常见航空器规格和性能参数：修订间差异

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第1行： 第1行：
{| class="wikitable" style="text-align: center"
{| class="wikitable" style="text-align: center"
|+Boeing 737 性能规格参数
|+
!
Boeing 737 Next Generation Characteristics<ref name="tech_specs">{{cite web|url=https://en.wikipedia.org/wiki/Boeing_737_Next_Generation|title=Boeing 737 Next Generation|at=Technical Specs|publisher=Wikipidia}}</ref>
! colspan="3" |Boeing 737 Next Generation
! colspan="4" |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&nbsp;m
| 39.47&nbsp;m
| 42.11&nbsp;m
|35.56 m
|39.52 m
|42.16 m
|43.8 m
|-
! 高度
|12.57&nbsp;m
| colspan="2" | 12.55&nbsp;m
| colspan="4" |12.3 m
|-
! 翼展
| colspan="3" |34.32&nbsp;m（无翼梢小翼）；35.79m（有翼梢小翼）
| colspan="4" |35.92 m
|-
! OEW
| 7,648&nbsp;kg
| 41,413&nbsp;kg
| 44,677&nbsp;kg
| -
|45,070 kg
|
| -
|-
! MTOW
| 70,080&nbsp;kg
| 79,016&nbsp;kg
| 85,139&nbsp;kg
|80,286 kg
|82,191 kg
|88,314 kg
| -
|-
! 最大燃料容量
| colspan="2" |26,022 L
| 29,666 L
| colspan="4" |25,817 L
|-
! 实用升限
| colspan="3" |12500 m（41000 ft）
|
|
|
|
|-
! 典型巡航马赫数
| colspan="7" | 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
| colspan="6" |7级
|-
! ICAO代码
|B737
|B738
|B739
|B37M
|M38M
|B39M
|B3JM
|}
 
{| class="wikitable" style="text-align: center"
|-
!Model
!747-400
!747-400ER
!747-400F
!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
! Variant
! 737-600
! 737-600
第153行： 第9行：
|-
|-
! Cockpit crew
! Cockpit crew
| colspan=4 | Two
| colspan="4" | Two
|-  
|-  
! 2-class{{rp|56–62}}
! 2-class
| 108 (8F@36" 100Y@32")
| 108 (8F@36" 100Y@32")
| 128 (8F@36" 120Y@32")
| 128 (8F@36" 120Y@32")
第161行： 第17行：
| 177 (12F@36" 165Y@32")
| 177 (12F@36" 165Y@32")
|-  
|-  
! 1-class{{rp|56–62}}
! 1-class
| 123 @32" - 130 @ 30"
| 123 @32" - 130 @ 30"
| 140 @32" - 148 @ 30"
| 140 @32" - 148 @ 30"
第167行： 第23行：
| 177 @32" - 215 @ 28"
| 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>
! Exit Limit
| colspan=2 | 149  
| colspan="2" | 149  
| 189
| 189
| 220
| 220
|-  
|-  
! Seat width{{rp|67}}
! Seat width
| colspan=4 | First : 22in / 56&nbsp;cm; Economy : 17in / 43&nbsp;cm  
| colspan="4" | First : 22in / 56&nbsp;cm; Economy : 17in / 43&nbsp;cm  
|-  
|-  
! Length{{rp|34–41}}
! Length
| 102&nbsp;ft 6&nbsp;in / 31.24&nbsp;m
| 102&nbsp;ft 6&nbsp;in / 31.24&nbsp;m
| 110&nbsp;ft 4&nbsp;in / 33.63&nbsp;m
| 110&nbsp;ft 4&nbsp;in / 33.63&nbsp;m
第181行： 第37行：
| 138&nbsp;ft 2&nbsp;in / 42.11&nbsp;m
| 138&nbsp;ft 2&nbsp;in / 42.11&nbsp;m
|-  
|-  
! Height{{rp|34–41}}
! Height
| colspan=2 | 41&nbsp;ft 3&nbsp;in / 12.57&nbsp;m
| 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)
| 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>
! Wing
| 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
| colspan="4" | Span: 112&nbsp;ft 7&nbsp;in / 34.32&nbsp;m, with winglets: 117&nbsp;ft 5in / 35.79m; Area: 124.60 m<sup>2</sup> (1,341.2 sq ft); Sweepback: 25°; AR: 9.44
|-  
|-  
! Fuselage{{rp|67}}
! Fuselage
| 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)
| 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}}
! Operating empty weight
| 80,200&nbsp;lb / 36,378&nbsp;kg
| 80,200&nbsp;lb / 36,378&nbsp;kg
| 83,000&nbsp;lb / 37,648&nbsp;kg
| 83,000&nbsp;lb / 37,648&nbsp;kg
第197行： 第53行：
| 98,495&nbsp;lb / 44,677&nbsp;kg
| 98,495&nbsp;lb / 44,677&nbsp;kg
|-  
|-  
! [[Maximum landing weight|MLW]]{{rp|21–24}}
! Maximum landing weight
| 121,500&nbsp;lb / 55,111&nbsp;kg
| 121,500&nbsp;lb / 55,111&nbsp;kg
| 129,200&nbsp;lb / 58,604&nbsp;kg
| 129,200&nbsp;lb / 58,604&nbsp;kg
第203行： 第59行：
| 157,300&nbsp;lb / 71,350&nbsp;kg
| 157,300&nbsp;lb / 71,350&nbsp;kg
|-  
|-  
! [[Maximum take-off weight|MTOW]]{{rp|21–24}}
! Maximum takeoff weight
| 144,500&nbsp;lb / 65,544&nbsp;kg
| 144,500&nbsp;lb / 65,544&nbsp;kg
| 154,500&nbsp;lb / 70,080&nbsp;kg
| 154,500&nbsp;lb / 70,080&nbsp;kg
第209行： 第65行：
| 187,700&nbsp;lb / 85,139&nbsp;kg
| 187,700&nbsp;lb / 85,139&nbsp;kg
|-  
|-  
! Fuel capacity{{rp|21–24}}
! Fuel capacity
| colspan=3 | 6,875 US gal / 26,022 L  
| colspan="3" | 6,875 US gal / 26,022 L  
| 7,837 US gal / 29,666 L{{efn|two auxiliary tanks}}
| 7,837 US gal / 29,666 L
|-  
|-  
! Lower deck cargo{{rp|21–24}}
! Lower deck cargo
| 720&nbsp;ft³ / 20.4&nbsp;m³
| 720&nbsp;ft³ / 20.4&nbsp;m³
| 966&nbsp;ft³ / 27.4&nbsp;m³
| 966&nbsp;ft³ / 27.4&nbsp;m³
第219行： 第75行：
| 1,826&nbsp;ft³ / 51.7&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/>
! Takeoff run
| {{convert|1878|m|ft|abbr=on|order=flip}}
|6,161 ft (1,878 m)
| {{convert|2042|m|ft|abbr=on|order=flip}}
|6,699 ft (2,042 m)
| {{convert|2316|m|ft|abbr=on|order=flip}}
|7,598 ft (2,316 m)
| {{convert|3000|m|ft|abbr=on|order=flip}}{{rp|159}}
|9,800 ft (3,000 m)
|-  
|-  
! Flight envelope<ref name=FAAcert/>
! Flight envelope
| colspan=4 | {{convert|41,000|ft|m|0}} Ceiling, {{cvt|0.82|Mach|41,000|knots km/h|0}} MMo
| colspan="4" |41,000 feet (12,497 m) Ceiling, Mach 0.82 (470 kn; 871 km/h) 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>
! Cruise
| {{convert|0.785|Mach|35,000|knots km/h|0}}
|Mach 0.785 (453 kn; 838 km/h)
| {{convert|0.781|Mach|35,000|knots km/h|0}}
|Mach 0.781 (450 kn; 834 km/h)
| {{convert|0.789|Mach|35,000|knots km/h|0}}
|Mach 0.789 (455 kn; 842 km/h)
| {{convert|0.79|Mach|35,000|knots km/h|0}}
|Mach 0.79 (455 kn; 844 km/h)
|-  
|-  
! 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>
! Range
| {{convert|3,235|nmi|km|abbr=on}}{{efn|110 passengers}}<ref name=backgrounder/>
|3,235 nmi (5,991 km)
| {{convert|3,010|nmi|km|abbr=on}}{{efn|126 passengers}}
|3,010 nmi (5,570 km)
| {{convert|2,935|nmi|km|abbr=on}}{{efn|162 passengers}}
|2,935 nmi (5,436 km)
| {{convert|2,950|nmi|km|abbr=on}}{{efn|178 passengers}}
|2,950 nmi (5,460 km)
|-
|-
! Engines (× 2)
! Engines (× 2)
| [[CFM International CFM56#CFM56-7 series|CFM56-7B]]18/20/22{{rp|126–133}}
|CFM56-7B18/20/22
| CFM56-7B20/22/24/26/27{{rp|134–149}}
|CFM56-7B20/22/24/26/27
| colspan=2 | CFM56-7B24/26/27{{rp|150–161}}
| colspan="2" |CFM56-7B24/26/27
|-
|-
! Thrust (× 2)
! Thrust (× 2)
| {{cvt|20,000|-|22,000|lbf|kN|disp=br}} {{rp|126–133}}
|20,000–22,000 lbf
| {{cvt|20,000|-|26,000|lbf|kN|disp=br}}{{rp|134–149}}
89–98 kN 
| {{cvt|24,000|-|27,000|lbf|kN|disp=br}}{{rp|150–153}}
|20,000–26,000 lbf
| {{cvt|24,000|-|27,000|lbf|kN|disp=br}}{{rp|154–161}}
89–116 kN
|24,000–27,000 lbf
110–120 kN
|24,000–27,000 lbf
110–120 kN
|-
|-
! Cruise max. thrust{{efn|35,000 ft – Mach 0.8 – ISA}}<ref name="CFM56-7B"/>
! Cruise max. thrust
| colspan=4 | {{cvt|5,960|lbf|kN}} (climb)
| colspan="4" |5,960 lbf (26.5 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>
! Engine dimensions
| colspan=4 | Fan tip diameter: {{cvt|61|in|cm|0}}, length: {{cvt|103.50|in|cm|0}}
| colspan="4" |Fan tip diameter: 61 in (155 cm), length: 103.50 in (263 cm)
|-
|-
! Engine ground clearance
! Engine ground clearance
| colspan=2 | 18 in / 46&nbsp;cm{{rp|44}}
| colspan="2" |18 in / 46 cm
| colspan=2 | 19 in / 48&nbsp;cm{{rp|45}}
| colspan="2" |19 in / 48 cm
|-
|-
! 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
|B736
|B736
|B737
|B737
第268行： 第128行：
|}
|}


{| style="text-align: center" class="wikitable"
{| class="wikitable" style="text-align: center"
|+ 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>
|+ Boeing 737 MAX Characteristics<ref name="brochure">{{cite web|url=https://en.wikipedia.org/wiki/Boeing_737_Next_Generation|title=Boeing 737 Next Generation|publisher=Wikipedia|date=July 2018}}</ref>
|-
|-
! Variant !! 737 MAX 7 !! 737 MAX 8 / MAX 200 !! 737 MAX 9 !! 737 MAX 10  
! Variant !! 737 MAX 7 !! 737 MAX 8 / MAX 200 !! 737 MAX 9 !! 737 MAX 10  
|-
!Cockpit crew
| colspan="4" |Two
|-  
|-  
! Seating
!Seating
| 138 (8{{abbr|J|business class}} + 130{{abbr|Y|economy class}}) to 172 max
|138 (8<abbr>J</abbr> + 130<abbr>Y</abbr>) to 172 max
| 162 (12{{abbr|J|business class}} + 150{{abbr|Y|economy class}}) to 210 max  
|162 (12<abbr>J</abbr> + 150<abbr>Y</abbr>) to 210 max
| 178 (16{{abbr|J|business class}} + 162{{abbr|Y|economy class}}) to 220 max
|178 (16<abbr>J</abbr> + 162<abbr>Y</abbr>) to 220 max
| 188 to 230 max
|188 to 230 max
|-   
|-   
! [[Airline seat#Seat pitch|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
| colspan="4" |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
!Cargo capacity
| 1,146 cu.ft / 32.45 m³
|1,146 cu.ft / 32.45 m³
| 1,543 cu.ft / 43.69 m³
|1,543 cu.ft / 43.69 m³
| 1,814 cu.ft / 51.37 m³
|1,814 cu.ft / 51.37 m³
|
|
|-  
|-  
! Length
!Length
| 116 ft 8 in / 35.56 m
|116 ft 8 in / 35.56 m
| 129 ft 8 in / 39.52 m
|129 ft 8 in / 39.52 m
| 138 ft 4 in / 42.16 m
|138 ft 4 in / 42.16 m
| 143 ft 8 in / 43.8 m
|143 ft 8 in / 43.8 m
|-  
|-  
! Wingspan
!Wingspan
| colspan=4 | 117 ft 10 in / 35.92 m
| colspan="4" |117 ft 10 in / 35.92 m
|-
|-
! Wing Area
!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/>
| colspan="4" |1,370 sq ft (127 m<sup>2</sup>) 
|-  
|-  
! 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>
!Overall height
| colspan=4 | 40 ft 4 in / 12.3 m
| colspan="4" |40 ft 4 in / 12.3 m
|-   
|-   
! [[Maximum takeoff weight]]
!Maximum takeoff weight
| 177,000 lb / 80,286 kg
|177,000 lb / 80,286 kg
| 181,200 lb / 82,191 kg
|181,200 lb / 82,191 kg
| 194,700 lb / 88,314 kg
|194,700 lb / 88,314 kg
|
|
|-   
|-   
! [[Maximum landing weight]]
!Maximum landing weight
| 145,600 lb / 66,043 kg
|145,600 lb / 66,043 kg
| 152,800 lb / 69,309 kg
|152,800 lb / 69,309 kg
| 163,900 lb / 74,344 kg
|163,900 lb / 74,344 kg
|
|
|-   
|-   
! [[Maximum zero fuel weight]]
!Maximum zero fuel weight
| 138,700 lb / 62,913 kg
|138,700 lb / 62,913 kg
| 145,400 lb / 65,952 kg
|145,400 lb / 65,952 kg
| 156,500 lb / 70,987 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>
!Operating empty weight
|  
|
| 99,360 lb / 45,070 kg
|99,360 lb / 45,070 kg
|  
|
|
|
|-
|-
! Fuel capacity
!Fuel capacity
| colspan=4 | 6,820 USgal / 25,817 L, excluding {{abbr|ACT|Auxiliary Center Tank}}
| colspan="4" |6,820 USgal / 25,817 L, excluding <abbr>ACT</abbr>
|-  
|-  
! Engine (× 2)
!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>
| colspan="4" |CFM International LEAP-1B, 69 in (175 cm) Fan diameter
|-  
|-  
! Thrust (× 2)
!Thrust (× 2)
| colspan=4 | {{convert|26,786|-|29,317|lbf|kN|0|abbr=on}}<ref name=FAA-TCDS/>
| colspan="4" |26,786–29,317 lbf (119–130 kN)
|-  
|-  
! Cruising speed
!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>
| colspan="4" |Mach 0.79 (453 kn; 839 km/h)
|-  
|-  
! Range (2-class)<ref name="tech_specs"/>
!Range (2-class)
| 3,850 nmi / 7,130 km
|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 
| 3,550 nmi / 6,570 km{{efn|With one auxiliary tank<ref name="tech_specs"/>}}
MAX 200: 2,700 nmi (5,000 km)
| 3,300 nmi / 6,110 km{{efn| With one auxiliary tank<ref name="tech_specs"/>}}
|3,550 nmi / 6,570 km
|3,300 nmi / 6,110 km
|-  
|-  
! Ceiling
!Ceiling
| colspan=4 | {{cvt|41000|feet|m}}<ref name=FAA-TCDS/>
| colspan="4" |41,000 ft (12,000 m)
|-  
|-  
! 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
|B37M
|B37M
|B38M
|B38M
第355行： 第219行：
|}
|}


{| style="text-align: center; font-size:95%;" class="wikitable"
{| class="wikitable" style="text-align: center; font-size:95%;"
|+Boeing 747 Characteristics<ref name="400pax">{{cite web|title=Boeing 747-400|publisher=Wikipedia|work=Startup|date=July 2018|url=https://en.wikipedia.org/wiki/Boeing_747-400}}</ref><ref name="400F">{{cite web|title=Boeing 747-8|publisher=Wikipedia|work=Startup|date=July 2018|url=https://en.wikipedia.org/wiki/Boeing_747-8}}</ref>
|-
|-
!Model
!Variant
!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>
!747-400
!747-400ER<ref name=400pax/>
!747-400ER
!747-400F<ref name=400F/>
!747-400F
!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>
!747-400ERF
!747-8
!747-8F
|-
|-
| Cockpit crew  
!Cockpit crew
| colspan="4"| 2
| colspan="6" |Two
|-
|-
| 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 lb / 124,330 kg
| 273,400&nbsp;lb / 124,010&nbsp;kg
|273,400 lb / 124,010 kg
|410 in 3-class
|303,700 lb / 137,700 kg
|-
|-
| [[Unit Load Device]]s
!Unit Load Devices
| 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<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>
!Exit limit
| colspan="2" | 550/660{{efn|550 main deck, 660 combined main and upper decks}}
| colspan="2" |550/660
| colspan="2" |
| colspan="2" |
|605
|8
|-
|-
| Overall length
!Overall length
| colspan="4" | 231&nbsp;ft 10 in (70.66&nbsp;m)
| colspan="4" |231 ft 10 in (70.66 m)
| colspan="2" |250 ft 2 in / 76.3 m
|-
|-
| Wingspan
!Wingspan
| colspan="4" | 211&nbsp;ft 5 in (64.44&nbsp;m)
| colspan="4" |211 ft 5 in (64.44 m)
| colspan="2" |224 ft 7 in / 68.4 m
|-
|-
| Wing area
!Wing area
| 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>
| colspan="4" |5,650 sq ft (525 m<sup>2</sup>)
| colspan="2" |554 m<sup>2</sup> (5,960 sq ft)
|-
|-
|Aspect ratio
!Aspect ratio
| colspan="4" | {{#expr:64.44/(525/64.44)round2}}
| colspan="4" |7.91
| colspan="2" | -
|-
|-
|Overall height
!Overall height
| colspan="4" | 63&nbsp;ft 8 in (19.4&nbsp;m)
| colspan="4" |63 ft 8 in (19.4 m)
| colspan="2" |63 ft 6 in / 19.4 m
|-
|-
| Max. takeoff weight
!Max. takeoff weight
| 875,000&nbsp;lb / 396,890&nbsp;kg
|875,000 lb / 396,890 kg
| 910,000&nbsp;lb / 412,775&nbsp;kg
|910,000 lb / 412,775 kg
| 875,000&nbsp;lb / 396,890&nbsp;kg
|875,000 lb / 396,890 kg
| 910,000&nbsp;lb / 412,775&nbsp;kg
|910,000 lb / 412,775 kg
| colspan="2" |987,000 lb / 447,700 kg
|-
|-
| Operating empty weight
!Operating empty weight
| PW: 404,600&nbsp;lb / 183,520&nbsp;kg
|404,600 lb / 183,520 kg
| PW: 412,300&nbsp;lb / 187,010&nbsp;kg
|412,300 lb / 187,010 kg
| GE: 360,900&nbsp;lb / 163,700&nbsp;kg
|360,900 lb / 163,700 kg
| GE: 361,600&nbsp;lb / 164,020&nbsp;kg
|361,600 lb / 164,020 kg
|485,300 lb / 220,128 kg
|434,600 lb / 197,131 kg
|-
|-
| Fuel capacity
!Fuel capacity
| 57,285 US gal (216,840&nbsp;L)  
|57,285 US gal (216,840 L)
| 63,705 US gal (241,140&nbsp;L)
|63,705 US gal (241,140 L)
| colspan="2" |53,985 US gal / 204,350L
| colspan="2" |53,985 US gal / 204,350L
|63,034 US gal / 238,610L
|59,734 US gal / 226,118L
|-
|-
| Cruise
!Cruise
| colspan="2" | {{convert|0.855|Mach|32,000|knots km/h|0}}
| colspan="2" |Mach 0.855 (504 kn; 933 km/h)
| colspan="2" | {{convert|0.845|Mach|32,000|knots km/h|0}}
| colspan="2" |Mach 0.845 (498 kn; 922 km/h)
|-
|Mach 0.86 (493 kn; 914 km/h)
| Airspeed limit<ref name="TypeCert"/>
|Mach 0.85 (488 kn; 903 km/h)
| 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
|-
| Engines (x 4)
| [[Pratt & Whitney PW4000|PW4000]] / [[General Electric CF6|GE CF6]] / [[Rolls-Royce RB211|RR RB211]]
| [[Pratt & Whitney PW4000|PW4000]] / [[General Electric CF6|GE CF6]]
| [[Pratt & Whitney PW4000|PW4000]] / [[General Electric CF6|GE CF6]] / [[Rolls-Royce RB211|RR RB211]]
| [[Pratt & Whitney PW4000|PW4000]] / [[General Electric CF6|GE CF6]]
|-
| Thrust (x 4)
| {{convert|56,500|-|63,300|lbf|kN|abbr=on}}
| {{convert|62,100|-|63,300|lbf|kN|abbr=on}}
| {{convert|56,400|-|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
!Airspeed limit
| 410 in 3-class
| colspan="4" |Mach 0.92 (542 kn; 1,004 km/h)
| 303,700&nbsp;lb / 137,700&nbsp;kg
| colspan="2" |Mach 0.9 (516 kn; 956 km/h)
|-
|-
! 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>
!Takeoff field length
| 605
|9,700 ft / 2,955m
| 8
|10,700 ft / 3,260m
|9,550 ft / 2,910m
|10,700 ft / 3,260m
| colspan="2" | -
|-
|-
! Overall length
!Range
| colspan=2| 250&nbsp;ft 2 in / 76.3 m
|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
|-
|-
! Height
!Engines (x 4)
| colspan=2| 63&nbsp;ft 6 in / 19.4 m
|PW4000 / GE CF6 / RR RB211
|PW4000 / GE CF6
|PW4000 / GE CF6 / RR RB211
|PW4000 / GE CF6
| colspan="2" |GEnx-2B67
|-
|-
! Wingspan
!Thrust (x 4)
| colspan=2| 224&nbsp;ft 7 in / 68.4 m
|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)
| colspan="2" |66,500 lbf (296 kN)
|-
|-
! Wing area
!ICAO Type
| 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>
| colspan="4" |B744
|-
| colspan="2" |B748
! [[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;"
{| class="wikitable" style="text-align:center; color:black;"
|+Boeing 757 Characteristics<ref name="757tech">{{cite web|url=https://en.wikipedia.org/wiki/Boeing_757|title=Boeing 757|publisher=Wikipedia|date=June 2018}}</ref>
|-
|-
! Variant
!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>
!757-200
! 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>
!757-200F
! 757-300<ref name=757tech/>
!757-300
|-
|-
! Cockpit crew
!Cockpit crew
| colspan=3 | Two
| colspan="3" |Two
|-
|-
! 2-class seating
!2-class seating
| 200 (12F+188Y)
|200 (12F+188Y)
|
| -
| 243 (12F+231Y)
|243 (12F+231Y)
|-
|-
! 1-class seating
!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>
|221/228, 239 max
| 5 max<ref name=Type_cert/>
|5 max
| 280, 295 max<ref name=Type_cert/>
|280, 295 max
|-
|-
! Cargo volume
!Cargo volume
| 1,670&nbsp;ft³ / 43.3 m³
|1,670 ft³ / 43.3 m³
| 6,600&nbsp;ft³ / 187 m³
|6,600 ft³ / 187 m³
| 2,370&nbsp;ft³ / 61.7 m³
|2,370 ft³ / 61.7 m³
|-
|-
! Width
!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>
| colspan="3" |148 in / 3.76 m fuselage, 139.3 in / 3.54 m cabin
|-
|-
! Length
!Length
| colspan=2 | 155&nbsp;ft 3 in / 47.3 m
| colspan="2" |155 ft 3 in / 47.3 m
| 178&nbsp;ft 7 in / 54.4 m
|178 ft 7 in / 54.4 m
|-
|-
! Height
!Height
| colspan=3 | 44&nbsp;ft 6 in / 13.6 m
| colspan="3" |44 ft 6 in / 13.6 m
|-
|-
! Wing
!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]]
| colspan="3" |124 ft 10 in / 38.0 m span, 1,994 sq ft (185.25 m<sup>2</sup>) area, 25° sweep, 7.8 AR
|-
|-
! [[Maximum takeoff weight|MTOW]]
!MTOW
| colspan=2 | 255,000&nbsp;lb / 115,660&nbsp;kg
| colspan="2" |255,000 lb / 115,660 kg
| 273,000&nbsp;lb / 123,830&nbsp;kg
|273,000 lb / 123,830 kg
|-
|-
! Max. [[Payload]]<!--MZFW - OEW-->
!Max. Payload
| {{formatnum:{{#expr:186000-128840}}}}&nbsp;lb / {{formatnum:{{#expr:84360-58440}}}}&nbsp;kg
|57,160 lb / 25,920 kg
| {{formatnum:{{#expr:200000-115580}}}}&nbsp;lb / {{formatnum:{{#expr:90720-52430}}}}&nbsp;kg
|84,420 lb / 38,290 kg
| {{formatnum:{{#expr:210000-141860}}}}&nbsp;lb / {{formatnum:{{#expr:95250-64340}}}}&nbsp;kg
|68,140 lb / 30,910 kg
|-
|-
! [[Operating empty weight|OEW]]
!OEW
| 128,840&nbsp;lb / 58,440&nbsp;kg
|128,840 lb / 58,440 kg
| 115,580&nbsp;lb / 52,430&nbsp;kg
|115,580 lb / 52,430 kg
| 141,860&nbsp;lb / 64,340&nbsp;kg
|141,860 lb / 64,340 kg
|-
|-
! Fuel capacity
!Fuel capacity
| 11,489 US gal / 43,490 L
|11,489 US gal / 43,490 L
| 11,276 US gal / 42,680 L
|11,276 US gal / 42,680 L
| 11,466 US gal / 43,400 L
|11,466 US gal / 43,400 L
|-
|-
! Speed
!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/>
| colspan="3" |Cruise Mach 0.8 (461 kn; 854 km/h), Max. Mach 0.86 (496 kn; 918 km/h)
|-
|-
! [[Range (aircraft)|Range]]
!Range
| 3,915nmi / 7,250&nbsp;km{{efn|200 passengers}}
|3,915nmi / 7,250 km
| 2,935nmi / 5,435&nbsp;km{{efn|72,210 lb / 32,755 kg payload}}
|2,935nmi / 5,435 km
| 3,400nmi / 6,295&nbsp;km{{efn|243 passengers}}
|3,400nmi / 6,295 km
|-
|-
! Takeoff{{efn|MTOW, sea level, {{convert|86|°F|°C}}, RB211-535E4B engines}}
!Takeoff
| 6,800&nbsp;ft / 2,070 m
|6,800 ft / 2,070 m
| 6,900&nbsp;ft / 2,103 m
|6,900 ft / 2,103 m
| 8,550&nbsp;ft / 2,605 m
|8,550 ft / 2,605 m
|-
|-
! Ceiling
!Ceiling
| colspan="3"| {{convert|42,000|ft|m|abbr=on}}<ref name=Type_cert/>
| colspan="3" |42,000 ft (13,000 m)
|-
|-
! Engines (×2)
!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
| colspan="3" |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
| colspan="2" |B752
|B753
|}
|}


{|class=wikitable style="text-align: center; width: 90%"  
{| 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>
|+ 767 Airplane Characteristics<ref name="767_airport_report">{{cite web|url=https://en.wikipedia.org/wiki/Boeing_767|title=Boeing 767|publisher=Wikipedia|date=June 2018}}</ref>
|-
|-
! style="width: 10%;" | Variant
! style="width: 10%;" |Variant
! style="width: 15%;" | 767-200
! style="width: 15%;" |767-200
! style="width: 15%;" | 767-200ER
! style="width: 15%;" |767-200ER
! style="width: 15%;" | 767-300
! style="width: 15%;" |767-300
! style="width: 15%;" | 767-300ER
! style="width: 15%;" |767-300ER
! style="width: 15%;" | 767-300F
! style="width: 15%;" |767-300F
! style="width: 15%;" | 767-400ER
! style="width: 15%;" |767-400ER
|-
|-
!Cockpit crew
!Cockpit crew
| colspan="6" | Two
| colspan="6" |Two
|-
!3-class
| colspan="2" |174 (15F, 40J, 119Y)
| colspan="2" |210 (18F, 42J, 150Y)
| rowspan="5" |15,469 ft³ / 438m³
58-ton / 52.7 tonnes
24 88×108in pallets
|243 (16F, 36J, 189Y)
|-
|-
! 3-class<ref name=767_airport_report/>{{rp|pages=23–29}}
!2-class
| colspan="2" | 174 (15F, 40J, 119Y)
| colspan="2" |214 (18J, 196 Y)
| colspan="2" | 210 (18F, 42J, 150Y)
| colspan="2" |261 (24J, 237Y)
| 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>
|296 (24J, 272Y)
| 243 (16F, 36J, 189Y)
|-
|-
! 2-class<ref name=767_airport_report/>{{rp|pages=23–29}}
!1-class
| colspan="2" | 214 (18J, 196 Y)
| colspan="2" |245Y
| colspan="2" | 261 (24J, 237Y)
| colspan="2" |290Y
| 296 (24J, 272Y)
|409Y
|-
|-
! 1-class<ref name=767_airport_report/>{{rp|pages=23–29}}
!Exit limit
| colspan="2" | 245Y
| colspan="2" |290
| colspan="2" | 290Y
| colspan="2" |351
| 409Y
|375
|-
|-
! 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}}
!Cargo
| colspan="2" | 290
| colspan="2" |3,070 ft³ / 86.9m³
| colspan="2" | 351
| colspan="2" |4,030 ft³ / 114.1m³
| 375
|4,905 ft³ / 138.9m³
|-
|-
! Cargo<ref name=767_airport_report/>{{rp|pages=9–14}}
!ULDs
| colspan="2" | 3,070&nbsp;ft³ / 86.9m³
| colspan="2" |22 LD2s
| colspan="2" | 4,030&nbsp;ft³ / 114.1m³
| colspan="3" |30 LD2s
| 4,905&nbsp;ft³ / 138.9m³
|38 LD2s
|-
|-
! [[Unit load device|ULD]]s<ref name=767_airport_report/>{{rp|pages=32–36}}
!Length
| colspan="2" | 22 LD2s
| colspan="2" |159 ft 2in / 48.51m
| colspan="3" | 30 LD2s
| colspan="3" |180 ft 3in / 54.94m
| 38 LD2s
|201 ft 4in / 61.37m
|-
|-
! Length<ref name=767_airport_report/>{{rp|pages=15–18}}
!Wingspan
| colspan="2" | 159&nbsp;ft 2in / 48.51m
| colspan="5" |156 ft 1in / 47.57m
| colspan="3" | 180&nbsp;ft 3in / 54.94m
|170 ft 4in / 51.92m
| 201&nbsp;ft 4in / 61.37m
|-
|-
! Wingspan<ref name=767_airport_report/>{{rp|pages=15–18}}
!Wing
| colspan="5" | 156&nbsp;ft 1in / 47.57m
| colspan="5" |3,050 ft² / 283.3m², 31.5° sweepback
| 170&nbsp;ft 4in / 51.92m
|3,130 ft² / 290.7m²
|-
|-
! Wing
!Fuselage
|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>
| colspan="6" |17 ft 9in / 5.41m height, 16 ft 6in / 5.03m width, 186in/ 4.72m Cabin width
| 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
!MTOW
| 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}}
|315,000 lb / 142,882 kg
|395,000 lb / 179,169 kg
|350,000 lb / 158,758 kg
| colspan="2" |412,000 lb / 186,880 kg
|450,000 lb / 204,116 kg
|-
|-
! [[Maximum takeoff weight|MTOW]]<ref name=767_airport_report/>{{rp|pages=9–14}}
!Max. payload
| 315,000&nbsp;lb / 142,882&nbsp;kg
|73,350 lb (33,271 kg)
| 395,000&nbsp;lb / 179,169&nbsp;kg
|78,390 lb (35,557 kg)
| 350,000&nbsp;lb / 158,758&nbsp;kg
|88,250 lb (40,030 kg)
| colspan=2 | 412,000&nbsp;lb / 186,880&nbsp;kg
|96,560 lb (43,799 kg)
| 450,000&nbsp;lb / 204,116&nbsp;kg
|119,000 lb (53,977 kg)
|101,000 lb (45,813 kg)
|-
|-
! Max. [[payload]]<ref name=767_airport_report/>{{rp|pages=9–14}}<!--MZFW-OEW-->
!OEW
| {{cvt|{{#expr:250000-176650}}|lb|kg|0}}
|176,650 lb / 80,127 kg
| {{cvt|{{#expr:260000-181610}}|lb|kg|0}}
|181,610 lb / 82,377 kg
| {{cvt|{{#expr:278000-189750}}|lb|kg|0}}
|189,750 lb / 86,069 kg
| {{cvt|{{#expr:295000-198440}}|lb|kg|0}}
|198,440 lb / 90,011 kg
| {{cvt|{{#expr:309000-190000}}|lb|kg|0}}
|190,000 lb / 86,183 kg
| {{cvt|{{#expr:330000-229000}}|lb|kg|0}}
|229,000 lb / 103,872 kg
|-
|-
! [[Operating empty weight|OEW]]<ref name=767_airport_report/>{{rp|pages=9–14}}
! rowspan="2" |Fuel capacity
| 176,650&nbsp;lb / 80,127&nbsp;kg
|16,700USgal / 63,217L
| 181,610&nbsp;lb / 82,377&nbsp;kg
|24,140Usgal / 91,380L
| 189,750&nbsp;lb / 86,069&nbsp;kg
|16,700USgal / 63,216L
| 198,440&nbsp;lb / 90,011&nbsp;kg
| colspan="3" |24,140USgal / 91,380L
| 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}}
|111,890 lb / 50,753 kg
| 16,700USgal / 63,217L
|161,738 lb / 73,363 kg
| 24,140Usgal / 91,380L
|111,890 lb / 50,753 kg
| 16,700USgal / 63,216L
| colspan="3" |161,740 lb / 73,364 kg
| colspan=3 | 24,140USgal / 91,380L
|-
|-
| 111,890&nbsp;lb / 50,753&nbsp;kg
!Range
| 161,738&nbsp;lb / 73,363&nbsp;kg
|3,900 nmi (7,200 km)
| 111,890&nbsp;lb / 50,753&nbsp;kg
|6,590nmi / 12,200 km
| colspan=3 | 161,740&nbsp;lb / 73,364&nbsp;kg
|3,900 nmi (7,200 km)
|5,980nmi / 11,070 km
|3,225nmi / 6,025 km 
|5,625nmi / 10,415 km
|-
|-
! 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>
!Cruise
| {{convert|3,900|nmi|km|abbr=on}}{{efn|216 pax, 176,100lb / 79,878kg OEW, ISA}}<ref name=767_airport_report/>{{rp|page=47}}
| colspan="6" |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)
| 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
!Takeoff
| 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}}
|6,300 ft (1,900 m)
|2,480m / 8,150 ft
|9,200 ft (2,800 m)
| colspan="2" |2,650m / 8,700 ft
|3,290m / 10,800 ft
|-
|-
! Takeoff{{efn|MTOW, SL, 30°C/86°F}}<ref name=767specs/>
!Engines (×2)
| {{convert|6,300|ft|m|abbr=on}}<ref name=767_airport_report/>{{rp|page=58}}
|P&W JT9D-7R4/7R4E / P&W PW4052 / GE CF6-80A/A2/C2-B2
| 2,480m / 8,150&nbsp;ft
|P&W JT9D-7R4/7R4E / P&W PW4052/56 / GE CF6-80A/A2/C2-B2/C2-B4 / RB211-524G/H
| {{convert|9,200|ft|m|abbr=on}}<ref name=767_airport_report/>{{rp|page=64}}
|P&W JT9D-7R4/7R4E / P&W PW4052 / GE CF6-80A/A2/C2-B2 / RB211-524H
| colspan=2 | 2,650m / 8,700&nbsp;ft
| colspan="2" |GE CF6-80C2-B4/0C2-B6/C2-B8F/C2-B7F1 / PW4056/60/62 / RB211-524G/H
| 3,290m / 10,800&nbsp;ft
|GE CF6-80C2-B8F/C2-B7F1 / PW4062
|-
|-
! Engines (×2)<ref name=767_airport_report/>{{rp|page=10}}
!Thrust (×2)
| [[Pratt & Whitney JT9D|P&W JT9D]]-7R4/7R4E / [[Pratt & Whitney PW4000|P&W PW4052]] / [[GE CF6]]-80A/A2/C2-B2
|48,000–52,500 lbf (214–234 kN)
| [[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
|48,000–60,600 lbf (214–270 kN)
| [[Pratt & Whitney JT9D|P&W JT9D]]-7R4/7R4E / [[Pratt & Whitney PW4000|P&W PW4052]] / [[GE CF6]]-80A/A2/C2-B2 / [[RB211]]-524H
|48,000–60,600 lbf (214–270 kN)
| colspan=2 | [[GE CF6]]-80C2-B4/0C2-B6/C2-B8F/C2-B7F1 / [[Pratt & Whitney PW4000|PW4056]]/60/62 / [[RB211]]-524G/H
| colspan="2" |56,750–61,500 lbf (252–274 kN)
| [[GE CF6]]-80C2-B8F/C2-B7F1 / [[Pratt & Whitney PW4000|PW4062]]
|60,600 lbf (270 kN)
|-
|-
! Thrust (×2)<ref name=767_airport_report/>{{rp|page=10}}
!ICAO Type
| {{cvt|48,000-52,500|lbf|kN|0}}
| colspan="2" |B762
| {{cvt|48,000-60,600|lbf|kN|0}}
| colspan="3" |B763
| {{cvt|48,000-60,600|lbf|kN|0}}
|B764
| 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%;"
{| class="wikitable" style="text-align:center; font-size:96%;"
|+ Boeing 777 specifications
|+ Boeing 777 specifications<ref name="Boeing_777_airport_report_gen1">{{Cite techreport|url=https://en.wikipedia.org/wiki/Boeing_777|title=Boeing 777|publisher=Wikipedia}}</ref>
|-
|-
! Model
!Variant
! 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>
!777-200
! 777-200ER<ref name=Boeing_777_airport_report_gen1/>
!777-200ER
! 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>
!777-200LR
! 777F<ref name=Boeing_777_airport_report_gen2/>
!777F
! 777-300<ref name=Boeing_777_airport_report_gen1/>
!777-300
! 777-300ER<ref name=Boeing_777_airport_report_gen2/>
!777-300ER
|-
|-
! Cockpit crew
!Cockpit crew
| colspan="6" | Two
| 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>
!3-class
| 305 (24F/54J/227Y)
|305 (24F/54J/227Y)
| colspan=2 | 301 (16F/58J/227Y)
| colspan="2" |301 (16F/58J/227Y)
|
|
| 368 (30F/84J/254Y)
|368 (30F/84J/254Y)
| 365 (22F/70J/273Y)
|365 (22F/70J/273Y)
|-
!2-class/capacity
| colspan="2" |313
|317
|224,900 lb / 102,010 kg
| colspan="2" |396
|-
|-
! 2-class/capacity<ref name=Characteristics>{{cite web |url= http://www.boeing.com/commercial/777/#/design-highlights/characteristics |title=777 Characteristics |publisher= Boeing }}</ref>
!Exit limit
| colspan=2 | 313
| colspan="3" |440
| 317
|11
| 224,900&nbsp;lb / 102,010&nbsp;kg
| colspan="2" |550
| 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>
!Length
| colspan="3" | 440
| colspan="4" |209 ft 1 in / 63.73 m
| 11
| colspan="2" |242 ft 4 in / 73.86 m
| colspan="2" | 550
|-
|-
! Length
!Wingspan
| colspan="4" | 209&nbsp;ft 1 in / 63.73 m
| colspan="2" |199 ft 11 in / 60.93 m
| colspan="2" | 242&nbsp;ft 4 in / 73.86 m
| colspan="2" |212 ft 7 in / 64.80 m
|199 ft 11 in / 60.93 m
|212 ft 7 in / 64.80 m
|-
|-
! Wingspan
!Wing sweep
| colspan="2" | 199&nbsp;ft 11 in / 60.93 m
| colspan="6" |31.6°
| 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]]
!Wing area
| 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>
| colspan="2" |4,605 sq ft (427.8 m<sup>2</sup>)
| colspan="2" |4,702 sq ft (436.8 m<sup>2</sup>)
|4,605 sq ft (427.8 m<sup>2</sup>)
|4,702 sq ft (436.8 m<sup>2</sup>)
|-
|-
! Wing area
!Aspect ratio
| colspan="2" | {{convert|427.8|m2|sqft|abbr=on|order=flip}}<ref name=elsevier/>
| colspan="2" |8.68
| 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>
| colspan="2" |9.04
| {{convert|427.8|m2|sqft|abbr=on|order=flip}}<ref name=elsevier/>
|8.68
| {{convert|436.8|m2|sqft|abbr=on|order=flip}}<ref name=AA120726/>
|9.04
|-
|-
! Aspect ratio
!Tail height
| colspan=2 | {{#expr:60.93/(427.8/60.93)round2}}
| colspan="2" |60 ft 9 in / 18.5 m
| colspan=2 | {{#expr:60.93/(436.8/64.80)round2}}
| colspan="2" |61 ft 1 in / 18.6 m
| {{#expr:60.93/(427.8/60.93)round2}}
| colspan="2" |60 ft 8 in / 18.5 m
| {{#expr:60.93/(436.8/64.80)round2}}
|-
|-
! Tail height<ref name=Characteristics/>
!Cabin width
| colspan="2" | 60&nbsp;ft 9 in / 18.5 m
| colspan="6" |231 in / 5.86 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>
!Seat width
| colspan="6" | 231 in / 5.86 m
| colspan="6" |18.5 in / 47 cm at 9 abreast, 17 in / 43 cm at 10 abreast
|-
|-
! Seat width
!Fuselage width
| colspan="6" | 18.5 in / 47&nbsp;cm at 9 abreast, 17 in / 43&nbsp;cm at 10 abreast
| colspan="6" |20 ft 4 in / 6.20 m
|-
|-
! Fuselage width
!Maximum cargo capacity
| colspan="6" | 20&nbsp;ft 4 in / 6.20 m
| colspan="3" |5,330 ft³ / 150.9 m³
|23,051 ft³ / 652.7 m³
| colspan="2" |7,120 ft³ / 201.6 m³
|-
|-
! Maximum cargo capacity<ref name=Characteristics/>
!Maximum takeoff weight (MTOW)
| colspan="3" | 5,330&nbsp;ft³ / 150.9 m³
|545,000 lb / 247,200 kg
| 23,051&nbsp;ft³ / 652.7 m³
|656,000 lb / 297,550 kg
| colspan="2" | 7,120&nbsp;ft³ / 201.6 m³
|766,000 lb / 347,452 kg
|766,800 lb / 347,815 kg
|660,000 lb / 299,370 kg
|775,000 lb / 351,533 kg
|-
|-
! [[Maximum takeoff weight]] (MTOW)
!Max. landing weight
| 545,000&nbsp;lb / 247,200&nbsp;kg
|445,000 lb / 201,840 kg
| 656,000&nbsp;lb / 297,550&nbsp;kg
|470,000 lb / 213,180 kg
| 766,000&nbsp;lb / 347,452&nbsp;kg
|492,000 lb / 223,168 kg
| 766,800&nbsp;lb / 347,815&nbsp;kg
|575,000 lb / 260,816 kg
| 660,000&nbsp;lb / 299,370&nbsp;kg
|524,000 lb / 237,680 kg
| 775,000&nbsp;lb / 351,533&nbsp;kg
|554,000 lb / 251,290 kg
|-
|-
! Max. landing weight
!Operating empty weight
| 445,000&nbsp;lb / 201,840&nbsp;kg
|299,550 lb / 135,850 kg
| 470,000&nbsp;lb / 213,180&nbsp;kg
|304,500 lb / 138,100 kg
| 492,000&nbsp;lb / 223,168&nbsp;kg
|320,000 lb / 145,150 kg
| 575,000&nbsp;lb / 260,816&nbsp;kg
|318,300 lb / 144,379 kg
| 524,000&nbsp;lb / 237,680&nbsp;kg
|353,800 lb / 160,530 kg
| 554,000&nbsp;lb / 251,290&nbsp;kg
|370,000 lb / 167,829 kg
|-
|-
! [[Operating empty weight]]
!Fuel capacity
| 299,550&nbsp;lb / 135,850&nbsp;kg
|31,000 US gal / 117,340 L / 207,700 lb / 94,240 kg
| 304,500&nbsp;lb / 138,100&nbsp;kg
|45,220 US gal / 171,171 L / 302,270 lb / 137,460 kg
| 320,000&nbsp;lb / 145,150&nbsp;kg
| colspan="2" |47,890 US gal / 181,283 L / 320,863 lb / 145,538 kg
| 318,300&nbsp;lb / 144,379&nbsp;kg
|45,220 US gal / 171,171 L / 302,270 lb / 137,460 kg
| 353,800&nbsp;lb / 160,530&nbsp;kg
|47,890 US gal / 181,283 L / 320,863 lb / 145,538 kg
| 370,000&nbsp;lb / 167,829&nbsp;kg
|-
|-
! Fuel capacity
!Service ceiling
| 31,000 US gal / 117,340 L / 207,700&nbsp;lb / 94,240&nbsp;kg
| colspan="6" |43,100 ft (13,100 m)
| 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/>
! scope="row" |Cruise speed
| colspan="6" | {{convert|43,100|ft|m|abbr=on}}
| colspan="6" |Mach 0.84 (892 km/h; 554 mph)
|-
|-
! scope="row" | Cruise speed
!Max. speed
| colspan="6" | {{convert|0.84|Mach|43100|0}}
| colspan="6" |Mach 0.89 (945 km/h; 587 mph)
|-
|-
! Max. speed
!Range
| 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>
|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
|-
|-
! Range<ref name=Characteristics/>
!Takeoff distance
| 5,240 nmi / 9,700&nbsp;km{{efn|305 passengers, Trents}}<ref name=777_perf/>
|8,000 ft
| 7,065 nmi / 13,080&nbsp;km{{efn|313 passengers}}
2,440 m
| 8,555 nmi / 15,843&nbsp;km{{efn|317 passengers}}
|11,100 ft
| 4,970 nmi / 9,200&nbsp;km{{efn|102,010 kg / 224,900 lb}}
3,380 m
| 6,030 nmi / 11,165&nbsp;km{{efn|368 passengers, GE90}}<ref name=777_perf/>
|9,200 ft
| 7,370 nmi / 13,649&nbsp;km{{efn|396 passengers}}
2,800 m
|9,300 ft
2,830 m
|10,600 ft
3,230 m
|10,000 ft
3,050 m
|-
|-
! Takeoff distance{{efn|MTOW, sea level, [[International standard atmosphere|ISA]]}}
! scope="row" |Turbofan (×2)
| {{convert|8000|ft|m|abbr=on|sigfig=3|disp=br}}
|PW 4077
| {{convert|11100|ft|m|abbr=on|sigfig=3|disp=br}}
RR 877
| {{convert|9200|ft|m|abbr=on|sigfig=3|disp=br}}
GE90-77B
| {{convert|9300|ft|m|abbr=on|sigfig=3|disp=br}}
|PW 4090
| {{convert|10600|ft|m|abbr=on|sigfig=3|disp=br}}
RR 895
| {{convert|10000|ft|m|abbr=on|sigfig=3|disp=br}}
GE90-94B
| colspan="2" |GE90-110B1
GE90-115B
|PW 4098
RR 892
GE90-92B/-94B
|GE90-115B
|-
|-
! scope="row" | Turbofan (×2)
!Max thrust (×2)
| [[Pratt & Whitney PW4000|PW 4077]] <br/>[[Rolls-Royce Trent 800|RR 877]] <br/>[[General Electric GE90|GE90-77B]]
|77,200 lbf (343 kN)
| PW 4090 <br/>RR 895<br/>GE90-94B
|93,700 lbf (417 kN)
| colspan="2" | GE90-110B1 <br/>GE90-115B
| colspan="2" |115,300 lbf (513 kN)
| PW 4098 <br/>RR 892 <br/>GE90-92B/-94B
|98,000 lbf (440 kN)
| GE90-115B
|115,300 lbf (513 kN)
|-
|-
! Max thrust (×2)
!ICAO Type
| {{convert|77,200|lbf|kN|abbr=on}}
| colspan="2" |B772
| {{convert|93,700|lbf|kN|abbr=on}}
| colspan="2" |B77L
| colspan="2" | {{convert|115,300|lbf|kN|abbr=on}}
|B773
| {{convert|98,000|lbf|kN|abbr=on}}
|B77W
| {{convert|115,300|lbf|kN|abbr=on}}
|}
|}


{| class="wikitable" style="text-align:center;"
{| 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>
|+Boeing 787 Dreamliner characteristics<ref name="787_Airport_report">{{cite web|url=https://en.wikipedia.org/wiki/Boeing_787_Dreamliner|title=Boeing 787 Dreamliner|publisher=Wikipedia}}</ref>
!Model
!Variant
! 787-8
!787-8
! 787-9
!787-9
! 787-10
!787-10
|-
|-
!Cockpit crew
!Cockpit crew
|colspan=3 |Two
| colspan="3" |Two
|-
|-
! Seating, 2-class
!Seating, 2-class
| 242 : 24J @85" + 218Y @32"
|242 : 24J @85" + 218Y @32"
| 290 : 28J @85" + 262Y @32"
|290 : 28J @85" + 262Y @32"
| 330 : 32J @85" + 298Y @32"
|330 : 32J @85" + 298Y @32"
|-
|-
! Seating, 1-class
!Seating, 1-class
| max. 359, exit limit 381
|max. 359, exit limit 381
| max. 406, exit limit 420
|max. 406, exit limit 420
| max. 440, exit limit 440
|max. 440, exit limit 440
|-
|-
!Length
!Length
| {{convert|186|ft|1|in|m|abbr=on|2}}
|186 ft 1 in (56.72 m)
| {{convert|206|ft|1|in|m|abbr=on|2}}
|206 ft 1 in (62.81 m)
| {{convert|224|ft|m|abbr=on|2}}
|224 ft (68.28 m)
|-
|-
! Wing<ref name=EASAtcds/>
!Wing
| 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
| colspan="3" |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 m<sup>2</sup>) area
|-
|-
! [[swept wing|Wing sweep]]
!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>
| colspan="3" |32.2°
|-
|-
!Height<ref name=787_Airport_report/>
!Height
| {{convert|55|ft|6|in|m|abbr=on|2}}
|55 ft 6 in (16.92 m)
| colspan=2 | {{convert|55|ft|10|in|m|abbr=on}}
| colspan="2" |55 ft 10 in (17.02 m)
|-
|-
!Fuselage
!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}}
| colspan="3" |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
!Cargo capacity
| 4,826&nbsp;ft³ /136.7 m³ <br />{{#expr:16+12}} [[LD3]] or {{#expr:5+4}} (88×125) pallets
|4,826 ft³ /136.7 m³
| 6,090&nbsp;ft³ / 172.5 m³ <br />{{#expr:20+16}} LD3 or {{#expr:6+5}} (96×125) pallets
28 LD3 or 9 (88×125) pallets
| 6,722&nbsp;ft³ / 191.4 m³ <br />{{#expr:22+18}} LD3 or {{#expr:7+6}} (96×125) 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
|-
|-
![[Maximum takeoff weight|MTOW]]
!MTOW
| 502,500&nbsp;lb / 227,930&nbsp;kg
|502,500 lb / 227,930 kg
| colspan=2 |560,000&nbsp;lb / 254,011&nbsp;kg
| colspan="2" |560,000 lb / 254,011 kg
|-
|-
![[Maximum landing weight|MLW]]
!MLW
| 380,000&nbsp;lb / 172,365&nbsp;kg
|380,000 lb / 172,365 kg
| 425,000&nbsp;lb / 192,777&nbsp;kg
|425,000 lb / 192,777 kg
| 445,000&nbsp;lb / 201,849&nbsp;kg
|445,000 lb / 201,849 kg
|-
|-
!Maximum [[zero-fuel weight|ZFW]]
!Maximum ZFW
| 355,000&nbsp;lb / 161,025&nbsp;kg
|355,000 lb / 161,025 kg
| 400,000&nbsp;lb / 181,437&nbsp;kg
|400,000 lb / 181,437 kg
| 425,000&nbsp;lb / 192,777&nbsp;kg
|425,000 lb / 192,777 kg
|-
|-
![[Operating empty weight|OEW]]
!OEW
| 264,500&nbsp;lb / 119,950&nbsp;kg
|264,500 lb / 119,950 kg
| 284,000&nbsp;lb / 128,850&nbsp;kg
|284,000 lb / 128,850 kg
| 298,700 lb / 135,500 kg
|298,700 lb / 135,500 kg
|-
|-
!Fuel capacity
!Fuel capacity
| 33,340 US gal / 126,206 L<br />223,378&nbsp;lb / 101,323&nbsp;kg
|33,340 US gal / 126,206 L
| colspan=2 | 33,384 US gal / 126,372 L<br />223,673&nbsp;lb / 101,456&nbsp;kg
223,378 lb / 101,323 kg
| colspan="2" |33,384 US gal / 126,372 L
223,673 lb / 101,456 kg
|-
|-
! Speed
!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}}
| colspan="3" |Max: Mach 0.90 (516 kn; 956 km/h); Cruise: Mach 0.85 (488 kn; 903 km/h)
|-
|-
! 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>
!Range
| {{cvt|7355|nmi|km|-1}}
|7,355 nmi (13,620 km)
| {{cvt|7635|nmi|km|-1}}
|7,635 nmi (14,140 km)
| {{cvt|6430|nmi|km|-1}}
|6,430 nmi (11,910 km)
|-
|-
!Takeoff{{efn|[[Maximum Takeoff Weight|MTOW]] ([[International Standard Atmosphere|ISA]], SL, hi thrust)}}
!Takeoff
| {{convert|8500|ft|m|abbr=on}}
|8,500 ft (2,600 m)
| {{convert|9300|ft|m|abbr=on}}
|9,300 ft (2,800 m)
| {{convert|9100|ft|m|abbr=on}}
|9,100 ft (2,800 m)
|-
|-
!Ceiling
!Ceiling
| colspan=3| {{convert|43000|ft|m|abbr=on|sigfig=3}}<ref name=FG070707/>
| colspan="3" |43,000 ft (13,100 m)
|-
|-
!Engines (×2)
!Engines (×2)
| colspan=3| [[General Electric GEnx|General Electric GEnx-1B]] ''or'' [[Rolls-Royce Trent 1000]]
| colspan="3" |General Electric GEnx-1B ''or'' Rolls-Royce Trent 1000
|-
|-
!Thrust (×2)
!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}}
|64,000 lbf (280 kN)||71,000 lbf (320 kN)||76,000 lbf (340 kN)
|}
|}

2018年7月7日 (六) 15:50的版本

Boeing 737 Next Generation Characteristics[1]
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[2]
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[3][4]
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[5]
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[6]
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[7]
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[8]
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)
  1. ↑ 模板:Cite web
  2. ↑ 模板:Cite web
  3. ↑ 模板:Cite web
  4. ↑ 模板:Cite web
  5. ↑ 模板:Cite web
  6. ↑ 模板:Cite web
  7. ↑ 模板:Cite techreport
  8. ↑ 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=2197”