19980415006899A

Accident · Destroyed

FAA accident report · Cessna 180J · Ashland, WI · April 15, 1998

Date
April 15, 1998 · 08:40 local
Place
Ashland, WI
Airport
John F Kennedy Memorial Airport
Phase of flight
In Traffic Pattern-Circling
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N828CE
NTSB investigation
NTSBCHI98FA123
Reported as
Cessna 180J
Reported engine
Continental O470R
People aboard
1
Fatal injuries
1
Pilot’s flight hours
11,725 total

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Acft crashed on takeoff under unk circumstances, pilot suffered fatal inj, acft was destroyed by fire. (.4)a witness heard the pilot call on the radio and ask, 'is the coffee on?' The witness told the pilot that the coffee was on. The pilot responded, 'well then, I'll come in.' The next thing the witness recalled was a loud sound of an airplane engine and then the sound of things breaking. The witness ran outside of the hangar and saw the airplane going away from him in a level, gradual climb. The airplane began a left turn and roll. The airplane reached the top of its climb and then came straight down in a combination of a continual roll and a spin. Examination of the accident site revealed that the tops of three water birch trees, located 75 feet from the southeast edge of a ramp, on the airport's northeast side, were sheared off through the trunks, approximately 25 feet up from their bases. The outboard 4 feet of the airplane's left wing was found on the ramp, approximately 130 feet from the trees. Pieces of tree trunks, tree branches, and the airplane's left aileron fanned out from the trees in a southwesterly direction. N o other anomalies were found. (-23) witnesses describe a high-speed low pass by a corporate hangar where friends of the pilot worked. Left wing struck trees just off nw edge of that hangar's ramp, separating 4 feet of left wing and left aileron. Aircraft observed entering steep climb followed by dive to ground. Extensive post-impact fire. Flight control cables remained connected and operable. Engine found to produce compression on all cylinders, and crank turned freely.

As the FAA filed it

ACFT CRASHED ON TAKEOFF UNDER UNK CIRCUMSTANCES, PILOT SUFFERED FATAL INJ, ACFT WAS DESTROYED BY FIRE. (.4)A WITNESS HEARD THE PILOT CALL ON THE RADIO AND ASK, 'IS THE COFFEE ON?' THE WITNESS TOLD THE PILOT THAT THE COFFEE WAS ON. THE PILOT RESPONDED, 'WELL THEN, I'LL COME IN.' THE NEXT THING THE WITNESS RECALLED WAS A LOUD SOUND OF AN AIRPLANE ENGINE AND THEN THE SOUND OF THINGS BREAKING. THE WITNESS RAN OUTSIDE OF THE HANGAR AND SAW THE AIRPLANE GOING AWAY FROM HIM IN A LEVEL, GRADUAL CLIMB. THE AIRPLANE BEGAN A LEFT TURN AND ROLL. THE AIRPLANE REACHED THE TOP OF ITS CLIMB AND THEN CAME STRAIGHT DOWN IN A COMBINATION OF A CONTINUAL ROLL AND A SPIN. EXAMINATION OF THE ACCIDENT SITE REVEALED THAT THE TOPS OF THREE WATER BIRCH TREES, LOCATED 75 FEET FROM THE SOUTHEAST EDGE OF A RAMP, ON THE AIRPORT'S NORTHEAST SIDE, WERE SHEARED OFF THROUGH THE TRUNKS, APPROXIMATELY 25 FEET UP FROM THEIR BASES. THE OUTBOARD 4 FEET OF THE AIRPLANE'S LEFT WING WAS FOUND ON THE RAMP, APPROXIMATELY 130 FEET FROM THE TREES. PIECES OF TREE TRUNKS, TREE BRANCHES, AND THE AIRPLANE'S LEFT AILERON FANNED OUT FROM THE TREES IN A SOUTHWESTERLY DIRECTION. N O OTHER ANOMALIES WERE FOUND. (-23) WITNESSES DESCRIBE A HIGH-SPEED LOW PASS BY A CORPORATE HANGAR WHERE FRIENDS OF THE PILOT WORKED. LEFT WING STRUCK TREES JUST OFF NW EDGE OF THAT HANGAR'S RAMP, SEPARATING 4 FEET OF LEFT WING AND LEFT AILERON. AIRCRAFT OBSERVED ENTERING STEEP CLIMB FOLLOWED BY DIVE TO GROUND. EXTENSIVE POST-IMPACT FIRE. FLIGHT CONTROL CABLES REMAINED CONNECTED AND OPERABLE. ENGINE FOUND TO PRODUCE COMPRESSION ON ALL CYLINDERS, AND CRANK TURNED FREELY.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.