- Date
- July 30, 2019, 16:30 local (21:30 UTC)
- Place
- Fairhope, AL
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N6754JPiper PA28
- Defining event
- Enroute: Loss of engine power (partial)
- Weather
- Visual (VMC) · Day
- Status
- Completed
- Report
- Approved by Office Director
- Investigation class
- Class 3
- NTSB office
- Central Region
- Parties
- FAA FSDO
- FAA report
- 20190730014909A
- Case key
- 100043
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
Failure of the No. 3 exhaust valve and the subsequent loss of engine power due to engine operation with an excessively lean fuel mixture over a period of time.
Findings · 2
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 flight instructor and student pilot had performed several touch-and-go landings; after the final landing, they departed for another airport. Shortly after takeoff, the engine started to vibrate severely and then lost power. The instructor performed a forced landing in a field, which resulted in substantial damage to the airplane's left wing. Postaccident engine examination revealed a failed No. 3 cylinder exhaust valve and extensive erosion on the No. 4 cylinder exhaust valve. The engine had accumulated 2,600 hours since the last overhaul, which was 600 hours beyond the manufacturer's recommended time before overhaul. The flight instructor reported that the leaning technique used while the airplane was on the ground was to lean the mixture during taxi or engine idle. For the engine run-up, they would use a full rich mixture. He added that during flight maneuvers at or below 3,000 ft mean sea level, they would not lean the mixture. However, the exhaust valve erosion is consistent with the engine being operated with an excessively lean fuel mixture over an extended period.
Factual narrative
On July 30, 2019, about 1630 central daylight time, a Piper PA28-140 airplane, N6754J, conducted a forced landing after departing the H L Sonny Callahan Airport (CQF), Fairhope, Alabama. The flight instructor and student pilot were not injured, and the airplane sustained substantial damage. The airplane was registered to and operated by Lightning Aviation, LLC under the provisions of Title 14 Code of Federal Regulations Part 91 as an instructional flight. The flight instructor reported that he was preparing the student pilot for his private pilot check ride and they had finished several touch-and-go landings. After the final landing, they planned to return to the Foley Municipal Airport (5R4). Shortly after take-off, the engine started a severe vibration, and then lost power. The instructor then preformed a forced landing in a cornfield, about two miles from the airport. An examination of the airplane by a Federal Aviation Administration inspector, found damage to the airplane's left wing and engine mount. Further examination of the engine's No. 3 cylinder revealed a failed exhaust valve. The examination also found extensive erosion on the No. 4 cylinder exhaust valve. He also noted that the engine had 2,600 hours since the last overhaul, adding that the engine manufacturer's recommended overhaul is 2,000 hours, and the flight school consistently ran the engines past the recommended overhaul time. Figure 1: Failed Exhaust valve FAA photo The flight instructor reported that the leaning technique used while on the ground, was to lean during taxi or engine idle. For the engine runup, they would go to a full rich mixture. He added that during flight maneuvers at or below 3,000 ft msl, they would not lean the mixture.
Aircraft
- Registration
- N6754J
- Reported as
- Piper PA28 (140)
- Category
- Airplane
- Serial number
- 28-24477
- Built
- 1968
- Engine
- Lycoming O-320 SERIES, reciprocating
- Damage
- Substantial damage
- Flight
- Instructional · Part 91
- Airworthiness certificate
- Standard, Normal
- Departed
- CQF · Fairhope, AL
- Destination
- 5R4 · Foley, AL
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
- 42
- Injuries
- None
- Certificates
- Commercial, Flight engineer
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 1, Without waivers/limitations
- Seat
- Right
- Restraint
- 3-point
- Flight hours
- 1,004 total · 300 in this make and model · 930 as pilot in command
- Role
- Student pilot
- Injuries
- None
- Seat
- Left
- Restraint
- 3-point
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 200° at 5 knots
- Visibility
- 10 statute miles
- Temperature
- 86 °F, dew point 72 °F
- Altimeter
- 30.02 inHg
- Observed at
- KCQF
Docket · 4
The files NTSB released with the investigation on March 30, 2020, on NTSB’s docket system: statements, records, photos and specialists’ reports. 3.5 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.