The pilot was on final approach when the engine started to run out of fuel. She said her boss
had a similar problem on a previous flight, and had to correct for it by pitching the nose up and
down to force fuel into the fuel lines. The pilot recalled pitching the nose up and down but
nothing after that. A witness, who saw the airplane pitching up and down several times before
it impacted the ground, responded to the crash. He noted that the fuel selector was set to the
"both" position and no fuel was leaking from either fuel tank’s gas cap. When the
airplane was righted, the witness said he saw several gallons of fuel drain from the left tank but
not the right tank. When he visually checked the right fuel tank, it was empty. The left tank had
about 9 gallons (about 6.5 gallons usable) still in the tank. A postaccident examination of the
airplane by a Federal Aviation Administration inspector revealed the airplane sustained
substantial damage to the firewall, forward engine mounts, right wing and vertical stabilizer
and rudder. About 6 gallons of fuel was drained from the left wing tank and the right tank was
empty. A review of the terrain where the airplane impacted the ground revealed the vegetation
around the left tank was discolored from fuel, but the area around the right tank was not. No
pre mishap mechanical discrepancies were noted with the engine or airplane that would have
precluded normal operation.
Category: C-182
According to the pilot’s report, he leveled the airplane about 11,000 feet and established a speed of 80 mph with 10 degrees of flaps extended. When the last skydiver exited the airplane, its nose pitched up. The pilot pushed forwarded on the control wheel and added full engine power
The pilot reported that, during the descent, he applied carburetor heat but that he then removed
carburetor heat when leveling off. The pilot reduced the throttle to slow the airplane while on final
approach. When he advanced the throttle to maintain airspeed, the engine power did not increase; the
pilot was unable to restore full engine power. The engine subsequently lost all power when the pilot
applied carburetor heat. During the forced landing to a field, the nose landing gear and propeller
contacted a barbed wire fence, and the airplane then nosed down, impacted the ground, and nosed over.
A postaccident examination revealed no mechanical failures that would have resulted in the loss of
engine power. The atmospheric conditions at the time of the accident were conducive to the formation of
serious carburetor icing at glide power. It is likely that carburetor ice developed after the pilot reduced
the engine power/closed the throttle while in the traffic pattern without applying carburetor heat, which
resulted in a loss of engine power. The manufacturer’s before landing checklist states to apply carburetor
heat before closing the throttle.
A Cessna 182L (182), the lead airplane, and a Cessna 185F (185), the trail airplane, collided during a
formation skydiving flight. Both pilots flew the airplanes in a rectangular pattern until they reached the
jump altitude of 12,700 ft mean sea level. The 182 pilot established a jump heading and visually
confirmed that the 185 was to the left side and aft of the 182. The 182 pilot then called out “door open”
and jumpers “climbing out.” Subsequently, the four skydivers on board the 182 climbed out onto the
airplane’s right wing strut and right wheel step. Almost immediately, the 182 was struck by the 185. The
182’s windshield was shattered, and the airplane entered an uncontrollable descent. During the descent,
the right wing separated from the airplane, and the right wing fuel tank exploded. The 182 pilot exited
the airplane and parachuted safely to the ground. The 185 pilot reported that “when it was time for the
skydivers to climb out, the two planes began to drift together and in seemingly no time at all, the two
were colliding.” After the collision, the skydivers on board the 185 jumped from the airplane as it
inverted; the pilot was able to recover the airplane and land.
Video of the collision from NBC News
DD.com Blog discussion.
The pilot reported that he was making a circling descent to the airport after dropping parachutists and
that he used carburetor heat during the descent. As the pilot was on the base leg of the landing pattern,
close to the turn onto the final leg, the engine lost power. The pilot landed the airplane short of the
runway, and the firewall buckled and the nose landing gear bent forward. The operator later functionally
tested the engine and it operated normally.
The pilot reported that, while on final approach, he performed the landing checklist and confirmed that
the carburetor heat was on. About 100 feet above ground level, he advanced the throttle; however, the
engine did not respond. The pilot verified that the mixture, throttle, and propeller setting were in the fullforward
position, but, despite his efforts, the engine would not restart. He subsequently initiated a forced
landing to an open area. During the landing, the airplane impacted a ditch and nosed over. Seven gallons
of fuel were found in the right fuel tank, and 11 gallons of fuel were found in the left fuel tank. A
postaccident examination and operational run of the recovered engine revealed no evidence of
mechanical malfunctions or failures that would have precluded normal operation. Although the reported
weather conditions at the time of the accident were conducive to the accumulation of carburetor icing at
glide power, the pilot reported that he used carburetor heat, which would have prevented the
accumulation of ice. The reason for the loss of engine power could not be determined.
The pilot reported that he had flown a group of skydivers to altitude for an intentional
parachute jump about 3 miles north of the airport and was returning for landing at the time of
the accident. The airplane was on final approach when the engine lost power. The pilot’s
attempts to restore engine power were unsuccessful, and he ditched the airplane into a lake
short of the runway. The pilot reported using carburetor heat during the descent; however, the
pilot did not periodically apply engine power (clear the engine) during the descent. According
to FAA Advisory Circular 20-113, Pilot Precautions and Procedures to be Taken in Preventing
Aircraft Reciprocating Engine Induction System and Fuel System Icing Problems, "Heat
should be applied for a short time to warm the induction system before beginning a prolonged
descent with the engine throttled and left on during the descent. Power lever advancement
should be performed periodically during descent to assure that power recovery can be
achieved." A postaccident engine examination did not reveal any anomalies consistent
with a preimpact failure or malfunction. Local weather conditions were conducive to the
formation of carburetor icing.
The pilot reported that the purpose of the accident flight was to release four skydivers at
10,500 feet mean sea level (msl). The pilot reported that, before the accident flight, he used a
calibrated dipstick to determine how much fuel was on board the airplane. The left and right
fuel tanks contained 10 and 5 gallons of fuel, respectively. He noted that the skydiving flight
typically took a single pass over the landing zone, which required about 20 to 25 minutes of
flight time and 8 gallons of fuel; however, the accident flight required two passes over the
landing zone at 10,500 feet msl, which added about 2 to 5 minutes to the accident flight. He
reported that the flight climbed to 10,500 feet msl and the skydivers were released without any
anomalies or malfunctions with the airplane. The pilot immediately initiated a descent to
reenter the traffic pattern at the departure airport, and the airplane experienced a loss of
engine power while on the downwind leg. A helicopter was approaching the airport at a similar
altitude, which delayed the turn onto the base leg. Believing he had insufficient altitude to
reach the runway, the pilot performed a forced landing to a field. The nose landing gear
collapsed shortly after touchdown, and the airplane subsequently nosed over. Following the
accident, the pilot reported to several individuals that the airplane "ran out of fuel,"
which resulted in the loss of engine power while in the traffic pattern. Additionally, the pilot
stated that there were no mechanical issues with the engine before the loss of engine power.
During a postaccident examination, 3.5 gallons of fuel were recovered from the airplane.
According to the Pilot Operating Handbook, the airplane has 3 gallons of unusable fuel
while operating in level flight and 10 gallons of unusable fuel while in flight attitudes other
than level flight; therefore, the airplane did not have enough fuel for the accident flight.
According to the pilot, he leveled the airplane at 8,500 feet for a tandem skydive. When the instructor
exited the airplane, the nose pitched up, then the airplane pitched over into a right, descending turn. The
pilot assessed the situation and determined that the right horizontal stabilizer was bent. He later
determined that the instructor’s drogue chute became trapped under the flap handle, resulting in a
premature deployment of the parachute. The drogue chute then caught the horizontal stabilizer, resulting
in a 45-degree downward bend. The pilot reported no pre-impact mechanical malfunctions or failures
with the airplane that would have precluded normal operation.
As a skydiver was exiting the airplane, his parachute inadvertently deployed and struck the
right horizontal stabilizer. He deployed his reserve parachute and landed without further
incident. After all the skydivers had exited the airplane, the pilot saw that the right horizontal
stabilizer and elevator were damaged. After an uneventful landing, postaccident examination
revealed the right stabilizer spar was bent.
The pilot was returning to the airport after dropping off parachutists at 9,000 feet. He said that
the flight lasted about 30 minutes, and as he turned onto final approach in the traffic pattern,
he pulled the throttle back, and the engine lost power. The pilot performed a forced landing in
a field, and the airplane struck some power poles lying on the ground, resulting in substantial
damage to the airframe. Postaccident examination of the airframe and engine revealed no
evidence of a mechanical malfunction or anomaly that would have precluded normal
operation. Only residual fuel was recovered from the wing tanks, and there was no fuel in the
line from the tanks to the engine. The pilot stated that he should have monitored his fuel
gauges more closely.
The pilot reported that, during the final leg of the approach, the airplane was above the
intended approach path and speed. Over the threshold of the runway, the airplane encountered
a gust of wind. The pilot announced on the common traffic advisory frequency his intention to
perform a go-around maneuver. He was unable to perform the maneuver prior to the hard
landing; he then proceeded to overrun the runway and the airplane nosed over, which resulted
in substantial damage to the left wing. The pilot reported that there were no mechanical
malfunctions or failures with the airplane that would have precluded normal operation. The
recorded wind at the airport about the time of the accident was variable at 4 knots and for the
hour before and an hour after the accident the wind was recorded as calm.
The pilot stated that he departed the airport for the 15-minute skydiving flight with about 20
gallons of fuel onboard. After completing a jump run, he was returning to the airport and
maneuvered the airplane on final approach. When the airplane was about 3 miles from the
runway and about 1,200 feet above ground level, the engine experienced a partial loss of
power. The pilot configured the airplane for the best glide speed, and, shortly thereafter, the
engine quit producing any power. The airplane subsequently collided with trees in an orchard
about 600 yards from the approach end of the runway.
The pilot stated that, before starting the engine by manually rotating the propeller, he set the
brakes, throttle, and trim. He exited the airplane and proceeded to rotate the propeller. When
the engine started, it went to full rpm, and the airplane started to move forward on the taxiway
at a high speed. The airplane veered off the taxiway and continued its high speed taxi until it
impacted a hangar door, damaging the engine, both wings, and the right main landing gear.
The pilot reported that he had not chocked the airplane and thought the brake was set. He
further reported there were no mechanical problems with the airplane.
The pilot reported that he was descending to land after his final flight of the day. The airplane was about 1,500 to 1,700 feet above ground level and about 1.25 miles from the airport when the engine lost total power. The pilot made an emergency landing to an open field, and the airplane sustained substantial damage to the fuselage.
The pilot stated that he was descending the airplane from an altitude of 8,000 feet after releasing skydivers. During the descent, at an altitude of about 3,000 feet, the airplane’s door opened and contacted the underside of the wing. The pilot slowed the airplane and attempted to close the door but noticed that the door had warped and that the window was missing.
On August 9, 2011, about 1714 mountain daylight time, a Cessna 182, N8718T, landed in a field while on approach to Boulder Municipal Airport (KBDL). The aircraft was substantially damaged and came to rest after striking a tree on the north side of the field.
The pilot stated that he fueled the airplane for two flights with skydivers and thirty minutes of reserve fuel. He further stated that during the second approach he had to adjust his intended flight path for other airplane traffic. Then, as the pilot decreased the pitch of the airplane on final approach, the engine sputtered and lost power.
According to the pilot, as he taxied the airplane to the runway for takeoff, the left main landing gear collapsed. Examination revealed that the left main landing gear had fractured and completely separated from the airplane about 6 inches outboard of its attachment point at the airframe.
The pilot flew four skydiving flights without refueling. On the last flight, after the skydivers exited the airplane, the pilot initiated a descent and the airplane experienced a total loss of engine power. The pilot knew he could not make it back to the airport and made a forced landing to a gravel area.
The flight departed to the east with four skydivers for a local jump. One witness stated that, immediately following the takeoff, about 200 feet above ground level, a “percussive” pop from the engine was heard. Two witnesses stated that the right wing dropped, and the airplane impacted the ground.
During flight at 10,000 feet above ground level, the engine began to vibrate and run rough. Shortly thereafter, a loud bang occurred and oil was present on the windscreen. The pilot attempted a forced landing, and during the forced landing, the airplane landed short of the runway and impacted a ditch.
The pilot was departing from a soft, dry, 2,200-foot turf airfield using soft/short field procedures. After becoming airborne, the airplane settled back onto the runway, became airborne, and settled onto the runway a second time. At this time the right main wheel separated and the landing gear strut dug into the terrain spinning the airplane around and bringing it to an abrupt stop.
The airplane landed from a skydiving flight with a remaining passenger after three parachutists had jumped from the airplane. The engine was not shut down and the airplane was pointed toward the vehicle waiting for the passenger to deplane. When the passenger exited the airplane, a ground crewmember leaned toward the airplane to talk to the pilot while the passenger went around the right side of the airplane.
The pilot stated that after departure and climbing to approximately 200 feet, the engine lost power and the airplane began to descend. During the forced landing the airplane struck a power line and impacted terrain resulting in substantial damage.