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Aviation safety reports, made easier to study

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NTSB Report

March 27, 2000 · North American T-28B · N28NE

Bridgeport, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 27, 2000
Injury Outcomes
2 injuries (2 minor injuries)
Location
Bridgeport, TX
Aircraft
North American T-28B
Tail Number
N28NE
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
FTW00LA108

The pilot and passenger reported that after flying for 45 minutes the airplane's engine began to 'run rough, vibrate, and lose power.' The pilot observed black smoke emitting from the exhaust, and he estimated the engine then began producing 'about 25% of cruise power. The right exhaust gases momentarily ignited,' but extinguished when the throttle was retarded. Following the partial loss of engine power, the oil pressure gauge indicated 40 psi, and the airplane was unable to maintain altitude. The pilot executed a gear-up, forced landing in an open field, where the airplane came to rest upright. An FAA inspector examined the airplane and stated that engine oil had been 'blown out the exhaust and down the sides of the fuselage.' The reason for the partial loss of engine power was not determined.

NTSB Probable Cause

The partial loss of engine power for an undetermined reason.

Full Narrative

On March 27, 2000, at 1200 central standard time, a North American T-28B airplane, N28NE, sustained substantial damage during a forced landing following a loss of engine power near Bridgeport, Texas. The commercial pilot and his pilot-rated passenger received minor injuries. The airplane was registered to and operated by Trojan Phlyers of Fort Worth, Texas. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 91 personal flight, for which no flight plan was filed. The local flight departed Hicks Airfield, Fort Worth, Texas, at 1115. According to the pilot and his passenger, the purpose of the flight was to practice formation flying. Approximately 45 minutes into the flight, the engine began to "run rough, vibrate, and lose power." They observed black smoke emitting from the exhaust, and the pilot estimated that the engine then began producing "about 25% of cruise power. The right exhaust gases momentarily ignited," but extinguished when the throttle was retarded. The pilot stated that the cowl flaps were open at the time that the engine lost power, and the oil temperature gauge was checked every 10 minutes during the flight and consistently indicated 65 degrees Celcius. Following the partial loss of engine power, the oil pressure gauge indicated 40 psi, and the airplane was unable to maintain altitude. During the ensuing forced landing, the pilot elected to keep the gear retracted. The airplane touched down in an open field and came to rest upright. According to the FAA inspector, who examined the airplane, the fuselage keel beams were deformed, and the propeller was damaged. The inspector reported that engine oil had been "blown out the exhaust and down the sides of the fuselage." The airframe and engine underwent their most recent annual and 100 hour inspections, respectively, on March 15, 2000. At the time of the accident, the airframe had accumulated a total of 8,993.2 hours, and the engine had accumulated a total of 269.5 hours since overhaul.

Flight

Event TypeAccident
Event Time12:00 CST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftNorth American T-28B
Tail NumberN28NE
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsWright · 1820-86A · Reciprocating · 1425

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 51 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 10 kt
Visibility20 sm
CeilingNone
Temperature / Dew Point70 F / 0 C
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data