Utente:MLWatts/Sandbox3: differenze tra le versioni

Versione delle 11:59, 11 lug 2011

Versione delle 12:59, 11 lug 2011

Riga 300:

==Specifiche per versione==

{| class="wikitable" style="text-align: center; font-size:95%;"

|-

!

!777-200 !!777-200ER !!777-200LR !!777F !!777-300 !!777-300ER

|-

!

!777-200

!777-200ER

!777-200LR

!777 Freighter

!777-300

!777-300ER

|-

!Piloti

| colspan="6" | 2

|-

!Capacità passeggeri Passeggeri<br/>in configurazione tipica

| 305colspan="3" | 301 (3- classi) <br/> 400 (2-classi) || 301 (3-classi) <br/> 400440 (2-classimassima) || 301 0<br>(3-classicargo) || N/Acolspan="2" || 368365 (3- classi) <br/> 451 (2- classi) ||<br/> 365550 (3-classimassima)

|-

!Config. posti

| colspan="6" | '''Classe turistica''': 3-4-3 (o 3-3-3), '''Prima classe''': 2-2-2, '''Lusso''':2-1-2

|-

!Lunghezza

| colspan="4" | 63,7 [[Metrom (unità209 dift misura1 in)|m]] || colspan="2" | 73,9 m (242 ft 4 in)

|-

!Apertura alare

| colspan="2" | 60,9 m (199 ft 11 in) || colspan="2" | 64,8 m (212 ft 7 in) || 60,9 m (199 ft 11 in) || 64,8 m (212 ft 7 in)

|-

!Freccia alare

!Angolo dell'ala

| colspan="6" | 31,.64[[Grado (unità di misura)|º]] °

|-

!Altezza della coda

| colspan="2" | 18,5 m ||(60 18,8ft m9 in) || colspan="2" | 18,6 m (61 ft 1 in) || colspan="2" | 18,5 m ||(60 18,7ft m9 in)

|-

!DiametroLarghezza interna della cabina

| colspan="6" | 5,8687 m (19 ft 3 in)

|-

!Diametro della fusoliera

| colspan="6" | 6,19.20 m (20 ft 4 in)

|-

!Capacità carburantedi carico merci

| colspan="3" | 150162 m³ (5&nbsp;720 cu ft) || 636653 m³ (23,051 cu ft) || colspan="2" |200 216 m³ (7,640 cu ft)

|-

!Capacità Cargo

| colspan="3" | 150 m³ || 636 m³ || colspan="2" |200 m³

|-

!Peso a vuoto

| 139.225134&nbsp;800&nbsp;kg<br/>(297&nbsp;300&nbsp;lb) || 142.900 138&nbsp;100&nbsp;kg<br/>(304&nbsp;500&nbsp;lb) || colspan="2"145&nbsp;150&nbsp;kg<br/>(320&nbsp;000&nbsp;lb) || 148.181144&nbsp;400&nbsp;kg<br/>(318&nbsp;300&nbsp;lb) || 160.120&nbsp;500&nbsp;kg<br/>(353&nbsp;800&nbsp;lb) || 166.881167&nbsp;800&nbsp;kg<br/>(370&nbsp;000&nbsp;lb)

|-

!Peso massimo all'atterraggio

| 201&nbsp;840&nbsp;kg<br/>(445&nbsp;000&nbsp;lb) || 213&nbsp;180&nbsp;kg<br/>(470&nbsp;000&nbsp;lb) || 223&nbsp;168&nbsp;kg<br/>(492&nbsp;000&nbsp;lb) || 575&nbsp;000&nbsp;lb<br/>(260&nbsp;816&nbsp;kg) || 237&nbsp;680&nbsp;kg<br/>(524&nbsp;000&nbsp;lb) || 251&nbsp;290&nbsp;kg<br/>(554&nbsp;000&nbsp;lb)

|-

!Peso massimo al decollo

| 247.210&nbsp;200&nbsp;kg<br/>(545&nbsp;000&nbsp;lb) || 297.560&nbsp;550&nbsp;kg<br/>(656&nbsp;000&nbsp;lb) || colspan="2"347&nbsp;500&nbsp;kg<br/>(766&nbsp;000&nbsp;lb) || 347.450&nbsp;800&nbsp;kg<br/>(766&nbsp;800&nbsp;lb) || 299.&nbsp;370&nbsp;kg<br/>(660&nbsp;000&nbsp;lb) || 351.534&nbsp;500&nbsp;kg<br/>(775&nbsp;000&nbsp;lb)

|-

!Velocità di crociera

| colspan="6" | Mach 0.,84 [[Numero di Mach|Mach]] (905&nbsp;km/h, 560&nbsp;mph, 490 &nbsp;[[Nodo (unità di misura)|Nodinodi]]) a 10.668&nbsp;700 m <ref>[http://www.airliners.net/info/stats.main?id=106(35&nbsp;000 Boeing 777-200 | Airliners.net<!-- Titolo generato automaticamente -->]</ref>ft)

|-

!Velocità massima

| colspan="6" | 0.89 Mach (945&nbsp;km/h, 510 nodi) a 10.668 m di altitudine

|-

!Raggio massimo

| 9.695&nbsp;km|| 14.260&nbsp;km || 17.500&nbsp;km || 9.065&nbsp;km || 11.135&nbsp;km || 14.685&nbsp;km

|-

!Capacità carburante

| 31.000 [[Gallone|US gal]] || 45.220 US gal || 53.440 US gal || 47.890 US gal || 45.220 US gal

| 47.890 US gal

|- align="center"

!Altitudine di servizio

| colspan="6" | 13.140 m

|-

!Motori (x 2)

| [[Pratt & Whitney PW4000|PW 4077]] <br> [[Rolls-Royce Trent|RR 877]] <br> [[General Electric GE90|GE90-77B]] || PW 4090 <br> RR 895 <br /> GE90-94B || GE90-110B <br> GE90-115B || GE90-110B || PW 4098 <br> RR 892 <br> GE90-94B || GE90-115B

|-

!Velocità di crociera massima

!Spinta (x 2)

| colspan="6" | Mach 0.89 (950&nbsp;km/h, 590&nbsp;mph, 512&nbsp;knots) a 10&nbsp;700 m (35&nbsp;000 ft)

| PW: 77&nbsp;000 [[Libbra forza|lbf]] (330&nbsp;kN) <br> RR: 77&nbsp;000&nbsp;lbf (330&nbsp;kN) <br> GE: 77&nbsp;000&nbsp;lbf (330&nbsp;kN) || PW: 90&nbsp;000&nbsp;lbf (400&nbsp;kN) <br> RR: 95&nbsp;000&nbsp;lbf (420&nbsp;kN) <br> GE: 94&nbsp;000&nbsp;lbf (410&nbsp;kN) || GE: 110&nbsp;000&nbsp;lbf (480&nbsp;kN) <br> GE: 115&nbsp;000&nbsp;lbf (510&nbsp;kN) || GE: 110&nbsp;000&nbsp;lbf (480&nbsp;kN) || PW: 98&nbsp;000&nbsp;lbf (430&nbsp;kN) <br> RR: 92&nbsp;000&nbsp;lbf (400&nbsp;kN) <br> GE: 94&nbsp;000&nbsp;lbf (410&nbsp;kN) || GE: 115&nbsp;000&nbsp;lbf (510&nbsp;kN)

|-

!Autonomia massima

| 9&nbsp;700&nbsp;km<br/>(5&nbsp;240&nbsp;NM) || 14&nbsp;310&nbsp;km<br/>(7&nbsp;725&nbsp;NM) || 17&nbsp;370&nbsp;km<br/>(9&nbsp;380&nbsp;NM) || 9&nbsp;070&nbsp;km<br/>(4&nbsp;900&nbsp;nmi) || 11&nbsp;120&nbsp;km<br/>(6&nbsp;005&nbsp;NM) || 14,690&nbsp;km<br/>(7,930&nbsp;NM)

|-

!Lunghezza della corsa di decollo<br>a pieno carico

| 2&nbsp;500&nbsp;m<br/>(8&nbsp;200&nbsp;ft) || colspan="3" | 3&nbsp;536&nbsp;m<br/>(11&nbsp;600&nbsp;ft) || 3&nbsp;410&nbsp;m<br/>(11&nbsp;200&nbsp;ft) || 3,200&nbsp;m<br/>(10&nbsp;500&nbsp;ft)

|-

!Capacità di carburante massima

| 31&nbsp;000 [[Gallone americano|U.S. gal]]<br/>(117,348&nbsp;L) || 45,220 US gal<br/>(171,176&nbsp;L) || 47,890 US gal<br />(181,283&nbsp;L) || 47,890&nbsp;US gal<br />(181,283&nbsp;L) || 45,220&nbsp;US gal<br/>(171,176&nbsp;L)

| 47,890 US gal<br/>(181,283&nbsp;L)

|-

!Tangenza

| colspan="6" | 43,100&nbsp;ft (13.,140 &nbsp;m)

|-

!Motore (×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 || GE90-110B110B1 <br/> GE90-115B115B1 || GE90-110B110B1 || PW 4098 <br/> RR 892 <br/> GE90-92B/GE90-94B || GE90-115B115B1

|-

!Spinta (x 2×2)

| PW: 77,000&nbsp;000 [[Libbra forzapound-force|lbf]] (330342&nbsp;kN) <br/> RR: 77&nbsp;76,000&nbsp;lbf (330338&nbsp;kN) <br/> GE: 77&nbsp;,000&nbsp;lbf (330342&nbsp;kN) || PW: 90&nbsp;,000&nbsp;lbf (400&nbsp;kN) <br /> RR: 95&nbsp;00093,400&nbsp;lbf (420415&nbsp;kN) <br/> GE: 94&nbsp;00093,700&nbsp;lbf (410417&nbsp;kN) || GE −110B: 110&nbsp;000,100&nbsp;lbf (480490&nbsp;kN) <br /> GE −115B: 115&nbsp;000,540&nbsp;lbf (510514&nbsp;kN) || GE: 110&nbsp;000,100&nbsp;lbf (480490&nbsp;kN) || PW: 98&nbsp;,000&nbsp;lbf (430436&nbsp;kN) <br/> RR: 92&nbsp;00093,400&nbsp;lbf (400415&nbsp;kN) <br/> GE: 94&nbsp;92,000/93,700&nbsp;lbf (410409&nbsp;kN)/(418&nbsp;kN) || GE: 115&nbsp;000,540&nbsp;lbf (510514&nbsp;kN)

|}

Fonti: ''Boeing 777 specifications'',<ref name=Boe_777_specs/> ''Boeing 777 airport planning report'',<ref name=boeing-airport-planning777>{{cite web|url=http://www.boeing.com/commercial/airports/777.htm |title=777 Airplane Characteristics for Airport Planning |work=[http://www.boeing.com/ Boeing] |date=Dicembre 2008|accessdate=11 luglio 2011}}</ref> ''Civil Aircraft'',<ref>{{Cita|Frawley|pp. 61-62.}}</ref> ''Rolls-Royce Trent 800 series data''.<ref>{{cite web|url=http://www.rolls-royce.com/civil_aerospace/products/airlines/trent800/technical.jsp |title=Trent 800 Technical data (archive) |work=[http://www.rolls-royce.com/ Rolls-Royce] |year=2007 |accessdate=11 luglio 2011 |archiveurl =http://web.archive.org/web/20071026200936/http://www.rolls-royce.com/civil_aerospace/products/airlines/trent800/technical.jsp |archivedate=26 ottobre 2007}}</ref>

==Incidenti==

Riga 384:

*<!-- Eden -->{{cita libro|nome=Eden |cognome=Paul |titolo=Civil Aircraft Today: The World's Most Successful Commercial Aircraft |editore=Amber Books Ltd |città=Londra |anno=2008 |id=ISBN 1-84509-324-0 |pagina= |cid=Eden}}

*<!-- Frawley -->{{cita libro|nome=Gerard |cognome=Frawley |titolo=The International Directory of Civil Aircraft 2003/2004 |editore=Aerospace Publications |città=Londra |anno=2003 |id= |pagina=ISBN 1-875671-58-7 |cid=Frawley}}

*<!-- Norris e Wagner 1996-->{{cita libro|nome=Guy |cognome=Norris |coautori=Mark Wagner |titolo=Boeing 777 |editore=Motorbooks International |città=St. Paul ([[Minnesota|MN]]) |anno=1996 |id=ISBN 0-7603-0091-7 |pagina= |cid=Norris e Wagner 1996}}