20041027028259A

Accident · Substantial damage

FAA accident report · Aerors J-2 · Camden, AR · October 27, 2004

Date
October 27, 2004 · 11:25 local
Place
Camden, AR
Airport
Harrell Field Airport
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N62SJ
NTSB investigation
NTSBDFW05CA024
Reported as
Aerors J2
Reported engine
Lycoming O360*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
604 total604 in this make and model20 in the last 90 days

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.

(-23) 10/27/04 At 1125AM, aircraft N62SJ, mccullock Aerors J-2 gyro-plane conducted an emergency landing onto a highway. One of the exhaust broke loose and struck the four bladed propeller. One of the blades broke at the root of the propeller causing a severe vibration in the engine. The engine was shut down and an emergency landing onto a highway bridge was completed by the pilot Mr. Jones. The severed propeller blade went through the r/h winglet and created a 3" hole through the stubby wing. The exhaust pipe struck the r/h tail boom and caused structural damage to the boom. Unnamed source of NTSB notification.

As the FAA filed it

(-23) 10/27/04 AT 1125AM, AIRCRAFT N62SJ, MCCULLOCK AERORS J-2 GYRO-PLANE CONDUCTED AN EMERGENCY LANDING ONTO A HIGHWAY. ONE OF THE EXHAUST BROKE LOOSE AND STRUCK THE FOUR BLADED PROPELLER. ONE OF THE BLADES BROKE AT THE ROOT OF THE PROPELLER CAUSING A SEVERE VIBRATION IN THE ENGINE. THE ENGINE WAS SHUT DOWN AND AN EMERGENCY LANDING ONTO A HIGHWAY BRIDGE WAS COMPLETED BY THE PILOT MR. JONES. THE SEVERED PROPELLER BLADE WENT THROUGH THE R/H WINGLET AND CREATED A 3" HOLE THROUGH THE STUBBY WING. THE EXHAUST PIPE STRUCK THE R/H TAIL BOOM AND CAUSED STRUCTURAL DAMAGE TO THE BOOM. UNNAMED SOURCE OF NTSB NOTIFICATION.

NTSB investigation

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