常见航空器规格和性能参数:修订间差异
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Kejia Deng(讨论 | 贡献) 无编辑摘要 |
Kejia Deng(讨论 | 贡献) 无编辑摘要 |
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{| class="wikitable" style="text-align: center | {| class="wikitable" style="text-align: center" | ||
|+Boeing 747 Characteristics | |+Boeing 747 Characteristics | ||
|- | |- | ||
第338行: | 第338行: | ||
|} | |} | ||
{| class="wikitable" style="text-align:center | {| class="wikitable" style="text-align: center" | ||
|+Boeing 757 Characteristics | |+Boeing 757 Characteristics | ||
|- | |- | ||
第556行: | 第556行: | ||
|} | |} | ||
{| class="wikitable" style="text-align:center | {| class="wikitable" style="text-align: center" | ||
|+ Boeing 777 specifications | |+ Boeing 777 specifications | ||
|- | |- | ||
第722行: | 第722行: | ||
|} | |} | ||
{| class="wikitable" style="text-align:center | {| class="wikitable" style="text-align: center" | ||
|+Boeing 787 Dreamliner characteristics | |+Boeing 787 Dreamliner characteristics | ||
!Variant | !Variant | ||
第819行: | 第819行: | ||
|B789 | |B789 | ||
|B78X | |B78X | ||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|- | |||
! colspan=2 |Subtype | |||
! A318<ref name="A318 specifications">{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/a318/specifications/ |title= A318 Dimensions & key data |publisher= Airbus}}</ref> | |||
! A319<ref name="A319 specifications">{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/a319/specifications/ |title= A319 Dimensions & key data |publisher= Airbus}}</ref> | |||
! A320<ref name="A320 specifications">{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/a320/specifications/ |title= A320 Dimensions & key data |publisher= Airbus}}</ref> | |||
! A321<ref name="A321 specifications">{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/a321/specifications/ |title= A321 Dimensions & key data |publisher= Airbus}}</ref> | |||
|- | |||
! colspan=2 |Cockpit crew | |||
| colspan="4" style="text-align:center;" |2 | |||
|- | |||
! colspan=2 |Exit limit [[EASA]]<ref name=cert>{{cite web |url= https://www.easa.europa.eu/system/files/dfu/TCDS_EASA%20A%20064_%20Airbus_%20A318_A319_A320_A321_Iss_22.pdf |title= Type Certificate Data Sheet |publisher= EASA |date= 28 June 2016 |deadurl= yes |archiveurl= https://web.archive.org/web/20160915235037/https://www.easa.europa.eu/system/files/dfu/TCDS_EASA%20A%20064_%20Airbus_%20A318_A319_A320_A321_Iss_22.pdf |archivedate= 15 September 2016 |df= dmy-all }}</ref>/[[FAA]]<ref name="FAA-Data">{{cite web |url= http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/57529f07d8f6e3b58625800d0057c1d4/$FILE/A28NM_Rev24.pdf |title= Type Certificate Data Sheet |date= August 12, 2016 |publisher= FAA}}</ref> | |||
|136 | |||
|160 | |||
|195/190 | |||
|230 | |||
|- | |||
! colspan=2 |1-class max. seating<ref name=AllAbout/> | |||
|132 at {{convert|29|-|30|in|cm|abbr=on}} pitch | |||
|156 at {{convert|28|-|30|in|cm|abbr=on}} pitch | |||
|186 at {{convert|29|in|cm|abbr=on}} pitch<ref>{{cite news |url= https://www.runwaygirlnetwork.com/2016/03/01/high-density-a320s-for-easyjet-will-retain-seat-pitch-assures-airline/ |title= High-density A320s for easyJet will retain seat pitch, assures airline |work= Runway Girl Network |date= 1 March 2016}}</ref> | |||
|236 at {{convert|28|in|cm|abbr=on}} pitch<ref>{{cite news |url= http://aviationweek.com/commercial-aviation/airbus-studies-236-seat-a321 |title= Airbus Studies 236-Seat A321 |date= December 10, 2012 |work= Aviation Week}}</ref> | |||
|- | |||
! colspan=2 |1-class, typical<ref name=AllAbout>{{cite web |url= https://fr.scribd.com/doc/30183955/All-About-Airbus-A-320-Family |title= All About the Airbus A320 Family |date= 2009 |publisher= Airbus}}</ref> | |||
|117 at {{convert|32|in|cm|abbr=on}} pitch | |||
|134 at {{convert|32|in|cm|abbr=on}} pitch | |||
|164 at {{convert|32|in|cm|abbr=on}} pitch | |||
|199 at {{convert|32|in|cm|abbr=on}} pitch | |||
|- | |||
! colspan=2 |2-class, typical<ref name=AllAbout/> | |||
|107 (8F @ 38 in, 99Y @ 32 in) | |||
|124 (8F @ 38 in, 116Y @ 32 in) | |||
|150 (12F @ 36 in, 138Y @ 32 in) | |||
|185 (16F @ 36 in, 169Y @ 32 in) | |||
|- | |||
! colspan=2 |Cargo volume | |||
|{{convert|21.20|m3|cuft|abbr=on}} | |||
|{{convert|27.70|m3|cuft|abbr=on}} | |||
|{{convert|37.40|m3|cuft|abbr=on}} | |||
|{{convert|51.70|m3|cuft|abbr=on}} | |||
|- | |||
! colspan=2 |[[Unit load device]]s | |||
| | |||
|4× LD3-45 | |||
|7× LD3-45 | |||
|10× LD3-45 | |||
|- | |||
! colspan=2 |Length | |||
|{{convert|31.44|m|ftin|abbr=on}} | |||
|{{convert|33.84|m|ftin|abbr=on}} | |||
|{{convert|37.57|m|ftin|abbr=on}} | |||
|{{convert|44.51|m|ftin|abbr=on}} | |||
|- | |||
! colspan=2 |[[Wheelbase]] | |||
|{{convert|10.25|m|ftin|abbr=on}} | |||
|{{convert|11.04|m|ftin|abbr=on}} | |||
|{{convert|12.64|m|ftin|abbr=on}} | |||
|{{convert|16.91|m|ftin|abbr=on}} | |||
|- | |||
! colspan=2 |Track | |||
|colspan="4" |{{convert|7.59|m|ftin|abbr=on}} | |||
|- | |||
! colspan=2 |Wingspan | |||
|{{convert|34.10|m|ftin|abbr=on}} | |||
|colspan="3" |{{convert|35.8|m|ftin|abbr=on}} {{efn|name=sharklets|with [[Sharklet (wingtip device)|sharklets]]}} | |||
|- | |||
! colspan=2 |Wing area<ref name="A321 described"/> | |||
| ||colspan=2 |{{cvt|124|m2|sqft}}, {{#expr:35.8/(124/35.8)round1}} aspect ratio | |||
|{{cvt|128|m2|sqft}}, {{#expr:35.8/(128/35.8)round1}} {{abbr|AR|aspect ratio}} | |||
|- | |||
! colspan=2 |Wing sweepback | |||
|colspan="4" |25 degrees<ref name=elsevier>{{cite web |url= http://booksite.elsevier.com/9780340741528/appendices/data-a/table-1/table.htm |title= Airbus Aircraft Data File |publisher= Elsevier |work= Civil Jet Aircraft Design |date= July 1999}}</ref> | |||
|- | |||
! colspan=2 |Tail height | |||
|{{convert|12.56|m|ftin|abbr=on}} | |||
|colspan=3 |{{convert|11.76|m|ftin|abbr=on}} | |||
|- | |||
! colspan=2 |Fuselage | |||
|colspan="4" |{{cvt|4.14|m|ftin}} height, {{cvt|3.95|m|ftin}} width, {{cvt|3.70|m|ftin}} cabin width | |||
|- | |||
! colspan=2 |[[Maximum takeoff weight|MTOW]] | |||
|{{convert|68|t|lb|abbr=on}} | |||
|{{convert|75.5|t|lb|abbr=on}} | |||
|{{convert|78|t|lb|abbr=on}} | |||
|{{convert|93.5|t|lb|abbr=on}} | |||
|- | |||
! colspan=2 |Max. [[payload]] <!--MZFW-OEW--> | |||
|{{convert|{{#expr:54.5-39.5}}|t|lb|abbr=on}} | |||
|{{convert|{{#expr:58.5-40.8}}|t|lb|abbr=on}} | |||
|{{convert|{{#expr:62.5-42.6}}|t|lb|abbr=on}} | |||
|{{convert|{{#expr:73.8-48.5}}|t|lb|abbr=on}} | |||
|- | |||
! colspan=2 |[[jet fuel|Fuel]] capacity | |||
|{{convert|24210|L|USgal|abbr=on|disp=br}} | |||
|{{convert|24210|-|30190|L|USgal|abbr=on|disp=br}} | |||
|{{convert|24210|-|27200|L|USgal|abbr=on|disp=br}} | |||
|{{convert|24050|-|30030|L|USgal|abbr=on|disp=br}} | |||
|- | |||
! colspan=2 |[[Operating empty weight|OEW]]<ref name=AllAbout/> | |||
|{{convert|39.5|t|lb|abbr=on|sigfig=3}} | |||
|{{convert|40.8|t|lb|abbr=on|sigfig=3}} | |||
|{{convert|42.6|t|lb|abbr=on|sigfig=3}} | |||
|{{convert|48.5|t|lb|abbr=on|sigfig=3}} | |||
|- | |||
! colspan=2 |Speed | |||
| colspan="4" |Cruise: {{cvt|0.78|Mach|39000|knots km/h|0}},<ref name="A320 Family Technology">{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/technology-and-innovation/ |title= A320 Family Technology |publisher= Airbus}}</ref> {{abbr|MMO|Maximum Operation Mach Number}}: {{cvt|0.82|Mach|39000|knots km/h|0}}<ref name="A320 Family Technology"/> | |||
|- | |||
! colspan=2 |Range, typical payload{{efn|Passengers and bags}} | |||
|3,100 nmi, 5,750 km | |||
|3,750 nmi, 6,950 km{{efn|name=sharklets}} | |||
|3,300 nmi, 6,100 km{{efn|name=sharklets}} | |||
|3,200 nmi, 5,950 km{{efn|name=sharklets}} | |||
|- | |||
! colspan=2 |[[Airbus Corporate Jets|ACJ]] range | |||
|4,200 nmi, 7,800 km<ref name=ACJ318>{{cite web |url= http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj318/ |title= ACJ318 |publisher= Airbus |deadurl= yes |archiveurl= https://web.archive.org/web/20180123000000/http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj318/ |archivedate= 23 January 2018 |df= dmy-all }}</ref> | |||
|6,000 nmi, 11,100 km<ref name=ACJ319>{{cite web |url= http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj319/ |title= ACJ319 |publisher= Airbus |deadurl= yes |archiveurl= https://web.archive.org/web/20130105054833/http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj319/ |archivedate= 5 January 2013 |df= dmy-all }}</ref> | |||
|4,300 nmi, 7,800 km<ref name=ACJ320>{{cite web |url= http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj320/ |title= ACJ320 |publisher= Airbus |deadurl= yes |archiveurl= https://web.archive.org/web/20180123000000/http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj320/ |archivedate= 23 January 2018 |df= dmy-all }}</ref> | |||
| | |||
|- | |||
! colspan=2 |Takeoff run (MTOW, SL, [[International standard atmosphere|ISA]]) | |||
|{{convert|1780|m|ft|abbr=on}}<ref name=ACJ318/> | |||
|{{convert|1850|m|ft|abbr=on}}<ref name=ACJ319/> | |||
|{{convert|2100|m|ft|abbr=on}}<ref name=ACJ320/> | |||
| | |||
|- | |||
! colspan=2 |Landing (MLW, SL, [[International standard atmosphere|ISA]]) | |||
|{{convert|1230|m|ft|abbr=on}}<ref name=ACJ318/> | |||
|{{convert|1360|m|ft|abbr=on}}<ref name=ACJ319/> | |||
|{{convert|1500|m|ft|abbr=on}}<ref name=ACJ320/> | |||
| | |||
|- | |||
! colspan=2 |Service ceiling | |||
|colspan="4" |{{convert|39,100|-|41,000|ft|m|abbr=on}}<ref name=cert/> | |||
|- | |||
! colspan=2 rowspan=2 |Engines (×2) | |||
| colspan="4" |[[CFM International CFM56]]-5B, {{convert|68.3|in|m|abbr=on}} fan | |||
|- | |||
|[[Pratt & Whitney PW6000|PW6000A]], {{convert|56.5|in|m|abbr=on}} fan | |||
|colspan="3" |[[IAE V2500]]A5, {{convert|63.5|in|m|abbr=on}} fan | |||
|- | |||
! colspan=2 |Thrust (×2) | |||
|{{convert|96|-|106|kN|abbr=on}} | |||
|colspan=2 |{{convert|98|-|120|kN|abbr=on}} | |||
|{{convert|133|-|147|kN|abbr=on}} | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+ Airbus family figures<ref name="Airbus Family figures">{{cite web |url= http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/Airbus-Family-Figures-booklet.pdf |publisher= Airbus |date= July 2017 |title= Airbus Family figures }}</ref> | |||
|- | |||
!Variant | |||
!A319neo | |||
!A320neo | |||
!A321neo | |||
|- | |||
! Cockpit crew | |||
| colspan="3" | Two | |||
|- | |||
! 2-class [[Seating capacity|seats]] | |||
| 140 | |||
| 165 | |||
| 206: 16{{abbr|J|business}} @36{{nbsp}}in + 190{{abbr|Y|economy}} @30{{nbsp}}in<ref name=a321LR >{{cite web |url= http://aviationweek.com/commercial-aviation/airbus-launches-long-range-a321neo-version |title= Airbus Launches Long-Range A321neo Version |publisher= [[Aviation Week]] |date= Jan 13, 2015}}</ref> | |||
|- | |||
! 1-class maximum | |||
| 160 | |||
| 195<ref name=typecert/> @ 27{{nbsp}}in<ref>{{cite news |url= http://leehamnews.com/2015/04/06/pontifications-meet-the-a320neo-max-195/ |title= Meet the "A320neo MAX 195 |publisher= Leeham News |date= April 6, 2015}}</ref> | |||
| 240 @ 28{{nbsp}}in<ref name=AusBT13jun2014>{{cite web |url= http://www.ausbt.com.au/airbus-reveals-new-a320neo-layout |title= Airbus reveals new A321neo layout: New 'Cabin-Flex' and larger doors |publisher= Australian business traveller |date= 13 June 2014}}</ref> | |||
|- | |||
! [[Seat pitch#Seat width|Seat width]] | |||
| colspan="3" | [[Economy class|Economy]] at [[Narrow-body aircraft#Six-abreast cabin|6 abreast]]: {{convert|18|in|cm|abbr=on}},<ref name=AusBT13jun2014/> 3.7{{nbsp}}m (12{{nbsp}}ft{{nbsp}}1{{nbsp}}in) cabin width | |||
|- | |||
! Cargo capacity | |||
| 27{{nbsp}}m³ (976 ft³) | |||
| 37{{nbsp}}m³ (1,322 ft³) | |||
| 51{{nbsp}}m³ (1,828 ft³){{efn|no Additional Centre Tank}} | |||
|- | |||
! Length | |||
| 33.84{{nbsp}}m (111{{nbsp}}ft) | |||
| 37.57{{nbsp}}m (123{{nbsp}}ft{{nbsp}}3{{nbsp}}in) | |||
| 44.51{{nbsp}}m (146{{nbsp}}ft) | |||
|- | |||
! Wingspan | |||
| colspan="3" | 35.80{{nbsp}}m (117{{nbsp}}ft{{nbsp}}5{{nbsp}}in) | |||
|- | |||
! Height | |||
| colspan="3" | 11.76{{nbsp}}m (38{{nbsp}}ft{{nbsp}}7{{nbsp}}in) | |||
|- | |||
! [[Maximum takeoff weight|Max. takeoff weight]] | |||
| 75.5{{nbsp}}t (166,400 lb) | |||
| 79{{nbsp}}t (174,200 lb) | |||
| 97{{nbsp}}t (213,800 lb) | |||
|- | |||
! Max. [[payload]] | |||
| {{cvt|17.7|t|lb|-2}}<ref>{{cite web |url= http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/techdata/aircraft_characteristics/Airbus-Commercial-Aircraft-AC-A319-Feb18.pdf |title= A319 aircraft characteristics: Airport and maintenance planning |publisher= Airbus |date= Feb 2018}}</ref>{{rp|3-2-1}} | |||
| {{cvt|20|t|lb|-2}}<ref>{{cite web |url= http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/techdata/aircraft_characteristics/Airbus-Commercial-Aircraft-AC-A320-Feb18.pdf |title= A320 aircraft characteristics: Airport and maintenance planning |publisher= Airbus |date= Feb 2018}}</ref>{{rp|3-2-1}} | |||
| {{cvt|25.5|t|lb|-2}}<ref>{{cite web |url= http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/techdata/aircraft_characteristics/Airbus-Commercial-Aircraft-AC-A321-Feb18.pdf |title= A321 aircraft characteristics: Airport and maintenance planning |publisher= Airbus |date= Feb 2018}}</ref>{{rp|3-2-1}} | |||
|- | |||
! Operating empty <!-- MZFW - max payload--> | |||
| {{cvt|{{#expr:60.3-17.7}}|t|lb|-2}} | |||
| {{cvt|{{#expr:64.3-20}}|t|lb|-2}} | |||
| {{cvt|{{#expr:75.6-25.5}}|t|lb|-2}} | |||
|- | |||
! [[jet fuel|Fuel]] capacity | |||
| colspan="2" | 26,730 l (7,060 USg) | |||
| 32,940 l (8,700 USg){{efn|A321LR with 3 Additional Centre Tank, no ACT: 23,700 l (6,261 Us gal)<ref>{{cite web |url= http://www.airbus.com/fileadmin/media_gallery/files/tech_data/AC/Airbus_AC_A321_Jun16.pdf |title= A321 aircraft characteristics - airport and maintenance planning |publisher= Airbus |date= May 2016 |deadurl= yes |archiveurl= https://web.archive.org/web/20161018231941/http://www.airbus.com/fileadmin/media_gallery/files/tech_data/AC/Airbus_AC_A321_Jun16.pdf |archivedate= 18 October 2016 |df= dmy-all }}</ref>}} | |||
|- | |||
! Engines (×2) | |||
| colspan="3" | [[CFM International LEAP]]-1A or [[Pratt & Whitney PW1000G|Pratt & Whitney PW1100G]]<ref name="Airbus A320neo Technology"/> | |||
|- | |||
! Fan diameter | |||
| colspan="3" |PW1100G: {{convert|81|in|cm|0|abbr=on}},<ref>{{cite web |url= https://www.pw.utc.com/Content/PurePowerPW1000G_Engine/pdf/B-1-1_PurePowerEngineFamily_SpecsChart.pdf |publisher= [[Pratt & Whitney]] |title= PurePower Engine Family Specs Chart}}</ref> LEAP-1A: {{convert|78|in|cm|0|abbr=on}}<ref>{{cite web|url=http://www.cfmaeroengines.com/files/brochures/LEAP-Brochure-2013.pdf |title=CFM LEAP Engine Brochure |publisher=[[CFM International]] |date=2013 |deadurl=yes |archiveurl=https://web.archive.org/web/20150923202053/http://www.cfmaeroengines.com/files/brochures/LEAP-Brochure-2013.pdf |archivedate=23 September 2015 }}</ref> | |||
|- | |||
! Max. [[Thrust]]<ref name=typecert/> | |||
| {{cvt|24,100|lbf|kN|order=flip}}<ref>{{cite web |title=Type Certificate data sheet for PW1100G-JM Series Engines |url= https://www.easa.europa.eu/system/files/dfu/EASA%20TCDS%20IM.E.093_issue2_20152311_1.0.pdf |publisher= [[EASA]] |date= 23 November 2015}}</ref><ref>{{cite web |title= Type Certificate data sheet for LEAP-1A & LEAP-1C Series Engines |url= https://www.easa.europa.eu/system/files/dfu/EASA%20E110%20TCDS%20Issue%204%20LEAP%201A_1C.pdf |publisher= [[EASA]] |date= 21 Dec 2016 |deadurl= yes |archiveurl= https://web.archive.org/web/20161223131701/https://www.easa.europa.eu/system/files/dfu/EASA%20E110%20TCDS%20Issue%204%20LEAP%201A_1C.pdf |archivedate= 23 December 2016 |df= dmy-all }}</ref> | |||
| {{cvt|27120|lbf|kN|order=flip}} | |||
| {{cvt|33110|lbf|kN|order=flip}} | |||
|- | |||
! Speed | |||
| colspan="3" | Cruise: {{cvt|0.78|Mach|35,000|knots km/h|0}},<ref name="Airbus A320neo Technology">{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/technology-and-innovation/ |title= Airbus A320neo Technology |publisher= [[Airbus]] }}</ref> Max.: {{cvt|0.82|Mach|35,000|knots km/h|0}}<ref name=Flight26May2017/> | |||
|- | |||
! Ceiling | |||
| colspan=3 | {{cvt|39100|-|39800|ft}}<ref name=typecert/> | |||
|- | |||
! Typical range | |||
| 6,950 km / 3,750 nmi{{efn|with 140 passengers, with 124 : 7,750km / 4,200nmi<ref>{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/a319neo/ |title= A319NEO Key figures |publisher= Airbus |deadurl= yes |archiveurl= https://web.archive.org/web/20170204002758/http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/a319neo/ |archivedate= 4 February 2017 |df= dmy-all }}</ref>}} | |||
| 6,500 km / 3,500 nmi{{efn|with 165 passengers, with 150 : 6,850km / 3,700nmi<ref>{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/a320neo/ |title= A320NEO Key figures |publisher= Airbus |deadurl= yes |archiveurl= https://web.archive.org/web/20170203003859/http://www.airbus.com/aircraftfamilies/passengeraircraft/a320family/a320neo/ |archivedate= 3 February 2017 |df= dmy-all }}</ref>}} | |||
|7,400 km / 4,000 nmi {{efn|with 206 passengers}} | |||
|- | |||
! Takeoff | |||
| | |||
| | |||
| {{cvt|1988|m}}<ref name=Flight26May2017>{{cite news |url= https://www.flightglobal.com/news/articles/flight-test-a321neo-stretches-its-legs-437215/ |title= Flight test: A321neo stretches its legs |date= 26 May 2017 |author= Mike Gerzanics |work= Flight Global}}</ref> | |||
|- | |||
! ICAO Type<ref>{{cite web |title= DOC 8643 – Aircraft Type Designators |url= http://www.icao.int/publications/DOC8643/Pages/default.aspx |publisher= ICAO}}</ref> | |||
|A19N | |||
|A20N | |||
|A21N | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+ Airbus A330 specifications<ref>{{cite web |url= http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/techdata/aircraft_characteristics/Airbus-Commercial-Aircraft-AC-A330-Jan-2017.pdf |title= A330 Airplane Characteristics - Airport and Maintenance Planning |publisher= Airbus |date= January 2017 }}</ref> unless noted | |||
! | |||
! A330-200 | |||
! A330-200F | |||
! A330-300 | |||
|- | |||
! Cockpit crew | |||
| colspan=3 | Two | |||
|- | |||
! Capacity | |||
| 246 (36J @ 60 in + 210Y @ 32 in) | |||
| 70,000 kg (154,324 lb) | |||
| 300 (36J @ 60 in + 264Y @ 32 in) | |||
|- | |||
! Max seating<ref name=Backgrounder>{{cite web |url= http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/Backgrounder-Airbus-Commercial-Aircraft-A330-Family-Facts-and-Figures-E.pdf |title= A330 Family facts & figures |publisher= Airbus |date= September 2017 |deadurl= yes |archiveurl= https://web.archive.org/web/20170916225408/http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/Backgrounder-Airbus-Commercial-Aircraft-A330-Family-Facts-and-Figures-E.pdf |archivedate= 16 September 2017 |df= dmy-all }}</ref> | |||
| 406 || | |||
| 440 | |||
|- | |||
! Length | |||
| colspan="2" | 58.82 m (192.98 ft) | |||
| 63.67 m (208.89 ft) | |||
|- | |||
! Span | |||
| colspan="3" | Wing: 60.3 m (197.83 ft), Main gear: 12.61 m (41.37 ft) | |||
|- | |||
! Wing | |||
| colspan="3" | 361.6 m² (3,892 ft²), 25% chord wingsweep : 30°,<ref name=A332prestige>{{cite web |url= http://www.airbus.com/fileadmin/media_gallery/files/tech_data/jetFamily/media_object_file_A330_200_specifications.pdf |title= A330-200 Prestige specifications |publisher= Airbus |deadurl= yes |archiveurl= https://web.archive.org/web/20121003003510/http://www.airbus.com/fileadmin/media_gallery/files/tech_data/jetFamily/media_object_file_A330_200_specifications.pdf |archivedate= 3 October 2012 |df= dmy-all }}</ref> {{#expr:60.3/(361.6/60.3)round2}} Aspect ratio | |||
|- | |||
! Tail height<ref name=Backgrounder/> | |||
| 17.39m / 57’ | |||
| 16.90m / 55’5’’ | |||
| 16.79m / 55’ | |||
|- | |||
! Fuselage | |||
| colspan="3" | 5.64 m (222 in) diameter, 5.18 m (204 in) cabin width | |||
|- | |||
! Seat width | |||
| colspan="3" | 0.46 m (18 in) in 8 abreast economy, 0.53 m (21 in) in 6 abreast business | |||
|- | |||
! Cargo volume | |||
| {{#expr:60.7+52+19.7}} m³ ({{#expr:2142+1836+695}} ft³) | |||
| {{#expr:336.8+60.7+52+19.7}} m³ ({{#expr:11894+2142+1836+695}} ft³) | |||
| {{#expr:78+60.7+19.7}} m³ ({{#expr:2754+2142+695}} ft³) | |||
|- | |||
! [[Maximum takeoff weight]] | |||
| 242,000 kg (533,519 lb) | |||
| 233,000 kg (513,677 lb) | |||
| 242,000 kg (533,519 lb) | |||
|- | |||
! [[Maximum landing weight]] | |||
| 182,000 kg (401,241 lb) | |||
| colspan=2 | 187,000 kg (412,264 lb) | |||
|- | |||
! Max zero fuel weight | |||
| 170,000 kg (374,786 lb) | |||
| 178,000 kg (392,423 lb) | |||
| 175,000 kg (385,809 lb) | |||
|- | |||
! Max Payload<!--from payload-range charts, ACAP section 3-2-1--> | |||
| {{cvt|49,400|kg|lb}} | |||
| {{cvt|68,600|kg|lb}} | |||
| {{cvt|45,600|kg|lb}} | |||
|- | |||
! Fuel capacity | |||
| colspan=3 | 139,090 l (36,744 US gal) - 109,185 kg (240,711 lb) | |||
|- | |||
! [[Operating empty weight]]<!-- OEW = MZFW - max PL --> | |||
| {{cvt|{{#expr:170000-49400}}|kg|lb}} | |||
| {{cvt|{{#expr:178000-68600}}|kg|lb}} | |||
| {{cvt|{{#expr:175000-45600}}|kg|lb}} | |||
|- | |||
! Cruise | |||
| colspan="3" | {{cvt|0.82|Mach|41100|knots km/h|0}} ({{cvt|0.86|Mach|41100|knots km/h|0}} M<sub>MO</sub>), {{cvt|41,100|ft|m|order=flip}} [[Service ceiling]]<ref name=Emirates>{{cite web |url= http://www.emirates.com/english/flying/our_fleet/airbus_a330_200.aspx |title= Airbus A330-200 |publisher= Emirates}}</ref> | |||
|- | |||
! Final approach speed (MLW) | |||
| {{Convert|136|knots|km/h|abbr=on|0}} | |||
| {{Convert|139|knots|km/h|abbr=on|0}} | |||
| {{Convert|137|knots|km/h|abbr=on|0}} | |||
|- | |||
! Range<ref name=Backgrounder/> | |||
| 13,450 km / 7,250 nm (247 pax) | |||
| 7,400 km / 4,000 nm | |||
| 11,750 km / 6,350 nm (277 pax) | |||
|- | |||
! Runway (SL, ISA, MTOW/MLW) | |||
| colspan="3" | Takeoff: 2,770 m (9,110 ft), Landing: 1,730 m (5,680 ft)<ref name=ACJ330>{{cite web |url= http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj330/ |publisher= Airbus Corporate Jets |title= ACJ330}}</ref> | |||
|- | |||
! Engines (×2)<ref name=EASA-TCDS/> | |||
| colspan=3 |{{convert|64,530|-|68,530|lbf|kN|abbr=on|0}} [[General Electric CF6]]-80E1 (except -200F)<br />{{convert|64,500|-|70,000|lbf|kN|abbr=on|0}} [[Pratt & Whitney PW4000]] PW4164/PW4168/PW4170<br />{{convert|67,500|-|71,100|lbf|kN|abbr=on|0}} [[Rolls-Royce Trent 700]] 768/772 | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|- | |||
! Variant | |||
! A340-200<ref name=200300ACAP>{{cite web |url= http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/techdata/aircraft_characteristics/Airbus-Commercial-Aircraft-AC-A340-200-300-Jan-2017.pdf |title= Aircraft Characteristics Airport Planning - A340-200/300 |publisher= Airbus |date= January 2017}}</ref> | |||
! A340-300<ref name=200300ACAP/> | |||
! A340-500<ref name=500600ACAP>{{cite web |url=http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/techdata/aircraft_characteristics/Airbus-Commercial-Aircraft-AC-A340-500_600-Jan-2017.pdf |title= Aircraft Characteristics Airport Planning - A340-500/600 |publisher= Airbus |date= January 2017}}</ref> | |||
! A340-600<ref name=500600ACAP/> | |||
|- | |||
! Cockpit crew | |||
| colspan="4"| Two | |||
|- | |||
! Seating | |||
| 261 (3-class) <ref>https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-200.html</ref> or 303 (30F + 273Y) | |||
| 277 (3-class) <ref>https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-300.html</ref> or 335 (30F + 305Y) | |||
| 293 <ref>https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-500.html</ref> or 313 (12F + 36J + 265Y) | |||
| 326 <ref>https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-600.html</ref> or 380 (12F + 54J + 314Y) | |||
|- | |||
! Exit limit<ref name="tcds"/> | |||
| 420{{efn|name=4tAdoors|4 Type A doors}}/375 | |||
| 375/440{{efn|name=4tAdoors}}/375 | |||
| 375 | |||
| 440 | |||
|- | |||
! Length | |||
| 59.39 m / 194.85 ft | |||
| 63.69 m / 208.96 ft | |||
| 67.93 m / 222.87 ft | |||
| 75.36 m / 247.24 ft | |||
|- | |||
! Wingspan | |||
| colspan="2"| 60.3 m / 197.83 ft | |||
| colspan="2"| 63.45 m / 208.17 ft | |||
|- | |||
! Wing<ref name=elsevier>{{cite web |url= http://booksite.elsevier.com/9780340741528/appendices/data-a/table-1/table.htm |title= Airbus Aircraft Data File |publisher= Elsevier |work= Civil Jet Aircraft Design |date= July 1999}}</ref> | |||
| colspan="2"| {{cvt|363.1|m2}}, 29.7° sweep, {{#expr:60.3/(363.1/60.3)round1}} [[Wing aspect ratio|AR]] | |||
| colspan="2"| {{cvt|437.3|m2}}, 31.1° sweep, {{#expr:63.45/(437.3/63.45)round1}} [[Wing aspect ratio|AR]] | |||
|- | |||
! Height | |||
| 17.03 m / 55.86 ft | |||
| 16.99 m / 55.72 ft | |||
| 17.53 m / 57.51 ft | |||
| 17.93 m / 58.84 ft | |||
|- | |||
! Fuselage | |||
| colspan="4"| 5.287 m / 208.15 in cabin width, 5.64 m / 18.5 ft outside width | |||
|- | |||
! Cargo volume | |||
| {{cvt|{{#expr:78+60.7+19.7}}|m3}} | |||
| {{cvt|{{#expr:60.7+52+19.7}}|m3}} | |||
| {{cvt|{{#expr:78+52+19.7}}|m3}} | |||
| {{cvt|{{#expr:104+78+19.7}}|m3}} | |||
|- | |||
! [[Maximum takeoff weight|MTOW]] | |||
| {{cvt|275|t|lb}} | |||
| {{cvt|276.5|t|lb}} | |||
| colspan=2 | {{cvt|380|t|lb}} | |||
|- | |||
! Max. [[Payload|PL]] | |||
| {{cvt|51|t|lb}} | |||
| {{cvt|52|t|lb}} | |||
| {{cvt|54|t|lb}} | |||
| {{cvt|66|t|lb}}< | |||
|- | |||
! [[Operating empty weight|OEW]] | |||
| {{cvt|{{#expr:169-51}}|t|lb}}<!--MZFW-maxPL--> | |||
| {{cvt|{{#expr:183-52}}|t|lb}}<!--MZFW-maxPL--> | |||
| {{cvt|168|t|lb}} | |||
| {{cvt|174|t|lb}} | |||
|- | |||
! Max. Fuel | |||
| colspan=2 | 110.4 t / 243,395 lb | |||
| 175.2 t / 386,292 lb | |||
| 155.5 t / 342,905 lb {{efn|no aux. tank, 164 t / 361 595 lb with 1 aux. tank}} | |||
|- | |||
! Engines (×4) | |||
| colspan=2| [[CFM International CFM56]]-5C | |||
| [[Rolls-Royce Trent 500|Trent 553]] || [[Rolls-Royce Trent 500|Trent 556]] | |||
|- | |||
! Thrust (×4)<ref name="tcds" /> | |||
| colspan=2| {{cvt|138.78|-|151.24|kN}} | |||
| colspan=2| {{cvt|55,780|-|61902|lbf|kN|order=flip}} | |||
|- | |||
! Speed | |||
| colspan="4"| {{cvt|0.86|Mach|39000|knots km/h|0}} max,<ref>{{Cite web |url= http://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-300.html |title= Previous-Generation Aircraft > A340-300 |publisher= Airbus}}</ref> {{cvt|0.82|Mach|39000|knots km/h|0}} cruise | |||
|- | |||
! Range, max pax | |||
| {{cvt|7600|nmi|km}} | |||
| {{cvt|7150|nmi|km}} | |||
| {{cvt|9000|nmi|km}} | |||
| {{cvt|7550|nmi|km}} | |||
|- | |||
! Take off{{efn|MTOW, SL, [[International standard atmosphere|ISA]]}} | |||
| {{cvt|9500|ft|m|abbr=on|order=flip}} | |||
| {{cvt|10000|ft|m|abbr=on|order=flip}} | |||
| {{cvt|3350|m}} | |||
| {{cvt|3400|m}} | |||
|- | |||
! Ceiling | |||
| colspan="2"| 12,500 m (41,000 ft)<ref>{{cite web |url= http://www.lufthansa.com/mediapool/pdf/75/media_998975.pdf |title= Airbus A340-300 |publisher= Lufthansa |date= August 2010}}</ref> | |||
| colspan="2"| 12,527 m (41,100 ft)<ref>{{cite web |url= http://www.lufthansa.com/mediapool/pdf/14/media_892514.pdf |title= Airbus A340-600 |publisher= Lufthansa |date= August 2010}}</ref> | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+ A350 aircraft characteristics<ref name=ACAP>{{cite web |url= http://www.airbus.com/content/dam/corporate-topics/publications/backgrounders/techdata/aircraft_characteristics/Airbus-Commercial-Aircraft-AC-A350-900-1000.pdf |title= A350 aircraft characteristics |date= 1 June 2018 |publisher= [[Airbus]]}}</ref> | |||
!Model | |||
!A350-900 | |||
!A350-1000 | |||
|- | |||
|Cockpit crew | |||
|colspan="2" |Two | |||
|- | |||
|Seating | |||
|325/315 (48B+267Y)<br/>ULR: 173=80J+93Y | |||
|366/369 (54B+315Y)<br/>387 (2-class)<ref>{{cite web |url= http://bloga350.blogspot.fr/2015/02/airbus-announces-18-additional-seats.html |title= Airbus announces 18 additional seats for A350-1000 |publisher= A350 XWB News |date= 3 February 2015}}</ref> <br/> | |||
|- | |||
|Exit limit | |||
|colspan=2 |440<ref name=TCDS/> | |||
|- | |||
|Overall length | |||
|66.8 m / 219.5 ft | |||
|73.78 m / 242.7 ft | |||
|- | |||
|Wing | |||
|colspan="2" |64.75 m / 212.43 ft span, 31.9° [[Swept wing|sweep]]<ref name=AvWeekPilotReport/> | |||
|- | |||
|Aspect ratio | |||
|{{#expr:64.75/(442/64.75)round2}} | |||
|{{#expr:64.75/((442+22.3)/64.75)round2}} | |||
|- | |||
|Wing area | |||
|{{cvt|442|m2|sqft}}<ref name=tech>{{cite web |url= http://www.airbus.com/aircraftfamilies/passengeraircraft/a350xwbfamily/technology-and-innovation/ |title= A350 XWB / Technology |publisher= [[Airbus]] |deadurl= yes |archiveurl= https://web.archive.org/web/20131129074833/http://www.airbus.com/aircraftfamilies/passengeraircraft/a350xwbfamily/technology-and-innovation/ |archivedate= 29 November 2013 |df= dmy-all }}</ref> | |||
|{{cvt|{{#expr:442+22.3}}|m2|sqft}}<ref name=Flight6jul2018>{{cite news |url= https://www.flightglobal.com/news/articles/flight-test-airbus-a350-1000-takes-growth-in-its-st-449603/ |title= Flight Test: Airbus A350-1000 takes growth in its stride |date= 6 July 2018 |author= Mike Gerzanics}}</ref> | |||
|- | |||
|Overall height | |||
|17.05 m / 55 ft 11 in<ref name="A350-900_specs">{{cite web |url= http://www.airbus.com/aircraft/passenger-aircraft/a350xwb-family/a350-900.html#details |title= A350-900 specs |publisher= [[Airbus]]}}</ref> | |||
|17.08 m / 56 ft 0 in<ref name="A350-1000_specs">{{cite web |url= http://www.airbus.com/aircraft/passenger-aircraft/a350xwb-family/a350-1000.html#details |title= A350-1000 specs |publisher= [[Airbus]] }}</ref> | |||
|- | |||
|Fuselage | |||
|colspan="2" |5.96 m / 19.7 ft width, 6.09 m / 19.98 ft height | |||
|- | |||
|Cabin width | |||
|colspan="2" |5.61 m / 18 ft 5 in,<ref name="A350-900_specs"/><ref name="A350-1000_specs"/> 9-abreast Seat : 18 in / 46 cm{{efn|10-abreast: {{cvt|16.8|in|cm}}<ref>{{cite web |url= http://www.runwaygirlnetwork.com/2015/06/19/airbus-works-to-make-10-abreast-a350-a-slice-more-comfortable/ |title= Airbus works to make 10-abreast A350 a smidge more comfortable |date= 2015-06-19 |publisher= Runway Girl Network }}</ref>}} | |||
|- | |||
|[[Maximum takeoff weight|MTOW]] | |||
|280 t / 617,295 lb | |||
|316 t / 696,661 lb | |||
|- | |||
| Max. [[payload]] | |||
| {{cvt|53.3|t|lb}} | |||
| {{cvt|64.2|t|lb}} | |||
|- | |||
|Fuel capacity<ref name=TCDS/> | |||
|{{cvt|140,795|L|USgal}}<br/>{{cvt|110,523|kg}}{{efn|name=ER}} | |||
|{{cvt|158,791|L|USgal}}<br/>{{cvt|124,651|kg}} | |||
|- | |||
| [[Operating empty weight|OEW]]<!--MZFW-max payload--> | |||
| {{cvt|{{#expr:195.7-53.3}}|t|lb}} typical<br/>{{cvt|297,000|-|320,000|lb|t|order=flip|1}}<ref name=AvWeekPilotReport/> | |||
| {{cvt|{{#expr:223-64.2}}|t|lb}}<br>{{cvt|155|t|lb}} dry<ref>{{cite news |url= http://aviationweek.com/aviation-week-space-technology/aviation-week-flies-airbus-biggest-twin-engine-a350-1000 |title= Aviation Week Flies Airbus’ Biggest Twin-Engine—A350-1000 |date= Jul 6, 2018 |author= Tim Wuerfel |work= Aviation Week & Space Technology}}</ref> | |||
|- | |||
|[[Manufacturer's empty weight|MEW]] | |||
|{{cvt|115.7|t|lb|0}}<ref name=ser1>{{cite news|last=Kingsley-Jones |first=Max |url=http://www.flightglobal.com/articles/2008/06/10/224578/a350-weight-growth-will-result-in-1-fuel-penalty-airbus.html |title=A350 weight growth will result in 1% fuel penalty: Airbus |work=Flight International |date=10 June 2008 |accessdate=24 May 2011 |deadurl=yes |archiveurl=https://web.archive.org/web/20090131185615/http://www.flightglobal.com/articles/2008/06/10/224578/a350-weight-growth-will-result-in-1-fuel-penalty-airbus.html |archivedate=31 January 2009 |df=dmy}}</ref> | |||
|129 t (284,000 lb)<ref name=AvWeek5feb2018>{{cite news |url= http://aviationweek.com/singapore-airshow-2018/airbus-debuts-a350-1000-singapore-airshow |title= Airbus Debuts A350-1000 at Singapore Airshow |date=5 February 2018 |author= Guy Norris |work= Aviation Week Network}}</ref> | |||
|- | |||
|Cargo capacity | |||
|36 [[Unit Load Device|LD3]] or 11 pallets | |||
|44 LD3 or 14 pallets | |||
|- | |||
|cruise | |||
|colspan="2" |{{cvt|0.85|Mach|43000|knots km/h|0}} Typical, {{cvt|0.89|Mach|34000|knots km/h|0}} Maximum<ref name=AvWeekPilotReport/> | |||
|- | |||
|Range | |||
|15,000 km / 8,100 nmi{{efn|325 passengers}}<ref name="A350-900_specs"/>{{efn|name=ER|-900ULR fuel capacity: {{cvt|165|m3|USgal|-2}},<ref name=ulr>{{cite press release |url= http://www.airbus.com/presscentre/pressreleases/press-release-detail/detail/airbus-launches-new-ultra-long-range-version-of-the-a350-900/ |title= Airbus launches new Ultra-Long Range version of the A350-900 |publisher= [[Airbus]] |date= 13 October 2015}}</ref>{{cvt|9700|nmi|km|order=flip|-2}} range,<ref name=FG170510>{{cite news |url= https://www.flightglobal.com/news/articles/a350-900ulr-range-figure-not-a-revision-airbus-437060/ |title= A350-900ULR range figure not a revision: Airbus |date= 10 May 2017 |author= David Kaminski-Morrow |work= Flight Global}}</ref> ACJ350 range: {{cvt|20000|km|nmi|-2}}<ref name=ACJ350>{{cite web |url= http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj350/ |title= ACJ350 Technical data |publisher= [[Airbus]] |deadurl= yes |archiveurl= https://web.archive.org/web/20180228000000/http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj350/ |archivedate= 28 February 2018 |df= dmy-all }}</ref>}} | |||
|{{cvt|8,400|nmi|km|order=flip}}{{efn|366 passengers, 316 t MTOW}}<ref name=AvWeek14jun2018/> | |||
|- | |||
|Takeoff (MTOW, SL, ISA) | |||
|{{cvt|2600|m|ft}} | |||
| | |||
|- | |||
|Landing (MLW, SL, ISA) | |||
|{{cvt|2000|m|ft}} | |||
| | |||
|- | |||
|Service ceiling<ref name=TCDS/> | |||
|{{cvt|43,100|ft}} | |||
|{{cvt|41,450|ft}} | |||
|- | |||
|Engines (2×) | |||
|colspan="2" |[[Rolls-Royce Trent XWB]] | |||
|- | |||
|Maximum thrust<ref name=TCDS/> | |||
|374.5 kN / 84,200 lbf | |||
|431.5 kN / 97,000 lbf | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|- | |||
! Variant | |||
! A380-800<ref name="a380_specs"/> | |||
|- | |||
| Cockpit crew | |||
| Two | |||
|- | |||
| Typical seating | |||
| 544 (4-class) | |||
|- | |||
| Exit limit | |||
| 868<ref name=TCDS/>{{efn|538 main deck, 330 upper deck}} | |||
|- | |||
| [[Length overall]] | |||
| {{convert|72.72|m|ftin|abbr=on}} | |||
|- | |||
| Wingspan | |||
| {{convert|79.75|m|ftin|abbr=on}} | |||
|- | |||
| Height | |||
| {{convert|24.09|m|ftin|abbr=on}} | |||
|- | |||
| [[Wheelbase]] | |||
| {{convert|31.88|m|ftin|abbr=on}} | |||
|- | |||
| Wheel track | |||
| {{convert|12.46|m|ftin|abbr=on}}, {{convert|14.34|m|ftin|abbr=on}} total width<ref name="ACAP">{{cite web |url= http://www.airbus.com/fileadmin/media_gallery/files/tech_data/AC/Airbus-AC-A380-Jan16.pdf |title= A380 Aircraft Characteristics – Airport and Maintenance Planning |publisher= Airbus |date= 1 December 2015 |deadurl= yes |archiveurl= https://web.archive.org/web/20161123045502/http://www.airbus.com/fileadmin/media_gallery/files/tech_data/AC/Airbus-AC-A380-Jan16.pdf |archivedate= 23 November 2016 |df= dmy-all }}</ref> | |||
|- | |||
| Outside fuselage<br />dimensions | |||
| Width: {{convert|7.14|m|ftin|abbr=on}}<br />Height: {{convert|8.41|m|ftin|abbr=on}} | |||
|- | |||
| Maximum <br />cabin width | |||
| {{convert|6.50|m|ftin|abbr=on}} main deck<br />{{convert|5.80|m|ftin|abbr=on}} upper deck | |||
|- | |||
| Cabin length | |||
| {{convert|49.9|m|ftin|abbr=on}} main deck<br />{{convert|44.93|m|ftin|abbr=on}} upper deck{{vn|date=October 2016}} | |||
|- | |||
| Wing area | |||
| {{convert|845|m2|sqft|abbr=on}}<ref name=prestigeSpecs>{{cite web |url= http://www.airbus.com/fileadmin/media_gallery/files/tech_data/jetFamily/media_object_file_A380_specifications.pdf |title= A380 Prestige Specifications |publisher= Airbus |deadurl= yes |archiveurl= https://web.archive.org/web/20161012152549/http://www.airbus.com/fileadmin/media_gallery/files/tech_data/jetFamily/media_object_file_A380_specifications.pdf |archivedate= 12 October 2016 |df= dmy-all }}</ref> | |||
|- | |||
| [[Aspect ratio (wing)|Aspect ratio]] | |||
| {{#expr:79.75/(845/79.75)round2}} | |||
|- | |||
| [[Swept wing|Wing sweep]] | |||
| 33.5°<ref name=prestigeSpecs/> | |||
|- | |||
| Maximum ramp weight | |||
| {{convert|577|t|lb|abbr=on}} | |||
|- | |||
| [[Maximum take-off weight]] | |||
| {{convert|575|t|lb|abbr=on}} | |||
|- | |||
| Max. landing weight | |||
| {{convert|394|t|lb|abbr=on}} | |||
|- | |||
| Max. zero fuel weight | |||
| {{convert|369|t|lb|abbr=on}} | |||
|- | |||
| Operating empty weight | |||
| {{convert|276.8|t|lb|abbr=on}}<ref>{{cite web |url= https://www.flightglobal.com/news/articles/everything-about-the-airbus-a380-205274/ |title= Airbus A380 Aircraft Profile |date= 27 February 2007 |publisher= Flightglobal }}</ref> | |||
|- | |||
| Max. structural payload | |||
| {{convert|84|t|lb|abbr=on}}<ref name=ACAP/> | |||
|- | |||
| Maximum cargo volume | |||
| {{convert|184|m3|cuft|abbr=on}} | |||
|- | |||
| Maximum operating speed | |||
| {{convert|0.89|Mach|43,000|km/h kn|sigfig=3}} | |||
|- | |||
| Maximum design speed | |||
| {{convert|0.96|Mach|39000|km/h kn|sigfig=3}}{{efn|in dive at cruise altitude}}<ref>{{cite web |url= https://www.flightglobal.com/news/articles/a380-powers-on-through-flight-test-203708/ |title= A380 powers on through flight-test |work=Flight International |date= 20 December 2005}}</ref> | |||
|- | |||
| Cruise speed | |||
| {{convert|0.85|Mach|43,000|km/h kn|sigfig=3}}<ref name=HuberStop/> | |||
|- | |||
| Take off ([[Maximum Takeoff Weight|MTOW]], SL, ISA) | |||
| {{convert|3000|m|ft|abbr=on}}<ref name="ACAP"/> | |||
|- | |||
| Landing speed | |||
| {{convert|130|kn|km/h|abbr=on|sigfig=2}}<ref name=HuberStop>{{cite news|author=Mark Huber |url=http://www.airspacemag.com/flight-today/how-things-work-stopping-the-a380-27549065/?no-ist |title=How Things Work: Stopping the A380 |work=Air & Space magazine |publisher=Smithsonian |date=August 2011 |deadurl=yes |archiveurl=https://web.archive.org/web/20140621141726/http://www.airspacemag.com/flight-today/how-things-work-stopping-the-a380-27549065/?no-ist |archivedate=21 June 2014 |df= }}</ref> | |||
|- | |||
| Range | |||
| 15,200 km / 8,200 nmi | |||
|- | |||
| [[Service ceiling]] | |||
| {{convert|43000|ft|m|abbr=on|sigfig=3|order=flip}}<ref>{{cite web |url= http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/083db0ec0506b38c86257ce500633f91/$FILE/A58NM_Rev_6.pdf |title= Airbus A380 Type Certificate Data Sheet |publisher=[[Federal Aviation Authority]] |date= 27 May 2014 }}</ref> | |||
|- | |||
| Max. fuel capacity | |||
| 323,545 L / 85,471 USgal<ref>{{cite web |url= http://www.aircraft.airbus.com/fileadmin/media_gallery/files/tech_data/AC/AC_A380_20161201.pdf |title= A380 Aircraft Characteristics – Airport and Maintenance Planning |publisher= Airbus |date= 1 December 2015 |deadurl= yes |archiveurl= https://web.archive.org/web/20171009042006/http://www.aircraft.airbus.com/fileadmin/media_gallery/files/tech_data/AC/AC_A380_20161201.pdf |archivedate= 9 October 2017 |df= dmy-all }}</ref> | |||
|- | |||
| Engines (4 ×) | |||
| [[Engine Alliance GP7200]] / [[Rolls-Royce Trent 900]] | |||
|- | |||
| Thrust (4 ×) | |||
| {{convert|311|kN|lbf|abbr=on}} | |||
|} | |} |
2018年7月7日 (六) 15:59的版本
Variant | 737-600 | 737-700 | 737-800 | 737-900ER |
---|---|---|---|---|
Cockpit crew | Two | |||
2-class | 108 (8F@36" 100Y@32") | 128 (8F@36" 120Y@32") | 160 (12F@36" 148Y@32") | 177 (12F@36" 165Y@32") |
1-class | 123 @32" - 130 @ 30" | 140 @32" - 148 @ 30" | 175 @32" - 184 @ 30" | 177 @32" - 215 @ 28" |
Exit Limit | 149 | 189 | 220 | |
Seat width | First : 22in / 56 cm; Economy : 17in / 43 cm | |||
Length | 102 ft 6 in / 31.24 m | 110 ft 4 in / 33.63 m | 129 ft 6 in / 39.47 m | 138 ft 2 in / 42.11 m |
Height | 41 ft 3 in / 12.57 m | 41 ft 2 in (12.55 m) | ||
Wing | Span: 112 ft 7 in / 34.32 m, with winglets: 117 ft 5in / 35.79m; Area: 124.60 m2 (1,341.2 sq ft); Sweepback: 25°; AR: 9.44 | |||
Fuselage | Width: 12 ft 4 in (3.76 m); Cabin width: 11 ft 7 in (3.54 m); Cabin height: 86.6 in (2.20 m) | |||
Operating empty weight | 80,200 lb / 36,378 kg | 83,000 lb / 37,648 kg | 91,300 lb / 41,413 kg | 98,495 lb / 44,677 kg |
Maximum landing weight | 121,500 lb / 55,111 kg | 129,200 lb / 58,604 kg | 146,300 lb / 66,361 kg | 157,300 lb / 71,350 kg |
Maximum takeoff weight | 144,500 lb / 65,544 kg | 154,500 lb / 70,080 kg | 174,200 lb / 79,016 kg | 187,700 lb / 85,139 kg |
Fuel capacity | 6,875 US gal / 26,022 L | 7,837 US gal / 29,666 L | ||
Lower deck cargo | 720 ft³ / 20.4 m³ | 966 ft³ / 27.4 m³ | 1,555 ft³ / 44.1 m³ | 1,826 ft³ / 51.7 m³ |
Takeoff run | 6,161 ft (1,878 m) | 6,699 ft (2,042 m) | 7,598 ft (2,316 m) | 9,800 ft (3,000 m) |
Flight envelope | 41,000 feet (12,497 m) Ceiling, Mach 0.82 (470 kn; 871 km/h) MMo | |||
Cruise | Mach 0.785 (453 kn; 838 km/h) | Mach 0.781 (450 kn; 834 km/h) | Mach 0.789 (455 kn; 842 km/h) | Mach 0.79 (455 kn; 844 km/h) |
Range | 3,235 nmi (5,991 km) | 3,010 nmi (5,570 km) | 2,935 nmi (5,436 km) | 2,950 nmi (5,460 km) |
Engines (× 2) | CFM56-7B18/20/22 | CFM56-7B20/22/24/26/27 | CFM56-7B24/26/27 | |
Thrust (× 2) | 20,000–22,000 lbf
89–98 kN |
20,000–26,000 lbf
89–116 kN |
24,000–27,000 lbf
110–120 kN |
24,000–27,000 lbf
110–120 kN |
Cruise max. thrust | 5,960 lbf (26.5 kN) (climb) | |||
Engine dimensions | Fan tip diameter: 61 in (155 cm), length: 103.50 in (263 cm) | |||
Engine ground clearance | 18 in / 46 cm | 19 in / 48 cm | ||
ICAO Type | B736 | B737 | B738 | B739 |
Variant | 737 MAX 7 | 737 MAX 8 / MAX 200 | 737 MAX 9 | 737 MAX 10 |
---|---|---|---|---|
Cockpit crew | Two | |||
Seating | 138 (8J + 130Y) to 172 max | 162 (12J + 150Y) to 210 max | 178 (16J + 162Y) to 220 max | 188 to 230 max |
Seat pitch | 28–29 in (71–74 cm) in high density, 31–32 in (79–81 cm) in economy, 36 in (91 cm) in business | |||
Cargo capacity | 1,146 cu.ft / 32.45 m³ | 1,543 cu.ft / 43.69 m³ | 1,814 cu.ft / 51.37 m³ | |
Length | 116 ft 8 in / 35.56 m | 129 ft 8 in / 39.52 m | 138 ft 4 in / 42.16 m | 143 ft 8 in / 43.8 m |
Wingspan | 117 ft 10 in / 35.92 m | |||
Wing Area | 1,370 sq ft (127 m2) | |||
Overall height | 40 ft 4 in / 12.3 m | |||
Maximum takeoff weight | 177,000 lb / 80,286 kg | 181,200 lb / 82,191 kg | 194,700 lb / 88,314 kg | |
Maximum landing weight | 145,600 lb / 66,043 kg | 152,800 lb / 69,309 kg | 163,900 lb / 74,344 kg | |
Maximum zero fuel weight | 138,700 lb / 62,913 kg | 145,400 lb / 65,952 kg | 156,500 lb / 70,987 kg | |
Operating empty weight | 99,360 lb / 45,070 kg | |||
Fuel capacity | 6,820 USgal / 25,817 L, excluding ACT | |||
Engine (× 2) | CFM International LEAP-1B, 69 in (175 cm) Fan diameter | |||
Thrust (× 2) | 26,786–29,317 lbf (119–130 kN) | |||
Cruising speed | Mach 0.79 (453 kn; 839 km/h) | |||
Range (2-class) | 3,850 nmi / 7,130 km | 3,550 nmi / 6,570 km
MAX 200: 2,700 nmi (5,000 km) |
3,550 nmi / 6,570 km | 3,300 nmi / 6,110 km |
Ceiling | 41,000 ft (12,000 m) | |||
ICAO Type | B37M | B38M | B39M | B3JM |
Variant | 747-400 | 747-400ER | 747-400F | 747-400ERF | 747-8 | 747-8F |
---|---|---|---|---|---|---|
Cockpit crew | Two | |||||
Capacity | 416 (23F @ 61" + 80J @ 39" + 313Y @ 32") | 274,100 lb / 124,330 kg | 273,400 lb / 124,010 kg | 410 in 3-class | 303,700 lb / 137,700 kg | |
Unit Load Devices | 30 LD1/LD3 | 28 LD1/LD3 | + 2 LD1 + 30 x 96 by 125-in pallet on Main deck | |||
Exit limit | 550/660 | 605 | 8 | |||
Overall length | 231 ft 10 in (70.66 m) | 250 ft 2 in / 76.3 m | ||||
Wingspan | 211 ft 5 in (64.44 m) | 224 ft 7 in / 68.4 m | ||||
Wing area | 5,650 sq ft (525 m2) | 554 m2 (5,960 sq ft) | ||||
Aspect ratio | 7.91 | - | ||||
Overall height | 63 ft 8 in (19.4 m) | 63 ft 6 in / 19.4 m | ||||
Max. takeoff weight | 875,000 lb / 396,890 kg | 910,000 lb / 412,775 kg | 875,000 lb / 396,890 kg | 910,000 lb / 412,775 kg | 987,000 lb / 447,700 kg | |
Operating empty weight | 404,600 lb / 183,520 kg | 412,300 lb / 187,010 kg | 360,900 lb / 163,700 kg | 361,600 lb / 164,020 kg | 485,300 lb / 220,128 kg | 434,600 lb / 197,131 kg |
Fuel capacity | 57,285 US gal (216,840 L) | 63,705 US gal (241,140 L) | 53,985 US gal / 204,350L | 63,034 US gal / 238,610L | 59,734 US gal / 226,118L | |
Cruise | Mach 0.855 (504 kn; 933 km/h) | Mach 0.845 (498 kn; 922 km/h) | Mach 0.86 (493 kn; 914 km/h) | Mach 0.85 (488 kn; 903 km/h) | ||
Airspeed limit | Mach 0.92 (542 kn; 1,004 km/h) | Mach 0.9 (516 kn; 956 km/h) | ||||
Takeoff field length | 9,700 ft / 2,955m | 10,700 ft / 3,260m | 9,550 ft / 2,910m | 10,700 ft / 3,260m | - | |
Range | 7,285nmi / 13,490 km | 7,585nmi / 14,045 km | 2,825nmi / 5,230 km | 4,045nmi / 7,585 km | 8,000 nmi (15,000 km) | 4,120nmi / 7,630 km |
Engines (x 4) | PW4000 / GE CF6 / RR RB211 | PW4000 / GE CF6 | PW4000 / GE CF6 / RR RB211 | PW4000 / GE CF6 | GEnx-2B67 | |
Thrust (x 4) | 56,500–63,300 lbf (251–282 kN) | 62,100–63,300 lbf (276–282 kN) | 56,400–63,300 lbf (251–282 kN) | 62,100–63,300 lbf (276–282 kN) | 66,500 lbf (296 kN) | |
ICAO Type | B744 | B748 |
Variant | 757-200 | 757-200F | 757-300 |
---|---|---|---|
Cockpit crew | Two | ||
2-class seating | 200 (12F+188Y) | - | 243 (12F+231Y) |
1-class seating | 221/228, 239 max | 5 max | 280, 295 max |
Cargo volume | 1,670 ft³ / 43.3 m³ | 6,600 ft³ / 187 m³ | 2,370 ft³ / 61.7 m³ |
Width | 148 in / 3.76 m fuselage, 139.3 in / 3.54 m cabin | ||
Length | 155 ft 3 in / 47.3 m | 178 ft 7 in / 54.4 m | |
Height | 44 ft 6 in / 13.6 m | ||
Wing | 124 ft 10 in / 38.0 m span, 1,994 sq ft (185.25 m2) area, 25° sweep, 7.8 AR | ||
MTOW | 255,000 lb / 115,660 kg | 273,000 lb / 123,830 kg | |
Max. Payload | 57,160 lb / 25,920 kg | 84,420 lb / 38,290 kg | 68,140 lb / 30,910 kg |
OEW | 128,840 lb / 58,440 kg | 115,580 lb / 52,430 kg | 141,860 lb / 64,340 kg |
Fuel capacity | 11,489 US gal / 43,490 L | 11,276 US gal / 42,680 L | 11,466 US gal / 43,400 L |
Speed | Cruise Mach 0.8 (461 kn; 854 km/h), Max. Mach 0.86 (496 kn; 918 km/h) | ||
Range | 3,915nmi / 7,250 km | 2,935nmi / 5,435 km | 3,400nmi / 6,295 km |
Takeoff | 6,800 ft / 2,070 m | 6,900 ft / 2,103 m | 8,550 ft / 2,605 m |
Ceiling | 42,000 ft (13,000 m) | ||
Engines (×2) | 40,200–43,500 lbf (179–193 kN) Rolls-Royce RB211-535E4(B)
36,600–42,600 lbf (163–189 kN) Pratt & Whitney PW2000-37/40/43 | ||
ICAO Type | B752 | B753 |
Variant | 767-200 | 767-200ER | 767-300 | 767-300ER | 767-300F | 767-400ER |
---|---|---|---|---|---|---|
Cockpit crew | Two | |||||
3-class | 174 (15F, 40J, 119Y) | 210 (18F, 42J, 150Y) | 15,469 ft³ / 438m³
58-ton / 52.7 tonnes 24 88×108in pallets |
243 (16F, 36J, 189Y) | ||
2-class | 214 (18J, 196 Y) | 261 (24J, 237Y) | 296 (24J, 272Y) | |||
1-class | 245Y | 290Y | 409Y | |||
Exit limit | 290 | 351 | 375 | |||
Cargo | 3,070 ft³ / 86.9m³ | 4,030 ft³ / 114.1m³ | 4,905 ft³ / 138.9m³ | |||
ULDs | 22 LD2s | 30 LD2s | 38 LD2s | |||
Length | 159 ft 2in / 48.51m | 180 ft 3in / 54.94m | 201 ft 4in / 61.37m | |||
Wingspan | 156 ft 1in / 47.57m | 170 ft 4in / 51.92m | ||||
Wing | 3,050 ft² / 283.3m², 31.5° sweepback | 3,130 ft² / 290.7m² | ||||
Fuselage | 17 ft 9in / 5.41m height, 16 ft 6in / 5.03m width, 186in/ 4.72m Cabin width | |||||
MTOW | 315,000 lb / 142,882 kg | 395,000 lb / 179,169 kg | 350,000 lb / 158,758 kg | 412,000 lb / 186,880 kg | 450,000 lb / 204,116 kg | |
Max. payload | 73,350 lb (33,271 kg) | 78,390 lb (35,557 kg) | 88,250 lb (40,030 kg) | 96,560 lb (43,799 kg) | 119,000 lb (53,977 kg) | 101,000 lb (45,813 kg) |
OEW | 176,650 lb / 80,127 kg | 181,610 lb / 82,377 kg | 189,750 lb / 86,069 kg | 198,440 lb / 90,011 kg | 190,000 lb / 86,183 kg | 229,000 lb / 103,872 kg |
Fuel capacity | 16,700USgal / 63,217L | 24,140Usgal / 91,380L | 16,700USgal / 63,216L | 24,140USgal / 91,380L | ||
111,890 lb / 50,753 kg | 161,738 lb / 73,363 kg | 111,890 lb / 50,753 kg | 161,740 lb / 73,364 kg | |||
Range | 3,900 nmi (7,200 km) | 6,590nmi / 12,200 km | 3,900 nmi (7,200 km) | 5,980nmi / 11,070 km | 3,225nmi / 6,025 km | 5,625nmi / 10,415 km |
Cruise | Long range: 459 kn (850 km/h), Maximum: 486 kn (900 km/h) at 39,000 ft (12,000 m), Ceiling: 43,100 ft (13,100 m) | |||||
Takeoff | 6,300 ft (1,900 m) | 2,480m / 8,150 ft | 9,200 ft (2,800 m) | 2,650m / 8,700 ft | 3,290m / 10,800 ft | |
Engines (×2) | P&W JT9D-7R4/7R4E / P&W PW4052 / GE CF6-80A/A2/C2-B2 | P&W JT9D-7R4/7R4E / P&W PW4052/56 / GE CF6-80A/A2/C2-B2/C2-B4 / RB211-524G/H | P&W JT9D-7R4/7R4E / P&W PW4052 / GE CF6-80A/A2/C2-B2 / RB211-524H | GE CF6-80C2-B4/0C2-B6/C2-B8F/C2-B7F1 / PW4056/60/62 / RB211-524G/H | GE CF6-80C2-B8F/C2-B7F1 / PW4062 | |
Thrust (×2) | 48,000–52,500 lbf (214–234 kN) | 48,000–60,600 lbf (214–270 kN) | 48,000–60,600 lbf (214–270 kN) | 56,750–61,500 lbf (252–274 kN) | 60,600 lbf (270 kN) | |
ICAO Type | B762 | B763 | B764 |
Variant | 777-200 | 777-200ER | 777-200LR | 777F | 777-300 | 777-300ER |
---|---|---|---|---|---|---|
Cockpit crew | Two | |||||
3-class | 305 (24F/54J/227Y) | 301 (16F/58J/227Y) | 368 (30F/84J/254Y) | 365 (22F/70J/273Y) | ||
2-class/capacity | 313 | 317 | 224,900 lb / 102,010 kg | 396 | ||
Exit limit | 440 | 11 | 550 | |||
Length | 209 ft 1 in / 63.73 m | 242 ft 4 in / 73.86 m | ||||
Wingspan | 199 ft 11 in / 60.93 m | 212 ft 7 in / 64.80 m | 199 ft 11 in / 60.93 m | 212 ft 7 in / 64.80 m | ||
Wing sweep | 31.6° | |||||
Wing area | 4,605 sq ft (427.8 m2) | 4,702 sq ft (436.8 m2) | 4,605 sq ft (427.8 m2) | 4,702 sq ft (436.8 m2) | ||
Aspect ratio | 8.68 | 9.04 | 8.68 | 9.04 | ||
Tail height | 60 ft 9 in / 18.5 m | 61 ft 1 in / 18.6 m | 60 ft 8 in / 18.5 m | |||
Cabin width | 231 in / 5.86 m | |||||
Seat width | 18.5 in / 47 cm at 9 abreast, 17 in / 43 cm at 10 abreast | |||||
Fuselage width | 20 ft 4 in / 6.20 m | |||||
Maximum cargo capacity | 5,330 ft³ / 150.9 m³ | 23,051 ft³ / 652.7 m³ | 7,120 ft³ / 201.6 m³ | |||
Maximum takeoff weight (MTOW) | 545,000 lb / 247,200 kg | 656,000 lb / 297,550 kg | 766,000 lb / 347,452 kg | 766,800 lb / 347,815 kg | 660,000 lb / 299,370 kg | 775,000 lb / 351,533 kg |
Max. landing weight | 445,000 lb / 201,840 kg | 470,000 lb / 213,180 kg | 492,000 lb / 223,168 kg | 575,000 lb / 260,816 kg | 524,000 lb / 237,680 kg | 554,000 lb / 251,290 kg |
Operating empty weight | 299,550 lb / 135,850 kg | 304,500 lb / 138,100 kg | 320,000 lb / 145,150 kg | 318,300 lb / 144,379 kg | 353,800 lb / 160,530 kg | 370,000 lb / 167,829 kg |
Fuel capacity | 31,000 US gal / 117,340 L / 207,700 lb / 94,240 kg | 45,220 US gal / 171,171 L / 302,270 lb / 137,460 kg | 47,890 US gal / 181,283 L / 320,863 lb / 145,538 kg | 45,220 US gal / 171,171 L / 302,270 lb / 137,460 kg | 47,890 US gal / 181,283 L / 320,863 lb / 145,538 kg | |
Service ceiling | 43,100 ft (13,100 m) | |||||
Cruise speed | Mach 0.84 (892 km/h; 554 mph) | |||||
Max. speed | Mach 0.89 (945 km/h; 587 mph) | |||||
Range | 5,240 nmi / 9,700 km | 7,065 nmi / 13,080 km | 8,555 nmi / 15,843 km | 4,970 nmi / 9,200 km | 6,030 nmi / 11,165 km | 7,370 nmi / 13,649 km |
Takeoff distance | 8,000 ft
2,440 m |
11,100 ft
3,380 m |
9,200 ft
2,800 m |
9,300 ft
2,830 m |
10,600 ft
3,230 m |
10,000 ft
3,050 m |
Turbofan (×2) | PW 4077
RR 877 GE90-77B |
PW 4090
RR 895 GE90-94B |
GE90-110B1
GE90-115B |
PW 4098
RR 892 GE90-92B/-94B |
GE90-115B | |
Max thrust (×2) | 77,200 lbf (343 kN) | 93,700 lbf (417 kN) | 115,300 lbf (513 kN) | 98,000 lbf (440 kN) | 115,300 lbf (513 kN) | |
ICAO Type | B772 | B77L | B773 | B77W |
Variant | 787-8 | 787-9 | 787-10 |
---|---|---|---|
Cockpit crew | Two | ||
Seating, 2-class | 242 : 24J @85" + 218Y @32" | 290 : 28J @85" + 262Y @32" | 330 : 32J @85" + 298Y @32" |
Seating, 1-class | max. 359, exit limit 381 | max. 406, exit limit 420 | max. 440, exit limit 440 |
Length | 186 ft 1 in (56.72 m) | 206 ft 1 in (62.81 m) | 224 ft (68.28 m) |
Wing | 197 ft 3 in (60.12 m) span, 246.9 in / 6.27 m mean chord, 9.59 aspect ratio, 4,058 sq ft (377 m2) area | ||
Wing sweep | 32.2° | ||
Height | 55 ft 6 in (16.92 m) | 55 ft 10 in (17.02 m) | |
Fuselage | Cabin width: 18 ft 0 in (5.49 m) External width: 18 ft 11 in (5.77 m), height: 19 ft 6 in (5.94 m) | ||
Cargo capacity | 4,826 ft³ /136.7 m³
28 LD3 or 9 (88×125) pallets |
6,090 ft³ / 172.5 m³
36 LD3 or 11 (96×125) pallets |
6,722 ft³ / 191.4 m³
40 LD3 or 13 (96×125) pallets |
MTOW | 502,500 lb / 227,930 kg | 560,000 lb / 254,011 kg | |
MLW | 380,000 lb / 172,365 kg | 425,000 lb / 192,777 kg | 445,000 lb / 201,849 kg |
Maximum ZFW | 355,000 lb / 161,025 kg | 400,000 lb / 181,437 kg | 425,000 lb / 192,777 kg |
OEW | 264,500 lb / 119,950 kg | 284,000 lb / 128,850 kg | 298,700 lb / 135,500 kg |
Fuel capacity | 33,340 US gal / 126,206 L
223,378 lb / 101,323 kg |
33,384 US gal / 126,372 L
223,673 lb / 101,456 kg | |
Speed | Max: Mach 0.90 (516 kn; 956 km/h); Cruise: Mach 0.85 (488 kn; 903 km/h) | ||
Range | 7,355 nmi (13,620 km) | 7,635 nmi (14,140 km) | 6,430 nmi (11,910 km) |
Takeoff | 8,500 ft (2,600 m) | 9,300 ft (2,800 m) | 9,100 ft (2,800 m) |
Ceiling | 43,000 ft (13,100 m) | ||
Engines (×2) | General Electric GEnx-1B or Rolls-Royce Trent 1000 | ||
Thrust (×2) | 64,000 lbf (280 kN) | 71,000 lbf (320 kN) | 76,000 lbf (340 kN) |
ICAO Type | B788 | B789 | B78X |
Subtype | A318[1] | A319[2] | A320[3] | A321[4] | |
---|---|---|---|---|---|
Cockpit crew | 2 | ||||
Exit limit EASA[5]/FAA[6] | 136 | 160 | 195/190 | 230 | |
1-class max. seating[7] | 132 at 模板:Convert pitch | 156 at 模板:Convert pitch | 186 at 模板:Convert pitch[8] | 236 at 模板:Convert pitch[9] | |
1-class, typical[7] | 117 at 模板:Convert pitch | 134 at 模板:Convert pitch | 164 at 模板:Convert pitch | 199 at 模板:Convert pitch | |
2-class, typical[7] | 107 (8F @ 38 in, 99Y @ 32 in) | 124 (8F @ 38 in, 116Y @ 32 in) | 150 (12F @ 36 in, 138Y @ 32 in) | 185 (16F @ 36 in, 169Y @ 32 in) | |
Cargo volume | 模板:Convert | 模板:Convert | 模板:Convert | 模板:Convert | |
Unit load devices | 4× LD3-45 | 7× LD3-45 | 10× LD3-45 | ||
Length | 模板:Convert | 模板:Convert | 模板:Convert | 模板:Convert | |
Wheelbase | 模板:Convert | 模板:Convert | 模板:Convert | 模板:Convert | |
Track | 模板:Convert | ||||
Wingspan | 模板:Convert | 模板:Convert 模板:Efn | |||
Wing area[10] | 模板:Cvt, 10.3 aspect ratio | 模板:Cvt, 10 模板:Abbr | |||
Wing sweepback | 25 degrees[11] | ||||
Tail height | 模板:Convert | 模板:Convert | |||
Fuselage | 模板:Cvt height, 模板:Cvt width, 模板:Cvt cabin width | ||||
MTOW | 模板:Convert | 模板:Convert | 模板:Convert | 模板:Convert | |
Max. payload | 模板:Convert | 模板:Convert | 模板:Convert | 模板:Convert | |
Fuel capacity | 模板:Convert | 模板:Convert | 模板:Convert | 模板:Convert | |
OEW[7] | 模板:Convert | 模板:Convert | 模板:Convert | 模板:Convert | |
Speed | Cruise: 模板:Cvt,[12] 模板:Abbr: 模板:Cvt[12] | ||||
Range, typical payload模板:Efn | 3,100 nmi, 5,750 km | 3,750 nmi, 6,950 km模板:Efn | 3,300 nmi, 6,100 km模板:Efn | 3,200 nmi, 5,950 km模板:Efn | |
ACJ range | 4,200 nmi, 7,800 km[13] | 6,000 nmi, 11,100 km[14] | 4,300 nmi, 7,800 km[15] | ||
Takeoff run (MTOW, SL, ISA) | 模板:Convert[13] | 模板:Convert[14] | 模板:Convert[15] | ||
Landing (MLW, SL, ISA) | 模板:Convert[13] | 模板:Convert[14] | 模板:Convert[15] | ||
Service ceiling | 模板:Convert[5] | ||||
Engines (×2) | CFM International CFM56-5B, 模板:Convert fan | ||||
PW6000A, 模板:Convert fan | IAE V2500A5, 模板:Convert fan | ||||
Thrust (×2) | 模板:Convert | 模板:Convert | 模板:Convert |
Variant | A319neo | A320neo | A321neo |
---|---|---|---|
Cockpit crew | Two | ||
2-class seats | 140 | 165 | 206: 16模板:Abbr @36模板:Nbspin + 190模板:Abbr @30模板:Nbspin[17] |
1-class maximum | 160 | 195[18] @ 27模板:Nbspin[19] | 240 @ 28模板:Nbspin[20] |
Seat width | Economy at 6 abreast: 模板:Convert,[20] 3.7模板:Nbspm (12模板:Nbspft模板:Nbsp1模板:Nbspin) cabin width | ||
Cargo capacity | 27模板:Nbspm³ (976 ft³) | 37模板:Nbspm³ (1,322 ft³) | 51模板:Nbspm³ (1,828 ft³)模板:Efn |
Length | 33.84模板:Nbspm (111模板:Nbspft) | 37.57模板:Nbspm (123模板:Nbspft模板:Nbsp3模板:Nbspin) | 44.51模板:Nbspm (146模板:Nbspft) |
Wingspan | 35.80模板:Nbspm (117模板:Nbspft模板:Nbsp5模板:Nbspin) | ||
Height | 11.76模板:Nbspm (38模板:Nbspft模板:Nbsp7模板:Nbspin) | ||
Max. takeoff weight | 75.5模板:Nbspt (166,400 lb) | 79模板:Nbspt (174,200 lb) | 97模板:Nbspt (213,800 lb) |
Max. payload | 模板:Cvt[21]模板:Rp | 模板:Cvt[22]模板:Rp | 模板:Cvt[23]模板:Rp |
Operating empty | 模板:Cvt | 模板:Cvt | 模板:Cvt |
Fuel capacity | 26,730 l (7,060 USg) | 32,940 l (8,700 USg)模板:Efn | |
Engines (×2) | CFM International LEAP-1A or Pratt & Whitney PW1100G[24] | ||
Fan diameter | PW1100G: 模板:Convert,[25] LEAP-1A: 模板:Convert[26] | ||
Max. Thrust[18] | 模板:Cvt[27][28] | 模板:Cvt | 模板:Cvt |
Speed | Cruise: 模板:Cvt,[24] Max.: 模板:Cvt[29] | ||
Ceiling | 模板:Cvt[18] | ||
Typical range | 6,950 km / 3,750 nmi模板:Efn | 6,500 km / 3,500 nmi模板:Efn | 7,400 km / 4,000 nmi 模板:Efn |
Takeoff | 模板:Cvt[29] | ||
ICAO Type[30] | A19N | A20N | A21N |
A330-200 | A330-200F | A330-300 | |
---|---|---|---|
Cockpit crew | Two | ||
Capacity | 246 (36J @ 60 in + 210Y @ 32 in) | 70,000 kg (154,324 lb) | 300 (36J @ 60 in + 264Y @ 32 in) |
Max seating[32] | 406 | 440 | |
Length | 58.82 m (192.98 ft) | 63.67 m (208.89 ft) | |
Span | Wing: 60.3 m (197.83 ft), Main gear: 12.61 m (41.37 ft) | ||
Wing | 361.6 m² (3,892 ft²), 25% chord wingsweep : 30°,[33] 10.06 Aspect ratio | ||
Tail height[32] | 17.39m / 57’ | 16.90m / 55’5’’ | 16.79m / 55’ |
Fuselage | 5.64 m (222 in) diameter, 5.18 m (204 in) cabin width | ||
Seat width | 0.46 m (18 in) in 8 abreast economy, 0.53 m (21 in) in 6 abreast business | ||
Cargo volume | 132.4 m³ (4673 ft³) | 469.2 m³ (16567 ft³) | 158.4 m³ (5591 ft³) |
Maximum takeoff weight | 242,000 kg (533,519 lb) | 233,000 kg (513,677 lb) | 242,000 kg (533,519 lb) |
Maximum landing weight | 182,000 kg (401,241 lb) | 187,000 kg (412,264 lb) | |
Max zero fuel weight | 170,000 kg (374,786 lb) | 178,000 kg (392,423 lb) | 175,000 kg (385,809 lb) |
Max Payload | 模板:Cvt | 模板:Cvt | 模板:Cvt |
Fuel capacity | 139,090 l (36,744 US gal) - 109,185 kg (240,711 lb) | ||
Operating empty weight | 模板:Cvt | 模板:Cvt | 模板:Cvt |
Cruise | 模板:Cvt (模板:Cvt MMO), 模板:Cvt Service ceiling[34] | ||
Final approach speed (MLW) | 模板:Convert | 模板:Convert | 模板:Convert |
Range[32] | 13,450 km / 7,250 nm (247 pax) | 7,400 km / 4,000 nm | 11,750 km / 6,350 nm (277 pax) |
Runway (SL, ISA, MTOW/MLW) | Takeoff: 2,770 m (9,110 ft), Landing: 1,730 m (5,680 ft)[35] | ||
Engines (×2)[36] | 模板:Convert General Electric CF6-80E1 (except -200F) 模板:Convert Pratt & Whitney PW4000 PW4164/PW4168/PW4170 模板:Convert Rolls-Royce Trent 700 768/772 |
Variant | A340-200[37] | A340-300[37] | A340-500[38] | A340-600[38] |
---|---|---|---|---|
Cockpit crew | Two | |||
Seating | 261 (3-class) [39] or 303 (30F + 273Y) | 277 (3-class) [40] or 335 (30F + 305Y) | 293 [41] or 313 (12F + 36J + 265Y) | 326 [42] or 380 (12F + 54J + 314Y) |
Exit limit[43] | 420模板:Efn/375 | 375/440模板:Efn/375 | 375 | 440 |
Length | 59.39 m / 194.85 ft | 63.69 m / 208.96 ft | 67.93 m / 222.87 ft | 75.36 m / 247.24 ft |
Wingspan | 60.3 m / 197.83 ft | 63.45 m / 208.17 ft | ||
Wing[11] | 模板:Cvt, 29.7° sweep, 10 AR | 模板:Cvt, 31.1° sweep, 9.2 AR | ||
Height | 17.03 m / 55.86 ft | 16.99 m / 55.72 ft | 17.53 m / 57.51 ft | 17.93 m / 58.84 ft |
Fuselage | 5.287 m / 208.15 in cabin width, 5.64 m / 18.5 ft outside width | |||
Cargo volume | 模板:Cvt | 模板:Cvt | 模板:Cvt | 模板:Cvt |
MTOW | 模板:Cvt | 模板:Cvt | 模板:Cvt | |
Max. PL | 模板:Cvt | 模板:Cvt | 模板:Cvt | 模板:Cvt< |
OEW | 模板:Cvt | 模板:Cvt | 模板:Cvt | 模板:Cvt |
Max. Fuel | 110.4 t / 243,395 lb | 175.2 t / 386,292 lb | 155.5 t / 342,905 lb 模板:Efn | |
Engines (×4) | CFM International CFM56-5C | Trent 553 | Trent 556 | |
Thrust (×4)[43] | 模板:Cvt | 模板:Cvt | ||
Speed | 模板:Cvt max,[44] 模板:Cvt cruise | |||
Range, max pax | 模板:Cvt | 模板:Cvt | 模板:Cvt | 模板:Cvt |
Take off模板:Efn | 模板:Cvt | 模板:Cvt | 模板:Cvt | 模板:Cvt |
Ceiling | 12,500 m (41,000 ft)[45] | 12,527 m (41,100 ft)[46] |
Model | A350-900 | A350-1000 |
---|---|---|
Cockpit crew | Two | |
Seating | 325/315 (48B+267Y) ULR: 173=80J+93Y |
366/369 (54B+315Y) 387 (2-class)[48] |
Exit limit | 440[49] | |
Overall length | 66.8 m / 219.5 ft | 73.78 m / 242.7 ft |
Wing | 64.75 m / 212.43 ft span, 31.9° sweep[50] | |
Aspect ratio | 9.49 | 9.03 |
Wing area | 模板:Cvt[51] | 模板:Cvt[52] |
Overall height | 17.05 m / 55 ft 11 in[53] | 17.08 m / 56 ft 0 in[54] |
Fuselage | 5.96 m / 19.7 ft width, 6.09 m / 19.98 ft height | |
Cabin width | 5.61 m / 18 ft 5 in,[53][54] 9-abreast Seat : 18 in / 46 cm模板:Efn | |
MTOW | 280 t / 617,295 lb | 316 t / 696,661 lb |
Max. payload | 模板:Cvt | 模板:Cvt |
Fuel capacity[49] | 模板:Cvt 模板:Cvt模板:Efn |
模板:Cvt 模板:Cvt |
OEW | 模板:Cvt typical 模板:Cvt[50] |
模板:Cvt 模板:Cvt dry[55] |
MEW | 模板:Cvt[56] | 129 t (284,000 lb)[57] |
Cargo capacity | 36 LD3 or 11 pallets | 44 LD3 or 14 pallets |
cruise | 模板:Cvt Typical, 模板:Cvt Maximum[50] | |
Range | 15,000 km / 8,100 nmi模板:Efn[53]模板:Efn | 模板:Cvt模板:Efn[58] |
Takeoff (MTOW, SL, ISA) | 模板:Cvt | |
Landing (MLW, SL, ISA) | 模板:Cvt | |
Service ceiling[49] | 模板:Cvt | 模板:Cvt |
Engines (2×) | Rolls-Royce Trent XWB | |
Maximum thrust[49] | 374.5 kN / 84,200 lbf | 431.5 kN / 97,000 lbf |
Variant | A380-800[59] |
---|---|
Cockpit crew | Two |
Typical seating | 544 (4-class) |
Exit limit | 868[49]模板:Efn |
Length overall | 模板:Convert |
Wingspan | 模板:Convert |
Height | 模板:Convert |
Wheelbase | 模板:Convert |
Wheel track | 模板:Convert, 模板:Convert total width[47] |
Outside fuselage dimensions |
Width: 模板:Convert Height: 模板:Convert |
Maximum cabin width |
模板:Convert main deck 模板:Convert upper deck |
Cabin length | 模板:Convert main deck 模板:Convert upper deck模板:Vn |
Wing area | 模板:Convert[60] |
Aspect ratio | 7.53 |
Wing sweep | 33.5°[60] |
Maximum ramp weight | 模板:Convert |
Maximum take-off weight | 模板:Convert |
Max. landing weight | 模板:Convert |
Max. zero fuel weight | 模板:Convert |
Operating empty weight | 模板:Convert[61] |
Max. structural payload | 模板:Convert[47] |
Maximum cargo volume | 模板:Convert |
Maximum operating speed | 模板:Convert |
Maximum design speed | 模板:Convert模板:Efn[62] |
Cruise speed | 模板:Convert[63] |
Take off (MTOW, SL, ISA) | 模板:Convert[47] |
Landing speed | 模板:Convert[63] |
Range | 15,200 km / 8,200 nmi |
Service ceiling | 模板:Convert[64] |
Max. fuel capacity | 323,545 L / 85,471 USgal[65] |
Engines (4 ×) | Engine Alliance GP7200 / Rolls-Royce Trent 900 |
Thrust (4 ×) | 模板:Convert |
- ↑ 模板:Cite web
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<ref>
标签;未给name属性为A321 described
的引用提供文字 - ↑ 11.0 11.1 模板:Cite web
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<ref>
标签;未给name属性为typecert
的引用提供文字 - ↑ 模板:Cite news
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标签;未给name属性为EASA-TCDS
的引用提供文字 - ↑ 37.0 37.1 模板:Cite web
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- ↑ https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-200.html
- ↑ https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-300.html
- ↑ https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-500.html
- ↑ https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-600.html
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<ref>
标签;未给name属性为tcds
的引用提供文字 - ↑ 模板:Cite web
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<ref>
标签;name属性“ACAP”使用不同内容定义了多次 - ↑ 模板:Cite web
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<ref>
标签;未给name属性为TCDS
的引用提供文字 - ↑ 50.0 50.1 50.2 引用错误:无效
<ref>
标签;未给name属性为AvWeekPilotReport
的引用提供文字 - ↑ 模板:Cite web
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<ref>
标签;未给name属性为AvWeek14jun2018
的引用提供文字 - ↑ 引用错误:无效
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标签;未给name属性为a380_specs
的引用提供文字 - ↑ 60.0 60.1 模板:Cite web
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