常见航空器规格和性能参数：修订间差异

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无编辑摘要
第822行： 第822行：


{| class="wikitable" style="text-align: center"
{| class="wikitable" style="text-align: center"
|+Airbus A320 family characteristics
|-
|-
! colspan=2 |Subtype
! 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>
! 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>
! 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>
第829行： 第830行：
! 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>
! 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="2" |Cockpit crew
| colspan="4" style="text-align:center;" |2
| 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/$FILE/A28NM_Rev24.pdf |title= Type Certificate Data Sheet |date= August 12, 2016 |publisher= FAA}}</ref>
! colspan="2" |Exit limit [[EASA]]<ref name="cert">{{cite web |url= https://www.easa.europa.eu/system/files/dfu/TCDS_EASA%20A%20064_%20Airbus_%20A318_A319_A320_A321_Iss_22.pdf |title= Type Certificate Data Sheet |publisher= EASA |date= 28 June 2016 |deadurl= yes |archiveurl= https://web.archive.org/web/20160915235037/https://www.easa.europa.eu/system/files/dfu/TCDS_EASA%20A%20064_%20Airbus_%20A318_A319_A320_A321_Iss_22.pdf |archivedate= 15 September 2016 |df= dmy-all }}</ref>/[[FAA]]<ref name="FAA-Data">{{cite web |url= http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/57529f07d8f6e3b58625800d0057c1d4/$FILE/A28NM_Rev24.pdf |title= Type Certificate Data Sheet |date= August 12, 2016 |publisher= FAA}}</ref>
|136
|136
|160
|160
第838行： 第839行：
|230
|230
|-
|-
! colspan=2 |1-class max. seating<ref name=AllAbout/>
! colspan="2" |1-class max. seating<ref name="AllAbout" />
|132 at {{convert|29|-|30|in|cm|abbr=on}} pitch
|132 at {{convert|29|-|30|in|cm|abbr=on}} pitch
|156 at {{convert|28|-|30|in|cm|abbr=on}} pitch
|156 at {{convert|28|-|30|in|cm|abbr=on}} pitch
第844行： 第845行：
|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>
|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>
! 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
|117 at {{convert|32|in|cm|abbr=on}} pitch
|134 at {{convert|32|in|cm|abbr=on}} pitch
|134 at {{convert|32|in|cm|abbr=on}} pitch
第850行： 第851行：
|199 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/>
! colspan="2" |2-class, typical<ref name="AllAbout" />
|107 (8F @ 38&nbsp;in, 99Y @ 32&nbsp;in)
|107 (8F @ 38&nbsp;in, 99Y @ 32&nbsp;in)
|124 (8F @ 38&nbsp;in, 116Y @ 32&nbsp;in)
|124 (8F @ 38&nbsp;in, 116Y @ 32&nbsp;in)
第856行： 第857行：
|185 (16F @ 36&nbsp;in, 169Y @ 32&nbsp;in)
|185 (16F @ 36&nbsp;in, 169Y @ 32&nbsp;in)
|-
|-
! colspan=2 |Cargo volume
! colspan="2" |Cargo volume
|{{convert|21.20|m3|cuft|abbr=on}}
|{{convert|21.20|m3|cuft|abbr=on}}
|{{convert|27.70|m3|cuft|abbr=on}}
|{{convert|27.70|m3|cuft|abbr=on}}
第862行： 第863行：
|{{convert|51.70|m3|cuft|abbr=on}}
|{{convert|51.70|m3|cuft|abbr=on}}
|-
|-
! colspan=2 |[[Unit load device]]s
! colspan="2" |[[Unit load device]]s
|
|
|4× LD3-45
|4× LD3-45
第868行： 第869行：
|10× LD3-45
|10× LD3-45
|-
|-
! colspan=2 |Length
! colspan="2" |Length
|{{convert|31.44|m|ftin|abbr=on}}
|{{convert|31.44|m|ftin|abbr=on}}
|{{convert|33.84|m|ftin|abbr=on}}
|{{convert|33.84|m|ftin|abbr=on}}
第874行： 第875行：
|{{convert|44.51|m|ftin|abbr=on}}
|{{convert|44.51|m|ftin|abbr=on}}
|-
|-
! colspan=2 |[[Wheelbase]]
! colspan="2" |[[Wheelbase]]
|{{convert|10.25|m|ftin|abbr=on}}
|{{convert|10.25|m|ftin|abbr=on}}
|{{convert|11.04|m|ftin|abbr=on}}
|{{convert|11.04|m|ftin|abbr=on}}
第880行： 第881行：
|{{convert|16.91|m|ftin|abbr=on}}
|{{convert|16.91|m|ftin|abbr=on}}
|-
|-
! colspan=2 |Track
! colspan="2" |Track
|colspan="4" |{{convert|7.59|m|ftin|abbr=on}}
| colspan="4" |{{convert|7.59|m|ftin|abbr=on}}
|-
|-
! colspan=2 |Wingspan
! colspan="2" |Wingspan
|{{convert|34.10|m|ftin|abbr=on}}
|{{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="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" |Wing area<ref name="A321 described" />
| ||colspan=2 |{{cvt|124|m2|sqft}}, {{#expr:35.8/(124/35.8)round1}} aspect ratio
| || 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}}
|{{cvt|128|m2|sqft}}, {{#expr:35.8/(128/35.8)round1}} {{abbr|AR|aspect ratio}}
|-
|-
! colspan=2 |Wing sweepback
! 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="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
! colspan="2" |Tail height
|{{convert|12.56|m|ftin|abbr=on}}
|{{convert|12.56|m|ftin|abbr=on}}
|colspan=3 |{{convert|11.76|m|ftin|abbr=on}}
| colspan="3" |{{convert|11.76|m|ftin|abbr=on}}
|-
|-
! colspan=2 |Fuselage
! 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="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]]
! colspan="2" |[[Maximum takeoff weight|MTOW]]
|{{convert|68|t|lb|abbr=on}}
|{{convert|68|t|lb|abbr=on}}
|{{convert|75.5|t|lb|abbr=on}}
|{{convert|75.5|t|lb|abbr=on}}
第907行： 第908行：
|{{convert|93.5|t|lb|abbr=on}}
|{{convert|93.5|t|lb|abbr=on}}
|-
|-
! colspan=2 |Max. [[payload]] <!--MZFW-OEW-->
! colspan="2" |Max. [[payload]] <!--MZFW-OEW-->
|{{convert|{{#expr:54.5-39.5}}|t|lb|abbr=on}}
|{{convert|{{#expr:54.5-39.5}}|t|lb|abbr=on}}
|{{convert|{{#expr:58.5-40.8}}|t|lb|abbr=on}}
|{{convert|{{#expr:58.5-40.8}}|t|lb|abbr=on}}
第913行： 第914行：
|{{convert|{{#expr:73.8-48.5}}|t|lb|abbr=on}}
|{{convert|{{#expr:73.8-48.5}}|t|lb|abbr=on}}
|-
|-
! colspan=2 |[[jet fuel|Fuel]] capacity
! colspan="2" |[[jet fuel|Fuel]] capacity
|{{convert|24210|L|USgal|abbr=on|disp=br}}
|{{convert|24210|L|USgal|abbr=on|disp=br}}
|{{convert|24210|-|30190|L|USgal|abbr=on|disp=br}}
|{{convert|24210|-|30190|L|USgal|abbr=on|disp=br}}
第919行： 第920行：
|{{convert|24050|-|30030|L|USgal|abbr=on|disp=br}}
|{{convert|24050|-|30030|L|USgal|abbr=on|disp=br}}
|-
|-
! colspan=2 |[[Operating empty weight|OEW]]<ref name=AllAbout/>
! colspan="2" |[[Operating empty weight|OEW]]<ref name="AllAbout" />
|{{convert|39.5|t|lb|abbr=on|sigfig=3}}
|{{convert|39.5|t|lb|abbr=on|sigfig=3}}
|{{convert|40.8|t|lb|abbr=on|sigfig=3}}
|{{convert|40.8|t|lb|abbr=on|sigfig=3}}
第925行： 第926行：
|{{convert|48.5|t|lb|abbr=on|sigfig=3}}
|{{convert|48.5|t|lb|abbr=on|sigfig=3}}
|-
|-
! colspan=2 |Speed
! 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="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}}
! colspan="2" |Range, typical payload{{efn|Passengers and bags}}
|3,100 nmi, 5,750&nbsp;km
|3,100 nmi, 5,750&nbsp;km
|3,750 nmi, 6,950&nbsp;km{{efn|name=sharklets}}
|3,750 nmi, 6,950&nbsp;km{{efn|name=sharklets}}
第934行： 第935行：
|3,200 nmi, 5,950&nbsp;km{{efn|name=sharklets}}
|3,200 nmi, 5,950&nbsp;km{{efn|name=sharklets}}
|-
|-
! colspan=2 |[[Airbus Corporate Jets|ACJ]] range
! colspan="2" |[[Airbus Corporate Jets|ACJ]] range
|4,200 nmi, 7,800&nbsp;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>
|4,200 nmi, 7,800&nbsp;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&nbsp;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>
|6,000 nmi, 11,100&nbsp;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&nbsp;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>
|4,300 nmi, 7,800&nbsp;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]])
! colspan="2" |Takeoff run (MTOW, SL, [[International standard atmosphere|ISA]])
|{{convert|1780|m|ft|abbr=on}}<ref name=ACJ318/>
|{{convert|1780|m|ft|abbr=on}}<ref name="ACJ318" />
|{{convert|1850|m|ft|abbr=on}}<ref name=ACJ319/>
|{{convert|1850|m|ft|abbr=on}}<ref name="ACJ319" />
|{{convert|2100|m|ft|abbr=on}}<ref name=ACJ320/>
|{{convert|2100|m|ft|abbr=on}}<ref name="ACJ320" />
|
|
|-
|-
! colspan=2 |Landing (MLW, SL, [[International standard atmosphere|ISA]])
! colspan="2" |Landing (MLW, SL, [[International standard atmosphere|ISA]])
|{{convert|1230|m|ft|abbr=on}}<ref name=ACJ318/>
|{{convert|1230|m|ft|abbr=on}}<ref name="ACJ318" />
|{{convert|1360|m|ft|abbr=on}}<ref name=ACJ319/>
|{{convert|1360|m|ft|abbr=on}}<ref name="ACJ319" />
|{{convert|1500|m|ft|abbr=on}}<ref name=ACJ320/>
|{{convert|1500|m|ft|abbr=on}}<ref name="ACJ320" />
|
|
|-
|-
! colspan=2 |Service ceiling
! colspan="2" |Service ceiling
|colspan="4" |{{convert|39,100|-|41,000|ft|m|abbr=on}}<ref name=cert/>
| colspan="4" |{{convert|39,100|-|41,000|ft|m|abbr=on}}<ref name="cert" />
|-
|-
! colspan=2 rowspan=2 |Engines (×2)
! colspan="2" rowspan="2" |Engines (×2)
| colspan="4" |[[CFM International CFM56]]-5B, {{convert|68.3|in|m|abbr=on}} fan
| 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
|[[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="3" |[[IAE V2500]]A5, {{convert|63.5|in|m|abbr=on}} fan
|-
|-
! colspan=2 |Thrust (×2)
! colspan="2" |Thrust (×2)
|{{convert|96|-|106|kN|abbr=on}}
|{{convert|96|-|106|kN|abbr=on}}
|colspan=2 |{{convert|98|-|120|kN|abbr=on}}
| colspan="2" |{{convert|98|-|120|kN|abbr=on}}
|{{convert|133|-|147|kN|abbr=on}}
|{{convert|133|-|147|kN|abbr=on}}
|}
|}
第981行： 第982行：
| 140
| 140
| 165
| 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>
| 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
! 1-class maximum
| 160
| 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>
| 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>
| 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]]
! [[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
| 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
! Cargo capacity
第1,027行： 第1,028行：
|-
|-
! Engines (×2)
! Engines (×2)
| colspan="3" | [[CFM International LEAP]]-1A or [[Pratt & Whitney PW1000G|Pratt & Whitney PW1100G]]<ref name="Airbus A320neo Technology"/>
| colspan="3" | [[CFM International LEAP]]-1A or [[Pratt & Whitney PW1000G|Pratt & Whitney PW1100G]]<ref name="Airbus A320neo Technology" />
|-
|-
! Fan diameter
! 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>
| 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/>
! 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|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|27120|lbf|kN|order=flip}}
第1,038行： 第1,039行：
|-
|-
! Speed
! 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/>
| 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
! Ceiling
| colspan=3 | {{cvt|39100|-|39800|ft}}<ref name=typecert/>
| colspan="3" | {{cvt|39100|-|39800|ft}}<ref name="typecert" />
|-
|-
! Typical range
! Typical range
第1,051行： 第1,052行：
|
|
|
|
| {{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>
| {{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>
! ICAO Type<ref>{{cite web |title= DOC 8643 – Aircraft Type Designators |url= http://www.icao.int/publications/DOC8643/Pages/default.aspx |publisher= ICAO}}</ref>
第1,067行： 第1,068行：
|-
|-
! Cockpit crew
! Cockpit crew
| colspan=3 | Two
| colspan="3" | Two
|-
|-
! Capacity
! Capacity
第1,074行： 第1,075行：
| 300 (36J @ 60 in + 264Y @ 32 in)
| 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>
! 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 ||
| 406 ||
| 440
| 440
第1,086行： 第1,087行：
|-
|-
! Wing
! Wing
| colspan="3" | 361.6 m² (3,892&nbsp;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
| colspan="3" | 361.6 m² (3,892&nbsp;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/>
! Tail height<ref name="Backgrounder" />
| 17.39m / 57’
| 17.39m / 57’
| 16.90m / 55’5’’
| 16.90m / 55’5’’
第1,111行： 第1,112行：
! [[Maximum landing weight]]
! [[Maximum landing weight]]
| 182,000&nbsp;kg (401,241&nbsp;lb)
| 182,000&nbsp;kg (401,241&nbsp;lb)
| colspan=2 | 187,000&nbsp;kg (412,264&nbsp;lb)
| colspan="2" | 187,000&nbsp;kg (412,264&nbsp;lb)
|-
|-
! Max zero fuel weight
! Max zero fuel weight
第1,124行： 第1,125行：
|-
|-
! Fuel capacity
! Fuel capacity
| colspan=3 | 139,090 l (36,744 US gal) - 109,185&nbsp;kg (240,711&nbsp;lb)
| colspan="3" | 139,090 l (36,744 US gal) - 109,185&nbsp;kg (240,711&nbsp;lb)
|-
|-
! [[Operating empty weight]]<!-- OEW = MZFW - max PL -->
! [[Operating empty weight]]<!-- OEW = MZFW - max PL -->
第1,132行： 第1,133行：
|-
|-
! Cruise
! 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>
| 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)
! Final approach speed (MLW)
第1,139行： 第1,140行：
| {{Convert|137|knots|km/h|abbr=on|0}}
| {{Convert|137|knots|km/h|abbr=on|0}}
|-
|-
! Range<ref name=Backgrounder/>
! Range<ref name="Backgrounder" />
| 13,450&nbsp;km / 7,250&nbsp;nm (247 pax)
| 13,450&nbsp;km / 7,250&nbsp;nm (247 pax)
| 7,400&nbsp;km / 4,000&nbsp;nm
| 7,400&nbsp;km / 4,000&nbsp;nm
第1,145行： 第1,146行：
|-
|-
! Runway (SL, ISA, MTOW/MLW)
! Runway (SL, ISA, MTOW/MLW)
| colspan="3" | Takeoff: 2,770 m (9,110&nbsp;ft), Landing: 1,730 m (5,680&nbsp;ft)<ref name=ACJ330>{{cite web |url= http://www.airbus.com/aircraftfamilies/corporate/acj-family/acj330/ |publisher= Airbus Corporate Jets |title= ACJ330}}</ref>
| colspan="3" | Takeoff: 2,770 m (9,110&nbsp;ft), Landing: 1,730 m (5,680&nbsp;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/>
! 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
| 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
|}
|}


第1,154行： 第1,155行：
|-
|-
! Variant
! 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>
! A340-200<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/>
! A340-300<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>
! A340-500<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/>
! A340-600<ref name="500600ACAP" />
|-
|-
! Cockpit crew
! Cockpit crew
| colspan="4"| Two
| colspan="4" | Two
|-
|-
! Seating
! Seating
第1,168行： 第1,169行：
| 326 <ref>https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-600.html</ref> or 380 (12F + 54J + 314Y)
| 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"/>
! Exit limit<ref name="tcds" />
| 420{{efn|name=4tAdoors|4 Type A doors}}/375
| 420{{efn|name=4tAdoors|4 Type A doors}}/375
| 375/440{{efn|name=4tAdoors}}/375
| 375/440{{efn|name=4tAdoors}}/375
第1,181行： 第1,182行：
|-
|-
! Wingspan
! Wingspan
| colspan="2"| 60.3 m / 197.83 ft
| colspan="2" | 60.3 m / 197.83 ft
| colspan="2"| 63.45 m / 208.17 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>
! 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|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]]
| colspan="2" | {{cvt|437.3|m2}}, 31.1° sweep, {{#expr:63.45/(437.3/63.45)round1}} [[Wing aspect ratio|AR]]
|-
|-
! Height
! Height
第1,195行： 第1,196行：
|-
|-
!  Fuselage
!  Fuselage
| colspan="4"| 5.287 m / 208.15 in cabin width, 5.64 m / 18.5 ft outside width
| colspan="4" | 5.287 m / 208.15 in cabin width, 5.64 m / 18.5 ft outside width
|-
|-
! Cargo volume
! Cargo volume
第1,206行： 第1,207行：
| {{cvt|275|t|lb}}
| {{cvt|275|t|lb}}
| {{cvt|276.5|t|lb}}
| {{cvt|276.5|t|lb}}
| colspan=2 | {{cvt|380|t|lb}}
| colspan="2" | {{cvt|380|t|lb}}
|-
|-
! Max. [[Payload|PL]]
! Max. [[Payload|PL]]
第1,221行： 第1,222行：
|-
|-
! Max. Fuel
! Max. Fuel
| colspan=2 | 110.4 t / 243,395 lb
| colspan="2" | 110.4 t / 243,395 lb
| 175.2 t / 386,292 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}}
| 155.5 t / 342,905 lb {{efn|no aux. tank, 164 t / 361 595 lb with 1 aux. tank}}
|-
|-
! Engines (×4)
! Engines (×4)
| colspan=2| [[CFM International CFM56]]-5C
| colspan="2" | [[CFM International CFM56]]-5C
| [[Rolls-Royce Trent 500|Trent 553]] || [[Rolls-Royce Trent 500|Trent 556]]
| [[Rolls-Royce Trent 500|Trent 553]] || [[Rolls-Royce Trent 500|Trent 556]]
|-
|-
! Thrust (×4)<ref name="tcds" />
! Thrust (×4)<ref name="tcds" />
| colspan=2| {{cvt|138.78|-|151.24|kN}}  
| colspan="2" | {{cvt|138.78|-|151.24|kN}}  
| colspan=2| {{cvt|55,780|-|61902|lbf|kN|order=flip}}
| colspan="2" | {{cvt|55,780|-|61902|lbf|kN|order=flip}}
|-
|-
! Speed
! 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
| 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
! Range, max pax
第1,249行： 第1,250行：
|-
|-
! Ceiling
! Ceiling
| colspan="2"| 12,500 m (41,000&nbsp;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" | 12,500 m (41,000&nbsp;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&nbsp;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>
| colspan="2" | 12,527 m (41,100&nbsp;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"
{| 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>
|+ 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
!Model
!A350-900
!A350-900
第1,260行： 第1,261行：
|-
|-
|Cockpit crew
|Cockpit crew
|colspan="2" |Two
| colspan="2" |Two
|-  
|-  
|Seating
|Seating
|325/315 (48B+267Y)<br/>ULR: 173=80J+93Y
|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/>
|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
|Exit limit
|colspan=2 |440<ref name=TCDS/>
| colspan="2" |440<ref name="TCDS" />
|-
|-
|Overall length
|Overall length
第1,274行： 第1,275行：
|-  
|-  
|Wing
|Wing
|colspan="2" |64.75 m / 212.43&nbsp;ft span, 31.9° [[Swept wing|sweep]]<ref name=AvWeekPilotReport/>
| colspan="2" |64.75 m / 212.43&nbsp;ft span, 31.9° [[Swept wing|sweep]]<ref name="AvWeekPilotReport" />
|-
|-
|Aspect ratio
|Aspect ratio
第1,281行： 第1,282行：
|-  
|-  
|Wing area
|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|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>
|{{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
|Overall height
第1,289行： 第1,290行：
|-  
|-  
|Fuselage  
|Fuselage  
|colspan="2" |5.96 m / 19.7&nbsp;ft width, 6.09 m / 19.98&nbsp;ft height
| colspan="2" |5.96 m / 19.7&nbsp;ft width, 6.09 m / 19.98&nbsp;ft height
|-  
|-  
|Cabin width
|Cabin width
|colspan="2" |5.61 m / 18&nbsp;ft 5 in,<ref name="A350-900_specs"/><ref name="A350-1000_specs"/> 9-abreast Seat : 18 in / 46&nbsp;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>}}
| colspan="2" |5.61 m / 18&nbsp;ft 5 in,<ref name="A350-900_specs" /><ref name="A350-1000_specs" /> 9-abreast Seat : 18 in / 46&nbsp;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]]
|[[Maximum takeoff weight|MTOW]]
第1,302行： 第1,303行：
| {{cvt|64.2|t|lb}}
| {{cvt|64.2|t|lb}}
|-
|-
|Fuel capacity<ref name=TCDS/>
|Fuel capacity<ref name="TCDS" />
|{{cvt|140,795|L|USgal}}<br/>{{cvt|110,523|kg}}{{efn|name=ER}}
|{{cvt|140,795|L|USgal}}<br />{{cvt|110,523|kg}}{{efn|name=ER}}
|{{cvt|158,791|L|USgal}}<br/>{{cvt|124,651|kg}}
|{{cvt|158,791|L|USgal}}<br />{{cvt|124,651|kg}}
|-  
|-  
| [[Operating empty weight|OEW]]<!--MZFW-max payload-->
| [[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: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>
| {{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]]
|[[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>
|{{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&nbsp;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>
|129 t (284,000&nbsp;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
|Cargo capacity
第1,319行： 第1,320行：
|-  
|-  
|cruise
|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/>
| 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
|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>}}
|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/>
|{{cvt|8,400|nmi|km|order=flip}}{{efn|366 passengers, 316 t MTOW}}<ref name="AvWeek14jun2018" />
|-
|-
|Takeoff (MTOW, SL, ISA)
|Takeoff (MTOW, SL, ISA)
第1,333行： 第1,334行：
|
|
|-
|-
|Service ceiling<ref name=TCDS/>
|Service ceiling<ref name="TCDS" />
|{{cvt|43,100|ft}}
|{{cvt|43,100|ft}}
|{{cvt|41,450|ft}}
|{{cvt|41,450|ft}}
|-  
|-  
|Engines (2×)
|Engines (2×)
|colspan="2" |[[Rolls-Royce Trent XWB]]
| colspan="2" |[[Rolls-Royce Trent XWB]]
|-  
|-  
|Maximum thrust<ref name=TCDS/>
|Maximum thrust<ref name="TCDS" />
|374.5&nbsp;kN / 84,200&nbsp;lbf
|374.5&nbsp;kN / 84,200&nbsp;lbf
|431.5&nbsp;kN / 97,000&nbsp;lbf
|431.5&nbsp;kN / 97,000&nbsp;lbf
第1,348行： 第1,349行：
|-
|-
! Variant
! Variant
! A380-800<ref name="a380_specs"/>
! A380-800<ref name="a380_specs" />
|-
|-
| Cockpit crew
| Cockpit crew
第1,357行： 第1,358行：
|-
|-
| Exit limit
| Exit limit
| 868<ref name=TCDS/>{{efn|538 main deck, 330 upper deck}}
| 868<ref name="TCDS" />{{efn|538 main deck, 330 upper deck}}
|-
|-
| [[Length overall]]
| [[Length overall]]
第1,384行： 第1,385行：
|-
|-
| Wing area
| 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>
| {{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]]
| [[Aspect ratio (wing)|Aspect ratio]]
第1,390行： 第1,391行：
|-
|-
| [[Swept wing|Wing sweep]]
| [[Swept wing|Wing sweep]]
| 33.5°<ref name=prestigeSpecs/>
| 33.5°<ref name="prestigeSpecs" />
|-
|-
| Maximum ramp weight
| Maximum ramp weight
第1,408行： 第1,409行：
|-
|-
| Max. structural payload
| Max. structural payload
| {{convert|84|t|lb|abbr=on}}<ref name=ACAP/>
| {{convert|84|t|lb|abbr=on}}<ref name="ACAP" />
|-
|-
| Maximum cargo volume
| Maximum cargo volume
第1,420行： 第1,421行：
|-
|-
| Cruise speed  
| Cruise speed  
| {{convert|0.85|Mach|43,000|km/h kn|sigfig=3}}<ref name=HuberStop/>
| {{convert|0.85|Mach|43,000|km/h kn|sigfig=3}}<ref name="HuberStop" />
|-
|-
| Take off ([[Maximum Takeoff Weight|MTOW]], SL, ISA)
| Take off ([[Maximum Takeoff Weight|MTOW]], SL, ISA)
| {{convert|3000|m|ft|abbr=on}}<ref name="ACAP"/>
| {{convert|3000|m|ft|abbr=on}}<ref name="ACAP" />
|-
|-
| Landing speed
| 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>
| {{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
| Range
第1,443行： 第1,444行：
| {{convert|311|kN|lbf|abbr=on}}
| {{convert|311|kN|lbf|abbr=on}}
|}
|}
<references />

2018年7月7日 (六) 08:02的版本

Boeing 737 Next Generation Characteristics
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
Boeing 737 MAX Characteristics
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
Boeing 747 Characteristics
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
Boeing 757 Characteristics
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
767 Airplane Characteristics
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
Boeing 777 specifications
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
Boeing 787 Dreamliner characteristics
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
Airbus A320 family characteristics
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
Airbus family figures[16]
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
Airbus A330 specifications[31] unless noted
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]
A350 aircraft characteristics[47]
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
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  36. ↑ 引证错误：<ref>标签无效；未给name（名称）为EASA-TCDS的ref（参考）提供文本
  37. ↑ 37.0 37.1 模板:Cite web
  38. ↑ 38.0 38.1 模板:Cite web
  39. ↑ https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-200.html
  40. ↑ https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-300.html
  41. ↑ https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-500.html
  42. ↑ https://www.airbus.com/aircraft/previous-generation-aircraft/a340-family/a340-600.html
  43. ↑ 43.0 43.1 引证错误：<ref>标签无效；未给name（名称）为tcds的ref（参考）提供文本
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  47. ↑ 47.0 47.1 47.2 47.3 模板:Cite web 引证错误：<ref>标签无效；同一name（名称）“ACAP”以不同内容定义了多次
  48. ↑ 模板:Cite web
  49. ↑ 49.0 49.1 49.2 49.3 49.4 引证错误：<ref>标签无效；未给name（名称）为TCDS的ref（参考）提供文本
  50. ↑ 50.0 50.1 50.2 引证错误：<ref>标签无效；未给name（名称）为AvWeekPilotReport的ref（参考）提供文本
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  55. ↑ 模板:Cite news
  56. ↑ 模板:Cite news
  57. ↑ 模板:Cite news
  58. ↑ 引证错误：<ref>标签无效；未给name（名称）为AvWeek14jun2018的ref（参考）提供文本
  59. ↑ 引证错误：<ref>标签无效；未给name（名称）为a380_specs的ref（参考）提供文本
  60. ↑ 60.0 60.1 模板:Cite web
  61. ↑ 模板:Cite web
  62. ↑ 模板:Cite web
  63. ↑ 63.0 63.1 模板:Cite news
  64. ↑ 模板:Cite web
  65. ↑ 模板:Cite web
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