CEN26FA064 · Piper PA-30
Piper PA-30 · Accident: loss of control in flight
Event
- NTSB case
- CEN26FA064
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Ongoing
- API-reported fatalities
- 2 · all aircraft and ground
- Ground fatalities
- 0
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Piper PA-30
- Aircraft type
- Piper PA-30
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N8693Y
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From not recordedTo not recorded
- Aircraft age
- About 56 years (built 1969)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Unknown
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Loss of control in flight
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
No findings designated as a cause are recorded in the NTSB data yet.
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
On December 17, 2025, about 1349 central standard time, a Piper PA-30 airplane, N8693Y, was substantially damaged when it was involved in an accident near West Chicago, Illinois. The pilot and pilot-rated passenger were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. Airport surveillance video captured the airplane during takeoff. In the video, the airplane appeared to drift to the right of the runway centerline during the initial climb and reached a maximum height of about 75 ft above ground level. The airplane appeared to maintain a nose-high attitude and banked to the left and right before the right bank angle increased to about 90°. The airplane then impacted terrain in a nose-low, right-wing-low attitude. Preliminary air traffic control information revealed that the pilot was cleared for takeoff from runway 20R, and there were no other radio calls made by the pilot after he repeated the takeoff clearance. The main wreckage came to rest about 567 ft west of runway 20R, south of taxiway T. The initial point of impact was about 106 ft east of the main wreckage. The path from the initial impact point to the main wreckage was a magnetic heading of 255°. The left engine propeller was found embedded in an impact crater along the debris field about 45 ft from the main wreckage. Ground scars consistent with propeller strikes were observed near the impact crater. The main wreckage came to rest upright, supported by the extended main landing gear. Both wings remained attached to the fuselage with damage consistent with the impact sequence. Both engines remained partially attached to the wings through control cables and wire harnesses. The left engine was found inverted and rested on top of the left wing. The right engine was found hanging from the nacelle firewall. The forward fuselage exhibited accordion crushing consistent with impact damage, and the fuselage was fractured aft of the rear seats. The empennage remained intact with compression damage consistent with the impact sequence. Initial examination of the airplane revealed no anomalies with the flight controls or engines that would have precluded normal operation. Two witnesses observed the accident sequence and stated that the airplane engines sounded normal (figure 1). The wreckage was retained for further examination.
Figure 1. Overview of Accident Site
Verbatim NTSB factual narrative from the NTSB dataset
Sources
NTSB record CEN26FA064
- Event ID
- 20251217202178
- Case number
- CEN26FA064
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 91cf2d5142707288e6710a6c28cac932a0f225ffb758f797202112adb9483f96; retrieved 2026-09-15T09:11:46.731Z.