ATR -500 SERIES

The ATR 42-500 offers a combination of high overall performance and comfort unmatched in its class, while keeping the competitive economics which are the trademark of ATR aircraft. A range of improvements in the field of noise and vibration attenuation has been implemented, namely:

u An optimized, efficient and technologically advanced acoustic treatment of the structure with the installation of Dynamic Vibration Absorbers and skin damping.

u Cabin interiors engineered for maximum noise attenuation and optimum comfort, through advanced materials and absorbent panels and carpets. Additional overhead bins volume compared to previous models, accommodating long items (up to 2m/6.5 ft).The ATR 42-500 is equipped with 2 engines PW127, providing an excellent level of performance with an outstanding take-off and single engine performance maintained even in hot and high conditions.

ATR42-500U n R i V A l l e D P e R f o R m A n C e

THe RefeRenCe in ReGionAl AiR TRAnSPoRT

48 seats at 30” pitch

STAnDARD ConfiGURATion

ATR DC/E Marketing September 2014 The information contained in this document is presented in good faith and does not in any way constitute an offer or a warranty. Avions de Transport Régional - 1, allée Pierre Nadot - 31712 Blagnac Cedex - France - Phone +33 (0)5 62 21 62 21www.atraircraft.comPhoto credit: ATR - Pierre Barthe. Printed by: Imprimerie Pascal Communication

© ATR. All rights reserved. Confidential and proprietary document.

This document shall not be reproduced or disclosed to a third party without the written consent of ATR. This document and its content shall not be used for any purpose other than that for which it is supplied.ATR, its logo, the distinctive ATR aircraft profiles and patented information relating to the ATR aircraft are the exclusive property of ATR and are

subject to copyright. This document and all information contained herein are the sole property of ATR. No intellectual property right is granted through, or induced by, the delivery of this document or the disclosure of its content.The statements made herein do not constitute an offer or a representation. They are based on the mentioned assumptions and are expressed in good faith.

7.59

m

( 24

' 11"

)

22.67 m

( 74' 5")

8.78 m

( 28' 10")24.57 m

( 80' 7")

4.10 m

( 13' 5")

8.10 m

( 26' 7")

0.835 m

( 2' 8.9")

Ø 3.93 m

(12.9')

WING AREA : 54.5 m2

(586 sq.ft)

Airfield performAnce

Take-off disTance:

• Basic (MTOW - ISA - SL) 1,165 m - 3,822 ft

• At TOW for 300 Nm - Max pax - SL - ISA 1,025 m - 3,363 ft

• At TOW for 300 Nm - Max pax - 3,000 ft - ISA +10 1,215 m - 3,986 ft

Take-off speed (V2 min @ MTOW) 112 kcas

LANdINg fIeLd LeNgTh (JAR 25)

• Basic (MLW - SL) 964 m - 3,163 ft

• At LW (max pax + reserves) - SL 904 m - 2,967 ft

• Reference speed at landing 104 kias

en-route performAnce

Optimum climb speed 160 kcas

Rate of climb (ISA, SL, MTOW) 1,851 ft/min

Max Cruise speed

(95% MTOW - ISA - Optimum fL)300 kTas - 556 km/h

fuel flow at cruise speed 811 kg/h - 1,788 lb/h

Range with max pax 716 nm

200 Nm Block fuel 565 kg - 1,246 lb

CO2 emission 1,780 kg - 3,925 lb

300 Nm Block fuel 783 kg - 1,727 lb

CO2 emission 2,467 kg - 5,439 lb

engines

PRATT & WhITNey CANAdA PW127e/M

Take-off power 2,160 ShP

Take-off power - One engine 2,400 ShP

Max continuous 2,400 ShP

Max climb 2,160 ShP

Max cruise 2,132 ShP

propellers

hamilton Standard 568f

Blades: 6; diameter: 3.93 m - 12.9 ft

Weights

Max take-off weight (basic) 18,600 kg - 41,005 lb

Max landing weight (basic) 18,300 kg - 40,344 lb

Max zero fuel weight (basic)* 16,700 kg - 36,817 lb

Operational empty weight (Tech. Spec.) 11,250 kg - 24,802 lb

Operational empty weight (Typical in-service) 11,700 kg - 25,794 lb

Max payload (at typical in-service OeW) 5,300 kg - 11,684 lb

Max fuel load 4,500 kg - 9,921 lb

Attendant seat Galley Toilet Baggage Emergency exit

ATR 42-500THe RefeRenCe in ReGionAl AiR TRAnSPoRT

* Optional MZFW@17,000 Kg available on demand.

NB: En-route performance computed assuming Max Optional TOW, Typical in-service OEW, 48 PAX@95 Kg, JAR fuel reserves, taxi time allowance: 4 min.

2.26 m (89”)

0.440 m (17.3”)

0.457 m (18”)

2.57 m (101.2”)

ATR -500 SERIES

ATR72-500THe UlTRA -eff iC ienTS T A n D A R D

THe RefeRenCe in ReGionAl AiR TRAnSPoRT

The ATR 72 is recognized as the most cost-effective regional aircraft, positioning it as the industry reference to serve

both low-cost/low yields environment. A range of improvements in the field of noise and vibration reduction has

been implemented namely:

u An efficient and technologically advanced acoustic treatment of the structure with the installation of Dynamic

Vibration Absorbers and skin damping.

u Cabin interiors engineered for maximum noise attenuation and optimum comfort, through advanced

materials and absorbent panels and carpets, and additional overhead bins including handrail to

facilitate passengers and crew movement along the cabin.

Powered by PW 127 engines, the ATR 72-500 provides outstanding short field performance

for an aircraft of this size, even on difficult "hot and high" airfields.

68 seats at 31” pitch

STAnDARD ConfiGURATion

ATR DC/E Marketing September 2014 The information contained in this document is presented in good faith and does not in any way constitute an offer or a warranty. Avions de Transport Régional - 1, allée Pierre Nadot - 31712 Blagnac Cedex - France - Phone +33 (0)5 62 21 62 21www.atraircraft.comPhoto credit: ATR - Pierre Barthe. Printed by: Imprimerie Pascal Communication

© ATR. All rights reserved. Confidential and proprietary document.

This document shall not be reproduced or disclosed to a third party without the written consent of ATR. This document and its content shall not be used for any purpose other than that for which it is supplied.ATR, its logo, the distinctive ATR aircraft profiles and patented information relating to the ATR aircraft are the exclusive property of ATR and are

subject to copyright. This document and all information contained herein are the sole property of ATR. No intellectual property right is granted through, or induced by, the delivery of this document or the disclosure of its content.The statements made herein do not constitute an offer or a representation. They are based on the mentioned assumptions and are expressed in good faith.

Airfield performAnce

Take-off disTance:

• Basic (MTOW - ISA - SL) 1,224 m - 4,016 ft

• Option 1 (MTOW - ISA - SL) 1,289 m - 4,229 ft

• Option 2 (MTOW - ISA - SL) 1,333 m - 4,373 ft

• At TOW for 300 Nm - Max pax - SL - ISA 1,163 m - 3,815 ft

• At TOW for 300 Nm - Max pax - 3,000 ft - ISA +10 1,399 m - 4,590 ft

Take-off speed (V2 min @ MTOW) 115 kcas

LANdINg fIeLd LeNgTh (JAR)

• Basic MLW - SL 898 m - 2,946 ft

• Option (MLW - SL) 915 m - 3,002 ft

• At LW (max pax + reserves) - SL 862 m - 2,828 ft

• Reference speed at landing 113 kias

en-route performAnce

Optimum climb speed 170 kcas

Rate of climb (ISA, SL, MTOW) 1,374 ft/min

Max Cruise speed (95% MTOW - ISA - Optimum fL) 275 kTas - 510 km/h

fuel flow at cruise speed 762 kg/h - 1,680 lb/h

Range with max pax 785 nm

200 Nm Block fuel 617 kg - 1,360 lb

CO2 emission 1,944 kg - 4,285 lb

300 Nm Block fuel 858 kg - 1,892 lb

CO2 emission 2,703 kg - 5,958 lb

EnginEs

ProPEllErs

WEights

27. 166 m

( 89 ' 1. 5" )

7.65

m

( 25

' 1")

10. 77 m

( 35' 4" )

WING AREA : 61 m 2

(6 57 sq.ft)

27. 050 m

(8 8' 9" )

4. 10 m

(13' 5" )

8. 10 m

(26' 7" )

0. 8 35 m

(2 ' 8. 9" )

Ø 3. 93 m

(1 2'9)

Attendant seat Galley Toilet Baggage Emergency exit2.26 m (89”)

0.440 m (17.3”)

0.457 m (18”)

2.57 m (101.2”)

ATR 72-500THe RefeRenCe in ReGionAl AiR TRAnSPoRT

NB: en-route performance computed assuming Max Optional TOW, Typical in-service OEW, 68 PAX@95 Kg, JAR fuel reserves, taxi time allowance: 4 min.