N6384H

MINR
None

PIPER J3CS/N: 19565

Accident Details

Date
Thursday, April 27, 2023
NTSB Number
CEN23LA218
Location
Romeoville, IL
Event ID
20230601192286
Coordinates
41.608067, -88.103775
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The inflight failure of the propeller blade due to fatigue cracking from corrosion pits, initiating at the midpoint of the cambered face.

Aircraft Information

Registration
Make
PIPER
Serial Number
19565
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
J3CJ3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
J3C-65

Registered Owner (Current)

Name
WOLFE BRUCE G
Address
5725 HILLCREST ROAD
City
DOWNERS GROVE
State / Zip Code
IL 60516
Country
United States

Analysis

On April 27, 2023, about 1400 central daylight time, a Piper J3C-65 airplane, N6384H, sustained minor damage when it was involved in an incident near Romeoville, Illinois. The pilot sustained no injuries. The airplane was operated as a Title 14 CFR Part 91 personal flight.

The pilot reported that during the preflight inspection of the airplane, no anomalies were noted. The pilot decided to use runway 09 for the departure at the Lewis University Airport (LOT), Romeoville, Illinois, for the local area flight. During the takeoff, about 650 ft agl, the airplane began to shake “very violently.” The pilot closed the throttle, issued an emergency transmission to the LOT air traffic control tower, and executed a 180° turn to the left to land back on the departure runway. About halfway through turn, the pilot turned off the engine as he felt the airplane could successfully make the landing. The pilot was able to land the airplane on the runway without further incident.

After the pilot exited the airplane, he noticed that about 5 inches of the outboard portion of one of the aluminum propeller blades had separated. The separated blade segment was not recovered. The propeller sustained minor damage. There was no other damage sustained to the propeller, the engine, and the airframe. The airplane was equipped with a McCauley 1B90/CM7144 fixed pitch propeller.

Postincident examination revealed features consistent with fatigue cracking initiating at the midpoint of the cambered face of the propeller blade. These initiation sites exhibited corrosion pits consistent with those found on the cambered face of the propeller, which had been present underneath the paint and primer.

An annual inspection was performed on the airplane on October 25, 2022. A review of the airplane’s maintenance records revealed that the airplane had accumulated 0.7 hours since the annual inspection was performed. The propeller was overhauled on January 28, 2015, and the total time since new was listed as “unknown.” The propeller was installed on the airplane on August 18, 2015.

The propeller had about 223 total hours since its installation. The maintenance records did not show any overhaul work performed on the propeller since it was installed on the airplane. According to McCauley, this propeller is to be overhauled at 2,000 hours or 72 calendar months, whichever occurs first. The FAA does not mandate that propellers be overhauled for 14 CFR Part 91 operations.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN23LA218