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Puing Pesawat Wapres Malawi Ditemukan, Tidak ada yang Selamat

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 >>>Pesawat yang membawa  rombongan Wakil Presiden (Wapres) Malawi, Saulos Chilima dan sembilan orang lainnya, telah ditemukan pada hari Selasa (11/6), sehari setelah pesawat tersebut hilang dalam cuaca buruk. Presiden Malawi Lazarus Chakwera mengatakan tidak ada yang selamat dalam tragedi itu.pesawat itu disebut jatuh di hutan. "Pesawat itu telah ditemukan dan saya sangat bersedih untuk memberi tahu Anda semua, ini ternyata menjadi tragedi yang mengerikan," katanya dalam pidato yang disiarkan televisi, dikutip dari kantor berita AFP, Selasa (11/6/2024). Foto-foto yang dibagikan kepada AFP oleh seorang anggota tim penyelamat militer menunjukkan para personel militer berdiri di lereng berkabut dekat puing-puing yang memuat nomor registrasi pesawat militer Malawi, Dornier 228-202K. Puing-puing Pesawat Wapres Malawi yang Hilang Telah Ditemukan Pesawat militer yang membawa Chilima (51) dan sembilan orang lainnya tersebut hilang pada hari Senin (10/6), setelah gagal menda...
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The Cessna CitationJet, CJ1 & CJ2

Powerplants CitationJet & CJ1 - Two 8.45kN (1900lb) Williams Rolls-Royce FJ44-1A turbofans. CJ2 - Two 10.2kN (2300lb) FJ442Cs. Performance CitationJet - Max cruising speed at 3990kg (8800lb) AUW 704km/h (380kt). Initial rate of climb 3311ft/min. Certificated ceiling 41,000ft. Range with max fuel and reserves 2750km (1485nm). CJ1 - Range with pilot, three passengers and IFR reserves 2315km (1250nm). CJ2 - Max cruising speed at 33,000ft 741km/h (400kt). Service ceiling 45,000ft. Range with pilot, three passengers and IFR reserves 2687km (1450nm). Weights CitationJet - Empty 2794kg (6160lb), max takeoff 4717kg (10,400lb). CJ1 - Max takeoff 4812kg (10,600lb). CJ2 - Max takeoff 5585kg (12,300lb). Dimensions CitationJet & CJ1 - Wing span 14.26m (46ft 10in), length 12.98m (42ft 7in), height 4.18m (13ft 8in). Wing area 22.3m2 (240.0sq ft). CJ2 - Wing span 15.18m (49ft 10in), length 14.30m (46ft 11in). Capacity CitationJet & CJ1 - Two flightdeck positions, one for pilot, other for a copilot or passenger. Main cabin seats five in standard layout. CJ2 - Main cabin seats six in standard club arrangement. Production 300th CitationJet due to be delivered in early 1999. 76 advance orders for the CJ2 held at late 1998. Type Light corporate jets History The highly successful CitationJet was developed as a replacement for the Citation and Citation I. Improved and stretched developments, the CJ1 and CJ2 respectively, are under development. Cessna launched the new Model 525 CitationJet at the annual US National Business Aircraft Association convention in 1989. First flight occurred on April 29 1991, FAA certification was awarded on October 16 1992 and the first delivery was on March 30 1993. The CitationJet is effectively an all new aircraft. The same basic Citation forward fuselage is mounted to a new T-tail configured tailplane and a new supercritical laminar flow wing, and it features Williams Rolls FJ44 turbofans (with paddle thrust reversers) and trailing link main undercarriage. The CitationJet's fuselage is 27cm (11in) shorter than the Citation/Citation I's, while cabin height is increased courtesy of a lowered centre aisle. It features EFIS avionics and is certificated for single pilot operation. At the 1998 NBAA convention Cessna revealed it was developing the improved CJ1 and stretched CJ2. The CJ1 will replace the CitationJet and will introduce a Collins Pro Line 21 EFIS avionics suite and a moderate increase in maximum takeoff weight. The CJ1 will be delivered from the first quarter of 2000. The CJ2 meanwhile is a stretched, faster and more powerful development. Due to fly in the second quarter of 1999 and be certificated 12 months later, the CJ2 will feature a 89cm (35in) cabin and 43cm (17in) tailcone stretch allowing standard seating for six in the main cabin. Like the CJ1 it will feature Collins Pro Line 21 EFIS avionics, plus uprated FJ44-2C engines, increased span wings, larger area tail, six cabin windows per side and greater range. It will be certificated for single pilot operation. Copyright Airliners.net, some information Copyright Aerospace Publications

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The Bell 206LT TwinRanger & Tridair Gemini ST

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Powerplants Two 335kW (450shp) takeoff rated Allison 250C20R turboshafts, driving a two blade main rotor and two blade tail rotor. Performance 206LT - Max cruising speed 217km/h (117kt), economical cruising speed 200km/h (108kt). Service ceiling 10,000ft. Hovering ceiling in ground effect 10,000ft, out of ground effect 6900ft. Range with max fuel and no reserves at long range cruising speed 463km (250nm). 206L3ST - Max cruising speed 217km/h (117kt). Initial rate of climb 1550ft/min. Service ceiling 20,000ft. Hovering ceiling in ground effect 15,800ft. Range with max payload and max internal fuel 643km (347nm). Weights 206LT - Standard empty 1246kg (2748lb), max takeoff 2018kg (4450lb), or 2064kg (4550lb) with an external sling load. 206L3ST - Empty 1175kg (2590lb), max takeoff 1928kg (4250lb). Dimensions Main rotor diameter 11.28m (37ft 0in), length overall 13.02m (42ft 9in), fuselage length 9.81m (32ft 3in), height 3...
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Pesawat Tenaga Surya Pertama Sukses Meluncur Di Langit Swiss

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SWISS (Suara Media News) - Solar Impulse, yang menjadi pelopor pesawat terbang tenaga surya, sukses melakukan uji coba penerbangan di langit Swiss bagian barat pekan ini. "Belum pernah ada pesawat terbang seperti itu di angkasa. Ini adalah sebuah karya yang tidak biasa," kata Bertrand Piccard yang turut dalam proyek penerbangan pesawat tenaga surya ini, diberitakan oleh AFP.
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The Boeing 707

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Powerplants 707-120B - Four 75.6kN (17,000lb) Pratt & Whitney JT3D-1 turbofans. 707-320B - Four 80kN (18,000lb) JT3D-3s or four 84.4kN (19,000lb) JT3D-7s. Performance 707-120B - Max speed 1010km/h (545kt), max cruising speed 1000km/h (540kt), economical cruising speed 897km/h (484kt). Range with max payload 6820km (3680nm), range with max fuel 8485km (4580nm). 707-320B - Max speed 1009km/h (545kt), max cruising speed 974km/h (525kt), long range cruising speed 885km/h (478kt). Range with max passengers 6920km (3735nm), range with max fuel and 147 passengers 9265km (5000nm). Weights 707-120B - Operating empty 55,589kg (122,533lb), max takeoff 116,575kg (257,000lb). 707-320B - Empty 66,406kg (146,400lb), max takeoff 151,315kg (333,600lb). Dimensions 707-120B - Wing span 39.90m (130ft 10in), length 44.07m (144ft 6in), height 12.94m (42ft 5in). Wing area 226.3m2 (2433sq ft). 707-320B - Wing span 44.42m (145ft 9in), length 46.61m (152ft 11in), height 12.93m ...
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