British Aerospace ATP: Perbedaan antara revisi
Konten dihapus Konten ditambahkan
Baris 81:
* [[Aireuropa Express]]
* [[United Feeder Service]]
==Insiden terkenal==
* Pada 19 April 1997 [[Merpati Nusantara Airlines Penerbangan 106]] kehilangan kendali pada ketinggian 2000 kaki saat melakukan pendekatan menuju [[Bandar Udara Tanjung Pandan-Bulutumbang]] di [[Indonesia]]. 15 orang tewas dan 43 selamat dalam kecelakaan yang menyebabkan Penerbangan 106 merupakan kecelakaan terburuk kedua yang melibatkan pesawat British Aerospace ATP.
* Pada 11 Desember 1999 [[SATA Air Açores Penerbangan 530M]] jatuh menabrak gunung di [[Pulau Sao Jorge]], [[Açores]], [[Portugal]] dalam sebuah penerbangan jarak pendek. Seluruh 35 penumpang tewas dan membuat insiden ini merupakan kecelakaan terburuk yang melibatkan British Aerospace ATP.
==Spesifikasi==
{{aircraft specifications
|plane or copter?=plane
|jet or prop?=prop
|ref= Jane's All the World's Aircraft, 1988-1989 <ref name="Janes88-89">{{cite book
| last = Taylor
| first = JWR (Editor)
| title = Jane's All the World's Aircraft, 1988-1989
| year = 1988
| publisher = Jane's Information Group
| language =
| isbn =0-7106-0867-5 }}</ref>
|crew=Empat (Dua penerbang dan dua pramugari)
|capacity=64 penumpang
|length main= 26,00 m
|length alt= 85 ft 4 in
|span main= 30,63 m
|span alt= 100 ft 6 in
|height main= 7,14 m
|height alt= 23 ft 5 in
|area main= 78,3 m² <ref name="aerospace-technology">{{cite web |url=http://www.aerospace-technology.com/projects/bae_atp/specs.html |title= BAE ATP Advanced Turboprop - Specifications |accessdate=2007-07-03 |work= Aerospace Technology}}</ref>
|area alt= 843 ft²
|airfoil=
|empty weight main= 13.595 kg
|empty weight alt= 29.970 [[pound (massa)|lb]]
|loaded weight main=
|loaded weight alt=
|useful load main=
|useful load alt=
|max takeoff weight main= 22.930 kg
|max takeoff weight alt= 50.550 lb
|more general=
|engine (prop)=[[Pratt & Whitney Canada PW100|Pratt & Whitney Canada PW126]]
|type of prop=[[turboprop]]
|number of props=2
|power main= 1,978 kW
|power alt= 2,653 [[tenaga kuda|pk]]
|max speed main=
|max speed alt=
|cruise speed main= 496 km/jam
|cruise speed alt= 268 [[knot|knots]], 308 mph
|stall speed main=
|stall speed alt=
|never exceed speed main=
|never exceed speed alt=
|range main= 1.825 km
|range alt= 985 nmi, 1.134 mi
|ceiling main= 7.600 m <ref name="aerospace-technology"/>
|ceiling alt= 25.000 ft
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
|armament=
|avionics=
}}
==Lihat juga==
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