TRIBUNMANADO.CO.ID, SATURN - WHO Headquarters Exercise implement the National Air Defense Operations in North Sulawesi, with the name of the exercise Tetuka XXXV/11, has two exercise scenarios that have been designed, namely the combat aircraft and civilian aircraft that enter the territory air sovereignty Republlik countries Indonesia, Monday (24/10/2011).
"The treatment of different safeguards for civil aircraft and fighter planes," said the commander of the air base (Danlanud) Sam Ratulangi Manado, Lt. Col. Jory PNB Koloay
Steps were taken to the scenario is a fighter, with radar detection of targets through the air, the next target manually implemented reporting and automatic digital command to the commander of the national air defense.
Furthermore Sukhoi fighter planes stationed in North Sulawesi was ordered to carry out fly ambush, which included flying combat air patrol, shadowing enemy aircraft, carrying out expulsion further destruction of the enemy fighters with the command of the Armed Forces Commander and President
While the steps taken in the scenario of commercial aircraft or civilian transport across the airspace of the Republic of Indonesia without a permit, then the radar will detect air targets, subsequent target reporting carried out manually and automatic digital command to the Commander of the national air defense.
Furthermore Sukhoi fighter planes stationed in North Sulawesi, was ordered to carry out an ambush that included flying combat air patrols flying, aircraft shadowing civil transport aircraft, forcing the plane landed at the airport Ratulangi Sam, then Sam Ratulangi Lanud Team carry out safety inspection and investigation procedures .
Admittedly, these activities are aimed at testing the preparedness of the national defense system that is in the TNI. "In this equipment the dominant equipment and personnel from the Air Force in maintaining security and air sovereignty of the Republic of Indonesia," he said
XXXV/11 Tetuka training activities based on the TNI commander Warrant sprint/134/VII/2011 number dated July 7, 2011, involving 1479 personnel training is divided in three regions, namely North Sulawesi, East Kalimantan and South Sulawesi with air operations control center nationally in Jakarta.
Cooperation with Airbus, SBY Visit PT DI ( Dirgantara Indomrsia)
As informed the Press Bureau of the Palace, the President is scheduled to visit PT DI in Bandung on Wednesday (26/10/2011).
Inauguration of cooperation it is for a product collaboration with PT Indonesia Aerospace and Airbus Military equipment for military weaponry.
In addition, the president also reiterated government's commitment to the procurement of aircraft to meet the needs of defense equipment CN 295, CN 295 Improved marketing agreements, products of PT Dirgantara Indonesia, the Asia-Pacific with Airbus Military.
The President will also witness the agreement (LOI-red) between the PT Dirgantara Indonesia with police.
In addition, the presence of the president is also intended to Give specific directions to the Managing Director of the production of combat vehicles Pindad about Jeep. [lal]
News The fall of Cassa 212 plane
Front 212 Cassa Aircraft Destroyed
SAR team was checking the Cassa 212-200 planes that crashed in the mountains of Bahorok. Condition of the aircraft were destroyed, especially in the front."The plane was destroyed in the front," says Police Chief Adjunct Senior Commissioner Langkat Mardiyono when talking with AFP on Saturday (20/01/2011).Mardiyono said the current officers are still trying to coordinate with officials in the post for the evacuation process. "We still continue to communicate," he said.Previously, Head of the National SAR Marshal TNI Daryatmo ensure all passengers were killed.Cassa 212-200 planes owned by PT Nusantara Buana Water (NBA) is known to carry 14 passengers and 4 crew. The plane crashed in the mountains Bohorok, Langkat, North Sumatra. The evacuation process was stalled last Friday (30/09/2011), due to heavy rain.All Passenger Aircraft Cassa diesA total of 14 passengers and 4 crew confirmed dead in plane crash Buana Nusantara Water (NBA) in Langkat, North Sumatra (North Sumatra). The assurance was obtained after rescue teams arrived at the crash site.National SAR Agency Daryatmo Marshal Marshal TNI states, it had to get confirmation of the SAR personnel who have reached the location.There are 16 personnel who had already arrived, and has performed initial checks on the condition of each passenger who was still in his seat each time is found."A total of death," said Daryatmo a news conference at the Air Force Base (air base) Medan.NBA plane crashed on Thursday (9/29/2011) morning on a flight from Medan to Kutacane, Southeast Aceh. Not known for sure what caused the crash.Aircraft Passenger Whole Cassa 212 Found in Each SeatSearch and Rescue team has ensured all passengers Cassa 212-200 owned by PT Nusantara Buana Water (NBA) were killed. All the passengers are found in a sitting position in aircraft seats."They are found in a sitting position in their seats," said Director of Operations Basarnas, First Marshal Sunarbowo, after a press conference in Langkat, Medan, Saturday (01/10/2011).Sunabowo say, the condition of the aircraft destroyed on the front. But overall, the fuselage is relatively intact."Others are intact, nothing was broken, just broken nose," said Sunarbowo.Previously, Head of the National SAR Marshal Marshal TNI Daryatmo ensure all passengers were killed.Cassa 212-200 planes owned by PT Nusantara Buana Water (NBA) is known to carry 14 passengers and 4 crew. The plane crashed in the mountains Bohorok, Langkat, North Sumatra. The evacuation process was stalled last Friday (30/09/2011), due to heavy rain.
Aircraft Passenger Whole Cassa 212 Killed, Family hystericallyAll the passengers Cassa 212-200 owned by PT Nusantara Buana Water (NBA) who falls in Pegununan Bahorok confirmed dead some time ago. Families who have been looking forward to the news was hysterical.Families who intentionally gathered to hear the news directly to cry hysterically. Even a number of relatives fainting was unable to hear the sad news.Some mothers even had to be carried to get care. They are unable to speak except to tears on Saturday (01/10/2011).But there is also a mother who appears emotionally to hear this news. Veiled women were constantly protesting about the slow pace of aid to try to rescue the passengers.Previously, Head of the National SAR Marshal Marshal TNI Daryatmo ensure all passengers were killed.Cassa 212-200 planes owned by PT Nusantara Buana Water (NBA) is known to carry 14 passengers and 4 crew. The plane crashed in the mountains Bohorok, Langkat, North Sumatra. The evacuation process was stalled last Friday (30/09/2011), due to heavy rain.Investigate the cause of the crash NTSC CassaTeam National Transportation Safety Committee (NTSC) arrived in Medan and will lead to the crash site Cassa 212-200 owned by PT Nusantara Buana Water (NBA). They will investigate the crash peyebab.NTSC teams totaling 12 people, including the elements of the Directorate General of Civil Aviation Ministry of Transportation arrived Air Force Base (air base) around Medan Polonia Airport, on Saturday (1/10/2011) morning. Preparation for the crash site being prepared.Chairman of the Subcommittee on Air NTSC, Masruri, has not received sufficient preliminary data related to possible causes of the accident. Planned, the team will soon be the location of the NTSC and will investigate further."Today's plan will be to the location if weather conditions are good," said Masruri.NTSC team effort to the crash site relies heavily on weather conditions. Basarnas evacuation team that has been seeking to enter the site had several failed location by helicopter. Although successful in reducing personnel, helicopter landing remains difficult because there is no open area around the site.
SAR team was checking the Cassa 212-200 planes that crashed in the mountains of Bahorok. Condition of the aircraft were destroyed, especially in the front."The plane was destroyed in the front," says Police Chief Adjunct Senior Commissioner Langkat Mardiyono when talking with AFP on Saturday (20/01/2011).Mardiyono said the current officers are still trying to coordinate with officials in the post for the evacuation process. "We still continue to communicate," he said.Previously, Head of the National SAR Marshal TNI Daryatmo ensure all passengers were killed.Cassa 212-200 planes owned by PT Nusantara Buana Water (NBA) is known to carry 14 passengers and 4 crew. The plane crashed in the mountains Bohorok, Langkat, North Sumatra. The evacuation process was stalled last Friday (30/09/2011), due to heavy rain.All Passenger Aircraft Cassa diesA total of 14 passengers and 4 crew confirmed dead in plane crash Buana Nusantara Water (NBA) in Langkat, North Sumatra (North Sumatra). The assurance was obtained after rescue teams arrived at the crash site.National SAR Agency Daryatmo Marshal Marshal TNI states, it had to get confirmation of the SAR personnel who have reached the location.There are 16 personnel who had already arrived, and has performed initial checks on the condition of each passenger who was still in his seat each time is found."A total of death," said Daryatmo a news conference at the Air Force Base (air base) Medan.NBA plane crashed on Thursday (9/29/2011) morning on a flight from Medan to Kutacane, Southeast Aceh. Not known for sure what caused the crash.Aircraft Passenger Whole Cassa 212 Found in Each SeatSearch and Rescue team has ensured all passengers Cassa 212-200 owned by PT Nusantara Buana Water (NBA) were killed. All the passengers are found in a sitting position in aircraft seats."They are found in a sitting position in their seats," said Director of Operations Basarnas, First Marshal Sunarbowo, after a press conference in Langkat, Medan, Saturday (01/10/2011).Sunabowo say, the condition of the aircraft destroyed on the front. But overall, the fuselage is relatively intact."Others are intact, nothing was broken, just broken nose," said Sunarbowo.Previously, Head of the National SAR Marshal Marshal TNI Daryatmo ensure all passengers were killed.Cassa 212-200 planes owned by PT Nusantara Buana Water (NBA) is known to carry 14 passengers and 4 crew. The plane crashed in the mountains Bohorok, Langkat, North Sumatra. The evacuation process was stalled last Friday (30/09/2011), due to heavy rain.
Aircraft Passenger Whole Cassa 212 Killed, Family hystericallyAll the passengers Cassa 212-200 owned by PT Nusantara Buana Water (NBA) who falls in Pegununan Bahorok confirmed dead some time ago. Families who have been looking forward to the news was hysterical.Families who intentionally gathered to hear the news directly to cry hysterically. Even a number of relatives fainting was unable to hear the sad news.Some mothers even had to be carried to get care. They are unable to speak except to tears on Saturday (01/10/2011).But there is also a mother who appears emotionally to hear this news. Veiled women were constantly protesting about the slow pace of aid to try to rescue the passengers.Previously, Head of the National SAR Marshal Marshal TNI Daryatmo ensure all passengers were killed.Cassa 212-200 planes owned by PT Nusantara Buana Water (NBA) is known to carry 14 passengers and 4 crew. The plane crashed in the mountains Bohorok, Langkat, North Sumatra. The evacuation process was stalled last Friday (30/09/2011), due to heavy rain.Investigate the cause of the crash NTSC CassaTeam National Transportation Safety Committee (NTSC) arrived in Medan and will lead to the crash site Cassa 212-200 owned by PT Nusantara Buana Water (NBA). They will investigate the crash peyebab.NTSC teams totaling 12 people, including the elements of the Directorate General of Civil Aviation Ministry of Transportation arrived Air Force Base (air base) around Medan Polonia Airport, on Saturday (1/10/2011) morning. Preparation for the crash site being prepared.Chairman of the Subcommittee on Air NTSC, Masruri, has not received sufficient preliminary data related to possible causes of the accident. Planned, the team will soon be the location of the NTSC and will investigate further."Today's plan will be to the location if weather conditions are good," said Masruri.NTSC team effort to the crash site relies heavily on weather conditions. Basarnas evacuation team that has been seeking to enter the site had several failed location by helicopter. Although successful in reducing personnel, helicopter landing remains difficult because there is no open area around the site.
sumber:detik.com
CASA 212 aircraft throughout Passengers Killed
Indonesian rescue team said the 18 passengers in a plane that crashed in Sumatra were killed.
Spanish-made CASA 221 aircraft was flying from Medan to Aceh province on Thursday, when the plane was sending an emergency signal and then disappeared from radar.
Hopes rise that perhaps there is a passenger who survived when the rescue team saw the wreckage from the air on Friday and said the fuselage was intact and an open door.
Search and Rescue team said the 14 passengers and four crew members was found in a sitting position in aircraft seats. Among the dead included four children.
Spanish-made CASA 221 aircraft was flying from Medan to Aceh province on Thursday, when the plane was sending an emergency signal and then disappeared from radar.
Hopes rise that perhaps there is a passenger who survived when the rescue team saw the wreckage from the air on Friday and said the fuselage was intact and an open door.
Search and Rescue team said the 14 passengers and four crew members was found in a sitting position in aircraft seats. Among the dead included four children.
The Beech 35 Bonanza
Photos
Powerplants
D35 - One 153kW (205hp) Continental E18511 flat six piston engine driving a two blade constant speed propeller. P35 - One 195kW (260hp) fuel injected Continental IO470N. V35TC - One 210kW (285hp) turbocharged and fuel injected Continental TSIO520D.
Performance
D35 - Max speed 306km/h (165kt), cruising speed 281km/h (152kt). Initial rate of climb 1100ft/min. Range with no reserves 1247km (673nm). P35 - Max speed 330km/h (178kt), cruising speed 306km/h (165kt). Initial rate of climb 1150ft/min. Range with optional fuel and no reserves 1955km (1056nm). V35TC - Max speed 386km/h (208kt), max cruising speed 360km/h (194kt), long range cruising speed 262km/h (141kt). Initial rate of climb 1225ft/min. Range with standard fuel and reserves 917km (495nm), with opt fuel 1770km (955nm).
Weights
D35 - Empty 760kg (1675lb), max takeoff 1236kg (2725lb). P35 - Empty 841kg (1855lb), max takeoff 1418kg (3125lb). V35TC - Empty 907kg (2000lb), max takeoff 1542kg (3400lb).
Dimensions
D35 - Wing span 10.00m (32ft 10in), length 7.67m (25ft 2in). Wing area 16.5m2 (177.6sq ft). P35 - Wing span 10.20m (33ft 6in), length 7.65m (25ft 1in). Wing area 16.8m2 (181sq ft). V35TC - Wing span 10.20m (33ft 6in), length 8.04m (26ft 5in), height 2.31m (7ft 7in). Wing area 16.8m2 (181sq ft).
Capacity
Models 35 through to J35 seat four people, K35 optional fifth passenger, later models from S35 onwards six people.
Production
Approximately 10,400 Model 35 Bonanzas of all variants were built between 1945 and 1982.
Type
Four & six seat high performance light aircraft
History
The distinctive Model 35 Bonanza is one of general aviation's most famous and prolific types, and enjoyed a production life spanning four decades.
The Bonanza first flew on December 22 1945. Featuring metal construction, retractable undercarriage and high performance, it heralded a new class of high performance GA aircraft. The design also featured the distinctive Vtail, incorporated for aerodynamic efficiency and reduced weight. Deliveries of production aircraft began in 1947.
Subsequent development led to a significant family of subtypes. Briefly these are the A35 of 1949 with a greater max takeoff weight; the B35 with a 146kW (196hp) E1858 engine; the 153kW (205hp) E18511 powered C, D and E models through to 1954; the F and G35 with third cabin window and 170kW (225hp) E2258 of the mid fifties; the 180kW (240hp) Continental O470G powered H35 of 1957; the fuel injected 187kW (250hp) powered J35; 1960's M35 with larger rear windows; and the N35 and P35 with a 195kW (260hp) IO470N and greater max takeoff weight.
Then followed the redeveloped S35 of 1964 with six seats and redesigned rear cabin, optional three blade prop, 215kW (285hp) IO520B engine and yet greater weights; the heavier V35 of 1966; and turbocharged V35TC; V35A and V35ATC of 1968 with more raked windscreen; and the V35B and V35BTC (just seven built) from 1970. The V35B remained in production until 1982 and underwent a number of detail changes in that time.
More photos of Beech 35 Bonanza
More cockpit photos...
D35 - One 153kW (205hp) Continental E18511 flat six piston engine driving a two blade constant speed propeller. P35 - One 195kW (260hp) fuel injected Continental IO470N. V35TC - One 210kW (285hp) turbocharged and fuel injected Continental TSIO520D.
Performance
D35 - Max speed 306km/h (165kt), cruising speed 281km/h (152kt). Initial rate of climb 1100ft/min. Range with no reserves 1247km (673nm). P35 - Max speed 330km/h (178kt), cruising speed 306km/h (165kt). Initial rate of climb 1150ft/min. Range with optional fuel and no reserves 1955km (1056nm). V35TC - Max speed 386km/h (208kt), max cruising speed 360km/h (194kt), long range cruising speed 262km/h (141kt). Initial rate of climb 1225ft/min. Range with standard fuel and reserves 917km (495nm), with opt fuel 1770km (955nm).
Weights
D35 - Empty 760kg (1675lb), max takeoff 1236kg (2725lb). P35 - Empty 841kg (1855lb), max takeoff 1418kg (3125lb). V35TC - Empty 907kg (2000lb), max takeoff 1542kg (3400lb).
Dimensions
D35 - Wing span 10.00m (32ft 10in), length 7.67m (25ft 2in). Wing area 16.5m2 (177.6sq ft). P35 - Wing span 10.20m (33ft 6in), length 7.65m (25ft 1in). Wing area 16.8m2 (181sq ft). V35TC - Wing span 10.20m (33ft 6in), length 8.04m (26ft 5in), height 2.31m (7ft 7in). Wing area 16.8m2 (181sq ft).
Capacity
Models 35 through to J35 seat four people, K35 optional fifth passenger, later models from S35 onwards six people.
Production
Approximately 10,400 Model 35 Bonanzas of all variants were built between 1945 and 1982.
Type
Four & six seat high performance light aircraft
History
The distinctive Model 35 Bonanza is one of general aviation's most famous and prolific types, and enjoyed a production life spanning four decades.
The Bonanza first flew on December 22 1945. Featuring metal construction, retractable undercarriage and high performance, it heralded a new class of high performance GA aircraft. The design also featured the distinctive Vtail, incorporated for aerodynamic efficiency and reduced weight. Deliveries of production aircraft began in 1947.
Subsequent development led to a significant family of subtypes. Briefly these are the A35 of 1949 with a greater max takeoff weight; the B35 with a 146kW (196hp) E1858 engine; the 153kW (205hp) E18511 powered C, D and E models through to 1954; the F and G35 with third cabin window and 170kW (225hp) E2258 of the mid fifties; the 180kW (240hp) Continental O470G powered H35 of 1957; the fuel injected 187kW (250hp) powered J35; 1960's M35 with larger rear windows; and the N35 and P35 with a 195kW (260hp) IO470N and greater max takeoff weight.
Then followed the redeveloped S35 of 1964 with six seats and redesigned rear cabin, optional three blade prop, 215kW (285hp) IO520B engine and yet greater weights; the heavier V35 of 1966; and turbocharged V35TC; V35A and V35ATC of 1968 with more raked windscreen; and the V35B and V35BTC (just seven built) from 1970. The V35B remained in production until 1982 and underwent a number of detail changes in that time.
The Beech 2000 Starship 1
Photos
Powerplants
Two 895kW (1200shp) Pratt & Whitney Canada PT6A67As, driving five blade constant speed McCauley propellers.
Performance
2000 - Max cruising speed 622km/h (335kt), economical cruising speed 546km/h (295kt). Initial rate of climb 3225ft/min. Max range 2630km (1634nm). 2000A - Max cruising speed 621km/h (335kt), economical cruising speed 570kt (307kt). Initial rate of climb 2748ft/min. Range with reserves 2920km (1576nm).
Weights
2000 - Empty equipped 4484kg (9887lb), max takeoff 6531kg (14,400lb). 2000A - Empty equipped 4574kg (10,085lb), max takeoff 6758kg (14,900lb).
Dimensions
Wing span 16.60m (54ft 5in), length 14.05m (46ft 1in), height 3.94m (12ft 11in). Wing area 26.1m2 (280.9sq ft).
Capacity
Flightcrew of one or two pilots. Standard passenger layout for eight in 2000 or six in 2000A.
Production
Production ceased in early 1995 after three prototypes, 18 Starship 2000s and 32 Starship 2000As had been built
Type
Advanced technology corporate transport
History
Despite its extensive use of modern technologies and innovative design the Starship was a commercial failure.
Conceived as a new generation light corporate transport in the King Air class, the Starship traces back to the 85% scale proof of concept demonstrator built by Scaled Composites, which first flew in August 1983. The prototype Starship 2000 proper made its first flight on February 26 1986, provisionally powered by PT6A65 turboprops. A second prototype equipped with Collins avionics entered the flight test program in June 1986, while a third development aircraft took flight in January 1987. Initial US FAA certification was awarded on June 14 1988, while the first production example was flown on April 25 1989.
The unconventional Starship design incorporates many innovations. Foremost of these is its rear mounted laminar flow wing and variable geometry canards or foreplanes. The foreplanes sweep forward with flap extension for pitch trim compensation, designed to make it impossible for the Starship to stall on takeoff or landing.
The wing itself is constructed almost entirely of composites (something which attracted much criticism because of the associated difficulties of inspecting it thoroughly), and has tip mounted tails. The rear mounted engines are in a pusher arrangement, being behind the cabin noise is reduced, while their relatively close proximity to each other also improves single engine handling. The EFIS flightdeck has Collins avionics with early generation colour and monochrome CRTs.
The improved Starship 2000A was certificated in April 1992. It introduced changes including seating for six instead of eight, a slightly higher max takeoff weight and increased range.
A lack of customer interest forced Beech to terminate Starship production in early 1995 after just 53 had been built (including three prototypes), a somewhat inglorious end to a technologically innovative and promising design.
More photos of Beech 2000 Starship 1
Two 895kW (1200shp) Pratt & Whitney Canada PT6A67As, driving five blade constant speed McCauley propellers.
Performance
2000 - Max cruising speed 622km/h (335kt), economical cruising speed 546km/h (295kt). Initial rate of climb 3225ft/min. Max range 2630km (1634nm). 2000A - Max cruising speed 621km/h (335kt), economical cruising speed 570kt (307kt). Initial rate of climb 2748ft/min. Range with reserves 2920km (1576nm).
Weights
2000 - Empty equipped 4484kg (9887lb), max takeoff 6531kg (14,400lb). 2000A - Empty equipped 4574kg (10,085lb), max takeoff 6758kg (14,900lb).
Dimensions
Wing span 16.60m (54ft 5in), length 14.05m (46ft 1in), height 3.94m (12ft 11in). Wing area 26.1m2 (280.9sq ft).
Capacity
Flightcrew of one or two pilots. Standard passenger layout for eight in 2000 or six in 2000A.
Production
Production ceased in early 1995 after three prototypes, 18 Starship 2000s and 32 Starship 2000As had been built
Type
Advanced technology corporate transport
History
Despite its extensive use of modern technologies and innovative design the Starship was a commercial failure.
Conceived as a new generation light corporate transport in the King Air class, the Starship traces back to the 85% scale proof of concept demonstrator built by Scaled Composites, which first flew in August 1983. The prototype Starship 2000 proper made its first flight on February 26 1986, provisionally powered by PT6A65 turboprops. A second prototype equipped with Collins avionics entered the flight test program in June 1986, while a third development aircraft took flight in January 1987. Initial US FAA certification was awarded on June 14 1988, while the first production example was flown on April 25 1989.
The unconventional Starship design incorporates many innovations. Foremost of these is its rear mounted laminar flow wing and variable geometry canards or foreplanes. The foreplanes sweep forward with flap extension for pitch trim compensation, designed to make it impossible for the Starship to stall on takeoff or landing.
The wing itself is constructed almost entirely of composites (something which attracted much criticism because of the associated difficulties of inspecting it thoroughly), and has tip mounted tails. The rear mounted engines are in a pusher arrangement, being behind the cabin noise is reduced, while their relatively close proximity to each other also improves single engine handling. The EFIS flightdeck has Collins avionics with early generation colour and monochrome CRTs.
The improved Starship 2000A was certificated in April 1992. It introduced changes including seating for six instead of eight, a slightly higher max takeoff weight and increased range.
A lack of customer interest forced Beech to terminate Starship production in early 1995 after just 53 had been built (including three prototypes), a somewhat inglorious end to a technologically innovative and promising design.
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