20080911851529A

Accident · Destroyed

FAA accident report · Cirrus SR22 · Minocqua-Woodr, WI · September 11, 2008

Date
September 11, 2008 · 19:15 local
Place
Minocqua-Woodr, WI
Airport
Lakeland/Noble F. Lee Memorial
Phase of flight
Approach
Operating rules
Air taxi and commuter (Part 135)
Operator
MVWA
Damage
Destroyed
Aircraft
N193BS
NTSB investigation
NTSBCHI08FA282
Reported as
Cirrus SR22
Reported engine
Continental IO550N
People aboard
3
Fatal injuries
3
Pilot’s flight hours
2,120 total96 in this make and model184 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) Aircraft was executing the localizer 36 approach into arv. At one mile final the aircraft was at minimum decision altitude for the approach. At 1/2 mile the aircraft climbed 300 feet, made a left turn, descended 200 feet and then lost control and crashed in a 80 degree nose down attitude. Radar tracking shows erratic altitude and groundspeed between the outer marker and the missed approach point. Based on METAR weather data, ceiling was at the minimum descent altitude allowed by the approach approximately 8 minutes after the crash and well below minimums within 45 minutes after. Engine was running at impact based on propeller scars and witness statements. All controls appeared to be intact until impact based on wreckage evaluation.

As the FAA filed it

(-23) AIRCRAFT WAS EXECUTING THE LOCALIZER 36 APPROACH INTO ARV. AT ONE MILE FINAL THE AIRCRAFT WAS AT MINIMUM DECISION ALTITUDE FOR THE APPROACH. AT 1/2 MILE THE AIRCRAFT CLIMBED 300 FEET, MADE A LEFT TURN, DESCENDED 200 FEET AND THEN LOST CONTROL AND CRASHED IN A 80 DEGREE NOSE DOWN ATTITUDE. RADAR TRACKING SHOWS ERRATIC ALTITUDE AND GROUNDSPEED BETWEEN THE OUTER MARKER AND THE MISSED APPROACH POINT. BASED ON METAR WEATHER DATA, CEILING WAS AT THE MINIMUM DESCENT ALTITUDE ALLOWED BY THE APPROACH APPROXIMATELY 8 MINUTES AFTER THE CRASH AND WELL BELOW MINIMUMS WITHIN 45 MINUTES AFTER. ENGINE WAS RUNNING AT IMPACT BASED ON PROPELLER SCARS AND WITNESS STATEMENTS. ALL CONTROLS APPEARED TO BE INTACT UNTIL IMPACT BASED ON WRECKAGE EVALUATION.

NTSB investigation

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