20051221029909A

Accident · Substantial damage

FAA accident report · Piper PA-28-235 · Colorado Sprin, CO · December 21, 2005

Date
December 21, 2005 · 11:53 local
Place
Colorado Sprin, CO
Airport
Meadow Lake Airport
Phase of flight
Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9318W
NTSB investigation
NTSBDEN06LA024
Reported as
Piper PA28235
Reported engine
Lycoming O540*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
107 total6 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.

(-23) Pilot was turning downwind for runway 33 at (7700 MSL) pattern altitude at meadowlake airport. As he went to apply power to keep altitude, the engine did not respond. He applied carb heat and had a further loss of power. He rechecked the fuel pump and it was on. All gauges were normal or in the green, and the prop control was all the way in. Manifold pressure was about 12 inches and tach was about 2000 RPM. He made a decision to try and land on the road. His descent was so fast he didn't make the road, and landed next to it. On impact, the pilot hit some fence posts that damaged the right wing and broke off the right landing gear also.

As the FAA filed it

(-23) PILOT WAS TURNING DOWNWIND FOR RUNWAY 33 AT (7700 MSL) PATTERN ALTITUDE AT MEADOWLAKE AIRPORT. AS HE WENT TO APPLY POWER TO KEEP ALTITUDE, THE ENGINE DID NOT RESPOND. HE APPLIED CARB HEAT AND HAD A FURTHER LOSS OF POWER. HE RECHECKED THE FUEL PUMP AND IT WAS ON. ALL GAUGES WERE NORMAL OR IN THE GREEN, AND THE PROP CONTROL WAS ALL THE WAY IN. MANIFOLD PRESSURE WAS ABOUT 12 INCHES AND TACH WAS ABOUT 2000 RPM. HE MADE A DECISION TO TRY AND LAND ON THE ROAD. HIS DESCENT WAS SO FAST HE DIDN'T MAKE THE ROAD, AND LANDED NEXT TO IT. ON IMPACT, THE PILOT HIT SOME FENCE POSTS THAT DAMAGED THE RIGHT WING AND BROKE OFF THE RIGHT LANDING GEAR ALSO.

NTSB investigation

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