast, refer to operation in icingconditions procedure.


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PHENOM 100

17

TAXI

Phase Callout/Challenge: Action/Response:Prior to Taxi

During Taxi

Insert Flight Plan.Ensure that all of the requiredinformation regarding taxi andtakeoff is known and confirmed.

Apply Emergency/Parking Brake onfull stops.

BEFORE TAKEOFF

Phase Callout/Challenge: Action/Response:Holding Short

Before Takeoff

Ensure that all of the requiredinformation regarding takeoff isknown and confirmed.

CHECKPress the T/O CONFIG button onthe center console and check if theaural “TAKEOFF OK” sounds.

CHECK

CHECKCheck if the GSPLR OPEN Light isnot illuminated on the maininstrument panel.

PED-BELTS/OFF

ADVISE

TakeoffConfiguration

CASMessages

GSPLR OPENLight (if applicable)

SIGNS/OUTLETSwitch

Passengers

AS REQUIREDLights


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PHENOM 100

18

TAKEOFF

Phase Callout/Challenge: Action/Response:Prior to Taxi OFF

TO/GADuring takeoff roll, after advancingthrust levers to TO/GA, check N1equal to N1 target and green ATRindication presented on MFD if ATRON is selected.

Continue TO or Abort.

Rotate the airplane according to thetable below:Flaps Position 1 2Pitch Angle 9.5° 9°

Flight Director

Thrust Levers

70 KIAS

Positive Rateof Climb

LDG GEAR Lever: Select UP.Verify three gear legs indicate upand locked.

AtAccelerationHeight(minimum 500 ft)

Autopilot: engage.Flight Level Change: press.Speed: 160 KIAS.Retract flaps on schedule.Thrust Levers: CON/CLB.

V1

VR


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PHENOM 100

19

TAKEOFF

Phase Callout/Challenge: Action/Response:After Takeoff

At TransitionAltitude

Climb

At 10000 ft

Check UP

ZERO

CON/CLB

SET & X-CHECK

ON

LDG GEARLever

CRUISE

Phase Callout/Challenge: Action/Response:CRUISE Thrust Levers: MAX CRZ.

Flaps

Thrust Levers

After passing safe altitude forairplane acceleration select FLCmode and speed 200 KIAS/M.55.

AS REQUIRED

Altimeters(pilots and IESI)

Yaw Damper

AS REQUIREDFlight Director

SIGNS/OUTLETSwitch

AS REQUIREDExternal Lights

AS REQUIRED

AS REQUIRED

WeatherRadar(if installed)

Airspeed


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PHENOM 100

20

DESCENT

Phase Callout/Challenge: Action/Response:Prior toDescent

1 MinuteBefore VerticalPath

Descent

Below 10000 ft

Insert Arrival and Approach intoFlight Plan.Perform Approach Briefing.

Select authorized descent altitudeand then select VNAV.

ON

SETSet VREF, VAP, VAC and VFS.

CHECK LFE

AS REQUIREDIf necessary, set the CKPT FANSwitch to HI position to avoid fogon the cockpit side windows.

CKPT FANSwitch

WSHLD 1 & 2Switches

Pressurization

LandingSpeeds

PED-BELTS/OFFSIGNS/OUTLETSwitch


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PHENOM 100

21

APPROACH

Phase Callout/Challenge: Action/Response:Approach

Prior to Startof Arrival

During Visualor InstrumentApproach

ADVISEPassengers

PUSHED OUT

SET & X-CHECK

FUEL XFRButton

Altimeters(pilots and IESI)

Ensure that all of the requiredinformation regarding approach andlanding is known and confirmed.

Use flap maneuvering speeds asfollows:

Airplanes Post-Mod.SB 500-27-0003 or with anequivalent modification factoryincorporated.

GEAR/FLAPS SPEEDUP/0 150 KIASUP/1 140 KIASDN/2 120 KIASDN/FULL 115 KIAS

GEAR/FLAPS SPEEDUP/0 150 KIASUP/1 140 KIASDN/2 120 KIASDN/3 120 KIASDN/FULL 115 KIAS


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PHENOM 100

22

BEFORE LANDING

Phase Callout/Challenge: Action/Response:BeforeLanding

OFFYaw Damper

LDG GEARLever

DN (check three green)

SET FOR LANDINGFlaps

VREFAirspeed


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PHENOM 100

LANDING

Phase Callout/Challenge: Action/Response:Landing IDLE

APPLY

Thrust Levers

Brakes

23

CONDITION CALL OUT/ACTION

The recommended Callouts and Actions for CAT I ILS are the following:

APR armedFlaps 1

Heading to intercept the localizer course.

“LOC ALIVE”At the first sign of movement ofthe Localizer deviation bar.

“GLIDE SLOPE”LDG GEAR Lever DNFlaps 2

When the glideslope is one dotabove.

“OUTER MARKER____FEET ALTITUDECROSS CHECKED”Landing FlapsBefore Landing Checklist

Passing Outer Marker underIMC, after checking that thealtitude over the OM is correct.

“LOC” or “GLIDE” or “SPEED” as appropriate

Any significant deviation from theLocalizer or GS (1/4 dot) or fromtarget speed (+10/-0 KIAS).

“ONE HUNDRED”100 ft above DA if under IMC.

“APPROACH LIGHTS” or“RUNWAY IN SIGHT” asappropriate

Perform Go-Around Procedure

Upon visual contact with theapproach lights or with therunway.

Reaching DA without visualcontact.


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PHENOM 100

24

GO-AROUND

Phase Callout/Challenge: Action/Response:Go-Around PRESSTO/GA Buttons

Thrust Levers TO/GAAirplanes Pre-Mod.SB 500-27-0003.

Rotate the airplane following theflight director guidance or accordingto the table below:

Landing Flaps Go-Around Position Pitch Angle 2 7.5° FULL 5.5°


Do not press the TO/GA buttonafter selecting go-around flaps.

Landing Flaps Go-Around Position Pitch Angle 2 1 FULL 2


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PHENOM 100

25

GO-AROUND (Continued)

Phase Callout/Challenge: Action/Response:Go-Around

With Positive Climb

At 1000 ft(accelerationaltitude) andV2 + 15 KIAS

Thrust Levers

LDG GEARLever

Airspeed VAC minimum.

UP

TO/GAAirplanes Post-Mod.SB 500-27-0003 or with anequivalent modification factoryincorporated.


Landing Flaps Go-Around Position Pitch Angle 3 7.5° FULL 5.5°

Select flaps according to the tablebelow:

Do not press the TO/GA buttonafter selecting go-around flaps.

Proceed as in a normal takeoff.Perform After Takeoff checklist.

Landing Flaps Go-Around Position Pitch Angle 3 1 FULL 2


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PHENOM 100

26

AFTER LANDING

Phase Callout/Challenge: Action/Response:After Landing

Taxi-In

Flaps

Lights AS REQUIRED

Apply Emergency/Parking Brake ifFull Stop is necessary during taxi.

ZERO

SHUTDOWN

Phase Callout/Challenge: Action/Response:Shutdown Thrust Levers

Emergency/Parking Brake

IDLEMaintain idle for at least 2 minutesprior to engine shutdown.

APPLY

GPU AS REQUIREDIf GPU is required, verify the GPUis connected before shutting downthe engine.

HEATINGPanel

ICEPROTECTIONPanel

CHECKCheck WSHLD 1 & 2 Switches inthe OFF position and ADS/AOAKnob in the AUTO position.

CHECKCheck ENG 1 & 2 Switches in theOFF position and WINGSTAB andINSP LIGHT Switches in the OFFposition.


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PHENOM 100

27

SHUTDOWN (Continued)

Phase Callout/Challenge: Action/Response:Shutdown ENG

START/STOPKnobs

SIGNS/OUTLETSwitch

STOPIf GPU is required, verify the GPUCONNECTED message isdisplayed before shutting down theengine.

OFF/ON

LEAVING THE AIRPLANE

Phase Callout/Challenge: Action/Response:Leaving theAirplane

OXYGENSUPPLYHandle

BATT 1 & 2Switches

PULL TO CUTOUT

OFF

External Lights AS REQUIRED

Gust Lock Pin

Rudder GustLock

INSTALL

LOCK


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PHENOM 100