20070305003259A

Accident · Destroyed

FAA accident report · Piper PA-28-140 · Crescent Lake, OR · March 5, 2007

Date
March 5, 2007 · 16:20 local
Place
Crescent Lake, OR
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N5547F
NTSB investigation
NTSBSEA07LA071
Reported as
Piper PA28140
Fatal injuries
0
Pilot’s flight hours
430 total200 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.

(-23) On 3-5-07 at 1630 local pdst, N5547F a Piper PA-28-140 departed eugene, OR (eug) and was 10 miles east of Crescent Lake, OR (5S2). The pilot has a CFI, with commercial, multi-engine land and instrument rating, with 200 hours in this aircraft at the time of the accident. The pilot said he completed the preflight inspection before take-off from eugene, OR airport was satisfactory, with the oil level at 6 1/2 qts and no water noted in the fuel tank samples. His run-up of the engine had all normal engine indications. The pilot said the engine had been running smoothly at 2450 RPM at cruise, burning 7 gal/hr. He started to climb, due to above approaching terrain, the engine started running rough. Pilot applied carburetor heat and the engine stopped running. Aircraft crashed into snowy heavy treed area. Aircraft was destroyed by impact forces. Pilot and the one passenger both received minor injuries. ELT aided in location and rescue of pilot and passenger. During the post accident investigation FAA witnessed the firing and timing of both magnetos, compression check, removal of the 4 cylinders, inspection of valves and springs, carburetor, carburetor heat box and all controls were all satisfactory.

As the FAA filed it

(-23) ON 3-5-07 AT 1630 LOCAL PDST, N5547F A PIPER PA-28-140 DEPARTED EUGENE, OR (EUG) AND WAS 10 MILES EAST OF CRESCENT LAKE, OR (5S2). THE PILOT HAS A CFI, WITH COMMERCIAL, MULTI-ENGINE LAND AND INSTRUMENT RATING, WITH 200 HOURS IN THIS AIRCRAFT AT THE TIME OF THE ACCIDENT. THE PILOT SAID HE COMPLETED THE PREFLIGHT INSPECTION BEFORE TAKE-OFF FROM EUGENE, OR AIRPORT WAS SATISFACTORY, WITH THE OIL LEVEL AT 6 1/2 QTS AND NO WATER NOTED IN THE FUEL TANK SAMPLES. HIS RUN-UP OF THE ENGINE HAD ALL NORMAL ENGINE INDICATIONS. THE PILOT SAID THE ENGINE HAD BEEN RUNNING SMOOTHLY AT 2450 RPM AT CRUISE, BURNING 7 GAL/HR. HE STARTED TO CLIMB, DUE TO ABOVE APPROACHING TERRAIN, THE ENGINE STARTED RUNNING ROUGH. PILOT APPLIED CARBURETOR HEAT AND THE ENGINE STOPPED RUNNING. AIRCRAFT CRASHED INTO SNOWY HEAVY TREED AREA. AIRCRAFT WAS DESTROYED BY IMPACT FORCES. PILOT AND THE ONE PASSENGER BOTH RECEIVED MINOR INJURIES. ELT AIDED IN LOCATION AND RESCUE OF PILOT AND PASSENGER. DURING THE POST ACCIDENT INVESTIGATION FAA WITNESSED THE FIRING AND TIMING OF BOTH MAGNETOS, COMPRESSION CHECK, REMOVAL OF THE 4 CYLINDERS, INSPECTION OF VALVES AND SPRINGS, CARBURETOR, CARBURETOR HEAT BOX AND ALL CONTROLS WERE ALL SATISFACTORY.

NTSB investigation

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