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February 7, 1996 · Piper PA-32-RT-300 PA-32-RT-3 · N2200J

Blountville, TN

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 7, 1996
Injury Outcomes
No injuries (2 uninjured)
Location
Blountville, TN
Aircraft
Piper PA-32-RT-300 PA-32-RT-3
Tail Number
N2200J
Operator
Steven a Walters
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ATL96LA045

The night instrument instruction flight was cruising at 9,000 feet, VFR on top, when the left half of the top engine cowling ripped off and lodged on the horizontal stabilizer. The airplane was difficult to control, and would not maintain level flight. The instructor and the student diverted to a nearby airport and landed uneventfully. An FAA inspector examined the airplane and stated that the left cowl pin was missing, but it did not fail, having been torn away along with the surrounding cowling material. The manager of the shop where the airplane was repaired stated that he had previously observed worn side latches and pin grommets that allowed the upper cowl pin to slide out of the lower pin hole, which would allow air flow to rip off the upper cowling. There were no FAA malfunction/defect reports of a similar failure, and the manufacturer did not have records of any previous failure.

NTSB Probable Cause

Inadequate maintenance, and subsequent in-flight separation of the cowling, due to worn cowling components.

Full Narrative

On February 7, 1996, at 0345 eastern standard time a PA-32-RT-300, N2200J, made a forced landing at Tri-City Regional Airport, Blountville, Tennessee, after a portion of the engine cowling departed the airplane and struck the right horizontal stabilizer. The dual training flight was operated under the provisions of Title 14 CFR Part 91, and instrument flight rules. An instrument flight plan was active and visual meteorological conditions prevailed. The airplane was enroute to Charlottesville, Virginia, and was approximately 35 miles southwest of Holston Mountain VOR at the time of the accident. The instrument rated certified flight instructor and his student were not injured, and the airplane was substantially damaged. The instrument instruction flight had departed Birmingham, Alabama about 0115 the same day. Both pilots agreed that during the preflight inspection the engine cowling was not opened, the cowling looked normal, and no fasteners were missing. According to the flight instructor, the airplane was above a cloud layer in visual meteorological conditions, at 9000 feet when approximately 1/2 of the engine cowling departed the airplane. Full up elevator was needed to maintain level flight. The flight instructor noted that the elevator trim was reacting opposite it's normal direction. They diverted to Tri-City Regional Airport. The morning following the accident the flight instructor found pieces of the engine cowling lying next to the airplane. The airplane maintenance records revealed that the airplane passed a 100 hour inspection on October 6, 1995, and had accumulated 51 hours since this inspection. A discrepancy report was filed on October 26, 1995 for a drip of oil on the head (left cowling). This discrepancy was resolved on October 27, 1995. The FAA Air Safety Representative that examined the airplane stated that the cowling had become lodged in the elevator and dislodged upon touchdown. All of the pieces of the cowling were recovered except for the left cowl pin. He stated that both of the left cowl latches were attached, and in the latched position. The FAA Coordinator stated that there are no maintenance or difficulty reports on this airplane's cowling, and that the cowl pin did not fail. The manufacturer had no record of a similar previous failure in the same make and model airplane.

Flight

Event TypeAccident
Event Time03:45 EST
Nearest AirportTri-City Regional Airport (0nm)
Runway5
Runway Length8000 ft
Runway Width150 ft
Flight Plan FiledIFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-32-RT-300 PA-32-RT-3
Tail NumberN2200J
Aircraft CategoryAir
DamageSubstantial
OperatorSteven a Walters
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540-K1G5D · Reciprocating · 300
Seats6

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 27 · First Class

Conditions

ConditionsVMC
LightBright Night
WindCalm
Visibility7 sm
CeilingOvercast 3500 ft
Temperature / Dew Point27 C / 18 C
Altimeter30.00 inHg
Observation Time12:53
Weather SourceWFAC

Appendix: Source Data