Piper PA28 accident near Foley, Alabama, May 6, 2019
On May 6, 2019 at about 5:47 pm local time, a 1969 Piper PA28, registered N5542U, was destroyed in an accident during initial climb near Foley, Alabama (Foley Municipal Airport). It was an instructional flight under general aviation rules (Part 91). 1 person was killed and 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
A partial loss of engine power due to a stuck exhaust valve and the flight instructor's exceedance of the airplane's critical angle of attack following the loss of power, which resulted in an aerodynamic stall at low altitude.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 6, 2019 · about 5:47 pm local time
- Place
- Foley, Alabama · Foley Municipal Airport · map
- Type
- Accident
- Injuries
- 1 person was killed and 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA28 140, built 1969 · all PA28s on the register
- Registration
- N5542U · no longer on the register · serial 28-26264
- Damage
- Destroyed
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The flight instructor and student pilot were conducting simulated engine-out emergency procedures in the airport traffic pattern. About 300-400 ft above ground level after takeoff, witnesses reported that the flight instructor announced on the radio that the engine had quit. Witnesses reported that the airplane then entered a nose-high, steep left turn before pitching down and impacting the ground. Postaccident examination of the airframe and flight controls revealed no mechanical anomalies that would have precluded normal operation. Examination of the engine revealed that the No. 4 cylinder exhaust valve was stuck in the valve guide due to excessive combustion deposits. It is likely that the stuck exhaust valve resulted in a partial loss of engine power. A flight instructor who flew the accident airplane the day before the accident flight reported experiencing engine roughness when performing simulated engine-out procedures. Following that flight, a mechanic cleaned the sparkplugs, performed an engine run-up, and returned the airplane to service; however, maintenance records did not show that the engine valves were inspected for sticking at that time. Manufacturer service instructions suggested inspecting for valve sticking at regular intervals or sooner if sticking was suspected. If a valve inspection had been completed in accordance with engine manufacturer guidance the day before the accident following the report of engine roughness, it is likely that the heavy carbon deposits on the exhaust valve would have been detected. Given that the flight instructor reportedly had students trim the airplane nose-up when landing, it is possible that the airplane was trimmed nose-high at the time of takeoff and the subsequent loss of engine power. Such a trim setting would have led to excessive pitch up, resulting in a rapid loss of airspeed, an exceedance of the airplane's critical angle of attack, and an aerodynamic stall at low altitude.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Loss of engine power (partial) during initial climb
- Aerodynamic stall/spin during initial climb defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Failure
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Instructor/check pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
Flight instructor
- Certificate: flight instructor, commercial pilot, private
- Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instrument: airplane
- Flight time: 977.5 hours in all; 507.2 in this make and model; 205.1 in the last 90 days; 90 in the last 30 days; 904.5 as pilot in command; 626.7 on instruments
- Last flight review: February 27, 2019
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: rgt
- Injury: serious injuries
Dual student
- Certificate: student
- Flight time: 15.6 hours in all; 15.6 in this make and model; 0 in the last 90 days; 0 in the last 30 days
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 6,985.8 hours
- Last inspection: annual inspection, March 12, 2019; 94 hours since
- Maximum gross weight: 2,150 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-320-D3G (piston); 6,295 hours total
- Operator: Lightning Aviation
The flight
- Departed from: 5R4 Foley AL at 5:47 pm
- Destination: 5R4 Foley AL
- Flight plan: none
- Runway 36, 3,700 ft by 74 ft
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 170° at 11 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 79°F (26°C), dew point 63°F (17°C)
- Altimeter: 30.03 inHg
- Observation at 5:55 pm from KJKA, 8 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
11 documents, released by the NTSB on March 30, 2020. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 2 | Witness Statements | PDF, 6 pages | View Download |
| 3 | Flight Instructor Logbook Excerpts | PDF, 32 pages | View Download |
| 4 | Student Pilot Logbook Excerpts | PDF, 7 pages | View Download |
| 5 | Engine Logbook Excerpts | PDF, 26 pages | View Download |
| 6 | Record of Engine Exam | PDF, 3 pages | View Download |
| 7 | Lycoming SB388C Exhaust Valve and Guide, Procedure to Determine Condition | PDF, 13 pages | View Download |
| 8 | Lycoming SI1485A Exhaust Valve and Guide Identification Procedure | PDF, 2 pages | View Download |
| 9 | Photo Array | PDF, 14 pages | View Download |
| 10 | Lycoming SI1425A Suggested Maintenance Procedures to Reduce the Possibility of Valve Sticking | PDF, 4 pages | View Download |
| 11 | Statement of Party Representatives to NTSB Investigation | PDF, 18 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
