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TYPE CERTiFICATE DATA $HEET No. EA-2008T09 EA-2008T09-0

Type Certificate HolderSheet 01

EMBRAEREMBRAER S.A.Av. Brigadeiro Faria Lima, 2.1701 2 227-901 -- S.J. dos Campos -- SPBrazil

EMB-500

) l\Hay 201

This data sheet. which is part of Type Certificate No. 2008T09, prescribes conditions and limitations under which theproduct. for which the Type Certificate was issued, meets the alrworthiness requirements of the Brazilian Civil AviationRegulations

1 -- Modem EMB-500 ÍNorma! Categor- approved on 09 December 2008

ENGANE Two Pratt & Whitney Canada PW61 7F-E turbofans for PHENOM 1 00and PHENOM 1 00E (see NOTE 6).Two Prata & Whitney Canada PW617Fl-E turbofans for PHENOM1 00EV (see NOTE 6).IANAC TCDS No. EM-2008T081.

FUEL Brazilian Specification ANP No. 1/2006, QAV-l .Specification ASTM-DI 655, type Jet A. Jet A-l .Specification MIL-DTL-831 33, type JP-8.Chinese Specification GB6537-2006 N'3 Jet Fuel

ENGINE LIMITS Static thrust limits, standard day, sea levei

For PW61 7F-E engine (see NOTE 7)

STANDARD TAKE.OFF THRUST

ENHAiqCED TAKEOFF THRUST

Takeoff (5 min)ATR (IO min)

753.9 daN (1 695 lb)765.1 daN (1 720 lb)

753.9 daN (1 695 lb)809.6 daN (1 820 lb)

Max. permissible engine rotor operating speeds0'akeoff and Maximum Continuous):NI (Fan) 1 00% (1 00% = 19 845 rpm)NI Transient (operation 20 sec) 101% (101% = 20 043 rpm)N2(Gas Gen.) 1 00.4%(1 00.4% = 40 200 rpm)N2 Transient (operation 20 sec) 1 02% (1 02% = 40 840 rpm)

EMBRAER 10 May 2017 EA-2008T09. Sheet 2/9

ENGANE LIMITA(cont'd)

Max. permissible interturbine gas temperatures:Takeoff (5 min) 830 'CATR (1 0 mini 845 'CMax. continuous 830 'CTransient (starting 5 sec) 892 'C (950 'C) (see NOTE 8)Transient (operation 20 sec) 862 'C

For PW61 7FI -E engine

Takeoff (5 min)ATR (lO mini

768.6 daN (1 728 lb)841.1 daN (1891 lb)

Max. permissible engine rotor operating speeds0'akeoff and Maximum Continuous) :NI (Fan) 1 00% (1 00% = 19 845 rpm)NI Transíent (operation 20 sec) 101% (101% = 20 043 rpm)N2(Gas Gen.) IO1 .6%(IO1 .6% = 40 676 rpm)N2 Transient(operation 20 sec) 103.2%(103.2% = 41 316 rpm)

Max, permissible interturbine gas temperaturesTakeoff (5 min) 830 'CATR (1 0 mini 845 'CMax, Continuous 830 'CTransient (starting 5 sec) 950 'CTransient (operation 20 sec) 862 'C

AIRSPEED LiMITS (IAS}

Note: The values presented above refer to the maximum vMC for theaircraft envelope jthe values can change according to the temperatureand altitude).

  km/h (knots) Mach

Maximum operating (Vwo):Sea levei to 28 000 ft. 509 3 (275) 0.70

Maximum operating (Mhao):Above 28 000 ft.   0.70

Maneuvering (vA) - sea levei: 345.0 (186)  Flaps extended (vFEI10' (takeofD:26' (takeoff and landing):36' (landing)

370.4 (200)296.3 (160)268.5 (145)  

Minimum control speed - Air (Vuc):Takeoff 1 80 (97)  

Maximum tire ground speed: 257.4 (139)  L. G. operation - extend (VLO): 333.4 (180)  L. G. operation - retract (VLO): 333.4 (180)  L. G. extended (VLE): 509.3 (275)  

EMBRAER 1 0 h/lay 201 7 EA-2008T09-09 Sheet 3/9

CG RANGE For PHENOM 1 00 and PHENO1\d l ooE (see NOTE 61Forward Limits:

Takeoff and Landing Conditions:Linear variation from 5.90 m (232.24 in) aft of datum (35% MAC) at 3000 kg l6 614 lb) to 5.68 m (223.53 in) aft of datum (21 .5% MAC) at3 220 kg (7 099 1b);Constant value of 5.68m (223.53 in) aft of datum (21 .5% MAC) at 3220 kg l7 099 lb) to 4 030 kg (8 885 lb);Linear variatlon from 5.68 m (223.53 in) aft of datum (21 .5% MAC) at4 030 kg (8 885 lb) to 5.71 m (224.82 in) aft of datum (23.5% MAC)at 4 750 kg (1 0 472 lb); andConstant value of 5.71 m (224.82 in) aft of datum (23.59á MAC) at 4750 kg 110 472 lb) to 4 770 kg(l0 516 lb)

Aft Limits:

Landing Conditions:Linear variation from 5.90 m 1232.24 in) aft of datum (35% MAC) at 3000 kg l6 61 4 lb) t0 5.96 m (234.50 in) aft of datum (38.5 % MACA at3 420 kg (7 540 1b);Constant value of 5.96 m (234.5 in) aft of datum (38.5 % MAC) at 3420 kg(7 540 lb) t0 4 030 kg(8 885 lb);Linear variation from 5.96 m (234.50 in) aft of datum (38.5% MAC) at4 030 kg (8 885 lb) to 5.93 m (233.47 in) aft of datum (36.9 % MAC)at 4 750 kg (1 0 472 lb); andConstant value of 5.93 m (233.47 in) aft of datum (36.9 % MAC) at 4750 kg ll 0 472 lb) t0 4 770 kg(l0 516 lb).

For PHENOM 1 00EV (see NOTE 6)Forward Limits

Takeo# and Landlng ConditionsLinear vanation from 5.90 m (232.24 in) aft of datum (35% MAC) at 3O1 9,96 kg (6 658 lb) to 5.68 m 1223.53 in) aft of datum (21 .5% l\4AC)at 3 220 kg (7 099 lb)Constant value of 5.68m (223.53 in) aft of datum (21 .5% MAC) at 3220 kg(7 099 lb) to 4 030 kg(8 885 lb);Linear vanatlon from 5.68 m (223.53 in) aft of datum (21 .5% IVIAC) at4 030 kg (8 885 lb) t0 5.71 m (224.82 in) aft of datum (23.5% MAC)at 4 854,72 kg (1 0 7031b)l andConstant vague of 5.71 m (224.82 in) aft of Qatum (23.5% MAC) at 4854.72kg(l0 703 lb) to 4 874,78kg(l0 747 Êb).

Aft Limlts=

Landing ConditionsLinear variation from 5.90 m (232.24 in) aü of datum (35% iViAC) at 301 9.96 kg (6 6581b) t0 5.96 m (234.50 in) aft of datum (38.5 % MAC)at 3 420 kg (7 540 lb)Constant vague of 5.96 m (234.5 in) aft of datum (38.5 % iVIAC) at 3420 kg (7 540 lb) to 4 030 kg (8 885 lb)Linear varlation from 5.96 m (234.50 in) aft of datum (38.5% ÍVIAC) at4 030 kg (8 885 lb) to 5.93 m (233.47 in) aft of datum (36.9 % iXaACIat 4 854.72kg (1 0 7031b)l andConstant value of 5.93 m (233.47 in) aft of daíum (36.9 % MIAC) at 4854,72kg(l0 7031b) ta 4 874,78kg(1 0 747ibl

Landing Gear retracting moment: -1 7.63 m-kg (-1 530.22 in-lb)

EMBRAER 10 May 2017 EA-2008T09-09 Sheet 4/9

DATUM

LEVELING MEAN$

2.51 m (98.82 in) forward of the jig point (nose pack pad location)

Located in the main doou between frames 9 and 1 0 (see AMM for furtherinformation) .

MEAN AERODYNAMIC CHORD 1 .64 m(64.57 in.)(L.E. of MAC at+5.32 m(209.65 in.) aft of datum)

MAXIMUM WEIGHT Takeoff: 475048004855

kgkgkgkgkgkgkgkgkgkgkgkgkgkg

jl0 472 1b)11 0 582 ib) I")11 0 703 lb) l"")l9 766 ib)(9 877 1b) (")l9 998 ib) ("")(8 444 1b)l8 775 1b) (*)l8 554 ib) (")l8 80S ib) ("*)lO 072 1b) ("")(I0 516 1b)(l 0 626 1b) (")11 0 747 ib) l"")

Landing: 44304480453538303980388040304115

Zero Fuel

Ramp: 477048204875

Nomes:

1*) for aircraft post-mod SB 500-00-0005 0R with an equivalentmodification factory-incorporated.

1") for aircraft post-mod SB 500-00-0009 or SB 500-00-001 8 0R withan equivalent modification factory-incorporated.I') for aircraft post-mod SB 500-00-0005 and SB 500-00-0009 0raircraft post-mod SB 500-00-0005 and SB 500-00-001 8 0R with theequivalent modifications factory-incorporated.1"") for PHENOM 1 00EV aircraft (see NOTE 61.

MINIMUM CREW Crew for all fllghts (see NOTE 5 for cockpit equipmenl/ arrangementrestrlctions): one pilot (in the left pilot seat) plus additional equipment, asspecified in the Kinds of Operations Equipment List (KOEL) in theLimitations Section of the ANAC Approved Airplane Manual, OR onepivot and one copilot.

MAXIMUM OCCUPANTS Maximum eight ltwo crew plus six passengers or one crew plus sevenpassengers). Refer to the Airplane Flight Manual (AFM-2655), Section 6Weight & Balance. for seat configurations and moment arms.

MAXIMUM BAGGAGE Forward baggagecompartment

30 kg(66 lb)(+1 .16 m(45.47 in) aft ofdatuml .

AFT baggage compartment 1 60 kg (353 lb) (+7.98 m (314.27 in) aft ofdatum).

Wardrobe

Lavatory cabinet

30 kg(66 lb)(+3.64 m(143.46 in) aft ofdatum) .1 5 kg l33 lb) (+6.34 m (249.76 in) aft ofdatum) .

EMBRAER 1 0 May 201 7 EA-2008T09-09 Sheet 5/9

FUEL CAPACI'TY Total usable fuel 1 272 kg (2 806 lb). Two wing tanks with 636.4 kg (l403 lb) usable each (see NOTE l for unusable fuel) +5.87 m (230.91 in)aft of datum, considering density of 0.803 kg/1 (6.70 lb/US gal).

Oil CAPAGI'IY Tank mounted on each engine: 4 quarta (3.79 liters) total each engine+7.68 m(302.52 in.) aft of datum(see NOTE l).

HYDRAULIC FLUID CAPACI'íY 1 .4 kg(3.09 lb.) at+0.87 m(34.17 in.) aR of datum, considering densityof 0.846 kg/1 (7.06 lb/gal);

6.29 kg (1 3.86 lb) at +1 .30 m (51 .1 8 in.) aft of datum, considering densityof 0.846 kg/1 (7.06/gal) -- for aircraft with Second Hydraulic Power SourceInstalled.

MAXiMUM OPERATING ALTITUDE 1 2 497 m (41 000 ftl

TEMPERATURE OPERATINGLIMiTa

Maximum: 52 'CMinimum: -54 'C

CONTROL SURFACEMOVEMENTS

Elevator: upDown

upDown

27' +1 '/-1 '1 9' +1 '/-1 '

Elevator trim tab (*): 6' +1 '/-1 '1 3' +1 '/-1 '

Rudder: RightLeft

RightLeR

upDown

27' +1 '/-1 '27' +1 '/-1 '

Rudder trim tab l*) 1 6.5' +1 '/-1 '1 6.5' +1 '/-1 '

Aileron 25' +1 '/-1 '15' +1 '/-1 '

Aileron trim tab (*): upDown

20' +1 '/-1 '20' +1 '/-1 '

Wing flaps: TOTO / LandLand

10' +1 '/-1 '26' +1 '/-1 '36' +1 .5'/-1 .5'

Ground spoiler / Speed Upbrake I'):

31 .5o +lo/-l o

Notes:1*) valid only for neutral position. See Aircraft Maintenance ManualIAMM) for rigging instructions.1") for aircraft post-mod SB 500-27-0008 or with an equivalentmodification factory-incorporated.

SERIAL NUMBERS 50000005 and subsequent

EMBRAER 10 May 2017 EA-2008T09. Sheet 6/9

CERTIFICATION BASIS 1) Brazilian Type Certificate No. 2008T09 issued on 09 December2008. based on the RBHA 23, which endorses the 14 CFR Part 23,effective l Feb. 1 965, as amended by 23-1 through 23-55 effectiveon 01 Mar. 2002, and the following additional requirements:

2) No1se requirements:RBHA 36, corresponding to ICAO Annex 16 Volume 1, Chapter 4(Fourth Edition) effective Jul. 2005, as amended on the applicationdate

3) Emission requirerDQlllsRBHA 34, corresponding to US 14 CFR Part 34 effective 10 Sep.1 990, as amended on the application date.

4) Special Condition$;'Resolução N' 39", dated 15 Aug. 2008, Special Condition forSubpart G (Operating Limitations and Information) -- EMB-500FCAR EV-04.

ja)

:Resolução N' 43", dated 15 Aug. 2008, High IntensityRadiated Fields (HIRF) Protection - EMB-500 FCAR SE-02Resolução N' 44", dated 18 Aug.

Operation - EMB-500 FCAR PR-09.2008, Hot Weather

ld) 'Resolução N' 45". dated 18 Aug. 2008. Fere Extinguishing forAircraft Fuselage Mounted Engines -- EMB-500 FCAR PR-03.Resolução NO 46", dated 18 Aug. 2008, Special Condition for

FADEC - EMB-500 FCAR PR-07.

(D

Ig)

lh)

'Resolução N' 47". dated 18 Aug. 2008, Brakes - Designationof Applicable Regulations -- EMB-500 FCAR SM-02.'Resolução N' 56", dated 09 Oct. 2008, Airspeed IndicatingSystem - EMB-500 FCAR EV-02.Resolução N' 66". dated 26 Nov. 2008. Special Condition forPerformance and Flight Characteristics - EMB-500 FCAR EV-01

li) Resolução N' 177", dated 14 Dec. 2010, Dynamic TestRequirements for Single Peace Side Facing Seat -- EMB-500FCAR El-05 and FCAR El-07.

EMBRAER 1 0 May 2017 EA-2008T09. Sheet 7/9

CERTIFICATION BASl$(cont'd}

5) Equivalent leveis of $ feluja) "Decisão N' 302", dated 18 Aug. 2008.

23.1555(d)(1), Control Markings - UsableEMB-500 FCAR PR-05.

RBHN14 CFRFuel Capacity --

(b) "Decisão N' 306", dated 18 Aug. 2008, RBHA/14 CFR23.807(e)(2), Ditching Emergency Exit for Passengers -- EMB-500 FCAR El-03.

lc) "Decisão N' 381 ". dated 24 Sep. 2008, RBHA/14 CFR 23.1 553Digital Fuel Quantity Indication - EMB-500 FCAR PR-l l .

Id) 'Portaria NO 3.676", dated 13 Dec. 2016. RBHA/14 CFR23.1 305 and 23.1549, Digital Only Display of Turbine EngineHigh Pressure Rotor Speed (N2), Oil Pressure, OilTemperature and Fuel Flow -- EMB-500 FCAR PR-1 3, whichsuperseded "Decisão N' 303", dated 1 8 Aug. 2008 RBHA/14CFR 23.1305(c)(5), Digital Only Display of Turbine EnganeHigh/Intermediate Pressure Rotor Speed (N2) -- EMB-500FCAR PR-02.

6) Exemptionsja) "Decisão N' 383", dated 24 Sep. 2008, RBHA/14 CFR

23.181(b), Exemption for RBHA/14 CFR Pari 23.181jb),Dynamic Stability -- EMB-500 FCAR EV-05.

Compliance with ice protection has been demonstrated inaccordance wlth RBHA/14 CFR 23.1416 and 23.141 9.

7)

8)

9)

Compliance with the provisions for ditching equipment has beendemonstrated in accordance with RBHA/1 4 CFR 23.1 41 5(a)(b).RVSM Approval: S/N 50000005 and on: all airplanes are equippedwith Garmin avionics systems with RVSM capable Air DataComputers and pilot's and copilot's Primary Flight Displays asstandard equipment. Each operator must obtain RVSM operatingapproval directly from the Civil Aviation Authority.

PRODUCTION BASIS Production approved under ANAC COP No. E-7203-01 (Embraer S.A.Brazil) and FAA PC No. 346CE (Embraer Executive Aircraft Inc.,Melbourne, Florida).The manufacturer Embraer Executive Aircraft Inc. located in Melbourne.Florida, is licensed by Embraer S.A. to manufacture the Model Aircraftlisted in this Type Certificate Data Sheet. S/N 50000255 and subsequentmay be produced either by Embraer Executive Aircraft Inc. inMelbourne, Florida or Embraer S.A. in Brazil. The manufacturer can beconflrmed by the aircraft data plate. Aircraft produced by EmbraerExecutive Aircraft Inc. in Melbourne, Florida, with S/N from 50000255 to50000269 were produced under the Type Certificate

REQUIRED EQUIPMENT The basic required equipment. as prescribed in the applicableairworthiness regulations (see Certification Basis) must be installed inthe airplane for certification.

EMBRAER 1 0 ivlay 201 7 EA-2008T09-09 Sheet 8/9

NOTES

NOTE l We qht and balance:Current weight and balance report, including the list of equipment that are part of the certificatedbasic empty weight and loading instructions, must be provided for each aircraft at the time oforiginal certification.The certlficated empty weight and corresponding center of gravity location must include:Unusable fuel: 20 kg (44 lb) at +5.81 m (228.90 in.) aft of datumFull oil(*): 8 kg(17.64 lb) at +7.68 m(302.52 in) aft of datumHydraulic Fluid: 1 .4 kg (3.09 lb) at +0.87 m (34.1 7 in) aft of datum

6.29 kg(13.86 lb) at +1 .30 m(51 .18 in.) aft of datum I")

1*) considering the oil from the engine installation jfilters and lhes).1") for aircraft with Second Hydraulic Power Source installed.

NOTE 2 Markinqs and placards:All marking and placards required by the applicable certification requirements (see certificationbasics) and by the operational requirements must be installed in the appropriated locations.Required placards and marking are listed in the Chapter 1 1 of the Aircraft lllustrated Parts CatalogIAIPC) and in the Airplane Maintenance Manual (AMM).

NOTE 3 Continuinq Airworthiness:See the Maintenance Manual, Chapter 4 "Airworthiness Limitations", for Systems AirworthinessLimitations (CMR), Structure Airworthiness Limitations (ALI) and Life-Limited ltems (LLI).

The ltfe limit for rotating parts on the PW617F-E and the PW617Fl-E engines is in theAirworthiness Limitations Manual of the Prata & Whitney Canada Engine P/N 3072699, latestrevision.

NOTE 4 All replacement seats (crew and passenger), although they may comply with TSO-CI 27? mustalso be demonstrated to comply with installation requirements into the aircraft llsted in RBHA/1 4CFR 23.2, 23.561 , 23.562, and 23.785.The foam cushion buildup of all seats (crew and passenger) may not be altered. Any deviationsin the foam construction or sttffness must be demonstrated by test or analysis to comply with theRBHA/14 CFR 23.562.

NOTE 5 Approval for operation with a minimum crew of one pllot is based upon the cockpit equipmentinstallation and arrangement evaluated during ANAC certification testing.

No significant changes may be made to the Installed cockpit equipment or arrangement (EFIS.autopilot, avionics etc.), except as permitted by the approved MMEL, without prior approval fromthe Civil Aviation Authority.

NOTE 6 The EMB-500 is often referred to in Embraer marketing literature as the "PHENOM 100PHENOM 100E" or "PHENOM 1 00EV'. These names are strictly marketing designation and are

not part of the official model designation.PHENOM 1 00: EMB-500 equipped with PW61 7F-E engines and GI 000 avionics system;PHENOM 1 00E: EMB-500 equipped with PW617F-E engines, GI 000 avionics system andspoiler panelsl andPHENOM 1 00EV: EMB-500 equipped with PW61 7FI -E engines. G3000 avionics system andspoiler panels.

EMBRAER 1 0 1May 201 7 EA-2008T09-01 Sheet 9/9

NOTE 7 Aircraft with serial numbers 50000005 up to 5000021 7 are considered "E/VflH/VCEt) THKE.OF:F7HR(./ST' version. In order to identily the correct version for aircraft with serial number 5000021 8and on, the cockpit placard must be verified

NOTE 8 The increase in the Maximum ITT is an optional item available through SB 500-73-0001 for aircraftwith serial number 50000006 and 50000008 thru 50000024. For aircraü with serial number50000005, 50000007, 50000025 and on, there is an equivalent modification factory-incorporated.

NOTE 9

NOTE q O

Removed

Removed

Original in the Portuguesa language signed by

# ,\ 22./ .iGüníoNiii.Áw

General Manager, Aen:\naütical Product Certification

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