20100117026159A

Accident · Destroyed

FAA accident report · Cessna 182R · Philomath, OR · January 17, 2010

Date
January 17, 2010 · 17:00 local
Place
Philomath, OR
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N702
NTSB investigation
NTSBWPR10GA113
Reported as
Cessna 182R
Reported engine
Continental IO-470 series
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
0 total0 in this make and model0 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.

On January 18, 2010, at approximately 1700, Cessna 182 operated by the us department of the interior, as a public use aircraft, departed newport, OR (konp) enroute to corvallis (kcvo). The aircraft crashed into heavily wooded, mountainous terrain approximately 8.5 miles west of corvallis. The right wing, broken off at spar attach points, with lift strut, broken off at the lower strut attach point was resting inverted in what appeared to be the lowest portion of the debris field. 35 feet uphill from the right wing, the left wing was resting inverted, displaying deep leading edge impact damage approximately 18 inches from the root, approximately 18 to 20 inches deep. The outboard 8 feet of the left wing was broken off, laying approximately 15 feet to the east of the rest of the wing. The empennage was suspended in a tree, approximately 100 ft above the surface, above the left wing. 20 ft uphill from the left wing, the aft portion of the cabin and portions of the cabin roof, came to rest. The front seats, the instrument panel and firewall were sitting in an upright position facing the opposite direction of apparent impact heading, 30 feet uphill from the aft cabin. The initial impact scar of the engine and was approximately 30 ft uphill from the forward cabin, breaking away from the engine mount at this point. The engine then bounced approximately 25 ft to the right, and slightly down hill, coming to rest inverted. The propeller was imp ailed, tip first, in the base of a tree 10 feet uphill from the engine. The propeller, with the spinner still attached and there was no tip curling or torsional twisting damage noted . This aircraft was operating as a public use aircraft and the investigation is being conducted by the NTSB and us department of interior.

As the FAA filed it

ON JANUARY 18, 2010, AT APPROXIMATELY 1700, CESSNA 182 OPERATED BY THE US DEPARTMENT OF THE INTERIOR, AS A PUBLIC USE AIRCRAFT, DEPARTED NEWPORT, OR (KONP) ENROUTE TO CORVALLIS (KCVO). THE AIRCRAFT CRASHED INTO HEAVILY WOODED, MOUNTAINOUS TERRAIN APPROXIMATELY 8.5 MILES WEST OF CORVALLIS. THE RIGHT WING, BROKEN OFF AT SPAR ATTACH POINTS, WITH LIFT STRUT, BROKEN OFF AT THE LOWER STRUT ATTACH POINT WAS RESTING INVERTED IN WHAT APPEARED TO BE THE LOWEST PORTION OF THE DEBRIS FIELD. 35 FEET UPHILL FROM THE RIGHT WING, THE LEFT WING WAS RESTING INVERTED, DISPLAYING DEEP LEADING EDGE IMPACT DAMAGE APPROXIMATELY 18 INCHES FROM THE ROOT, APPROXIMATELY 18 TO 20 INCHES DEEP. THE OUTBOARD 8 FEET OF THE LEFT WING WAS BROKEN OFF, LAYING APPROXIMATELY 15 FEET TO THE EAST OF THE REST OF THE WING. THE EMPENNAGE WAS SUSPENDED IN A TREE, APPROXIMATELY 100 FT ABOVE THE SURFACE, ABOVE THE LEFT WING. 20 FT UPHILL FROM THE LEFT WING, THE AFT PORTION OF THE CABIN AND PORTIONS OF THE CABIN ROOF, CAME TO REST. THE FRONT SEATS, THE INSTRUMENT PANEL AND FIREWALL WERE SITTING IN AN UPRIGHT POSITION FACING THE OPPOSITE DIRECTION OF APPARENT IMPACT HEADING, 30 FEET UPHILL FROM THE AFT CABIN. THE INITIAL IMPACT SCAR OF THE ENGINE AND WAS APPROXIMATELY 30 FT UPHILL FROM THE FORWARD CABIN, BREAKING AWAY FROM THE ENGINE MOUNT AT THIS POINT. THE ENGINE THEN BOUNCED APPROXIMATELY 25 FT TO THE RIGHT, AND SLIGHTLY DOWN HILL, COMING TO REST INVERTED. THE PROPELLER WAS IMP AILED, TIP FIRST, IN THE BASE OF A TREE 10 FEET UPHILL FROM THE ENGINE. THE PROPELLER, WITH THE SPINNER STILL ATTACHED AND THERE WAS NO TIP CURLING OR TORSIONAL TWISTING DAMAGE NOTED . THIS AIRCRAFT WAS OPERATING AS A PUBLIC USE AIRCRAFT AND THE INVESTIGATION IS BEING CONDUCTED BY THE NTSB AND US DEPARTMENT OF INTERIOR.

NTSB investigation

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