19980604015329A

Accident · Substantial damage

FAA accident report · Cessna A185F · Ilimna, AK · June 4, 1998

Date
June 4, 1998 · 20:10 local
Place
Ilimna, AK
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Operator
UKHC
Damage
Substantial damage
Aircraft
N32663
NTSB investigation
NTSBANC98LA064
Reported as
Cessna A185F
Reported engine
Continental IO520F
People aboard
1
Fatal injuries
0
Pilot’s flight hours
11,500 total5,000 in this make and model

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.

Lost power on maintenance test flight. Crash landed on a hillside. (.4) the certificated commercial pilot stated the airplane was in cruise flight when the engine began to run rough, and lose power. The engine continued to lose power until altitude could no longer be maintained, and the pilot selected a hillside as an emergency landing site. During the emergency landing, the airplane's fuselage sustained substantial damage. On July 1, NTSB personnel performed an engine examination at wick air, inc., wasilla, Alaska. No preaccident engine anomalies were noted. On September 11, FAA personnel operated the engine on the airframe, and reported that the engine operated normally at idle power. (-23) while a/c was in cruise flight engine power decreased to about 18' mpreason for power reduction is unknown at this time. A/c could not sustain flight at that power setting and crashed.

As the FAA filed it

LOST POWER ON MAINTENANCE TEST FLIGHT. CRASH LANDED ON A HILLSIDE. (.4) THE CERTIFICATED COMMERCIAL PILOT STATED THE AIRPLANE WAS IN CRUISE FLIGHT WHEN THE ENGINE BEGAN TO RUN ROUGH, AND LOSE POWER. THE ENGINE CONTINUED TO LOSE POWER UNTIL ALTITUDE COULD NO LONGER BE MAINTAINED, AND THE PILOT SELECTED A HILLSIDE AS AN EMERGENCY LANDING SITE. DURING THE EMERGENCY LANDING, THE AIRPLANE'S FUSELAGE SUSTAINED SUBSTANTIAL DAMAGE. ON JULY 1, NTSB PERSONNEL PERFORMED AN ENGINE EXAMINATION AT WICK AIR, INC., WASILLA, ALASKA. NO PREACCIDENT ENGINE ANOMALIES WERE NOTED. ON SEPTEMBER 11, FAA PERSONNEL OPERATED THE ENGINE ON THE AIRFRAME, AND REPORTED THAT THE ENGINE OPERATED NORMALLY AT IDLE POWER. (-23) WHILE A/C WAS IN CRUISE FLIGHT ENGINE POWER DECREASED TO ABOUT 18' MPREASON FOR POWER REDUCTION IS UNKNOWN AT THIS TIME. A/C COULD NOT SUSTAIN FLIGHT AT THAT POWER SETTING AND CRASHED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.