B_Ambuj wrote:Henrik,
Do you mind referring to the link below :
http://en.wikipedia.org/wiki/Accidents_ ... _39_Gripen
Of the Multiple number of incidents involving Grippen, the below mentioned ones do not seem to be pilot induced. Most of them depicts the inherent inability of Grippen. Most of the incidents are quite recent.
As you will see below, most of the incidents was caused by man, not machine. For heavens sake, all the reasons behind the incidents are on the same page as the one you copied from! Either you are just being ignorant and desperately trying to pick a fight, or you just lie in hope everyone will believe you.
January 2011
On 12 January 2011, a Gripen from F 17 Kallinge slid off the hard surface when taxiing after landing.
Iced down runway,
plane was back in the air two days later.
May 2010
On 31 May 2010, a Gripen from F 21 Luleå came loose and sped away during an engine test.
Stupid mechanic had put the throttle in the wrong position.
August 2009
On 6 August 2009, a Gripen from F 17 Kallinge belly-landed after a routine mission and skidded off the runway.
Pilot forgot to extend the landing-gear.
November 2008
On 17 November 2008, the landing gear of a Swedish Air Force Gripen collapsed after landing at F 17 Kallinge. The pilot was on a routine mission.
On 17 November 2008, the landing gear of a Swedish Air Force Gripen collapsed after landing at F 17 Kallinge. The pilot was on a routine mission, when he received an error indication. He decided to abort the mission and return to the airfield. When taxiing, he felt that the brakes did not work properly, so he decided to stop as soon as possible. As the engine was switched off, the front landing gear suddenly collapsed, and the aircraft fell on its nose. The pilot escaped unharmed.
http://en.wikipedia.org/wiki/Accidents_ ... _39_Gripen
Do not make it sound more dramatic than it actually was. A minor mechanical failure, it just showed that the warning-systems worked properly.
April 2007
On 19 April 2007, a JAS 39C Gripen (serial no 39-259) from Airwing F 21 Luleå crashed at the Vidsel airfield in northern Sweden. The pilot, Stefan Kaarle, was involuntarily ejected out of the aircraft in mid-air while approaching the airstrip in order to land.
A design flaw after modifications in the cockpit. It was the G-suit that somehow had activated the ejection-seat. The problem was solved afterwards.
June 2005
On 1 June 2005, a JAS 39A Gripen (serial no 39-184) from Airwing F 17 Kallinge, when acting as a target in a dogfight exercise, apparently ceased to obey commands from the pilot.
Pilot error.
SHK's investigation — report published in June 2007 — showed that the aircraft initially travelled at Mach 0.6 in a shallow dive at an altitude of 5500 m. When attacked, the pilot, not fully aware of the rather low speed, tried to escape by taking the plane into a steep (60 degrees) climb. This led to a "low speed"-warning, for which the pilot tried to compensate by lighting the afterburner and manoeuvering into an offset looping, briefly applying maximum angle of attack. The intent was to regain speed at the top of the loop. However, the speed was too low, and the aircraft ended up in an inverted (upside-down) superstall, and started to descend slowly.
While there are measures to get out of this situation, those taken by the not-fully-trained pilot were either inadequate, insufficient or counter-productive, and he ultimately had to abandon the aircraft
http://en.wikipedia.org/wiki/Accidents_ ... _39_Gripen
September 1999
On 20 September 1999, a JAS 39A Gripen (serial no 39-156) from Airwing F 7 Såtenäs crashed into Lake Vänern during a dogfight exercise. After passing through the wake vortex of the other aircraft, the aircraft abruptly changed course.
The crash-report.
The Swedish Accident Investigation Board (SHK) could not fully determine the cause of the crash until the black box was found some 15 months later. The preliminary report is available in English.[3]
SHK's final report — not available in English — concluded that the plane had passed through the other aircraft's wake vortex while in a steep (−70 degrees) dive. When passing, the pilot's pitch command was "up", but instead the vortex inflicted a large aerodynamic transient on the aircraft, throwing it down into an almost vertical (−85 degrees) dive. These factors combined to create an angle of attack that was too large for the command to be obeyed, and so the ground-collision warning system alerted the pilot that a turn to avoid a crash would require more than 10 g. He then chose, in full accordance with the flight manual, to eject. At the same moment, however, the vortex effect ceased as suddenly as it had appeared, instantly reducing the angle of attack to within limits, and thus the plane was flyable again, and could in theory have been saved.
The flight status in the moment of ejection was: altitude 750 m, flight angle −75 degrees, speed 350 km/h, angle of attack −8 degrees, and load −1.5 g
http://en.wikipedia.org/wiki/Accidents_ ... _39_Gripen
This could have happened to any fighter-aircraft. As stated above, if the pilot was a little more cool-headed, the plane could have been saved.
If you copied all that from Wikipedia, why didn't you also copy the stated reasons behind the incidents? I used the information from the very same page as you.
Maybe you just wanted it to look more dramatic?