What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On July 24, 2004 at approximately 12:05 pm, N69CL a Beech baron 58P impacted the ground at the intersection of carrick road and stonehaven drive Fort Collins, Colorado approximately five miles north of Fort Collins/loveland airport (fnl) on 355 degrees. The aircraft impacted flat with a heading of 322 degrees and was destroyed on impact with a post crash fire. All three persons on board received fatal injuries. The aircraft was being operated under 14CFR part 91 in IMC conditions under a IFR flight plan fnl to oma. A total of thirteen witness statements were obtained from local law enforcement. Summary of the statements describe the engines making erratic noises, emerges from the clouds in a flat spin (one states in a counterclockwise rotation of three to four rotations, prior to impact) and the elevator in a full up position. Wreckage was contained in a small area with one right propeller blade being thrown sixty to eighty feet. The pilot held a private certificate with sel, MEL and instrument ratings. An interview with the CFI who administered a refresher on July 23, 2004, stated that the N69CL had no abnormalities during the 3.1 hour flight.
As the FAA filed it
(-23) ON JULY 24, 2004 AT APPROXIMATELY 12:05 PM, N69CL A BEECH BARON 58P IMPACTED THE GROUND AT THE INTERSECTION OF CARRICK ROAD AND STONEHAVEN DRIVE FORT COLLINS, COLORADO APPROXIMATELY FIVE MILES NORTH OF FORT COLLINS/LOVELAND AIRPORT (FNL) ON 355 DEGREES. THE AIRCRAFT IMPACTED FLAT WITH A HEADING OF 322 DEGREES AND WAS DESTROYED ON IMPACT WITH A POST CRASH FIRE. ALL THREE PERSONS ON BOARD RECEIVED FATAL INJURIES. THE AIRCRAFT WAS BEING OPERATED UNDER 14CFR PART 91 IN IMC CONDITIONS UNDER A IFR FLIGHT PLAN FNL TO OMA. A TOTAL OF THIRTEEN WITNESS STATEMENTS WERE OBTAINED FROM LOCAL LAW ENFORCEMENT. SUMMARY OF THE STATEMENTS DESCRIBE THE ENGINES MAKING ERRATIC NOISES, EMERGES FROM THE CLOUDS IN A FLAT SPIN (ONE STATES IN A COUNTERCLOCKWISE ROTATION OF THREE TO FOUR ROTATIONS, PRIOR TO IMPACT) AND THE ELEVATOR IN A FULL UP POSITION. WRECKAGE WAS CONTAINED IN A SMALL AREA WITH ONE RIGHT PROPELLER BLADE BEING THROWN SIXTY TO EIGHTY FEET. THE PILOT HELD A PRIVATE CERTIFICATE WITH SEL, MEL AND INSTRUMENT RATINGS. AN INTERVIEW WITH THE CFI WHO ADMINISTERED A REFRESHER ON JULY 23, 2004, STATED THAT THE N69CL HAD NO ABNORMALITIES DURING THE 3.1 HOUR FLIGHT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N69CL · 3
Matched to the same aircraft by N-number and date.