20220117001139A

Accident · Substantial damage

FAA accident report · Piper PA-28 · Scottsdale, AZ · January 17, 2022

Date
January 17, 2022 · 10:50 local
Place
Scottsdale, AZ
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5276W
NTSB investigation
NTSBWPR22LA081
Reported as
Piper PA-28
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
265 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.

On January 17, 2022, about 2256 mountain standard time, a Piper PA-28 airplane, N5276W, was substantially damaged when it was involved in an accident near Scottsdale, Arizona. The pilot sustained minor injuries. The airplane was operated as a title 14 code of federal regulations part 91 personal flight. The pilot reported an engine failure to P50 in flight.

The postaccident examination of the engine revealed the separation of the no. 2 connecting rod from the crankshaft. The crankshaft connecting rod journal and connecting rod bearing showed thermal distress and material deformation. Mechanical damage was noted in the no. 1 and 2 cylinder internal bay areas.

As the FAA filed it

ON JANUARY 17, 2022, ABOUT 2256 MOUNTAIN STANDARD TIME, A PIPER PA-28 AIRPLANE, N5276W, WAS SUBSTANTIALLY DAMAGED WHEN IT WAS INVOLVED IN AN ACCIDENT NEAR SCOTTSDALE, ARIZONA. THE PILOT SUSTAINED MINOR INJURIES. THE AIRPLANE WAS OPERATED AS A TITLE 14 CODE OF FEDERAL REGULATIONS PART 91 PERSONAL FLIGHT. THE PILOT REPORTED AN ENGINE FAILURE TO P50 IN FLIGHT.

THE POSTACCIDENT EXAMINATION OF THE ENGINE REVEALED THE SEPARATION OF THE NO. 2 CONNECTING ROD FROM THE CRANKSHAFT. THE CRANKSHAFT CONNECTING ROD JOURNAL AND CONNECTING ROD BEARING SHOWED THERMAL DISTRESS AND MATERIAL DEFORMATION. MECHANICAL DAMAGE WAS NOTED IN THE NO. 1 AND 2 CYLINDER INTERNAL BAY AREAS.

NTSB investigation

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