Helikopter TNI Hilang Saat Evakuasi Susi Air

11/09/2011 12:07
Liputan6.com, Wamena: The search for the Army's helicopter Bell 412 type of aircraft lost contact when evacuating Susi Air is still done until Sunday (11 / 9). Heli carrying five military personnel including the pilot and copilot Capt. Siagian, First Lieutenant CPN Fathoni, Pelda Eko, Serka Yafeth, and Heru.

News of the loss of the Army's helicopter reported Papua Timika Airport control tower. Since at 15.00 CEST, loss of contact and communication with the tower of Timika. Heli is flying to help the evacuation process Susi Air plane that crashed in the District Pasema, Yahukimo District.

Meanwhile Susi Air aircraft evacuation process is still constrained weather. Through satellite technology known plane crashed in the Village District Pasema Saminage precisely. Susi Air plane took off from Wamena Airport to Kenyam transport four drums of diesel and food supplies. Dave pilots steered the plane from Australia Cootes.

Pesawat Batavia Air Pecah Ban di Malang

02/09/2011 20:48 Liputan6.com, New York: Batavia Air plane from Jakarta to Malang majoring rupture a tire on landing at airport Abdul Rahman Saleh, Malang, East Java, on Friday (2 / 9) afternoon. There were no fatalities. The incident led to the next flight to Jakarta schedule delayed four hours. Batavia Air must first wait for the arrival of new tires from Surabaya. Until now, the cause of damage is still being investigated. (WIL / ADO)

Evakuasi Pesawat Susi Temui Titik Terang

10/09/2011 20:05 Liputan6.com, Yahukimo: The process of evacuation of the plane's two pilots Susi Air airline that crashed in Pasema, Yahukimo regency, Papua, until Saturday (10 / 9), started there a bright spot. A rescue team down in a nearby village from the scene. Rescuers had reached the village of Saminage 1, is three kilometers from the scene. "The position of plane itself is known, the team will conduct an evacuation has been able to penetrate to the vicinity of the location," said corporate secretary Susi Air Gunanjar in Pangandaran, Ciamis regency, West Java, this afternoon. But they have not reached the crash site and the fate of the two crews are also unknown. As known Susi Air plane on Friday afternoon, falling in District Pasema, Yahukimo District, on the way from Wamena to Kenyam. Path-Kenyam Wamena is a routine path flown by Susi Air to transport supplies staples. The plane lost contact, 15 minutes after the flight. The aircraft of the type C208B Caravan with registration number PK-VVE depart from Wamena at around 12:20 CET by Kenyam purpose. The plane carrying the four drums of different solar food items, weighing 1159 pounds. "Bring the food and it was amazing," said Gunanjar. Flight crew, Dave Cootes as a pilot and copilot from Australia Thomas Munk Slovak origin. Properly, the aircraft arriving at around 13:30 CEST Kenyam, but does not go landing. "There is no danger or radio call sign of the crew, so we just found out does not go down after landing," said Susi, owner of Susi Air. Finally, the airline was doing a search on the plane. Apparently, the plane crashed in the area Pasema District. According Gunanjar, the plane was not carrying passengers, except the two pilots did. Aviator's fate, it is not certain. Currently flights to Papua suspended. Because the crew Susi Air is still affected conditions. Including aviation in the area of ​​Sumatra and Kalimantan. (AIS)

Evakuasi Pesawat Susi Air Terkendala Cuaca

Liputan6.com, Yahukimo: Evacuation Susi Air plane that crashed in the District Pasema, Yahukimo, Papua, is plagued severe weather and terrain on Sunday (11 / 9). SAR team, members of the TNI, and a number of local residents in Kampung Saminage, about three miles from the crash site. Susi Air's management suspended all commercial services in Papua, because attention was focused on the evacuation plane. Army helicopter that had lost contact on Saturday (yesterday has found. The five crew members survived and has landed in Wamena. Heli prepared to assist the evacuation process Susi Air plane lost contact with airport towers Timika

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

The Cessna 680 Citation Sovereign

Powerplants Two 25.3kN (5690lb) Pratt & Whitney Canada PW-306C turbofans. Performance Max cruising speed 821km/h (444kt) at 35,000ft. Certificated ceiling 47,000ft. Time to 43,000ft 26min. Takeoff distance at max takeoff weight 1220m (4000ft). Design range 5222km (2820nm) Weights Not published at late 2001 except design max payload weight 1134kg (2500lb), full fuel payload 726kg (1600lb). Dimensions Wing span 19.24m (63ft 1in), length 18.87m (61ft 10in), height 5.85m (19ft 2in). Wing area 47.4m2 (510sq ft). Capacity Flightcrew of two. Typical seating for eight passengers in a double club arrangement, max seating for 12. Production First customer deliveries scheduled for the first quarter of 2004. 79 advance orders announced at NBAA in October 1998. Type Mid size corporate jet History Cessna is developing the new Citation Sovereign mid size corporate jet to meet what it sees as a large replacement market for ageing business aircraft such as the Falcon 10, Westwind and Sabreliner. Cessna market research showed that of the 1760 or so mid sized corporate jets in service worldwide almost half are early generation aircraft which it felt would come up for replacement in the coming years. Its answer to this emerging market is to develop the Citation Excel based Model 680 Citation Sovereign, which it revealed at the October 1998 NBAA exhibition in Las Vegas. Certification is planned for late 2003 with customer deliveries getting underway in the first quarter of 2004. The Sovereign is based on the Excel's fuselage and shares some common systems but features an all new wing and numerous other differences. Cessna looked at an all new fuselage cross section for the Sovereign but opted instead to stretch the Excel fuselage (by 1.5m/4.9ft) to keep down costs and reduce development time. Even so Cessna claims the Sovereign's eight seat cabin is the largest in its class with 40% more volume than the Bombardier Learjet 60 and 18% more than the Raytheon Hawker 800XP. Power for the Sovereign will be from two FADEC equipped 25.3kN (5690lb) Pratt & Whitney Canada PW-306Cs. The PW-306 was selected in part as it also powers the 328JET regional airliner which should give maintenance and reliability benefits because of the airline industry's more rigorous operating demands. The mildly swept wing is an all new, supercritical design, based on Cessna's experience with the Citation III/VII, V and X. The horizontal stabiliser is also slightly swept. The Sovereign will enjoy good field performance, being able to operate from 1220m (4000ft) runways at max takeoff weight. Another feature is trailing link main undercarriage. The Sovereign will be equipped with a Honeywell Epic CDS avionics suite, with four 20 x 25cm (8 x 10in) colour flat panel liquid crystal displays, a digital dual channel autopilot and flight director, dual long range navigation systems and dual attitude/heading reference systems. Other standard equipment will include TCAS and an EGPWS (enhanced ground proximity warning system). The first flight of the prototype was made on February 27, 2002. The first production model is scheduled to fly by July 2002 Copyright Airliners.net, some information Copyright Aerospace Publications

The Cessna 208 Caravan I, Grand Caravan & Cargomaster

Powerplants 208 - One 450kW (600shp) Pratt & Whitney Canada PT6A-114 turboprop driving a three blade variable pitch Hartzell propeller. 208-675, 208B Super Cargomaster & Grand Caravan - One 505kW (675shp) PT6A-114A. Performance 208A - Max cruising speed 340km/h (184kt). Initial rate of climb 1215ft/min. Range with max fuel and reserves 1797km (970nm), range with max fuel and reserves 2066km (1115nm). 208B Super Cargomaster - Max cruising speed 317km/h (171kt). Max initial rate of climb 770ft/min. Range with max fuel and reserves 2000km (1080nm). Grand Caravan - Max cruising speed 337km/h (182kt). Max initial rate of climb 975ft/min. Range with max fuel and reserves 1667km (900nm). Weights 208A - Empty 1725kg (3800lb), max takeoff 3310kg (7300lb). 208B Super Cargomaster - Empty 2073kg (4570lb), max takeoff 3970kg (8750lb). Grand Caravan - Empty equipped 2250kg (4965lb), max takeoff 3970kg (8750lb). Dimensions 208A - Wing span 15.88m (52ft 1in), length 11.46m (37ft 7in), height 4.32m (14ft 2in). Wing area 26.0m2 (279.4sq ft). 208B - Same except for length 12.67m (41ft 7in). Capacity 208A - Pilot and typically nine passengers, or up to 14 with an FAA FAR Part 23 waiver. Cargo capacity 1360kg (3000lb). 208B - Passenger accommodation same. Cargo capacity for 1587kg (3500lb). Grand Caravan - One pilot and up to 14 passengers. Production 1000th unit delivered in October 1998. More than 60% of production sold outside the United States. Type Single turboprop utility transport History With sales exceeding the 1000 mark the useful Caravan is a popular utility workhorse worldwide. Design work for the Caravan dates back to the early eighties. First flight of a prototype occurred on December 9 1982 and certification was granted in October 1984. When production began the following year it became the first all new single engine turboprop powered aircraft to achieve production status. The Caravan I has had a close association with US package freight specialist Federal Express (FedEx), on whose request Cessna especially developed two pure freight versions. The first of these was the 208A Cargomaster (40 delivered), the second was the stretched 208B Super Cargomaster (260 delivered). The first Super Cargomaster flew in 1986 and features a 1.22m (4ft) stretch and greater payload capacity, including an under fuselage cargo pannier. FedEx's aircraft lack cabin windows. The 208B Grand Caravan first flew in 1990 and like the Super Cargomaster is a stretched version of the basic Caravan powered by a 505kW (675shp) PT6A-114. It can seat up to 14 passengers. Announced at the 1997 NBAA convention, the 208-675 has replaced the basic 208. It combines the standard length airframe of the 208 with the more powerful PT6A-114 of the 208B. Underbelly cargo pods, floats and skis are offered as options on the Caravan I family, and the type is easily converted from freight to passenger configurations. A military/special missions version of the 208A, dubbed the U-27A, is also on offer. The Brazilian Air Force designation is C-98. Soloy is offering a dual-engine conversion of the 208B, named Pathfinder 21. This version is powered by a 991kW (1329shp) Pratt & Whitney Canada/Soloy Dual Pac powerplant, consisting of two PT6D-114A engines driving a single propeller. Other distinguishing features of the Pathfinder 21 include a 72in cabin stretch behind the wing and a large integral cargo pod. Copyright Airliners.net, some information Copyright Aerospace Publications