Piper PA-28-151 accident near Hope Mills, North Carolina, May 26, 2024
On May 26, 2024 at about 3:00 pm local time, a 1975 Piper PA-28-151, registered N33563, was substantially damaged in an accident during initial climb near Hope Mills, North Carolina (Grays Creek airport). It was a personal flight under general aviation rules (Part 91). 2 people were seriously injured and 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
A loss of engine performance due to carbon fouling of three spark plugs that, when combined with the airplane’s high gross weight condition, resulted in a collision with trees and terrain.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 26, 2024 · about 3:00 pm local time
- Place
- Hope Mills, North Carolina · Grays Creek · map
- Type
- Accident
- Injuries
- 2 people were seriously injured and 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA-28-151, built 1975 · all PA-28-151s on the register
- Registration
- N33563 · registry record · serial 28-7515346
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The private pilot and two passengers boarded the fully fueled airplane for a cross-country flight. Weight and balance calculations showed that the airplane was about 150 to 200 lbs below the maximum gross weight and the weather conditions were warm and humid at the time. A witness, who observed the loading of the airplane and noted the heat and humidity, expressed some concern to the pilot who assured him that he was within limits. There were no reported anomalies during the taxi, engine run-up, or the subsequent takeoff roll, but shortly after beginning the initial climb, while climbing through 450 ft mean sea level (msl), 290 ft above ground level (agl), the pilot noticed a drop in airspeed and was unable to maintain altitude. The passenger stated the engine sounded good, but the airplane wasn’t climbing. Unable to maintain level flight, the pilot lowered the airplane’s nose to maintain airspeed and avoid a stall. The airplane impacted trees and terrain about 3/4 of a mile from the departure end of the runway. The resulting impact caused a postcrash fire. Postaccident examination of the engine and components revealed the propeller was likely under power at the time of impact. In addition, three of the eight spark plugs were carbon-fouled, two of which were on the No. 1 cylinder. This fouling is typically caused by a rich fuel-air mixture, especially during ground operations or low power settings. The deposits can hinder the spark plug's ability to fire effectively, leading to reduced engine performance. The reduced spark plug efficiency led to reduced engine performance and, when combined with the airplane’s high gross weight and the ambient temperature and humidity, led to the airplane’s inability to climb and maintain altitude and resulted in impact with trees and terrain.
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 control in flight during initial climb
- Powerplant sys/comp malf/fail during initial climb defining event
The NTSB's findings
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Climb rate › Attain/maintain not possible
- Aircraft › Aircraft power plant › Ignition system › Spark plugs/igniters › Damaged/degraded
- Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › High temperature › Effect on equipment
- Aircraft › Aircraft oper/perf/capability › Aircraft capability › Climb capability › Attain/maintain not possible
- Personnel issues › Action/decision › Info processing/decision › Understanding/comprehension › Pilot
- Aircraft › Aircraft oper/perf/capability › Aircraft capability › CG/weight distribution › Related operating info
- Environmental issues › Physical environment › Object/animal/substance › Tree(s) › Contributed to outcome
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 99 hours in all; 16 in this make and model; 6 in the last 90 days; 4 in the last 30 days; 51 as pilot in command; 0 on instruments
- Last flight review: March 7, 2023
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: minor injuries
Passenger
- Seat: rgt
- Injury: serious injuries
Passenger
- Seat: rgt
- Injury: serious injuries
The aircraft
- Airframe total time: 9,048 hours
- Last inspection: 100-hour inspection, March 16, 2024
- Maximum gross weight: 2,325 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-320-E3D (piston); 1,740 hours total
- Operator: Cape Fear Aviation Services LLC
The flight
- Destination: JNX Smithfield NC
- Flight plan: none
Weather at the time
- Light: daylight
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 82°F (28°C), dew point 70°F (21°C)
- Altimeter: 29.90 inHg
- Observation at 10:53 am from FAY, 6 miles away
Weather report (METAR): KFAY 261453Z 00000KT 10SM CLR 28/21 A2990 RMK AO2 SLP120 T02780211 51004
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 2 |
Photographs from the investigation 11 pictures from the NTSB's docket, as the NTSB released them
Photograph 1 – Empennage and wreckage at the site.
Photograph 2 – View of fuselage wreckage at the accident site.
Photograph 3 – View of wreckage at hangar facility. (NTSB)
Photograph 4 – View of left wing at hangar facility (NTSB)
Photograph 5 – View of propeller assembly and engine on hoist. (NTSB)
Photograph 6 – View of number 2 and 4 side of engine. (NTSB)
Photograph 7 – View of right wing damage at hangar facility. (NTSB)
Photograph 8 – View of number 1 and 3 side of engine on hoist. (NTSB)
Photograph 9 – View of damaged magnetos.
Photograph 10 – View of spark plugs.
Photograph 11 – View of removed cylinder assemblies. (NTSB)The NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
11 documents, released by the NTSB on November 5, 2025. 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, 11 pages | View Download |
| 2 | Operator's Statements Pre and Post Accident | PDF, 3 pages | View Download |
| 3 | Memo for Record_passenger | PDF, 2 pages | View Download |
| 4 | FAA Interview Statement (PIC Interview) | PDF, 2 pages | View Download |
| 5 | Maintenance Logbooks Excerpt | PDF, 12 pages | View Download |
| 6 | NTSB Wreckage Examination Report | PDF, 10 pages | View Download |
| 7 | Carb Icing Probability Chart | PDF, 1 page | View Download |
| 8 | Weight and Balance | PDF, 3 pages | View Download |
| 9 | Photo Array_investigation Photographs | PDF, 12 pages · our copy | View Download |
| 10 | NTSB Certification of Party Representative Form (Airframe and Engine) | PDF, 10 pages | View Download |
| 11 | Wreckage Release | PDF, 1 page | 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.
