TM

PHENOM 100
Airplane Flight Manual
Performance

SECTION 5

PERFORMANCE
TABLE OF CONTENTS
Block Page
Introduction ........................................................................ 5-00.......... 02
Performance Configuration................................................ 5-01.......... 01
Definitions .......................................................................... 5-01.......... 02
Noise Levels ...................................................................... 5-01.......... 05
Software Presentation ....................................................... 5-02.......... 01
Position Error Corrections ................................................. 5-05.......... 01
Stall Speed ........................................................................ 5-08.......... 01
Thrust Setting Tables ........................................................ 5-10.......... 01
Takeoff Data ...................................................................... 5-15.......... 01
Driftdown Tables (Gross Gradient).................................... 5-18.......... 01
Enroute Gradient ............................................................... 5-18.......... 04
Approach Data................................................................... 5-20.......... 01
Landing Data ..................................................................... 5-25.......... 01
AFM-2655

ANAC APPROVED 5-00

REVISION 2 code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

INTRODUCTION
The performance information given in this Section is applicable to the
PHENOM 100 airplane.
The performance data are based on the following conditions:
í Pertinent power less installation, air bleed, and accessory
losses.
í Full temperature accountability within the operational limits for
which the airplane is certified.
The performance information is not valid if:
í The airplane’s gross weight exceeds the appropriate maximum
allowable limits.
í Any of the limitations in Section 2 is not observed.
í A reading from any performance analysis is obtained by
extrapolation (i.e. using values of parameters outside the range
given on the graph).

AFM-2655

5-00 ANAC APPROVED

Page 2 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

PERFORMANCE CONFIGURATION
NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
The configurations applicable to each performance phase are shown
below.

OPERATING
TLA FLAPS GEAR AIRSPEED
ENGINES

TAKEOFF 2 until VEF,

TO/GA 1 or 2 DOWN 0 TO VLOF
RUN 1 after VEF

DOWN TO
1ST SEGMENT 1 TO/GA 1 or 2 VLOF TO V2
UP

2ND SEGMENT 1 TO/GA 1 or 2 UP V2

V2 TO FINAL
TAKEOFF
3RD SEGMENT 1 TO/GA UP SEGMENT
FLAPS TO 0
SPEED

FINAL
FINAL
1 MAX CON 0 UP SEGMENT
SEGMENT
SPEED

ENROUTE
ENROUTE 1 MAX CON 0 UP CLIMB
SPEED

APPROACH
APPROACH
1 TO/GA 1 or 2 UP CLIMB
CLIMB
SPEED

LANDING
LANDING
2 TO/GA 3 or FULL DOWN CLIMB
CLIMB
SPEED

LANDING 2 IDLE 3 or FULL DOWN VREF

AFM-2655

ANAC APPROVED 5-01

REVISION 5 code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

DEFINITIONS
OUTSIDE AIR TEMPERATURE – OAT OR SAT
Free static (ambient) temperature.

TOTAL AIR TEMPERATURE – TAT

Total temperature measured and corrected by the ADS system with
airplane in motion.

INDICATED AIRSPEED – KIAS

It is the reading on the airspeed indicator (knots), as installed in the
airplane. Zero instrument error is assumed by the OPERA.

CALIBRATED AIRSPEED – KCAS

It is the indicated airspeed corrected for the anemometric system
position error.

TRUE AIRSPEED – TAS

It is the airplane speed in relation to the air and equal to the equivalent
air speed corrected for air density. At sea level, ISA, the true airspeed
is equal to the equivalent airspeed.

GROUND SPEED – GS
It is the airplane speed in relation to the ground. It is the true airspeed
corrected for the wind speed.

TAKEOFF DECISION SPEED – V1

It is the maximum speed in the takeoff at which the pilot must take the
first action (e.g., apply brakes, reduce thrust) to stop the airplane
within the accelerate-stop distance. V1 also means the minimum speed
in the takeoff, following a failure of the critical engine at VEF, at which
the pilot can continue the takeoff and achieve the required height
above the takeoff surface within the takeoff distance.
AFM-2655

5-01 ANAC APPROVED

Page 2 code 01 REVISION 17
 TM

PHENOM 100
Airplane Flight Manual
Performance

STALL SPEED – VS
It is the minimum steady flight speed at which the airplane is
controllable.

ROTATION SPEED – VR
It is the speed at which the pilot starts to rotate the airplane during the
takeoff ground run.

LIFT-OFF SPEED – VLOF

It is the speed at which the airplane first becomes airborne during
takeoff.

FIRST SEGMENT
Starts at 35 ft above the takeoff surface, at the end of the one-engine-
inoperative takeoff distance, and extends to the point where the
landing gear is fully retracted using a constant V2 speed and takeoff
flaps.

TAKEOFF SAFETY SPEED – V2

It is the target speed to be attained at 35 ft height above runway
surface, the critical engine having failed at VEF.

SECOND SEGMENT
Extends from the end of the first segment up to the level-off height,
with takeoff flaps, gear up, and constant V2 speed.

LEVEL-OFF HEIGHT
It is the height or altitude where the airplane is leveled for acceleration
and flap retraction.

MINIMUM LEVEL-OFF HEIGHT

It is defined by regulations as 400 ft AGL. The user can define higher
levels.
AFM-2655

ANAC APPROVED 5-01

ORIGINAL code 01 Page 3
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LEVEL-OFF HEIGHT

It is the height where the takeoff thrust time limit occurs at the end of
the final segment.

EXTENDED SECOND SEGMENT

It is an extension of the second takeoff climb segment, above the
maximum level off height, to improve obstacle clearance performance.

THIRD (OR ACCELERATION) SEGMENT

Extends from the end of the second segment, at the level-off height,
up to a point where the airplane is accelerated to final segment speed
(VFS) while retracting flaps.

FINAL SEGMENT SPEED – VFS

It is the speed to be achieved at the end of the acceleration segment
and start of the final segment of the takeoff flight path, with one engine
inoperative, landing gear retracted, and flaps retracted.

FINAL SEGMENT
Extends from the end of the third segment to a gross height at least at
1500 ft AGL, with flaps up and at final segment speed (VFS).
AFM-2655

5-01 ANAC APPROVED

Page 4 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

NOISE LEVELS
AIRPLANES PRE-MOD. SB 500-00-0009
The following Effective Perceived Noise Levels (EPNL's) comply with
the Chapter 4 noise limits set forth in RBHA 36, equivalent to ICAO
Annex 16, Volume 1, Appendix 2, Amendment 8, effective July 11,
2005.

NOISE LEVEL IN EPNdb

CONDITION
Noise
Level
Engine Flyover Lateral Approach
Model
Maximum
89.0 94.0 98.0
Allowable

PW617F-E Actual 70.4 81.4 86.1

The noise levels for EMB-500 equipped with two Pratt & Whitney
PW617F-E engines, were established as follows:
í Flyover: at maximum takeoff weight, flap setting 1, using thrust
power cutback and V2 + 20 KIAS;
í Lateral: at maximum takeoff weight, flap setting 1 and with all
engines at maximum takeoff power setting;
í Approach: at maximum landing weight, 3° glide slope,
VREF + 10 KIAS and flap setting FULL.
No determination has been made by the Airworthiness Authority that
the noise levels of this airplane are or should be acceptable or
unacceptable for operation at, into, or out of any airport.
AFM-2655

ANAC APPROVED 5-01

REVISION 16 code 01 Page 5
 TM

PHENOM 100
Airplane Flight Manual
Performance

AIRPLANES POST-MOD. SB 500-00-0009

NOTE: Applicable to airplanes Post-Mod. SB 500-00-0009 or with an
equivalent modification factory incorporated.
The following Effective Perceived Noise Levels (EPNL's) comply with
RBAC 36, corresponding to Title 14 CFR Part 36, Appendix B, Stage 4
maximum noise level requirements and were obtained by analysis of
approved data from noise tests conducted under the provisions of
Part 36, Amendment 36-28. The noise measurement and evaluation
procedures used to obtain these noise levels are considered by ANAC
to be equivalent to the Chapter 4 noise level required by the
International Civil Aviation Organization (ICAO) in Annex 16, Volume I,
Appendix 2, Amendment 7, effective March 21, 2002.

NOISE LEVEL IN EPNdb

CONDITION
Noise
Level
Engine Flyover Lateral Approach
Model
Maximum
89.0 94.0 98.0
Allowable

PW617F-E Actual 70.8 81.4 86.1

The noise levels for EMB-500 equipped with two Pratt & Whitney
PW617F-E engines, were established as follows:
í Flyover: at maximum takeoff weight, flap setting 1, using thrust
power cutback and V2 + 20 KIAS;
í Lateral: at maximum takeoff weight, flap setting 1 and with all
engines at maximum takeoff power setting;
í Approach: at maximum landing weight, 3° glide slope,
VREF + 10 KIAS and flap setting FULL.
No determination has been made by the Airworthiness Authority that
the noise levels of this airplane are or should be acceptable or
unacceptable for operation at, into, or out of any airport.
AFM-2655

5-01 ANAC APPROVED

Page 6 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SOFTWARE PRESENTATION
OPERA is the Optimized Performance Analyzer software certified to
provide takeoff, landing and enroute approved performance data.
The OPERA replaces or supplements portions of the paper AFM, and
is an ANAC approved source for that AFM information. As paper AFM
performance information is generally based on a simplified analysis, it
may show performance data more conservative than OPERA. Any
modification to the ANAC approved OPERA software application, or
subsequent alteration to the generated output, will cancel the
airworthiness approval of the information, unless this change was
approved by the appropriate airworthiness authority. This statement
applies regardless of any approval notation printed on a generated
output.
Performance wise, OPERA offers applicable aerodynamic and
systems calculation options, to be selected according to the airplane
specific configuration.
The OPERA installer incorporates the media identification, which will
be displayed on the screen after installation and must be
crosschecked with the AFM OPERA configuration.
The OPERA version is composed of two numbers. The second
number identifies different databases. If there is an update only to the
databases, only the second number moves on. When the OPERA is
revised with changes on the Main Computer Interface or Calculation
Modules the version moves on (e.g.: version 4.1 evolves to version
5.1).
Any time OPERA is revised, a new installer media is issued and the
AFM is revised accordingly. After approval, both are provided to
operators. Previous installer remains valid only if listed at Valid
Versions table.
A dedicated User's Guide is also issued, as a separate document,
providing detailed information on software usage aspects. In addition,
the OPERA interface provides a Help feature with useful on line
information.
If not mentioned, the latest Software Configuration Media incorporates
all capabilities of the previous media.
®
The OPERA has been tested only on WINDOWS XP and
®
WINDOWS 7 Operational Systems.
AFM-2655

ANAC APPROVED 5-02

REVISION 12 code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

SOFTWARE CONFIGURATION

OP500AN617FE version 10.2

The software OP500AN617FE version 10.2 allows performance
calculations for airplanes with the following configuration:
í PHENOM 100.
í PW617F-E engines.
í FADEC Software 5.3 and on.
í Placard "Standard Takeoff Thrust OPERA Type B".

WARNING: x OPERA VERSION MUST BE IN ACCORDANCE WITH

AIRPLANE CONFIGURATION.
x REFER TO SUPPLEMENT 2 OR 6 FOR OTHER
AIRPLANES CONFIGURATIONS ACCORDING TO
VALID VERSIONS TABLE.
x VERSIONS NOT PRESENTED IN AFM ARE
AUTOMATICALLY CANCELLED AND MUST NOT BE
USED.
x FOR AIRPLANES PRE-MOD. SB 500-27-0001,
OPERA LANDING PERFORMANCE WITH ICE
PROTECTION OFF MUST NOT BE USED. REFER TO
EAD 2009-02-04.

CAUTION: AFTER USING THE AIRPORT ANALYSIS OPTION,

CHECK THE MINIMUM REQUIRED RUNWAY LENGTH
FOR TAKEOFF BY INPUTING THE ACTUAL TAKEOFF
WEIGHT IN THE GIVEN WEIGHT OPTION.

NOTE: OPERA software provides guidance information when

operating from contaminated runways.
AFM-2655

5-02 ANAC APPROVED

Page 2 code 01 REVISION 17
 TM

PHENOM 100
Airplane Flight Manual
Performance

VALID VERSIONS
The table below presents valid OPERA versions.

AIRPLANE
VALID
SERIAL AFM
AIRPLANE CONFIGURATION OPERA
NUMBER LOCATION
VERSIONS
500:
00005 thru
00118; 00121; Supplement
Pre-Mod. SB 500-27-0003. 10.0
00123 thru 2
00131; 00133;
00134; 00136;
00137;
00139 thru
00144; 00148; Post-Mod. SB 500-27-0003.
00149;
00152 thru
00154
00120; 00122;
00132; 00135;
Supplement
00138; 10.1
6
00145 thru
ALL
00147;
00150; 00151;
00155 thru
00216

Enhanced Takeoff Thrust

OPERA Type A
cockpit placard installed.
00218 and on
Standard Takeoff Thrust
OPERA Type B Section 5-02 10.2
cockpit placard installed.
AFM-2655

ANAC APPROVED 5-02

REVISION 17 code 01 Page 3
 TM

PHENOM 100
Airplane Flight Manual
Performance

INTENTIONALLY BLANK

AFM-2655

5-02 ANAC APPROVED

Page 4 code 01 REVISION 5
 TM

PHENOM 100
Airplane Flight Manual
Performance

POSITION ERROR CORRECTIONS

The corrections to be applied to indicated airspeed or altitude in order
to eliminate the effect of location of the static port on instrument
readings are shown in the Airspeed Position Error Correction charts
and in the Altitude Position Error Correction charts. No position error
correction is required for ADS 1 and ADS 2, as their indication is
already corrected. The position correction charts are only applicable
for ADS Stand-by for flaps 0 (zero) according to the following
conditions:
- Airspeed Position Error Correction for landing gear down and up.
- Altitude Position Error Correction for landing gear down and up.

AIRSPEED POSITION ERROR CORRECTION CHART

USE
Enter the chart with indicated airspeed, considering the appropriate
configuration, to read airspeed correction. The calibrated airspeed will
be the sum of the indicated airspeed and airspeed correction.

EXAMPLE
Given:
ADS Stand-by
Indicated Airspeed.............................................. 270 KIAS
Landing Gear...................................................... UP
Flaps ................................................................... ZERO
Altitude................................................................ SEA LEVEL

Determine:
Airspeed Correction............................................ -2.0
Calibrated Airspeed ............................................ 268 KCAS
AFM-2655

ANAC APPROVED 5-05

ORIGINAL code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

AIRSPEED POSITION ERROR CORRECTION

ADS STAND-BY
LANDING GEAR DOWN - FLAPS ZERO

ALL WEIGHTS

-1
CORRECTION - kt

-2

ALL ALTITUDES

-3

-4
500ANAC07 -25SEP2008

-5
80 100 120 140 160 180 200 220 240 260 280 300 320

INDICATED AIRSPEED - kt
AFM-2655

5-05 ANAC APPROVED

Page 2 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

AIRSPEED POSITION ERROR CORRECTION

ADS STAND-BY
LANDING GEAR UP - FLAPS ZERO

5
ALL WEIGHTS

2
CORRECTION - kt

1
40000 ft

30000 ft
0

20000 ft

-1
10000 ft

SEA LEVEL
-2

-3

-4
500ANAC08-25SEP2008

-5
80 100 120 140 160 180 200 220 240 260 280 300 320

INDICATED AIRSPEED - kt
AFM-2655

ANAC APPROVED 5-05

ORIGINAL code 01 Page 3
 TM

PHENOM 100
Airplane Flight Manual
Performance

ALTITUDE POSITION ERROR CORRECTION CHARTS

USE
Enter the appropriate chart with indicated airspeed, the indicated
pressure altitude considering the appropriate airplane configuration to
read the altimetric correction. The true pressure altitude will be the
indicated pressure altitude plus the altimetric correction.

EXAMPLE
Given:
ADS Stand-by
Indicated Airspeed .............................................. 190 KIAS
Landing Gear ...................................................... UP
Flaps ...................................................................ZERO
Altitude ................................................................ 30000 ft

Determine:
Altimetric Correction ........................................... 20 ft
True Pressure Altitude ........................................ 30020 ft

AFM-2655

5-05 ANAC APPROVED

Page 4 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

ALTITUDE POSITION ERROR CORRECTION

ADS STAND-BY
LANDING GEAR DOWN - FLAPS ZERO

50

ALL WEIGHTS
40

30

20

10

-10
CORRECTION - ft

-20

-30

-40

-50

-60

-70 ALL ALTITUDES

-80

-90
500ANAC09 -25SEP2008

-100
80 100 120 140 160 180 200 220 240 260 280 300 320

INDICATED AIRSPEED - kt
AFM-2655

ANAC APPROVED 5-05

ORIGINAL code 01 Page 5
 TM

PHENOM 100
Airplane Flight Manual
Performance

ALTITUDE POSITION ERROR CORRECTION

ADS STAND-BY
LANDING GEAR UP - FLAPS ZERO

140 ALL WEIGHTS

120

100

80

60
CORRECTION - ft

40000 ft
40

20

30000 ft
0

-20

20000 ft
-40
10000 ft
AND
-60 BELOW

-80
500ANAC10 -25SEP2008

-100
80 100 120 140 160 180 200 220 240 260 280 300 320

INDICATED AIRSPEED - kt
AFM-2655

5-05 ANAC APPROVED

Page 6 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

STALL SPEED
NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
This table presents the stall speed value according to the airplane
bank angle for the MTOW with landing gear and flap up.

STALL SPEEDS (KIAS)

MTOW BANK ANGLE

(kg) 0° 15° 30° 45° 60°
4750 100 102 108 119 141
4800 101 103 108 120 142

This table presents the stall speed values according to the airplane
bank angle for the MLW with landing gear down and landing flap 3 or
FULL.

STALL SPEEDS (KIAS)

MLW BANK ANGLE

FLAP
(kg) 0° 15° 30° 45° 60°
3 81 82 87 96 115
4430
FULL 77 79 83 92 109
3 82 83 88 97 116
4480
FULL 78 80 84 93 111
AFM-2655

ANAC APPROVED 5-08

REVISION 16 code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

INTENTIONALLY BLANK

AFM-2655

5-08 ANAC APPROVED

Page 2 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

THRUST SETTING TABLES

Thrust setting table is presented for various pressure altitudes and
static air temperatures, with engine bleed open, and anti-ice on or off.
The following tables present Takeoff N1 setting for TO/GA mode on
PW617F-E engines.
AFM-2655

ANAC APPROVED 5-10

ORIGINAL code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

INTENTIONALLY BLANK

AFM-2655

5-10 ANAC APPROVED

Page 2 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

N1 FOR T/O MODE

ANTI-ICE OFF
AIRSPEED: 0 KIAS
PW617F-E ENGINES

Pressure
Altitude
Static Air Temperature (°C)
(ft) -40 -35 -30 -25 -20 -15 -10 -5 0
-1000 78.3 79.1 80.0 80.8 81.6 82.4 83.2 84.0 84.8
0 79.5 80.3 81.2 82.0 82.9 83.7 84.5 85.4 86.2
1000 79.6 80.5 81.3 82.2 83.0 83.8 84.7 85.5 86.3
2000 79.7 80.6 81.4 82.3 83.1 84.0 84.8 85.6 86.4
3000 79.7 80.6 81.4 82.2 83.1 83.9 84.8 85.6 86.4
4000 79.9 80.7 81.6 82.4 83.3 84.1 85.0 85.8 86.6
5000 79.9 80.7 81.6 82.4 83.3 84.1 85.0 85.8 86.7
6000 80.0 80.8 81.7 82.5 83.4 84.2 85.1 85.9 86.8
7000 80.1 81.0 81.8 82.7 83.5 84.4 85.2 86.1 86.9
8000 80.3 81.2 82.0 82.9 83.7 84.6 85.4 86.3 87.1
9000 80.4 81.3 82.1 83.0 83.8 84.7 85.5 86.4 87.2
10000 80.6 81.5 82.3 83.2 84.0 84.9 85.7 86.6 87.4

Pressure
Altitude
Static Air Temperature (°C)
(ft) 5 10 15 20 25 30 35 40 45
-1000 85.6 86.3 87.1 87.8 88.6 88.7 87.9 87.0 86.0
0 86.9 87.7 88.5 89.2 89.8 89.0 88.0 87.0 86.0
1000 87.1 87.8 88.6 89.4 89.8 88.8 87.8 86.8 85.8
2000 87.2 88.0 88.8 89.5 89.6 88.7 87.7 86.6 85.6
3000 87.3 88.0 88.8 89.6 89.4 88.4 87.3 86.3 -
4000 87.4 88.2 89.0 89.6 89.2 88.2 87.1 86.2 -
5000 87.5 88.3 89.1 89.7 88.9 87.9 86.8 85.8 -
6000 87.6 88.4 89.2 89.6 88.7 87.6 86.6 - -
7000 87.8 88.5 89.3 89.4 88.5 87.4 86.4 - -
8000 87.9 88.7 89.5 89.4 88.3 87.2 - - -
9000 88.1 88.9 89.7 89.2 88.1 86.9 - - -
10000 88.3 89.1 89.8 89.0 87.8 86.6 - - -
AFM-2655

ANAC APPROVED 5-10

ORIGINAL code 01 Page 3
 TM

PHENOM 100
Airplane Flight Manual
Performance

N1 FOR T/O MODE

ANTI-ICE ON
AIRSPEED: 0 KIAS
PW617F-E ENGINES

Pressure
Altitude
Static Air Temperature (°C)
(ft) -40 -35 -30 -25 -20 -15
-1000 78.3 79.1 80.0 80.8 81.6 82.4
0 79.5 80.4 81.2 82.1 82.9 83.7
1000 79.6 80.5 81.3 82.2 83.0 83.8
2000 79.7 80.6 81.4 82.2 83.1 83.9
3000 79.7 80.6 81.4 82.3 83.1 84.0
4000 79.9 80.7 81.6 82.4 83.2 84.1
5000 79.9 80.7 81.6 82.4 83.3 84.1
6000 80.0 80.8 81.7 82.5 83.4 84.2
7000 80.1 81.0 81.8 82.7 83.5 84.4
8000 80.3 81.2 82.0 82.9 83.7 84.6
9000 80.5 81.3 82.2 83.0 83.9 84.7
10000 80.6 81.5 82.3 83.2 84.0 84.9

Pressure
Altitude
Static Air Temperature (°C)
(ft) -10 -5 0 5 10
-1000 83.2 84.0 84.8 85.6 86.3
0 84.6 85.4 86.2 86.9 87.7
1000 84.7 85.5 86.3 87.1 87.9
2000 84.8 85.6 86.4 87.2 88.0
3000 84.8 85.6 86.5 87.3 88.0
4000 84.9 85.8 86.6 87.4 88.2
5000 85.0 85.8 86.7 87.5 88.3
6000 85.1 85.9 86.8 87.6 88.4
7000 85.2 86.1 86.9 87.8 88.5
8000 85.4 86.3 87.1 87.9 88.7
9000 85.6 86.4 87.3 88.1 88.9
10000 85.7 86.6 87.4 88.3 89.1
AFM-2655

5-10 ANAC APPROVED

Page 4 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

TAKEOFF DATA

TAKEOFF TECHNIQUE
The takeoff performance data in this manual is based on the following
conditions:
 Thrust lever set to TO/GA position with the airplane stopped and
brakes applied;
 Brakes released after N1 stabilized;
 When VR is attained the airplane is rotated to appropriate pitch
angle according to flap selection until 35 ft or until reaching V2;
 Pitch angle adjusted as required to maintain V2;
 Landing gear retracted when a positive rate of climb is
established.

SIMPLIFIED TAKEOFF ANALYSIS TABLES

Simplified Takeoff Analysis tables are presented for a set of pressure
altitudes, temperatures and minimum required runway lengths for the
conditions below:
 Takeoff flap 1 or 2;
 Ice Protection OFF or ON (WINGSTAB+ENG 1/2);
 ATR OFF;
 Given weight calculation type;
 Dry runway;
 No clearway;
 No stopway;
 Zero slope;
 Zero wind;
 Minimum level-off height (400 ft);
 Balanced V1;
 No obstacles (analysis assumption).

(Continues on the next page)

AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

(Continued from the previous page)

NOTE: - ATR OFF does not ensure a conservative performance

when compared to ATR ON due to VMCG characteristics.
- The Limited Weight columns represent the weight limited by
climb or brake energy for the given temperature. Always
check the structural weight limitation on Section 2.
- Refer to the OPERA software configuration to check if any
special setting is required in addition to the choices above.

EXAMPLE
Given:
Airplane Takeoff Weight ..................................... 4000 kg
Airport Pressure Altitude..................................... 2000 ft
Outside Air Temperature .................................... 20°C
Ice Protection ...................................................... OFF
Flap ..................................................................... 2
Determine:
Minimum Required Runway Length ................... 846 m
V1 ........................................................................ 87 KIAS
VR ........................................................................ 87 KIAS
V2 ........................................................................ 91 KIAS
VFS ....................................................................... 120 KIAS
Limited Weight ....................................................4431 kg
AFM-2655

5-15 ANAC APPROVED

Page 2 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: -1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 614 621 686 759 833 910 988 4800

91/93/99 91/95/101 95/98/103 99/102/106 103/105/108 107/107/111 110/110/113
-35 625 632 698 772 848 925 1005 4800
91/93/99 91/95/101 95/98/103 99/102/106 103/105/108 107/107/111 110/110/113
-30 636 643 710 785 862 941 1022 4800
91/93/99 91/95/101 95/98/103 99/102/106 103/105/108 107/107/111 110/110/113
-25 647 655 721 798 876 956 1039 4800
91/93/99 91/95/101 95/98/103 99/102/106 103/105/108 106/107/111 110/110/113
-20 658 666 733 811 890 972 1056 4800
91/93/99 91/95/101 95/98/103 99/102/106 103/105/108 106/107/111 110/110/113
-15 669 677 744 823 904 987 1073 4800
91/93/99 91/95/101 94/98/103 99/102/106 103/105/108 106/107/111 109/110/113
-10 680 688 756 836 919 1003 1090 4800
91/93/99 90/95/101 94/98/103 99/102/106 103/105/108 106/107/111 109/110/113
-5 690 699 768 849 933 1019 1107 4800
91/93/99 90/95/101 94/98/103 99/102/106 103/105/108 106/107/111 109/110/113
0 701 710 779 862 948 1035 1125 4800
91/93/99 90/95/101 94/98/103 99/102/106 102/105/108 106/107/111 109/110/113
5 712 721 791 876 962 1051 1142 4800
91/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
10 723 732 803 889 977 1067 1160 4800
91/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
15 732 742 817 904 993 1085 1179 4800
90/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
20 742 752 831 920 1011 1104 1200 4800
90/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
25 752 762 845 935 1028 1123 1220 4800
90/92/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
30 752 796 887 981 1077 1175 1277 4800
89/92/98 91/95/101 95/99/103 99/102/106 103/105/108 107/108/111 110/110/113
35 766 860 956 1054 1154 1259 1367 4800
88/93/98 93/96/101 97/99/103 101/103/106 105/106/108 108/108/111 111/111/113
40 833 931 1032 1135 1243 1356 1512 4800
90/93/98 95/97/101 99/100/103 102/103/106 106/106/108 109/109/111 111/111/113
45 899 1002 1108 1219 1341 1530 1770 4800
92/94/98 96/97/101 100/101/103 104/104/106 107/107/108 109/109/111 112/112/113
50 968 1077 1193 1320 1533 1780 - 4640
94/95/98 98/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
51 982 1093 1213 1341 1583 - - 4591
94/95/98 98/98/101 101/101/103 104/104/106 107/107/108 - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 3
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 0 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 634 641 706 781 857 936 1017 4800

91/93/99 91/95/101 95/98/103 99/102/106 103/105/108 107/107/111 110/110/113
-35 645 653 718 794 872 952 1034 4800
91/93/99 91/95/101 95/98/103 99/102/106 103/105/108 106/107/111 110/110/113
-30 657 664 729 807 886 968 1051 4800
91/93/99 91/95/101 94/98/103 99/102/106 103/105/108 106/107/111 110/110/113
-25 668 676 741 820 901 983 1069 4800
91/93/99 91/95/101 94/98/103 99/102/106 103/105/108 106/107/111 109/110/113
-20 679 687 753 833 915 1000 1086 4800
91/93/99 91/95/101 94/98/103 99/102/106 103/105/108 106/107/111 109/110/113
-15 690 699 765 847 930 1016 1104 4800
91/93/99 91/95/101 94/98/103 99/102/106 103/105/108 106/107/111 109/110/113
-10 701 710 778 861 946 1033 1122 4800
91/93/99 90/95/101 94/98/103 99/102/106 102/105/108 106/107/111 109/110/113
-5 713 721 790 875 961 1050 1141 4800
91/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
0 723 732 803 889 976 1067 1159 4800
91/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
5 734 743 815 903 992 1084 1178 4800
91/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
10 745 755 829 917 1008 1101 1197 4800
91/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
15 755 765 843 934 1026 1121 1218 4800
90/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
20 765 775 858 950 1044 1140 1239 4800
90/93/99 90/95/101 94/98/103 98/102/106 102/105/108 106/107/111 109/110/113
25 775 785 877 970 1065 1162 1263 4800
90/92/99 90/95/101 94/99/103 99/102/106 102/105/108 106/107/111 109/110/113
30 762 852 948 1047 1148 1253 1361 4800
87/92/98 92/96/101 96/99/103 100/102/106 104/105/108 107/108/111 110/111/113
35 827 926 1027 1131 1239 1350 1468 4800
89/93/98 94/97/101 98/100/103 102/103/106 105/106/108 108/109/111 111/111/113
40 897 1001 1108 1218 1333 1478 1720 4800
91/94/98 96/97/101 100/101/103 103/104/106 106/106/108 109/109/111 112/112/113
45 968 1077 1191 1315 1492 1742 - 4712
93/94/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
50 1041 1158 1289 1486 1741 - - 4469
94/95/98 98/98/101 102/102/103 105/105/106 107/107/108 - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 4 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 639 683 761 840 920 1004 1091 4800

89/92/98 91/96/101 96/99/103 100/102/106 104/105/108 107/108/111 110/110/113
-35 650 694 773 853 936 1021 1109 4800
89/92/98 91/96/101 96/99/103 100/102/106 104/105/108 107/108/111 110/110/113
-30 662 705 785 867 952 1038 1127 4800
89/92/98 91/96/101 96/99/103 100/102/106 104/105/108 107/108/111 110/110/113
-25 673 716 798 882 967 1055 1146 4800
89/92/98 91/96/101 96/99/103 100/102/106 104/105/108 107/108/111 110/110/113
-20 684 728 811 896 983 1073 1165 4800
89/92/98 91/96/101 96/99/103 100/102/106 104/105/108 107/108/111 110/110/113
-15 696 740 825 911 999 1090 1184 4800
89/92/98 91/96/101 96/99/103 100/102/106 104/105/108 107/108/111 110/110/113
-10 708 752 838 926 1015 1108 1203 4800
89/92/98 91/96/101 96/99/103 100/102/106 103/105/108 107/108/111 110/110/113
-5 719 764 851 940 1032 1126 1223 4800
89/92/98 91/96/101 95/99/103 100/102/106 103/105/108 107/108/111 110/110/113
0 730 776 865 955 1048 1144 1242 4800
89/92/98 91/96/101 95/99/103 100/102/106 103/105/108 107/108/111 110/110/113
5 741 788 878 970 1065 1162 1262 4800
89/92/98 91/96/101 95/99/103 100/102/106 103/105/108 107/108/111 110/110/113
10 751 801 893 987 1083 1182 1284 4800
89/92/98 91/96/101 95/99/103 99/102/106 103/105/108 107/108/111 110/110/113
15 762 815 908 1004 1101 1202 1306 4800
89/92/98 91/96/101 95/99/103 99/102/106 103/105/108 107/108/111 110/110/113
20 773 829 924 1021 1120 1222 1328 4800
88/92/98 91/96/101 95/99/103 99/102/106 103/105/108 107/108/111 110/110/113
25 780 858 955 1054 1156 1261 1370 4800
88/92/98 91/96/101 96/99/103 100/102/106 104/105/108 107/108/111 110/111/113
30 829 929 1031 1136 1244 1356 1472 4800
89/93/98 93/96/101 98/100/103 101/103/106 105/106/108 108/109/111 111/111/113
35 900 1005 1113 1224 1340 1464 1696 4800
91/94/98 95/97/101 99/100/103 103/103/106 106/106/108 109/109/111 112/112/113
40 972 1083 1197 1317 1466 1718 - 4768
93/94/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
45 1047 1165 1292 1464 1722 - - 4516
94/95/98 98/98/101 102/102/103 105/105/106 107/107/108 - -
48 1094 1220 1357 1612 - - - 4380
95/95/98 99/99/101 102/102/103 105/105/106 - - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 5
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 2000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 656 736 818 902 988 1077 1177 4800

88/93/98 93/96/101 97/99/103 101/102/106 105/105/108 108/108/111 111/111/113
-35 667 749 832 917 1005 1096 1195 4800
88/93/98 93/96/101 97/99/103 101/102/106 105/105/108 108/108/111 111/111/113
-30 678 761 846 933 1022 1114 1214 4800
88/93/98 93/96/101 97/99/103 101/102/106 105/105/108 108/108/111 111/111/113
-25 689 774 860 948 1039 1133 1232 4800
88/93/98 93/96/101 97/99/103 101/102/106 105/105/108 108/108/111 111/111/113
-20 700 786 874 964 1056 1151 1250 4800
88/93/98 93/96/101 97/99/103 101/102/106 105/105/108 108/108/111 111/111/113
-15 711 799 888 979 1073 1170 1270 4800
88/93/98 92/96/101 97/99/103 101/102/106 104/105/108 108/108/111 111/111/113
-10 722 811 902 995 1090 1188 1291 4800
88/93/98 92/96/101 97/99/103 101/102/106 104/105/108 108/108/111 111/111/113
-5 733 824 916 1010 1107 1207 1311 4800
88/93/98 92/96/101 97/99/103 101/102/106 104/105/108 108/108/111 111/111/113
0 745 836 930 1026 1124 1226 1332 4800
88/93/98 92/96/101 97/99/103 101/102/106 104/105/108 107/108/111 110/111/113
5 757 850 945 1043 1143 1247 1354 4800
88/93/98 92/96/101 97/99/103 101/102/106 104/105/108 107/108/111 110/111/113
10 769 864 961 1060 1162 1268 1377 4800
88/93/98 92/96/101 97/99/103 101/102/106 104/105/108 107/108/111 110/111/113
15 782 879 978 1078 1182 1289 1400 4800
88/93/98 92/96/101 97/99/103 101/102/106 104/105/108 107/108/111 110/111/113
20 796 894 994 1096 1202 1311 1424 4800
88/93/98 92/96/101 97/99/103 100/102/106 104/105/108 107/108/111 110/111/113
25 837 938 1042 1148 1258 1372 1490 4800
89/93/98 93/96/101 97/100/103 101/103/106 105/106/108 108/108/111 111/111/113
30 903 1009 1118 1230 1346 1468 1665 4800
90/94/98 95/97/101 99/100/103 102/103/106 106/106/108 109/109/111 112/112/113
35 977 1088 1204 1324 1452 1694 1947 4800
92/94/98 96/98/101 100/101/103 104/104/106 107/107/108 110/110/111 112/112/113
40 1054 1173 1297 1445 1709 - - 4554
94/95/98 98/98/101 101/101/103 105/105/106 107/107/108 - -
45 1136 1267 1435 1705 - - - 4315
95/95/98 99/99/101 102/102/103 105/105/106 - - -
46 1153 1289 1488 1758 - - - 4267
95/96/98 99/99/101 102/102/103 105/105/106 - - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 6 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 3000 ft
TAKEOFF WEIGHT (kg)
TEMP MINIMUM REQUIRED RUNWAY LENGTH (m)
(ºC) V1/VR/V2 (KIAS)

3600 3800 4000 4200 4400 4600 4800 LIMITED

WEIGHT

-40 709 794 880 969 1061 1162 1268 4800

90/93/98 94/96/101 98/100/103 102/103/106 106/106/108 109/109/111 111/111/113
-35 721 807 895 986 1079 1181 1288 4800
89/93/98 94/96/101 98/100/103 102/103/106 106/106/108 109/109/111 111/111/113
-30 733 821 910 1002 1097 1199 1309 4800
89/93/98 94/96/101 98/100/103 102/103/106 106/106/108 109/109/111 111/111/113
-25 745 834 926 1019 1116 1217 1329 4800
89/93/98 94/96/101 98/100/103 102/103/106 105/106/108 109/109/111 111/111/113
-20 757 848 941 1036 1134 1236 1348 4800
89/93/98 94/96/101 98/100/103 102/103/106 105/106/108 109/109/111 111/111/113
-15 769 861 956 1052 1152 1256 1368 4800
89/93/98 94/96/101 98/100/103 102/103/106 105/106/108 108/109/111 111/111/113
-10 781 875 971 1069 1171 1276 1388 4800
89/93/98 94/96/101 98/100/103 102/103/106 105/106/108 108/109/111 111/111/113
-5 793 888 986 1086 1189 1296 1408 4800
89/93/98 94/96/101 98/100/103 102/103/106 105/106/108 108/109/111 111/111/113
0 805 901 1001 1102 1207 1316 1429 4800
89/93/98 93/96/101 98/100/103 102/103/106 105/106/108 108/109/111 111/111/113
5 818 916 1017 1120 1227 1338 1453 4800
89/93/98 93/96/101 98/100/103 101/103/106 105/106/108 108/109/111 111/111/113
10 831 931 1034 1139 1248 1360 1477 4800
89/93/98 93/96/101 98/100/103 101/103/106 105/106/108 108/109/111 111/111/113
15 845 947 1051 1158 1269 1383 1502 4800
89/93/98 93/96/101 98/100/103 101/103/106 105/106/108 108/109/111 111/111/113
20 863 966 1072 1181 1294 1411 1533 4800
89/93/98 93/97/101 98/100/103 101/103/106 105/106/108 108/109/111 111/111/113
25 910 1017 1127 1240 1358 1480 1647 4800
90/94/98 94/97/101 99/100/103 102/103/106 106/106/108 109/109/111 112/112/113
30 982 1095 1211 1332 1458 1664 1920 4800
92/94/98 96/98/101 100/101/103 103/104/106 107/107/108 109/109/111 112/112/113
35 1061 1180 1305 1437 1681 1946 - 4616
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
40 1144 1272 1415 1690 - - - 4356
95/95/98 99/99/101 102/102/103 105/105/106 - - -
44 1210 1353 1609 - - - - 4180
96/96/98 99/99/101 102/102/103 - - - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 7
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 4000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 762 851 943 1037 1139 1248 1398 4800

91/94/98 95/97/101 99/100/103 103/103/106 106/106/108 109/109/111 112/112/113
-35 775 866 959 1055 1157 1268 1419 4800
91/93/98 95/97/101 99/100/103 103/103/106 106/106/108 109/109/111 112/112/113
-30 788 880 975 1073 1175 1288 1439 4800
91/93/98 95/97/101 99/100/103 103/103/106 106/106/108 109/109/111 112/112/113
-25 801 895 992 1091 1194 1307 1459 4800
91/93/98 95/97/101 99/100/103 103/103/106 106/106/108 109/109/111 112/112/113
-20 814 910 1008 1109 1214 1327 1479 4800
90/93/98 95/97/101 99/100/103 103/103/106 106/106/108 109/109/111 112/112/113
-15 827 924 1024 1127 1233 1346 1499 4800
90/93/98 95/97/101 99/100/103 103/103/106 106/106/108 109/109/111 112/112/113
-10 840 939 1040 1145 1253 1366 1519 4800
90/93/98 95/97/101 99/100/103 102/103/106 106/106/108 109/109/111 112/112/113
-5 853 953 1057 1163 1273 1387 1539 4800
90/93/98 95/97/101 99/100/103 102/103/106 106/106/108 109/109/111 112/112/113
0 866 968 1073 1180 1292 1408 1559 4800
90/93/98 94/97/101 99/100/103 102/103/106 106/106/108 109/109/111 112/112/113
5 879 983 1090 1199 1313 1431 1584 4800
90/93/98 94/97/101 99/100/103 102/103/106 106/106/108 109/109/111 112/112/113
10 894 999 1108 1220 1335 1456 1612 4800
90/93/98 94/97/101 98/100/103 102/103/106 106/106/108 109/109/111 112/112/113
15 909 1016 1126 1240 1357 1480 1640 4800
90/93/98 94/97/101 98/100/103 102/103/106 106/106/108 109/109/111 112/112/113
20 929 1038 1150 1266 1387 1512 1692 4800
90/94/98 94/97/101 99/100/103 102/103/106 106/106/108 109/109/111 112/112/113
25 985 1099 1216 1338 1465 1635 1894 4800
91/94/98 96/97/101 99/101/103 103/104/106 106/107/108 109/109/111 112/112/113
30 1063 1184 1309 1439 1646 1913 - 4681
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
35 1148 1277 1414 1656 1932 - - 4418
94/95/98 98/99/101 102/102/103 105/105/106 108/108/108 - -
40 1235 1379 1639 - - - - 4182
96/96/98 99/99/101 102/102/103 - - - -
42 1272 1448 1740 - - - - 4095
96/96/98 99/99/101 103/103/103 - - - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 8 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 5000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 824 918 1016 1120 1233 1378 1601 4800

92/94/98 96/97/101 100/101/103 104/104/106 107/107/108 109/109/111 112/112/113
-35 838 934 1033 1137 1252 1398 1624 4800
92/94/98 96/97/101 100/101/103 104/104/106 107/107/108 109/109/111 112/112/113
-30 852 949 1051 1155 1271 1418 1647 4800
92/94/98 96/97/101 100/101/103 104/104/106 107/107/108 109/109/111 112/112/113
-25 866 965 1068 1174 1290 1438 1670 4800
92/94/98 96/97/101 100/101/103 104/104/106 107/107/108 109/109/111 112/112/113
-20 880 981 1085 1194 1309 1458 1694 4800
92/94/98 96/97/101 100/101/103 103/104/106 107/107/108 109/109/111 112/112/113
-15 894 997 1103 1213 1329 1477 1716 4800
92/94/98 96/97/101 100/101/103 103/104/106 107/107/108 109/109/111 112/112/113
-10 908 1012 1120 1232 1348 1497 1739 4800
91/94/98 96/97/101 100/101/103 103/104/106 107/107/108 109/109/111 112/112/113
-5 921 1028 1138 1251 1370 1516 1762 4800
91/94/98 96/97/101 100/101/103 103/104/106 106/107/108 109/109/111 112/112/113
0 935 1043 1155 1270 1391 1536 1784 4800
91/94/98 96/97/101 100/101/103 103/104/106 106/107/108 109/109/111 112/112/113
5 950 1060 1173 1291 1413 1558 1809 4800
91/94/98 95/97/101 99/101/103 103/104/106 106/107/108 109/109/111 112/112/113
10 965 1077 1192 1312 1436 1583 1838 4800
91/94/98 95/97/101 99/101/103 103/104/106 106/107/108 109/109/111 112/112/113
15 981 1094 1212 1333 1459 1609 1866 4800
91/94/98 95/97/101 99/101/103 103/104/106 106/107/108 109/109/111 112/112/113
20 1001 1117 1237 1361 1490 1655 1917 4800
91/94/98 95/97/101 99/101/103 103/104/106 106/107/108 109/109/111 112/112/113
25 1073 1194 1321 1453 1633 1902 - 4724
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
30 1157 1287 1423 1638 1916 - - 4464
94/95/98 98/99/101 102/102/103 105/105/106 108/108/108 - -
35 1251 1393 1642 1930 - - - 4206
95/96/98 99/99/101 102/102/103 105/105/106 - - -
40 1351 1606 - - - - - 3984
96/96/98 100/100/101 - - - - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 9
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 6000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 886 986 1090 1207 1333 1565 - 4765

93/94/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-35 901 1003 1109 1225 1352 1588 - 4770
93/94/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-30 916 1020 1127 1244 1371 1610 - 4774
93/94/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-25 931 1036 1146 1263 1390 1632 - 4778
93/94/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-20 946 1053 1165 1281 1410 1655 - 4783
93/94/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-15 961 1070 1184 1301 1431 1677 - 4787
93/94/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-10 976 1087 1202 1322 1451 1699 - 4791
92/94/98 97/98/101 100/101/103 104/104/106 107/107/108 110/110/111 -
-5 991 1104 1221 1342 1472 1721 - 4796
92/94/98 97/98/101 100/101/103 104/104/106 107/107/108 110/110/111 -
0 1006 1121 1240 1363 1492 1743 - 4800
92/94/98 96/98/101 100/101/103 104/104/106 107/107/108 110/110/111 -
5 1022 1138 1259 1385 1515 1767 2029 4800
92/94/98 96/98/101 100/101/103 104/104/106 107/107/108 110/110/111 112/112/113
10 1038 1157 1280 1407 1541 1796 - 4800
92/94/98 96/98/101 100/101/103 104/104/106 107/107/108 110/110/111 -
15 1055 1175 1301 1430 1566 1824 - 4797
92/94/98 96/98/101 100/101/103 104/104/106 107/107/108 110/110/111 -
20 1088 1212 1341 1474 1644 1918 - 4740
93/95/98 97/98/101 100/101/103 104/104/106 107/107/108 110/110/111 -
25 1166 1297 1434 1619 1901 - - 4510
94/95/98 98/98/101 101/102/103 105/105/106 107/107/108 - -
30 1259 1400 1619 1910 - - - 4254
95/96/98 99/99/101 102/102/103 105/105/106 - - -
35 1360 1597 1902 - - - - 4015
96/96/98 100/100/101 103/103/103 - - - -
38 1441 1751 - - - - - 3892
97/97/98 100/100/101 - - - - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 10 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 7000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 949 1056 1172 1296 1511 1752 - 4608

94/95/98 98/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-35 966 1074 1190 1316 1533 1778 - 4612
94/95/98 98/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-30 982 1092 1209 1337 1555 1803 - 4617
94/95/98 98/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-25 998 1111 1228 1357 1577 1828 - 4621
94/95/98 98/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-20 1015 1129 1248 1378 1598 1854 - 4625
93/95/98 98/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-15 1031 1147 1268 1398 1620 1879 - 4629
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-10 1047 1165 1288 1418 1642 1904 - 4633
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
-5 1063 1183 1308 1438 1663 1928 - 4637
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
0 1079 1201 1328 1460 1684 1953 - 4641
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
5 1096 1220 1349 1483 1708 1980 - 4643
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
10 1114 1241 1372 1508 1737 2012 - 4641
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
15 1133 1261 1394 1533 1765 2045 - 4637
93/95/98 97/98/101 101/101/103 104/104/106 107/107/108 110/110/111 -
20 1180 1313 1452 1618 1902 - - 4539
94/95/98 98/98/101 101/102/103 105/105/106 107/107/108 - -
25 1268 1409 1594 1888 - - - 4304
95/96/98 99/99/101 102/102/103 105/105/106 - - -
30 1369 1580 1888 - - - - 4055
96/96/98 99/99/101 103/103/103 - - - -
35 1530 1848 - - - - - 3844
97/97/98 100/100/101 - - - - -
36 1581 1901 - - - - - 3804
97/97/98 100/100/101 - - - - -

VFS 114 117 120 122 125 128 -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 11
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 8000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1018 1133 1261 1448 1698 - - 4455

95/95/98 99/99/101 102/102/103 105/105/106 108/108/108 - -
-35 1036 1151 1281 1469 1723 - - 4460
95/95/98 98/99/101 102/102/103 105/105/106 108/108/108 - -
-30 1053 1171 1301 1491 1748 - - 4464
94/95/98 98/99/101 102/102/103 105/105/106 108/108/108 - -
-25 1071 1191 1320 1512 1773 - - 4468
94/95/98 98/99/101 102/102/103 105/105/106 108/108/108 - -
-20 1089 1210 1340 1533 1798 - - 4472
94/95/98 98/99/101 102/102/103 105/105/106 108/108/108 - -
-15 1106 1230 1360 1554 1822 - - 4476
94/95/98 98/98/101 102/102/103 105/105/106 108/108/108 - -
-10 1124 1249 1381 1574 1846 - - 4480
94/95/98 98/98/101 102/102/103 105/105/106 108/108/108 - -
-5 1141 1269 1403 1595 1871 - - 4484
94/95/98 98/98/101 102/102/103 105/105/106 108/108/108 - -
0 1159 1288 1424 1615 1894 - - 4488
94/95/98 98/98/101 101/102/103 105/105/106 108/108/108 - -
5 1176 1308 1446 1636 1919 - - 4492
94/95/98 98/98/101 101/102/103 105/105/106 108/108/108 - -
10 1195 1330 1470 1663 1949 - - 4490
94/95/98 98/98/101 101/102/103 105/105/106 108/108/108 - -
15 1216 1353 1495 1692 1981 - - 4488
94/95/98 98/99/101 101/102/103 105/105/106 108/108/108 - -
20 1273 1415 1565 1855 - - - 4361
94/95/98 98/99/101 102/102/103 105/105/106 - - -
25 1374 1540 1852 - - - - 4115
96/96/98 99/99/101 103/103/103 - - - -
30 1510 1831 - - - - - 3885
97/97/98 100/100/101 - - - - -
34 1740 - - - - - - 3705
97/97/98 - - - - - -

VFS 114 117 120 123 125 - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 12 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 9000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1114 1244 1402 1669 - - - 4306

95/96/98 99/99/101 102/102/103 105/105/106 - - -
-35 1133 1264 1423 1693 - - - 4310
95/96/98 99/99/101 102/102/103 105/105/106 - - -
-30 1152 1283 1443 1717 - - - 4314
95/95/98 99/99/101 102/102/103 105/105/106 - - -
-25 1172 1303 1463 1741 - - - 4319
95/95/98 99/99/101 102/102/103 105/105/106 - - -
-20 1191 1323 1483 1764 - - - 4323
95/95/98 99/99/101 102/102/103 105/105/106 - - -
-15 1210 1345 1503 1788 - - - 4327
95/95/98 99/99/101 102/102/103 105/105/106 - - -
-10 1229 1366 1522 1811 - - - 4331
95/95/98 99/99/101 102/102/103 105/105/106 - - -
-5 1248 1388 1542 1834 - - - 4335
95/95/98 99/99/101 102/102/103 105/105/106 - - -
0 1267 1409 1561 1857 - - - 4339
95/95/98 98/99/101 102/102/103 105/105/106 - - -
5 1287 1431 1584 1883 - - - 4342
95/95/98 98/99/101 102/102/103 105/105/106 - - -
10 1308 1454 1611 1912 - - - 4341
94/95/98 98/99/101 102/102/103 105/105/106 - - -
15 1331 1480 1642 1947 - - - 4338
94/95/98 98/99/101 102/102/103 105/105/106 - - -
20 1413 1571 1869 - - - - 4160
95/96/98 99/99/101 102/102/103 - - - -
25 1526 1845 - - - - - 3929
96/96/98 100/100/101 - - - - -
30 1813 - - - - - - 3704
97/97/98 - - - - - -
32 1934 - - - - - - 3617
97/97/98 - - - - - -

VFS 114 117 120 123 - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 13
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 10000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1221 1367 1626 - - - - 4181

96/96/98 99/99/101 102/102/103 - - - -
-35 1240 1388 1649 - - - - 4184
96/96/98 99/99/101 102/102/103 - - - -
-30 1261 1410 1673 - - - - 4187
96/96/98 99/99/101 102/102/103 - - - -
-25 1282 1431 1696 - - - - 4189
96/96/98 99/99/101 102/102/103 - - - -
-20 1303 1453 1720 - - - - 4192
96/96/98 99/99/101 102/102/103 - - - -
-15 1325 1474 1743 - - - - 4195
96/96/98 99/99/101 102/102/103 - - - -
-10 1346 1495 1766 - - - - 4198
95/96/98 99/99/101 102/102/103 - - - -
-5 1367 1519 1789 2099 - - - 4201
95/96/98 99/99/101 102/102/103 105/105/106 - - -
0 1388 1542 1811 2126 - - - 4204
95/96/98 99/99/101 102/102/103 105/105/106 - - -
5 1409 1566 1835 2154 - - - 4205
95/96/98 99/99/101 102/102/103 105/105/106 - - -
10 1432 1592 1863 2185 - - - 4204
95/96/98 99/99/101 102/102/103 105/105/106 - - -
15 1458 1621 1903 - - - - 4196
95/96/98 99/99/101 102/102/103 - - - -
20 1569 1866 - - - - - 3967
96/96/98 100/100/101 - - - - -
25 1835 - - - - - - 3745
97/97/98 - - - - - -

VFS 114 117 120 123 - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 14 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: -1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 657 659 664 670 679 794 922 4800

92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 96/96/98
-35 669 671 676 682 690 805 935 4800
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 96/96/98
-30 680 683 688 694 702 816 947 4800
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 96/96/98
-25 692 695 700 706 714 827 960 4800
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 96/96/98
-20 703 707 712 719 727 838 972 4800
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 96/96/98
-15 715 718 724 731 739 848 985 4800
91/91/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 96/96/98
-10 726 730 736 743 751 859 997 4800
91/91/96 91/91/96 91/91/95 91/91/94 90/91/94 94/94/96 96/96/98
-5 738 742 748 755 764 870 1010 4800
91/91/96 91/91/96 91/91/95 91/91/94 90/91/94 94/94/96 96/96/98
0 749 754 760 767 776 881 1022 4800
91/91/96 91/91/96 91/91/95 91/91/94 90/91/94 94/94/96 96/96/98
5 761 765 772 780 789 891 1035 4800
91/91/96 91/91/96 91/91/95 91/91/94 90/91/94 94/94/96 96/96/98
10 772 776 783 791 801 904 1049 4800
91/91/96 91/91/96 91/91/95 91/91/94 90/91/94 94/94/96 96/96/98
15 782 787 794 802 812 921 1067 4800
91/91/96 91/91/95 91/91/95 90/90/94 90/91/94 94/94/96 96/96/98
20 793 798 805 813 824 938 1086 4800
91/91/96 91/91/95 91/91/95 90/90/94 90/91/94 94/94/96 96/96/98
25 803 808 816 825 835 955 1105 4800
91/91/96 91/91/95 90/90/94 90/90/94 90/91/94 94/94/96 96/96/98
30 801 807 815 825 894 1048 - 4663
90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 94/94/96 -
35 784 792 802 889 1047 - - 4423
87/87/92 87/87/91 86/87/90 90/90/92 92/92/94 - -
40 767 777 887 - - - - 4189
84/84/89 84/85/88 88/88/90 - - - -
45 753 867 - - - - - 3977
82/82/86 85/85/88 - - - - -
50 839 - - - - - - 3782
83/83/86 - - - - - -
51 869 - - - - - - 3745
83/83/86 - - - - - -

VFS 114 117 120 122 125 128 130

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 15
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 0 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 678 681 685 692 699 811 - 4740

92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 -
-35 690 693 698 704 712 822 - 4747
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 -
-30 702 705 710 717 725 832 - 4753
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 -
-25 714 717 723 730 738 842 - 4760
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 -
-20 726 730 735 742 751 853 - 4763
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 -
-15 738 742 748 755 764 865 - 4765
92/92/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 -
-10 750 754 760 767 776 877 - 4766
91/91/96 91/91/96 91/91/95 91/91/94 91/91/94 94/94/96 -
-5 761 766 772 780 789 890 - 4767
91/91/96 91/91/96 91/91/95 91/91/94 90/91/94 94/94/96 -
0 773 777 784 792 801 903 - 4767
91/91/96 91/91/96 91/91/95 91/91/94 90/91/94 94/94/96 -
5 784 789 796 804 814 916 - 4768
91/91/96 91/91/96 91/91/95 91/91/94 90/91/94 94/94/96 -
10 796 801 808 816 826 930 - 4766
91/91/96 91/91/95 91/91/95 90/90/94 90/91/94 94/94/96 -
15 806 811 819 828 838 949 - 4757
91/91/96 91/91/95 91/91/95 90/90/94 90/91/94 94/94/96 -
20 817 822 830 839 850 967 - 4748
91/91/96 91/91/95 90/90/94 90/90/94 90/91/94 94/94/96 -
25 826 832 840 850 863 994 - 4724
91/91/96 90/90/95 90/90/94 90/90/94 90/91/94 94/94/96 -
30 809 816 826 858 1003 - - 4500
88/88/93 88/88/92 87/87/91 88/89/92 92/92/94 - -
35 790 800 853 1014 - - - 4257
85/85/90 85/85/89 87/87/91 90/90/92 - - -
40 776 837 1010 - - - - 4032
82/82/87 85/85/88 88/88/91 - - - -
45 812 994 - - - - - 3824
83/83/86 86/86/88 - - - - -
50 962 - - - - - - 3642
83/83/86 - - - - - -

VFS 114 117 120 122 125 128 -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 16 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 680 684 690 697 787 - - 4576

90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 - -
-35 692 696 703 710 797 - - 4582
90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 - -
-30 704 709 715 723 806 - - 4588
90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 - -
-25 716 721 728 736 816 - - 4593
90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 - -
-20 728 733 740 749 827 - - 4596
90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 - -
-15 741 746 753 762 839 - - 4599
90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 - -
-10 753 758 766 775 851 998 - 4600
90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 94/94/96 -
-5 765 771 778 788 863 1012 - 4602
90/90/94 89/89/94 89/89/93 89/89/92 92/92/94 94/94/96 -
0 777 783 791 800 876 1026 - 4603
89/89/94 89/89/94 89/89/93 89/89/92 92/92/94 94/94/96 -
5 788 794 802 812 888 1040 - 4604
89/89/94 89/89/93 89/89/93 89/89/92 92/92/94 94/94/96 -
10 799 806 814 824 903 1057 - 4601
89/89/94 89/89/93 89/89/93 89/89/92 92/92/94 94/94/96 -
15 810 817 826 836 920 - - 4594
89/89/94 89/89/93 89/89/93 88/89/92 92/92/94 - -
20 821 828 837 848 938 - - 4587
89/89/94 89/89/93 89/89/92 88/89/92 92/92/94 - -
25 828 836 846 858 994 - - 4519
88/88/93 88/88/92 88/88/92 88/89/92 92/92/94 - -
30 811 821 846 995 - - - 4305
86/86/90 86/86/90 86/87/91 90/90/92 - - -
35 794 831 995 - - - - 4076
83/83/87 84/85/88 88/88/91 - - - -
40 807 978 - - - - - 3866
82/83/86 86/86/88 - - - - -
45 951 - - - - - - 3671
83/83/86 - - - - - -

VFS 114 117 120 122 125 128 -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 17
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 2000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 683 689 696 758 900 - - 4416

88/88/92 88/88/92 87/87/91 90/90/92 92/92/94 - -
-35 695 701 709 767 912 - - 4421
88/88/92 87/87/92 87/87/91 90/90/92 92/92/94 - -
-30 708 714 722 777 923 - - 4425
88/88/92 87/87/92 87/87/91 90/90/92 92/92/94 - -
-25 720 726 735 787 935 - - 4429
88/88/92 87/87/92 87/87/91 90/90/92 92/92/94 - -
-20 732 739 747 797 947 - - 4433
88/88/92 87/87/92 87/87/91 89/90/92 92/92/94 - -
-15 745 752 760 810 960 - - 4436
88/88/92 87/87/92 87/87/91 89/90/92 92/92/94 - -
-10 757 764 773 823 973 - - 4439
88/88/92 87/87/92 87/87/91 89/90/92 92/92/94 - -
-5 769 776 785 835 986 - - 4441
88/88/92 87/87/92 87/87/91 89/90/92 92/92/94 - -
0 781 788 798 848 999 - - 4444
88/88/92 87/87/91 87/87/91 89/90/92 92/92/94 - -
5 792 800 809 862 1014 - - 4445
87/87/92 87/87/91 87/87/91 89/90/92 92/92/94 - -
10 803 812 822 877 1030 - - 4441
87/87/92 87/87/91 87/87/91 89/90/92 92/92/94 - -
15 815 823 834 892 1048 - - 4436
87/87/92 87/87/91 87/87/91 89/90/92 92/92/94 - -
20 826 835 846 908 1065 - - 4431
87/87/92 87/87/91 87/87/91 89/90/92 92/92/94 - -
25 828 838 852 994 - - - 4327
86/86/90 86/86/90 86/87/91 90/90/92 - - -
30 814 829 976 - - - - 4122
83/83/88 83/85/88 88/88/91 - - - -
35 808 963 - - - - - 3904
81/82/86 86/86/88 - - - - -
40 939 - - - - - - 3703
83/83/86 - - - - - -

VFS 114 117 120 122 125 - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 18 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 3000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 687 694 727 872 - - - 4266

86/86/90 86/86/90 87/87/91 90/90/92 - - -
-35 699 707 739 884 - - - 4270
86/86/90 86/86/90 87/87/91 90/90/92 - - -
-30 712 719 750 896 - - - 4274
86/86/90 86/86/90 87/87/91 90/90/92 - - -
-25 724 732 762 908 - - - 4277
86/86/90 86/86/89 87/87/91 90/90/92 - - -
-20 737 745 774 919 - - - 4281
86/86/90 85/85/89 86/87/91 90/90/92 - - -
-15 749 758 785 931 - - - 4284
86/86/90 85/85/89 86/87/91 90/90/92 - - -
-10 762 770 797 943 - - - 4288
86/86/90 85/85/89 86/87/91 90/90/92 - - -
-5 774 783 808 954 - - - 4291
86/86/90 85/85/89 86/87/91 90/90/92 - - -
0 787 796 820 966 - - - 4294
86/86/90 85/85/89 86/87/91 90/90/92 - - -
5 799 808 833 979 - - - 4296
86/86/90 85/85/89 86/87/91 90/90/92 - - -
10 810 820 848 996 - - - 4292
85/85/90 85/85/89 86/87/91 90/90/92 - - -
15 821 831 863 1012 - - - 4288
85/85/90 85/85/89 86/87/91 90/90/92 - - -
20 833 844 884 1039 - - - 4274
85/85/90 85/85/89 86/87/91 90/90/92 - - -
25 832 843 970 - - - - 4159
84/84/88 84/85/89 88/88/91 - - - -
30 818 947 - - - - - 3951
81/82/86 85/85/89 - - - - -
35 924 - - - - - - 3746
83/83/86 - - - - - -

VFS 114 117 120 122 - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 19
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 4000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 694 703 828 - - - - 4119

84/84/88 84/85/89 88/88/91 - - - -
-35 707 716 840 - - - - 4122
84/84/88 84/85/89 88/88/91 - - - -
-30 719 728 851 - - - - 4126
84/84/88 84/85/89 88/88/91 - - - -
-25 732 741 862 - - - - 4130
84/84/88 84/85/89 88/88/91 - - - -
-20 745 754 873 - - - - 4134
84/84/88 84/85/89 88/88/91 - - - -
-15 757 767 884 - - - - 4137
84/84/88 84/85/89 88/88/91 - - - -
-10 770 780 895 - - - - 4141
84/84/88 84/85/89 88/88/91 - - - -
-5 783 793 906 - - - - 4144
84/84/88 84/85/89 88/88/91 - - - -
0 796 806 917 - - - - 4148
84/84/88 84/85/89 88/88/91 - - - -
5 808 819 930 - - - - 4150
84/84/88 84/85/89 88/88/91 - - - -
10 820 831 946 - - - - 4147
84/84/88 84/85/89 88/88/91 - - - -
15 832 843 961 - - - - 4144
84/84/88 83/85/89 88/88/91 - - - -
20 843 855 991 - - - - 4130
83/83/88 83/85/89 88/88/91 - - - -
25 838 926 - - - - - 3993
82/82/86 85/85/89 - - - - -
30 899 - - - - - - 3791
83/83/86 - - - - - -

VFS 114 117 120 - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 20 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 5000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 700 787 - - - - - 3973

82/82/86 85/85/89 - - - - -
-35 713 798 - - - - - 3977
82/82/86 85/85/89 - - - - -
-30 725 808 - - - - - 3980
82/82/86 85/85/89 - - - - -
-25 738 819 - - - - - 3984
82/82/86 85/85/89 - - - - -
-20 751 829 - - - - - 3987
82/82/86 85/85/89 - - - - -
-15 764 840 - - - - - 3991
82/82/86 85/85/89 - - - - -
-10 777 850 - - - - - 3994
82/82/86 85/85/89 - - - - -
-5 790 861 - - - - - 3997
82/82/86 85/85/89 - - - - -
0 803 873 1051 - - - - 4000
82/82/86 85/85/89 88/88/91 - - - -
5 816 887 1065 - - - - 4003
82/82/86 85/85/89 88/88/91 - - - -
10 828 901 1081 - - - - 4002
82/82/86 85/85/89 88/88/91 - - - -
15 841 915 1097 - - - - 4000
82/82/86 85/85/89 88/88/91 - - - -
20 852 939 - - - - - 3984
82/82/86 85/85/89 - - - - -
25 899 1086 - - - - - 3820
82/83/86 86/86/89 - - - - -
30 1060 - - - - - - 3623
83/83/86 - - - - - -

VFS 114 117 120 - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 21
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 6000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 736 899 - - - - - 3845

82/83/86 86/86/89 - - - - -
-35 748 912 - - - - - 3849
82/83/86 86/86/89 - - - - -
-30 759 924 - - - - - 3852
82/83/86 86/86/89 - - - - -
-25 771 936 - - - - - 3855
82/83/86 86/86/89 - - - - -
-20 783 948 - - - - - 3858
82/83/86 86/86/89 - - - - -
-15 795 960 - - - - - 3861
81/83/86 86/86/89 - - - - -
-10 807 972 - - - - - 3865
81/83/86 86/86/89 - - - - -
-5 819 983 - - - - - 3868
81/83/86 86/86/89 - - - - -
0 831 995 - - - - - 3871
81/83/86 86/86/89 - - - - -
5 844 1007 - - - - - 3874
81/83/86 86/86/89 - - - - -
10 858 1023 - - - - - 3872
81/83/86 86/86/89 - - - - -
15 871 1038 - - - - - 3870
81/83/86 86/86/89 - - - - -
20 909 1094 - - - - - 3827
82/83/86 86/86/89 - - - - -
25 1050 - - - - - - 3656
83/83/86 - - - - - -

VFS 114 117 - - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 22 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 7000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 836 - - - - - - 3723

83/83/86 - - - - - -
-35 847 - - - - - - 3727
83/83/86 - - - - - -
-30 859 - - - - - - 3730
83/83/86 - - - - - -
-25 870 - - - - - - 3733
83/83/86 - - - - - -
-20 881 - - - - - - 3736
83/83/86 - - - - - -
-15 892 - - - - - - 3739
83/83/86 - - - - - -
-10 903 - - - - - - 3742
83/83/86 - - - - - -
-5 914 - - - - - - 3746
83/83/86 - - - - - -
0 925 - - - - - - 3749
83/83/86 - - - - - -
5 936 - - - - - - 3751
83/83/86 - - - - - -
10 952 - - - - - - 3750
83/83/86 - - - - - -
15 967 - - - - - - 3747
83/83/86 - - - - - -
20 1050 - - - - - - 3678
83/83/86 - - - - - -

VFS 114 - - - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 23
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) OFF – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 8000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 948 - - - - - - 3604

83/83/86 - - - - - -
-35 961 - - - - - - 3608
83/83/86 - - - - - -
-30 974 - - - - - - 3611
83/83/86 - - - - - -
-25 987 - - - - - - 3614
83/83/86 - - - - - -
-20 999 - - - - - - 3617
83/83/86 - - - - - -
-15 1012 - - - - - - 3620
83/83/86 - - - - - -
-10 1024 - - - - - - 3623
83/83/86 - - - - - -
-5 1037 - - - - - - 3626
83/83/86 - - - - - -
0 1049 - - - - - - 3629
83/83/86 - - - - - -
5 1062 - - - - - - 3632
83/83/86 - - - - - -
10 1078 - - - - - - 3631
83/83/86 - - - - - -
15 1097 - - - - - - 3628
83/83/86 - - - - - -

VFS 114 - - - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 24 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: -1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 745 833 926 1022 1120 1220 1324 4800

101/107/112 106/111/115 111/114/118 115/117/121 119/120/124 122/123/126 126/126/129
-35 758 847 942 1040 1139 1242 1348 4800
101/107/112 106/111/115 111/114/118 115/117/121 119/120/124 122/123/126 126/126/129
-30 771 861 958 1058 1159 1264 1371 4800
101/107/112 106/111/115 111/114/118 115/117/121 118/120/124 122/123/126 125/126/129
-25 784 875 974 1075 1179 1285 1395 4800
101/107/112 106/111/115 111/114/118 115/117/121 118/120/124 122/123/126 125/126/129
-20 796 889 990 1093 1199 1307 1419 4800
101/107/112 106/111/115 110/114/118 115/117/121 118/120/124 122/123/126 125/126/129
-15 809 904 1006 1111 1218 1328 1442 4800
101/107/112 106/111/115 110/114/118 115/117/121 118/120/124 122/123/126 125/126/129
-10 822 918 1022 1129 1238 1350 1466 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 122/123/126 125/126/129
-5 835 933 1038 1147 1258 1372 1490 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 122/123/126 125/126/129
0 848 947 1055 1165 1278 1394 1515 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 122/123/126 125/126/129
5 862 963 1072 1184 1299 1417 1540 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 122/123/126 125/126/129
10 875 978 1090 1203 1320 1441 1565 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 121/123/126 125/126/129

VFS 131 134 137 140 143 146 149

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 25
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 0 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 767 857 954 1052 1153 1257 1364 4800

101/107/112 106/111/115 111/114/118 115/117/121 118/120/124 122/123/126 125/126/129
-35 780 872 970 1071 1173 1279 1389 4800
101/107/112 106/111/115 111/114/118 115/117/121 118/120/124 122/123/126 125/126/129
-30 794 886 987 1089 1194 1302 1413 4800
101/107/112 106/111/115 110/114/118 115/117/121 118/120/124 122/123/126 125/126/129
-25 807 901 1003 1107 1214 1324 1437 4800
101/107/112 106/111/115 110/114/118 115/117/121 118/120/124 122/123/126 125/126/129
-20 820 916 1020 1126 1234 1346 1462 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 122/123/126 125/126/129
-15 833 930 1036 1144 1255 1369 1486 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 122/123/126 125/126/129
-10 847 946 1053 1163 1275 1392 1511 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 122/123/126 125/126/129
-5 861 961 1070 1181 1296 1415 1537 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 121/123/126 125/126/129
0 875 977 1088 1202 1319 1439 1563 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 121/123/126 125/126/129
5 889 993 1107 1222 1341 1464 1590 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 121/123/126 125/126/129
10 904 1010 1125 1243 1364 1488 1617 4800
101/107/112 106/111/115 110/114/118 114/117/121 118/120/124 121/123/126 125/126/129

VFS 131 134 137 141 143 146 149

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 26 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 824 924 1025 1130 1237 1347 1462 4800

102/108/112 107/111/115 112/114/118 116/118/121 119/121/124 123/124/126 126/127/129
-35 838 939 1043 1149 1259 1371 1488 4800
102/108/112 107/111/115 112/114/118 116/118/121 119/121/124 123/124/126 126/127/129
-30 852 955 1061 1169 1280 1395 1514 4800
102/108/112 107/111/115 112/114/118 116/118/121 119/120/124 123/124/126 126/127/129
-25 866 971 1079 1189 1302 1419 1541 4800
102/108/112 107/111/115 112/114/118 116/118/121 119/120/124 123/124/126 126/127/129
-20 880 987 1097 1209 1324 1443 1567 4800
102/108/112 107/111/115 111/114/118 115/118/121 119/120/124 122/124/126 126/127/129
-15 894 1003 1115 1229 1346 1468 1594 4800
102/108/112 107/111/115 111/114/118 115/117/121 119/120/124 122/124/126 126/127/129
-10 909 1020 1133 1249 1369 1492 1621 4800
102/108/112 107/111/115 111/114/118 115/117/121 119/120/124 122/124/126 126/127/129
-5 924 1036 1152 1270 1392 1518 1648 4800
102/108/112 107/111/115 111/114/118 115/117/121 119/120/124 122/124/126 126/127/129
0 939 1053 1171 1291 1415 1543 1676 4800
102/108/112 107/111/115 111/114/118 115/118/121 119/120/124 122/124/126 126/127/129
5 954 1071 1190 1313 1439 1569 1705 4800
102/108/112 107/111/115 111/114/118 115/118/121 119/120/124 122/124/126 126/127/129
10 970 1088 1210 1335 1463 1596 1734 4800
102/108/112 107/111/115 111/114/118 115/118/121 119/121/124 122/124/126 126/127/129

VFS 131 134 137 141 144 146 149

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 27
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 2000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 890 995 1102 1213 1327 1445 1630 4800

104/108/112 109/112/115 113/115/118 117/118/121 120/121/124 124/124/126 127/127/129
-35 905 1012 1122 1235 1351 1471 1654 4800
104/108/112 109/112/115 113/115/118 117/118/121 120/121/124 123/124/126 127/127/129
-30 921 1030 1141 1256 1375 1498 1678 4800
104/108/112 108/112/115 113/115/118 117/118/121 120/121/124 123/124/126 127/127/129
-25 936 1047 1161 1278 1398 1524 1702 4800
104/108/112 108/112/115 113/115/118 116/118/121 120/121/124 123/124/126 127/127/129
-20 951 1064 1180 1299 1422 1550 1726 4800
104/108/112 108/112/115 113/115/118 116/118/121 120/121/124 123/124/126 127/127/129
-15 967 1082 1200 1321 1446 1576 1750 4800
104/108/112 108/112/115 113/115/118 116/118/121 120/121/124 123/124/126 127/127/129
-10 982 1099 1219 1342 1470 1602 1773 4800
103/108/112 108/112/115 112/115/118 116/118/121 120/121/124 123/124/126 127/127/129
-5 998 1117 1239 1364 1494 1629 1797 4800
103/108/112 108/112/115 112/115/118 116/118/121 120/121/124 123/124/126 127/127/129
0 1013 1134 1258 1386 1518 1655 1846 4800
103/108/112 108/112/115 112/115/118 116/118/121 120/121/124 123/124/126 126/127/129
5 1030 1153 1279 1409 1544 1683 1976 4800
103/108/112 108/112/115 112/115/118 116/118/121 119/121/124 123/124/126 125/127/129
10 1048 1173 1301 1434 1570 1713 2135 4800
103/108/112 108/112/115 112/115/118 116/118/121 119/121/124 123/124/126 124/127/129

VFS 131 134 137 141 144 146 149

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 28 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 3000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 960 1071 1185 1302 1424 1594 1859 4800

105/109/112 110/112/115 114/115/118 117/118/121 121/121/124 124/124/126 127/127/129
-35 977 1089 1206 1326 1450 1617 1886 4800
105/109/112 110/112/115 114/115/118 117/118/121 121/121/124 124/124/126 127/127/129
-30 993 1108 1227 1349 1476 1640 1913 4800
105/109/112 110/112/115 114/115/118 117/118/121 121/121/124 124/124/126 127/127/129
-25 1010 1127 1248 1372 1501 1663 1940 4800
105/109/112 110/112/115 114/115/118 117/118/121 121/121/124 124/124/126 127/127/129
-20 1027 1146 1269 1395 1527 1686 1967 4800
105/109/112 109/112/115 114/115/118 117/118/121 120/121/124 124/124/126 127/127/129
-15 1043 1165 1290 1419 1553 1709 1993 4800
105/109/112 109/112/115 113/115/118 117/118/121 120/121/124 124/124/126 127/127/129
-10 1060 1183 1310 1442 1578 1736 2057 4800
105/108/112 109/112/115 113/115/118 117/118/121 120/121/124 124/124/126 127/127/129
-5 1076 1202 1331 1465 1604 1763 2221 4800
105/108/112 109/112/115 113/115/118 117/118/121 120/121/124 124/124/126 125/127/129
0 1093 1220 1352 1488 1629 1790 2420 4800
105/108/112 109/112/115 113/115/118 117/118/121 120/121/124 124/124/126 124/127/129
5 1111 1241 1375 1513 1657 1820 2651 4800
105/108/112 109/112/115 113/115/118 117/118/121 120/121/124 124/124/126 123/127/129
10 1130 1262 1399 1540 1686 1854 2856 4800
105/108/112 109/112/115 113/115/118 117/118/121 120/121/124 124/124/126 121/127/129

VFS 131 134 138 141 144 146 149

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 29
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 4000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1030 1147 1268 1393 1531 1805 - 4726

106/109/112 111/112/115 115/116/118 118/119/121 122/122/124 125/125/126 -
-35 1048 1167 1291 1418 1558 1831 - 4729
106/109/112 111/112/115 114/116/118 118/119/121 122/122/124 125/125/126 -
-30 1066 1188 1313 1443 1585 1857 - 4732
106/109/112 110/112/115 114/116/118 118/119/121 121/122/124 125/125/126 -
-25 1084 1208 1336 1468 1611 1883 - 4735
106/109/112 110/112/115 114/116/118 118/119/121 121/122/124 125/125/126 -
-20 1102 1228 1358 1494 1638 1909 - 4738
106/109/112 110/112/115 114/116/118 118/119/121 121/122/124 125/125/126 -
-15 1120 1248 1381 1519 1665 1935 - 4742
106/109/112 110/112/115 114/116/118 118/119/121 121/122/124 125/125/126 -
-10 1138 1268 1404 1544 1692 1960 - 4745
106/109/112 110/112/115 114/116/118 118/119/121 121/122/124 125/125/126 -
-5 1156 1289 1426 1569 1719 1986 - 4748
106/109/112 110/112/115 114/116/118 118/119/121 121/122/124 125/125/126 -
0 1173 1309 1449 1594 1745 2011 - 4751
106/109/112 110/112/115 114/116/118 118/119/121 121/122/124 125/125/126 -
5 1193 1330 1472 1620 1775 2113 - 4749
106/109/112 110/112/115 114/116/118 117/119/121 121/122/124 124/125/126 -
10 1213 1353 1498 1648 1807 2288 - 4745
106/109/112 110/112/115 114/116/118 117/119/121 121/122/124 122/125/126 -

VFS 131 134 138 141 144 147 -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 30 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 5000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1112 1236 1365 1500 1768 - - 4545

107/109/112 112/113/115 115/116/118 119/119/121 122/122/124 - -
-35 1131 1258 1390 1527 1794 - - 4549
107/109/112 111/113/115 115/116/118 119/119/121 122/122/124 - -
-30 1150 1280 1414 1554 1819 - - 4552
107/109/112 111/113/115 115/116/118 119/119/121 122/122/124 - -
-25 1170 1302 1439 1581 1844 - - 4555
107/109/112 111/113/115 115/116/118 119/119/121 122/122/124 - -
-20 1189 1324 1463 1608 1869 - - 4559
107/109/112 111/113/115 115/116/118 118/119/121 122/122/124 - -
-15 1209 1345 1487 1635 1894 - - 4562
107/109/112 111/113/115 115/116/118 118/119/121 122/122/124 - -
-10 1228 1367 1512 1662 1918 - - 4566
107/109/112 111/113/115 115/116/118 118/119/121 122/122/124 - -
-5 1247 1389 1536 1689 1943 - - 4569
107/109/112 111/113/115 115/116/118 118/119/121 122/122/124 - -
0 1267 1411 1560 1716 1967 - - 4572
107/109/112 111/113/115 115/116/118 118/119/121 122/122/124 - -
5 1287 1433 1586 1744 1994 - - 4573
107/109/112 111/113/115 115/116/118 118/119/121 122/122/124 - -
10 1308 1457 1612 1773 2026 - - 4571
107/109/112 111/113/115 115/116/118 118/119/121 122/122/124 - -

VFS 131 134 138 141 144 - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 31
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 6000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1194 1327 1465 1700 - - - 4389

108/110/112 112/113/115 116/116/118 119/119/121 - - -
-35 1215 1350 1491 1725 - - - 4392
108/110/112 112/113/115 116/116/118 119/119/121 - - -
-30 1236 1374 1518 1749 - - - 4395
108/110/112 112/113/115 116/116/118 119/119/121 - - -
-25 1257 1397 1544 1773 - - - 4399
108/110/112 112/113/115 116/116/118 119/119/121 - - -
-20 1278 1421 1570 1796 2111 - - 4402
108/110/112 112/113/115 116/116/118 119/119/121 122/122/124 - -
-15 1299 1444 1596 1820 2139 - - 4405
108/110/112 112/113/115 116/116/118 119/119/121 122/122/124 - -
-10 1320 1468 1622 1844 2166 - - 4409
108/110/112 112/113/115 116/116/118 119/119/121 122/122/124 - -
-5 1341 1491 1648 1867 2194 - - 4412
108/110/112 112/113/115 115/116/118 119/119/121 122/122/124 - -
0 1361 1515 1674 1890 2221 - - 4415
108/110/112 112/113/115 115/116/118 119/119/121 122/122/124 - -
5 1383 1539 1702 1916 - - - 4416
108/110/112 112/113/115 115/116/118 119/119/121 - - -
10 1406 1565 1730 1947 - - - 4413
108/110/112 112/113/115 115/116/118 119/119/121 - - -

VFS 131 134 138 141 144 - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 32 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 7000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1279 1420 1609 1919 - - - 4244

109/110/112 113/114/115 117/117/118 120/120/121 - - -
-35 1302 1446 1632 1946 - - - 4247
109/110/112 113/114/115 117/117/118 120/120/121 - - -
-30 1324 1471 1655 1974 - - - 4250
109/110/112 113/114/115 117/117/118 120/120/121 - - -
-25 1347 1497 1678 2001 - - - 4253
109/110/112 113/114/115 117/117/118 120/120/121 - - -
-20 1370 1522 1701 2028 - - - 4257
109/110/112 113/114/115 117/117/118 120/120/121 - - -
-15 1393 1548 1727 2055 - - - 4260
109/110/112 113/114/115 117/117/118 120/120/121 - - -
-10 1416 1573 1754 2082 - - - 4263
109/110/112 112/113/115 117/117/118 120/120/121 - - -
-5 1438 1599 1781 2108 - - - 4267
109/110/112 112/113/115 116/117/118 120/120/121 - - -
0 1461 1624 1808 2134 - - - 4270
108/110/112 112/113/115 116/117/118 120/120/121 - - -
5 1484 1650 1837 2164 - - - 4271
108/110/112 112/113/115 116/117/118 120/120/121 - - -
10 1509 1679 1869 - - - - 4268
108/110/112 112/113/115 116/117/118 - - - -

VFS 131 134 138 141 - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 33
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 8000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1371 1522 1828 - - - - 4102

110/110/112 113/114/115 117/117/118 - - - -
-35 1396 1550 1855 - - - - 4105
110/110/112 113/114/115 117/117/118 - - - -
-30 1420 1577 1881 - - - - 4108
110/110/112 113/114/115 117/117/118 - - - -
-25 1445 1605 1908 - - - - 4111
109/110/112 113/114/115 117/117/118 - - - -
-20 1470 1632 1934 - - - - 4114
109/110/112 113/114/115 117/117/118 - - - -
-15 1494 1660 1959 - - - - 4116
109/110/112 113/114/115 117/117/118 - - - -
-10 1519 1687 1985 - - - - 4119
109/110/112 113/114/115 117/117/118 - - - -
-5 1543 1715 2010 - - - - 4122
109/110/112 113/114/115 117/117/118 - - - -
0 1567 1742 2036 - - - - 4125
109/110/112 113/114/115 117/117/118 - - - -
5 1592 1770 2062 - - - - 4127
109/110/112 113/114/115 117/117/118 - - - -
10 1620 1801 - - - - - 4124
109/110/112 113/114/115 - - - - -

VFS 131 135 138 - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 34 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 9000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1499 1753 - - - - - 3968

110/111/112 114/114/115 - - - - -
-35 1526 1778 - - - - - 3971
110/111/112 114/114/115 - - - - -
-30 1553 1803 - - - - - 3974
110/111/112 114/114/115 - - - - -
-25 1580 1828 - - - - - 3977
110/111/112 114/114/115 - - - - -
-20 1607 1853 - - - - - 3979
110/111/112 114/114/115 - - - - -
-15 1634 1878 - - - - - 3982
110/111/112 114/114/115 - - - - -
-10 1661 1903 - - - - - 3985
110/111/112 114/114/115 - - - - -
-5 1688 1927 - - - - - 3988
110/111/112 114/114/115 - - - - -
0 1715 1951 - - - - - 3990
110/111/112 114/114/115 - - - - -
5 1742 1976 - - - - - 3993
110/111/112 114/114/115 - - - - -
10 1771 2007 - - - - - 3991
110/111/112 114/114/115 - - - - -

VFS 131 135 - - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 35
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 1 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 10000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 1660 2024 - - - - - 3837

111/111/112 115/115/115 - - - - -
-35 1684 2053 - - - - - 3840
111/111/112 115/115/115 - - - - -
-30 1713 2082 - - - - - 3843
111/111/112 115/115/115 - - - - -
-25 1741 2111 - - - - - 3846
111/111/112 115/115/115 - - - - -
-20 1770 2140 - - - - - 3848
111/111/112 115/115/115 - - - - -
-15 1798 2168 - - - - - 3851
111/111/112 115/115/115 - - - - -
-10 1827 2197 - - - - - 3854
111/111/112 115/115/115 - - - - -
-5 1856 2225 - - - - - 3857
111/111/112 114/114/115 - - - - -
0 1885 2253 - - - - - 3860
111/111/112 114/114/115 - - - - -
5 1914 - - - - - - 3862
110/111/112 - - - - - -
10 1949 - - - - - - 3858
110/111/112 - - - - - -

VFS 131 135 - - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 36 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: -1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 662 727 800 873 - - - 4337

92/97/101 96/100/103 100/102/106 103/105/108 - - -
-35 673 739 814 888 - - - 4340
92/97/101 96/100/103 100/102/106 103/105/108 - - -
-30 684 752 828 903 - - - 4343
92/97/101 96/100/103 99/102/106 103/105/108 - - -
-25 696 764 841 919 - - - 4347
92/97/101 96/100/103 99/102/106 103/105/108 - - -
-20 707 776 855 934 - - - 4350
92/97/101 96/100/103 99/102/106 103/105/108 - - -
-15 718 789 869 949 - - - 4354
92/97/101 95/100/103 99/102/106 103/105/108 - - -
-10 729 801 883 964 - - - 4355
92/97/101 95/100/103 99/102/106 103/105/108 - - -
-5 740 813 896 980 - - - 4354
92/97/101 95/100/103 99/102/106 102/105/108 - - -
0 752 826 911 996 - - - 4354
91/97/101 95/100/103 99/102/106 102/105/108 - - -
5 763 840 925 1012 - - - 4353
91/97/101 95/100/103 99/102/106 102/105/108 - - -
10 775 853 940 1028 - - - 4352
91/97/101 95/100/103 99/102/106 102/105/108 - - -

VFS 131 134 137 140 - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 37
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 0 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 681 748 824 899 - - - 4343

92/97/101 96/100/103 99/102/106 103/105/108 - - -
-35 693 761 838 915 - - - 4347
92/97/101 96/100/103 99/102/106 103/105/108 - - -
-30 704 774 852 931 - - - 4350
92/97/101 96/100/103 99/102/106 103/105/108 - - -
-25 716 787 867 946 - - - 4353
92/97/101 95/100/103 99/102/106 103/105/108 - - -
-20 727 799 881 962 - - - 4357
92/97/101 95/100/103 99/102/106 103/105/108 - - -
-15 739 812 895 978 - - - 4360
91/97/101 95/100/103 99/102/106 102/105/108 - - -
-10 751 825 909 994 - - - 4358
91/97/101 95/100/103 99/102/106 102/105/108 - - -
-5 762 838 924 1010 - - - 4356
91/97/101 95/100/103 99/102/106 102/105/108 - - -
0 775 852 940 1027 - - - 4354
91/97/101 95/100/103 99/102/106 102/105/108 - - -
5 788 867 956 1045 - - - 4351
91/97/101 95/100/103 99/102/106 102/105/108 - - -
10 801 881 972 1062 - - - 4349
91/97/101 95/100/103 99/102/106 102/105/108 - - -

VFS 131 134 137 141 - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 38 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 1000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 728 805 884 - - - - 4184

93/97/101 97/100/103 101/103/106 - - - -
-35 740 819 900 - - - - 4187
93/97/101 97/100/103 100/103/106 - - - -
-30 753 833 915 - - - - 4190
93/97/101 97/100/103 100/103/106 - - - -
-25 765 846 930 - - - - 4193
93/97/101 97/100/103 100/103/106 - - - -
-20 778 860 946 - - - - 4196
93/97/101 97/100/103 100/103/106 - - - -
-15 790 874 961 - - - - 4198
93/97/101 97/100/103 100/103/106 - - - -
-10 803 888 977 - - - - 4198
92/97/101 97/100/103 100/103/106 - - - -
-5 816 903 993 - - - - 4197
92/97/101 96/100/103 100/103/106 - - - -
0 829 918 1010 - - - - 4195
92/97/101 96/100/103 100/103/106 - - - -
5 842 933 1026 - - - - 4194
92/97/101 96/100/103 100/103/106 - - - -
10 856 949 1044 - - - - 4191
92/97/101 96/100/103 100/103/106 - - - -

VFS 131 134 137 - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 39
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 2000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 783 866 958 - - - - 4027

94/98/101 98/100/103 102/103/106 - - - -
-35 796 881 975 - - - - 4029
94/98/101 98/100/103 102/103/106 - - - -
-30 810 896 991 - - - - 4032
94/98/101 98/100/103 102/103/106 - - - -
-25 823 911 1007 - - - - 4034
94/98/101 98/100/103 102/103/106 - - - -
-20 836 925 1023 - - - - 4036
94/98/101 98/100/103 102/103/106 - - - -
-15 850 941 1040 - - - - 4039
94/98/101 98/100/103 101/103/106 - - - -
-10 863 956 1056 - - - - 4041
94/98/101 98/100/103 101/103/106 - - - -
-5 877 971 1074 - - - - 4042
94/98/101 98/100/103 101/103/106 - - - -
0 892 987 1091 - - - - 4042
94/98/101 98/100/103 101/103/106 - - - -
5 906 1004 1110 - - - - 4040
94/98/101 98/100/103 101/103/106 - - - -
10 922 1021 1130 - - - - 4034
94/98/101 98/100/103 101/103/106 - - - -

VFS 131 134 137 - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 40 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 3000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 843 930 - - - - - 3878

95/98/101 99/101/103 - - - - -
-35 858 946 - - - - - 3881
95/98/101 99/101/103 - - - - -
-30 872 963 - - - - - 3883
95/98/101 99/101/103 - - - - -
-25 887 979 - - - - - 3885
95/98/101 99/101/103 - - - - -
-20 902 996 - - - - - 3887
95/98/101 99/101/103 - - - - -
-15 916 1012 - - - - - 3889
95/98/101 99/101/103 - - - - -
-10 931 1028 - - - - - 3892
95/98/101 99/101/103 - - - - -
-5 945 1045 - - - - - 3894
95/98/101 99/101/103 - - - - -
0 960 1061 - - - - - 3896
95/98/101 99/101/103 - - - - -
5 976 1079 - - - - - 3896
95/98/101 99/101/103 - - - - -
10 992 1097 - - - - - 3891
95/98/101 99/101/103 - - - - -

VFS 131 134 - - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 41
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 4000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 903 - - - - - - 3748

96/98/101 - - - - - -
-35 919 - - - - - - 3750
96/98/101 - - - - - -
-30 935 - - - - - - 3753
96/98/101 - - - - - -
-25 951 - - - - - - 3755
96/98/101 - - - - - -
-20 967 - - - - - - 3757
96/98/101 - - - - - -
-15 983 - - - - - - 3760
96/98/101 - - - - - -
-10 999 - - - - - - 3762
96/98/101 - - - - - -
-5 1014 - - - - - - 3764
96/98/101 - - - - - -
0 1030 - - - - - - 3767
96/98/101 - - - - - -
5 1047 - - - - - - 3766
96/98/101 - - - - - -
10 1064 - - - - - - 3762
96/98/101 - - - - - -

VFS 131 - - - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655

5-15 ANAC APPROVED

Page 42 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

SIMPLIFIED TAKEOFF ANALYSIS

FLAP 2 – DRY RUNWAY
ICE PROTECTION (WINGSTAB+ENG) ON – ATR OFF
PW617F-E ENGINES
Airport Pressure Altitude: 5000 ft
TAKEOFF WEIGHT (kg)
MINIMUM REQUIRED RUNWAY LENGTH (m)
TEMP
V1/VR/V2 (KIAS)
(ºC)
LIMITED
3600 3800 4000 4200 4400 4600 4800 WEIGHT

-40 986 - - - - - - 3600

98/99/101 - - - - - -
-35 1003 - - - - - - 3603
98/99/101 - - - - - -
-30 1020 - - - - - - 3605
98/99/101 - - - - - -
-25 1037 - - - - - - 3608
98/99/101 - - - - - -
-20 1053 - - - - - - 3610
97/99/101 - - - - - -
-15 1070 - - - - - - 3612
97/99/101 - - - - - -
-10 1087 - - - - - - 3615
97/99/101 - - - - - -
-5 1104 - - - - - - 3617
97/99/101 - - - - - -
0 1120 - - - - - - 3620
97/99/101 - - - - - -
5 1138 - - - - - - 3622
97/99/101 - - - - - -
10 1157 - - - - - - 3620
97/99/101 - - - - - -

VFS 131 - - - - - -

WARNING: THE VALUES ABOVE DO NOT TAKE INTO ACCOUNT

OBSTACLES.
AFM-2655
AFM-2655

ANAC APPROVED 5-15

REVISION 16 code 01 Page 43
 TM

PHENOM 100
Airplane Flight Manual
Performance

INTENTIONALLY BLANK

AFM-2655

5-15 ANAC APPROVED

Page 44 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

DRIFTDOWN TABLES (GROSS GRADIENT)

In the event of an engine failure during cruise the maximum airplane
operating altitude is affected. The Driftdown tables present the one
engine ceiling according to the airplane weight and temperature.
The airplane should level-off at the ceiling altitude.

EXAMPLE
Given:
Airplane Weight .................................................. 4400 kg
Temperature ....................................................... ISA + 10°C
Ice Protection...................................................... OFF
Determine:
Ceiling................................................................. 21000 ft
Driftdown Speed ................................................. 125 KIAS
AFM-2655

ANAC APPROVED 5-18

REVISION 16 code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

PW617F-E ENGINES

DRIFT CEILING ALTITUDE (x 100 ft)

WEIGHT DOWN ICE PROTECTION (WINGSTAB+ENG) OFF
(kg) SPEED
(KIAS) ISA - 10 ISA ISA + 10 ISA + 20 ISA + 35
3200 119 310 330 310 270 200
3300 121 310 320 300 260 190
3400 123 310 320 290 250 180
3500 124 310 310 280 240 170
3600 126 300 300 270 230 160
3700 127 300 300 270 220 150
3800 129 290 290 260 210 140
3900 131 280 280 250 200 120
4000 132 280 270 240 190 120
4100 134 270 270 230 180 100
4200 135 260 260 220 170 90
4300 136 260 260 220 160 80
4400 138 250 250 210 150 70
4500 139 240 240 200 140 60
4600 141 230 230 200 130 50
4700 142 220 230 180 130 40
4800 143 220 220 170 120 30
AFM-2655

5-18 ANAC APPROVED

Page 2 code 01 REVISION 17
 TM

PHENOM 100
Airplane Flight Manual
Performance

PW617F-E ENGINES

DRIFT CEILING ALTITUDE (x 100 ft)

WEIGHT DOWN ICE PROTECTION (WINGSTAB+ENG) ON
(kg) SPEED
(KIAS) ISA - 30 ISA - 20 ISA - 10 ISA ISA + 10
3200 141 190 240 280 250 220
3300 143 190 240 260 240 200
3400 145 190 240 250 240 200
3500 147 190 240 240 230 180
3600 149 190 240 240 220 160
3700 151 190 230 230 210 150
3800 153 190 230 230 200 140
3900 155 190 220 220 190 130
4000 156 190 210 210 180 120
4100 158 190 200 200 170 110
4200 160 180 180 180 150 90
4300 161 160 160 170 140 80
4400 162 140 140 150 140 70
4500 163 130 130 130 130 60
4600 165 100 110 110 110 50
4700 166 90 90 90 90 40
4800 167 90 90 90 90 30
AFM-2655

ANAC APPROVED 5-18

REVISION 16 code 01 Page 3
 TM

PHENOM 100
Airplane Flight Manual
Performance

ENROUTE GRADIENT
This table presents the corrected gradient value due to the wind effect
on the enroute gradient of climb/descent with one engine inoperative.
The wing effect correction is applicable for all weights, temperature
and altitudes, considering the landing gear and flap up, and must
replace the gradient for zero wind.

EXAMPLE
Given:
Headwind Wind................................................... 40 kt
Gradient for Zero Wind ....................................... 4.0%
Determine:
Gradient for 40 kt (headwind) ............................. 4.6%

CORRECTED GRADIENT %
ZERO HEADWIND (kt) TAILWIND (kt)
WIND 60 40 20 20 40 60
-6.0 -6.7 -6.4 -6.2 -5.4 -5.0 -4.7
-4.0 -4.6 -4.4 -4.1 -3.6 -3.2 -3.0
-2.0 -2.4 -2.2 -2.1 -1.7 -1.5 -1.4
0.0 0.0 0.0 0.0 0.0 0.0 0.0
2.0 2.5 2.3 2.1 1.7 1.4 1.2
4.0 5.0 4.6 4.3 3.2 2.7 2.3
6.0 7.7 7.0 6.5 4.7 3.9 3.3
7.0 9.0 8.2 7.6 5.4 4.5 3.8
AFM-2655

5-18 ANAC APPROVED

Page 4 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

APPROACH DATA
APPROACH CLIMB, LANDING CLIMB AND LANDING
REFERENCE SPEEDS

NOTE: - Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
- For Approach Flap 1, Landing Flap 3 and Engine Ice
Protection ON – Wingstab ON (SWPS Ice Speed), the
Approach Climb Speed, Landing Climb Speed and Landing
Reference Speed have the same value.
- For Approach Flap 2, Landing Flap FULL and Engine Ice
Protection ON – Wingstab ON (SWPS Ice Speed), the
Approach Climb Speed, Landing Climb Speed and Landing
Reference Speed have the same value.
- For airplanes Pre-Mod. SB 500-27-0001, the Wingstab OFF
performance data must be used according to
EAD 2009-02-04 (item e).

EXAMPLE
Given:
Airplane Landing Weight .................................... 4000 kg
Approach Flap .................................................... 2
Landing Flap....................................................... FULL
Engine Ice Protection ......................................... OFF
Wingstab............................................................. OFF
Determine:
Approach Climb Speed ...................................... 101 KIAS
Landing Climb Speed ......................................... 95 KIAS
VREF ..................................................................... 95 KIAS
AFM-2655

ANAC APPROVED 5-20

REVISION 16 code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

APPROACH FLAP 1 AND LANDING FLAP 3

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF

PW617F-E ENGINES

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

VAC – KIAS VREF – KIAS

3200 99 91
3300 101 91
3400 102 92
3500 103 93
3600 105 95
3700 106 96
3800 107 97
3900 109 98
4000 110 100
4100 111 101
4200 112 102
4300 114 104
4400 115 105
4500 116 106
4600 117 107
4700 119 109
4800 120 110

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT WAS EXCEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-20 ANAC APPROVED

Page 2 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

APPROACH FLAP 2 AND LANDING FLAP FULL

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF

PW617F-E ENGINES

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

VAC – KIAS VREF – KIAS

3200 92 91
3300 93 91
3400 94 91
3500 95 91
3600 97 91
3700 98 92
3800 99 93
3900 100 94
4000 101 95
4100 102 96
4200 103 98
4300 104 99
4400 105 100
4500 107 101
4600 108 103
4700 109 104
4800 110 105

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT WAS EXCEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-20

REVISION 16 code 01 Page 3
 TM

PHENOM 100
Airplane Flight Manual
Performance

APPROACH FLAP 1 AND LANDING FLAP 3

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)

PW617F-E ENGINES

APPROACH CLIMB/LANDING
WEIGHT (CLIMB/REFERENCE)
(kg)
SPEED – KIAS

3200 109
3300 111
3400 113
3500 114
3600 116
3700 118
3800 119
3900 121
4000 122
4100 124
4200 125
4300 127
4400 129
4500 130
4600 132
4700 133
4800 135

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT WAS EXCEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-20 ANAC APPROVED

Page 4 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

APPROACH FLAP 2 AND LANDING FLAP FULL

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)

PW617F-E ENGINES

APPROACH CLIMB/LANDING
WEIGHT (CLIMB/REFERENCE)
(kg)
SPEED – KIAS

3200 105
3300 107
3400 108
3500 110
3600 112
3700 113
3800 115
3900 116
4000 118
4100 119
4200 121
4300 122
4400 124
4500 125
4600 127
4700 128
4800 130

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT WAS EXCEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-20

REVISION 16 code 01 Page 5
 TM

PHENOM 100
Airplane Flight Manual
Performance

INTENTIONALLY BLANK

AFM-2655

5-20 ANAC APPROVED

Page 6 code 01 ORIGINAL
 TM

PHENOM 100
Airplane Flight Manual
Performance

LANDING DATA
LANDING TECHNIQUE
The landing performance data in this manual is based on the following
conditions:
 Steady three degree angle approach at VREF in landing
configuration;
 VREF airspeed maintained at runway threshold;
 Idle thrust established at runway threshold;
 Attitude maintained until MLG touchdown;
 Maximum brake applied immediately after MLG touchdown;
 Antiskid system operative.
If these performance techniques are not strictly used for a typical
landing made during normal operations, the distances may be longer.

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

The Maximum Landing Weight – Climb Limited tables present the
maximum landing climb weight in compliance with the airworthiness
climb requirements in function of the temperature and altitude and
according to the ice protection system configuration.
The landing climb weights shown may be above the Maximum
Landing Weight and are codified as follows:
 (A) Approach Climb Limited;
 (L) Landing Climb Limited;
 (E) Enroute Climb Limited;
 (O) Overweight Landing Weight.

(Continues on the next page)

AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 1
 TM

PHENOM 100
Airplane Flight Manual
Performance

(Continued from the previous page)

NOTE: - The overweight landing notation (O) is used to indicate that

the airplane is not climb limited. Always check this structural
limitation on Section 2.
- For airplanes Pre-Mod. SB 500-27-0001, the Wingstab OFF
performance data must be used according to
EAD 2009-02-04 (item f).

EXAMPLE
Given:
Airport Pressure Altitude..................................... 2000 ft
Approach Flap .................................................... 1
Landing Flap ....................................................... 3
Engine Ice Protection.......................................... OFF
Wingstab ............................................................. OFF
Temperature ....................................................... 20°C
Determine:
Maximum Landing Weight –
Overweight Landing Limited .......................... 4800 kg

AFM-2655

5-25 ANAC APPROVED

Page 2 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-35 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-30 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-25 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-20 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-15 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-10 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-5 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
0 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
5 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
10 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
15 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
20 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
25 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
30 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4751 (A)
35 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4693 (A) 4486 (A)
40 4800 (O) 4800 (O) 4800 (O) 4633 (A) 4431 (A) 4245 (A)
45 4800 (O) 4794 (A) 4585 (A) 4385 (E) - -
50 4708 (E) 4510 (E) - - - -

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 3
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 4800 (O) 4800 (O) 4671 (A) 4515 (A) 4364 (A) 4268 (A)
-35 4800 (O) 4800 (O) 4675 (A) 4520 (A) 4369 (A) 4271 (A)
-30 4800 (O) 4800 (O) 4680 (A) 4524 (A) 4373 (A) 4274 (A)
-25 4800 (O) 4800 (O) 4684 (A) 4528 (A) 4378 (A) 4278 (A)
-20 4800 (O) 4800 (O) 4689 (A) 4533 (A) 4382 (A) 4281 (A)
-15 4800 (O) 4800 (O) 4693 (A) 4537 (A) 4386 (A) 4284 (A)
-10 4800 (O) 4800 (O) 4697 (A) 4541 (A) 4391 (A) 4287 (A)
-5 4800 (O) 4800 (O) 4702 (A) 4545 (A) 4395 (A) 4290 (A)
0 4800 (O) 4800 (O) 4706 (A) 4549 (A) 4399 (A) 4293 (A)
5 4800 (O) 4800 (O) 4708 (A) 4553 (A) 4402 (A) 4296 (A)
10 4800 (O) 4800 (O) 4705 (A) 4550 (A) 4401 (A) 4295 (A)
15 4800 (O) 4800 (O) 4701 (A) 4547 (A) 4397 (A) 4271 (A)
20 4800 (O) 4800 (O) 4614 (A) 4427 (A) 4227 (A) 4032 (A)
25 4795 (A) 4579 (A) 4376 (A) 4179 (A) 3983 (A) 3794 (A)
30 4533 (A) 4321 (A) 4124 (A) 3941 (A) 3767 (A) 3581 (A)
35 4271 (A) 4081 (A) 3906 (A) - - -
40 4049 (A) - - - - -

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 4 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 4800 (O) 4757 (A) 4589 (A) 4426 (A) 4275 (A) 4125 (A)
-35 4800 (O) 4761 (A) 4593 (A) 4430 (A) 4279 (A) 4129 (A)
-30 4800 (O) 4766 (A) 4598 (A) 4434 (A) 4283 (A) 4133 (A)
-25 4800 (O) 4771 (A) 4602 (A) 4438 (A) 4287 (A) 4137 (A)
-20 4800 (O) 4775 (A) 4606 (A) 4442 (A) 4290 (A) 4141 (A)
-15 4800 (O) 4779 (A) 4609 (A) 4446 (A) 4294 (A) 4144 (A)
-10 4800 (O) 4781 (A) 4613 (A) 4450 (A) 4297 (A) 4148 (A)
-5 4800 (O) 4783 (A) 4616 (A) 4454 (A) 4301 (A) 4152 (A)
0 4800 (O) 4784 (A) 4620 (A) 4458 (A) 4304 (A) 4156 (A)
5 4800 (O) 4786 (A) 4620 (A) 4457 (A) 4305 (A) 4157 (A)
10 4800 (O) 4783 (A) 4614 (A) 4453 (A) 4301 (A) 4154 (A)
15 4800 (O) 4774 (A) 4608 (A) 4448 (A) 4297 (A) 4151 (A)
20 4800 (O) 4766 (A) 4602 (A) 4443 (A) 4284 (A) 4137 (A)
25 4800 (O) 4755 (A) 4531 (A) 4338 (A) 4169 (A) 3998 (A)
30 4673 (A) 4509 (A) 4311 (A) 4126 (A) 3955 (A) 3789 (A)
35 4431 (A) 4262 (A) 4080 (A) 3908 (A) 3744 (A) 3584 (A)
40 4191 (A) 4030 (A) 3866 (A) 3701 (A) 3544 (A) 3397 (A)
45 3977 (A) 3826 (A) 3665 (A) 3509 (A) - -
50 3773 (A) 3629 (A) - - - -

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 5
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION OFF – WINGSTAB OFF
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 3977 (A) 3847 (A) 3723 (A) 3603 (A) 3485 (A) 3410 (A)
-35 3981 (A) 3850 (A) 3727 (A) 3606 (A) 3488 (A) 3412 (A)
-30 3984 (A) 3854 (A) 3730 (A) 3610 (A) 3492 (A) 3415 (A)
-25 3988 (A) 3857 (A) 3734 (A) 3613 (A) 3495 (A) 3417 (A)
-20 3992 (A) 3861 (A) 3737 (A) 3616 (A) 3498 (A) 3419 (A)
-15 3995 (A) 3864 (A) 3740 (A) 3619 (A) 3501 (A) 3422 (A)
-10 3998 (A) 3867 (A) 3743 (A) 3623 (A) 3504 (A) 3424 (A)
-5 4002 (A) 3870 (A) 3747 (A) 3626 (A) 3508 (A) 3426 (A)
0 4005 (A) 3874 (A) 3750 (A) 3629 (A) 3511 (A) 3429 (A)
5 4007 (A) 3877 (A) 3752 (A) 3631 (A) 3513 (A) 3431 (A)
10 4006 (A) 3875 (A) 3750 (A) 3630 (A) 3512 (A) 3429 (A)
15 4005 (A) 3872 (A) 3747 (A) 3627 (A) 3509 (A) 3409 (A)
20 3988 (A) 3828 (A) 3678 (A) 3535 (A) 3378 (A) 3223 (A)
25 3821 (A) 3654 (A) 3496 (A) 3345 (A) 3198 (A) 3083 (A)
30 3619 (A) 3455 (A) 3302 (A) 3175 (A) 3068 (A) 3000 (A)
35 3416 (A) 3268 (A) 3154 (A) - - -
40 3242 (A) - - - - -

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 6 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION ON – WINGSTAB OFF
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-35 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-30 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-25 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-20 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-15 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-10 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
-5 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
0 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
5 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)
10 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O) 4800 (O)

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 7
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION ON – WINGSTAB OFF
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 4800 (O) 4800 (O) 4651 (A) 4497 (A) 4349 (A) 4254 (A)
-35 4800 (O) 4800 (O) 4656 (A) 4502 (A) 4354 (A) 4257 (A)
-30 4800 (O) 4800 (O) 4660 (A) 4506 (A) 4358 (A) 4260 (A)
-25 4800 (O) 4800 (O) 4665 (A) 4511 (A) 4362 (A) 4264 (A)
-20 4800 (O) 4800 (O) 4670 (A) 4515 (A) 4367 (A) 4267 (A)
-15 4800 (O) 4800 (O) 4674 (A) 4519 (A) 4371 (A) 4270 (A)
-10 4800 (O) 4800 (O) 4679 (A) 4524 (A) 4375 (A) 4273 (A)
-5 4800 (O) 4800 (O) 4684 (A) 4528 (A) 4379 (A) 4277 (A)
0 4800 (O) 4800 (O) 4688 (A) 4532 (A) 4384 (A) 4280 (A)
5 4800 (O) 4800 (O) 4691 (A) 4536 (A) 4388 (A) 4283 (A)
10 4800 (O) 4800 (O) 4690 (A) 4535 (A) 4386 (A) 4245 (E)

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2. AFM-2655

5-25 ANAC APPROVED

Page 8 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION ON – WINGSTAB OFF
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 4800 (O) 4738 (A) 4571 (A) 4408 (A) 4258 (A) 4108 (A)
-35 4800 (O) 4743 (A) 4575 (A) 4412 (A) 4261 (A) 4112 (A)
-30 4800 (O) 4748 (A) 4580 (A) 4416 (A) 4265 (A) 4116 (A)
-25 4800 (O) 4753 (A) 4584 (A) 4420 (A) 4269 (A) 4121 (A)
-20 4800 (O) 4758 (A) 4589 (A) 4424 (A) 4273 (A) 4125 (A)
-15 4800 (O) 4763 (A) 4593 (A) 4428 (A) 4277 (A) 4129 (A)
-10 4800 (O) 4763 (A) 4595 (A) 4432 (A) 4280 (A) 4132 (A)
-5 4800 (O) 4763 (A) 4597 (A) 4435 (A) 4284 (A) 4136 (A)
0 4800 (O) 4763 (A) 4597 (A) 4437 (A) 4287 (A) 4140 (A)
5 4800 (O) 4762 (A) 4598 (A) 4438 (A) 4289 (A) 4142 (A)
10 4800 (O) 4761 (A) 4595 (A) 4433 (A) 4285 (A) 4140 (A)

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 9
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION ON – WINGSTAB OFF
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 3961 (A) 3831 (A) 3708 (A) 3589 (A) 3473 (A) 3399 (A)
-35 3965 (A) 3835 (A) 3712 (A) 3593 (A) 3477 (A) 3401 (A)
-30 3969 (A) 3839 (A) 3715 (A) 3596 (A) 3480 (A) 3404 (A)
-25 3973 (A) 3842 (A) 3719 (A) 3600 (A) 3483 (A) 3406 (A)
-20 3977 (A) 3846 (A) 3722 (A) 3603 (A) 3487 (A) 3409 (A)
-15 3980 (A) 3849 (A) 3726 (A) 3606 (A) 3490 (A) 3411 (A)
-10 3984 (A) 3852 (A) 3729 (A) 3610 (A) 3493 (A) 3414 (A)
-5 3988 (A) 3856 (A) 3732 (A) 3613 (A) 3496 (A) 3416 (A)
0 3991 (A) 3859 (A) 3736 (A) 3616 (A) 3499 (A) 3418 (A)
5 3994 (A) 3863 (A) 3739 (A) 3619 (A) 3502 (A) 3421 (A)
10 3993 (A) 3862 (A) 3738 (A) 3618 (A) 3502 (A) 3419 (A)

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2. AFM-2655

5-25 ANAC APPROVED

Page 10 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 1 – LANDING FLAP 3
ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 4307 (A) 4241 (A) 4101 (A) 3961 (A) 3831 (A) 3702 (A)
-35 4310 (A) 4245 (A) 4104 (A) 3964 (A) 3834 (A) 3706 (A)
-30 4313 (A) 4250 (A) 4108 (A) 3968 (A) 3838 (A) 3710 (A)
-25 4316 (A) 4254 (A) 4112 (A) 3971 (A) 3841 (A) 3713 (A)
-20 4319 (A) 4259 (A) 4116 (A) 3975 (A) 3844 (A) 3717 (A)
-15 4323 (A) 4263 (A) 4119 (A) 3978 (A) 3848 (A) 3721 (A)
-10 4323 (A) 4264 (A) 4122 (A) 3982 (A) 3851 (A) 3724 (A)
-5 4323 (A) 4265 (A) 4124 (A) 3985 (A) 3854 (A) 3727 (A)
0 4321 (A) 4263 (A) 4124 (A) 3988 (A) 3857 (A) 3731 (A)
5 4319 (A) 4261 (A) 4124 (A) 3989 (A) 3859 (A) 3733 (A)
10 4317 (A) 4259 (A) 4121 (A) 3985 (A) 3855 (A) 3731 (A)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP ALTITUDE
(°C)
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 3573 (A) 3458 (A) 3349 (A) 3241 (A) 3153 (A) 3100 (A)
-35 3577 (A) 3461 (A) 3352 (A) 3244 (A) 3156 (A) 3102 (A)
-30 3580 (A) 3465 (A) 3355 (A) 3247 (A) 3158 (A) 3104 (A)
-25 3584 (A) 3468 (A) 3358 (A) 3250 (A) 3161 (A) 3105 (A)
-20 3587 (A) 3471 (A) 3362 (A) 3254 (A) 3163 (A) 3107 (A)
-15 3591 (A) 3474 (A) 3365 (A) 3257 (A) 3165 (A) 3109 (A)
-10 3594 (A) 3478 (A) 3368 (A) 3260 (A) 3168 (A) 3111 (A)
-5 3598 (A) 3481 (A) 3371 (A) 3263 (A) 3170 (A) 3113 (A)
0 3601 (A) 3484 (A) 3374 (A) 3266 (A) 3172 (A) 3115 (A)
5 3604 (A) 3486 (A) 3376 (A) 3268 (A) 3175 (A) 3116 (A)
10 3602 (A) 3485 (A) 3375 (A) 3266 (A) 3175 (A) 3106 (A)

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 11
 TM

PHENOM 100
Airplane Flight Manual
Performance

MAXIMUM LANDING WEIGHT – CLIMB LIMITED

APPROACH FLAP 2 – LANDING FLAP FULL
ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
PW617F-E ENGINES

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
-1000 ft 0 ft 1000 ft 2000 ft 3000 ft 4000 ft
-40 3669 (A) 3611 (A) 3489 (A) 3369 (A) 3258 (A) 3163 (A)
-35 3672 (A) 3614 (A) 3492 (A) 3372 (A) 3261 (A) 3165 (A)
-30 3674 (A) 3618 (A) 3495 (A) 3375 (A) 3264 (A) 3168 (A)
-25 3677 (A) 3622 (A) 3499 (A) 3378 (A) 3266 (A) 3170 (A)
-20 3679 (A) 3626 (A) 3502 (A) 3381 (A) 3269 (A) 3173 (A)
-15 3682 (A) 3629 (A) 3504 (A) 3384 (A) 3272 (A) 3175 (A)
-10 3683 (A) 3630 (A) 3506 (A) 3387 (A) 3275 (A) 3177 (A)
-5 3683 (A) 3630 (A) 3507 (A) 3389 (A) 3277 (A) 3180 (A)
0 3682 (A) 3629 (A) 3508 (A) 3391 (A) 3280 (A) 3182 (A)
5 3680 (A) 3629 (A) 3509 (A) 3392 (A) 3281 (A) 3183 (A)
10 3678 (A) 3628 (A) 3507 (A) 3389 (A) 3278 (A) 3181 (A)

MAXIMUM LANDING WEIGHT – CLIMB LIMITED (kg)

TEMP
(°C) ALTITUDE
5000 ft 6000 ft 7000 ft 8000 ft 9000 ft 10000 ft
-40 3075 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
-35 3078 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
-30 3080 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
-25 3082 (A) 3003 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
-20 3085 (A) 3005 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
-15 3087 (A) 3007 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
-10 3089 (A) 3009 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
-5 3091 (A) 3011 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
0 3094 (A) 3013 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
5 3096 (A) 3015 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)
10 3095 (A) 3015 (A) 3000 (A) 3000 (A) 3000 (A) 3000 (A)

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

used for dispatch.
- Applicable to airplanes Post-Mod. SB 500-27-0003 or with an
equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 12 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCES

Unfactored landing distance is the actual distance to land the airplane
from a point 50 ft above runway threshold to complete stop, using the
landing technique described in the beginning of this section.
Unfactored Landing Distance tables are presented for a set of
pressure altitudes and winds for the conditions below:
 Dry runway;
 Zero slope;
 Ice Protection System:
For Wingstab OFF, Engine Ice Protection OFF or ON,
For Wingstab ON, Engine Ice Protection ON;
 Temperature: ISA;
 No SAT effect;
 No VREF Overspeed;
 No Drag Index.

NORMAL OPERATION
The required landing distance for dispatch is the unfactored landing
distance increased by a factor according to the operating regulations.

EXAMPLE
Given:
Airplane Landing Weight .................................... 4000 kg
Airport Pressure Altitude .................................... 2000 ft
Engine Ice Protection ......................................... OFF
Wingstab............................................................. OFF
Flap..................................................................... 3
Wind.................................................................... 10 kt
Determine:
Unfactored Landing Distance ............................. 793 m
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 13
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3 – ISA CONDITIONS
PW617F-E 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
3200 849 705 660 615 865 720 674 629
3300 843 700 655 610 858 714 669 624
3400 847 705 659 615 863 719 674 629
3500 864 720 674 630 880 735 689 644
3600 878 734 688 643 895 749 703 657
3700 893 748 701 656 910 763 717 671
3800 908 762 715 670 926 778 731 685
3900 924 777 730 684 941 793 745 699
4000 940 791 744 698 957 808 760 714
4100 954 805 757 710 972 822 774 727
4200 970 820 772 725 988 837 789 741
4300 986 835 787 739 1005 853 804 756
4400 1003 850 802 754 1022 869 820 772
4500 1018 864 816 768 1037 883 834 785
4600 1035 880 831 783 1055 899 849 801
4700 1050 895 845 797 1070 914 864 815
4800 1065 909 859 811 1086 929 879 829

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 14 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3 – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 1000 ft 2000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 880 735 688 643 895 749 702 656
3300 873 729 683 638 888 743 697 651
3400 879 734 688 643 894 748 702 657
3500 895 750 703 658 911 765 718 672
3600 911 764 718 672 927 780 733 687
3700 927 779 732 686 943 795 747 701
3800 943 794 747 700 960 810 762 716
3900 959 809 762 715 976 826 778 731
4000 975 825 777 730 993 842 793 746
4100 990 839 790 743 1008 856 807 760
4200 1007 855 806 758 1026 872 823 775
4300 1024 871 822 774 1043 889 839 791
4400 1042 887 838 789 1061 905 856 807
4500 1057 902 852 803 1077 920 870 821
4600 1075 918 868 819 1095 937 887 837
4700 1091 934 883 834 1112 953 902 852
4800 1107 949 898 848 1128 969 918 867

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 15
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3 – ISA CONDITIONS
PW617F-E 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
3200 911 764 717 671 928 780 732 686
3300 905 758 712 666 921 774 727 681
3400 910 764 717 672 927 780 733 687
3500 928 781 733 687 945 797 749 703
3600 944 796 748 702 962 812 765 718
3700 961 811 764 717 979 828 780 733
3800 978 827 779 732 996 844 796 749
3900 995 843 795 747 1014 861 812 764
4000 1012 859 811 763 1031 878 828 780
4100 1028 874 825 777 1047 893 843 795
4200 1045 891 841 793 1066 910 860 811
4300 1063 908 858 809 1084 927 877 828
4400 1082 925 875 825 1103 945 894 845
4500 1098 940 890 840 1120 961 910 860
4600 1117 958 907 857 1139 979 927 877
4700 1134 974 923 872 1156 995 943 893
4800 1151 990 938 888 1174 1012 960 909

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 16 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3 – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 5000 ft 6000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 945 796 748 702 963 813 765 718
3300 938 790 743 696 957 807 759 713
3400 944 796 749 702 963 813 766 719
3500 963 813 766 719 982 831 783 736
3600 980 830 781 734 1000 848 799 752
3700 998 846 798 750 1018 865 816 768
3800 1015 863 814 766 1036 882 833 784
3900 1033 879 830 782 1054 899 849 801
4000 1051 897 847 798 1073 917 867 818
4100 1068 912 862 813 1090 933 882 833
4200 1087 930 879 830 1109 951 900 850
4300 1106 947 897 847 1128 969 918 868
4400 1125 966 915 864 1148 987 936 885
4500 1142 982 930 880 1166 1004 952 901
4600 1162 1000 948 898 1186 1023 971 920
4700 1180 1017 965 914 1204 1040 988 936
4800 1198 1034 982 930 1223 1058 1005 953

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 17
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3 – ISA CONDITIONS
PW617F-E 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
3200 983 831 783 736 1003 850 802 754
3300 976 825 777 730 996 844 796 748
3400 982 832 784 736 1003 851 802 755
3500 1002 850 802 754 1023 870 821 773
3600 1020 867 818 770 1042 887 838 789
3700 1039 884 835 787 1060 905 855 806
3800 1057 902 852 804 1080 923 873 824
3900 1076 920 870 821 1099 941 891 841
4000 1095 938 887 838 1119 960 909 859
4100 1113 954 903 854 1137 976 925 875
4200 1132 973 921 871 1157 995 944 893
4300 1152 991 940 889 1177 1015 963 912
4400 1173 1010 958 907 1198 1034 982 930
4500 1191 1028 975 924 1217 1052 999 947
4600 1211 1047 994 943 1238 1072 1019 966
4700 1230 1065 1012 960 1257 1090 1036 984
4800 1249 1083 1029 977 1277 1108 1054 1001

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 18 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP 3 – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 9000 ft 10000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 1045 888 837 788 1088 926 874 824
3300 1038 881 831 782 1080 919 868 818
3400 1045 888 838 789 1088 927 875 825
3500 1066 908 857 808 1110 947 895 845
3600 1085 926 875 825 1130 966 914 863
3700 1105 945 893 843 1151 986 933 881
3800 1125 963 912 861 1172 1006 952 900
3900 1145 983 931 880 1193 1026 972 919
4000 1166 1002 949 898 1214 1046 992 939
4100 1184 1020 967 915 1234 1064 1010 957
4200 1205 1039 986 934 1256 1085 1030 977
4300 1227 1060 1006 953 1278 1106 1051 997
4400 1249 1080 1026 973 1301 1128 1072 1017
4500 1268 1099 1044 991 1322 1147 1091 1036
4600 1290 1119 1065 1011 1345 1169 1112 1057
4700 1311 1138 1083 1029 1366 1189 1132 1076
4800 1331 1158 1102 1047 1387 1209 1152 1095

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 19
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP FULL – ISA CONDITIONS
PW617F-E 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
3200 881 732 685 639 897 748 700 653
3300 872 724 678 632 888 739 692 646
3400 863 717 671 625 879 732 685 640
3500 856 711 665 620 871 726 679 634
3600 849 705 659 614 864 720 673 628
3700 849 705 660 615 865 720 674 629
3800 864 720 674 629 880 735 688 643
3900 878 733 686 641 894 748 701 656
4000 892 746 699 654 908 761 714 668
4100 906 759 712 666 923 775 728 681
4200 920 772 725 679 938 789 741 695
4300 935 786 739 692 953 803 755 708
4400 951 802 754 707 970 819 770 723
4500 966 815 767 720 985 833 784 737
4600 981 830 781 734 1000 847 798 751
4700 997 844 795 747 1016 862 813 765
4800 1012 859 809 761 1032 877 827 779

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 20 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP FULL – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 1000 ft 2000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 913 762 714 668 928 777 729 681
3300 903 754 707 660 919 769 721 674
3400 895 747 700 654 910 761 714 667
3500 887 740 693 648 902 755 707 661
3600 880 734 688 642 895 748 702 656
3700 880 735 688 643 895 749 703 657
3800 896 750 703 657 912 765 718 672
3900 911 763 716 670 927 778 731 685
4000 925 777 730 683 942 793 745 698
4100 940 791 743 697 957 807 759 712
4200 955 805 757 710 973 821 773 726
4300 970 819 771 724 988 836 788 740
4400 988 836 787 740 1006 853 804 756
4500 1004 850 801 753 1022 868 819 770
4600 1019 865 816 768 1038 883 833 785
4700 1036 880 831 782 1055 899 849 800
4800 1052 896 846 797 1072 914 864 815

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 21
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP FULL – ISA CONDITIONS
PW617F-E 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
3200 945 793 744 697 962 809 760 712
3300 935 784 736 689 952 800 752 704
3400 927 777 729 682 943 793 745 698
3500 919 770 723 676 935 786 738 691
3600 912 764 717 671 928 780 732 686
3700 912 765 718 672 929 781 733 687
3800 929 781 733 687 946 797 749 702
3900 944 795 747 701 962 811 763 716
4000 960 809 761 714 978 826 778 731
4100 975 824 776 728 994 841 793 745
4200 991 839 790 743 1010 857 808 760
4300 1007 854 805 757 1026 872 823 774
4400 1025 871 822 773 1045 890 840 791
4500 1042 886 837 788 1062 905 855 806
4600 1059 902 852 803 1079 922 871 822
4700 1076 918 868 818 1097 938 887 837
4800 1093 934 883 834 1114 954 903 853

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 22 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP FULL – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 5000 ft 6000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 980 825 776 728 999 843 794 745
3300 970 817 768 720 989 835 785 737
3400 961 809 761 713 980 827 778 730
3500 953 802 754 707 972 820 771 724
3600 946 796 748 702 964 813 765 718
3700 946 797 749 703 965 815 767 719
3800 964 814 766 719 983 832 783 736
3900 980 829 780 733 1000 847 798 750
4000 996 844 795 748 1016 863 814 765
4100 1013 859 810 762 1033 879 829 781
4200 1030 875 826 777 1050 895 845 796
4300 1046 891 841 792 1068 911 861 812
4400 1066 909 859 810 1088 929 879 829
4500 1083 925 875 825 1105 946 895 845
4600 1101 942 891 841 1123 963 912 861
4700 1118 958 907 857 1142 980 929 878
4800 1137 975 924 873 1160 998 946 894

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 23
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP FULL – ISA CONDITIONS
PW617F-E 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
3200 1019 862 812 763 1040 882 832 782
3300 1009 854 804 755 1030 873 823 774
3400 1000 846 796 748 1020 865 815 767
3500 991 838 790 742 1012 858 808 760
3600 984 832 783 736 1004 851 802 754
3700 985 833 785 737 1005 852 803 755
3800 1003 850 802 754 1024 870 821 772
3900 1020 866 817 769 1042 886 837 788
4000 1037 882 833 784 1059 903 853 804
4100 1055 899 849 800 1077 920 869 820
4200 1072 915 865 816 1095 937 886 836
4300 1090 932 881 832 1113 954 903 852
4400 1110 951 900 850 1134 973 922 871
4500 1129 968 917 866 1153 991 939 888
4600 1147 985 934 883 1172 1009 956 905
4700 1166 1003 951 900 1191 1027 974 922
4800 1185 1021 968 917 1211 1045 992 940

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 24 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION OFF/ON – WINGSTAB OFF
FLAP FULL – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 9000 ft 10000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 1083 921 869 818 1128 961 907 855
3300 1073 911 860 809 1117 951 898 846
3400 1063 903 852 802 1107 942 890 838
3500 1054 895 845 795 1098 934 882 831
3600 1046 888 838 788 1089 927 875 824
3700 1047 890 839 790 1090 928 876 826
3800 1067 908 858 808 1111 948 896 844
3900 1085 925 874 824 1130 966 913 861
4000 1104 943 891 841 1149 984 931 879
4100 1122 960 908 857 1169 1002 949 896
4200 1141 978 926 874 1189 1021 967 914
4300 1160 996 943 892 1209 1040 985 932
4400 1182 1016 963 911 1231 1061 1006 953
4500 1201 1035 981 929 1252 1080 1025 971
4600 1221 1053 999 947 1273 1100 1044 990
4700 1242 1072 1018 965 1294 1120 1064 1009
4800 1262 1092 1037 983 1315 1140 1083 1028

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 25
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP 3 – ISA CONDITIONS
PW617F-E 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
3200 1210 1036 980 925 1233 1058 1001 946
3300 1233 1057 1001 945 1256 1079 1023 967
3400 1256 1079 1023 967 1280 1102 1045 989
3500 1281 1103 1046 990 1306 1127 1069 1012
3600 1304 1125 1067 1011 1330 1149 1091 1034
3700 1328 1147 1089 1032 1354 1172 1113 1056
3800 1352 1170 1112 1054 1379 1195 1136 1078
3900 1377 1193 1134 1077 1404 1219 1160 1101
4000 1399 1215 1155 1097 1427 1241 1181 1123
4100 1425 1239 1179 1120 1453 1266 1206 1146
4200 1452 1264 1204 1145 1481 1292 1231 1172
4300 1477 1289 1228 1168 1507 1317 1256 1196
4400 1505 1315 1254 1193 1536 1344 1282 1221
4500 1532 1340 1279 1218 1563 1370 1308 1246
4600 1560 1367 1305 1243 1592 1397 1334 1273
4700 1587 1392 1329 1268 1619 1423 1360 1297
4800 1612 1416 1353 1291 1645 1447 1384 1321

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 26 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP 3 – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 1000 ft 2000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 1256 1079 1022 967 1277 1099 1042 986
3300 1279 1101 1044 988 1301 1122 1065 1008
3400 1304 1125 1067 1011 1327 1147 1089 1032
3500 1330 1150 1092 1035 1354 1172 1114 1056
3600 1355 1173 1114 1057 1379 1196 1137 1079
3700 1380 1196 1137 1079 1405 1220 1161 1103
3800 1405 1220 1161 1103 1431 1245 1185 1126
3900 1431 1245 1185 1126 1458 1270 1210 1151
4000 1455 1267 1207 1148 1482 1293 1233 1173
4100 1482 1293 1232 1172 1510 1320 1258 1198
4200 1510 1320 1258 1198 1539 1347 1285 1224
4300 1537 1345 1284 1223 1566 1373 1311 1250
4400 1566 1373 1310 1249 1596 1401 1339 1277
4500 1595 1400 1337 1275 1625 1429 1366 1303
4600 1624 1428 1364 1302 1656 1458 1394 1331
4700 1652 1454 1390 1327 1684 1485 1421 1357
4800 1678 1479 1415 1352 1711 1511 1446 1382

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 27
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP 3 – ISA CONDITIONS
PW617F-E 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
3200 1302 1123 1065 1008 1326 1146 1088 1031
3300 1326 1146 1088 1031 1351 1170 1111 1054
3400 1353 1171 1113 1055 1378 1195 1137 1079
3500 1381 1197 1138 1080 1407 1223 1163 1105
3600 1406 1222 1162 1104 1433 1248 1188 1129
3700 1433 1247 1187 1128 1460 1273 1213 1154
3800 1459 1272 1212 1152 1488 1299 1239 1179
3900 1487 1298 1237 1177 1516 1326 1265 1204
4000 1512 1322 1260 1200 1542 1350 1289 1228
4100 1540 1349 1287 1226 1571 1378 1316 1255
4200 1570 1377 1314 1253 1602 1407 1344 1282
4300 1598 1404 1341 1279 1631 1435 1372 1309
4400 1629 1433 1369 1307 1663 1465 1401 1338
4500 1659 1461 1397 1334 1693 1494 1429 1366
4600 1690 1490 1426 1363 1725 1524 1459 1395
4700 1719 1518 1453 1389 1755 1553 1487 1423
4800 1747 1545 1479 1415 1784 1580 1514 1449

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 28 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP 3 – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 5000 ft 6000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 1352 1170 1112 1054 1379 1196 1137 1079
3300 1378 1195 1136 1078 1406 1222 1163 1104
3400 1406 1221 1162 1104 1435 1249 1189 1130
3500 1435 1249 1189 1131 1465 1278 1217 1158
3600 1462 1275 1215 1155 1493 1304 1243 1183
3700 1490 1301 1240 1181 1522 1331 1270 1209
3800 1518 1328 1267 1207 1551 1359 1297 1236
3900 1547 1356 1294 1233 1580 1387 1324 1263
4000 1574 1381 1318 1257 1608 1413 1350 1288
4100 1604 1409 1346 1284 1638 1442 1378 1316
4200 1635 1439 1375 1313 1671 1472 1408 1345
4300 1665 1467 1403 1341 1702 1502 1437 1374
4400 1697 1498 1433 1370 1734 1533 1468 1404
4500 1729 1528 1463 1399 1767 1564 1498 1433
4600 1762 1559 1493 1428 1800 1596 1529 1464
4700 1793 1588 1522 1457 1832 1626 1559 1493
4800 1822 1616 1549 1484 1862 1654 1587 1521

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 29
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP 3 – ISA CONDITIONS
PW617F-E 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
3200 1409 1224 1165 1106 1440 1253 1193 1134
3300 1437 1251 1191 1132 1468 1280 1220 1160
3400 1466 1278 1218 1159 1498 1309 1248 1188
3500 1497 1308 1247 1187 1530 1339 1277 1217
3600 1526 1335 1274 1213 1559 1367 1305 1244
3700 1555 1363 1301 1240 1589 1395 1333 1271
3800 1585 1391 1329 1267 1620 1424 1361 1299
3900 1615 1420 1357 1295 1651 1454 1390 1328
4000 1643 1447 1383 1321 1680 1481 1417 1354
4100 1675 1477 1412 1349 1712 1512 1447 1384
4200 1708 1508 1443 1380 1746 1544 1479 1415
4300 1740 1538 1473 1409 1779 1575 1509 1445
4400 1774 1570 1504 1440 1814 1608 1542 1476
4500 1807 1602 1535 1470 1848 1641 1574 1508
4600 1841 1634 1567 1502 1883 1674 1607 1540
4700 1874 1665 1598 1531 1917 1706 1638 1571
4800 1905 1695 1627 1560 1948 1736 1668 1600

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 30 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP 3 – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 9000 ft 10000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 1501 1309 1247 1186 1564 1367 1303 1241
3300 1531 1337 1275 1214 1596 1397 1332 1269
3400 1562 1367 1304 1242 1629 1428 1363 1299
3500 1595 1399 1335 1273 1663 1461 1396 1331
3600 1626 1428 1364 1301 1696 1492 1426 1361
3700 1658 1458 1393 1330 1729 1523 1456 1391
3800 1690 1488 1423 1359 1762 1555 1488 1422
3900 1723 1519 1454 1389 1797 1587 1520 1453
4000 1753 1548 1482 1417 1828 1617 1549 1482
4100 1787 1580 1514 1448 1864 1651 1582 1515
4200 1822 1614 1547 1480 1901 1686 1617 1549
4300 1856 1646 1579 1512 1937 1720 1651 1582
4400 1893 1681 1612 1545 1975 1757 1686 1617
4500 1929 1715 1646 1578 2012 1792 1721 1651
4600 1965 1750 1680 1612 2051 1829 1757 1686
4700 2001 1783 1713 1644 2088 1864 1792 1720
4800 2034 1815 1744 1674 2122 1897 1824 1752

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 31
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP FULL – ISA CONDITIONS
PW617F-E 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
3200 1210 1032 975 918 1233 1053 995 939
3300 1234 1054 996 940 1257 1076 1018 960
3400 1255 1075 1017 960 1279 1097 1038 981
3500 1279 1097 1038 981 1303 1120 1061 1003
3600 1303 1120 1061 1003 1328 1143 1084 1026
3700 1325 1141 1081 1023 1350 1165 1105 1046
3800 1347 1162 1102 1043 1373 1186 1126 1067
3900 1370 1183 1123 1064 1397 1209 1148 1089
4000 1394 1206 1145 1086 1421 1232 1171 1111
4100 1418 1229 1168 1108 1446 1255 1194 1133
4200 1444 1254 1192 1132 1473 1281 1219 1158
4300 1471 1279 1217 1156 1501 1307 1244 1183
4400 1501 1307 1244 1183 1531 1335 1272 1210
4500 1530 1334 1271 1209 1561 1364 1300 1237
4600 1557 1360 1296 1234 1589 1390 1326 1262
4700 1588 1389 1325 1262 1621 1420 1355 1291
4800 1616 1416 1351 1287 1649 1447 1382 1317

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 32 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP FULL – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 1000 ft 2000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 1255 1074 1016 959 1275 1093 1035 977
3300 1279 1097 1039 981 1300 1117 1058 1000
3400 1302 1119 1060 1002 1324 1139 1080 1022
3500 1327 1143 1083 1025 1349 1164 1104 1045
3600 1353 1167 1107 1048 1376 1189 1128 1069
3700 1376 1188 1128 1069 1399 1211 1150 1091
3800 1399 1211 1150 1091 1424 1234 1173 1113
3900 1423 1234 1173 1113 1449 1258 1196 1136
4000 1448 1257 1196 1135 1474 1282 1220 1159
4100 1474 1281 1219 1158 1500 1307 1244 1183
4200 1501 1308 1245 1184 1529 1334 1271 1209
4300 1530 1334 1271 1209 1558 1361 1298 1235
4400 1561 1364 1300 1237 1590 1391 1327 1264
4500 1592 1393 1328 1265 1621 1421 1356 1293
4600 1620 1420 1355 1291 1651 1449 1383 1319
4700 1653 1450 1385 1321 1684 1480 1414 1349
4800 1682 1478 1412 1347 1714 1509 1442 1377

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 33
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP FULL – ISA CONDITIONS
PW617F-E 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
3200 1298 1115 1057 999 1322 1138 1078 1020
3300 1324 1140 1081 1023 1348 1163 1103 1045
3400 1349 1163 1104 1045 1373 1187 1127 1068
3500 1375 1188 1128 1069 1401 1212 1152 1092
3600 1402 1214 1153 1093 1428 1239 1178 1118
3700 1426 1237 1176 1116 1453 1263 1201 1140
3800 1451 1261 1199 1138 1479 1287 1225 1164
3900 1477 1285 1223 1162 1506 1312 1250 1188
4000 1503 1310 1247 1186 1533 1338 1275 1213
4100 1530 1335 1272 1210 1560 1364 1300 1238
4200 1560 1363 1299 1237 1590 1392 1328 1265
4300 1589 1391 1327 1264 1621 1421 1357 1293
4400 1622 1422 1357 1294 1655 1453 1388 1324
4500 1654 1452 1387 1323 1688 1484 1419 1354
4600 1684 1481 1415 1350 1719 1513 1447 1382
4700 1718 1513 1447 1381 1754 1547 1480 1414
4800 1750 1542 1475 1409 1786 1577 1509 1443

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 34 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP FULL – ISA CONDITIONS
PW617F-E ENGINES

ALTITUDE
Weight 5000 ft 6000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 1346 1161 1102 1043 1374 1187 1127 1068
3300 1374 1187 1127 1068 1402 1214 1153 1094
3400 1400 1212 1151 1092 1428 1239 1178 1118
3500 1428 1238 1177 1117 1457 1266 1204 1144
3600 1456 1265 1204 1143 1487 1294 1232 1171
3700 1482 1290 1228 1167 1513 1319 1257 1195
3800 1509 1315 1252 1191 1540 1345 1282 1220
3900 1536 1341 1278 1216 1568 1371 1308 1245
4000 1564 1367 1304 1241 1597 1398 1334 1271
4100 1592 1394 1330 1267 1626 1426 1362 1298
4200 1623 1423 1359 1295 1658 1456 1391 1327
4300 1654 1453 1388 1324 1690 1487 1421 1356
4400 1689 1485 1420 1355 1725 1520 1454 1388
4500 1723 1518 1451 1386 1760 1553 1486 1420
4600 1754 1548 1481 1415 1793 1584 1516 1450
4700 1790 1582 1514 1447 1830 1619 1551 1483
4800 1823 1613 1544 1477 1863 1651 1582 1514

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 35
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP FULL – ISA CONDITIONS
PW617F-E 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
3200 1403 1214 1154 1094 1433 1243 1182 1122
3300 1432 1242 1181 1121 1463 1271 1210 1149
3400 1459 1268 1206 1146 1491 1298 1236 1175
3500 1489 1296 1234 1173 1521 1327 1264 1202
3600 1519 1324 1262 1200 1552 1356 1293 1230
3700 1546 1350 1287 1225 1580 1383 1319 1256
3800 1574 1377 1313 1251 1609 1410 1345 1282
3900 1603 1404 1340 1277 1638 1438 1373 1309
4000 1632 1432 1367 1304 1668 1466 1401 1336
4100 1662 1460 1395 1331 1699 1495 1429 1364
4200 1695 1491 1425 1361 1732 1527 1460 1395
4300 1728 1522 1456 1391 1766 1559 1492 1426
4400 1764 1557 1490 1424 1803 1594 1527 1460
4500 1800 1591 1523 1456 1840 1629 1561 1493
4600 1833 1622 1554 1487 1875 1662 1593 1525
4700 1871 1658 1589 1521 1914 1699 1629 1560
4800 1906 1691 1621 1553 1949 1732 1662 1593

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

5-25 ANAC APPROVED

Page 36 code 01 REVISION 16
 TM

PHENOM 100
Airplane Flight Manual
Performance

UNFACTORED LANDING DISTANCE (m)

ENGINE ICE PROTECTION ON
WINGSTAB ON (SWPS ICE SPEED)
FLAP FULL – ISA CONDITONS
PW617F-E ENGINES

ALTITUDE
Weight 9000 ft 10000 ft
(kg)
WIND
-10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
3200 1494 1298 1235 1173 1556 1355 1290 1226
3300 1525 1328 1264 1202 1589 1386 1321 1256
3400 1554 1356 1292 1229 1620 1416 1350 1285
3500 1586 1386 1321 1257 1653 1447 1381 1315
3600 1619 1416 1351 1287 1687 1479 1412 1346
3700 1648 1444 1379 1314 1718 1509 1441 1374
3800 1678 1473 1407 1341 1750 1538 1470 1403
3900 1709 1502 1435 1370 1782 1569 1500 1433
4000 1740 1532 1465 1398 1815 1600 1531 1463
4100 1772 1562 1494 1428 1848 1632 1562 1494
4200 1807 1596 1527 1460 1885 1667 1597 1527
4300 1843 1629 1560 1492 1922 1702 1631 1561
4400 1882 1666 1596 1528 1963 1741 1669 1598
4500 1921 1703 1632 1563 2004 1779 1707 1635
4600 1956 1737 1666 1596 2041 1815 1742 1670
4700 1997 1775 1704 1633 2084 1855 1781 1709
4800 2034 1811 1738 1667 2123 1892 1818 1744

CAUTION: SHADED AREAS REPRESENT CONDITIONS WHERE

THE MAXIMUM LANDING WEIGHT OR CLIMB LIMITED
WEIGHT WAS EXCEEEDED.

NOTE: Applicable to airplanes Post-Mod. SB 500-27-0003 or with an

equivalent modification factory incorporated, for airplanes
Pre-Mod. SB 500-27-0003, refer to Supplement 2.
AFM-2655

ANAC APPROVED 5-25

REVISION 16 code 01 Page 37
 TM

PHENOM 100
Airplane Flight Manual
Performance

INTENTIONALLY BLANK

AFM-2655

5-25 ANAC APPROVED

Page 38 code 01 REVISION 16