20260813011259I

Incident · Minor damage

FAA incident report · Dehavilland DHC-2 · Juneau, AK · August 13, 2026

Date
August 13, 2026 · 11:24 local
Place
Juneau, AK
Airport
Juneau International
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Operator
P9KA
Damage
Minor damage
Aircraft
N777DH
Reported as
Dehavilland DHC-2
Reported engine
Pratt & Whitney R-985
People aboard
1
Fatal injuries
0
Other injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

The aircraft lost engine power shortly after departure from the float pond. The pilot subsequently landed in the river, where the aircraft floated into a log jam. The pilot was the sole person on board. No injuries were reported, and the aircraft sustained minor damage.

During the post-incident engine inspection, the no. 1 cylinder compression was measured at 20/80, while the remaining cylinders were below 10 PSI. The oil filter and oil sump were also found to contain metal debris.

The cause of the engine failure was determined to be a supercharger failure. Material from the failed supercharger was ingested and distributed into all cylinders, resulting in the loss of engine power. The pilot statement, maintenance findings, and photographs have been added to the office accident file.

Accident file: IAL0520260005

Incident closed satisfactorily.

As the FAA filed it

THE AIRCRAFT LOST ENGINE POWER SHORTLY AFTER DEPARTURE FROM THE FLOAT POND. THE PILOT SUBSEQUENTLY LANDED IN THE RIVER, WHERE THE AIRCRAFT FLOATED INTO A LOG JAM. THE PILOT WAS THE SOLE PERSON ON BOARD. NO INJURIES WERE REPORTED, AND THE AIRCRAFT SUSTAINED MINOR DAMAGE.

DURING THE POST-INCIDENT ENGINE INSPECTION, THE NO. 1 CYLINDER COMPRESSION WAS MEASURED AT 20/80, WHILE THE REMAINING CYLINDERS WERE BELOW 10 PSI. THE OIL FILTER AND OIL SUMP WERE ALSO FOUND TO CONTAIN METAL DEBRIS.

THE CAUSE OF THE ENGINE FAILURE WAS DETERMINED TO BE A SUPERCHARGER FAILURE. MATERIAL FROM THE FAILED SUPERCHARGER WAS INGESTED AND DISTRIBUTED INTO ALL CYLINDERS, RESULTING IN THE LOSS OF ENGINE POWER. THE PILOT STATEMENT, MAINTENANCE FINDINGS, AND PHOTOGRAPHS HAVE BEEN ADDED TO THE OFFICE ACCIDENT FILE.

ACCIDENT FILE: IAL0520260005

INCIDENT CLOSED SATISFACTORILY.