19970725019679A

Accident · Substantial damage

FAA accident report · Waco YMF · Sedona, AZ · July 25, 1997

Date
July 25, 1997 · 19:09 local
Place
Sedona, AZ
Airport
Sedona Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N369BP
NTSB investigation
NTSBLAX97LA261
Reported as
Waco YMF
Reported engine
JACOBP R755B2
People aboard
3
Fatal injuries
0
Pilot’s flight hours
4,638 total1,539 in this make and model96 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.

Aircraft lost engine power and made emergency landing on a highway, hit a sign, ran into a ditch. (.4)during a local sightseeing flight, the engine started running rough. The pilot began a turn back toward the airport and noticed a decrease in power, which continued to escalate. He was unable to maintain altitude and selected a road to attempt a forced landing. During the landing, the airplane's right wing struck a telephone junction box. An exam revealed that the number 6 cylinder exhaust valve rocker arm adjustment nut was loose and the exhaust valve was not functioning. Review of the maintenance records disclosed that the valves were adjusted at the factory about 5 months and 200 hours prior to the accident.

As the FAA filed it

AIRCRAFT LOST ENGINE POWER AND MADE EMERGENCY LANDING ON A HIGHWAY, HIT A SIGN, RAN INTO A DITCH. (.4)DURING A LOCAL SIGHTSEEING FLIGHT, THE ENGINE STARTED RUNNING ROUGH. THE PILOT BEGAN A TURN BACK TOWARD THE AIRPORT AND NOTICED A DECREASE IN POWER, WHICH CONTINUED TO ESCALATE. HE WAS UNABLE TO MAINTAIN ALTITUDE AND SELECTED A ROAD TO ATTEMPT A FORCED LANDING. DURING THE LANDING, THE AIRPLANE'S RIGHT WING STRUCK A TELEPHONE JUNCTION BOX. AN EXAM REVEALED THAT THE NUMBER 6 CYLINDER EXHAUST VALVE ROCKER ARM ADJUSTMENT NUT WAS LOOSE AND THE EXHAUST VALVE WAS NOT FUNCTIONING. REVIEW OF THE MAINTENANCE RECORDS DISCLOSED THAT THE VALVES WERE ADJUSTED AT THE FACTORY ABOUT 5 MONTHS AND 200 HOURS PRIOR TO THE ACCIDENT.

NTSB investigation

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