20080322014069A

Accident · Substantial damage

FAA accident report · Scwzer G164B · Juliaetta, ID · March 22, 2008

Date
March 22, 2008 · 09:35 local
Place
Juliaetta, ID
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Operator
WRUG
Damage
Substantial damage
Aircraft
N8148K
NTSB investigation
NTSBLAX08LA083
Reported as
Scwzer G164B
Reported engine
WALTER M601E11
Fatal injuries
0
Pilot’s flight hours
15,000 total14,000 in this make and model1 in the last 90 days

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) During take-off from the pilot's privately-owned airstrip, the aircraft experienced a sudden failure of the rudder. The pilot reported that the aircraft immediately veered to the left between two telephone poles and under the wires. Pilot operated the aircraft for approximately 20 minutes while dumping its load of dry fertilizer and ascertaining landing options. The pilot landed the aircraft in a soft field approximately 800' west of the runway, traveled approximately 500', where upon the aircraft nosed in and flipped the aircraft over into an inverted position. Initial observation revealed that the aircraft sustained major damage to the propeller, left upper wing structure, and vertical tail, including the rudder. Initial investigation of post-crash damage revealed that the lower portion of the rudder main tubular spar showed signs of heavy corrosion and separation from the rudder control assembly.

As the FAA filed it

(-23) DURING TAKE-OFF FROM THE PILOT'S PRIVATELY-OWNED AIRSTRIP, THE AIRCRAFT EXPERIENCED A SUDDEN FAILURE OF THE RUDDER. THE PILOT REPORTED THAT THE AIRCRAFT IMMEDIATELY VEERED TO THE LEFT BETWEEN TWO TELEPHONE POLES AND UNDER THE WIRES. PILOT OPERATED THE AIRCRAFT FOR APPROXIMATELY 20 MINUTES WHILE DUMPING ITS LOAD OF DRY FERTILIZER AND ASCERTAINING LANDING OPTIONS. THE PILOT LANDED THE AIRCRAFT IN A SOFT FIELD APPROXIMATELY 800' WEST OF THE RUNWAY, TRAVELED APPROXIMATELY 500', WHERE UPON THE AIRCRAFT NOSED IN AND FLIPPED THE AIRCRAFT OVER INTO AN INVERTED POSITION. INITIAL OBSERVATION REVEALED THAT THE AIRCRAFT SUSTAINED MAJOR DAMAGE TO THE PROPELLER, LEFT UPPER WING STRUCTURE, AND VERTICAL TAIL, INCLUDING THE RUDDER. INITIAL INVESTIGATION OF POST-CRASH DAMAGE REVEALED THAT THE LOWER PORTION OF THE RUDDER MAIN TUBULAR SPAR SHOWED SIGNS OF HEAVY CORROSION AND SEPARATION FROM THE RUDDER CONTROL ASSEMBLY.

NTSB investigation

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

Other reports on N8148K · 1

Matched to the same aircraft by N-number and date.