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Aviation safety reports, made easier to study

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January 10, 2000 · Piper PA-32-300 · N8954N

Sweeney, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 10, 2000
Injury Outcomes
No injuries (2 uninjured)
Location
Sweeney, TX
Aircraft
Piper PA-32-300
Tail Number
N8954N
Operator
Eagle Air Service
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW00LA059

The airplane was in level cruise flight during dark night conditions when the 'engine stopped.' The instructor elected to make a forced landing to a field. On final approach, the instructor noticed what appeared to be power lines. The instructor banked the airplane to parallel the power lines and rotated the airplane to a nose high pitch attitude for touchdown. The touchdown was made on both main wheels; however, 'the nose of the aircraft came down hard,' and the airplane skidded to a stop. An FAA inspector supervised a 35-minute test run of the engine and found no anomalies.

NTSB Probable Cause

The pilot's excessive flare resulting in a hard landing. Factors were the loss of engine power for undetermined reasons, the power lines on final approach and the dark night conditions.

Full Narrative

On January 9, 2000, at 1845 central standard time, a Piper PA-32-300 airplane, N8954N, was substantially damaged when it impacted terrain during a forced landing following a loss of engine power near Sweeney, Texas. The airplane was registered to a private individual, and operated by Eagle Air Service, LTD. of Angleton, Texas. The flight instructor and student pilot were not injured. Dark night visual meteorological conditions prevailed and a flight plan was not filed for 14 Code of Federal Regulations Part 91 instructional flight. The flight departed the Brazoria County Airport near Angleton, Texas, at 1830, and was destined for the Bay City Municipal Airport, Bay City, Texas. In the enclosed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the flight instructor stated that the airplane was in cruise flight level at 1,500 feet msl when the "engine stopped." The instructor stated that his attempts to restart the engine were unsuccessful. The instructor elected to make a forced landing to a field. Just before the airplane crossed a tree line at the end of the field, the instructor "noticed what appeared to be power lines crossing the field." The instructor banked the airplane to parallel the power lines. After clearing the tree line, the instructor rotated the airplane to a nose high pitch attitude for touchdown. According to the instructor, "touchdown was made with a nose high attitude, squarely on both main wheels." Upon touchdown, "the nose of the aircraft came down hard," and the airplane skidded to a stop. An FAA inspector examined the airplane at the accident site. The inspector stated there was structural damage to the firewall. In addition, the nose landing gear was collapsed aft, and the propeller and engine cowling sustained damage. On March 2, 2000, an FAA inspector supervised a test run of the engine. The engine was run for 35 minutes at various power settings. No anomalies were noted during the engine test run.

Flight

Event TypeAccident
Event Time18:45 CST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-32-300
Tail NumberN8954N
Aircraft CategoryAir
DamageSubstantial
OperatorEagle Air Service
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540-KIAS · Reciprocating · 300
Seats6

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 29 · First Class

Conditions

ConditionsVMC
LightDark Night
Wind220° @ 4 kt
Visibility9 sm
CeilingOvercast 2300 ft
Temperature / Dew Point66 F / 63 F
Altimeter29.00 inHg
Observation Time23:53
Weather SourceWFAC

Appendix: Source Data