N40437

Substantial
None

Piper PA-28R-201T S/N: 28R-7703304

Accident Details

Date
Tuesday, December 31, 1996
NTSB Number
FTW97LA077
Location
RATON, NM
Event ID
20001208X07171
Coordinates
36.880725, -104.439132
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

failure of the exhaust rocker arm retaining studs due to over torquing of the attachment bolts by maintenance personnel during installation. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N40437
Make
PIPER
Serial Number
28R-7703304
Engine Type
Reciprocating
Model / ICAO
PA-28R-201T P28S
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MCKENNA RANCH
Address
7110 HWY 10
Status
Deregistered
City
WALSENBURG
State / Zip Code
CO 81089
Country
United States

Analysis

On December 31, 1996, approximately 1350 mountain standard time, a Piper PA-28R-201T, N40437, was substantially damaged during a forced landing after a power loss near Raton, New Mexico. The private pilot and her three passengers were not injured. The airplane was registered to and operated by a private owner under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the cross country flight which originated from Midland, Texas, with the intended destination of Trinidad, Colorado. No flight plan had been filed and the flight had begun at 1210.

The pilot reported in the NTSB Pilot/Operator Aircraft Accident Report that while in cruise flight "the airplane shuddered" and began to lose power. She changed the fuel selector from the right to left tank; checked the fuel mixture, the exhaust gas temperature, and the instrument panel. The pilot reported that the engine performance continued to decay and she began looking for a place to land. She initiated a forced landing to a "pasture." Subsequently, during the landing roll, the landing gear separated from the airplane, the wings were damaged, and both wing spars were fractured.

Examination and tear down of the engine revealed that the number two cylinder exhaust rocker arm retaining studs had separated. Examination of the studs by a metallurgist revealed evidence of plastic deformation and a fatigue crack which was associated with "small cracks in the threads" (see enclosed metallurgist report).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW97LA077