Ultralight aircraft accidents, experimental aircraft accidents, light sport aircraft accident reports 7 |
|||||
|
|||||
Controller: "Air Force 53, it appears your engine has... oh... disregard, I see you've already ejected." |
|||||
|
|||||
|
|||||
|
|||||
|
|||||
Ultralight Aircraft Accident Data |
|||||
THE EXPERIMENTAL AIRPLANE EXPERIENCED A POWER LOSS DURING CRUISE
FLIGHT. THE PILOT ATTEMPTED TO EXECUTE A FORCED LANDING IN A FRESHLY PLOWED FIELD, BUT
NOSED OVER IN THE SOFT SOIL. THE PILOT STATED THAT ALL HE COULD THINK OF IS CARB ICING. HE
STATED THAT THE TEMPERATURE WAS DROPPING FAST, WITH AIR TEMPERATURE AT 66 DEGREES F
(FAHRENHEIT), DEW POINT 38 DEGREES F. THE AIRCRAFT ENGINE IS NOT EQUIPPED WITH A
CARBURETOR HEAT SYSTEM. ACCORDING TO THE ICING PROBABILITY CHARTS, THE FLIGHT CONDITIONS
WERE SUCH THAT THE PROBABILITY FOR CARBURETOR ICING WAS HIGH DURING CRUISE AND GLIDING
FLIGHT. Accident occurred JUN-12-93 at GRAYSLAKE, IL JUST AFTER INITIAL TAKE-OFF, THE PILOT EXPERIENCED AN
"UNCONTROLLABLE TURN TO THE LEFT." THE PILOT REPORTED THE TURN "BACAME
STEEPER AND SOON WAS IN THE PROCESS OF PUTTING THE PLANE IN AN INVERTED POSITION."
THE AIRCRAFT IMPACTED THE GROUND, AND WAS DESTROYED BY AN ON-GROUND EXPLOSION AND FIRE.
POSTACCIDENT EXAMINATION REVEALED NO EVIDENCE OF PREIMPACT MECHANICAL MALFUNCTION WITH
AIRFRAME, ENGINE OR ACCESSORIES. Accident occurred JUN-12-93 at WHITE PIGEON, MI FOLLOWING AN ENGINE FAILURE ON APPROACH TO HIS PRIVATE GRASS
AIRSTRIP, THE PILOT TOUCHED DOWN 3/4 OF THE WAY DOWN THE RUNWAY, AND WAS UNABLE TO STOP
THE AIRPLANE BEFORE OVERRUNNING THE AIRSTRIP, CROSSING A DIRT ROAD AND FINALLY COMING TO
REST IN A SOYBEAN FIELD. Accident occurred JUL-18-93 at ALAMOGORDO, NM THE PROPELLER SEPARATED FROM THE HOMEBUILT AIRPLANE WHILE IN
CRUISE FLIGHT DUE TO THE SEIZURE OF THE PROPELLER SHAFT BEARING. DURING THE SUBSEQUENT
DOWNWIND FORCED LANDING TO AN OPEN FIELD THE PILOT OVERSHOT THE LANDING AREA AND THE
AIRPLANE IMPACTED THE TOP OF A BERM AND BOUNCED. THE WINDS AT THE TIME OF THE ACCIDENT
WERE FROM THE WEST AT TEN KNOTS, GUSTING TO 17 KNOTS. Accident occurred JUL-27-93 at PICKETT, WI THE FLIGHT DEPARTED ALMA, MICHIGAN AT 1305 CENTRAL DAYLIGHT TIME
WITH 30 GALLONS OF FUEL. AT 1645 THE AIRPLANE EXPERIENCED A TOTAL POWER LOSS AND A FORCED
LANDING WAS PERFORMED IN ROUGH TERRAIN ONE MILE WEST OF PICKETT, WISCONSIN, APPROXIMATELY
15 MILES SHORT OF THE INTENDED DESTINATION. NO USABLE FUEL WAS REMAINING IN EITHER FUEL
TANK. Accident occurred APR-04-94 at CLARKSBURG, WV THE AIRPLANE HAD JUST TAKEN OFF AND WAS IN ITS INITIAL CLIMB WHEN
CONTROL WAS LOST. THE AIRPLANE COLLIDED WITH TERRAIN IN AN UNCONTROLLED DESCENT. THE PILOT
STATED, "AFTER A GOOD PRE-FLIGHT THE TOWER CLEARED ME TO DEPART...IMMEDIATELY ON LIFT
OFF, THE AIRCRAFT JUMPED TO THE RIGHT. THERE WAS DEFINITELY A CONTROL PROBLEM BUT I HAVE
NOT PINPOINTED WHERE." THE FAA INSPECTOR'S POST ACCIDENT EXAMINATION REVEALED THE
BOLT CONNECTING THE TWO RODS IN THE AILERON PUSH/PULL ROD ASSEMBLY WAS MISSING. THE BOLT
HOLES IN BOTH RODS SHOWED NO DEFORMATION. ADDITIONALLY, THIS BOLT WAS CONNECTED WITH THE
JAM NUT FOUND LOOSE DURING THE CONFORMITY INSPECTION. THE AIRPLANE HAD A TOTAL OF 4 HOURS.
A CONFORMITY INSPECTION WAS PERFORMED BY AN FAA DESIGNATED AIRWORTHINESS REPRESENTATIVE
(DAR) ON NOVEMBER 29, 1993. THE DAR'S CONFORMITY INSPECTION REPORT STATED "JAM NUT
LOOSE ON AILERON CONTROL IN OVERHEAD." THE REPORT REVEALED THAT THE CORRECTIVE ACTION
TAKEN WAS THAT THE BOLT WAS "TIGHTENED." THE KIT MANUFACTURER SPECIFIES THE USE
OF A SELF LOCKING NUT, HOWEVER, THE PILOT USED A JAM NUT. Accident occurred JAN-23-94 at STAFFORD, KS THE PILOT WAS NOT QUALIFIED TO FLY THE AMATEUR BUILT AIRPLANE. HE
WAS NOT CERTIFICATED AS REQUIRED BY THE FAA, AND NO RECORD OF FORMAL TRAINING WAS CLAIMED.
THE PILOT STATED THAT WHILE CRUISING ABOUT 2000 FEET AGL, THE AIRPLANE LOST ALL ENGINE
POWER. WHILE HE WAS TURNING TO CHANGE DIRECTION, THE AIRPLANE STALLED. THE PILOT WAS ABLE
TO REGAIN CONTROL AT APPROXIMATELY 100 TO 200 FEET AGL BEFORE IMPACTING THE GROUND.
POSTACCIDENT EXAMINATION REVEALED NO FUEL IN THE FUEL TANK. Accident occurred MAR-08-94 at VANCOUVER, WA WHEN THE PILOT, WHO WAS ALSO THE MANUFACTURER, PUT THE SEAT IN
THE "KIT-BUILT" AIRCRAFT, HE DID NOT ATTACH THE SEAT TO THE AIRFRAME AS
RECOMMENDED BY THE KIT DESIGNER. AFTER APPROXIMATELY 28 HOURS OF TOTAL FLYING TIME, THE
SEAT SLIPPED FROM ITS NORMAL POSITION IN THE AIRFRAME DURING A TOUCH-AND-GO LANDING, AND
FELL UPON THE AILERON CONTROL ROD. THIS CAUSED THE AILERON CONTROL SYSTEM TO JAM, AND THE
PILOT EXECUTED A GO-AROUND USING RUDDER AND ELEVATOR CONTROL INPUTS. DURING THE ENSUING
FULL STOP LANDING, THE PILOT LOST CONTROL OF THE AIRCRAFT AS HE INITIATED THE LANDING
FLARE. Accident occurred MAR-20-94 at OXFORD, IA The certified flight instructor was attempting to land the
airplane after the student pilot's first instructional flight. During the landing attempt
a gust of wind raised the left wing. The flight instructor could not level the wings
because the student had his leg against the control stick. The instructor landed in a soft
field next to the runway, and the airplane nosed-over. Accident occurred APR-29-94 at MERRITT ISLAND, FL THE PILOT AND PILOT-RATED PASSENGER DEPARTED ON A LOCAL FLIGHT
WITH FULL FUEL. ON RETURN, THE PILOT ENCOUNTERED STRONGER THAN EXPECTED WINDS ALOFT, AND
THE ENGINE FAILED DUE TO FUEL EXHAUSTION. THE PILOT EXECUTED A FORCED LANDING AND WHILE
ROLLING TO A STOP, THE AIRPLANE COLLIDED WITH A FENCE AND WAS SUBSTANTIALLY DAMAGED. Accident occurred MAY-07-94 at MUNJACK CAY On May 7, 1994, about 1430 eastern daylight time, a homebuilt float equipped Kitfox IV 1200, N31PH, registered to Larry Blackmun, experienced in flight loss of control and crashed about 100 yards offshore of Munjack Cay, near the Great Abaco Island, Bahamas, while on a 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The airplane was destroyed and the airline transport-rated pilot was seriously injured. The passenger was fatally injured. The time of departure has not been determined. According to Bahamian Civil Aviation personnel, the pilot stated that while maneuvering at a low altitude, the airplane stalled, pitched nose down, and impacted the water. The pilot was airlifted to a hospital in Charleston, South Carolina. The investigation is under the jurisdiction of the government of the Bahamas. Any further information pertaining to this accident may be obtained from: Director of Civil Aviation, Bahamas P.O. Box N-975 Nassau, N.P. Bahamas Phone: (809) 327-7117 This report is for information purposes only and contains only information released by the Bahamian Government. Accident occurred MAY-21-94 at ISLAMORADA, FL THE PILOT STATED HE WAS AT 1,200 FEET AGL FLYING TOWARDS THE
COASTLINE FROM THE EAST, AND HE ENCOUNTERED TURBULENT AIR CONDITIONS OVER THE EDGE OF THE
LAND MASS. THE AIRPLANE ROLLED TO THE LEFT AND THE NOSE PITCHED DOWN. HE PUSHED THE
CONTROL STICK FORWARD, AND APPLIED RIGHT AILERON AND RUDDER. HE REGAINED CONTROL OF THE
AIRPLANE AT ABOUT 600 FEET AND CIRCLED BACK FOR LANDING. WHILE ON FINAL APPROACH FOR
LANDING AT ABOUT 75 TO 150 FEET AGL OVER THE SAME LAND MASS, THE AIRPLANE ROLLED TO THE
LEFT AND THE NOSE PITCHED DOWN. HE ATTEMPTED THE SAME RECOVERY PROCEDURE AS BEFORE WITHOUT
SUCCESS. THE AIRPLANE COLLIDED WITH THE WATER IN A NOSE-DOWN ATTITUDE. HE STATED HE COULD
NOT REMEMBER WHAT HIS AIRSPEED WAS BEFORE THE AIRPLANE ROLLED TO THE LEFT, AND THAT HE HAD
NOT DETERMINED THE NEW STALL SPEED FOR THE AIRPLANE AFTER THE INSTALLATION OF THE FLOAT
KIT. HE FURTHER STATED THERE WAS NO EVIDENCE OF A PRECRASH MECHANICAL FAILURE OF THE
AIRFRAME, FLIGHT CONTROLS, ENGINE ASSEMBLY OR ACCESSORIES. Accident occurred APR-16-94 at YELM, WA SHORTLY AFTER TAKEOFF, THE ENGINE LOST POWER. THE PILOT MADE A
FORCED LANDING TO AN OPEN FIELD, AND DURING THE LANDING ROLL THE AIRPLANE COLLIDED WITH A
FENCE. THE PILOT REPORTED THAT A FUEL LINE BECAME KINKED AND STARVED THE ENGINE OF FUEL. Accident occurred JUL-01-94 at PALMAS DEL MAR, PR THE PILOT OF THE EXPERIMENTAL HOMEBUILT AIRPLANE WAS OBSERVED
MANEUVERING ALONG THE SHORELINE AT ABOUT 20 FT ABOVE THE WATER. THE SURVIVING PASSENGER
STATED THE PILOT WAS LOWERING THE FLAPS TO SLOW THE AIRPLANE TO POINT OUT AN APARTMENT. AS
THE PILOT QUICKLY LOWERED THE FLAPS THE AIRPLANE PITCHED DOWN, HIT THE WATER, AND SANK. Accident occurred MAY-01-94 at BUCKEYE, AZ Witnesses stated that the student pilot, who had no confirmed
flight experience, assembled the aircraft on the day of the accident at the airport from a
kit of preassembled major components. The pilot told the witnesses that he was going to
perform some taxi tests and proceeded to do several taxi runs along the runway. The
aircraft was then observed to line up on the runway, add what was described as full power,
then takeoff. The witnesses said the aircraft leveled off about 30 feet above the runway
and flew down the complete length of the pavement. Past the departure end of the runway,
the aircraft abruptly pitched nose down and impacted the ground about 1,000 feet from the
runway end. An FAA inspector reported that control system continuity was established
throughout the aircraft during his examination. The witnesses reported that the engine
sounds were consistent and strong up to the point of ground impact. A review of FAA system
records revealed no evidence of a registration or airworthiness certificate application by
the pilot. |
|||||
|
|||||
|
|||||
Ultralight Aircraft News Web Magazine Covering the World of Ultralight Aviation You may link to these pages or print them out for your own personal use, but no part of this publication may be copied or distributed, transmitted, transcribed, stored in a retrieval system, or translated into any human or computer language, in any form or by any means, electronic, mechanical, manual, or otherwise, without the written permission of Ultralight News. By copying or paraphrasing the intellectual property on this site, you're automatically signing a binding contract and agreeing to be billed $10,000 payable immediately. Copyright Ultralight News |
|||||
Return to Main Index for this section | |||||