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Aviation safety reports, made easier to study

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NTSB Report

April 11, 2008 · North American T-28C · N9022N

Kingman, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 11, 2008
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Kingman, AZ
Aircraft
North American T-28C
Tail Number
N9022N
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX08LA098

About 15 minutes after takeoff, during cruise flight, the pilot observed the engine oil pressure drop and the temperature increase, followed by a total loss of engine power. The pilot made an intentional gear-up forced landing on rough terrain. A partial teardown examination of the engine revealed ferrous and non-ferrous metal in the oil screens. The number 3 connecting rod was found bent, and the number 4 and number 5 cylinders were damaged. Numerous pieces of metal were observed in the crankcase that were associated with the number 4 and number 5 cylinders and pistons. The internal engine component that initially broke at the beginning of the sequence was not identified.

NTSB Probable Cause

A total loss of engine power during cruise flight due to an undetermined catastrophic internal engine failure.

Full Narrative

On April 11, 2008, about 0730 mountain standard time, an experimental North American T-28C, N9022N, experienced a total loss of engine power while cruising about 5 miles east-southeast of the Kingman Airport, Kingman, Arizona. The pilot made a forced landing on open, rocky, desert terrain, and the airplane was substantially damaged. The private pilot was not injured, and the passenger sustained minor injuries. The airplane was owned and operated by the pilot. Visual meteorological conditions prevailed at the time of the personal flight, and no flight plan was filed. The flight was performed under the provisions of 14 Code of Federal Regulations Part 91, and it originated from Kingman about 0715. The pilot reported to the National Transportation Safety Board investigator that the engine started running rough while cruising about 5,000 feet mean sea level (about 2,000 feet above ground level). The pilot checked the engine gauges and observed that the oil pressure was decreasing and the oil temperature was "maxing out." According to the pilot, the engine then lost all power and he made an intentional gear up landing because the tricycle gear airplane likely would have nosed over during rollout on the soft terrain. The propeller continued to rotate throughout the mishap. The pilot stated that his airplane's Curtis Wright model 1820-86B engine had been operated about 175 hours since receiving an overhaul. At the direction of the Safety Board investigator, a Federal Aviation Administration (FAA) airworthiness inspector oversaw an examination of the accident engine. In pertinent part, the FAA inspector reported finding "an excessive amount of ferrous and non-ferrous" material in the oil screens. The number 3 cylinder was removed from the crank case and exhibited a bent connecting rod, along with "major damage to its piston and cylinder skirt." Also, numerous pieces of metal were observed in the crankcase that was associated with the number 4 and number 5 cylinders. The internal engine component that initially broke was not identified.

Flight

Event TypeAccident
Event Time07:30 MST
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftNorth American T-28C
Tail NumberN9022N
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsCurtis Wright · R-1820-86B · Reciprocating · 1425
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 44 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility50 sm
CeilingNone
Temperature / Dew Point64 F / 0 C
Altimeter0
Observation Time14:15
Weather SourcePILO

Appendix: Source Data