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Fatal T-6 Plane Crash in Santa Rosa, Florida - 3/6/2010

martialv.blogspot.com On March 6, 2010, at 1236 central standard time, a North American SNJ-6, N47LF, was destroyed when it impacted the Gulf of Mexico about 1 mile south of Topsail Hill Reserve State Park, Santa Rosa Beach, Florida. The certificated commercial pilot and the passenger were fatally injured. Visual meteorological conditions prevailed. The airplane, part of a five-airplane formation, was not operating on a flight plan. The personal flight was being conducted under the provisions of 14 Code of Federal Regulations Part 91.


 


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Air Show Crashes | Air Show compilation part # 4
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T-6 Landing Mishap (check update vid: 'T-6 Landing Mishap - Explanation!')
check update vid: T-6 Landing Mishap (Explanation!: http://www.youtube.com/watch?v=3xx0pV_AUQE north american t-6 texan landing mishap (after loss of tailwheel steering due to broken spring..), pilot walter eichhorn has pictures of broken spring laying in the tail after landing. if interested please feel free to contact walter on his privat phone: +4964348529 pete ruppert photography, division flyyy, sky monkeys, no casualties- glory2he LORDjesus!





Vintage Pair Crash, RAF Mildenhall 1986
ITN TV news report on crash of 'Vintage Pair' Meteor and Vampire at RAF Mildenhall Air Fete, Sunday 25th May 1986





Yak 52 Crash in Romania
Yak-52 with propeller trouble. crash and his pilot die 1994. taken From Chilean TV MEGAVISION Channel





SQ2 GOT STOL?
STOL Quest 2, aka SQ2, in action. If you are interested in the SQ2 please contact us for more information at www.alaska-stol-specialists.com or (302) GOT-STOL No airplanes were damaged during the filming of this movie.





B-52 flyover of 2010 Independence Bowl. Air Force vs Georgia Tech
B-52 flyover of 2010 Independence Bowl. Air Force vs Georgia Tech





Stearman Aircraft Crash Taildragger Airplane Tips Over As Pilot Applies Too Much Braking Power.
Stearman aircraft airplane crashes and ends up upside down because the pilot tried to slow too quickly and nosed the aircraft over.





USS Nimitz Catapult Takeoff Grumman C-2A
Video taken from the bridge of the USS Nimitz showing Grumman C-2A wings unfolding and catapult takeoff.





Ramstein air show accident
For more information about this go to : http://www.robert-stetter.de/Ramstein/ramstein.html Wiki page : http://en.wikipedia.org/wiki/Ramstein_airshow_disaster .





B-52 Crash at Fairchild Air Force Base
B-52 Crash at Fairchild Air Force Base in 1994.





180 Autorotation accident - Low rotor RPM
According to the pilot-in-command (PIC), he was performing autorotations at the lower part of the main rotor rpm green arc in part due to weight considerations. Upon entering the accident autorotation, he maintained an airspeed between 85-90 knots in the hope that extra speed would allow a more aggressive deceleration flare prior to touchdown, which should in turn further slow the rate of descent and forward speed. The helicopter's rate of descent was high, and as the PIC turned the helicopter onto the runway heading it was apparent to him that the rate of descent was excessive and that he was too low to execute either a proper deceleration flare or perform a power recovery. He attempted to level the helicopter as much as possible prior to impact to minimize the damage to the helicopter and prevent injury. The helicopter landed hard with the left skid contacting the runway first. The left skid collapsed, damaging the outboard landing gear damper attachment structure. The helicopter slid about 100 yards before coming to a stop. According to the manufacturer, the main rotor rpm range is 90 percent to 106.4 percent. At the helicopter's weight and the density altitude on the day of the accident, the main rotor rpm during the autorotation should have been above the 106.4 percent limit (red line), requiring the pilot to increase collective pitch to maintain the rotor rpm within limits. Performing autorotations at the lower part of the green arc provides less availability of rotor energy to perform an autorotation landing. The pilot should have recognized that he was not achieving the required main rotor rpm for the autorotations and terminated the maneuvers. The helicopter was within weight and balance limits. The National Transportation Safety Board determines the probable cause(s) of this accident as follows: The pilot's failure to maintain adequate main rotor rpm during an autorotation, which resulted in a hard landing.





Midair Collision - Aussie Bristol Beauforts collide and crash
A flight of three World War II Royal Australian (notBritish) Air Force Beauforts perform a picture-perfect low pass for the cameras when something goes terribly wrong. "The two Beauforts A9-27 and A9-268, of the RAAF's 8 OTU, collided over Jervis Bay on 14 April 1943 while performing a 'Prince of Wales' break for people of the media." "All eight crew members were killed when both aircraft hit the water: Crew of A9-27 F/O Raymond Sydney Green (Pilot), F/O Maurice Francis Hoban, F/Sgt Eric William Sweetnam, Sgt Albert John Bailey. Crew of A9-268 F/Lt David George Dey (Pilot), P/O Jack Norman, P/O Rex Lindsay Solomon, Sgt Hugh Sydney George Richardson."





2006-3-11_bob_hoover.avi





HQ: LOW-ASS A-10 FLY-BY!!
Pilot shows off a bit, The Hog where it belongs, down low, down and dirty, in the pen.





best helicopter crash ever




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