Redigerer Boeing 747 (avsnitt)

== Spesifikasjoner ==
[[File:B747FAMILYv1.0.png|thumb|Sammenligning av Boeing 747SP, -100, -400, -8 og LCF.]]
{| style="text-align: center; font-size:95%;" class="wikitable"
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! Mål<ref name="specs" /><ref name="plan"/><ref>[https://web.archive.org/web/20060619030241/http://www.boeing.com/commercial/airports/acaps/7478brochure.pdf "Preliminary 747-8 Airport Compatibility."] ''The Boeing Company''. Hentet: 8. juli 2009.</ref><ref>[http://konzern.lufthansa.com/en/themen/boeing-747-8-roll-out.html "Lufthansa - Boeing 747-8 Roll out: 747-8 I vs. 747-400."]   {{Wayback|url=http://konzern.lufthansa.com/en/themen/boeing-747-8-roll-out.html |date=20121230173833 }} ''Lufthansa.'' Hentet: 5. oktober 2011.</ref> || 747-100B || 747-200B || 747-300 || 747-400<br />747-400ER || 747-8I
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|Cockpitmannskap || colspan="3"| Tre || colspan="2"| To
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|Typisk setekapasitet || colspan="2" |452 (2-klasser)<br /> 366 (3-klasser) || 496 (2-klasser)<br /> 412 (3-klasser) || 660 (1-klasser)<ref name="747sp">[https://web.archive.org/web/20111018224452/http://www.boeing.com/commercial/airports/misc/A20WE-Rev-45.pdf "747."]  |''The Boeing Company.'' Hentet: 9. januar 2012.</ref><br />524 (2-klasser)<br /> 416 (3-klasser) || 605 (maximum)<ref name="747_8">[https://www.federalregister.gov/articles/2011/06/01/2011-13433/special-conditions-boeing-model-747-8-airplanes-stairway-between-the-main-deck-and-upper-deck "747-8."]  |''Federal Register.'' 29. april 2012.</ref><br /> 467 (3-klasser)
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|Lengde || colspan="4" | 70,6&nbsp;m || 76,25&nbsp;m
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|Inre kabinbredde || colspan="5" | 6,1 m (20 fot)
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|Vingespenn || colspan="3" | 59,6&nbsp;m || 64,4&nbsp;m || 68,5&nbsp;m
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|Vingeflate || colspan="3" |  510,95&nbsp;m² (5&nbsp;500&nbsp;fot²) ||  525&nbsp;m² (5&nbsp;650&nbsp;fot²)||  (554&nbsp;m²) (5&nbsp;963&nbsp;fot²)
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|Vingens vinkel || colspan="6" | 37,5°
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|Aspect ratio || colspan="3" | 6,9 || 7,9 || 8,5-->
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|Halehøyde || colspan="3" | 19,3&nbsp;m || 19,4&nbsp;m || 19,4&nbsp;m
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|Vekt <!--  uten last-->||162&nbsp;400&nbsp;kg || 174&nbsp;000&nbsp;kg|| 178&nbsp;100&nbsp;kg ||178&nbsp;756&nbsp;kg <br />'''ER:''' 184&nbsp;600&nbsp;kg|| 214&nbsp;503&nbsp;kg
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|Maksimumsvekt || 333&nbsp;390&nbsp;kg || colspan="2" |377&nbsp;842&nbsp;kg|| 396&nbsp;890&nbsp;kg <br /> '''ER:''' 412&nbsp;775&nbsp;kg ||442&nbsp;253&nbsp;kg
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|Cruising[[fart]] <br />(ved {{Konverter|35000|ft|m|0|abbr=on}} høyde) || colspan="3" | [[Mach]] 0,84 <br />(893&nbsp;km/h, 481 [[knot]] ) || Mach 0,85 <br /> (913&nbsp;km/h, 493&nbsp;kn) <br />'''ER:''' Mach 0,855 <br /> (918&nbsp;km/h, 495&nbsp;kn)|| Mach 0,855 <br /> (918&nbsp;km/h, 495&nbsp;kn)
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|Maximumsfart|| colspan="3" | Mach 0,89 <br />(955&nbsp;km/h, 516&nbsp;kn) || colspan="2" |Mach 0,92 <br /> (988&nbsp;km/h, 533&nbsp;kn)
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|Nødvendig rullebane<br />når fullastet<ref>«Nødvendig rullebane» er lengde påkrevet av sikkerhetsgrunner. Den egentlige distansen som er nødvendig, er mye kortere enn de som er listet her.</ref> || colspan="2" | 3&nbsp;190&nbsp;m|| 3&nbsp;320&nbsp;m || 3&nbsp;018&nbsp;m <br />'''ER:''' 3&nbsp;090&nbsp;m ||3&nbsp;090&nbsp;m
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|Maximumsrekkevidde<br />når fullastet|| 5&nbsp;300 [[nautiske mil|nmi]] <br /> (9&nbsp;800&nbsp;km) || 6&nbsp;850&nbsp;nmi <br /> (12&nbsp;700&nbsp;km) || 6&nbsp;700&nbsp;nmi <br /> (12&nbsp;400&nbsp;km) || 7&nbsp;260&nbsp;nmi <br /> (13&nbsp;450&nbsp;km) <br />'''ER:''' 7&nbsp;670&nbsp;nmi <br /> (14&nbsp;205&nbsp;km) || 8&nbsp;000&nbsp;nmi <br /> (14&nbsp;815&nbsp;km)
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|Maximal drivstoffskapasitet || 183&nbsp;380&nbsp;[[Liter|L]] || colspan="2" |199&nbsp;158&nbsp;L ||216&nbsp;840&nbsp;L <br />'''ER:''' 241&nbsp;140&nbsp;L || 243&nbsp;120&nbsp;L
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|Motor (x 4) || [[Pratt & Whitney JT9D|PW JT9D-7A/-7F/-7J]] <br /> [[Rolls-Royce RB211#RB211-524 series|RR RB211-524B2]] || PW JT9D-7R4G2 <br /> [[General Electric CF6|GE CF6-50E2]] <br /> RR RB211-524D4 || PW JT9D-7R4G2 <br /> GE CF6-80C2B1 <br /> RR RB211-524D4 || [[Pratt & Whitney PW4000|PW 4062]] <br /> GE CF6-80C2B5F <br /> RR RB211-524G/H <br />'''ER:''' GE CF6-80C2B5F || [[General Electric GEnx|GEnx-2B67]]
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|Kraft per motor || | PW 207&nbsp;kN <br /> RR223&nbsp;kN|| PW 244&nbsp;kN <br /> GE 234&nbsp;kN <br /> RR 236&nbsp;kN || PW 244&nbsp;kN <br /> GE 247&nbsp;kN <br /> RR 236&nbsp;kN || PW 282&nbsp;kN<br /> GE 276&nbsp;kN <br /> RR 265/270&nbsp;kN <br />'''ER:''' GE 276&nbsp;kN || 296&nbsp;kN
|}
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* The 747 parasitic drag, C<sub>DP</sub>, is 0.022, and the wing area is {{Konverter|5500|sqft|m2|0|}}, so that ''f'' equals about {{Konverter|121|sqft|m2|abbr=on}}. The [[parasitic drag]] is given by ''½ f ρ<sub>air</sub> v²'' in which ''f'' is the product of drag coefficient C<sub>Dp</sub> and the wing area.<ref>[https://web.archive.org/web/20080224015351/http://selair.selkirk.bc.ca/aerodynamics1/Drag/Page4.html "Calculating and Plotting Parasite Drag."] ''Aerodynamics Text''. Retrieved: July 15, 2011.</ref> -->