N5494J

MINR
None

CESSNA 310R S/N: 310R0292

Accident Details

Date
Tuesday, October 11, 1994
NTSB Number
NYC95IA020
Location
ROCHESTER, NY
Event ID
20001206X02502
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Inadequate maintenance which resulted in undertorqued bolts, fatigue cracking of the hub, and the separation of the propeller assembly from the engine.

Aircraft Information

Registration
N5494J
Make
CESSNA
Serial Number
310R0292
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
310R C310
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
PARTNERSHIP GOLF
Address
1667 FOXWOOD TRAIL
Status
Deregistered
City
LOVELAND
State / Zip Code
OH 45140
Country
United States

Analysis

On October 11, 1994, at 1835 eastern daylight time, a Cessna 310R, N5494J, operated by Northland Aviation Inc., and piloted by Raymond Jacqus, aborted the takeoff at the Rochester Airport, Rochester, New York. The pilot was not injured. Visual meteorological conditions prevailed and an IFR flight plan had been filed for the flight operating under 14 CFR 135.

The pilot heard a loud "bang" after he applied full power to begin the takeoff roll. He then noticed that the right propeller had separated from the engine.

Six pieces of the three bladed feathering hub, part number E- 5887, other internal and external components from the right propeller were sent to the NTSB, Material Laboratory, Washington, DC. Three stud holes, a second dowel pin hole were not submitted for examination.

Metallurgical examination of the propeller hub revealed that the hub separated as a result of fatigue cracking that initiated from the holes for the studs used to attach the hub to the crankshaft flange. The fatigue initiated in about the third thread root from the bottom of the holes. The examination revealed combined fatigue cracking initiated from stud holes, labeled "1" and "2" and propagated almost all of the way from one blade socket to another. Examination of the portions of the hub mounting face revealed the presences of "extensive fretting damage." There were no defects found in the hub that may have contributed to the cracking.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC95IA020