CEN10LA272

NTSB accident investigation · North American T-28A · Oklahoma City, OK · May 27, 2010

Accident · No injuriesLimited investigationFinal report
Date
May 27, 2010
Place
Oklahoma City, OK
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N128AFNorth American T-28A
Defining event
Approach-VFR pattern downwind: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Completed · report May 21, 2012
Report
Approved by Office Director
NTSB office
Central Region
Parties
FAA
FAA report
20100527005909A
Case key
76141

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The failure of the master rod bearing, which resulted in a loss of engine power.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilots stated that they were flying in the traffic pattern when the airplane's engine started losing power. They were unable to reach the runway and landed short of the prepared surface. A postaccident examination of the airplane revealed that the main landing gear had punctured both wings, damaging the spars, and two of the engine mounts had pulled loose from the firewall. Metal material was found in the outer casing of the oil filter. According to one of the airplane’s owners, the engine was later disassembled for salvage, and the master rod bearing was found to have failed.

Factual narrative

On May 27, 2010, about 2010 central daylight time, a North American T-28A airplane, N128AF, was substantially damaged following a loss of engine power and subsequent forced landing at Sundance Airpark (HSD), Oklahoma City, Oklahoma. The commercial pilot and the certified flight instructor were not injured. The local, personal flight was being conducted under the provisions of 14 Code of Federal Regulations Part 91 without a flight plan. Visual meteorological conditions prevailed at the time of the accident. The pilots stated they were flying in the traffic pattern when the engine started losing power. They were unable to make the runway and landed short of the prepared surface. Postaccident examination of the airplane revealed the main landing gear had punctured both wings, damaging the spars, and two engine mounts had pulled loose from the firewall. Fuel was found in both wings and the fuel selector was in the BOTH position. Metal material was found in the outer casing of the oil filter. According to one of the airplane’s owners, the engine was later disassembled for salvage and the master rod bearing was found failed and several of the cylinders had seized. According to maintenance records, the engine’s last major overhaul occurred on August 15, 1989. The last annual inspection occurred on December 5, 2009, at 77.7 hours time since major overhaul. According to the operator of the airplane, it had accumulated 99.9 hours time since major overhaul at the time of the accident.

Aircraft

Registration
N128AF
Reported as
North American T-28A
Category
Airplane
Serial number
491619A
Airframe hours
1,741
Engine
Wright C7BA SERIES, 1,475 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · December 5, 2009 · 22 hours before
Departed
HSD · Oklahoma City, OK
Destination
HSD · Oklahoma City, OK
Airport
HSD · Sundance Airpark

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Injuries
None
Certificates
Private, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Without waivers/limitations
Seat
Front
Flight hours
6,100 total · 10 in this make and model
Role
Flight instructor
Age
48
Injuries
None
Certificates
Flight instructor, Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Last flight review
May 26, 2009
Seat
Front
Flight hours
12,100 total · 650 in this make and model · 9,000 as pilot in command · 50 in the last 90 days · 50 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
8° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
82 °F, dew point 66 °F
Altimeter
29.94 inHg
Observed at
PWA, 6 nm away

Docket · 3

The files NTSB released with the investigation on April 27, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 3.8 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N128AF · 1

Matched to the same aircraft by N-number and date.