2 fatalities

17 Dec 2025: PIPER PA-30 (N8693Y) — PEREGRINE AVIATION LLC — West Chicago, IL

West Chicago, IL, United States

On 17 Dec 2025, a PIPER PA-30 (registration N8693Y) operated by PEREGRINE AVIATION LLC was involved in an aviation accident near West Chicago, IL. 2 people were killed. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Piper PA-30 (N8693Y) was substantially damaged after a takeoff accident near West Chicago, Illinois on December 17, 2025. The pilot and pilot-rated passenger sustained fatal injuries. The aircraft drifted right, reached 75 ft, banked sharply, and impacted terrain.

Overview

On December 17, 2025, at about 1349 central standard time, a Piper PA-30 airplane, registration 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.

Accident Sequence

Airport surveillance video captured the airplane during takeoff. The video showed the airplane drifting to the right of the runway centerline during the initial climb, reaching a maximum height of about 75 ft above ground level. The airplane maintained a nose-high attitude and banked left and right before the right bank 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 no other radio calls were made by the pilot after he repeated the takeoff clearance.

Wreckage Examination

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, with a debris path on a magnetic heading of 255°. The left engine propeller was found embedded in an impact crater about 45 ft from the main wreckage, and ground scars consistent with propeller strikes were observed nearby.

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 inverted and rested on top of the left wing; the right engine hung from the nacelle firewall. The forward fuselage exhibited accordion crushing, and the fuselage was fractured aft of the rear seats. The empennage remained intact with compression damage.

Initial Findings and Witnesses

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.

The wreckage was retained for further examination.