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
无编辑摘要
第2行： 第2行：
|+Boeing 737 性能规格参数
|+Boeing 737 性能规格参数
!
!
! colspan="4" |Boeing 737 Next Generation
! colspan="3" |Boeing 737 Next Generation
! colspan="4" |Boeing 737 MAX
! colspan="4" |Boeing 737 MAX
|-
|-
! 机型
! 机型
! 737-600
! 737-700
! 737-700
! 737-800
! 737-800
第16行： 第15行：
|-  
|-  
!长度
!长度
| 31.24 m
| 33.63 m
| 33.63 m
| 39.47 m
| 39.47 m
第26行： 第24行：
|-  
|-  
! 高度
! 高度
| colspan="2" | 12.57 m
|12.57 m
| colspan="2" | 12.55 m
| colspan="2" | 12.55 m
| colspan="4" |12.3 m
| colspan="4" |12.3 m
|-  
|-  
! 翼展
! 翼展
| colspan="4" | 34.32 m（无翼梢小翼）；35.79m（有翼梢小翼）
| colspan="3" |34.32 m（无翼梢小翼）；35.79m（有翼梢小翼）
| colspan="4" |35.92 m
| colspan="4" |35.92 m
|-  
|-  
! 空重（OEW）
! OEW
| 36,378 kg
| 7,648 kg
| 7,648 kg
| 41,413 kg
| 41,413 kg
第44行： 第41行：
| -
| -
|-  
|-  
! 最大起飞重量（MTOW）
! MTOW
| 65,998 kg
| 70,080 kg
| 70,080 kg
| 79,016 kg
| 79,016 kg
第52行： 第48行：
|82,191 kg
|82,191 kg
|88,314 kg
|88,314 kg
| -
|-
! 最大降落重量（MLW）
| 55,111 kg
| 58,604 kg
| 66,361 kg
| 71,350 kg
|66,043 kg
|69,309 kg
|74,344 kg
| -
| -
|-  
|-  
! 最大燃料容量
! 最大燃料容量
| colspan="3" | 26,022 L  
| colspan="2" |26,022 L
| 29,666 L
| 29,666 L
| colspan="4" |25,817 L
| colspan="4" |25,817 L
|-  
|-  
! 实用升限
! 实用升限
| colspan="4" | 12500 m（41000 ft）
| colspan="3" |12500 m（41000 ft）
|
|
|
|
第76行： 第62行：
|
|
|-  
|-  
! 巡航速度
! 典型巡航马赫数
| Mach 0.785 (453 kn; 838 km/h)
| colspan="7" | Mach 0.785
| Mach 0.781 (450 kn; 834 km/h)
| Mach 0.789 (455 kn; 842 km/h)
| Mach 0.79 (455 kn; 844 km/h)
| colspan="4" |Mach 0.79 (453 kn; 839 km/h)
|-  
|-  
! 航程
! 航程
| 5,991 km
| 3,010 nmi
| 3,010 nmi
| 5,436 km)
| 5,436 km)
第96行： 第77行：
|-
|-
!消防保障等级
!消防保障等级
| colspan="2" |6级
|6级
| colspan="6" |7级
| colspan="6" |7级
|-
|-
! ICAO代码
! ICAO代码
|B736
|B737
|B737
|B738
|B738
第114行： 第94行：
!Model
!Model
!747-400
!747-400
!747-400ER<ref name="400pax" />
!747-400ER
!747-400F<ref name="400F" />
!747-400F
!747-400ERF
!747-400
|-
| Overall length
| colspan="4" | 70.66&nbsp;m
|-
|Overall height
| colspan="4" | 63&nbsp;ft 8 in (19.4&nbsp;m)
|-
| Wingspan
| colspan="4" | 211&nbsp;ft 5 in (64.44&nbsp;m)
|-
| Operating empty weight
| PW: 404,600&nbsp;lb / 183,520&nbsp;kg
| PW: 412,300&nbsp;lb / 187,010&nbsp;kg
| GE: 360,900&nbsp;lb / 163,700&nbsp;kg
| GE: 361,600&nbsp;lb / 164,020&nbsp;kg
|-
| Max. takeoff weight
| 875,000&nbsp;lb / 396,890&nbsp;kg
| 910,000&nbsp;lb / 412,775&nbsp;kg
| 875,000&nbsp;lb / 396,890&nbsp;kg
| 910,000&nbsp;lb / 412,775&nbsp;kg
|-
| Fuel capacity
| 57,285 US gal (216,840&nbsp;L)
| 63,705 US gal (241,140&nbsp;L)
| colspan="2" |53,985 US gal / 204,350L
|-
| Cruise
| colspan="2" | {{convert|0.855|Mach|32,000|knots km/h|0}}
| colspan="2" | {{convert|0.845|Mach|32,000|knots km/h|0}}
|-
| Airspeed limit<ref name="TypeCert" />
| colspan="4" |{{convert|0.92|Mach|32,000|knots km/h|0}}
|-
| Takeoff field length{{efn|SL, 86°F, MTOW}}
| 9,700&nbsp;ft / 2,955m
| 10,700&nbsp;ft / 3,260m
| 9,550&nbsp;ft / 2,910m
| 10,700&nbsp;ft / 3,260m
|-
| Range
| 7,285nmi / 13,490&nbsp;km{{efn|name=PW416pax|PW engines, 416 pax}}
| 7,585nmi / 14,045&nbsp;km{{efn|name=PW416pax}}
| 2,825nmi / 5,230&nbsp;km
| 4,045nmi / 7,585&nbsp;km
|}
 
{| style="text-align: center" class="wikitable"
|+Boeing 737 Characteristics<ref name=Boeing_airp_report>{{cite web |url= http://www.boeing.com/assets/pdf/commercial/airports/acaps/737.pdf |title= Boeing 737 Airplane Characteristics for Airport Planning |publisher= Boeing Commercial Airplanes |date= September 2013}}</ref>
! Variant
! 737-600
! 737-700
! 737-800
! 737-900ER
|-
! Cockpit crew
| colspan=4 | Two
|-
! 2-class{{rp|56–62}}
| 108 (8F@36" 100Y@32")
| 128 (8F@36" 120Y@32")
| 160 (12F@36" 148Y@32")
| 177 (12F@36" 165Y@32")
|-
! 1-class{{rp|56–62}}
| 123 @32" - 130 @ 30"
| 140 @32" - 148 @ 30"
| 175 @32" - 184 @ 30"
| 177 @32" - 215 @ 28"
|-
! Exit Limit<ref name=FAAcert>{{cite web |url= http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/cb5a51687a9853cd86257fcb0064c0a9/$FILE/A16WE_Rev56.pdf |title= Type Certificate Data Sheet |publisher= FAA |date= June 3, 2016}}</ref>
| colspan=2 | 149
| 189
| 220
|-
! Seat width{{rp|67}}
| colspan=4 | First : 22in / 56&nbsp;cm; Economy : 17in / 43&nbsp;cm
|-
! Length{{rp|34–41}}
| 102&nbsp;ft 6&nbsp;in / 31.24&nbsp;m
| 110&nbsp;ft 4&nbsp;in / 33.63&nbsp;m
| 129&nbsp;ft 6&nbsp;in / 39.47&nbsp;m
| 138&nbsp;ft 2&nbsp;in / 42.11&nbsp;m
|-
! Height{{rp|34–41}}
| colspan=2 | 41&nbsp;ft 3&nbsp;in / 12.57&nbsp;m
| colspan=2 | 41&nbsp;ft 2&nbsp;in &nbsp;(12.55&nbsp;m)
|-
! Wing<ref name=Elsevier>{{cite web |url= http://booksite.elsevier.com/9780340741528/appendices/data-a/table-2/table.htm |title= Civil jet aircraft design |publisher= Elsevier |at= Aircraft Data File - Boeing Aircraft |date= 2001}}</ref>
| colspan=4 | Span: 112&nbsp;ft 7&nbsp;in / 34.32&nbsp;m, with winglets: 117&nbsp;ft 5in / 35.79m;{{rp|34–41}} Area: {{cvt|124.60|m2|sqft}}; Sweepback: 25°; {{abbr|AR|Aspect ratio}}: 9.44
|-
! Fuselage{{rp|67}}
| colspan=4 | Width: 12&nbsp;ft 4&nbsp;in (3.76&nbsp;m); Cabin width: 11&nbsp;ft 7&nbsp;in (3.54&nbsp;m); Cabin height: 86.6&nbsp;in (2.20&nbsp;m)
|-
! [[Operating empty weight|OEW]]{{rp|21–24}}
| 80,200&nbsp;lb / 36,378&nbsp;kg
| 83,000&nbsp;lb / 37,648&nbsp;kg
| 91,300&nbsp;lb / 41,413&nbsp;kg
| 98,495&nbsp;lb / 44,677&nbsp;kg
|-
! [[Maximum landing weight|MLW]]{{rp|21–24}}
| 121,500&nbsp;lb / 55,111&nbsp;kg
| 129,200&nbsp;lb / 58,604&nbsp;kg
| 146,300&nbsp;lb / 66,361&nbsp;kg
| 157,300&nbsp;lb / 71,350&nbsp;kg
|-
! [[Maximum take-off weight|MTOW]]{{rp|21–24}}
| 144,500&nbsp;lb / 65,544&nbsp;kg
| 154,500&nbsp;lb / 70,080&nbsp;kg
| 174,200&nbsp;lb / 79,016&nbsp;kg
| 187,700&nbsp;lb / 85,139&nbsp;kg
|-
! Fuel capacity{{rp|21–24}}
| colspan=3 | 6,875 US gal / 26,022 L
| 7,837 US gal / 29,666 L{{efn|two auxiliary tanks}}
|-
! Lower deck cargo{{rp|21–24}}
| 720&nbsp;ft³ / 20.4&nbsp;m³
| 966&nbsp;ft³ / 27.4&nbsp;m³
| 1,555&nbsp;ft³ / 44.1&nbsp;m³
| 1,826&nbsp;ft³ / 51.7&nbsp;m³
|-
! Takeoff run{{efn|[[MTOW]], sea level, [[International standard atmosphere|ISA]]+20°C}}<ref name=Elsevier/>
| {{convert|1878|m|ft|abbr=on|order=flip}}
| {{convert|2042|m|ft|abbr=on|order=flip}}
| {{convert|2316|m|ft|abbr=on|order=flip}}
| {{convert|3000|m|ft|abbr=on|order=flip}}{{rp|159}}
|-
! Flight envelope<ref name=FAAcert/>
| colspan=4 | {{convert|41,000|ft|m|0}} Ceiling, {{cvt|0.82|Mach|41,000|knots km/h|0}} MMo
|-
! Cruise<ref name=backgrounder>{{cite web |url=  http://www.boeing.com/resources/boeingdotcom/media/paris2015/pdf/Backgrounders/bkg_NG_737_family.pdf |title= Next-Generation 737 Family Backgrounder |publisher= Boeing |date= February 2015}}</ref>
| {{convert|0.785|Mach|35,000|knots km/h|0}}
| {{convert|0.781|Mach|35,000|knots km/h|0}}
| {{convert|0.789|Mach|35,000|knots km/h|0}}
| {{convert|0.79|Mach|35,000|knots km/h|0}}
|-
! Range<ref>{{cite news |url= https://www.flightglobal.com/news/articles/boeing-revises-obsolete-performance-assumptions-415293/ |title= Boeing revises "obsolete" performance assumptions |date= 3 August 2015 |work= Flight Global}}</ref>
| {{convert|3,235|nmi|km|abbr=on}}{{efn|110 passengers}}<ref name=backgrounder/>
| {{convert|3,010|nmi|km|abbr=on}}{{efn|126 passengers}}
| {{convert|2,935|nmi|km|abbr=on}}{{efn|162 passengers}}
| {{convert|2,950|nmi|km|abbr=on}}{{efn|178 passengers}}
|-
! Engines (× 2)
| [[CFM International CFM56#CFM56-7 series|CFM56-7B]]18/20/22{{rp|126–133}}
| CFM56-7B20/22/24/26/27{{rp|134–149}}
| colspan=2 | CFM56-7B24/26/27{{rp|150–161}}
|-
! Thrust (× 2)
| {{cvt|20,000|-|22,000|lbf|kN|disp=br}} {{rp|126–133}}
| {{cvt|20,000|-|26,000|lbf|kN|disp=br}}{{rp|134–149}}
| {{cvt|24,000|-|27,000|lbf|kN|disp=br}}{{rp|150–153}}
| {{cvt|24,000|-|27,000|lbf|kN|disp=br}}{{rp|154–161}}
|-
! Cruise max. thrust{{efn|35,000 ft – Mach 0.8 – ISA}}<ref name="CFM56-7B"/>
| colspan=4 | {{cvt|5,960|lbf|kN}} (climb)
|-
! Engine dimensions<ref name="CFM56-7B">{{cite news |url= http://www.safran-aircraft-engines.com/file/download/fiche_cfm56-7b_ang.pdf |title= CFM56-7B |publisher= Safran/Snecma |date= March 2011}}</ref>
| colspan=4 | Fan tip diameter: {{cvt|61|in|cm|0}}, length: {{cvt|103.50|in|cm|0}}
|-
! Engine ground clearance
| colspan=2 | 18 in / 46&nbsp;cm{{rp|44}}
| colspan=2 | 19 in / 48&nbsp;cm{{rp|45}}
|-
! ICAO Type<ref>{{cite web |title= DOC 8643 – Aircraft Type Designators |url= http://www.icao.int/publications/DOC8643/Pages/default.aspx |publisher= ICAO}}</ref>
|B736
|B737
|B738
|B739
|}
 
{| style="text-align: center" class="wikitable"
|+ 737 MAX Brochure<ref name=brochure>{{cite web |url= http://www.boeing.com/assets/pdf/commercial/airports/acaps/737MaxBrochure.pdf |title= 737 MAX Airport Compatibility Brochure |publisher= [[Boeing]] |date= June 2017}}</ref><ref name="tech_specs">{{cite web |url= http://www.boeing.com/commercial/737max/#/technical-specs |title= 737 MAX |at= Technical Specs |publisher= Boeing}}</ref>
|-
! Variant !! 737 MAX 7 !! 737 MAX 8 / MAX 200 !! 737 MAX 9 !! 737 MAX 10
|-
! Seating
| 138 (8{{abbr|J|business class}} + 130{{abbr|Y|economy class}}) to 172 max
| 162 (12{{abbr|J|business class}} + 150{{abbr|Y|economy class}}) to 210 max
| 178 (16{{abbr|J|business class}} + 162{{abbr|Y|economy class}}) to 220 max
| 188 to 230 max
|- 
! [[Airline seat#Seat pitch|Seat pitch]]
| colspan=4 | {{cvt|28|-|29|in|cm}} in high density, {{cvt|31|-|32|in|cm}} in economy, {{cvt|36|in|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
| colspan=4 | 117 ft 10 in / 35.92 m
|-
! Wing Area
| colspan=4 | {{cvt|{{#expr:155.81/12*(117-12+(10-4)/12)round0}}|sqft|m2}} <!-- 155.81 in Mean Aerodynamic Chord * wingspan - 12 ft 4 fuselage width --><ref name=FAA-TCDS/>
|-
! Overall height<ref name=characteristics>{{cite web |url= http://www.boeing.com/commercial/737max/#/design-highlights/characteristics/ |title= Boeing 737 MAX characteristics |publisher= [[Boeing]]}}</ref>
| colspan=4 | 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]]<ref name=ACAP>{{cite web |url= http://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/737MAX_RevA.pdf |title= 737 MAX Airplane Characteristics for Airport Planning |date= August 2017 |publisher= Boeing }}</ref>
|
| 99,360 lb / 45,070 kg
|
|
|-
! Fuel capacity
| colspan=4 | 6,820 USgal / 25,817 L, excluding {{abbr|ACT|Auxiliary Center Tank}}
|-
! Engine (× 2)
| colspan=4 | [[CFM International LEAP|CFM International LEAP-1B]], {{cvt|69|in|cm|0}} Fan diameter<ref name="LEAP-Brochure">{{cite web |url= http://www.cfmaeroengines.com/files/brochures/LEAP-Brochure-2013.pdf |title= LEAP Brochure |publisher= [[CFM International]] |date= 2013 |archive-url= https://web.archive.org/web/20150923202053/http://www.cfmaeroengines.com/files/brochures/LEAP-Brochure-2013.pdf |archive-date= September 23, 2015}}</ref>
|-
! Thrust (× 2)
| colspan=4 | {{convert|26,786|-|29,317|lbf|kN|0|abbr=on}}<ref name=FAA-TCDS/>
|-
! Cruising speed
| colspan=4 | {{cvt|0.79|Mach|41000|knots km/h|0}}<ref>{{cite news |url= http://aviationweek.com/blog/737max-and-md-12 |title= 737MAX and the MD-12 |work= Aviation Week |date=2013-12-09 |df=mdy-all}}</ref>
|-
! Range (2-class)<ref name="tech_specs"/>
| 3,850 nmi / 7,130 km
| 3,550 nmi / 6,570 km <br />MAX 200: {{convert|2,700|nmi|km|0|abbr=on}}<ref name=FG_range_upd>[https://www.flightglobal.com/news/articles/boeing-revises-obsolete-performance-assumptions-415293/ "Boeing Revises "Obsolete" Performance Assumptions (2015)"] Flight Global.com.</ref>
| 3,550 nmi / 6,570 km{{efn|With one auxiliary tank<ref name="tech_specs"/>}}
| 3,300 nmi / 6,110 km{{efn| With one auxiliary tank<ref name="tech_specs"/>}}
|-
! Ceiling
| colspan=4 | {{cvt|41000|feet|m}}<ref name=FAA-TCDS/>
|-
! ICAO Type<ref>{{cite web |title= DOC 8643 – Aircraft Type Designators |url= http://www.icao.int/publications/DOC8643/Pages/default.aspx |publisher= ICAO}}</ref>
|B37M
|B38M
|B39M
|B3JM
|}
 
{| style="text-align: center; font-size:95%;" class="wikitable"
|-
!Model
!747-400<ref name=400pax>{{cite web |title= 747-400/-400ER |publisher= Boeing |work= Startup |date= May 2010 |url= http://www.boeing.com/resources/boeingdotcom/company/about_bca/startup/pdf/historical/747-400-passenger.pdf}}</ref>
!747-400ER<ref name=400pax/>
!747-400F<ref name=400F/>
!747-400ERF<ref name=400F>{{cite web |title= 747-400/-400ER Freighters |publisher= Boeing |work= Startup |date= May 2010 |url= http://www.boeing.com/resources/boeingdotcom/company/about_bca/startup/pdf/freighters/747-400f.pdf}}</ref>
|-
|-
| Cockpit crew  
| Cockpit crew  
| colspan="4" | 2
| colspan="4"| 2
|-
|-
| Capacity
| Capacity
| colspan="2" | 416 (23F @ 61" + 80J @ 39" + 313Y @ 32")
| colspan="2"| 416 (23F @ 61" + 80J @ 39" + 313Y @ 32")
| 274,100&nbsp;lb / 124,330&nbsp;kg
| 274,100&nbsp;lb / 124,330&nbsp;kg
| 273,400&nbsp;lb / 124,010&nbsp;kg
| 273,400&nbsp;lb / 124,010&nbsp;kg
第128行： 第373行：
| [[Unit Load Device]]s
| [[Unit Load Device]]s
| 30 LD1/LD3 || 28 LD1/LD3
| 30 LD1/LD3 || 28 LD1/LD3
| colspan="2" | + 2 LD1 + 30 x 96 by 125-in pallet on Main deck
| colspan="2"| + 2 LD1 + 30 x 96 by 125-in pallet on Main deck
|-
|-
| Exit limit
| Exit limit<ref name="TypeCert">{{cite web |title= Type Certificate Data Sheet NO. A20WE |publisher= FAA |date= February 27, 2015 |url= http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/75d4c3215c58345386257df9007c3763/$FILE/A20WE_Rev_57.pdf}}</ref>
| colspan="2" | 550/660{{efn|550 main deck, 660 combined main and upper decks}}
| colspan="2" | 550/660{{efn|550 main deck, 660 combined main and upper decks}}
| colspan="2" |
| colspan="2" |
第141行： 第386行：
|-
|-
| Wing area
| Wing area
| colspan="4" | {{convert|525|m2|ft2|abbr=on|order=flip}}
| colspan="4" | {{convert|525|m2|ft2|abbr=on|order=flip}}<ref>{{cite web |url= http://konzern.lufthansa.com/en/themen/boeing-747-8-roll-out.html|archive-url= https://web.archive.org/web/20121230173833/http://konzern.lufthansa.com/en/themen/boeing-747-8-roll-out.html |dead-url= yes |archive-date= December 30, 2012  |publisher= Lufthansa |title= Premiere of Boeing 747-8 Intercontinental |date= February 13, 2011}}</ref>
|-
|-
|Aspect ratio
|Aspect ratio
第170行： 第415行：
| colspan="2" | {{convert|0.845|Mach|32,000|knots km/h|0}}
| colspan="2" | {{convert|0.845|Mach|32,000|knots km/h|0}}
|-
|-
| Airspeed limit<ref name="TypeCert" />
| Airspeed limit<ref name="TypeCert"/>
| colspan="4" |{{convert|0.92|Mach|32,000|knots km/h|0}}
| colspan=4 |{{convert|0.92|Mach|32,000|knots km/h|0}}
|-
|-
| Takeoff field length{{efn|SL, 86°F, MTOW}}
| Takeoff field length{{efn|SL, 86°F, MTOW}}
第196行： 第441行：
| {{convert|56,400|-|63,300|lbf|kN|abbr=on}}
| {{convert|56,400|-|63,300|lbf|kN|abbr=on}}
| {{convert|62,100|-|63,300|lbf|kN|abbr=on}}
| {{convert|62,100|-|63,300|lbf|kN|abbr=on}}
|}
{| class="wikitable" style="text-align:center;"
|+ 747-8 characteristics<ref name="747-8_specs">{{cite web |url= http://www.boeing.com/commercial/747/#/design-highlights/characteristics/ |title= 747-8 characteristics |publisher= Boeing}}</ref>
! Variant
! 747-8
! 747-8F
|-
! Cockpit crew
| colspan=2| Two
|-
! Capacity
| 410 in 3-class
| 303,700&nbsp;lb / 137,700&nbsp;kg
|-
! Exit limit<ref name=TCDS>{{cite web |url= http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/b3bb8eb44b6d73748625804400536f22/$FILE/A20WE_Rev58.pdf |title= Type Certificate data sheet No. A20WE |date= October 5, 2016 |publisher= FAA}}</ref>
| 605
| 8
|-
! Overall length
| colspan=2| 250&nbsp;ft 2 in / 76.3 m
|-
! Height
| colspan=2| 63&nbsp;ft 6 in / 19.4 m
|-
! Wingspan
| colspan=2| 224&nbsp;ft 7 in / 68.4 m
|-
! Wing area
| colspan=2| {{convert|554|m2|sqft|abbr=on}}<ref name="flight-tech-desc">{{cite news |url= https://www.flightglobal.com/news/articles/in-focus-boeing-747-8-technical-description-amp-cutaway-378866/ |title= Boeing 747-8 technical description & cutaway |date= 13 November 2012 |work= Flight Global}}</ref>
|-
! [[Swept wing|Wing sweep]]
| colspan=2| 37.5°<ref name="flight-tech-desc"/>
|-
! [[Aspect ratio (wing)|Aspect ratio]]
| colspan=2| {{#expr:68.4/(554/68.4)round2}}
|-
! Cabin width
| colspan=2| {{convert|{{#expr:2*(1.03+.51+1.51)}}|m|ft|order=flip|abbr=on}}<ref name="747-8_airport"/>{{rp|17}}
|-
! [[Maximum takeoff weight]]<ref name="747-8_airport"/>{{rp|7–8}}
| colspan=2| 987,000&nbsp;lb / 447,700&nbsp;kg
|-
! [[Maximum landing weight]]<ref name="747-8_airport"/>{{rp|7–8}}
| 688,000&nbsp;lb / 312,072&nbsp;kg
| 763,000&nbsp;lb / 346,091&nbsp;kg
|-
! Maximum [[zero-fuel weight]]<ref name="747-8_airport"/>{{rp|7–8}}
| 651,000&nbsp;lb / 295,289&nbsp;kg
| 727,000&nbsp;lb / 329,762&nbsp;kg
|-
! Operating Empty weight<ref name="747-8_airport">{{cite web |url= http://www.boeing.com/assets/pdf/commercial/airports/acaps/747_8.pdf |title= 747-8 Airplane Characteristics for Airport Planning |publisher= Boeing |date= December 2012}}</ref>{{rp|7–8}}
| 485,300&nbsp;lb / 220,128&nbsp;kg
| 434,600&nbsp;lb / 197,131&nbsp;kg
|-
! Maximum structural payload<ref name="747-8_airport"/>{{rp|7–8}}
| 167,700&nbsp;lb / 76,067&nbsp;kg
| 292,400&nbsp;lb / 132,630&nbsp;kg
|-
! Fuel capacity<ref name="747-8_airport"/>{{rp|7–8}}
| 63,034USgal / 238,610L<br/>426,109&nbsp;lb / 193,280&nbsp;kg
| 59,734USgal / 226,118L<br/>400,218&nbsp;lb / 181,536&nbsp;kg
|-
! Cruise speed
| {{convert|0.86|Mach|43100|knots km/h|0}}
| {{convert|0.85|Mach|43100|knots km/h|0}}
|-
! [[V speeds|Mach Maximum Operating]]
| colspan=2 |{{convert|0.9|Mach|43100|knots km/h|0}}<ref name=TCDS/>
|-
! Range
| {{convert|8000|nmi|km|abbr=on}}<ref name="flight-rev-perf">{{cite news |url= http://www.boeing.com/commercial/747/#/technical-specs|date= May 6, 2018|work= Flight Global}}</ref><br>BBJ: {{convert|8875|nmi|km|abbr=on}}<ref>{{cite web|url=http://www.boeing.com/commercial/bbj/#/aircraft/bbj-747/characteristics/747-8/|title=Boeing: Boeing Business Jets|website=www.boeing.com}}</ref>
| 4,120nmi / 7,630&nbsp;km<ref name=backgrounder>{{cite web |url= http://www.boeing.com/resources/boeingdotcom/media/dubai2015/pdf/Backgrounders/747-8_Family_Backgrounder_English.pdf |title= 747-8 Family Backgrounder |date= September 2015 |publisher= Boeing}}</ref>
|-
! Cargo Volume
| {{convert|6,225|cuft|m3|sigfig=3|abbr=on}}
| {{convert|30,288|cuft|m3|sigfig=3|abbr=on}}
|-
! Ceiling
| colspan=2| {{convert|43100|ft|m|abbr=on}}<ref name=TCDS/>
|-
! Engines (4×)
| colspan=2| [[General Electric GEnx|GEnx-2B67]]
|-
! Thrust (4×)
| colspan=2| {{convert|66500|lbf|kN|sigfig=3|abbr=on}}
|}
{| class="wikitable" style="text-align:center; color:black;"
|-
! Variant
! 757-200<ref name=757tech>{{cite web |url= http://www.boeing.com/resources/boeingdotcom/company/about_bca/startup/pdf/historical/757_passenger.pdf |title= 757 Passenger |publisher= Boeing |date= 2007}}</ref>
! 757-200F<ref name=757pftech>{{cite web |url= http://www.boeing.com/resources/boeingdotcom/company/about_bca/startup/pdf/freighters/757f.pdf |title= 757 Freighter |publisher= Boeing |date= 2007}}</ref>
! 757-300<ref name=757tech/>
|-
! Cockpit crew
| colspan=3 | Two
|-
! 2-class seating
| 200 (12F+188Y)
|
| 243 (12F+231Y)
|-
! 1-class seating
| 221/228, 239 max<ref name=Type_cert>{{cite web |url= http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/e114c6bafec130a086257f5b007aeb12/$FILE/A2NM_Rev32.pdf |title= Type Certificate Data Sheet |publisher= FAA |date= February 16, 2016}}</ref>
| 5 max<ref name=Type_cert/>
| 280, 295 max<ref name=Type_cert/>
|-
! Cargo volume
| 1,670&nbsp;ft³ / 43.3 m³
| 6,600&nbsp;ft³ / 187 m³
| 2,370&nbsp;ft³ / 61.7 m³
|-
! Width
| colspan=3 | 148 in / 3.76 m fuselage, 139.3 in / 3.54 m cabin<ref name=757plan>{{cite web |url= http://www.boeing.com/assets/pdf/commercial/airports/acaps/757_23.pdf |title= 757 Airplane Characteristics for Airport Planning |publisher= Boeing |date= August 2002 |page= 21}}</ref>
|-
! Length
| colspan=2 | 155&nbsp;ft 3 in / 47.3 m
| 178&nbsp;ft 7 in / 54.4 m
|-
! Height
| colspan=3 | 44&nbsp;ft 6 in / 13.6 m
|-
! Wing
| colspan=3 | 124&nbsp;ft 10 in / 38.0 m span, {{cvt|185.25|m2|sqft|order=flip|0}} area,<ref>{{cite book |url= http://booksite.elsevier.com/9780340741528/appendices/data-a/table-3/table.htm |title= Civil Jet Aircraft Design |at= Aircraft Data File |publisher= Elsevier |date= January 1999}}</ref> 25° sweep,<ref>{{cite book |url= https://books.google.com/?id=XMMe4DIgshkC&lpg=PA71&dq=757%20wing%20sweep&pg=PA71#v=onepage&q=757%20wing%20sweep&f=false |title= Boeing Jetliners |publisher= Barnes & Noble |date= 1998 |isbn= 9781610607063 }}</ref> {{#expr:38/(185.25/38)round1}} [[wing aspect ratio|AR]]
|-
! [[Maximum takeoff weight|MTOW]]
| colspan=2 | 255,000&nbsp;lb / 115,660&nbsp;kg
| 273,000&nbsp;lb / 123,830&nbsp;kg
|-
! Max. [[Payload]]<!--MZFW - OEW-->
| {{formatnum:{{#expr:186000-128840}}}}&nbsp;lb / {{formatnum:{{#expr:84360-58440}}}}&nbsp;kg
| {{formatnum:{{#expr:200000-115580}}}}&nbsp;lb / {{formatnum:{{#expr:90720-52430}}}}&nbsp;kg
| {{formatnum:{{#expr:210000-141860}}}}&nbsp;lb / {{formatnum:{{#expr:95250-64340}}}}&nbsp;kg
|-
! [[Operating empty weight|OEW]]
| 128,840&nbsp;lb / 58,440&nbsp;kg
| 115,580&nbsp;lb / 52,430&nbsp;kg
| 141,860&nbsp;lb / 64,340&nbsp;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
| colspan=3 | Cruise {{cvt|0.8|Mach|35,000|knots km/h|0}}, Max. {{cvt|0.86|Mach|35,000|knots km/h|0}}<ref name=Type_cert/>
|-
! [[Range (aircraft)|Range]]
| 3,915nmi / 7,250&nbsp;km{{efn|200 passengers}}
| 2,935nmi / 5,435&nbsp;km{{efn|72,210 lb / 32,755 kg payload}}
| 3,400nmi / 6,295&nbsp;km{{efn|243 passengers}}
|-
! Takeoff{{efn|MTOW, sea level, {{convert|86|°F|°C}}, RB211-535E4B engines}}
| 6,800&nbsp;ft / 2,070 m
| 6,900&nbsp;ft / 2,103 m
| 8,550&nbsp;ft / 2,605 m
|-
! Ceiling
| colspan="3"| {{convert|42,000|ft|m|abbr=on}}<ref name=Type_cert/>
|-
! Engines (×2)
| colspan="3"|{{convert|40,200|-|43,500|lbf|kN|abbr=on}} [[Rolls-Royce RB211]]-535E4(B)<br/>{{convert|36,600|-|42,600|lbf|kN|abbr=on}} [[Pratt & Whitney PW2000]]-37/40/43
|}
{|class=wikitable style="text-align: center; width: 90%"
|+ 767 Airplane Characteristics<ref name=767_airport_report>{{cite web|url=http://www.boeing.com/assets/pdf/commercial/airports/acaps/767.pdf|title=767 Airplane Characteristics for Airport Planning|publisher=Boeing|date=May 2011|pages=4–6, 9–14, 23, 28, 32, 35, 37|accessdate=October 20, 2013}}</ref>
|-
! style="width: 10%;" | Variant
! style="width: 15%;" | 767-200
! style="width: 15%;" | 767-200ER
! style="width: 15%;" | 767-300
! style="width: 15%;" | 767-300ER
! style="width: 15%;" | 767-300F
! style="width: 15%;" | 767-400ER
|-
!Cockpit crew
| colspan="6" | Two
|-
! 3-class<ref name=767_airport_report/>{{rp|pages=23–29}}
| colspan="2" | 174 (15F, 40J, 119Y)
| colspan="2" | 210 (18F, 42J, 150Y)
| rowspan=5 | 15,469&nbsp;ft³ / 438m³<br/>58-ton / 52.7 tonnes<br/>24 88×108in pallets<ref name=backgrounder>{{cite web|url=http://www.boeing.com/farnborough2014/pdf/BCA/bck-767_5_13_2014.pdf|title=767 Backgrounder|publisher=Boeing Commercial Airplanes|date=February 2014}}</ref>
| 243 (16F, 36J, 189Y)
|-
! 2-class<ref name=767_airport_report/>{{rp|pages=23–29}}
| colspan="2" | 214 (18J, 196 Y)
| colspan="2" | 261 (24J, 237Y)
| 296 (24J, 272Y)
|-
! 1-class<ref name=767_airport_report/>{{rp|pages=23–29}}
| colspan="2" | 245Y
| colspan="2" | 290Y
| 409Y
|-
! Exit limit<ref name="rgl.faa.gov">{{cite web|url=http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/b9e61e631046f10186257fd900588ed4/$FILE/A1NM_Rev35.pdf|title=Type Certificate Data Sheet No. A1NM|date=June 20, 2016}}</ref>{{rp|page=10}}
| colspan="2" | 290
| colspan="2" | 351
| 375
|-
! Cargo<ref name=767_airport_report/>{{rp|pages=9–14}}
| colspan="2" | 3,070&nbsp;ft³ / 86.9m³
| colspan="2" | 4,030&nbsp;ft³ / 114.1m³
| 4,905&nbsp;ft³ / 138.9m³
|-
! [[Unit load device|ULD]]s<ref name=767_airport_report/>{{rp|pages=32–36}}
| colspan="2" | 22 LD2s
| colspan="3" | 30 LD2s
| 38 LD2s
|-
! Length<ref name=767_airport_report/>{{rp|pages=15–18}}
| colspan="2" | 159&nbsp;ft 2in / 48.51m
| colspan="3" | 180&nbsp;ft 3in / 54.94m
| 201&nbsp;ft 4in / 61.37m
|-
! Wingspan<ref name=767_airport_report/>{{rp|pages=15–18}}
| colspan="5" | 156&nbsp;ft 1in / 47.57m
| 170&nbsp;ft 4in / 51.92m
|-
! Wing
|colspan="5" | 3,050&nbsp;ft² / 283.3m², 31.5° sweepback<ref name=civilJetAircraftDesign>{{cite web|url=http://booksite.elsevier.com/9780340741528/appendices/data-a/table-3/table.htm|title=Aircraft Data File: Boeing Aircraft|publisher=Elsevier|work=civil jet aircraft design|date=1999}}</ref>
| 3,130&nbsp;ft² / 290.7m²<ref>{{cite web |url= http://www.flugzeuginfo.net/acdata_php/acdata_7674_en.php |title= Boeing 767-400 |work= Flugzeuginfo |author= Karsten Palt}}</ref>
|-
! Fuselage
| colspan="6"| 17&nbsp;ft 9in / 5.41m height, 16&nbsp;ft 6in / 5.03m width,<ref name=767_airport_report/>{{rp|pages=15–18}} 186in/ 4.72m Cabin width<ref name=767_airport_report/>{{rp|pages=30}}
|-
! [[Maximum takeoff weight|MTOW]]<ref name=767_airport_report/>{{rp|pages=9–14}}
| 315,000&nbsp;lb / 142,882&nbsp;kg
| 395,000&nbsp;lb / 179,169&nbsp;kg
| 350,000&nbsp;lb / 158,758&nbsp;kg
| colspan=2 | 412,000&nbsp;lb / 186,880&nbsp;kg
| 450,000&nbsp;lb / 204,116&nbsp;kg
|-
! Max. [[payload]]<ref name=767_airport_report/>{{rp|pages=9–14}}<!--MZFW-OEW-->
| {{cvt|{{#expr:250000-176650}}|lb|kg|0}}
| {{cvt|{{#expr:260000-181610}}|lb|kg|0}}
| {{cvt|{{#expr:278000-189750}}|lb|kg|0}}
| {{cvt|{{#expr:295000-198440}}|lb|kg|0}}
| {{cvt|{{#expr:309000-190000}}|lb|kg|0}}
| {{cvt|{{#expr:330000-229000}}|lb|kg|0}}
|-
! [[Operating empty weight|OEW]]<ref name=767_airport_report/>{{rp|pages=9–14}}
| 176,650&nbsp;lb / 80,127&nbsp;kg
| 181,610&nbsp;lb / 82,377&nbsp;kg
| 189,750&nbsp;lb / 86,069&nbsp;kg
| 198,440&nbsp;lb / 90,011&nbsp;kg
| 190,000&nbsp;lb / 86,183&nbsp;kg
| 229,000&nbsp;lb / 103,872&nbsp;kg
|-
! rowspan=2 | Fuel capacity<ref name=767_airport_report/>{{rp|pages=9–14}}
| 16,700USgal / 63,217L
| 24,140Usgal / 91,380L
| 16,700USgal / 63,216L
| colspan=3 | 24,140USgal / 91,380L
|-
| 111,890&nbsp;lb / 50,753&nbsp;kg
| 161,738&nbsp;lb / 73,363&nbsp;kg
| 111,890&nbsp;lb / 50,753&nbsp;kg
| colspan=3 | 161,740&nbsp;lb / 73,364&nbsp;kg
|-
! Range<ref name=767specs>{{cite web|url=http://www.boeing.com/assets/pdf/commercial/startup/pdf/767_perf.pdf|title=767 performance summary|publisher=Boeing|date=2006|deadurl=bot: unknown|archiveurl=https://web.archive.org/web/20150415224410/http://www.boeing.com/assets/pdf/commercial/startup/pdf/767_perf.pdf|archivedate=April 15, 2015}}</ref>
| {{convert|3,900|nmi|km|abbr=on}}{{efn|216 pax, 176,100lb / 79,878kg OEW, ISA}}<ref name=767_airport_report/>{{rp|page=47}}
| 6,590nmi / 12,200&nbsp;km{{efn|181 pax (15F/40J/126Y), CF6}}
| {{convert|3,900|nmi|km|abbr=on}}{{efn|269 pax, 187,900lb / 85235kg OEW, ISA}}<ref name=767_airport_report/>{{rp|page=49}}
| 5,980nmi / 11,070&nbsp;km{{efn|218 pax (18F/46J/154Y), PW4000}}
| 3,225nmi / 6,025&nbsp;km {{efn|58-ton / 52.7 tonnes payload}}<ref name=backgrounder/>
| 5,625nmi / 10,415&nbsp;km{{efn|245 pax (20F/50J/175Y), CF6}}
|-
! Cruise
| colspan="6" | Long range: {{cvt|459|kn|km/h}}, Maximum: {{cvt|486|kn|km/h}} at {{cvt|39,000|ft|m}},<ref name=civilJetAircraftDesign/> Ceiling: {{cvt|43,100|ft|m}}<ref name="rgl.faa.gov"/>{{rp|page=10}}
|-
! Takeoff{{efn|MTOW, SL, 30°C/86°F}}<ref name=767specs/>
| {{convert|6,300|ft|m|abbr=on}}<ref name=767_airport_report/>{{rp|page=58}}
| 2,480m / 8,150&nbsp;ft
| {{convert|9,200|ft|m|abbr=on}}<ref name=767_airport_report/>{{rp|page=64}}
| colspan=2 | 2,650m / 8,700&nbsp;ft
| 3,290m / 10,800&nbsp;ft
|-
! Engines (×2)<ref name=767_airport_report/>{{rp|page=10}}
| [[Pratt & Whitney JT9D|P&W JT9D]]-7R4/7R4E / [[Pratt & Whitney PW4000|P&W PW4052]] / [[GE CF6]]-80A/A2/C2-B2
| [[Pratt & Whitney JT9D|P&W JT9D]]-7R4/7R4E / [[Pratt & Whitney PW4000|P&W PW4052]]/56 / [[GE CF6]]-80A/A2/C2-B2/C2-B4 / [[RB211]]-524G/H
| [[Pratt & Whitney JT9D|P&W JT9D]]-7R4/7R4E / [[Pratt & Whitney PW4000|P&W PW4052]] / [[GE CF6]]-80A/A2/C2-B2 / [[RB211]]-524H
| colspan=2 | [[GE CF6]]-80C2-B4/0C2-B6/C2-B8F/C2-B7F1 / [[Pratt & Whitney PW4000|PW4056]]/60/62 / [[RB211]]-524G/H
| [[GE CF6]]-80C2-B8F/C2-B7F1 / [[Pratt & Whitney PW4000|PW4062]]
|-
! Thrust (×2)<ref name=767_airport_report/>{{rp|page=10}}
| {{cvt|48,000-52,500|lbf|kN|0}}
| {{cvt|48,000-60,600|lbf|kN|0}}
| {{cvt|48,000-60,600|lbf|kN|0}}
| colspan=2 | {{cvt|56,750-61,500|lbf|kN|0}}
| {{cvt|60,600|lbf|kN|0}}
|}
{| class="wikitable" style="text-align:center; font-size:96%;"
|+ Boeing 777 specifications
|-
! Model
! 777-200<ref name=Boeing_777_airport_report_gen1>{{Cite techreport |url= http://www.boeing.com/assets/pdf/commercial/airports/acaps/777_23.pdf |title=777-200/300 Airplane Characteristics for Airport Planning |publisher=Boeing |date= December 2008 }}</ref>
! 777-200ER<ref name=Boeing_777_airport_report_gen1/>
! 777-200LR<ref name=Boeing_777_airport_report_gen2>{{cite techreport |url= http://www.boeing.com/assets/pdf/commercial/airports/acaps/777_2lr3er.pdf |title= 777-200LR/-300ER/-Freighter Airplane Characteristics for Airport Planning |publisher=Boeing |date= May 2015 }}</ref>
! 777F<ref name=Boeing_777_airport_report_gen2/>
! 777-300<ref name=Boeing_777_airport_report_gen1/>
! 777-300ER<ref name=Boeing_777_airport_report_gen2/>
|-
! Cockpit crew
| colspan="6" | Two
|-
! 3-class<ref name=777_perf>{{cite web|url=http://www.boeing.com/assets/pdf/commercial/startup/pdf/777_perf.pdf |title=777 performance summary |publisher=Boeing |date=2009 |deadurl=bot: unknown |archiveurl=https://web.archive.org/web/20140802021208/http://www.boeing.com/assets/pdf/commercial/startup/pdf/777_perf.pdf |archivedate=August 2, 2014 |df=mdy }}</ref>
| 305 (24F/54J/227Y)
| colspan=2 | 301 (16F/58J/227Y)
|
| 368 (30F/84J/254Y)
| 365 (22F/70J/273Y)
|-
! 2-class/capacity<ref name=Characteristics>{{cite web |url= http://www.boeing.com/commercial/777/#/design-highlights/characteristics |title=777 Characteristics |publisher= Boeing }}</ref>
| colspan=2 | 313
| 317
| 224,900&nbsp;lb / 102,010&nbsp;kg
| colspan=2 | 396
|-
! Exit limit<ref name=TypeCert>{{cite web |url= http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/8bff0e63469dd8eb862580190055ffa6/$FILE/T00001SE_Rev40.pdf |title=  Type Certificate data sheet No. T00001SE |date= August 12, 2016 |publisher= FAA}}</ref>
| colspan="3" | 440
| 11
| colspan="2" | 550
|-
! Length
| colspan="4" | 209&nbsp;ft 1 in / 63.73 m
| colspan="2" | 242&nbsp;ft 4 in / 73.86 m
|-
! Wingspan
| colspan="2" | 199&nbsp;ft 11 in / 60.93 m
| colspan="2" | 212&nbsp;ft 7 in / 64.80 m
| 199&nbsp;ft 11 in / 60.93 m
| 212&nbsp;ft 7 in / 64.80 m
|-
! [[Wing sweep]]
| colspan="6" | 31.6°<ref name=elsevier>{{cite web |url= http://booksite.elsevier.com/9780340741528/appendices/data-a/table-4/table.htm |title= Boeing Aircraft Data File |publisher= Elsevier |work= Civil Jet Aircraft Design |date= July 1999}}</ref>
|-
! Wing area
| colspan="2" | {{convert|427.8|m2|sqft|abbr=on|order=flip}}<ref name=elsevier/>
| colspan="2" | {{convert|436.8|m2|sqft|abbr=on|order=flip}}<ref name=AA120726>{{cite web |url= http://www.aspireaviation.com/2012/07/26/boeing-chooses-largest-wingspan-for-777x/ |date= 26 Jul 2012 |title= Boeing chooses largest wingspan for 777X |author= Daniel Tsang |work= Aspire Aviation}}</ref>
| {{convert|427.8|m2|sqft|abbr=on|order=flip}}<ref name=elsevier/>
| {{convert|436.8|m2|sqft|abbr=on|order=flip}}<ref name=AA120726/>
|-
! Aspect ratio
| colspan=2 | {{#expr:60.93/(427.8/60.93)round2}}
| colspan=2 | {{#expr:60.93/(436.8/64.80)round2}}
| {{#expr:60.93/(427.8/60.93)round2}}
| {{#expr:60.93/(436.8/64.80)round2}}
|-
! Tail height<ref name=Characteristics/>
| colspan="2" | 60&nbsp;ft 9 in / 18.5 m
| colspan="2" | 61&nbsp;ft 1 in / 18.6 m
| colspan="2" | 60&nbsp;ft 8 in / 18.5 m
|-
! Cabin width<ref>{{cite web |url= http://www.boeing.com/farnborough2014/pdf/BCA/bck-777%20Family%20Backgrounder.pdf |title= Backgrounder: The Boeing 777 Family |date= May 2014 |publisher= Boeing Commercial Airplanes}}</ref>
| colspan="6" | 231 in / 5.86 m
|-
! Seat width
| colspan="6" | 18.5 in / 47&nbsp;cm at 9 abreast, 17 in / 43&nbsp;cm at 10 abreast
|-
! Fuselage width
| colspan="6" | 20&nbsp;ft 4 in / 6.20 m
|-
! Maximum cargo capacity<ref name=Characteristics/>
| colspan="3" | 5,330&nbsp;ft³ / 150.9 m³
| 23,051&nbsp;ft³ / 652.7 m³
| colspan="2" | 7,120&nbsp;ft³ / 201.6 m³
|-
! [[Maximum takeoff weight]] (MTOW)
| 545,000&nbsp;lb / 247,200&nbsp;kg
| 656,000&nbsp;lb / 297,550&nbsp;kg
| 766,000&nbsp;lb / 347,452&nbsp;kg
| 766,800&nbsp;lb / 347,815&nbsp;kg
| 660,000&nbsp;lb / 299,370&nbsp;kg
| 775,000&nbsp;lb / 351,533&nbsp;kg
|-
! Max. landing weight
| 445,000&nbsp;lb / 201,840&nbsp;kg
| 470,000&nbsp;lb / 213,180&nbsp;kg
| 492,000&nbsp;lb / 223,168&nbsp;kg
| 575,000&nbsp;lb / 260,816&nbsp;kg
| 524,000&nbsp;lb / 237,680&nbsp;kg
| 554,000&nbsp;lb / 251,290&nbsp;kg
|-
! [[Operating empty weight]]
| 299,550&nbsp;lb / 135,850&nbsp;kg
| 304,500&nbsp;lb / 138,100&nbsp;kg
| 320,000&nbsp;lb / 145,150&nbsp;kg
| 318,300&nbsp;lb / 144,379&nbsp;kg
| 353,800&nbsp;lb / 160,530&nbsp;kg
| 370,000&nbsp;lb / 167,829&nbsp;kg
|-
! Fuel capacity
| 31,000 US gal / 117,340 L / 207,700&nbsp;lb / 94,240&nbsp;kg
| 45,220 US gal / 171,171 L / 302,270&nbsp;lb / 137,460&nbsp;kg
| colspan="2" | 47,890 US gal / 181,283 L / 320,863&nbsp;lb / 145,538&nbsp;kg
| 45,220 US gal / 171,171 L / 302,270&nbsp;lb / 137,460&nbsp;kg
| 47,890 US gal / 181,283 L / 320,863&nbsp;lb / 145,538&nbsp;kg
|-
! [[Service ceiling]]<ref name=TypeCert/>
| colspan="6" | {{convert|43,100|ft|m|abbr=on}}
|-
! scope="row" | Cruise speed
| colspan="6" | {{convert|0.84|Mach|43100|0}}
|-
! Max. speed
| colspan="6" | {{convert|0.89|Mach|43100|0}}<ref>{{cite news |url= https://www.flightglobal.com/news/articles/flight-test-boeing-777-300er-fast-and-heavy-176585/ |title= Flight Test: Boeing 777-300ER - Fast and heavy |work= Flight Global |date= 20 January 2004}}</ref>
|-
! Range<ref name=Characteristics/>
| 5,240 nmi / 9,700&nbsp;km{{efn|305 passengers, Trents}}<ref name=777_perf/>
| 7,065 nmi / 13,080&nbsp;km{{efn|313 passengers}}
| 8,555 nmi / 15,843&nbsp;km{{efn|317 passengers}}
| 4,970 nmi / 9,200&nbsp;km{{efn|102,010 kg / 224,900 lb}}
| 6,030 nmi / 11,165&nbsp;km{{efn|368 passengers, GE90}}<ref name=777_perf/>
| 7,370 nmi / 13,649&nbsp;km{{efn|396 passengers}}
|-
! Takeoff distance{{efn|MTOW, sea level, [[International standard atmosphere|ISA]]}}
| {{convert|8000|ft|m|abbr=on|sigfig=3|disp=br}}
| {{convert|11100|ft|m|abbr=on|sigfig=3|disp=br}}
| {{convert|9200|ft|m|abbr=on|sigfig=3|disp=br}}
| {{convert|9300|ft|m|abbr=on|sigfig=3|disp=br}}
| {{convert|10600|ft|m|abbr=on|sigfig=3|disp=br}}
| {{convert|10000|ft|m|abbr=on|sigfig=3|disp=br}}
|-
! scope="row" | Turbofan (×2)
| [[Pratt & Whitney PW4000|PW 4077]] <br/>[[Rolls-Royce Trent 800|RR 877]] <br/>[[General Electric GE90|GE90-77B]]
| PW 4090 <br/>RR 895<br/>GE90-94B
| colspan="2" | GE90-110B1 <br/>GE90-115B
| PW 4098 <br/>RR 892 <br/>GE90-92B/-94B
| GE90-115B
|-
! Max thrust (×2)
| {{convert|77,200|lbf|kN|abbr=on}}
| {{convert|93,700|lbf|kN|abbr=on}}
| colspan="2" | {{convert|115,300|lbf|kN|abbr=on}}
| {{convert|98,000|lbf|kN|abbr=on}}
| {{convert|115,300|lbf|kN|abbr=on}}
|}
{| class="wikitable" style="text-align:center;"
|+787 characteristics<ref name=787_Airport_report>{{cite web |url= http://www.boeing.com/assets/pdf/commercial/airports/acaps/787.pdf |title= 787 Airplane Characteristics for Airport Planning |publisher= Boeing Commercial Aircraft |date= March 2018}}</ref>
!Model
! 787-8
! 787-9
! 787-10
|-
!Cockpit crew
|colspan=3 |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
| {{convert|186|ft|1|in|m|abbr=on|2}}
| {{convert|206|ft|1|in|m|abbr=on|2}}
| {{convert|224|ft|m|abbr=on|2}}
|-
! Wing<ref name=EASAtcds/>
| colspan="3" | {{convert|197|ft|3|in|m|abbr=on|2}} span, 246.9 in / 6.27 m mean chord, {{#expr:197.25/(246.9/12)round2}} aspect ratio, {{cvt|{{#expr:197.25*246.9/12round0}}|sqft|sqm|0}} area
|-
! [[swept wing|Wing sweep]]
| colspan="3" | 32.2°<ref>{{cite web |url= http://www.lissys.demon.co.uk/samp1/ |title= Boeing 787 -8 (Dreamliner) sample analysis |publisher= Lissys Ltd |date= 2006}}</ref>
|-
!Height<ref name=787_Airport_report/>
| {{convert|55|ft|6|in|m|abbr=on|2}}
| colspan=2 | {{convert|55|ft|10|in|m|abbr=on}}
|-
!Fuselage
| colspan=3| Cabin width: {{convert|5.49|m|ftin|abbr=on|sigfig=3|order=flip}}<ref name=FG070707>{{cite web |url= https://www.flightglobal.com/news/articles/everything-about-the-boeing-787-dreamliner-209212/ |title= Everything about the Boeing 787 Dreamliner |publisher= [[Flightglobal]] |date= July 7, 2007}}</ref> External width: {{convert|18|ft|11|in|abbr=on|2}}, height: {{convert|19|ft|6|in|abbr=on|2}}
|-
!Cargo capacity
| 4,826&nbsp;ft³ /136.7 m³ <br />{{#expr:16+12}} [[LD3]] or {{#expr:5+4}} (88×125) pallets
| 6,090&nbsp;ft³ / 172.5 m³ <br />{{#expr:20+16}} LD3 or {{#expr:6+5}} (96×125) pallets
| 6,722&nbsp;ft³ / 191.4 m³ <br />{{#expr:22+18}} LD3 or {{#expr:7+6}} (96×125) pallets
|-
![[Maximum takeoff weight|MTOW]]
| 502,500&nbsp;lb / 227,930&nbsp;kg
| colspan=2 |560,000&nbsp;lb / 254,011&nbsp;kg
|-
![[Maximum landing weight|MLW]]
| 380,000&nbsp;lb / 172,365&nbsp;kg
| 425,000&nbsp;lb / 192,777&nbsp;kg
| 445,000&nbsp;lb / 201,849&nbsp;kg
|-
!Maximum [[zero-fuel weight|ZFW]]
| 355,000&nbsp;lb / 161,025&nbsp;kg
| 400,000&nbsp;lb / 181,437&nbsp;kg
| 425,000&nbsp;lb / 192,777&nbsp;kg
|-
![[Operating empty weight|OEW]]
| 264,500&nbsp;lb / 119,950&nbsp;kg
| 284,000&nbsp;lb / 128,850&nbsp;kg
| 298,700 lb / 135,500 kg
|-
!Fuel capacity
| 33,340 US gal / 126,206 L<br />223,378&nbsp;lb / 101,323&nbsp;kg
| colspan=2 | 33,384 US gal / 126,372 L<br />223,673&nbsp;lb / 101,456&nbsp;kg
|-
! Speed
| colspan=3 | Max: {{cvt|0.90|Mach|40,000|knots km/h|0}};<ref name=EASAtcds>{{cite web |url= https://www.easa.europa.eu/system/files/dfu/TCDS%20EASA%20IM%20A%20115%20B787%20Iss%2019%20-%2016%20Nov%202017.pdf |title= Type certificate data sheet for Boeing 787 |date= 16 Nov 2017 |publisher= EASA}}</ref> Cruise: {{cvt|0.85|Mach|40,000|knots km/h|0}}
|-
! Range{{efn|Typical seating}}<ref name=characteristics>{{cite web |url= http://www.boeing.com/commercial/787/by-design/#/all-model-performance-summary |title= 787 performance summary |publisher= Boeing}}</ref>
| {{cvt|7355|nmi|km|-1}}
| {{cvt|7635|nmi|km|-1}}
| {{cvt|6430|nmi|km|-1}}
|-
!Takeoff{{efn|[[Maximum Takeoff Weight|MTOW]] ([[International Standard Atmosphere|ISA]], SL, hi thrust)}}
| {{convert|8500|ft|m|abbr=on}}
| {{convert|9300|ft|m|abbr=on}}
| {{convert|9100|ft|m|abbr=on}}
|-
!Ceiling
| colspan=3| {{convert|43000|ft|m|abbr=on|sigfig=3}}<ref name=FG070707/>
|-
!Engines (×2)
| colspan=3| [[General Electric GEnx|General Electric GEnx-1B]] ''or'' [[Rolls-Royce Trent 1000]]
|-
!Thrust (×2)
| {{convert|64000|lbf|kN|abbr=on|sigfig=2}} || {{convert|71000|lbf|kN|abbr=on|sigfig=2}} || {{convert|76000|lbf|kN|abbr=on|sigfig=2}}
|}
|}

2018年7月7日 (六) 14:59的版本

Boeing 737 性能规格参数
Boeing 737 Next Generation Boeing 737 MAX
机型 737-700 737-800 737-900ER 737 MAX 7 737 MAX 8 / MAX 200 737 MAX 9 737 MAX 10
长度 33.63 m 39.47 m 42.11 m 35.56 m 39.52 m 42.16 m 43.8 m
高度 12.57 m 12.55 m 12.3 m
翼展 34.32 m（无翼梢小翼）；35.79m（有翼梢小翼） 35.92 m
OEW 7,648 kg 41,413 kg 44,677 kg - 45,070 kg -
MTOW 70,080 kg 79,016 kg 85,139 kg 80,286 kg 82,191 kg 88,314 kg -
最大燃料容量 26,022 L 29,666 L 25,817 L
实用升限 12500 m（41000 ft）
典型巡航马赫数 Mach 0.785
航程 3,010 nmi 5,436 km) 5,460 km 7,130 km 6,570 km

MAX 200: 5,000 km

6,570 km 6,110 km
消防保障等级 6级 7级
ICAO代码 B737 B738 B739 B37M M38M B39M B3JM
Model 747-400 747-400ER 747-400F 747-400
Overall length 70.66 m
Overall height 63 ft 8 in (19.4 m)
Wingspan 211 ft 5 in (64.44 m)
Operating empty weight PW: 404,600 lb / 183,520 kg PW: 412,300 lb / 187,010 kg GE: 360,900 lb / 163,700 kg GE: 361,600 lb / 164,020 kg
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
Fuel capacity 57,285 US gal (216,840 L) 63,705 US gal (241,140 L) 53,985 US gal / 204,350L
Cruise 模板:Convert 模板:Convert
Airspeed limit[1] 模板:Convert
Takeoff field length模板:Efn 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模板:Efn 7,585nmi / 14,045 km模板:Efn 2,825nmi / 5,230 km 4,045nmi / 7,585 km
Boeing 737 Characteristics[2]
Variant 737-600 737-700 737-800 737-900ER
Cockpit crew Two
2-class模板:Rp 108 (8F@36" 100Y@32") 128 (8F@36" 120Y@32") 160 (12F@36" 148Y@32") 177 (12F@36" 165Y@32")
1-class模板:Rp 123 @32" - 130 @ 30" 140 @32" - 148 @ 30" 175 @32" - 184 @ 30" 177 @32" - 215 @ 28"
Exit Limit[3] 149 189 220
Seat width模板:Rp First : 22in / 56 cm; Economy : 17in / 43 cm
Length模板:Rp 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模板:Rp 41 ft 3 in / 12.57 m 41 ft 2 in  (12.55 m)
Wing[4] Span: 112 ft 7 in / 34.32 m, with winglets: 117 ft 5in / 35.79m;模板:Rp Area: 模板:Cvt; Sweepback: 25°; 模板:Abbr: 9.44
Fuselage模板:Rp 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)
OEW模板:Rp 80,200 lb / 36,378 kg 83,000 lb / 37,648 kg 91,300 lb / 41,413 kg 98,495 lb / 44,677 kg
MLW模板:Rp 121,500 lb / 55,111 kg 129,200 lb / 58,604 kg 146,300 lb / 66,361 kg 157,300 lb / 71,350 kg
MTOW模板:Rp 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模板:Rp 6,875 US gal / 26,022 L 7,837 US gal / 29,666 L模板:Efn
Lower deck cargo模板:Rp 720 ft³ / 20.4 m³ 966 ft³ / 27.4 m³ 1,555 ft³ / 44.1 m³ 1,826 ft³ / 51.7 m³
Takeoff run模板:Efn[4] 模板:Convert 模板:Convert 模板:Convert 模板:Convert模板:Rp
Flight envelope[3] 模板:Convert Ceiling, 模板:Cvt MMo
Cruise[5] 模板:Convert 模板:Convert 模板:Convert 模板:Convert
Range[6] 模板:Convert模板:Efn[5] 模板:Convert模板:Efn 模板:Convert模板:Efn 模板:Convert模板:Efn
Engines (× 2) CFM56-7B18/20/22模板:Rp CFM56-7B20/22/24/26/27模板:Rp CFM56-7B24/26/27模板:Rp
Thrust (× 2) 模板:Cvt 模板:Rp 模板:Cvt模板:Rp 模板:Cvt模板:Rp 模板:Cvt模板:Rp
Cruise max. thrust模板:Efn[7] 模板:Cvt (climb)
Engine dimensions[7] Fan tip diameter: 模板:Cvt, length: 模板:Cvt
Engine ground clearance 18 in / 46 cm模板:Rp 19 in / 48 cm模板:Rp
ICAO Type[8] B736 B737 B738 B739
737 MAX Brochure[9][10]
Variant 737 MAX 7 737 MAX 8 / MAX 200 737 MAX 9 737 MAX 10
Seating 138 (8模板:Abbr + 130模板:Abbr) to 172 max 162 (12模板:Abbr + 150模板:Abbr) to 210 max 178 (16模板:Abbr + 162模板:Abbr) to 220 max 188 to 230 max
Seat pitch 模板:Cvt in high density, 模板:Cvt in economy, 模板:Cvt 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 模板:Cvt [11]
Overall height[12] 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[13] 99,360 lb / 45,070 kg
Fuel capacity 6,820 USgal / 25,817 L, excluding 模板:Abbr
Engine (× 2) CFM International LEAP-1B, 模板:Cvt Fan diameter[14]
Thrust (× 2) 模板:Convert[11]
Cruising speed 模板:Cvt[15]
Range (2-class)[10] 3,850 nmi / 7,130 km 3,550 nmi / 6,570 km
MAX 200: 模板:Convert[16] 		3,550 nmi / 6,570 km模板:Efn 3,300 nmi / 6,110 km模板:Efn
Ceiling 模板:Cvt[11]
ICAO Type[17] B37M B38M B39M B3JM
Model 747-400[18] 747-400ER[18] 747-400F[19] 747-400ERF[19]
Cockpit crew 2
Capacity 416 (23F @ 61" + 80J @ 39" + 313Y @ 32") 274,100 lb / 124,330 kg 273,400 lb / 124,010 kg
Unit Load Devices 30 LD1/LD3 28 LD1/LD3 + 2 LD1 + 30 x 96 by 125-in pallet on Main deck
Exit limit[1] 550/660模板:Efn
Overall length 231 ft 10 in (70.66 m)
Wingspan 211 ft 5 in (64.44 m)
Wing area 模板:Convert[20]
Aspect ratio 7.91
Overall height 63 ft 8 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
Operating empty weight PW: 404,600 lb / 183,520 kg PW: 412,300 lb / 187,010 kg GE: 360,900 lb / 163,700 kg GE: 361,600 lb / 164,020 kg
Fuel capacity 57,285 US gal (216,840 L) 63,705 US gal (241,140 L) 53,985 US gal / 204,350L
Cruise 模板:Convert 模板:Convert
Airspeed limit[1] 模板:Convert
Takeoff field length模板:Efn 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模板:Efn 7,585nmi / 14,045 km模板:Efn 2,825nmi / 5,230 km 4,045nmi / 7,585 km
Engines (x 4) PW4000 / GE CF6 / RR RB211 PW4000 / GE CF6 PW4000 / GE CF6 / RR RB211 PW4000 / GE CF6
Thrust (x 4) 模板:Convert 模板:Convert 模板:Convert 模板:Convert
747-8 characteristics[21]
Variant 747-8 747-8F
Cockpit crew Two
Capacity 410 in 3-class 303,700 lb / 137,700 kg
Exit limit[22] 605 8
Overall length 250 ft 2 in / 76.3 m
Height 63 ft 6 in / 19.4 m
Wingspan 224 ft 7 in / 68.4 m
Wing area 模板:Convert[23]
Wing sweep 37.5°[23]
Aspect ratio 8.45
Cabin width 模板:Convert[24]模板:Rp
Maximum takeoff weight[24]模板:Rp 987,000 lb / 447,700 kg
Maximum landing weight[24]模板:Rp 688,000 lb / 312,072 kg 763,000 lb / 346,091 kg
Maximum zero-fuel weight[24]模板:Rp 651,000 lb / 295,289 kg 727,000 lb / 329,762 kg
Operating Empty weight[24]模板:Rp 485,300 lb / 220,128 kg 434,600 lb / 197,131 kg
Maximum structural payload[24]模板:Rp 167,700 lb / 76,067 kg 292,400 lb / 132,630 kg
Fuel capacity[24]模板:Rp 63,034USgal / 238,610L
426,109 lb / 193,280 kg 		59,734USgal / 226,118L
400,218 lb / 181,536 kg
Cruise speed 模板:Convert 模板:Convert
Mach Maximum Operating 模板:Convert[22]
Range 模板:Convert[25]
BBJ: 模板:Convert[26] 		4,120nmi / 7,630 km[5]
Cargo Volume 模板:Convert 模板:Convert
Ceiling 模板:Convert[22]
Engines (4×) GEnx-2B67
Thrust (4×) 模板:Convert
Variant 757-200[27] 757-200F[28] 757-300[27]
Cockpit crew Two
2-class seating 200 (12F+188Y) 243 (12F+231Y)
1-class seating 221/228, 239 max[29] 5 max[29] 280, 295 max[29]
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[30]
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, 模板:Cvt area,[31] 25° sweep,[32] 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 模板:Cvt, Max. 模板:Cvt[29]
Range 3,915nmi / 7,250 km模板:Efn 2,935nmi / 5,435 km模板:Efn 3,400nmi / 6,295 km模板:Efn
Takeoff模板:Efn 6,800 ft / 2,070 m 6,900 ft / 2,103 m 8,550 ft / 2,605 m
Ceiling 模板:Convert[29]
Engines (×2) 模板:Convert Rolls-Royce RB211-535E4(B)
模板:Convert Pratt & Whitney PW2000-37/40/43
767 Airplane Characteristics[33]
Variant 767-200 767-200ER 767-300 767-300ER 767-300F 767-400ER
Cockpit crew Two
3-class[33]模板:Rp 174 (15F, 40J, 119Y) 210 (18F, 42J, 150Y) 15,469 ft³ / 438m³
58-ton / 52.7 tonnes
24 88×108in pallets[5] 		243 (16F, 36J, 189Y)
2-class[33]模板:Rp 214 (18J, 196 Y) 261 (24J, 237Y) 296 (24J, 272Y)
1-class[33]模板:Rp 245Y 290Y 409Y
Exit limit[34]模板:Rp 290 351 375
Cargo[33]模板:Rp 3,070 ft³ / 86.9m³ 4,030 ft³ / 114.1m³ 4,905 ft³ / 138.9m³
ULDs[33]模板:Rp 22 LD2s 30 LD2s 38 LD2s
Length[33]模板:Rp 159 ft 2in / 48.51m 180 ft 3in / 54.94m 201 ft 4in / 61.37m
Wingspan[33]模板:Rp 156 ft 1in / 47.57m 170 ft 4in / 51.92m
Wing 3,050 ft² / 283.3m², 31.5° sweepback[35] 3,130 ft² / 290.7m²[36]
Fuselage 17 ft 9in / 5.41m height, 16 ft 6in / 5.03m width,[33]模板:Rp 186in/ 4.72m Cabin width[33]模板:Rp
MTOW[33]模板:Rp 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[33]模板:Rp 模板:Cvt 模板:Cvt 模板:Cvt 模板:Cvt 模板:Cvt 模板:Cvt
OEW[33]模板:Rp 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[33]模板:Rp 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[37] 模板:Convert模板:Efn[33]模板:Rp 6,590nmi / 12,200 km模板:Efn 模板:Convert模板:Efn[33]模板:Rp 5,980nmi / 11,070 km模板:Efn 3,225nmi / 6,025 km 模板:Efn[5] 5,625nmi / 10,415 km模板:Efn
Cruise Long range: 模板:Cvt, Maximum: 模板:Cvt at 模板:Cvt,[35] Ceiling: 模板:Cvt[34]模板:Rp
Takeoff模板:Efn[37] 模板:Convert[33]模板:Rp 2,480m / 8,150 ft 模板:Convert[33]模板:Rp 2,650m / 8,700 ft 3,290m / 10,800 ft
Engines (×2)[33]模板:Rp 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)[33]模板:Rp 模板:Cvt 模板:Cvt 模板:Cvt 模板:Cvt 模板:Cvt
Boeing 777 specifications
Model 777-200[38] 777-200ER[38] 777-200LR[39] 777F[39] 777-300[38] 777-300ER[39]
Cockpit crew Two
3-class[40] 305 (24F/54J/227Y) 301 (16F/58J/227Y) 368 (30F/84J/254Y) 365 (22F/70J/273Y)
2-class/capacity[41] 313 317 224,900 lb / 102,010 kg 396
Exit limit[1] 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°[42]
Wing area 模板:Convert[42] 模板:Convert[43] 模板:Convert[42] 模板:Convert[43]
Aspect ratio 8.68 9.04 8.68 9.04
Tail height[41] 60 ft 9 in / 18.5 m 61 ft 1 in / 18.6 m 60 ft 8 in / 18.5 m
Cabin width[44] 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[41] 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[1] 模板:Convert
Cruise speed 模板:Convert
Max. speed 模板:Convert[45]
Range[41] 5,240 nmi / 9,700 km模板:Efn[40] 7,065 nmi / 13,080 km模板:Efn 8,555 nmi / 15,843 km模板:Efn 4,970 nmi / 9,200 km模板:Efn 6,030 nmi / 11,165 km模板:Efn[40] 7,370 nmi / 13,649 km模板:Efn
Takeoff distance模板:Efn 模板:Convert 模板:Convert 模板:Convert 模板:Convert 模板:Convert 模板:Convert
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) 模板:Convert 模板:Convert 模板:Convert 模板:Convert 模板:Convert
787 characteristics[46]
Model 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 模板:Convert 模板:Convert 模板:Convert
Wing[47] 模板:Convert span, 246.9 in / 6.27 m mean chord, 9.59 aspect ratio, 模板:Cvt area
Wing sweep 32.2°[48]
Height[46] 模板:Convert 模板:Convert
Fuselage Cabin width: 模板:Convert[49] External width: 模板:Convert, height: 模板:Convert
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: 模板:Cvt;[47] Cruise: 模板:Cvt
Range模板:Efn[12] 模板:Cvt 模板:Cvt 模板:Cvt
Takeoff模板:Efn 模板:Convert 模板:Convert 模板:Convert
Ceiling 模板:Convert[49]
Engines (×2) General Electric GEnx-1B or Rolls-Royce Trent 1000
Thrust (×2) 模板:Convert 模板:Convert 模板:Convert
  1. ↑ 1.0 1.1 1.2 1.3 1.4 模板:Cite web 引用错误：无效<ref>标签；name属性“TypeCert”使用不同内容定义了多次
  2. ↑ 模板:Cite web
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  5. ↑ 5.0 5.1 5.2 5.3 5.4 模板:Cite web 引用错误：无效<ref>标签；name属性“backgrounder”使用不同内容定义了多次 引用错误：无效<ref>标签；name属性“backgrounder”使用不同内容定义了多次
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  7. ↑ 7.0 7.1 模板:Cite news
  8. ↑ 模板:Cite web
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  11. ↑ 11.0 11.1 11.2 引用错误：无效<ref>标签；未给name属性为FAA-TCDS的引用提供文字
  12. ↑ 12.0 12.1 模板:Cite web 引用错误：无效<ref>标签；name属性“characteristics”使用不同内容定义了多次
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  16. ↑ "Boeing Revises "Obsolete" Performance Assumptions (2015)" Flight Global.com.
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  30. ↑ 模板:Cite web
  31. ↑ Civil Jet Aircraft Design. Elsevier. January 1999. Aircraft Data File. 
  32. ↑ Boeing Jetliners. Barnes & Noble. 1998. ISBN 9781610607063. 
  33. ↑ 33.00 33.01 33.02 33.03 33.04 33.05 33.06 33.07 33.08 33.09 33.10 33.11 33.12 33.13 33.14 33.15 33.16 33.17 33.18 33.19 模板:Cite web
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  35. ↑ 35.0 35.1 模板:Cite web
  36. ↑ 模板:Cite web
  37. ↑ 37.0 37.1 模板:Cite web
  38. ↑ 38.0 38.1 38.2 模板:Cite techreport
  39. ↑ 39.0 39.1 39.2 模板:Cite techreport
  40. ↑ 40.0 40.1 40.2 模板:Cite web
  41. ↑ 41.0 41.1 41.2 41.3 模板:Cite web
  42. ↑ 42.0 42.1 42.2 模板:Cite web
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  46. ↑ 46.0 46.1 模板:Cite web
  47. ↑ 47.0 47.1 模板:Cite web
  48. ↑ 模板:Cite web
  49. ↑ 49.0 49.1 模板:Cite web
取自“https://wiki.sinofsx.com/index.php?title=常见航空器规格和性能参数&oldid=2196”