MIA04LA099

NTSB accident investigation · North American T-28C · Deland, FL · June 20, 2004

Accident · No injuriesLimited investigationFinal report
Date
June 20, 2004, 10:50 local (14:50 UTC)
Place
Deland, FL
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N28BZNorth American T-28C
Weather
Visual (VMC) · Day
Status
Completed · report September 13, 2005
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20040620017459A
Case key
59616

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

On this page

Probable cause

A loss of engine power due to an engine master rod bearing failure for undetermined reasons, resulting in damage to the airplane during the subsequent forced landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - mech failure/malfTakeoff - initial climb
Engine assembly,master rod - failure
Forced landingEmergency descent/landing
In flight collision with terrain/waterEmergency landing
Terrain condition - ditch

Analysis

The pilot stated that during a slow climb after takeoff, a lighted chip light in the airplane's cockpit illuminated. Shortly thereafter, he said he felt the first engine shudder/backfire, and he then made a "Mayday" call, and proceeded to the nearest airport to land. Along the way, the pilot said he increased power in an attempt to ensure he would reach the airport, and initially felt the airplane accelerate, but about 30 seconds later, in addition to the illuminated chip light and vibration associated with the engine, suddenly there was a severe rumble again, followed by the engine operating distinctively rough. He noted little puffs of black smoke, coming out of the stacks around the fuselage, and since there was a heavy forested area ahead, he said he turned the airplane toward a field, to affect a landing. The approach and landing flare/touchdown were uneventful, but during the landing rollout the airplane impacted a ditch, and incurred substantial damage. According to the FAA inspector who responded to the accident, an engine master rod bearing failed.

Factual narrative

On June 20, 2004, about 1050 eastern daylight time, a North American T-28C, N28BZ, registered to and operated by a private individual, as a Title 14 CFR Part 91 personal flight, made a forced landing to a field in the area of Deland, Florida. Visual meteorological conditions prevailed, and a visual flight rules flight plan was filed. The pilot and one passenger were not injured, and the airplane incurred substantial damage. The flight had originated from New Smyrna Beach, Florida, a few minutes before the accident.

The pilot stated that he had just departed from New Smyrna Beach Municipal Airport, New Smyrna Beach, Florida, and during a slow climb, at an altitude of about 5,000 feet, the pilot-rated passenger in the back seat alerted him to a flickering chip light. According to the pilot, the passenger said the light flickered dimly for about a second and then illuminated full bright. The pilot said that he then confirmed a lighted chip light on his panel as well, and shortly thereafter felt the first engine shudder/backfire. He then made a "Mayday" call, and proceeded to the nearest airport, Deland Municipal Airport, Deland, Florida, to affect a landing. Along the way, the pilot said he increased power in an attempt to ensure he would reach the airport, and initially felt the airplane accelerate, but about 30 seconds later, in addition to the illuminated chip light and vibration in the engine, suddenly there was a severe rumble again, followed by the engine operating distinctively rough. He noted little puffs of black smoke, coming out of the stacks around the fuselage, and since there was a heavy forested area ahead, turned the airplane toward a field to the east, to affect a landing. As he prepared to land, the pilot said he opened the canopy, secured the fuel flow, placed the propeller control in high pitch setting to minimize drag, secured battery power, and established a glide. He said the approach and landing flare/touchdown were uneventful, but during the landing rollout the airplane impacted a ditch, and incurred substantial damage.

According to the FAA inspector who responded to the accident, an engine master rod bearing failed. The inspector further stated that there were metal fragments throughout the oil, and the degree of damage and metal fragments made it difficult to determine what may precipitated the bearing failure.

Aircraft

Registration
N28BZ
Reported as
North American T-28C
Category
Airplane
Serial number
140637
Airframe hours
9,034
Engine
Curtis Wright R1820-86B, 1,420 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Daniel H. Serrato MD
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · June 1, 2004 · 1 hours before
Departed
EVB · New Smyrna Beac, FL
Destination
CSG · Columbus, GA
Flight plan
VFR
Airport
EVB · New Smyrna Beach

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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
50
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2
Last flight review
January 1, 2003
Seat
Front
Flight hours
800 total · 0 in this make and model · 700 as pilot in command · 40 in the last 90 days · 8 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
250° at 10 knots
Visibility
10 statute miles
Lowest ceiling
4,000 ft broken
Temperature
90 °F, dew point 75 °F
Altimeter
30.01 inHg
Observed at
DAB

FAA reports on this event · 1

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