20040501006009I

Incident

FAA incident report · Piper PA-18-150 · Hailey, ID · May 1, 2004

Date
May 1, 2004 · 08:38 local
Place
Hailey, ID
Phase of flight
Final Approach
Operating rules
General operating rules (Part 91)
Aircraft
N82727
Reported as
Piper PA18150
Reported engine
Lycoming O320*
People aboard
1
Fatal injuries
0

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 experienced engine failure approximately 5 miles north of Hailey Idaho airport during approach for landing. Pilot elected to land in a field by elementary school. Aircraft landing accomplished without incident and with no damage or injury to pilot or aircraft. Pilot stated that engine had started running rough prior to quitting. He was in contact with the Hailey airport control tower at the time of incident. Investigation revealed that the carburetor heat control cable clamp was loose at the control arm attachment, and therefore, the carburetor heat control did not function properly allowing carburetor ice to develop resulting in engine failure.

As the FAA filed it

(-23) AIRCRAFT EXPERIENCED ENGINE FAILURE APPROXIMATELY 5 MILES NORTH OF HAILEY IDAHO AIRPORT DURING APPROACH FOR LANDING. PILOT ELECTED TO LAND IN A FIELD BY ELEMENTARY SCHOOL. AIRCRAFT LANDING ACCOMPLISHED WITHOUT INCIDENT AND WITH NO DAMAGE OR INJURY TO PILOT OR AIRCRAFT. PILOT STATED THAT ENGINE HAD STARTED RUNNING ROUGH PRIOR TO QUITTING. HE WAS IN CONTACT WITH THE HAILEY AIRPORT CONTROL TOWER AT THE TIME OF INCIDENT. INVESTIGATION REVEALED THAT THE CARBURETOR HEAT CONTROL CABLE CLAMP WAS LOOSE AT THE CONTROL ARM ATTACHMENT, AND THEREFORE, THE CARBURETOR HEAT CONTROL DID NOT FUNCTION PROPERLY ALLOWING CARBURETOR ICE TO DEVELOP RESULTING IN ENGINE FAILURE.

Other reports on N82727 · 2

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