N87424

Substantial
None

Ercoupe (Eng & Research Corp.) 415-C S/N: 597

Accident Details

Date
Sunday, January 14, 1996
NTSB Number
BFO96LA038
Location
HURLOCK, MD
Event ID
20001208X05102
Coordinates
38.619297, -75.870681
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

inadequate inspection by maintenance personnel which failed to detect a fatigue crack, and resulted in an in-flight crankshaft fracture and propeller assembly separation. A related factor was the deep snow encountered during the subsequent forced landing.

Aircraft Information

Registration
Make
ERCOUPE (ENG & RESEARCH CORP.)
Serial Number
597
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
415-C ERCO
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
415-C

Registered Owner (Current)

Name
PORTERFIELD TOM
Address
121 JAMESON RD
City
ABERNATHY
State / Zip Code
TX 79311-6036
Country
United States

Analysis

On January 14, 1996, at about 1600 eastern standard time, an Ercoupe 415-C, N87424, made an emergency landing in a snow covered field after the propeller separated from the airplane near Hurlock, Maryland. The flight originated at 1545 eastern standard time from Easton/Newnan Field, in Easton, Maryland, with an intended destination of Salisbury-Wicomico County Regional Airport, in Salisbury, Maryland. The pilot and the one passenger reported no injuries. The airplane sustained substantial damage. No flight plan had been filed and visual meteorological conditions prevailed at the time of the accident. The flight was conducted under 14 CFR Part 91.

The pilot stated that the airplane was in cruise flight at 1,500 feet mean sea level (MSL), when the propeller assembly separated. He reported that the propeller assembly impacted the airplanes left wing as it departed the aircraft.

The separated propeller assembly and the attached forward portion of the crankshaft flange were found in a field near the where the airplane impacted the snow. The crankshaft and the recovered forward fragment of the crankshaft flange were sent to the Office of Research and Engineering of the National Transportation Safety Board. An examination of the separated crankshaft P/N A5334, S/N 15C6 from the Continental C85-12 engine was conducted. The examination revealed that the crankshaft had separated at the propeller flange. The forward portion of the crankshaft contained a spiral crack that intersected the fracture at the bottom corner of the keyway. The scanning electron microscope examination of both halves of the mating fractures showed that original microscopic fracture features were mechanically damaged by relative movement between the mating fractures. The metallurgist's factual report stated: "No anomalies, such as corrosion pits or gouge marks were noted at the surface of the keyway."

Maintenance records indicate that in October, 1994, the main journals and pins of the crankshaft were ground 0.02 inch undersize, nitrided, inspected by visual and magnetic particle method, and installed with replacement main bearing and rod bearing set.

According to the metallurgist's report, a light colored layer extended approximately 0.06 inches deep from the bottom corner of the keyway. The metallurgist reported that further examination of this layer revealed a spectrum consistent with an iron nitride white layer.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# BFO96LA038