Atr Family - AEROPOLIS Associazione Italiana Dell'aerospazio
atr familyATR 42-300ATR 42-400ATR 42-500ATR 42-600ATR 72-200ATR 72-210ATR 72-500ATR 72-600FREIGHTERCORPORATESURVEYOR
-600Freighter VersionATR CorporateATR Surveyorp. 4 - 5p. 6 - 7p. 8 - 9p. 10 - 11p. 12 - 13p. 14 - 15p. 16 - 17p. 18 - 19p. 20 - 21p. 22 - 23p. 24 - 25p. 26 - 27
IntroductionThe ATR family booklet provides the readerwith the main technical data for all ATRaircraft, including:general dimensionscross-sectionstandard cabin layoutpowerplant characteristicsoperating weightsbasic airfield and en-route performance.Furthermore, a short introduction is made ofderivative versions:FreighterCorporateSurveyor.Assumptions for en-route performance:u Max optional TOW & LWu Payload: max paxu OEW: typical in-serviceu Pax weight: 95 kg (including baggage)u Reserves: 5% trip fuel 30 min hold 100 Nm diversionu Taxi: 4 min
7.59 m( 24' 11")ATR 42-3008.78 m( 28' 10")22.67 m( 74' 5")8.10 m( 26' 7")Ø 3.96 m(13')2WING AREA : 54.5 m(586 sq.ft)0.82 m( 2' 7")4.10 m( 13' 5")24.57 m( 80' 7")0.440 m17.3"0.457 m18"1.91 m75.2"1.425 m56.1"0.635 m/25"1.92 m/76"3 m3106 cu.ft4.8 m3169.5 cu.ft2.263 m/89"2.570 m/101.2"3 m3106 cu.ft48 pax at 30” pitch1.8 m363.5 cu.ft4.8 m3169.5 cu.ft3 m3106 cu.ftAttendant seat1.8 m363.5 cu.ft4 ATR Family1.8 m363.5 cu.ftGalleyToiletBaggageEmergency exit4.8 m3169.5 cu.ft
ATR 42-300Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max take-off weight (option)Max landing weight (basic)Max zero fuel weight (basic)Max zero fuel weight (option)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distanceu Basic - MTOW - ISA - SLu Option - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 10Take-off speed (V2 min @ MTOW)Landing field length (FAR25)u Basic MLW - SLu LW (max pax reserves) - SLu Reference speed at landingEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Block Time300 Nm Block Fuel300 Nm Block Time48 seatsPW1201,800 SHP2,000 SHP1,700 SHP1,700 SHP1,619 SHP14 SF-54, 3.96 m - 13 ft16,700 kg - 36,817 lb16,900 kg - 37,257 lb16,400 kg - 36,155 lb15,200 kg - 33,510 lb15,540 kg - 34,259 lb10,285 kg - 22,674 lb10,900 kg - 24,030 lb4,640 kg - 10,229 lb4,500 kg - 9,921 lb1,090 m - 3,576 ft1,123 m - 3,684 ft1,073 m - 3,520 ft1,271 m - 4,170 ft108 KCAS1,033 m - 3,389 ft1,008 m - 3,307 ft103 KIAS160 KCAS1,320 ft/min15.1 min9,580 ft266 KTAS - 493 km/h568 kg/hr - 1,252 lb/h456 Nm500 kg - 1,102 lb55.9 min685 kg - 1,510 lb79.3 minATR Family 5
7.59 m( 24' 11")ATR 42-3208.78 m( 28' 10")22.67 m( 74' 5")8.10 m( 26' 7")Ø 3.96 m(13')2WING AREA : 54.5 m(586 sq.ft)0.82 m( 2' 7")4.10 m( 13' 5")24.57 m( 80' 7")0.440 m0.457 m17.3"18"1.91 m75.2"1.425 m56.1"0.635 m/25"3 m3106 cu.ft1.92 m/76"4.8 m3169.5 cu.ft2.263 m/89"3 m3106 cu.ft2.570 m/101.2"48 pax at 30” pitch1.8 m363.5 cu.ft4.8 m3169.5 cu.ft3 m3106 cu.ftAttendant seat1.8 m363.5 cu.ft6 ATR Family1.8 m363.5 cu.ftGalleyToiletBaggageEmergency exit4.8 m3169.5 cu.ft
ATR 42-320Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max take-off weight (option1)Max landing weight (basic)Max zero fuel weight (basic)Max zero fuel weight (option)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distanceu Basic - MTOW - ISA - SLu Option - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 10Take-off speed (V2 min @ MTOW)Landing field length (FAR25)u Basic MLW - SLu LW (max pax reserves) - SLu Reference speed at landingEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Block Time300 Nm Block Fuel300 Nm Block Time48 seatsPW1211,900 SHP2,100 SHP1,900 SHP1,700 SHP1,700 SHP14 SF-54, 3.96 m - 13 ft16,700 kg - 36,817 lb16,900 kg - 37,257 lb16,400 kg - 36,155 lb15,200 kg - 33,510 lb15,540 kg - 34,259 lb10,290 kg - 22,685 lb10,900 kg - 24,030 lb4,640 kg - 10,229 lb4,500 kg - 9,921 lb1,041 m - 3,415 ft1,068 m - 3,504 ft1,026 m - 3,366 ft1,222 m - 4,009 ft108 KCAS1,030 m - 3,379 ft1,008 m - 3,307 ft103 KIAS160 KCAS1,320 ft/min14.8 min10,940 ft270 KTAS - 500 km/h584 kg/hr - 1,287 lb/h459 Nm495 kg - 1,091 lb55.9 min676 kg - 1,490 lb79.3 minATR Family 7
7.59 m( 24' 11")ATR 42-4008.78 m( 28' 10")22.67 m( 74' 5")8.10 m( 26' 7")Ø 3.93 m(12.9')2WING AREA : 54.5 m(586 sq.ft)0.835 m( 2' 8.9")4.10 m( 13' 5")24.57 m( 80' 7")0.440 m0.457 m17.3"18"1.91 m75.2"1.425 m56.1"0.635 m/25"3 m3106 cu.ft1.92 m/76"4.8 m3169.5 cu.ft2.263 m/89"3 m3106 cu.ft2.570 m/101.2"48 pax at 30” pitch1.8 m363.5 cu.ft4.8 m3169.5 cu.ft3 m3106 cu.ftAttendant seat1.8 m363.5 cu.ft8 ATR Family1.8 m363.5 cu.ftGalleyToiletBaggageEmergency exit4.8 m3169.5 cu.ft
ATR 42-400Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max take-off weight (option1)Max landing weight (basic)Max landing weight (option)Max zero fuel weight (basic)Max zero fuel weight (option)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distanceu Basic - MTOW - ISA - SLu Option - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 10Take-off speed (V2 min @ MTOW)Landing field length (FAR25)u Basic MLW - SLu Option MLW - SLu LW (max pax reserves) - SLu Reference speed at landingEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Block Time300 Nm Block Fuel300 Nm Block Time48 seatsPW121A1,980 SHP2,200 SHP1,900 SHP1,700 SHP1,700 SHP568F6, 3.93 m - 12.9 ft17,900 kg - 39,462 lb18,200 kg - 40,123 lb17,600 kg - 38,801 lb17,900 kg - 39,462 lb16,300 kg - 35,935 lb16,600 kg - 36,596 lb11,050 kg - 24,361 lb11,400 kg - 25,132 lb5,200 kg - 11,464 lb4,500 kg - 9,921 lb1,205 m - 3,953 ft1,264 m - 4,147 ft1,071 m - 3,514 ft1,310 m - 4,298 ft111 KCAS1,120 m - 3,675 ft1,135 m - 3,724 ft1,063 m - 3,488 ft105 KIAS160 KCAS1,135 ft/min17.9 min7,705 ft261 KTAS - 484 km/h588 kg/hr - 1,296 lb/h794 Nm511 kg - 1,127 lb57.4 min706 kg - 1,556 lb81.5 minATR Family 9
7.59 m( 24' 11")ATR 42-5008.78 m( 28' 10")22.67 m( 74' 5")8.10 m( 26' 7")Ø 3.93 m(12.9')2WING AREA : 54.5 m(586 sq.ft)0.835 m( 2' 8.9")4.10 m( 13' 5")24.57 m( 80' 7")0.440 m(17.3”)3 m3106 cu.ft0.457 m(18”)4.8 m3169.5 cu.ft2.26 m (89”)2.57 m (101.2”)3 m3106 cu.ft48 pax at 30” pitch1.8 m363.5 cu.ft4.8 m3169.5 cu.ft3 m3106 cu.ftAttendant seat1.8 m363.5 cu.ft10 ATR Family1.8 m363.5 cu.ftGalleyToiletBaggageEmergency exit4.8 m3169.5 cu.ft
ATR 42-500Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max landing weight (basic)Max zero fuel weight (basic)Max zero fuel weight (Option)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distance Basic - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 1048 seatsPW127E/M2,160 SHP2,400 SHP2,400 SHP2,160 SHP2,132 SHP568F6, 3.93 m - 12.9 ft18,600 kg - 41,005 lb18,300 kg - 40,344 lb16,700 kg - 36,817 lb17,000 kg - 37,478 lb11,250 kg - 24,802 lb11,500 kg - 25,353 lb5,500 kg - 12,125 lb4,500 kg - 9,921 lb1,165 m - 3,822 ft1,000 m - 3,281 ft1,181 m - 3,875 ftTake-off speed (V2 min @ MTOW)Landing field length (FAR25)112 KCASu Basic MLW - SLu LW (max pax reserves) - SLu Reference speed at landing1,126 m - 3,694 ftEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Block Time300 Nm Block Fuel300 Nm Block Time1,045 m - 3,428 ft104 KIAS160 KCAS1,851 ft/min12.7 min13,010 ft300 KTAS - 556 km/h811 kg/hr - 1,788 lb/h801 Nm602 kg - 1,327 lb52.0 min835 kg - 1,841 lb72.9 minATR Family 11
ATR 42-6007.59 m0042-600( 24' 11")ATRATR8.78 m( 28' 10")22.67 m( 74' 5")8.10 m( 26' 7")Ø 3.93 m(12.9')2WING AREA : 54.5 m(586 sq.ft)0.82 m( 2' 7")4.10 m( 13' 5")24.57 m( 80' 7")482 mm(19’’)1.91 m(75.2’’)468 mm(18.4’’)3 m3106 cu.ft4.8 m3169.5 cu.ft2.26 m (89’’)2.57 m (101.2’’)3 m3106 cu.ft48 pax at 30” pitch1.8 m363.5 cu.ft4.8 m3169.5 cu.ft3 m3106 cu.ftAttendant seat1.8 m363.5 cu.ft12 ATR Family1.8 m363.5 cu.ftGalleyToiletBaggageEmergency exit4.8 m3169.5 cu.ft
ATR 42-600Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max landing weight (basic)Max zero fuel weight (basic)Max zero fuel weight (Option)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distanceu Basic - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 1048 seatsPW127M2,160 SHP2,400 SHP2,400 SHP2,160 SHP2,132 SHP568F6, 3.93 m - 12.9 ft18,600 kg - 41,005 lb18,300 kg - 40,344 lb16,700 kg - 36,817 lb17,000 kg - 37,478 lb11,300 kg - 24,912 lb11,500 kg - 25,353 lb5,500 kg - 12,125 lb4,500 kg - 9,921 lb1,165 m - 3,822 ft1,000 m - 3,281 ft1,181 m - 3,875 ftTake-off speed (V2 min @ MTOW)Landing field length (FAR25)112 KCASu Basic MLW - SLu LW (max pax reserves) - SLu Reference speed at landing1,126 m - 3,694 ftEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Blo ck Time300 Nm Block Fuel300 Nm Block Time1,045 m - 3,428 ft104 KIAS160 KCAS1,851 ft/min12.7 min13,010 ft300 KTAS - 556 km/h811 kg/hr - 1,788 lb/h801 Nm602 kg - 1,327 lb52.0 min835 kg - 1,841 lb72.9 minATR Family 13
7. 65 m( 25 ' 1" )ATR 72-20010. 77 m( 35' 4" )27. 166 m( 89 ' 1. 5" )8. 10 m(26' 7" )Ø 3. 96 m(1 3')WING AREA : 61 m 2(6 57 sq.ft)0.82m(2.7’)4. 10 m27. 050 m(13' 5" )(8 8' 9" )0.440 m17.3"0.457 m18"1.91 m75.2"1.425 m56.1"0.635 m/25"1.92 m/76"2.263 m/89"2.570 m/101.2"66 pax at 31” pitchAttendant seat14 ATR FamilyGalleyToiletBaggageEmergency exit
ATR 72-200Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max take-off weight (option)Max landing weight (basic)Max zero fuel weight (basic)Max zero fuel weight (option)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distanceu Basic - MTOW - ISA - SLu Option - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 10Take-off speed (V2 min @ MTOW)Landing field length (FAR25)u Basic MLW - SLu LW (max pax reserves) - SLu Reference speed at landingEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Block Time300 Nm Block Fuel300 Nm Block Time66 seatsPW124B2,160 SHP2,400 SHP2,400 SHP2,088 SHP2,088 SHP14 SF-114, 3.96 m - 13 ft21,500 kg - 47,399 lb22,000 kg - 48,501 lb21,350 kg - 47,068 lb19,700 kg - 43,430 lb20,000 kg - 44,092 lb12,400 kg - 27,337 lb13,000 kg - 28,660 lb7,000 kg - 15,432 lb5,000 kg - 11,023 lb1,409 m - 4,623 ft1,506 m - 4,941 ft1,251 m - 4,104 ft1,522 m - 4,993 ft115 KCAS1,207 m - 3,960 ft1,145 m - 3,757 ft114 KIAS170 KCAS1,390 ft/min16.7 min8,505 ft278 KTAS - 515 km/h720 kg/hr - 1,587 lb/h872 Nm570 kg - 1,257 lb55.5 min793 kg - 1,748 lb77.8 minATR Family 15
7. 65 m( 25 ' 1" )ATR 72-21010. 77 m( 35' 4" )27. 166 m( 89 ' 1. 5" )8. 10 m(26' 7" )Ø 3. 96 m(1 3')WING AREA : 61 m 2(6 57 sq.ft)0.82m(2.7’)4. 10 m27. 050 m(13' 5" )(8 8' 9" )0.440 m17.3"0.457 m18"1.91 m75.2"1.425 m56.1"0.635 m/25"1.92 m/76"2.263 m/89"2.570 m/101.2"66 pax at 31” pitchAttendant seat16 ATR FamilyGalleyToiletBaggageEmergency exit
ATR 72-210Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max take-off weight (option)Max landing weight (basic)Max zero fuel weight (basic)Max zero fuel weight (option)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distanceu Basic - MTOW - ISA - SLu Option - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 10Take-off speed (V2 min @ MTOW)Landing field length (FAR25)u Basic MLW - SLu LW (max pax reserves) - SLu Reference speed at landingEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Block Time300 Nm Block Fuel300 Nm Block Time66 seatsPW1272,475 SHP2,750 SHP2,500 SHP2,192 SHP2,132 SHP247F-14, 3.96 m - 13 ft21,500 kg - 47,399 lb22,000 kg - 48,501 lb21,350 kg - 47,068 lb19,700 kg - 43,430 lb20,000 kg - 44,092 lb12,450 kg - 27,447 lb13,000 kg - 28,660 lb7,000 kg - 15,432 lb5,000 kg - 11,023 lb1,211 m - 3,973 ft1,291 m - 4,236 ft1,106 m - 3,629 ft1,333 m - 4,373 ft113 KCAS1,052 m - 3,451 ft997 m - 3,271 ft109 KIAS170 KCAS1,462 ft/min16.6 min10,000 ft279 KTAS - 517 km/h760 kg/hr - 1,675 lb/h805 Nm598 kg - 1,318 lb55.4 min837 kg - 1,845 lb77.5 minATR Family 17
7. 65 m( 25 ' 1" )ATR 72-50010. 77 m( 35' 4" )27. 166 m( 89 ' 1. 5" )8. 10 m(26' 7" )Ø 3. 93 m(1 2'9)0. 8 35 m(2 ' 8. 9" )2WING AREA : 61 m(6 57 sq.ft)4. 10 m27. 050 m(13' 5" )(8 8' 9" )0.440 m(17.3”)0.457 m(18”)2.26 m (89”)2.57 m (101.2”)68 pax at 31” pitch3 m3106 cu.ft34.8 m169.5 cu.ft2.8 m399 cu.ftAttendant seat18 ATR FamilyGalleyToiletBaggageEmergency exit
ATR 72-500Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max take-off weight (option 1)Max take-off weight (option 2)Max landing weight (basic)Max landing weight (option)Max zero fuel weight (basic)Max zero fuel weight (option 1)Max zero fuel weight (option 2)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distanceu Basic - MTOW - ISA - SLu Option 1 - MTOW - ISA - SLu Option 2 - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 10Take-off speed (V2 min @ MTOW)Landing field length (FAR25)u Basic MLW - SLu Option MLW - SLu LW (max pax reserves) - SLu Reference speed at landingEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Block Time300 Nm Block Fuel300 Nm Block Time68 seatsPW127F/M2,475 SHP2,750 SHP2,500 SHP2,192 SHP2,132 SHP568F6, 3.93 m - 12.9 ft22,000 kg - 48,501 lb22,500 kg - 49,603 lb22,800 kg - 50,265 lb21,850 kg - 48,170 lb22,350 kg - 49,272 lb20,000 kg - 45,194 lb20,300 kg - 44,753 lb20,500 kg - 45,194 lb12,950 kg - 28,549 lb13,500 kg - 29,762 lb7,000 kg - 15,432 lb5,000 kg - 11,023 lb1,224 m - 4,016 ft1,289 m - 4,229 ft1,333 m - 4,373 ft1,150 m - 3,773 ft1,384 m - 4,541 ft115 KCAS1,048 m - 3,438 ft1,067 m - 3,501 ft1,000 m - 3,281 ft113 KIAS170 KCAS1,374 ft/min17.2 min10,000 ft275 KTAS - 510 km/h762 kg/hr - 1,680 lb/h824 Nm610 kg - 1,345 lb55.6 min852 kg - 1,878 lb78.0 minATR Family 19
ATR7.65 m00ATR72-600( 25' 1")ATR 72-60010.77 m( 35' 4")27.166 m( 89' 1.5")8.10 m(26' 7")Ø 3.93 m(12'11" )0.835 m2(2' 8.9")WING AREA : 61 m(657 sq.ft)4.10 m27.050 m(13' 5")(88' 9")482 mm(19’’)1.91 m(75.2’’)468 mm(18.4’’)2.26 m (89’’)2.57 m (101.2’’)68 pax at 31” pitch3 m3106 cu.ft34.8 m169.5 cu.ft2.8 m399 cu.ftAttendant seat20 ATR FamilyGalleyToiletBaggageEmergency exit
ATR 72-600Standard configurationEngines Pratt & Whitney CanadaTake-off powerTake-off power - One engineMax continuousMax climbMax cruisePropellers Hamilton StandardBlades, diameterWeightsMax take-off weight (basic)Max take-off weight (option)Max landing weight (basic)Max zero fuel weight (basic)Max zero fuel weight (option 1)Operational empty weight (Tech. Spec.)Operational empty weight (Typical in-service)Max payload (at typical in-service OEW)Max fuel loadAirfield performanceTake-off distanceu Basic - MTOW - ISA - SLu Option 1 - MTOW - ISA - SLu TOW for 300 Nm - Max pax - SL - ISAu TOW for 300 Nm - Max pax - 3,000 ft - ISA 10Take-off speed (V2 min @ MTOW)Landing field length (FAR25)u Basic MLW - SLu LW (max pax reserves) - SLu Reference speed at landingEn-route performanceOptimum climb speedRate of climb (ISA, SL, MTOW)Time to climb to FLI170One engine net ceiling (95% MTOW, ISA 10)Max Cruise speed (95% MTOW - ISA - Optimum FL)Fuel flow at cruise speedRange with max pax200 Nm Block Fuel200 Nm Block Time300 Nm Block Fuel300 Nm Block Time68 seatsPW127M2,475 SHP2,750 SHP2,500 SHP2,192 SHP2,132 SHP568F6, 3.93 m - 12.9 ft22,800 kg - 50,265 lb23,000 kg - 50,705 lb22,350 kg - 49,272 lb20,800 kg - 45,855 lb21,000 kg - 46,296 lb13,010 kg - 28,682 lb13,500 kg - 29,762 lb7,500 kg - 16,534 lb5,000 kg - 11,023 lb1,333 m - 4,373 ft1,367 m - 4,485 ft1,150 m - 3,773 ft1,384 m - 4,541 ft116 KCAS1,067 m - 3,501 ft1,000 m - 3,281 ft113 KIAS170 KCAS1,355 ft/min17.5 min10,000 ft275 KTAS - 510 km/h762 kg/hr - 1,680 lb/h899 Nm610 kg - 1,345 lb55.6 min852 kg - 1,878 lb78.0 minATR Family 21
FreighterversionLARGE CARGO DOOR CONVERSIONWeights and values - Large Cargo DoorMTOWMLWMZFWOEW (typical, 9g stop net)Provision for CLS**Max gross payloadNb of LD3Nb of 88" x 108"Nb of 88" x 62"Max linear load (st)Max linear load (opt.)ATR 42-300/-32016,900 kg - 37,257 lb16,400 kg - 36,155 lb15,540 kg - 34,259 lb10,029 kg - 22,110 lb211 kg - 465 lb5,300 kg - 11,684 lb536510 kg/m - 28 lb/inch610 kg/m - 34 lb/inchATR 72-200*22,000 kg - 48,501 lb21,350 kg - 47,068 lb20,000 kg - 44,092 lb11,638 kg - 25,657 lb269 kg - 593 lb8,093 kg - 17,842 lb759510 kg/m - 28 lb/inch610 kg/m - 34 lb/inch* Optional weights ** CLS weight for 88" x 108" palletsQuiet overnight operationsICAO - Annex 16 - Chapter III (EPNdB)Ch III limitsFlyover89Sideline94Approach
atr 42-300 atr 42-400 atr 42-500 atr 42-600 atr 72-200 atr 72-210 atr 72-500 atr 72-600
COMITATO INTERSOCIETARIO DI COORDINAMENTO DELLE ASSOCIAZIONI ODONTOSTOMATOLOGICHE ITALIANE 2003 LINEE GUIDA IN ODONTOIATRIA A.I.C Accademia Italiana di Conservativa A.I.E. Accademia Italiana Endodonzia A.I.G. Associazione Italiana di Gnatologia A.I.O.P. Accademia Italiana di Odontoiatria Protesica A.N.D.I. Associazione Nazionale Dentisti Italiani
Tech Sheet: Aerospatiale ATR-42/72 (aerospatiale-ATR.pdf) ATR-42 Cockpit Cover ATR-42 Cockpit Cover Section 1: Canopy/Cockpit/Fuselage Covers Engine Inlet Plugs are custom fit for your Aerospatiale ATR-42/72
The most fuel efficient regional aircraft ATR 72-600 A shorter runway to wider horizons ATR 42-600S Born to be a freighter ATR 72-600F Versatile and growing family of aircraft ATR Overview 7 8. . savings compared to fossil fuel 116 L fuel saving (-11%) compared to flight in regular conditions-47% emissions compared to flight in regular .
he ATR 72-500 is the latest de-velop ment of the ATR 72. It benefits from the in-service experience of about 700 ATR aircraft flying world-wide, with a proven aver-age dispatch reliability of more than 99%. The ATR 72-500 incorporates: Totally renewed cabin interior design Technol
ATR-42 Main Goodrich 3-1518-2 10-1607 229024 ATR-42 Main ABSC 5006856 209808 ATR-42 Nose ABSC 5006858 209809 ATR-72 Main Dunlop PNAHA1752; PNAHA1890 209688 ATR-72 Nose Dunlop 20
CODICE ETICO dell’associazione AGESCI – Associazione Guide e Scout Cattolici Italiani indice pagina 1. PRINCIPI GENERALI 3 1.1 Ruolo e attività di Agesci 3 1.2 Presupposti e finalità del Codice Etico 3 1.3 Impegni di Agesci 4 1.4 Impegni dei fornitori e dei consulenti 5 1.5 Impegni dei dipendenti 5 1.6 Impegni dei componenti degli Organi 5
Associazione Istituto Psicosociale 1 ASSOCIAZIONE ISTITUTO PSICOSOCIALE Roma – Napoli – Palermo istitutops@gmail.com Silvia Mendico 347.2657350 – Mariapaola Ramaglia 338.1587085 L’Istituto Psicosociale è un’Associazione di promozione sociale, che organizza e gestisce attività di formazi
ACCOUNTING 0452/21 Paper 2 May/June 2018 1 hour 45 minutes Candidates answer on the Question Paper. No Additional Materials are required. READ THESE INSTRUCTIONS FIRST Write your Centre number, candidate number and name on all the work you hand in. Write in dark blue or black pen. You may use an HB pencil for any diagrams or graphs. Do not use staples, paper clips, glue or correction fluid. DO .