- 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.
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.