Fatal T-6 Plane Crash in Santa Rosa, Florida - 3/6/2010
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.
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!:
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:
pete ruppert photography, division flyyy, sky monkeys,
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)
No airplanes were damaged during the filming of this movie.
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."