Macready Field/Merced Municipal Airport, Merced, CA
Airport History:
Merced Macready Airport Today
Special Events:
Airport Area Accident History:
Accident occurred
Monday, August 31, 2009 in Merced, CA
Probable Cause Approval Date: 12/15/2009
Aircraft: CESSNA 152, registration: N5155B
Injuries: 1 Uninjured.
During the landing flare for a full-stop landing, the airplane touched down
hard, and bounced into the air. The student pilot attempted to arrest the
descent, but the airplane's nose wheel hit the runway surface with sufficient
force to collapse the nose gear strut and to damage the firewall.
Accident occurred Tuesday, May 15, 2007 in
Merced, CA
Probable Cause Approval Date: 7/25/2007
Aircraft: Aircraft Mfg & Dev. Co. (AMD) CH 2000,
registration: N363AM
Injuries: 2 Uninjured.
The flight instructor said the instructional
flight was to prepare the student for his stage two check, which was to be
followed by his first solo flight. The student had received 41.2 hours of
instruction, with 5.4 hours in this make/model aircraft. The flight instructor
had planned for a simulated engine failure after takeoff; it was the flight
instructor's first practice simulated engine failure after takeoff in this
make/model aircraft. He pulled the throttle to idle, but the student held the
yoke in the climb attitude as opposed to nosing the airplane down for best glide
speed. The flight instructor said that he realized the airspeed was low and the
aircraft was in a high rate of descent, but his remedial attempts did not
prevent a hard landing . The airplane's firewall was wrinkled, and the empennage
and horizontal stabilizer were bent. The National Transportation Safety Board
determines the probable cause(s) of this accident as follows: The student
pilot's inadvertent stall/mush during a simulated power loss after takeoff and
the flight instructor's delayed remedial action, which resulted in a hard
landing. A contributing factor was the flight instructor's lack of familiarity
with the make/model of aircraft. ===
Accident occurred Wednesday, April 19, 2006 in
Merced, CA
Probable Cause Approval Date: 8/29/2006
Aircraft: Cessna 152 , registration: N757GF
Injuries: 2 Uninjured.
The airplane settled to the ground during an
attempted go-around from a bounced landing. The certified flight instructor
(CFI) said that the accident occurred following the student's bounced landing on
runway 30 and attempted go-around. The student applied full engine power,
retracted the wing flaps to the 10-degree setting, turned the carburetor heat
off, and lost directional control of the airplane. The CFI reported that the
airplane yawed violently left, at which point he took the flight controls from
his student while the airplane was still in ground effect . The CFI decided to
continue the go-around procedure, but he was not able to salvage the maneuver,
and the airplane continued a slow descent to the ground. The CFI further
reported that the airplane touched down on the ground adjacent to the runway.
Thereafter, directional control was lost and the airplane was substantially
damaged when the left wing impacted the ground. At the time of the occurrence,
the wind speed was 3 knots. The CFI had been a flight instructor for about 6
months prior to the accident.
The National Transportation Safety Board
determines the probable cause(s) of this accident as follows: the failure of the
student and certified flight instructor to maintain directional control and
obtain/maintain an adequate airspeed during the attempted go-around. The flight
instructor's inadequate supervision of the flight was also causal. ===
Accident occurred Tuesday, August 05, 2003 in
Merced, CA
Probable Cause Approval Date: 12/28/2004
Aircraft: Bell 206B, registration: N9254Y
Injuries: 3 Uninjured.
The pilot reported he was landing on a concrete
pad at a construction site . The helicopter was not positioned completely on the
concrete landing pad, and the aft section of the skids were hanging off the pad.
While lowering the collective, the helicopter rocked back and the tail rotor
skid touched the ground. The pilot abruptly attempted to pull the helicopter
back into a hover, and the helicopter moved forward and started to roll to the
right. The pilot was unable to stop the rolling movement, and the helicopter
struck the ground, coming to rest on its right side. The National Transportation
Safety Board determines the probable cause(s) of this accident as follows: The
pilot's excessive movement of the helicopter's controls during an aborted
landing, which resulted in a loss of control (dynamic rollover) and an in-flight
collision with terrain. ===
Accident occurred Friday, August 31, 2001 in
Merced, CA
Probable Cause Approval Date: 5/28/2002
Aircraft: Funk Aircraft Co. C, registration:
N22694
Injuries: 1 Uninjured.
The pilot stated that he had departed the Merced
airport approximately 1400. He climbed upwind until reaching an indicated
altitude of 700 feet, and then began a left turn to 210 degrees for an on-course
heading to Frazier Lake. At this point, he began to feel a slight loss of engine
power, followed by a slow reduction of engine power, which eventually reached a
nearly wind milling condition. He pumped the throttle, but the engine did not
respond. He attempted to return to the airport, but realized he was too far away
to land on the runway. He landed in a plowed field, where the airplane nosed
over. According to the pilot, the wing tanks were empty at the time of
departure, and the only tank in use was the fuselage tank. He stated that a
possible cause of the engine failure was the use of a non-vented fuel tank cap .
A post accident examination of the engine revealed the only discrepancy was a
non-vented fuel cap on the fuselage tank. As fuel was being drained from the
tank through the carburetor the drain flow ceased. The fuselage fuel tank cap
was removed, a vacuum sound was heard, and the drain flow began again. The pilot
stated he had switched the fuselage fuel tank cap prior to the last annual
inspection that occurred 6 months and 8 hours prior to this flight. The National
Transportation Safety Board determines the probable cause(s) of this accident as
follows: The pilot's improper modification of the airplane when he switched a
non-vented fuel cap to the fuselage tank. A factor was the inadequate annual
inspection.
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