20000408013389A

Accident · No damage

FAA accident report · SZD SZD-45A OGAR · Libby, MT · April 8, 2000

Date
April 8, 2000 · 16:00 local
Place
Libby, MT
Airport
Libby Airport
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N54AS
NTSB investigation
NTSBSEA00LA068
Reported as
SZD SZD45AOGAR

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.

(-23) On 4/8/00, while in cruise flight (approx 7500 feet MSL) near Libby, MT, N54AS, an Szd-45A ogar lost a propeller blade. The pilot recognized the problem, shut the engine down and executed an emergency landing at Libby, MT. With no additional damage to a/c. the blade separated at the hub at an attaching bolt hole. Post accident investigation showed that there was possibly as pre-existing crack in the blade. In addition to the separated propeller blade, which was not recovered, the engine mount was damaged to the point it will require a major repair to return it to an airworthiness condition. Also, there was damage to engine components due to the extreme vibration.

As the FAA filed it

(-23) ON 4/8/00, WHILE IN CRUISE FLIGHT (APPROX 7500 FEET MSL) NEAR LIBBY, MT, N54AS, AN SZD-45A OGAR LOST A PROPELLER BLADE. THE PILOT RECOGNIZED THE PROBLEM, SHUT THE ENGINE DOWN AND EXECUTED AN EMERGENCY LANDING AT LIBBY, MT. WITH NO ADDITIONAL DAMAGE TO A/C. THE BLADE SEPARATED AT THE HUB AT AN ATTACHING BOLT HOLE. POST ACCIDENT INVESTIGATION SHOWED THAT THERE WAS POSSIBLY AS PRE-EXISTING CRACK IN THE BLADE. IN ADDITION TO THE SEPARATED PROPELLER BLADE, WHICH WAS NOT RECOVERED, THE ENGINE MOUNT WAS DAMAGED TO THE POINT IT WILL REQUIRE A MAJOR REPAIR TO RETURN IT TO AN AIRWORTHINESS CONDITION. ALSO, THERE WAS DAMAGE TO ENGINE COMPONENTS DUE TO THE EXTREME VIBRATION.

NTSB investigation

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