LAX07LA016

NTSB accident investigation · Cessna 152 · Prunedale, CA · October 22, 2006

Accident · Minor injuriesLimited investigationFinal report
Date
October 22, 2006, 07:41 local (14:41 UTC)
Place
Prunedale, CA
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N45929Cessna 152
Weather
Visual (VMC) · Day
Status
Completed · report September 27, 2007
Report
Approved by Office Director
Parties
San Jose Flight Standards District Office
FAA report
20061022024699A
Case key
64745

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

Total loss of engine power due to failure of connecting rod cap during cruise flight for undetermined reasons.

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/malfCruise - normal
Engine assembly,connecting rod cap - failure
Forced landingEmergency descent/landing
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - open field
Nose overEmergency landing

Analysis

According to the flight instructor, he and his student departed on the flight when, about halfway to their destination, the engine cowling and instrument panel began to shake violently. He adjusted the mixture setting and scanned the instruments and noted that the engine oil temperature and pressure were still indicating in the normal range. Shortly after that, the engine began shaking and then stopped entirely and gray smoke filled the cockpit. The flight instructor noted flames coming from the nose area of the aircraft and attempted to find a suitable landing site through the smoke and haze. The flight instructor elected to land in an agricultural field. The airplane touched down on the main landing gear, and as the nose wheel touched down it dug into the dirt and the airplane nosed over. When the instructor and student exited the airplane, they again observed a small fire near the front engine area, but it extinguished itself. According to a Federal Aviation Administration (FAA) inspector, the engine was examined and a large hole was found on the bottom side of the engine crankcase between the number 1 and number 2 cylinders. A concentration of oil was found on the inside of the cowling at the same approximate location as the crankcase hole. FAA inspectors discovered that the number 1 connecting rod cap had separated from the connecting rod during engine operation. The reason for this occurrence is undetermined.

Factual narrative

On October 22, 2006, at 0741 Pacific daylight time, a Cessna 152 airplane, N45929, nosed over during a forced landing near Prunedale, California. A loss of engine power preceded the forced landing. The airplane was operated by United Flight Services of Watsonville, California, under the provisions of 14 CFR Part 91 as an instructional flight. The certified flight instructor sustained minor injuries and the student pilot was not injured. The airplane was substantially damaged. Visual meteorological conditions prevailed and a flight plan was not filed. The flight originated from Watsonville, California, about 25 minutes prior to the accident, and was destined for Salinas, California.

According to the flight instructor, he and his student departed on the flight to Salinas when, about halfway to their destination, the engine cowling and instrument panel began to shake violently. He adjusted the mixture setting and scanned the instruments and noted that the engine oil temperature and pressure were still indicating in the normal range. Shortly after that, the engine began shaking and then stopped entirely and gray smoke filled the cockpit. The flight instructor noted flames coming from the nose area of the aircraft and attempted to find a suitable landing site through the smoke and haze. The flight instructor elected to land in an agricultural field. The airplane touched down on the main landing gear, and as the nose wheel touched down it dug into the dirt and the airplane nosed over.

When the instructor and student exited the airplane, they again observed a small fire near the front engine area, but it extinguished itself.

According to a Federal Aviation Administration (FAA) inspector, the engine was examined and a large hole was found on the bottom side of the engine crankcase between the number 1 and number 2 cylinders. A concentration of oil was found on the inside of the cowling at the same approximate location as the crankcase hole. FAA inspectors discovered that the number 1 connecting rod cap had separated from the connecting rod during engine operation. The reason for this occurrence is undetermined.

Aircraft

Registration
N45929
Reported as
Cessna 152
Category
Airplane
Serial number
15282946
Airframe hours
11,695.5
Engine
Lycoming O-235-L2C, 115 horsepower, reciprocating
Damage
Substantial damage
Fire
In-Flight
Flight
Instructional · Part 91
Operator
United Flight Services
Registered owner
Roger Fernandez
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 1, 2006 · 56.3 hours before
Departed
WVI · Watsonville, CA
Destination
SNS · Salinas, CA
Airport
Off Airport

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
Flight instructor
Age
37
Injuries
Minor
Certificates
Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Without waivers/limitations
Last flight review
August 1, 2005
Seat
Right
Flight hours
4,000 total · 800 in this make and model · 3,800 as pilot in command · 200 in the last 90 days · 100 in the last 30 days · 5 in the last 24 hours
Role
Student pilot
Age
31
Injuries
None
Certificates
Student, Private
Medical
Class 3
Last flight review
August 1, 2005
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Wind
140° at 7 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
50 °F, dew point 41 °F
Altimeter
29.96 inHg
Observed at
SNS

FAA reports on this event · 1

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