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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 205, 206 & 207

Powerplants 207A - One 225kW (300hp) Continental IO-520-F fuel injected flat six driving a three blade c/s McCauley prop. 206H - One 224kW (300hp) Textron Lycoming IO-540-AC1A driving a three blade c/s prop. T206H - One 231kW (310hp) turbocharged TIO-540-AJ1A. Performance 207A - Max speed 278km/h (150kt), max cruising speed 266km/h (144kt), long range cruising speed 220km/h (118kt). Initial rate of climb 810ft/min. Service ceiling 13,300ft. Range with standard fuel and reserves 870km (470nm), with optional fuel and reserves 1280km (690nm). 206H - Max speed 278km/h (150kt), cruising speed at 75% power at 6500ft 143kt (265km/h). Initial rate of climb 920ft/min. Service ceiling 16,000ft. Takeoff distance 275m (900ft). T206H - Max speed 315km/h (170kt), cruising speed at 75% at 20,000ft 306km/h (165kt). Initial rate of climb 1010ft/min. Service ceiling 27,000ft. Takeoff distance 255m (835ft). Weights 207A - Empty 951kg (2095lb), max takeoff 1639kg (3612lb). 206H - Empty 974kg (2146lb), max ramp 1640kg (3614lb). T206H - Empty 1011kg (2227lb), max ramp 1641kg (3616lb). Dimensions 206H & T206H - Wing span 10.92m (35ft 10in), length 8.62m (28ft 3in), height 2.92m (9ft 7in). Wing area 16.2m2 (174sq ft). 207A - Same as 206 except length 9.68m (32ft 9in). Capacity 205 & 206 seat six, 207 seats seven or eight. Production 574 205s, 7556 206s and 790 207s were built through to 1984. 206H & T206H deliveries began in late 1998. Type Six seat utility light aircraft History The popular 205/206/207 line began life as a four seat utility aircraft, stretched from the 182 Skylane. In its initial form the 205 (originally 210-5) was essentially a fixed undercarriage derivative of the 210 Centurion, optimised for utility roles, giving more baggage space. Introduced to the Cessna lineup in 1962, the 205 was powered by the same IO-470 engine as the 210B and featured an additional small cargo door on the left side of the fuselage. It later gained it's 6th seat. The 205 lasted in production until 1964 when it was replaced by the more powerful 206, which came in 2 options, the P206 Super Skylane and the U206 Super Skywagon, which respectively meant Passenger and Utility, the U206 featuring larger double cargo doors on the right fuselage side. Continuous improvement followed, including introduction of turbocharged and fuel injected models. The 'Super' prefix for the Super Skywagon was dropped in 1969 and the Stationair name was adopted in 1971. Production originally ceased in 1985. The 207 Skywagon meanwhile featured a 1.07m (3ft 6in) fuselage stretch (allowing seating for seven) and became available from 1969. Known as the Stationair 7 from 1978, it was replaced by the 207A Stationair 8 from 1979 which had seating for an eighth occupant. Production ended in 1984. A few were built in France by Reims as the F207. Several 206 and 207 aircraft have been converted to turbine power by Soloy as the Turbine 206 and 207. The 206 is the third Cessna single to be returned to production at the company's new Independence plant in Kansas. Two versions are offered, the normally aspirated 206H and turbo T206H. The T206H first flew on August 6 1996, powered by a TIO-580, while the normally aspirated 206H, powered by an IO-580, followed on November 6. A decision to switch to the TIO-540 and IO-540 because of reliability concerns pushed back production by about 10 months. The 206H was certificated on September 9 1998, the T206H on October 1. 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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