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Phenom 300 Checklist

This document provides limitations and procedures for the Phenom 300 airplane. Key limitations include maximum speeds for different flap settings between 160-180 knots, a maximum altitude of 18,000 feet for flaps extended, and a maximum tire ground speed of 182 knots. Maneuvering is limited to no acrobatic maneuvers or spins, and positive load factors are limited to 3.0g for flaps up and 2.0g for flaps down. Normal procedures include a cockpit/cabin safety inspection, external inspection, and recommended walk-around sequence.

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1K views103 pages

Phenom 300 Checklist

This document provides limitations and procedures for the Phenom 300 airplane. Key limitations include maximum speeds for different flap settings between 160-180 knots, a maximum altitude of 18,000 feet for flaps extended, and a maximum tire ground speed of 182 knots. Maneuvering is limited to no acrobatic maneuvers or spins, and positive load factors are limited to 3.0g for flaps up and 2.0g for flaps down. Normal procedures include a cockpit/cabin safety inspection, external inspection, and recommended walk-around sequence.

Uploaded by

maverickoneshot
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
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TM

PHENOM 300
Airplane Flight Manual
Limitations

MAXIMUM FLAP EXTENDED SPEED (VFE)


Flap 1 ....................................................................... 180 KIAS
Flap 2 ....................................................................... 170 KIAS
Flap 3 ....................................................................... 170 KIAS
Flap FULL ................................................................ 160 KIAS

MAXIMUM ALTITUDE FOR FLAPS EXTENDED


Maximum Altitude for Flaps Extended..................... 18000 ft

MAXIMUM TIRE GROUND SPEED


Maximum Tire Ground Speed ................................. 182 kt

MANEUVERING
No acrobatic maneuvers, including spins, are authorized.

MANEUVERING FLIGHT LOAD FACTORS


These corresponding accelerations limit bank angle during turns and
limit pull-up maneuvers.

FLAP DOWN
LOAD FACTOR LIMIT FLAP 0
(1, 2, 3 AND FULL)
Positive 3.00 g 2.00 g

MINIMUM CREW
Minimum Flight Crew ............................................... 1 PILOT

NOTE: - The pilot must occupy the left cockpit seat.


- Operating rules may require an operative autopilot or a
second pilot in command.
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REVISION 12 code 01 Page 5
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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

COCKPIT/CABIN SAFETY INSPECTION


Emergency Door Locking Pin .................................. REMOVE
Emergency Door...................................................... SECURED AND
LOCKED
Documents, Manuals and Charts ............................ CHECK ON
BOARD
Maintenance Status ................................................. CHECK
Emergency Equipment ............................................ CHECK
Verify Fire Extinguisher, Flashlight, First Aid Kit, Water Barrier and
the following optional items, if installed: Protective Breathing
Equipment (PBE), Smoke Goggles, Over Water Life Vest and
Survival Kit.
Oxygen Bottle Valve Handle.................................... PUSH TO
RESTORE
SUPPLY CONTROL Knob ...................................... PAX AUTO
Oxygen Mask Regulator .......................................... CHECK 100%
ELECTRICAL Panel ................................................ CHECK
Check BATT 1 & 2 Switches in the OFF position. BUS TIE Knob
and GEN 1 & 2 Switches in the AUTO position and set GPU Button
as required and check.
BLEED 1 & 2 Switches ............................................ AUTO
XBLEED Knob ......................................................... AUTO
TEST Panel ............................................................. OFF
Circuit Breakers ....................................................... CHECK
If any circuit breaker is not IN, investigate the cause prior to
resetting.
FUEL PUMP 1 & 2 Switches ................................... AUTO
XFEED Knob ........................................................... OFF
HYD PUMP SOV 1 & 2 Switches ............................ OPEN
ELT Switch............................................................... ARMED

(Continues on the next page)


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REVISION 12 code 01 Page 1
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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

(Continued from the previous page)


PUSHER CUTOUT Button....................................... PUSHED OUT
Gust Lock Pin........................................................... REMOVE
Rudder Pedals ......................................................... CHECK
UNLOCKED
HEATING Panel....................................................... CHECK
Check WSHLD 1 & 2 Switches in the OFF position and ADS
PROBES Knob in the AUTO position.
ICE PROTECTION Panel ........................................ CHECK
Check ENG 1 & 2 Switches, WINGSTAB and INSP LIGHT
Switches in the OFF position.
LDG GEAR Lever .................................................... DN
PRESSURIZATION Panel ....................................... CHECK
Check Pressurization MODE Switch in the AUTO position, ECS
Knob in the BOTH position and DUMP Button pushed out.
AIR CONDITIONING Panel ..................................... AS REQUIRED
ENG FIRE EXTINGUISHER Panel.......................... CHECK
Check SHUTOFF 1 & 2 Buttons pushed out and BOTTLE Switch in
the OFF position.
Start/Stop Knobs...................................................... STOP
Flap Lever ................................................................ ZERO
SPEED BRAKE Switch ............................................ CLOSE
Parking Brake .......................................................... SET

NOTE: If parking brake pressure is suspected to be low, use wheel


chocks to secure the airplane.
Seats and Belts........................................................ CONDITION
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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

EXTERNAL INSPECTION
External Lights ......................................................... CHECK
Turn the lights OFF immediately after check them to avoid batteries
discharge.
Recommended Walk-Around sequence:

EM500ENAOM140228B.DGN

IASP......................................................................... CONDITION, NO
OBSTRUCTION
Oxygen Discharge Indicator .................................... GREEN DISK IN
PLACE
Ice Detector (if installed).......................................... CHECK
Antennas.................................................................. CONDITION
Red Beacon Light .................................................... CONDITION
NLG Doors, Wheel and Tire .................................... CONDITION

(Continues on the next page)


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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

(Continued from the previous page)


NLG Torque Link...................................................... CONNECTED
AND
SECURED
NLG Safety Pin ........................................................ REMOVED
Forward LH Baggage Compartment Door............... LATCHED
Radome.................................................................... CONDITION
Forward RH Baggage Compartment Door .............. LATCHED
IASP ......................................................................... CONDITION, NO
OBSTRUCTION
Stand-By Pitot Tube................................................. CONDITION, NO
OBSTRUCTION
Refueling Panel........................................................ CLOSED
LDG/Taxi Lights ....................................................... CONDITION
Fuselage Air Inlet ..................................................... NO
OBSTRUCTION
Engine Fan............................................................... CONDITION
Engine Air Inlet......................................................... NO
OBSTRUCTION
Starter/Generator Air Inlets ...................................... CLEAR
* Fuel Drains ............................................................ DRAIN AND
CHECK FOR
CONTAMINATION

CAUTION: USING AN INADEQUATE TOOL TO ACCOMPLISH THE


FUEL DRAINAGE MAY CAUSE DAMAGE TO THE
DRAIN VALVE.
Fuel Drains and Dump Valves ................................. NO LEAKS
Right Wing Leading Edge ........................................ CONDITION
MLG Doors, Wheels, Brakes and Tires ................... CONDITION
MLG Safety Pin ........................................................ REMOVED

(Continues on the next page)


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Page 4 code 01 REVISION 10
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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

(Continued from the previous page)


Fuel Cap .................................................................. CLOSED AND
LOCKED
Fuel Tank Air Inlet.................................................... NO
OBSTRUCTION
Navigation/Strobe Lights ......................................... CONDITION
Right Winglet ........................................................... CONDITION
Right Winglet Static Dischargers ............................. NUMBER (2) AND
CONDITION
Right Aileron ............................................................ CHECK FREE
Right Aileron Static Dischargers.............................. NUMBER AND
CONDITION
NOTE: Verify 2 or 3 static dischargers on each aileron, according
to airplane configuration.
Right Spoilers .......................................................... CONDITION
Right Flap ................................................................ CONDITION
Battery Access Door................................................ LATCHED
Cowlings .................................................................. LATCHED
Engine Exhausts...................................................... CLEAR
Drain Masts.............................................................. CONDITION
Engine Oil Level....................................................... CHECK
Heat Exchanger Air Exhaust ................................... CLEAR
Pylon (air exhaust)................................................... CONDITION
Vertical Stabilizer ..................................................... CONDITION
Rudder ..................................................................... CONDITION
Rudder Static Dischargers....................................... NUMBER (2) AND
CONDITION
Yaw Trim Tab .......................................................... CONDITION
Horizontal Stabilizer................................................. CONDITION

(Continues on the next page)


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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

(Continued from the previous page)


Elevator ....................................................................CONDITION
Pitch Trim Tab.......................................................... CONDITION
Elevators Static Dischargers.................................... NUMBER (4) AND
CONDITION
Antennas .................................................................. CONDITION
Ventral Rudder......................................................... CONDITION
Air Exhausts ............................................................. NO
OBSTRUCTION
Engine Exhaust........................................................ CLEAR
Aft Baggage Compartment Door ............................. LATCHED
Pylon (air exhaust) ................................................... CONDITION
Cowlings................................................................... LATCHED
Drain Masts .............................................................. CONDITION
Engine Oil Level....................................................... CHECK
DC Power Receptacle.............................................. CHECK
Hydraulic Reservoir Access Door ............................ LATCHED
Left Flap ................................................................... CONDITION
Left Spoilers ............................................................. CONDITION
Left Aileron ............................................................... CHECK FREE
Left Aileron Static Dischargers ................................ NUMBER AND
CONDITION
NOTE: Verify 2 or 3 static dischargers on each aileron, according
to airplane configuration.
Roll Trim Tab ........................................................... CONDITION
Navigation/Strobe Lights.......................................... CONDITION
Left Winglet .............................................................. CONDITION
Left Winglet Static Dischargers................................ NUMBER (2) AND
CONDITION

(Continues on the next page)


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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

(Continued from the previous page)


Fuel Tank Air Inlet.................................................... NO
OBSTRUCTION
Left Wing Leading Edge .......................................... CONDITION
Fuel Cap .................................................................. CLOSED AND
LOCKED
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

POWER UP
BATT 1 & 2 Switches............................................... ON

NOTE: - For airplanes Pre-Mod. SB 505-24-0015: If the battery has


been cold soaked for 2 hours or longer at ambient
temperature of -10°C (14°F) or lower, it must be pre-heated
to above -10°C (14°F) prior to engine start.
- For airplanes Post-Mod. SB 505-24-0015 or with an
equivalent modification factory incorporated: If the battery
has been cold soaked for 2 hours or longer at ambient
temperature of -18°C (-0.4°F) or lower, it must be pre-
heated to above -18°C (-0.4°F) prior to engine start.
GPU Button (if applicable) ....................................... AS REQUIRED
Verify AVAIL light illuminated before pushing the GPU Button in.
When GPU is not available or is not necessary, maintain GPU
Button pushed out.
(Continues on the next page)
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REVISION 12 code 01 Page 7
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

(Continued from the previous page)


CVDR Panel............................................................. CHECK
Set the toggle Switch to TEST HOLD 5 SEC position and hold for
5 seconds. Verify no fail indication on CVDR panel annunciators.
Transponder/TCAS II (if applicable) ........................ CHECK
Verify transponder mode as required by local rules.
If airplane is equipped with TCAS II, set TCAS II in STBY mode.

BEFORE START
Oxygen Mask Flow and Microphone ....................... CHECK
Set MASK MIC Switch to the ON position and press TEST/RESET
Button. Set MASK MIC Switch to the OFF position.
TEST Panel.............................................................. TEST
Test Fire Protection, Smoke Detector and Annunciator.
SIGNS/OUTLET Switch ........................................... BELTS/ON
External Lights ......................................................... AS REQUIRED
EMER LT Switch...................................................... ARM
Fuel Quantity and Balance....................................... CHECK
Oxygen Pressure ..................................................... CHECK MINIMUM
FOR DISPATCH
ENG IGNITION Switches......................................... AUTO
Thrust Levers ........................................................... IDLE
Parking Brake .......................................................... SET
Doors........................................................................ CLOSED

ENGINE START
Associated Start/Stop Knob ..................................... START, THEN
RUN
Engine Parameters .................................................. MONITOR
Check N2, ITT, N1 and oil pressure within operational limits.
Repeat the sequence for the other engine.
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Page 8 code 01 REVISION 12
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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

AFTER START
GPU (if applicable) .................................................. DISCONNECT
ELEC EMER Button................................................. PUSH IN
Battery 1 & 2 Voltage............................................... CHECK

CAUTION: EACH BATTERY VOLTAGE MUST BE AT LEAST


23.5 VOLTS.
ELEC EMER Button................................................. PUSH OUT
Stall Protection System (TEST panel) ..................... TEST
AFCS Control Unit ................................................... SET
Engine Takeoff Data ................................................ SET
OAT .................................................................... SET
ATR..................................................................... ON OR OFF
Landing Field Elevation ........................................... SET
Takeoff Speeds (V1, VR, V2, VFS) ............................. SET
Transponder/TCAS II (if applicable) ........................ SET
Set CODE and verify transponder mode as required by local rules.
If airplane is equipped with TCAS II, set TCAS II in STBY mode.
Altimeters (pilots and IESI) ...................................... SET & X-CHECK
Flight Controls.......................................................... CHECK FREE
Trims ........................................................................ CHECK/SET
Verify that Roll, Yaw and Pitch (NORM and BKP) trims are
operating properly in both directions. Adjust Yaw and Roll trims to
the neutral position and Pitch trim to Takeoff (green band).
Flap .......................................................................... SET FOR
TAKEOFF
External Lights ......................................................... AS REQUIRED

(Continues on the next page)


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REVISION 12 code 01 Page 9
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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

(Continued from the previous page)


Ice Protection ........................................................... AS REQUIRED

WARNING: IF ICING CONDITIONS EXIST OR ARE FORECAST,


REFER TO OPERATION IN ICING CONDITIONS
PROCEDURE.

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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

BEFORE TAKEOFF
Takeoff Configuration .............................................. CHECK
Press the T/O CONFIG Button on the central console and check if
the aural TAKEOFF OK sounds.
CAS Messages ........................................................ CHECK
SIGNS/OUTLET Switch........................................... PED-BELTS/OFF
Yaw Damper ............................................................ OFF
--------------------------SHORTLY BEFORE TAKEOFF-------------------------
Passengers.............................................................. ADVISE
Lights ....................................................................... AS REQUIRED

TAKEOFF
Thrust Levers........................................................... TO/GA

NOTE: After checking thrust levers in TO/GA, check N1 equal to N1


target and green ATR indication presented on MFD if ATR ON
is selected.
Engine Parameters .................................................. MONITOR
At VR rotate the airplane according to the table below.

FLAP POSITION 1 2
PITCH ANGLE 10.5° 8°

With positive rate of climb:


LDG GEAR Lever ............................................... UP
Airspeed ............................................................. V2 + 10 KIAS
MINIMUM
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PHENOM 300
Airplane Flight Manual
Normal Procedures

AFTER TAKEOFF/CLIMB
LDG GEAR Lever .................................................... CHECK UP
Flap .......................................................................... ZERO
Retract flap in a speed at or below to the Maximum Flap Extended
Speed (VFE) for each position.
Thrust Levers ........................................................... CON/CLB
Altimeters (pilots and IESI) ...................................... SET & X-CHECK
Yaw Damper ............................................................ ON
Icing Conditions ....................................................... VERIFY
------------------------------------ABOVE 10000 ft-----------------------------------
SIGNS/OUTLET Switch ........................................... AS REQUIRED
External Lights ......................................................... AS REQUIRED
Weather Radar (if installed) ..................................... AS REQUIRED
Airspeed ................................................................... AS REQUIRED

DESCENT
Windshield Heating .................................................. ON
Pressurization .......................................................... CHECK LFE
Landing Speeds ....................................................... SET
Set VREF, VAC and VFS.
Icing Conditions ....................................................... VERIFY
------------------------------------BELOW 10000 ft-----------------------------------
SIGNS/OUTLET Switch ........................................... PED-BELTS/OFF
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Page 2 code 01 ORIGINAL
TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

APPROACH
External Lights ......................................................... AS REQUIRED
Passengers.............................................................. ADVISE
XFEED Knob ........................................................... OFF
Altimeters (pilots and IESI) ...................................... SET & X-CHECK
Icing Conditions ....................................................... VERIFY

BEFORE LANDING
Yaw Damper ............................................................ OFF
LDG GEAR Lever .................................................... DN AND
CHECK
Flap .......................................................................... SET FOR
LANDING
Airspeed................................................................... VREF

LANDING
Thrust Levers........................................................... IDLE
Brakes (after touchdown) ........................................ APPLY MAXIMUM
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REVISION 12 code 01 Page 1
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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

GO-AROUND
TO/GA Button........................................................... PRESS
Thrust Levers ........................................................... TO/GA
Rotate the airplane following the flight director guidance or according
to the table below.

LANDING FLAP GO-AROUND PITCH


POSITION ANGLE
3 8°
FULL 6°

Select flaps according to the table below.

LANDING FLAP GO-AROUND FLAP


POSITION POSITION
3 1
FULL 2

With positive rate of climb:


LDG GEAR Lever ............................................... UP
Minimum Airspeed .............................................. VAC
At the acceleration altitude proceed as in a normal takeoff.

AFTER LANDING
Flap .......................................................................... ZERO
Lights........................................................................ AS REQUIRED
Transponder............................................................. AS REQUIRED
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Page 2 code 01 REVISION 12
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TM

PHENOM 300
Airplane Flight Manual
Normal Procedures

SHUTDOWN
Thrust Levers........................................................... IDLE
Emergency/Parking Brake....................................... APPLY

CAUTION: MAINTAIN IDLE FOR ǹȉ LEAST 2 MINUTES PRIOR TO


ENGINE SHUTDOWN.
HEATING Panel....................................................... CHECK
Check WSHLD 1 & 2 Switches in the OFF position and ADS
PROBES Knob in the AUTO position.
ICE PROTECTION Panel........................................ CHECK
Check ENG 1 & 2, WINGSTAB and INSP LIGHT Switches in the
OFF position.
Start/Stop Knobs...................................................... STOP
MFD Status Pages................................................... CHECK
Check MFD status page for engine message.
SIGNS/OUTLET Switch........................................... OFF/ON

LEAVING THE AIRPLANE


Oxygen Bottle Valve Handle.................................... PULL TO CUTOUT
EMER LT Switch...................................................... OFF
BATT 1 & 2 Switches............................................... OFF
Gust Lock Pin .......................................................... INSTALL
Rudder Pedals ......................................................... LOCK
Lights ....................................................................... OFF
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REVISION 12 code 01 Page 3
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

N1 FOR T/O MODE


ANTI-ICE OFF
AIRSPEED: 0 KIAS
PW535E ENGINES

Pressure
Altitude
Static Air Temperature (°C)
(ft) -40 -35 -30 -25 -20 -15 -10 -5 0
-1000 77.0 77.9 78.7 79.5 80.3 81.1 81.9 82.6 83.4
0 78.1 79.0 79.8 80.6 81.4 82.2 83.0 83.8 84.5
1000 79.2 80.1 80.9 81.8 82.6 83.4 84.2 85.0 85.7
2000 80.4 81.2 82.1 82.9 83.7 84.5 85.4 86.1 86.9
3000 81.5 82.3 83.2 84.0 84.9 85.7 86.5 87.3 88.1
4000 82.5 83.4 84.3 85.2 86.0 86.9 87.7 88.5 89.3
5000 83.7 84.6 85.5 86.3 87.2 88.0 88.9 89.7 90.5
6000 84.5 85.4 86.3 87.2 88.1 88.9 89.8 90.6 91.5
7000 84.7 85.7 86.6 87.5 88.4 89.3 90.1 91.0 91.6
8000 85.0 85.9 86.9 87.8 88.7 89.6 90.4 91.3 91.0
9000 85.5 86.4 87.3 88.2 89.1 90.0 90.8 91.5 90.9
10000 85.8 86.7 87.6 88.5 89.4 90.3 91.2 91.6 91.1
11000 86.3 87.2 88.1 89.0 89.9 90.8 91.7 91.5 90.9
12000 86.7 87.6 88.6 89.5 90.4 91.3 91.9 91.4 90.7
13000 87.4 88.3 89.2 90.1 91.0 91.9 91.8 91.2 90.5
14000 87.8 88.8 89.8 90.8 91.7 92.4 91.7 91.0 90.3

Pressure
Altitude
Static Air Temperature (°C)
(ft) 5 10 15 20 25 30 35 40 45
-1000 84.1 84.9 85.6 86.3 87.1 87.8 88.4 87.0 85.6
0 85.3 86.0 86.8 87.5 88.3 89.0 88.2 86.8 85.4
1000 86.5 87.3 88.0 88.8 89.5 89.3 87.9 86.4 85.0
2000 87.7 88.5 89.2 90.0 90.0 89.0 87.5 86.1 84.6
3000 88.9 89.7 90.4 90.6 89.8 88.6 87.2 85.7 -
4000 90.1 90.9 91.1 90.4 89.6 88.3 86.8 85.3 -
5000 91.3 91.6 91.0 90.4 89.5 88.1 86.6 85.1 -
6000 91.8 91.2 90.6 90.0 89.2 87.6 86.1 - -
7000 91.2 90.7 90.1 89.5 88.4 86.9 85.4 - -
8000 90.5 90.2 89.8 89.0 87.6 86.0 - - -
9000 90.5 90.1 89.8 88.9 87.2 85.6 - - -
10000 90.7 90.3 89.8 88.8 87.2 85.6 - - -
11000 90.4 89.9 89.1 88.0 86.3 - - - -
12000 90.1 89.5 88.5 87.1 85.5 - - - -
13000 89.8 89.1 87.9 86.5 - - - - -
14000 89.6 88.7 87.5 85.9 - - - - -
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ORIGINAL code 01 Page 3
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PHENOM 300
Airplane Flight Manual
Performance

N1 FOR T/O MODE


ANTI-ICE ON
AIRSPEED: 0 KIAS
PW535E ENGINES

Pressure
Altitude
Static Air Temperature (°C)
(ft) -35 -30 -25 -20 -15
-1000 78.0 78.8 79.6 80.4 81.2
0 79.1 79.9 80.7 81.5 82.3
1000 80.2 81.0 81.8 82.7 83.5
2000 81.3 82.2 83.0 83.8 84.6
3000 82.4 83.3 84.1 84.9 85.8
4000 83.6 84.4 85.3 86.1 86.9
5000 84.7 85.6 86.4 87.3 88.1
6000 85.5 86.4 87.3 88.2 89.0
7000 85.8 86.7 87.6 88.5 89.4
8000 86.2 87.0 87.9 88.8 89.4
9000 86.5 87.4 88.3 89.2 89.1
10000 86.8 87.7 88.6 89.5 89.2

Pressure
Altitude
Static Air Temperature (°C)
(ft) -10 -5 0 5
-1000 82.0 82.7 83.5 84.2
0 83.1 83.8 84.6 85.4
1000 84.3 85.0 85.8 86.6
2000 85.4 86.2 87.0 87.8
3000 86.6 87.4 88.2 89.0
4000 87.8 88.6 89.4 88.9
5000 89.0 89.8 89.4 88.4
6000 89.7 89.7 88.8 87.9
7000 89.5 88.7 87.9 86.9
8000 88.6 87.7 86.8 85.5
9000 88.3 87.4 86.4 85.1
10000 88.3 87.4 86.3 84.9
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Page 4 code 01 ORIGINAL
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: -1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 648 665 710 755 809 899 983 8340


104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-35 657 674 720 766 820 911 997 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-30 667 684 730 776 831 923 1010 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-25 677 693 740 787 843 936 1024 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-20 687 703 750 798 854 949 1039 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-15 696 713 760 808 866 962 1053 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-10 706 723 770 819 878 975 1067 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-5 715 733 780 830 890 988 1081 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
0 725 743 789 840 901 1001 1096 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
5 734 752 800 851 914 1015 1111 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
10 743 762 810 862 927 1030 1128 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
15 752 771 820 873 941 1046 1144 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
20 761 780 831 884 954 1062 1162 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
25 770 790 842 896 968 1078 1179 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
30 777 806 863 918 1003 1124 1227 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 108/108/118 110/110/120
35 778 837 895 998 1123 1249 1358 8340
99/99/111 99/99/110 99/99/109 102/102/112 105/105/115 108/108/118 111/111/120
40 810 868 985 1115 1246 1382 1517 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
45 839 960 1098 1234 1382 1547 1690 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
50 930 1073 1218 1378 1550 1724 1892 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
52 975 1121 1272 1445 1620 1810 1982 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 3
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 0 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 666 682 726 773 826 915 1002 8340


105/105/118 104/104/117 104/104/116 104/104/115 104/104/115 107/107/118 110/110/120
-35 677 693 736 784 837 927 1015 8340
105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-30 687 703 747 795 849 940 1030 8340
105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-25 696 713 757 806 861 953 1044 8340
105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-20 706 724 767 817 873 967 1059 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-15 716 734 777 828 885 981 1074 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-10 726 744 788 839 898 995 1089 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-5 736 754 798 850 910 1008 1104 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
0 745 764 808 861 922 1022 1119 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
5 755 774 819 872 936 1038 1136 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
10 764 784 830 884 950 1054 1153 8340
104/104/117 104/104/116 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
15 773 793 841 895 964 1070 1171 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
20 782 803 852 907 978 1087 1189 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
25 792 813 872 927 1004 1121 1225 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
30 786 840 898 977 1097 1224 1333 8340
101/101/113 100/100/112 100/100/111 102/102/112 105/105/115 108/108/118 111/111/120
35 812 872 963 1092 1223 1357 1483 8340
97/97/109 97/97/108 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
40 843 939 1078 1214 1353 1517 1659 8340
94/94/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 112/112/120
45 909 1051 1197 1345 1517 1691 1848 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 111/111/118 113/113/120
50 1021 1171 1334 1514 1695 1898 2076 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 4 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 684 700 744 792 847 938 1027 8340


105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-35 694 711 755 804 859 952 1041 8340
105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-30 705 722 765 815 871 965 1056 8340
105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-25 715 732 776 826 884 979 1071 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-20 725 743 787 838 896 993 1087 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-15 735 753 797 849 909 1007 1102 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-10 745 764 808 861 922 1021 1118 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-5 755 775 819 872 934 1035 1133 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
0 765 785 829 883 947 1050 1149 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
5 775 795 840 895 961 1066 1166 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
10 784 805 851 907 975 1082 1184 8340
104/104/117 104/104/116 103/103/115 103/103/115 104/104/115 107/107/118 110/110/120
15 794 815 863 919 990 1099 1202 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
20 803 825 880 936 1012 1128 1233 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
25 801 848 908 979 1096 1224 1333 8340
101/101/114 101/101/113 101/101/112 101/101/112 105/105/115 108/108/118 111/111/120
30 816 877 952 1074 1206 1339 1455 8340
98/98/110 98/98/109 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
35 848 930 1062 1200 1339 1494 1637 8340
95/95/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
40 900 1035 1182 1326 1494 1668 1819 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
45 1003 1154 1308 1488 1669 1863 2042 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
48 1074 1230 1408 1594 1787 2001 2186 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 5
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 2000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 701 719 764 813 872 967 1058 8340


104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-35 712 729 775 825 885 981 1073 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-30 722 740 786 837 897 995 1088 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-25 733 751 797 849 910 1009 1104 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-20 743 762 808 860 923 1024 1120 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
-15 754 773 819 872 936 1038 1136 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
-10 764 784 830 884 949 1053 1152 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
-5 774 794 841 895 963 1068 1169 8340
104/104/117 104/104/116 103/103/115 103/103/115 104/104/115 107/107/118 110/110/120
0 784 805 852 907 977 1084 1186 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
5 794 815 863 919 991 1100 1203 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
10 804 825 875 931 1005 1117 1221 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
15 814 835 887 945 1022 1137 1243 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
20 814 858 918 986 1102 1232 1342 8340
101/101/114 101/101/113 101/101/112 101/101/112 105/105/115 108/108/118 111/111/120
25 823 885 952 1069 1202 1337 1453 8340
99/99/111 98/98/110 99/99/109 102/102/112 105/105/115 109/109/118 111/111/120
30 853 919 1044 1182 1321 1466 1610 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
35 892 1021 1168 1313 1472 1648 1799 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
40 988 1139 1294 1465 1647 1832 2012 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
45 1106 1265 1451 1641 1842 2062 2251 8340
95/95/103 98/98/106 102/102/109 105/105/112 108/108/115 112/112/118 114/114/120
46 1131 1292 1486 1678 1888 2110 2302 8340
95/95/103 98/98/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 6 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 3000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 714 734 787 837 911 1015 1109 8340


103/103/117 103/103/116 103/103/115 102/102/114 104/104/115 107/107/118 110/110/120
-35 725 744 798 849 924 1030 1125 8340
103/103/117 103/103/116 103/103/115 102/102/114 104/104/115 107/107/118 110/110/120
-30 736 755 809 861 937 1045 1141 8340
103/103/117 103/103/115 103/103/114 102/102/114 104/104/115 107/107/118 110/110/120
-25 746 766 821 873 951 1060 1158 8340
103/103/116 103/103/115 103/103/114 102/102/114 104/104/115 107/107/118 110/110/120
-20 757 777 832 885 965 1075 1175 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 107/107/118 110/110/120
-15 768 788 843 898 979 1091 1192 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 107/107/118 110/110/120
-10 778 799 855 910 993 1107 1209 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 107/107/118 110/110/120
-5 789 809 866 922 1007 1122 1226 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 107/107/118 110/110/120
0 799 820 878 934 1021 1138 1244 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 107/107/118 110/110/120
5 809 831 889 947 1036 1156 1263 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 107/107/118 110/110/120
10 819 842 901 959 1051 1173 1282 8340
103/103/116 102/102/115 102/102/114 102/102/113 104/104/115 108/108/118 110/110/120
15 827 867 929 995 1110 1241 1353 8340
102/102/114 101/101/113 101/101/112 101/101/112 105/105/115 108/108/118 111/111/120
20 832 895 958 1074 1208 1344 1462 8340
99/99/111 99/99/110 99/99/109 102/102/112 105/105/115 109/109/118 111/111/120
25 860 923 1037 1176 1316 1458 1597 8340
96/96/108 96/96/107 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
30 890 1004 1152 1297 1446 1623 1775 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
35 973 1125 1280 1442 1626 1812 1982 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
40 1091 1251 1427 1618 1812 2031 2221 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
44 1190 1365 1568 1767 1994 2225 - 8279
95/95/103 99/99/106 102/102/109 106/106/112 109/109/115 112/112/118 -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 7
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 4000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 727 757 812 863 956 1070 1168 8340


102/102/115 102/102/114 102/102/113 101/101/112 104/104/115 108/108/118 110/110/120
-35 738 768 824 876 970 1086 1185 8340
102/102/115 102/102/114 102/102/113 101/101/112 104/104/115 108/108/118 110/110/120
-30 749 779 835 888 984 1102 1202 8340
102/102/115 102/102/114 102/102/113 101/101/112 104/104/115 108/108/118 110/110/120
-25 760 790 847 900 999 1118 1220 8340
102/102/115 102/102/114 101/101/113 101/101/112 104/104/115 108/108/118 110/110/120
-20 771 801 859 913 1013 1134 1238 8340
102/102/115 102/102/114 101/101/113 101/101/112 104/104/115 108/108/118 110/110/120
-15 782 812 870 926 1028 1151 1255 8340
102/102/115 102/102/114 101/101/113 101/101/112 104/104/115 108/108/118 110/110/120
-10 793 823 882 939 1043 1167 1274 8340
102/102/115 102/102/114 101/101/113 101/101/112 104/104/115 108/108/118 110/110/120
-5 803 834 894 952 1057 1184 1292 8340
102/102/115 102/102/114 101/101/113 101/101/112 104/104/115 108/108/118 110/110/120
0 814 845 906 965 1073 1201 1310 8340
102/102/115 102/102/114 101/101/113 101/101/112 105/105/115 108/108/118 110/110/120
5 824 856 918 980 1090 1220 1331 8340
102/102/115 101/101/114 101/101/113 101/101/112 105/105/115 108/108/118 110/110/120
10 837 875 938 1004 1119 1251 1365 8340
102/102/114 101/101/113 101/101/112 101/101/112 105/105/115 108/108/118 111/111/120
15 841 906 968 1082 1218 1355 1474 8340
99/99/111 99/99/110 99/99/109 102/102/112 105/105/115 109/109/118 111/111/120
20 869 934 1039 1179 1320 1464 1600 8340
97/97/108 96/96/107 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
25 897 993 1136 1282 1430 1599 1751 8340
94/94/105 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 112/112/120
30 961 1108 1264 1418 1600 1787 1949 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
35 1076 1237 1404 1596 1790 2001 2192 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
40 1200 1375 1581 1783 2010 2244 2446 8340
95/95/103 99/99/106 102/102/109 106/106/112 109/109/115 112/112/118 114/114/120
42 1253 1445 1655 1871 2107 2347 - 8140
95/95/103 99/99/106 102/102/109 106/106/112 109/109/115 112/112/118 -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 8 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 5000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 741 785 840 910 1017 1135 1236 8340


101/101/114 101/101/113 100/100/112 101/101/112 105/105/115 108/108/118 111/111/120
-35 753 796 852 923 1032 1152 1255 8340
101/101/114 101/101/113 100/100/112 101/101/112 105/105/115 108/108/118 111/111/120
-30 764 807 865 936 1046 1168 1273 8340
101/101/114 101/101/113 100/100/112 101/101/112 105/105/115 108/108/118 111/111/120
-25 775 818 877 950 1062 1186 1291 8340
101/101/114 101/101/113 100/100/112 101/101/112 105/105/115 108/108/118 111/111/120
-20 786 830 889 964 1077 1203 1310 8340
101/101/113 100/100/112 100/100/111 101/101/112 105/105/115 108/108/118 111/111/120
-15 797 841 901 978 1093 1220 1330 8340
101/101/113 100/100/112 100/100/111 101/101/112 105/105/115 108/108/118 111/111/120
-10 808 852 913 991 1108 1238 1349 8340
101/101/113 100/100/112 100/100/111 101/101/112 105/105/115 108/108/118 111/111/120
-5 819 864 925 1006 1125 1256 1368 8340
101/101/113 100/100/112 100/100/111 101/101/112 105/105/115 108/108/118 111/111/120
0 830 875 938 1020 1140 1274 1388 8340
101/101/113 100/100/112 100/100/111 101/101/112 105/105/115 108/108/118 111/111/120
5 841 887 950 1035 1158 1293 1409 8340
101/101/113 100/100/112 100/100/111 101/101/112 105/105/115 108/108/118 111/111/120
10 852 917 981 1089 1226 1366 1486 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
15 879 945 1046 1185 1329 1474 1609 8340
97/97/108 97/97/107 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
20 907 997 1137 1284 1434 1598 1751 8340
95/95/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
25 948 1086 1242 1397 1567 1754 1915 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
30 1051 1212 1377 1560 1755 1954 2145 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
35 1179 1348 1548 1750 1966 2200 2402 8340
95/95/103 98/98/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120
40 1310 1516 1733 1965 2209 - - 7983
95/95/103 99/99/106 103/103/109 106/106/112 109/109/115 - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 9
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 6000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 757 813 870 961 1081 1204 1310 8340


100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-35 768 825 882 975 1097 1222 1329 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-30 780 836 895 989 1112 1239 1348 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-25 791 848 908 1004 1129 1258 1368 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-20 802 860 920 1019 1146 1276 1389 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-15 814 872 933 1033 1162 1295 1409 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-10 825 884 946 1048 1179 1314 1429 8340
99/99/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-5 837 895 958 1063 1196 1332 1450 8340
99/99/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
0 847 907 971 1078 1213 1352 1471 8340
99/99/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
5 865 931 995 1115 1255 1397 1519 8340
99/99/111 99/99/110 99/99/109 102/102/112 105/105/115 109/109/118 111/111/120
10 893 960 1068 1211 1357 1505 1645 8340
97/97/108 96/96/107 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
15 920 1016 1160 1310 1463 1632 1788 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
20 960 1101 1259 1416 1589 1778 1942 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
25 1042 1205 1371 1549 1745 1944 2132 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
30 1169 1340 1533 1737 1946 2182 2385 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
35 1301 1500 1719 1944 2189 2439 - 8177
95/95/103 99/99/106 102/102/109 106/106/112 109/109/115 112/112/118 -
38 1389 1610 1839 2089 2344 - - 7828
96/96/103 99/99/106 103/103/109 106/106/112 109/109/115 - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 10 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 7000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 787 846 926 1044 1172 1301 1412 8340


98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-35 798 859 940 1059 1189 1321 1434 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-30 809 871 953 1074 1206 1340 1455 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-25 821 883 967 1090 1224 1360 1476 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-20 832 895 981 1106 1242 1380 1498 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-15 844 908 995 1122 1260 1400 1520 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-10 855 920 1009 1138 1278 1420 1542 8340
97/97/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-5 866 932 1024 1155 1297 1441 1565 8340
97/97/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
0 879 945 1039 1172 1317 1463 1589 8340
97/97/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
5 911 978 1106 1253 1402 1554 1704 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
10 937 1046 1197 1350 1506 1684 1844 8340
94/94/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 112/112/120
15 985 1131 1292 1452 1631 1824 1991 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
20 1059 1224 1393 1573 1772 1974 2163 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
25 1171 1344 1535 1741 1950 2186 2392 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
30 1304 1501 1721 1944 2192 2445 2664 8340
95/95/103 99/99/106 102/102/109 106/106/112 109/109/115 112/112/118 115/115/120
35 1461 1689 1933 2192 2456 - - 7783
96/96/103 100/100/106 103/103/109 106/106/112 110/110/115 - -
36 1498 1728 1982 2245 2512 - - 7673
96/96/103 100/100/106 103/103/109 107/107/112 110/110/115 - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 11
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 8000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 820 883 1000 1133 1268 1405 1540 8340


96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-35 832 896 1014 1150 1287 1425 1563 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-30 843 909 1028 1166 1305 1446 1585 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-25 855 922 1044 1183 1325 1468 1609 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-20 867 935 1059 1201 1344 1489 1633 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-15 879 949 1074 1218 1363 1511 1657 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-10 891 962 1089 1235 1383 1533 1681 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-5 903 976 1105 1253 1403 1555 1705 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
0 930 1013 1152 1303 1456 1617 1775 8340
95/95/106 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
5 957 1084 1243 1401 1561 1752 1915 8340
93/93/103 96/96/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
10 1013 1166 1332 1497 1688 1886 2057 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
15 1079 1246 1417 1598 1800 2004 2194 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
20 1181 1355 1542 1750 1961 2194 2401 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
25 1315 1510 1733 1955 2205 2461 2684 8340
95/95/103 99/99/106 102/102/109 106/106/112 109/109/115 112/112/118 115/115/120
30 1481 1713 1960 2224 2491 - - 7843
96/96/103 100/100/106 103/103/109 106/106/112 110/110/115 - -
34 1632 1882 2162 2439 - - - 7411
96/96/103 100/100/106 104/104/109 107/107/112 - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 12 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 9000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 850 935 1065 1204 1345 1495 1639 8340


95/95/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-35 862 949 1081 1222 1364 1517 1664 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-30 874 963 1097 1240 1385 1540 1688 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-25 887 977 1113 1258 1405 1563 1713 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-20 899 991 1129 1276 1426 1586 1739 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-15 911 1005 1145 1295 1447 1610 1765 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-10 924 1020 1162 1314 1468 1634 1791 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-5 937 1035 1180 1334 1490 1659 1819 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
0 970 1097 1259 1419 1581 1773 1939 8340
93/93/103 96/96/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
5 1032 1188 1355 1522 1714 1914 2088 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
10 1099 1269 1442 1627 1831 2039 2232 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
15 1181 1357 1540 1750 1962 2192 2401 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
20 1293 1478 1701 1921 2162 2418 2640 8340
95/95/103 99/99/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120
25 1447 1679 1917 2179 2446 2720 - 8054
96/96/103 99/99/106 103/103/109 106/106/112 109/109/115 113/113/118 -
30 1640 1888 2171 2452 - - - 7500
96/96/103 100/100/106 104/104/109 107/107/112 - - -
32 1718 1986 2277 2565 - - - 7284
97/97/103 100/100/106 104/104/109 107/107/112 - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 13
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 10000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 881 991 1135 1280 1427 1596 1746 8340


93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-35 894 1006 1152 1299 1448 1620 1772 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 112/112/120
-30 906 1020 1169 1318 1470 1644 1799 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 112/112/120
-25 919 1035 1186 1338 1492 1669 1826 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 112/112/120
-20 932 1051 1204 1358 1514 1694 1853 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-15 945 1066 1221 1378 1536 1719 1881 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-10 958 1081 1239 1398 1559 1744 1909 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-5 974 1100 1261 1422 1586 1775 1943 8340
93/93/103 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
0 1035 1189 1358 1526 1715 1917 2093 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
5 1107 1279 1455 1642 1849 2061 2255 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
10 1190 1369 1553 1767 1983 2214 2426 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
15 1290 1477 1694 1917 2153 2410 2633 8340
95/95/103 98/98/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120
20 1413 1632 1869 2117 2383 2655 - 8215
95/95/103 99/99/106 103/103/109 106/106/112 109/109/115 112/112/118 -
25 1585 1830 2099 2377 2662 - - 7679
96/96/103 100/100/106 103/103/109 107/107/112 110/110/115 - -
30 1791 2073 2373 - - - - 7136
97/97/103 100/100/106 104/104/109 - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 14 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 11000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 925 1056 1209 1361 1521 1703 1860 8340


93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
-35 938 1071 1227 1381 1543 1729 1888 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
-30 952 1087 1245 1401 1566 1754 1916 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
-25 966 1103 1264 1422 1589 1781 1945 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
-20 980 1119 1282 1443 1613 1807 1974 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
-15 994 1135 1301 1464 1637 1834 2003 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
-10 1008 1152 1320 1486 1661 1861 2033 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
-5 1051 1206 1378 1548 1739 1945 2123 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
0 1131 1306 1485 1676 1888 2103 2303 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
5 1225 1407 1600 1817 2038 2278 2494 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
10 1321 1511 1735 1962 2204 2466 2693 8340
95/95/103 98/98/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120
15 1435 1656 1897 2146 2416 2692 - 8245
95/95/103 99/99/106 103/103/109 106/106/112 109/109/115 112/112/118 -
20 1592 1840 2108 2390 2677 - - 7740
96/96/103 100/100/106 103/103/109 107/107/112 110/110/115 - -
25 1792 2072 2375 2677 - - - 7214
97/97/103 100/100/106 104/104/109 107/107/112 - - -
28 1931 2238 2554 - - - - 6894
97/97/103 101/101/106 104/104/109 - - - -

VFS 117 121 125 129 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 15
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 12000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 982 1129 1288 1447 1627 1818 1982 8340


93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
-35 996 1145 1308 1468 1651 1845 2012 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
-30 1010 1162 1327 1490 1676 1873 2042 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
-25 1025 1179 1346 1512 1701 1901 2073 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
-20 1040 1196 1366 1535 1726 1929 2104 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
-15 1055 1214 1386 1557 1752 1958 2135 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
-10 1072 1232 1408 1581 1779 1988 2169 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
-5 1144 1322 1504 1696 1910 2128 2329 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
0 1245 1431 1627 1848 2072 2316 2536 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
5 1349 1543 1773 2004 2252 2518 2749 8340
95/95/103 99/99/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120
10 1458 1683 1927 2180 2455 2736 - 8267
95/95/103 99/99/106 103/103/109 106/106/112 109/109/115 112/112/118 -
15 1604 1855 2122 2407 2698 - - 7807
96/96/103 100/100/106 103/103/109 106/106/112 110/110/115 - -
20 1796 2073 2379 2684 - - - 7295
97/97/103 100/100/106 104/104/109 107/107/112 - - -
25 2029 2347 - - - - - 6786
97/97/103 101/101/106 - - - - -
26 2084 2406 - - - - - 6693
97/97/103 101/101/106 - - - - -

VFS 117 121 125 129 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 16 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 13000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 1040 1204 1371 1540 1738 1937 2115 8340


94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
-35 1056 1221 1391 1563 1764 1966 2146 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
-30 1071 1239 1411 1586 1790 1996 2178 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
-25 1087 1257 1432 1610 1817 2026 2211 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
-20 1103 1276 1453 1634 1844 2056 2245 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
-15 1119 1294 1475 1658 1871 2087 2278 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
-10 1159 1339 1523 1716 1933 2154 2356 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
-5 1260 1448 1645 1869 2096 2342 2565 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
0 1368 1565 1797 2032 2283 2554 2789 8340
95/95/103 99/99/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120
5 1481 1709 1957 2212 2491 2776 - 8286
95/95/103 99/99/106 103/103/109 106/106/112 109/109/115 112/112/118 -
10 1616 1870 2137 2426 2720 - - 7863
96/96/103 100/100/106 103/103/109 106/106/112 110/110/115 - -
15 1796 2069 2378 2684 - - - 7396
96/96/103 100/100/106 104/104/109 107/107/112 - - -
20 2014 2334 2663 - - - - 6889
97/97/103 101/101/106 104/104/109 - - - -
24 2230 2567 - - - - - 6527
98/98/103 101/101/106 - - - - -

VFS 117 121 125 129 132 136 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 17
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 14000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 1110 1282 1457 1648 1855 2064 2262 8340


94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
-35 1127 1301 1479 1672 1882 2095 2296 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
-30 1143 1320 1501 1697 1910 2126 2331 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
-25 1160 1340 1523 1723 1939 2159 2366 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
-20 1177 1359 1545 1748 1968 2191 2401 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
-15 1194 1379 1568 1774 1997 2223 2437 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
-10 1275 1466 1664 1891 2122 2369 2596 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
-5 1385 1585 1819 2056 2309 2584 2822 8340
95/95/103 99/99/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120
0 1500 1729 1981 2239 2522 2811 - 8313
95/95/103 99/99/106 103/103/109 106/106/112 109/109/115 112/112/118 -
5 1632 1890 2159 2451 2749 - - 7906
96/96/103 100/100/106 103/103/109 106/106/112 110/110/115 - -
10 1796 2066 2377 2685 - - - 7488
96/96/103 100/100/106 104/104/109 107/107/112 - - -
15 1995 2314 2645 - - - - 7013
97/97/103 101/101/106 104/104/109 - - - -
20 2258 2601 - - - - - 6554
98/98/103 101/101/106 - - - - -
22 2373 - - - - - - 6377
98/98/103 - - - - - -

VFS 117 121 125 129 132 136 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 18 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: -1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 747 735 724 715 714 770 820 8340


109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-35 758 746 735 726 724 782 833 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-30 769 757 746 737 735 794 846 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-25 780 768 757 747 746 806 859 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-20 791 779 768 758 757 818 872 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-15 802 790 779 769 768 830 884 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-10 813 800 790 780 779 842 897 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-5 824 811 800 790 790 854 910 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
0 835 822 811 800 801 866 924 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
5 845 832 821 811 813 878 937 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
10 856 842 831 821 824 891 951 8340
109/109/121 106/106/118 102/102/114 100/100/111 98/98/108 101/101/111 104/104/113
15 866 853 841 831 836 904 965 8340
109/109/121 105/105/117 102/102/114 100/100/110 98/98/108 101/101/111 104/104/113
20 876 863 851 841 848 917 979 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 101/101/111 104/104/113
25 886 873 861 851 860 931 994 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 102/102/111 104/104/113
30 895 882 871 860 883 956 1022 8340
108/108/120 105/105/116 102/102/113 99/99/109 99/99/108 102/102/111 105/105/113
35 888 876 864 866 943 1038 1134 8340
104/104/115 101/101/112 98/98/108 96/96/106 100/100/108 103/103/111 106/106/113
40 883 871 860 927 1035 1161 1278 8340
101/101/111 98/98/107 95/95/104 97/97/106 101/101/108 104/104/111 107/107/113
45 878 867 905 1025 1160 1310 1448 8340
97/97/106 94/94/103 95/95/103 98/98/106 102/102/108 105/105/111 107/107/113
50 873 883 1011 1155 1316 1494 - 8141
94/94/102 92/92/100 96/96/103 99/99/106 102/102/108 106/106/111 -
52 872 925 1063 1217 1386 - - 7922
92/92/100 92/92/100 96/96/103 100/100/106 103/103/108 - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 19
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 0 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 769 756 745 735 732 790 842 8340


110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-35 780 767 756 746 743 802 855 8340
110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-30 792 779 768 758 755 815 868 8340
110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-25 803 790 779 768 766 827 881 8340
110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-20 814 801 790 779 777 839 895 8340
109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-15 826 812 801 790 789 852 908 8340
109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-10 837 823 812 801 800 864 922 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-5 848 834 823 812 812 877 935 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
0 859 845 833 823 823 889 949 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
5 870 855 844 833 835 903 963 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
10 880 866 854 843 847 916 978 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
15 891 876 865 854 859 929 992 8340
109/109/121 106/106/118 102/102/114 100/100/111 98/98/108 101/101/111 104/104/113
20 901 887 875 864 872 943 1007 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 101/101/111 104/104/113
25 912 899 887 876 889 963 1029 8340
109/109/121 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
30 906 894 882 871 937 1017 1111 8340
105/105/117 102/102/113 99/99/110 97/97/106 99/99/108 103/103/111 105/105/113
35 901 889 877 922 1014 1132 1248 8340
102/102/112 99/99/109 96/96/105 97/97/106 100/100/108 104/104/111 106/106/113
40 896 885 902 1006 1133 1276 1413 8340
98/98/108 95/95/104 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
45 892 880 991 1127 1280 1448 - 8314
95/95/104 92/92/100 95/95/103 99/99/106 102/102/108 105/105/111 -
50 887 968 1117 1281 1462 - - 7774
92/92/99 93/93/100 96/96/103 100/100/106 103/103/108 - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 20 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 789 776 765 754 752 812 865 8340


110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-35 801 787 776 766 764 825 879 8340
109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-30 813 799 788 777 775 837 893 8340
109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-25 824 810 799 789 787 850 906 8340
109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-20 836 822 810 800 799 863 920 8340
109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-15 847 833 822 811 811 876 934 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-10 859 845 833 822 822 889 948 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-5 870 856 844 834 834 902 962 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
0 882 867 855 845 846 915 976 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
5 893 878 866 855 858 928 991 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
10 904 889 877 866 871 942 1006 8340
109/109/121 106/106/118 102/102/114 100/100/111 98/98/108 101/101/111 104/104/113
15 914 900 888 877 883 956 1021 8340
109/109/121 105/105/118 102/102/114 99/99/110 98/98/108 101/101/111 104/104/113
20 926 911 899 888 899 974 1040 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 102/102/111 104/104/113
25 923 910 898 887 945 1025 1112 8340
106/106/118 103/103/114 100/100/110 97/97/107 99/99/108 102/102/111 105/105/113
30 919 906 895 920 1003 1116 1225 8340
103/103/114 100/100/110 97/97/106 97/97/106 100/100/108 103/103/111 106/106/113
35 914 902 901 993 1115 1257 1388 8340
99/99/109 96/96/106 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
40 910 898 977 1106 1255 1422 1575 8340
96/96/105 93/93/101 95/95/103 99/99/106 102/102/108 105/105/111 108/108/113
45 906 953 1094 1252 1427 - - 7928
93/93/101 92/92/100 96/96/103 99/99/106 103/103/108 - -
48 903 1019 1180 1356 1553 - - 7608
91/91/98 93/93/100 97/97/103 100/100/106 103/103/108 - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 21
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 2000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 809 795 784 774 775 836 892 8340


109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-35 821 807 796 785 786 850 906 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-30 833 819 808 797 798 863 920 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-25 845 831 820 809 810 876 934 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-20 857 843 831 820 823 889 949 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-15 869 855 843 832 835 903 963 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-10 881 866 854 843 847 916 977 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-5 892 878 866 855 859 929 992 8340
109/109/121 106/106/118 102/102/114 100/100/111 98/98/108 101/101/111 104/104/113
0 904 889 877 866 872 943 1007 8340
109/109/121 106/106/118 102/102/114 100/100/111 98/98/108 101/101/111 104/104/113
5 915 900 888 877 884 957 1022 8340
109/109/121 105/105/118 102/102/114 99/99/110 98/98/108 101/101/111 104/104/113
10 926 912 899 888 897 971 1037 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 101/101/111 104/104/113
15 937 923 910 899 910 986 1053 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 102/102/111 104/104/113
20 938 925 913 902 955 1036 1119 8340
106/106/118 103/103/114 100/100/111 97/97/107 99/99/108 102/102/111 105/105/113
25 936 923 912 926 1009 1113 1218 8340
103/103/114 100/100/111 97/97/107 96/96/106 100/100/108 103/103/111 106/106/113
30 932 920 909 985 1099 1233 1358 8340
100/100/110 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
35 928 916 965 1092 1237 1398 1544 8340
97/97/106 94/94/102 95/95/103 98/98/106 102/102/108 105/105/111 108/108/113
40 924 939 1075 1229 1401 1590 - 8077
93/93/102 92/92/100 96/96/103 99/99/106 103/103/108 106/106/111 -
45 923 1050 1216 1400 - - - 7550
90/90/98 93/93/100 97/97/103 100/100/106 - - -
46 932 1078 1251 1436 - - - 7445
89/89/97 93/93/100 97/97/103 100/100/106 - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 22 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 3000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 824 810 799 789 804 869 927 8340


108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-35 836 823 811 801 816 883 942 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-30 848 835 823 813 829 896 957 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-25 860 847 835 824 842 910 972 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-20 872 859 847 836 854 924 987 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-15 885 871 859 848 867 938 1002 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-10 897 883 871 860 880 952 1017 8340
108/108/120 105/105/117 102/102/113 99/99/109 98/98/108 102/102/111 104/104/113
-5 909 895 883 871 893 966 1033 8340
108/108/120 105/105/116 102/102/113 99/99/109 98/98/108 102/102/111 104/104/113
0 920 906 894 883 905 981 1048 8340
108/108/120 105/105/116 101/101/113 99/99/109 98/98/108 102/102/111 104/104/113
5 932 918 906 894 919 995 1064 8340
108/108/120 104/104/116 101/101/113 99/99/109 98/98/108 102/102/111 104/104/113
10 944 929 917 906 932 1010 1080 8340
108/108/120 104/104/116 101/101/113 98/98/109 98/98/108 102/102/111 104/104/113
15 952 939 927 916 966 1048 1128 8340
107/107/118 103/103/115 100/100/111 97/97/108 99/99/108 102/102/111 105/105/113
20 951 939 927 936 1020 1120 1224 8340
104/104/115 101/101/111 98/98/108 96/96/106 100/100/108 103/103/111 106/106/113
25 950 937 925 990 1094 1223 1348 8340
101/101/111 98/98/108 95/95/104 97/97/106 100/100/108 104/104/111 106/106/113
30 946 934 963 1077 1215 1369 1516 8340
98/98/107 95/95/104 95/95/103 98/98/106 101/101/108 105/105/111 107/107/113
35 942 937 1062 1210 1376 1556 - 8225
94/94/103 92/92/100 96/96/103 99/99/106 102/102/108 105/105/111 -
40 939 1036 1196 1373 1568 - - 7694
91/91/99 93/93/100 96/96/103 100/100/106 103/103/108 - -
44 983 1142 1328 1530 - - - 7283
90/90/97 94/94/100 97/97/103 101/101/106 - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 23
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 4000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 838 826 814 804 837 905 970 8340


107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-35 851 838 827 816 850 920 984 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-30 863 851 839 828 863 934 999 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-25 876 863 851 840 876 949 1014 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-20 888 875 863 853 889 963 1030 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-15 901 887 876 865 903 978 1046 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-10 913 900 888 877 916 993 1062 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-5 925 912 900 889 929 1008 1078 8340
107/107/119 103/103/115 100/100/112 98/98/108 99/99/108 102/102/111 105/105/113
0 937 924 911 900 943 1022 1094 8340
107/107/119 103/103/115 100/100/111 98/98/108 99/99/108 102/102/111 105/105/113
5 949 935 923 912 957 1038 1111 8340
107/107/119 103/103/115 100/100/111 98/98/108 99/99/108 102/102/111 105/105/113
10 964 951 938 927 978 1061 1138 8340
106/106/118 103/103/115 100/100/111 97/97/108 99/99/108 102/102/111 105/105/113
15 966 953 941 947 1032 1129 1234 8340
104/104/115 101/101/112 98/98/108 96/96/106 100/100/108 103/103/111 106/106/113
20 966 954 942 999 1098 1225 1351 8340
101/101/112 98/98/108 95/95/105 97/97/106 100/100/108 104/104/111 106/106/113
25 965 953 964 1063 1194 1347 1489 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
30 961 949 1047 1188 1347 1527 1694 8340
95/95/104 92/92/101 95/95/103 99/99/106 102/102/108 105/105/111 108/108/113
35 958 1023 1177 1348 1535 - - 7853
92/92/100 93/93/100 96/96/103 100/100/106 103/103/108 - -
40 991 1150 1337 1538 - - - 7337
90/90/97 93/93/100 97/97/103 100/100/106 - - -
42 1037 1210 1409 - - - - 7134
90/90/97 94/94/100 97/97/103 - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 24 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 5000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 855 843 831 821 876 949 1030 8340


106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-35 868 855 844 833 890 965 1045 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-30 881 868 857 846 904 980 1060 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-25 893 881 869 858 918 995 1076 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-20 906 893 881 870 932 1010 1093 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-15 919 906 894 883 946 1026 1109 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-10 931 918 906 895 960 1042 1125 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-5 944 931 919 908 974 1057 1142 8340
106/106/117 102/102/114 99/99/110 96/96/106 99/99/108 102/102/111 105/105/113
0 956 943 931 920 988 1073 1158 8340
105/105/117 102/102/113 99/99/110 96/96/106 99/99/108 102/102/111 105/105/113
5 969 955 943 932 1003 1089 1177 8340
105/105/117 102/102/113 99/99/110 96/96/106 99/99/108 102/102/111 105/105/113
10 982 969 957 958 1043 1137 1244 8340
104/104/116 101/101/112 98/98/108 96/96/106 100/100/108 103/103/111 106/106/113
15 982 969 957 1010 1105 1233 1358 8340
102/102/112 99/99/109 96/96/105 97/97/106 100/100/108 104/104/111 106/106/113
20 983 970 972 1066 1197 1347 1486 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
25 981 969 1029 1164 1319 1491 1646 8340
96/96/106 93/93/102 95/95/103 98/98/106 102/102/108 105/105/111 108/108/113
30 978 1001 1146 1311 1495 1698 - 8011
93/93/101 92/92/100 96/96/103 99/99/106 103/103/108 106/106/111 -
35 978 1122 1300 1495 - - - 7486
90/90/97 93/93/100 97/97/103 100/100/106 - - -
40 1088 1273 1484 - - - - 6990
90/90/97 94/94/100 98/98/103 - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 25
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 6000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 873 860 849 845 919 1000 1094 8340


104/104/116 101/101/112 98/98/109 96/96/106 99/99/108 103/103/111 105/105/113
-35 886 874 862 858 933 1015 1110 8340
104/104/116 101/101/112 98/98/109 96/96/106 99/99/108 103/103/111 105/105/113
-30 899 887 875 872 948 1030 1126 8340
104/104/116 101/101/112 98/98/109 96/96/106 99/99/108 103/103/111 105/105/113
-25 912 899 888 885 963 1046 1144 8340
104/104/116 101/101/112 98/98/109 96/96/106 99/99/108 103/103/111 105/105/113
-20 925 912 900 898 978 1062 1161 8340
104/104/116 101/101/112 98/98/108 96/96/106 99/99/108 103/103/111 105/105/113
-15 938 925 913 912 992 1078 1178 8340
104/104/116 101/101/112 98/98/108 96/96/106 99/99/108 103/103/111 105/105/113
-10 951 938 926 925 1007 1095 1196 8340
104/104/116 101/101/112 98/98/108 96/96/106 99/99/108 103/103/111 105/105/113
-5 964 951 939 939 1022 1111 1213 8340
104/104/116 101/101/112 98/98/108 96/96/106 99/99/108 103/103/111 105/105/113
0 977 963 951 952 1037 1128 1231 8340
104/104/116 101/101/112 98/98/108 96/96/106 99/99/108 103/103/111 105/105/113
5 994 981 968 977 1065 1164 1273 8340
104/104/115 101/101/111 98/98/108 96/96/106 100/100/108 103/103/111 106/106/113
10 995 982 970 1030 1129 1260 1389 8340
101/101/112 98/98/108 95/95/105 97/97/106 100/100/108 104/104/111 106/106/113
15 996 984 990 1087 1222 1376 1519 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
20 997 984 1045 1180 1337 1512 1670 8340
96/96/106 93/93/102 95/95/103 98/98/106 102/102/108 105/105/111 108/108/113
25 995 1002 1139 1301 1481 1679 - 8094
94/94/102 92/92/100 96/96/103 99/99/106 102/102/108 106/106/111 -
30 993 1112 1286 1478 - - - 7582
90/90/98 93/93/100 97/97/103 100/100/106 - - -
35 1078 1257 1465 - - - - 7083
90/90/97 94/94/100 97/97/103 - - - -
38 1161 1362 - - - - - 6797
91/91/97 94/94/100 - - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 26 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 7000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 887 874 863 895 975 1084 1189 8340


102/102/113 99/99/110 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-35 900 888 876 909 990 1101 1207 8340
102/102/113 99/99/110 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-30 913 901 889 923 1006 1117 1225 8340
102/102/113 99/99/110 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-25 927 914 903 937 1022 1134 1243 8340
102/102/113 99/99/110 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-20 940 927 916 952 1038 1151 1262 8340
102/102/113 99/99/110 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-15 953 941 929 966 1054 1168 1281 8340
102/102/113 99/99/109 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-10 967 954 942 981 1070 1186 1301 8340
102/102/113 99/99/109 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-5 980 967 955 995 1086 1203 1320 8340
102/102/113 99/99/109 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
0 993 980 968 1011 1103 1222 1341 8340
102/102/113 99/99/109 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
5 1007 994 982 1059 1169 1307 1440 8340
101/101/111 98/98/107 95/95/104 97/97/106 101/101/108 104/104/111 107/107/113
10 1009 996 1016 1122 1261 1422 1571 8340
98/98/108 95/95/104 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
15 1011 999 1071 1212 1374 1554 1716 8340
96/96/105 93/93/102 95/95/103 98/98/106 102/102/108 105/105/111 108/108/113
20 1013 1021 1158 1322 1505 1704 - 8119
94/94/102 92/92/100 96/96/103 99/99/106 102/102/108 106/106/111 -
25 1011 1115 1288 1478 1688 - - 7648
91/91/99 93/93/100 96/96/103 100/100/106 103/103/108 - -
30 1080 1257 1464 - - - - 7126
90/90/97 94/94/100 97/97/103 - - - -
35 1222 1435 - - - - - 6657
91/91/97 95/95/100 - - - - -
36 1253 1474 - - - - - 6569
91/91/97 95/95/100 - - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 27
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 8000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 901 889 877 949 1053 1179 1299 8340


100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-35 915 902 891 964 1069 1196 1318 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-30 929 916 905 979 1085 1214 1338 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-25 942 930 918 995 1101 1232 1358 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-20 956 943 932 1010 1118 1251 1379 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-15 970 957 945 1025 1134 1269 1399 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-10 983 970 959 1041 1151 1288 1420 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-5 997 984 972 1057 1168 1308 1441 8340
100/100/110 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
0 1018 1005 995 1092 1216 1365 1502 8340
100/100/110 97/97/106 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
5 1021 1009 1047 1166 1315 1481 1639 8340
97/97/107 94/94/103 95/95/103 98/98/106 101/101/108 105/105/111 107/107/113
10 1025 1013 1104 1252 1421 1611 1786 8340
96/96/105 93/93/101 95/95/103 99/99/106 102/102/108 105/105/111 108/108/113
15 1030 1041 1180 1346 1530 1731 - 8147
94/94/102 92/92/100 96/96/103 99/99/106 102/102/108 106/106/111 -
20 1030 1125 1296 1486 1692 - - 7750
91/91/99 93/93/100 96/96/103 100/100/106 103/103/108 - -
25 1089 1267 1473 1697 - - - 7216
90/90/97 94/94/100 97/97/103 101/101/106 - - -
30 1239 1456 - - - - - 6705
91/91/97 95/95/100 - - - - -
34 1381 - - - - - - 6360
91/91/97 - - - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 28 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 9000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 921 909 911 998 1120 1259 1388 8340


99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-35 936 923 926 1014 1137 1278 1409 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-30 950 937 940 1030 1154 1298 1430 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-25 964 951 955 1046 1172 1317 1452 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-20 978 966 969 1063 1189 1337 1474 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-15 992 980 984 1079 1207 1358 1496 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-10 1006 993 999 1096 1225 1378 1519 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-5 1020 1007 1014 1113 1244 1400 1543 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
0 1037 1024 1062 1181 1331 1499 1659 8340
98/98/107 95/95/104 95/95/103 98/98/106 101/101/108 105/105/111 107/107/113
5 1041 1028 1125 1275 1446 1637 1812 8340
95/95/104 92/92/101 95/95/103 99/99/106 102/102/108 105/105/111 108/108/113
10 1046 1061 1203 1371 1559 1762 - 8146
93/93/102 92/92/100 96/96/103 99/99/106 102/102/108 106/106/111 -
15 1049 1127 1295 1482 1686 - - 7812
92/92/99 93/93/100 96/96/103 100/100/106 103/103/108 - -
20 1069 1238 1436 1649 - - - 7387
90/90/97 93/93/100 97/97/103 100/100/106 - - -
25 1210 1419 1657 - - - - 6876
91/91/97 94/94/100 98/98/103 - - - -
30 1384 1634 - - - - - 6432
91/91/97 95/95/100 - - - - -
32 1461 - - - - - - 6260
92/92/97 - - - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 29
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 10000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 943 930 959 1063 1195 1346 1489 8340


98/98/108 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-35 957 945 974 1079 1213 1367 1511 8340
98/98/108 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-30 972 959 989 1095 1231 1387 1534 8340
98/98/108 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-25 987 974 1004 1112 1250 1409 1558 8340
98/98/107 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-20 1001 988 1020 1129 1269 1430 1582 8340
98/98/107 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-15 1016 1003 1036 1146 1288 1452 1606 8340
98/98/107 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-10 1030 1017 1052 1163 1308 1474 1630 8340
98/98/107 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-5 1048 1035 1071 1184 1332 1500 1659 8340
98/98/107 94/94/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
0 1060 1047 1128 1275 1447 1636 1807 8340
96/96/105 93/93/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/113
5 1064 1073 1212 1382 1572 1778 - 8123
94/94/102 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
10 1069 1136 1305 1494 1701 - - 7807
92/92/100 93/93/100 96/96/103 100/100/106 103/103/109 - -
15 1072 1231 1426 1640 - - - 7437
90/90/97 93/93/100 97/97/103 100/100/106 - - -
20 1174 1370 1597 - - - - 7014
90/90/97 94/94/100 97/97/103 - - - -
25 1328 1562 - - - - - 6577
91/91/97 95/95/100 - - - - -
30 1528 - - - - - - 6139
92/92/97 - - - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 30 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 11000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 964 952 1009 1133 1280 1444 1596 8340


96/96/106 93/93/102 95/95/103 98/98/106 102/102/109 105/105/111 108/108/113
-35 980 967 1025 1150 1299 1466 1620 8340
96/96/106 93/93/102 95/95/103 98/98/106 102/102/109 105/105/111 108/108/113
-30 995 982 1041 1167 1319 1488 1645 8340
96/96/106 93/93/102 95/95/103 98/98/106 102/102/109 105/105/111 108/108/113
-25 1010 997 1057 1185 1339 1510 1670 8340
96/96/106 93/93/102 95/95/103 98/98/106 102/102/109 105/105/111 108/108/113
-20 1025 1012 1074 1203 1359 1533 1695 8340
96/96/106 93/93/102 95/95/103 98/98/106 102/102/109 105/105/111 108/108/113
-15 1040 1027 1090 1221 1380 1556 1721 8340
96/96/106 93/93/102 95/95/103 98/98/106 102/102/109 105/105/111 108/108/113
-10 1054 1041 1107 1239 1400 1580 1747 8340
96/96/106 93/93/102 95/95/103 98/98/106 102/102/109 105/105/111 108/108/113
-5 1078 1064 1147 1295 1468 1660 1833 8340
96/96/105 93/93/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/113
0 1080 1094 1238 1413 1607 1818 - 8117
94/94/102 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
5 1085 1169 1345 1541 1754 - - 7755
91/91/99 93/93/100 96/96/103 100/100/106 103/103/109 - -
10 1093 1263 1463 1681 - - - 7416
89/89/97 93/93/100 97/97/103 100/100/106 - - -
15 1192 1391 1621 - - - - 7032
90/90/97 94/94/100 97/97/103 - - - -
20 1334 1568 - - - - - 6624
91/91/97 95/95/100 - - - - -
25 1526 - - - - - - 6202
92/92/97 - - - - - -

VFS 117 121 125 129 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 31
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 12000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 987 975 1068 1209 1371 1552 1716 8340


95/95/104 92/92/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/114
-35 1003 990 1084 1227 1392 1575 1741 8340
95/95/104 92/92/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/114
-30 1018 1005 1100 1245 1413 1599 1768 8340
95/95/104 92/92/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/114
-25 1034 1021 1117 1264 1435 1623 1795 8340
95/95/104 92/92/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/114
-20 1049 1036 1134 1283 1457 1648 1822 8340
95/95/104 92/92/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/114
-15 1065 1052 1151 1303 1478 1673 1849 8340
95/95/104 92/92/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/114
-10 1081 1068 1169 1323 1502 1700 1879 8340
95/95/104 92/92/101 95/95/103 99/99/106 102/102/109 105/105/111 108/108/114
-5 1099 1111 1254 1430 1625 1838 - 8147
94/94/102 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
0 1102 1189 1369 1567 1784 - - 7760
91/91/99 93/93/100 96/96/103 100/100/106 103/103/109 - -
5 1117 1292 1497 1719 - - - 7399
90/90/97 93/93/100 97/97/103 100/100/106 - - -
10 1212 1414 1647 - - - - 7045
90/90/97 94/94/100 97/97/103 - - - -
15 1345 1580 - - - - - 6669
91/91/97 95/95/100 - - - - -
20 1525 - - - - - - 6266
92/92/97 - - - - - -

VFS 117 121 125 129 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 32 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 13000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 1010 1013 1139 1296 1471 1664 - 8204


94/94/103 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
-35 1026 1029 1156 1315 1493 1689 - 8213
94/94/103 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
-30 1042 1045 1174 1335 1515 1714 - 8221
94/94/103 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
-25 1059 1061 1192 1355 1538 1741 - 8229
94/94/103 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
-20 1074 1078 1209 1376 1562 1767 - 8236
94/94/103 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
-15 1090 1094 1227 1396 1585 1794 - 8242
94/94/103 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
-10 1116 1128 1271 1448 1645 1858 - 8157
94/94/102 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
-5 1122 1204 1385 1585 1803 - - 7785
91/91/99 93/93/100 96/96/103 100/100/106 103/103/109 - -
0 1134 1310 1518 1743 - - - 7413
90/90/97 93/93/100 97/97/103 100/100/106 - - -
5 1233 1437 1673 - - - - 7055
90/90/97 94/94/100 97/97/103 - - - -
10 1355 1590 - - - - - 6708
91/91/97 95/95/100 - - - - -
15 1522 - - - - - - 6342
92/92/97 - - - - - -

VFS 117 121 125 129 132 136 -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 33
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 14000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 1033 1067 1214 1387 1580 1791 - 8001


93/93/101 92/92/100 96/96/103 99/99/106 103/103/109 106/106/111 -
-35 1050 1084 1232 1408 1604 1818 - 8009
93/93/101 92/92/100 96/96/103 99/99/106 103/103/109 106/106/111 -
-30 1066 1101 1251 1430 1628 1845 - 8017
93/93/101 92/92/100 96/96/103 99/99/106 103/103/109 106/106/111 -
-25 1083 1118 1270 1452 1653 1873 - 8025
93/93/101 92/92/100 96/96/103 99/99/106 103/103/109 106/106/111 -
-20 1100 1136 1289 1473 1678 1902 - 8033
93/93/101 92/92/100 96/96/103 99/99/106 103/103/109 106/106/111 -
-15 1116 1154 1308 1495 1703 1930 - 8039
93/93/101 92/92/100 96/96/103 99/99/106 103/103/109 106/106/111 -
-10 1141 1219 1401 1603 1825 - - 7809
92/92/100 93/93/100 96/96/103 100/100/106 103/103/109 - -
-5 1151 1326 1536 1764 - - - 7437
90/90/97 93/93/100 97/97/103 100/100/106 - - -
0 1248 1455 1693 - - - - 7077
90/90/97 94/94/100 97/97/103 - - - -
5 1370 1607 - - - - - 6737
91/91/97 94/94/100 - - - - -
10 1518 1789 - - - - - 6409
91/91/97 95/95/100 - - - - -
15 1721 - - - - - - 6036
92/92/97 - - - - - -

VFS 117 121 125 129 132 136 -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 34 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: -1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 649 667 713 758 810 901 985 8340


105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-35 659 676 722 768 822 913 999 8340
105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-30 669 686 732 779 833 926 1013 8340
105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-25 678 695 742 789 845 939 1027 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-20 688 704 752 800 857 952 1042 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-15 697 714 762 811 869 966 1057 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-10 707 724 772 821 881 979 1071 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-5 716 734 782 832 893 993 1087 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
0 725 743 792 843 906 1007 1102 8340
104/104/117 104/104/116 103/103/115 103/103/115 104/104/115 107/107/118 110/110/120
5 734 752 802 854 919 1022 1119 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 35
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 0 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 669 685 730 777 827 917 1003 8340


105/105/118 104/104/117 104/104/116 104/104/115 104/104/115 107/107/118 110/110/120
-35 678 694 739 786 839 930 1018 8340
105/105/118 104/104/117 104/104/116 104/104/115 104/104/115 107/107/118 110/110/120
-30 688 704 749 797 851 943 1032 8340
105/105/118 104/104/117 104/104/116 104/104/115 104/104/115 107/107/118 110/110/120
-25 698 715 759 808 863 957 1047 8340
105/105/118 104/104/117 104/104/116 104/104/115 104/104/115 107/107/118 110/110/120
-20 707 725 769 819 876 971 1063 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-15 717 735 780 830 889 985 1079 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-10 726 744 790 841 901 1000 1094 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-5 736 754 801 852 914 1015 1110 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
0 745 764 811 864 928 1029 1127 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
5 754 773 822 875 942 1046 1145 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 36 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 686 703 748 796 848 941 1029 8340


105/105/118 104/104/117 104/104/116 104/104/115 104/104/115 107/107/118 110/110/120
-35 696 713 757 806 861 955 1044 8340
105/105/118 104/104/117 104/104/116 104/104/115 104/104/115 107/107/118 110/110/120
-30 706 723 768 818 874 968 1060 8340
105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-25 716 734 779 829 886 983 1075 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-20 726 744 789 840 900 997 1091 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-15 736 754 800 852 913 1012 1107 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-10 745 764 811 863 926 1027 1124 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-5 755 774 821 875 939 1042 1140 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
0 765 784 832 886 953 1058 1157 8340
104/104/117 104/104/116 103/103/115 103/103/115 104/104/115 107/107/118 110/110/120
5 774 794 843 898 968 1075 1176 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 37
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 2000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 704 722 768 818 874 969 1060 8340


105/105/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-35 714 731 778 828 887 984 1076 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-30 724 742 788 839 900 999 1092 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-25 734 752 799 851 913 1013 1108 8340
104/104/118 104/104/117 104/104/116 103/103/115 104/104/115 107/107/118 110/110/120
-20 744 763 810 863 927 1028 1125 8340
104/104/118 104/104/117 103/103/116 103/103/115 104/104/115 107/107/118 110/110/120
-15 754 774 821 875 940 1044 1141 8340
104/104/117 104/104/116 103/103/115 103/103/115 104/104/115 107/107/118 110/110/120
-10 764 784 833 886 954 1060 1159 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
-5 774 794 844 898 968 1076 1177 8340
104/104/117 104/104/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
0 784 804 855 910 983 1093 1195 8340
104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
5 792 813 872 927 1009 1126 1231 8340
103/103/116 103/103/115 103/103/114 102/102/114 104/104/115 107/107/118 110/110/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 38 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 3000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 717 737 791 841 913 1018 1111 8340


104/104/117 103/103/116 103/103/115 103/103/114 104/104/115 107/107/118 110/110/120
-35 727 747 801 852 927 1033 1128 8340
103/103/117 103/103/116 103/103/115 102/102/114 104/104/115 107/107/118 110/110/120
-30 737 757 812 864 940 1049 1145 8340
103/103/117 103/103/116 103/103/115 102/102/114 104/104/115 107/107/118 110/110/120
-25 748 768 824 876 954 1064 1162 8340
103/103/116 103/103/115 103/103/114 102/102/114 104/104/115 107/107/118 110/110/120
-20 758 778 835 889 969 1081 1180 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 107/107/118 110/110/120
-15 768 789 847 901 983 1097 1198 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 107/107/118 110/110/120
-10 778 799 858 913 998 1114 1216 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 108/108/118 110/110/120
-5 788 810 870 925 1013 1131 1235 8340
103/103/116 103/103/115 102/102/114 102/102/113 104/104/115 108/108/118 110/110/120
0 798 821 881 937 1028 1148 1254 8340
103/103/116 102/102/115 102/102/114 102/102/113 104/104/115 108/108/118 110/110/120
5 800 850 910 992 1112 1240 1350 8340
101/101/113 100/100/112 100/100/111 102/102/112 105/105/115 108/108/118 111/111/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 39
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 4000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 730 761 816 867 959 1073 1170 8340


102/102/115 102/102/114 102/102/113 101/101/112 105/105/115 108/108/118 110/110/120
-35 740 771 827 879 974 1089 1188 8340
102/102/115 102/102/114 102/102/113 101/101/112 105/105/115 108/108/118 110/110/120
-30 751 782 838 891 988 1106 1206 8340
102/102/115 102/102/114 102/102/113 101/101/112 105/105/115 108/108/118 110/110/120
-25 762 793 850 904 1003 1123 1225 8340
102/102/115 102/102/114 102/102/113 101/101/112 105/105/115 108/108/118 110/110/120
-20 772 804 862 917 1019 1140 1243 8340
102/102/115 102/102/114 101/101/113 101/101/112 105/105/115 108/108/118 110/110/120
-15 782 815 874 930 1034 1157 1263 8340
102/102/115 102/102/114 101/101/113 101/101/112 105/105/115 108/108/118 110/110/120
-10 793 826 885 944 1050 1175 1282 8340
102/102/115 102/102/114 101/101/113 101/101/112 105/105/115 108/108/118 110/110/120
-5 803 837 897 959 1067 1193 1302 8340
102/102/115 101/101/114 101/101/113 101/101/112 105/105/115 108/108/118 110/110/120
0 813 860 921 997 1116 1246 1357 8340
101/101/113 101/101/113 100/100/112 101/101/112 105/105/115 108/108/118 111/111/120
5 828 890 970 1093 1227 1363 1480 8340
98/98/110 98/98/109 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 40 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 5000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 745 789 845 912 1019 1138 1239 8340


101/101/114 101/101/113 101/101/112 101/101/112 105/105/115 108/108/118 111/111/120
-35 755 799 856 926 1035 1155 1258 8340
101/101/114 101/101/113 100/100/112 101/101/112 105/105/115 108/108/118 111/111/120
-30 766 810 868 939 1050 1173 1277 8340
101/101/114 101/101/113 100/100/112 101/101/112 105/105/115 108/108/118 111/111/120
-25 776 821 880 953 1066 1191 1297 8340
101/101/113 101/101/112 100/100/111 101/101/112 105/105/115 108/108/118 111/111/120
-20 787 833 892 968 1083 1209 1317 8340
101/101/113 100/100/112 100/100/111 101/101/112 105/105/115 108/108/118 111/111/120
-15 798 844 904 983 1100 1228 1337 8340
101/101/113 100/100/112 100/100/111 102/102/112 105/105/115 108/108/118 111/111/120
-10 809 856 917 998 1117 1246 1358 8340
101/101/113 100/100/112 100/100/111 102/102/112 105/105/115 108/108/118 111/111/120
-5 820 868 929 1013 1134 1266 1379 8340
101/101/113 100/100/112 100/100/111 102/102/112 105/105/115 108/108/118 111/111/120
0 839 902 976 1098 1233 1371 1489 8340
98/98/110 98/98/109 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
5 869 942 1069 1210 1352 1499 1645 8340
95/95/106 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 41
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 6000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 760 817 874 963 1084 1207 1312 8340


100/100/112 100/100/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-35 770 828 886 978 1100 1225 1332 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-30 781 839 898 992 1117 1244 1353 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-25 793 851 911 1008 1134 1263 1374 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-20 804 863 923 1023 1152 1283 1396 8340
100/100/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-15 815 875 936 1039 1169 1303 1417 8340
99/99/112 99/99/111 99/99/110 102/102/112 105/105/115 108/108/118 111/111/120
-10 827 891 953 1060 1194 1329 1446 8340
99/99/111 99/99/110 99/99/109 102/102/112 105/105/115 108/108/118 111/111/120
-5 855 920 997 1123 1261 1400 1521 8340
98/98/110 98/98/109 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
0 885 956 1086 1228 1372 1522 1670 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
5 914 1042 1193 1342 1498 1679 1834 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 42 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 7000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 792 851 928 1046 1175 1304 1416 8340


98/98/110 98/98/109 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-35 802 862 942 1062 1193 1324 1438 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-30 812 874 956 1078 1211 1344 1460 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 111/111/120
-25 824 886 971 1095 1229 1365 1482 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 112/112/120
-20 835 898 986 1112 1248 1386 1505 8340
98/98/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 112/112/120
-15 847 911 1000 1129 1267 1408 1529 8340
97/97/109 97/97/108 99/99/109 102/102/112 106/106/115 109/109/118 112/112/120
-10 875 940 1039 1178 1319 1463 1597 8340
97/97/109 97/97/108 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-5 906 993 1133 1280 1428 1591 1744 8340
95/95/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
0 948 1086 1241 1394 1563 1748 1908 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
5 1037 1197 1359 1537 1728 1924 2109 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 43
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 8000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 824 885 1002 1136 1271 1408 1544 8340


96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-35 835 899 1018 1153 1290 1429 1568 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-30 846 912 1033 1171 1310 1451 1592 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-25 858 926 1048 1188 1330 1473 1616 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-20 870 940 1065 1207 1351 1496 1642 8340
96/96/107 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-15 887 961 1090 1235 1381 1531 1681 8340
95/95/106 96/96/106 99/99/109 103/103/112 106/106/115 109/109/118 112/112/120
-10 925 1023 1171 1321 1472 1646 1802 8340
94/94/105 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 112/112/120
-5 983 1131 1290 1447 1630 1820 1983 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
0 1074 1236 1403 1591 1788 1991 2184 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
5 1202 1374 1578 1784 2004 2241 2447 8340
95/95/103 98/98/106 102/102/109 105/105/112 109/109/115 112/112/118 114/114/120

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 44 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 9000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 854 938 1068 1207 1348 1500 1644 8340


95/95/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-35 865 952 1084 1226 1369 1523 1669 8340
95/95/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-30 877 966 1101 1244 1390 1547 1695 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-25 890 981 1118 1264 1411 1571 1722 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-20 902 996 1135 1283 1433 1596 1749 8340
94/94/105 96/96/106 100/100/109 103/103/112 106/106/115 110/110/118 112/112/120
-15 931 1038 1188 1340 1494 1672 1829 8340
94/94/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 112/112/120
-10 986 1134 1294 1453 1632 1824 1989 8340
93/93/103 97/97/106 101/101/109 104/104/112 107/107/115 110/110/118 113/113/120
-5 1084 1249 1417 1604 1802 2005 2199 8340
94/94/103 98/98/106 101/101/109 105/105/112 108/108/115 111/111/118 114/114/120
0 1198 1371 1569 1776 1991 2229 2435 8340
95/95/103 98/98/106 102/102/109 105/105/112 108/108/115 112/112/118 114/114/120
5 1333 1541 1763 1997 2247 2502 - 8201
95/95/103 99/99/106 103/103/109 106/106/112 109/109/115 112/112/118 -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 45
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 10000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 886 993 1138 1283 1430 1601 1751 8340


94/94/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-35 897 1009 1156 1304 1453 1626 1779 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-30 910 1024 1174 1324 1475 1651 1807 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-25 922 1040 1192 1344 1498 1677 1834 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-20 935 1056 1210 1365 1522 1704 1864 8340
93/93/104 96/96/106 100/100/109 103/103/112 107/107/115 110/110/118 113/113/120
-15 981 1123 1284 1444 1617 1810 1976 8340
93/93/103 97/97/106 100/100/109 104/104/112 107/107/115 110/110/118 113/113/120
-10 1076 1242 1411 1593 1792 1995 2185 8340
94/94/103 97/97/106 101/101/109 104/104/112 108/108/115 111/111/118 113/113/120
-5 1180 1353 1541 1748 1957 2190 2395 8340
94/94/103 98/98/106 102/102/109 105/105/112 108/108/115 111/111/118 114/114/120
0 1301 1492 1713 1931 2177 2429 2647 8340
95/95/103 99/99/106 102/102/109 106/106/112 109/109/115 112/112/118 115/115/120
5 1465 1695 1938 2199 2465 - - 7774
96/96/103 100/100/106 103/103/109 106/106/112 110/110/115 - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 46 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: -1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 749 737 726 717 714 771 821 8340


109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-35 760 747 737 727 725 783 834 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-30 771 758 748 738 736 795 847 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-25 782 769 759 749 747 807 860 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-20 792 780 769 759 758 819 873 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-15 803 791 780 770 770 831 886 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-10 814 801 790 780 781 844 900 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-5 824 812 801 791 792 856 913 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
0 835 822 811 801 804 869 927 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
5 845 832 821 811 815 882 941 8340
109/109/121 105/105/117 102/102/114 100/100/110 98/98/108 101/101/111 104/104/113

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 47
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 0 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 772 759 748 738 733 791 843 8340


110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-35 782 769 758 748 744 803 856 8340
110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-30 793 780 769 759 756 816 869 8340
110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-25 805 791 780 770 767 828 883 8340
110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-20 815 802 791 780 779 841 897 8340
109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-15 826 813 802 791 791 854 911 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-10 837 824 812 802 802 867 925 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-5 848 834 823 812 814 880 939 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
0 859 845 833 823 826 893 952 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
5 869 855 843 833 838 906 967 8340
109/109/121 106/106/118 102/102/114 100/100/110 98/98/108 101/101/111 104/104/113

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 48 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 791 778 767 757 753 813 866 8340


110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-35 802 789 778 768 765 826 880 8340
110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-30 814 800 789 779 777 839 894 8340
110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-25 825 812 800 790 789 852 908 8340
109/109/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-20 837 823 812 801 801 865 923 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-15 848 834 823 812 813 878 937 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-10 859 845 834 823 825 891 951 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-5 870 856 844 834 837 905 966 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
0 881 867 855 844 849 918 980 8340
109/109/121 106/106/118 102/102/114 100/100/111 98/98/108 101/101/111 104/104/113
5 892 877 866 855 862 932 995 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 101/101/111 104/104/113

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 49
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 2000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 812 799 787 777 776 838 893 8340


110/110/122 106/106/118 103/103/115 100/100/111 98/98/108 101/101/111 104/104/113
-35 823 809 798 787 788 851 908 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-30 834 821 809 799 800 864 922 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-25 846 832 821 810 812 878 937 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-20 858 844 832 821 825 892 951 8340
109/109/122 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-15 869 855 844 833 837 905 966 8340
109/109/121 106/106/118 103/103/114 100/100/111 98/98/108 101/101/111 104/104/113
-10 881 867 855 844 850 919 981 8340
109/109/121 106/106/118 102/102/114 100/100/111 98/98/108 101/101/111 104/104/113
-5 892 878 866 855 862 933 996 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 101/101/111 104/104/113
0 903 889 877 866 875 947 1011 8340
109/109/121 105/105/117 102/102/114 99/99/110 98/98/108 102/102/111 104/104/113
5 912 899 887 876 894 968 1034 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 50 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 3000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 827 814 803 792 805 870 929 8340


109/109/121 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-35 838 825 813 803 818 884 944 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-30 850 837 825 814 831 898 959 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-25 862 848 837 826 843 913 974 8340
108/108/120 105/105/117 102/102/113 99/99/110 98/98/108 102/102/111 104/104/113
-20 874 860 849 838 857 927 990 8340
108/108/120 105/105/117 102/102/113 99/99/109 98/98/108 102/102/111 104/104/113
-15 885 872 860 849 870 941 1006 8340
108/108/120 105/105/116 102/102/113 99/99/109 98/98/108 102/102/111 104/104/113
-10 897 883 871 860 883 956 1021 8340
108/108/120 105/105/116 101/101/113 99/99/109 98/98/108 102/102/111 104/104/113
-5 908 895 883 872 896 971 1037 8340
108/108/120 104/104/116 101/101/113 99/99/109 98/98/108 102/102/111 104/104/113
0 920 906 894 883 909 985 1053 8340
108/108/120 104/104/116 101/101/113 98/98/109 98/98/108 102/102/111 105/105/113
5 922 909 897 886 955 1036 1127 8340
105/105/117 102/102/113 99/99/110 96/96/106 99/99/108 102/102/111 105/105/113

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 51
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 4000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 841 829 817 807 838 907 972 8340


107/107/119 104/104/116 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-35 853 840 829 818 851 922 987 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-30 865 853 841 830 865 936 1002 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-25 877 865 853 842 878 951 1018 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-20 890 877 865 854 892 966 1034 8340
107/107/119 104/104/115 101/101/112 98/98/108 99/99/108 102/102/111 105/105/113
-15 901 888 877 866 906 982 1050 8340
107/107/119 104/104/115 100/100/112 98/98/108 99/99/108 102/102/111 105/105/113
-10 913 900 888 877 919 997 1067 8340
107/107/119 103/103/115 100/100/111 98/98/108 99/99/108 102/102/111 105/105/113
-5 925 912 900 889 934 1012 1084 8340
107/107/119 103/103/115 100/100/111 98/98/108 99/99/108 102/102/111 105/105/113
0 937 924 912 901 964 1046 1132 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
5 935 923 911 941 1025 1137 1246 8340
103/103/114 99/99/110 97/97/106 97/97/106 100/100/108 103/103/111 106/106/113

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 52 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 5000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 859 847 835 825 877 951 1032 8340


106/106/118 103/103/114 100/100/110 97/97/107 99/99/108 102/102/111 105/105/113
-35 870 858 846 836 892 966 1048 8340
106/106/117 103/103/114 100/100/110 97/97/107 99/99/108 102/102/111 105/105/113
-30 883 870 858 848 906 982 1064 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-25 895 882 871 860 920 998 1081 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-20 907 895 883 872 934 1014 1098 8340
106/106/117 102/102/114 99/99/110 97/97/107 99/99/108 102/102/111 105/105/113
-15 920 907 895 884 949 1030 1115 8340
106/106/117 102/102/114 99/99/110 97/97/106 99/99/108 102/102/111 105/105/113
-10 932 919 907 896 964 1046 1133 8340
105/105/117 102/102/113 99/99/110 96/96/106 99/99/108 102/102/111 105/105/113
-5 944 931 919 908 979 1063 1151 8340
105/105/117 102/102/113 99/99/110 96/96/106 99/99/108 102/102/111 105/105/113
0 952 939 927 950 1035 1143 1252 8340
103/103/114 100/100/110 97/97/107 97/97/106 100/100/108 103/103/111 106/106/113
5 950 938 926 1011 1126 1263 1390 8340
100/100/110 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 53
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 6000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 876 864 852 847 920 1002 1096 8340


105/105/116 101/101/112 98/98/109 96/96/106 99/99/108 103/103/111 105/105/113
-35 888 876 864 860 935 1018 1113 8340
105/105/116 101/101/112 98/98/109 96/96/106 99/99/108 103/103/111 105/105/113
-30 901 889 877 874 950 1034 1130 8340
104/104/116 101/101/112 98/98/109 96/96/106 99/99/108 103/103/111 105/105/113
-25 914 901 890 887 965 1050 1149 8340
104/104/116 101/101/112 98/98/108 96/96/106 99/99/108 103/103/111 105/105/113
-20 927 914 902 901 981 1067 1167 8340
104/104/116 101/101/112 98/98/108 96/96/106 99/99/108 103/103/111 105/105/113
-15 939 926 914 915 996 1084 1185 8340
104/104/116 101/101/112 98/98/108 96/96/106 99/99/108 103/103/111 105/105/113
-10 954 941 929 932 1015 1107 1210 8340
104/104/115 101/101/112 98/98/108 96/96/106 100/100/108 103/103/111 106/106/113
-5 968 955 943 969 1056 1169 1282 8340
103/103/114 100/100/110 97/97/107 97/97/106 100/100/108 103/103/111 106/106/113
0 969 956 944 1028 1144 1283 1411 8340
100/100/110 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
5 968 956 997 1118 1262 1422 1572 8340
97/97/107 94/94/103 95/95/103 98/98/106 102/102/108 105/105/111 107/107/113

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 54 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 7000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 891 879 867 896 976 1087 1192 8340


103/103/113 99/99/110 97/97/106 97/97/106 100/100/108 103/103/111 106/106/113
-35 903 891 879 911 992 1104 1211 8340
102/102/113 99/99/110 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-30 916 903 891 925 1008 1121 1230 8340
102/102/113 99/99/110 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-25 929 916 904 940 1025 1139 1250 8340
102/102/113 99/99/110 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-20 942 929 917 955 1041 1157 1270 8340
102/102/113 99/99/109 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-15 955 942 930 970 1058 1175 1290 8340
102/102/113 99/99/109 96/96/106 97/97/106 100/100/108 103/103/111 106/106/113
-10 976 963 951 1002 1097 1224 1349 8340
102/102/112 99/99/109 96/96/105 97/97/106 100/100/108 104/104/111 106/106/113
-5 980 968 968 1062 1193 1343 1481 8340
99/99/109 96/96/106 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
0 981 968 1028 1163 1317 1488 1642 8340
97/97/106 94/94/102 95/95/103 98/98/106 102/102/108 105/105/111 108/108/113
5 980 992 1132 1292 1471 - - 7923
94/94/102 92/92/100 96/96/103 99/99/106 103/103/108 - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 55
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 8000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 905 893 882 951 1056 1182 1302 8340


101/101/111 97/97/107 95/95/104 97/97/106 101/101/108 104/104/111 107/107/113
-35 917 905 894 966 1072 1201 1323 8340
100/100/111 97/97/107 94/94/104 97/97/106 101/101/108 104/104/111 107/107/113
-30 931 918 907 982 1089 1219 1344 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-25 944 932 920 997 1106 1238 1365 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-20 958 945 933 1013 1123 1258 1386 8340
100/100/111 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-15 973 960 949 1035 1150 1290 1420 8340
100/100/110 97/97/107 94/94/103 97/97/106 101/101/108 104/104/111 107/107/113
-10 995 982 993 1098 1234 1390 1536 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-5 994 982 1071 1213 1375 1556 1722 8340
96/96/105 93/93/101 95/95/103 99/99/106 102/102/108 105/105/111 108/108/113
0 996 1023 1171 1339 1527 - - 7892
93/93/101 92/92/100 96/96/103 99/99/106 103/103/108 - -
5 998 1147 1329 1527 - - - 7376
90/90/97 93/93/100 97/97/103 100/100/106 - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 56 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 9000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 925 913 913 1000 1123 1263 1392 8340


99/99/109 96/96/106 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-35 938 926 927 1016 1141 1283 1414 8340
99/99/109 96/96/106 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-30 952 939 942 1033 1159 1303 1437 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-25 966 953 957 1050 1177 1324 1460 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-20 980 967 972 1066 1196 1345 1484 8340
99/99/109 96/96/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-15 1001 988 1007 1114 1252 1411 1561 8340
98/98/108 95/95/105 94/94/103 98/98/106 101/101/108 104/104/111 107/107/113
-10 1013 1001 1074 1214 1377 1557 1721 8340
96/96/105 93/93/102 95/95/103 99/99/106 102/102/108 105/105/111 108/108/113
-5 1014 1034 1182 1352 1539 - - 7974
93/93/102 92/92/100 96/96/103 99/99/106 103/103/108 - -
0 1013 1140 1319 1516 - - - 7515
90/90/98 93/93/100 97/97/103 100/100/106 - - -
5 1106 1292 1506 - - - - 7002
90/90/97 94/94/100 98/98/103 - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

ANAC APPROVED 5-15


REVISION 7 code 01 Page 57
PHENOM 300 TM

Airplane Flight Manual

Performance

SIMPLIFIED TAKEOFF ANALYSIS


FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW535E ENGINES
Airport Pressure Altitude: 10000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
6000 6400 6800 7200 7600 8000 8340 WEIGHT

-40 948 936 960 1066 1198 1350 1493 8340


98/98/108 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-35 960 948 976 1083 1218 1372 1518 8340
98/98/108 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-30 974 962 992 1100 1237 1394 1542 8340
98/98/107 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-25 988 976 1008 1117 1257 1416 1566 8340
98/98/107 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-20 1003 990 1024 1135 1277 1439 1592 8340
98/98/107 95/95/104 94/94/103 98/98/106 101/101/109 105/105/111 107/107/113
-15 1033 1020 1071 1205 1364 1539 1700 8340
97/97/107 94/94/103 95/95/103 98/98/106 102/102/109 105/105/111 108/108/113
-10 1034 1036 1176 1342 1526 1726 - 8064
94/94/103 92/92/100 96/96/103 99/99/106 102/102/109 106/106/111 -
-5 1037 1125 1296 1485 1692 - - 7635
92/92/99 93/93/100 96/96/103 100/100/106 103/103/109 - -
0 1078 1252 1455 - - - - 7165
90/90/97 94/94/100 97/97/103 - - - -
5 1227 1440 - - - - - 6647
91/91/97 94/94/100 - - - - -

VFS 117 121 125 128 132 135 138

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT


OBSTACLES.
AFM-2664

5-15 ANAC APPROVED


Page 58 code 01 REVISION 7
PHENOM 300 TM

Airplane Flight Manual

Performance

APPROACH FLAP 1 AND LANDING FLAP 3


ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF

PW535E ENGINES

LANDING
APPROACH
(CLIMB/REFERENCE)
WEIGHT
VFS – KIAS
(kg) FLAP 1 FLAP 3

VAC – KIAS VREF – KIAS


5600 104 100 113
5800 105 102 115
6000 107 104 117
6200 109 106 119
6400 110 107 121
6600 112 109 123
6800 114 110 125
7000 115 112 126
7200 117 114 128
7400 118 115 130
7600 120 117 132
7800 121 118 133
8000 123 120 135
8200 124 121 137
8340 125 122 138

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT WAS EXCEEDED.
AFM-2664

5-20 ANAC APPROVED


Page 2 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

APPROACH FLAP 1 AND LANDING FLAP 3


ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED)

PW535E ENGINES

APPROACH CLIMB/LANDING
WEIGHT (CLIMB/REFERENCE) VFS – KIAS
(kg)
SPEED – KIAS
5600 108 127
5800 110 129
6000 111 131
6200 113 133
6400 115 135
6600 117 137
6800 118 139
7000 120 141
7200 122 143
7400 124 145
7600 125 147
7800 127 149
8000 128 151
8200 130 152
8340 131 154

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-20


REVISION 7 code 01 Page 3
PHENOM 300 TM

Airplane Flight Manual

Performance

APPROACH FLAP 2 AND LANDING FLAP FULL


ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF

PW535E ENGINES

LANDING
APPROACH
(CLIMB/REFERENCE)
WEIGHT
VFS – KIAS
(kg) FLAP 2 FLAP FULL

VAC – KIAS VREF FULL – KIAS


5600 100 100 113
5800 101 101 115
6000 103 103 117
6200 105 105 119
6400 106 106 121
6600 108 108 123
6800 109 109 125
7000 111 111 126
7200 112 112 128
7400 114 114 130
7600 115 115 132
7800 117 117 133
8000 118 118 135
8200 120 120 137
8340 121 121 138

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT WAS EXCEEDED.
AFM-2664

5-20 ANAC APPROVED


Page 4 code 01 REVISION 7
TM

PHENOM 300
Airplane Flight Manual
Performance

APPROACH FLAP 2 AND LANDING FLAP FULL


ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED)

PW535E ENGINES

APPROACH CLIMB/LANDING
WEIGHT (CLIMB/REFERENCE) VFS – KIAS
(kg)
SPEED – KIAS
5600 106 126
5800 108 128
6000 109 131
6200 111 133
6400 113 135
6600 114 137
6800 116 139
7000 118 141
7200 119 143
7400 121 145
7600 122 147
7800 124 149
8000 125 151
8200 127 152
8340 128 154

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-20


REVISION 7 code 01 Page 5
TM

PHENOM 300
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
0 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
45 8340 (O) 8340 (O) 8340 (O) 8340 (O) - -
50 8340 (O) 8340 (O) - - - -

NOTE: The values above Maximum Landing Weight must not be


used for dispatch.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 3
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
0 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8236 (A)
25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8153 (A) 7679 (A)
30 8340 (O) 8340 (O) 8340 (O) 7938 (A) 7587 (A) 7126 (A)
35 8340 (O) 8212 (E) 7825 (E) - - -
40 8015 (E) - - - - -

NOTE: The values above Maximum Landing Weight must not be


used for dispatch.
AFM-2664

5-25 ANAC APPROVED


Page 4 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
11000 ft 12000 ft 13000 ft 14000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-5 8340 (O) 8340 (O) 8340 (O) 8340 (O)
0 8340 (O) 8340 (O) 8340 (O) 8340 (O)
5 8340 (O) 8340 (O) 8333 (A) 7941 (A)
10 8340 (O) 8305 (A) 7896 (A) 7516 (A)
15 8275 (A) 7829 (A) 7410 (A) 7023 (A)
20 7751 (A) 7304 (A) 6892 (A) 6549 (A)
25 7212 (A) 6781 (A) - -

NOTE: The values above Maximum Landing Weight must not be


used for dispatch.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 5
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION ON – WINGSTAB OFF
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
11000 ft 12000 ft 13000 ft 14000 ft
5 8340 (O) 8340 (O) 8065 (A) 7675 (A)
10 8340 (O) 8051 (A) 7641 (A) 7269 (A)

NOTE: - The values above Maximum Landing Weight must not be


used for dispatch.
- Applicable to airplanes Post-Mod. SB 505-00-0001 or with
an equivalent modification factory incorporated.
AFM-2664

5-25 ANAC APPROVED


Page 6 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED)
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
0 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
8 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8329 (E)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8303 (E)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8294 (E) 7839 (E)
-5 8340 (O) 8340 (O) 8340 (O) 8267 (E) 7843 (E) 7404 (E)
0 8340 (O) 8340 (O) 8170 (E) 7780 (E) 7358 (E) 6910 (E)
5 8340 (O) 8008 (E) 7600 (E) 7213 (E) 6803 (E) 6384 (E)
8 8072 (E) 7650 (E) 7386 (E) 6963 (E) 6534 (E) 6093 (E)

NOTE: - The shaded area and values above Maximum Landing


Weight must not be used for dispatch.
- Applicable to airplanes Post-Mod. SB 505-00-0001 or with
an equivalent modification factory incorporated.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 7
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED)
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-35 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-30 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-25 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-20 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-15 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-10 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-5 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
0 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
5 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
8 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-35 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-30 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-25 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-20 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-15 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O)
-10 8150 (O) 8150 (O) 8150 (O) 8150 (O) 8150 (O) 7839 (E)
-5 8150 (O) 8150 (O) 8150 (O) 8150 (O) 7844 (E) 7403 (E)
0 8150 (O) 8150 (O) 8150 (O) 7780 (E) 7358 (E) 6910 (E)
5 8150 (O) 8008 (E) 7601 (E) 7213 (E) 6803 (E) 6384 (E)
8 8150 (O) 7900 (E) 7200 (E) 6900 (E) 6450 (E) 6050 (E)

NOTE: - The shaded area and values above Maximum Landing


Weight must not be used for dispatch.
- Applicable to airplanes Pre-Mod. SB 505-00-0001 or with an
equivalent modification factory incorporated.
AFM-2664

5-25 ANAC APPROVED


Page 8 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
0 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8172 (A) 7801 (A)
40 8340 (O) 8340 (O) 8340 (O) 8023 (A) 7640 (A) 7283 (A)
45 8340 (O) 8257 (A) 7873 (A) 7494 (A) - -
50 8084 (A) 7719 (A) - - - -

NOTE: The values above Maximum Landing Weight must not be


used for dispatch.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 9
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
0 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8027 (A)
10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8110 (A) 7705 (A)
15 8340 (O) 8340 (O) 8340 (O) 8109 (A) 7770 (A) 7327 (A)
20 8340 (O) 8340 (O) 8073 (A) 7705 (A) 7338 (A) 6894 (A)
25 8340 (O) 8042 (A) 7597 (A) 7165 (A) 6827 (A) 6454 (A)
30 7959 (A) 7530 (A) 7073 (A) 6653 (A) 6376 (A) 6009 (A)
35 7433 (A) 7028 (A) 6603 (A) - - -
40 6934 (A) - - - - -

NOTE: The values above the Maximum Landing Weight must not be
used for dispatch.
AFM-2664

5-25 ANAC APPROVED


Page 10 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
11000 ft 12000 ft 13000 ft 14000 ft
-40 8340 (O) 8340 (O) 8153 (A) 7949 (A)
-35 8340 (O) 8340 (O) 8159 (A) 7954 (A)
-30 8340 (O) 8340 (O) 8163 (A) 7958 (A)
-25 8340 (O) 8340 (O) 8164 (A) 7959 (A)
-20 8340 (O) 8340 (O) 8165 (A) 7961 (A)
-15 8340 (O) 8340 (O) 8166 (A) 7963 (A)
-10 8340 (O) 8340 (O) 8067 (A) 7721 (A)
-5 8340 (O) 8055 (A) 7696 (A) 7346 (A)
0 8021 (A) 7665 (A) 7318 (A) 6983 (A)
5 7659 (A) 7302 (A) 6958 (A) 6644 (A)
10 7315 (A) 6942 (A) 6611 (A) 6310 (A)
15 6922 (A) 6565 (A) 6234 (A) 5924 (A)
20 6510 (A) 6151 (A) 5821 (A) 5536 (A)
25 6080 (A) 5726 (A) - -

NOTE: The values above the Maximum Landing Weight must not be
used for dispatch.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION ON – WINGSTAB OFF
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8166 (A) 7795 (A)
10 8340 (O) 8340 (O) 8340 (O) 8153 (A) 7881 (A) 7482 (A)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
11000 ft 12000 ft 13000 ft 14000 ft
5 7428 (A) 7074 (A) 6741 (A) 6435 (A)
10 7094 (A) 6734 (A) 6412 (A) 6113 (A)

NOTE: The values above the Maximum Landing Weight must not be
used for dispatch.
AFM-2664

5-25 ANAC APPROVED


Page 12 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED


APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED)
PW535E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
0 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
5 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
8 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8329 (E)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)


TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-35 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-30 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-25 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-20 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O)
-15 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8303 (E)
-10 8340 (O) 8340 (O) 8340 (O) 8340 (O) 8294 (E) 7839 (E)
-5 8340 (O) 8340 (O) 8340 (O) 8267 (E) 7843 (E) 7404 (E)
0 8340 (O) 8340 (O) 8170 (E) 7780 (E) 7358 (E) 6910 (E)
5 8340 (O) 8008 (E) 7600 (E) 7213 (E) 6803 (E) 6384 (E)
8 8072 (E) 7650 (E) 7386 (E) 6963 (E) 6534 (E) 6093 (E)

NOTE: The shaded area and values above Maximum Landing Weight
must not be used for dispatch.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 13
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3
PW535E ENGINES

ALTITUDE
Weight -1000 ft 0 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 777 652 613 574 790 665 625 586
5800 793 667 627 589 807 680 640 601
6000 809 683 642 603 823 696 656 616
6200 825 698 657 618 840 712 671 631
6400 842 713 673 633 857 728 687 646
6600 857 728 687 647 873 743 701 661
6800 873 743 702 661 889 758 716 675
7000 889 758 716 676 905 773 731 690
7200 905 773 731 690 922 789 747 705
7400 920 788 745 704 937 804 761 719
7600 936 802 759 718 953 819 776 733
7800 952 817 774 732 973 833 790 748
8000 974 831 788 746 996 849 805 762
8200 996 846 803 760 1019 864 820 777

ALTITUDE
Weight 1000 ft 2000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 805 679 639 599 820 693 652 613
5800 821 694 654 614 837 709 668 628
6000 838 710 670 630 854 725 684 644
6200 855 726 685 645 872 742 700 660
6400 873 743 701 661 889 758 716 676
6600 889 758 716 676 906 774 732 691
6800 906 774 732 691 923 790 748 706
7000 923 790 747 706 940 806 763 722
7200 939 806 763 721 957 823 779 737
7400 955 821 777 735 974 838 795 752
7600 972 836 792 750 995 853 810 767
7800 995 851 807 765 1018 869 825 782
8000 1019 866 822 779 1043 885 841 797
8200 1043 882 838 794 1068 901 856 812

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 15
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3
PW535E ENGINES

ALTITUDE
Weight 3000 ft 4000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 835 707 666 626 851 722 681 641
5800 852 724 682 642 869 739 697 657
6000 870 740 699 658 887 756 714 673
6200 888 757 715 675 905 773 731 690
6400 906 774 732 691 924 791 748 707
6600 923 790 748 706 941 807 765 723
6800 941 807 764 722 959 824 781 739
7000 958 823 780 738 977 841 798 755
7200 976 840 797 754 995 858 814 771
7400 994 856 812 769 1018 874 830 787
7600 1018 872 828 784 1042 891 846 803
7800 1042 888 843 800 1068 907 862 818
8000 1068 904 859 815 1094 924 879 834
8200 1094 923 875 831 1122 947 895 850

ALTITUDE
Weight 5000 ft 6000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 867 737 696 655 887 756 714 673
5800 885 755 713 672 906 774 731 690
6000 904 772 730 689 925 791 749 707
6200 923 790 747 706 944 810 767 725
6400 942 808 765 723 964 828 785 742
6600 960 825 782 739 982 845 802 759
6800 978 842 798 756 1001 863 819 776
7000 997 859 815 772 1020 881 836 793
7200 1017 877 833 789 1045 899 854 810
7400 1042 893 849 805 1070 916 871 826
7600 1067 910 865 821 1097 933 887 843
7800 1094 927 882 837 1125 952 904 859
8000 1122 948 898 854 1154 976 922 876
8200 1150 972 918 870 1184 1001 945 893

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

5-25 ANAC APPROVED


Page 16 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3
PW535E ENGINES

ALTITUDE
Weight 7000 ft 8000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 906 773 731 690 926 792 749 707
5800 926 792 749 707 946 810 767 725
6000 945 810 767 725 966 829 786 743
6200 965 829 785 743 986 848 804 761
6400 985 847 804 761 1006 867 823 780
6600 1004 865 821 778 1025 886 841 797
6800 1023 883 839 795 1045 904 859 815
7000 1044 902 857 813 1071 923 878 833
7200 1072 920 875 830 1100 942 896 851
7400 1098 937 892 847 1128 960 913 868
7600 1126 955 909 864 1157 981 931 886
7800 1156 978 926 881 1188 1006 951 903
8000 1186 1003 948 898 1219 1032 975 921
8200 1218 1029 972 918 1253 1059 1001 945

ALTITUDE
Weight 9000 ft 10000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 946 810 767 725 967 830 786 744
5800 966 830 786 743 988 850 806 762
6000 987 849 805 762 1009 870 825 781
6200 1007 868 824 781 1030 890 845 801
6400 1028 888 843 800 1051 910 864 820
6600 1048 907 862 818 1072 929 883 839
6800 1070 926 880 836 1099 948 902 857
7000 1099 945 899 854 1129 968 922 876
7200 1129 964 918 873 1160 988 941 895
7400 1158 983 936 890 1191 1011 959 913
7600 1189 1008 954 908 1223 1037 981 932
7800 1221 1035 978 926 1257 1065 1007 952
8000 1254 1062 1004 948 1292 1094 1034 977
8200 1289 1090 1030 973 1329 1124 1062 1003

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 17
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3
PW535E ENGINES

ALTITUDE
Weight 11000 ft 12000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 990 851 807 764 1013 873 828 784
5800 1011 871 827 783 1035 893 848 804
6000 1032 891 846 802 1057 914 868 824
6200 1054 912 867 822 1079 935 889 844
6400 1076 933 887 842 1101 956 910 865
6600 1099 952 906 861 1130 977 930 884
6800 1129 972 926 880 1161 997 950 904
7000 1161 992 946 900 1194 1018 970 923
7200 1193 1014 965 919 1228 1044 991 944
7400 1226 1041 985 938 1262 1072 1015 963
7600 1260 1069 1011 956 1298 1101 1042 985
7800 1295 1098 1038 981 1335 1132 1071 1012
8000 1332 1128 1066 1008 1374 1164 1100 1040
8200 1371 1159 1096 1036 1415 1197 1131 1069

ALTITUDE
Weight 13000 ft 14000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 1037 895 849 805 1061 918 872 827
5800 1059 916 870 825 1084 939 893 848
6000 1082 937 891 846 1107 961 914 869
6200 1104 959 912 867 1130 983 936 890
6400 1130 981 934 888 1161 1006 958 912
6600 1161 1001 954 908 1195 1027 979 932
6800 1194 1022 975 928 1229 1048 1000 953
7000 1229 1046 995 948 1265 1077 1021 974
7200 1265 1076 1018 969 1303 1109 1050 995
7400 1301 1105 1046 989 1341 1139 1079 1021
7600 1338 1136 1075 1017 1380 1172 1109 1049
7800 1377 1168 1105 1045 1422 1205 1140 1079
8000 1419 1201 1136 1074 1466 1240 1173 1109
8200 1462 1236 1168 1104 1512 1277 1208 1142

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

5-25 ANAC APPROVED


Page 18 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED) – FLAP 3
PW535E ENGINES

ALTITUDE
Weight -1000 ft 0 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 851 721 680 640 866 736 694 654
5800 869 739 697 657 885 754 712 671
6000 887 756 714 673 903 771 729 688
6200 905 773 731 689 922 788 746 704
6400 924 790 747 706 940 806 763 721
6600 941 806 763 721 958 823 779 737
6800 959 824 781 738 977 841 797 754
7000 977 841 797 754 995 858 814 771
7200 994 856 813 770 1013 874 830 786
7400 1016 873 829 786 1039 891 847 803
7600 1041 890 845 801 1064 908 863 819
7800 1066 906 861 817 1091 925 879 835
8000 1092 922 877 833 1118 945 896 851
8200 1118 943 892 848 1145 967 913 867

ALTITUDE
Weight 1000 ft 2000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 882 751 709 668 899 767 724 683
5800 902 769 727 686 919 785 743 701
6000 920 787 744 703 938 803 761 719
6200 939 805 762 720 957 822 778 736
6400 958 823 780 737 977 840 797 754
6600 976 840 796 754 995 858 814 771
6800 996 858 814 771 1015 877 832 789
7000 1014 876 832 788 1035 894 850 806
7200 1037 892 848 804 1061 911 866 822
7400 1063 910 865 821 1088 930 884 840
7600 1090 927 882 838 1116 947 901 857
7800 1117 945 899 854 1144 969 919 873
8000 1145 969 916 871 1174 993 939 890
8200 1173 992 937 886 1203 1017 961 908

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 19
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED) – FLAP 3
PW535E ENGINES

ALTITUDE
Weight 3000 ft 4000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 916 783 740 699 933 799 756 715
5800 936 802 759 717 954 819 776 734
6000 956 820 777 735 974 838 794 752
6200 976 839 796 753 995 857 813 770
6400 996 858 814 771 1015 877 832 789
6600 1015 876 832 788 1035 895 850 806
6800 1035 895 851 807 1057 915 870 825
7000 1059 914 869 824 1085 934 888 844
7200 1086 931 886 841 1112 951 906 861
7400 1115 950 904 859 1142 971 924 879
7600 1143 969 922 876 1172 994 942 897
7800 1173 994 940 894 1203 1020 964 914
8000 1204 1019 964 911 1235 1047 989 935
8200 1234 1044 987 932 1267 1073 1014 958

ALTITUDE
Weight 5000 ft 6000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 952 816 773 731 974 837 793 751
5800 973 837 793 750 996 858 814 771
6000 994 856 812 769 1017 878 833 790
6200 1014 876 831 788 1038 898 853 809
6400 1035 896 851 807 1060 918 873 829
6600 1055 914 869 825 1081 938 892 847
6800 1082 935 889 845 1112 958 912 867
7000 1111 954 908 863 1142 978 932 886
7200 1139 972 926 881 1172 997 950 904
7400 1171 995 945 900 1205 1024 970 924
7600 1202 1020 965 918 1237 1051 994 942
7800 1234 1047 990 936 1272 1079 1020 965
8000 1268 1075 1017 961 1307 1108 1048 991
8200 1302 1102 1042 985 1343 1137 1075 1016

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

5-25 ANAC APPROVED


Page 20 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED) – FLAP 3
PW535E ENGINES

ALTITUDE
Weight 7000 ft 8000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 996 857 813 770 1017 878 833 789
5800 1018 878 834 790 1040 899 854 810
6000 1040 899 854 810 1062 920 875 830
6200 1061 919 874 829 1085 941 895 850
6400 1083 940 894 849 1108 963 916 871
6600 1109 960 914 868 1138 983 936 890
6800 1141 981 935 889 1171 1005 958 911
7000 1173 1001 954 908 1204 1026 978 931
7200 1204 1024 973 927 1237 1053 997 950
7400 1238 1053 996 947 1273 1083 1025 971
7600 1272 1081 1023 967 1309 1112 1053 996
7800 1308 1110 1050 993 1347 1143 1082 1023
8000 1346 1141 1079 1020 1386 1175 1112 1051
8200 1383 1171 1107 1047 1426 1207 1141 1079

ALTITUDE
Weight 9000 ft 10000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 1040 899 853 809 1064 921 875 830
5800 1063 921 875 831 1088 944 897 852
6000 1086 942 896 851 1111 965 919 873
6200 1109 964 917 872 1134 988 941 895
6400 1137 986 939 893 1167 1010 963 916
6600 1168 1007 959 913 1201 1031 984 937
6800 1203 1029 981 935 1237 1055 1006 959
7000 1238 1055 1002 955 1273 1085 1028 980
7200 1272 1083 1026 975 1309 1115 1056 1000
7400 1310 1115 1055 999 1349 1148 1087 1029
7600 1348 1145 1084 1026 1389 1181 1118 1058
7800 1387 1178 1115 1054 1431 1214 1150 1088
8000 1429 1211 1146 1084 1475 1250 1183 1119
8200 1471 1245 1177 1113 1519 1285 1215 1149

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 21
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION OFF – WINGSTAB OFF
FLAP FULL
PW535E ENGINES

ALTITUDE
Weight -1000 ft 0 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 759 636 597 559 773 649 610 572
5800 774 650 611 573 788 663 624 585
6000 790 665 626 587 804 679 639 600
6200 805 680 640 601 820 693 653 614
6400 821 694 654 615 835 708 668 628
6600 836 709 668 629 851 723 682 642
6800 851 722 682 642 866 737 696 656
7000 865 736 695 655 881 751 710 669
7200 880 750 709 669 897 766 724 683
7400 895 765 723 682 912 780 738 697
7600 909 778 736 695 926 794 752 710
7800 924 791 749 708 942 808 765 723
8000 943 806 763 722 964 823 780 738
8200 963 820 777 735 985 837 793 751

ALTITUDE
Weight 1000 ft 2000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 787 662 623 584 801 676 636 597
5800 802 677 637 598 817 691 651 612
6000 819 693 653 613 834 707 667 627
6200 835 708 667 628 851 723 682 642
6400 851 723 682 642 867 738 697 657
6600 867 738 697 657 884 754 712 672
6800 883 753 711 671 900 768 727 686
7000 898 767 725 685 915 783 741 700
7200 914 782 740 699 931 799 756 715
7400 930 797 754 713 948 814 771 729
7600 944 811 768 726 964 828 785 743
7800 964 825 782 740 986 842 799 757
8000 986 840 797 754 1010 858 814 772
8200 1009 854 811 768 1033 873 829 786

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

5-25 ANAC APPROVED


Page 22 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION OFF – WINGSTAB OFF
FLAP FULL
PW535E ENGINES

ALTITUDE
Weight 3000 ft 4000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 817 690 650 611 832 705 664 625
5800 833 706 665 626 849 721 680 640
6000 850 722 681 641 867 738 696 656
6200 867 738 697 656 884 754 712 672
6400 884 754 712 672 901 770 728 687
6600 901 770 728 687 919 786 744 703
6800 917 785 743 702 935 802 759 718
7000 933 800 758 716 952 818 775 733
7200 950 816 773 731 968 833 790 748
7400 966 831 788 746 988 849 806 763
7600 987 846 802 760 1010 864 821 778
7800 1009 861 817 774 1034 879 835 792
8000 1034 877 833 790 1059 896 851 808
8200 1058 892 847 804 1084 915 867 823

ALTITUDE
Weight 5000 ft 6000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 848 720 679 639 868 738 697 657
5800 865 736 695 655 886 755 713 672
6000 884 753 712 671 905 773 731 689
6200 901 770 728 687 922 790 747 706
6400 919 787 744 703 941 807 764 722
6600 937 803 761 719 959 824 781 739
6800 954 819 776 734 976 840 797 754
7000 971 835 792 750 994 857 813 770
7200 988 852 808 765 1014 873 829 786
7400 1011 868 824 781 1039 890 845 802
7600 1035 883 839 796 1064 906 861 817
7800 1059 899 854 811 1089 922 877 832
8000 1086 917 871 827 1117 944 893 849
8200 1112 938 886 842 1145 966 912 865

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 23
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION OFF – WINGSTAB OFF
FLAP FULL
PW535E ENGINES

ALTITUDE
Weight 7000 ft 8000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 887 756 714 673 906 774 732 690
5800 905 773 731 689 925 791 749 707
6000 924 791 748 707 945 810 767 725
6200 943 808 765 723 963 828 784 742
6400 961 826 782 740 982 845 802 759
6600 980 843 800 757 1001 864 819 776
6800 998 860 816 773 1020 881 836 793
7000 1015 877 833 789 1041 898 853 809
7200 1040 894 849 806 1067 915 870 826
7400 1066 911 866 822 1095 933 888 843
7600 1092 927 882 838 1122 950 904 859
7800 1119 946 898 853 1149 973 920 875
8000 1148 970 916 870 1180 998 943 892
8200 1177 994 938 886 1210 1023 966 912

ALTITUDE
Weight 9000 ft 10000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 926 792 750 708 947 812 769 726
5800 945 810 767 725 967 830 786 744
6000 965 829 786 743 987 850 806 763
6200 985 847 804 761 1007 868 824 781
6400 1004 866 822 778 1027 887 842 799
6600 1024 884 840 796 1047 906 861 817
6800 1042 902 857 813 1070 924 879 834
7000 1068 920 874 830 1097 942 897 852
7200 1096 937 892 847 1126 961 915 869
7400 1125 956 910 865 1156 980 933 887
7600 1153 976 926 881 1185 1005 950 904
7800 1182 1000 945 897 1216 1030 973 921
8000 1214 1027 970 916 1250 1058 1000 944
8200 1246 1053 995 939 1283 1085 1025 968

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

5-25 ANAC APPROVED


Page 24 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION OFF – WINGSTAB OFF
FLAP FULL
PW535E ENGINES

ALTITUDE
Weight 11000 ft 12000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 970 833 789 746 993 854 810 766
5800 989 851 807 764 1013 873 828 785
6000 1011 871 827 783 1035 894 849 805
6200 1031 890 846 802 1055 913 868 823
6400 1051 910 864 820 1076 933 887 842
6600 1072 929 884 839 1102 953 907 862
6800 1100 948 902 857 1131 972 925 880
7000 1129 966 920 875 1161 991 944 898
7200 1159 985 938 893 1192 1013 963 917
7400 1190 1010 957 911 1225 1040 984 936
7600 1221 1035 979 928 1258 1067 1009 954
7800 1253 1061 1003 948 1292 1094 1035 978
8000 1289 1091 1031 974 1329 1125 1064 1005
8200 1324 1119 1058 999 1367 1155 1092 1031

ALTITUDE
Weight 13000 ft 14000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 1016 876 831 787 1041 899 853 809
5800 1037 895 850 806 1062 919 873 828
6000 1059 917 871 826 1085 940 894 849
6200 1080 937 891 846 1106 961 914 869
6400 1102 957 911 865 1133 982 935 889
6600 1133 978 931 885 1165 1003 955 909
6800 1163 997 950 904 1197 1023 975 928
7000 1195 1016 969 922 1230 1046 995 948
7200 1228 1043 988 942 1265 1075 1018 967
7400 1262 1072 1014 961 1301 1105 1046 989
7600 1296 1100 1040 984 1337 1135 1074 1015
7800 1332 1129 1068 1009 1375 1165 1102 1042
8000 1372 1161 1098 1038 1417 1199 1134 1072
8200 1411 1193 1127 1065 1459 1233 1165 1101

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 25
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED) – FLAP FULL
PW535E ENGINES

ALTITUDE
Weight -1000 ft 0 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 820 693 653 614 835 707 667 627
5800 838 710 669 629 853 724 683 643
6000 854 725 684 644 870 740 699 658
6200 871 741 700 659 887 756 714 674
6400 888 757 715 675 904 772 730 689
6600 904 772 730 689 921 788 746 704
6800 921 788 746 705 938 805 762 720
7000 938 804 761 719 955 820 777 735
7200 953 818 775 733 971 835 792 750
7400 970 834 791 748 990 851 808 765
7600 990 849 805 763 1013 867 823 780
7800 1013 864 820 777 1036 882 838 794
8000 1036 879 835 792 1061 897 853 809
8200 1062 895 850 807 1087 917 869 825

ALTITUDE
Weight 1000 ft 2000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 851 722 681 641 867 737 696 655
5800 869 739 698 657 885 755 713 672
6000 886 755 714 673 903 771 729 688
6200 904 772 730 689 921 788 746 704
6400 921 789 746 705 939 805 763 721
6600 938 804 762 720 956 822 779 736
6800 956 822 778 736 975 839 796 753
7000 973 838 794 752 993 856 812 769
7200 990 853 809 767 1011 871 827 784
7400 1013 869 825 782 1037 888 844 800
7600 1036 885 841 797 1061 904 859 816
7800 1061 901 856 812 1087 920 875 831
8000 1086 917 872 828 1113 941 891 847
8200 1114 940 888 844 1142 964 910 863

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

5-25 ANAC APPROVED


Page 26 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.
TM

PHENOM 300
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED) – FLAP FULL
PW535E ENGINES

ALTITUDE
Weight 3000 ft 4000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 883 753 711 670 901 769 727 686
5800 902 771 729 687 920 787 745 703
6000 921 788 745 704 939 805 762 720
6200 939 805 762 721 957 822 779 737
6400 958 823 780 737 977 840 797 754
6600 975 839 796 753 995 857 814 771
6800 994 857 813 770 1014 876 832 788
7000 1012 874 830 787 1035 893 849 805
7200 1035 890 846 802 1060 910 865 821
7400 1061 907 863 819 1087 927 882 838
7600 1087 924 879 834 1114 944 899 854
7800 1113 942 895 850 1142 967 915 870
8000 1141 965 911 866 1170 990 936 887
8200 1171 989 935 883 1202 1016 960 906

ALTITUDE
Weight 5000 ft 6000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 918 785 743 702 940 806 763 721
5800 938 804 761 720 961 825 782 739
6000 957 822 779 737 980 843 800 757
6200 977 840 797 754 1000 862 818 775
6400 996 859 815 772 1020 881 836 793
6600 1014 876 832 789 1039 899 854 810
6800 1034 895 851 807 1062 918 873 829
7000 1060 913 868 824 1090 936 891 846
7200 1086 930 884 840 1117 953 908 863
7400 1114 948 902 858 1146 973 926 881
7600 1142 968 919 874 1175 997 943 898
7800 1171 992 938 891 1206 1022 966 915
8000 1201 1017 961 908 1237 1048 990 936
8200 1234 1044 986 931 1272 1076 1017 961

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

ANAC APPROVED 5-25


REVISION 11 code 01 Page 27
Copyright © by Embraer S.A. All rights reserved – See title page for details.
PHENOM 300 TM

Airplane Flight Manual

Performance

UNFACTORED LANDING DISTANCE (m)


ENGINE ICE PROTECTION ON – WINGSTAB ON
(SWPS ICE SPEED) – FLAP FULL
PW535E ENGINES

ALTITUDE
Weight 7000 ft 8000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 961 825 781 739 982 845 801 758
5800 982 845 801 758 1004 865 821 777
6000 1002 864 819 776 1024 884 840 796
6200 1022 883 838 795 1045 904 859 815
6400 1042 902 857 813 1066 924 878 834
6600 1062 920 875 831 1088 942 897 852
6800 1090 940 894 850 1119 963 917 871
7000 1119 959 913 868 1149 982 935 890
7200 1147 976 930 885 1178 1001 953 907
7400 1178 1000 949 903 1210 1028 973 926
7600 1208 1025 969 920 1242 1055 998 944
7800 1240 1051 994 940 1276 1082 1024 968
8000 1273 1078 1020 964 1311 1111 1050 993
8200 1309 1108 1047 990 1349 1141 1079 1020

ALTITUDE
Weight 9000 ft 10000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
5600 1004 865 821 777 1027 887 842 798
5800 1026 886 841 797 1050 908 863 818
6000 1047 906 861 816 1071 928 883 838
6200 1068 926 880 836 1093 949 903 858
6400 1090 946 900 855 1118 970 923 878
6600 1117 965 919 874 1148 989 943 897
6800 1149 986 939 894 1181 1011 963 917
7000 1180 1006 959 913 1214 1033 983 937
7200 1211 1030 977 931 1246 1060 1004 955
7400 1245 1058 1001 950 1282 1090 1031 976
7600 1278 1086 1027 971 1317 1119 1059 1001
7800 1314 1114 1054 997 1354 1149 1087 1028
8000 1350 1144 1082 1023 1393 1180 1116 1056
8200 1391 1177 1113 1052 1435 1214 1148 1086

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE


THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEDED.
AFM-2664

5-25 ANAC APPROVED


Page 28 code 01 REVISION 11
Copyright © by Embraer S.A. All rights reserved – See title page for details.

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