20191218023219I

Incident · Minor damage

FAA incident report · Piper PA-28-151 · Rome, GA · December 18, 2019

Date
December 18, 2019 · 19:16 local
Place
Rome, GA
Airport
Rome Georgia
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N6919J
Reported as
Piper PA-28-151
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot

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.

A portion of the propeller separated from aircraft while at 5,500 feet. The resulting vibration caused damage to the soft engine mounts, crank shaft, baffling, and cowling. Aircraft diverted to rmg and landed without incident. Preliminary inspection revealed a portion off one propeller blade had separated at mid span from unknown cause. There was no indication of FOD or other damage.

Propeller was high time and had been throught several overhauls. Propeller had been dynamic balanced in the log book history. There was evidence of fatigue on the fracture surface, but the age or progression of it is unknown

privacy data omitted

Pilot did not contribute to the accident, but he saved their lives with his training and quick actions. He ok'd me using their names because these reports are reviewed by faast team, and I felt he may be eligible for commendation.

This record was amended however to follow atqa instructions.

As the FAA filed it

A PORTION OF THE PROPELLER SEPARATED FROM AIRCRAFT WHILE AT 5,500 FEET. THE RESULTING VIBRATION CAUSED DAMAGE TO THE SOFT ENGINE MOUNTS, CRANK SHAFT, BAFFLING, AND COWLING. AIRCRAFT DIVERTED TO RMG AND LANDED WITHOUT INCIDENT. PRELIMINARY INSPECTION REVEALED A PORTION OFF ONE PROPELLER BLADE HAD SEPARATED AT MID SPAN FROM UNKNOWN CAUSE. THERE WAS NO INDICATION OF FOD OR OTHER DAMAGE.

PROPELLER WAS HIGH TIME AND HAD BEEN THROUGHT SEVERAL OVERHAULS. PROPELLER HAD BEEN DYNAMIC BALANCED IN THE LOG BOOK HISTORY. THERE WAS EVIDENCE OF FATIGUE ON THE FRACTURE SURFACE, BUT THE AGE OR PROGRESSION OF IT IS UNKNOWN

^PRIVACY DATA OMITTED^

PILOT DID NOT CONTRIBUTE TO THE ACCIDENT, BUT HE SAVED THEIR LIVES WITH HIS TRAINING AND QUICK ACTIONS. HE OK'D ME USING THEIR NAMES BECAUSE THESE REPORTS ARE REVIEWED BY FAAST TEAM, AND I FELT HE MAY BE ELIGIBLE FOR COMMENDATION.

THIS RECORD WAS AMENDED HOWEVER TO FOLLOW ATQA INSTRUCTIONS.

Other reports on N6919J · 1

Matched to the same aircraft by N-number and date.