Mason RV-9A
Pacific City, OR — May 17, 2008
Event Information
| Date | May 17, 2008 |
| Event Type | ACC |
| NTSB Number | LAX08CA143 |
| Event ID | 20080613X00864 |
| Location | Pacific City, OR |
| Country | USA |
| Coordinates | 45.19972, -123.96222 |
| Airport | Pacific City State Airport |
| Highest Injury | NONE |
Aircraft
| Make | Mason |
| Model | RV-9A |
| Category | AIR |
| FAR Part | 091 |
| Aircraft Damage | SUBS |
Conditions
| Light Condition | DAYL |
| Weather | VMC |
Injuries
| Fatal | 0 |
| Serious | 0 |
| Minor | 0 |
| None | 1 |
| Total Injured | 0 |
Event Location
Probable Cause
The pilot's inadequate flare and failure to maintain control following a hard landing. Contributing to the accident was a temporary partial loss of power due to carburetor icing conditions.
Full Narrative
In a written statement and in telephone conversations with a National Transportation Safety Board investigator, the pilot reported that earlier in the morning he had picked up passengers and was planning a full stop at the destination airport. While on final approach in the traffic pattern, he noted that the airplane was descending too fast. He attempted to increase the engine rpm by pushing the throttle forward. The engine did not respond as he expected, with no increase in rpm occurring from the throttle movement until just prior to touchdown. The airplane touched down hard on the runway surface. The airplane bounced back airborne and the pilot manipulated the throttle full aft to bring the engine to idle. The airplane touched down again and the pilot experienced a loss of control. The nose landing gear collapsed and the airplane continued to skid; it came to rest inverted
The closest official weather observation station was 15 miles east of the airport. A Meteorological Terminal Aviation Routine Weather Report (METAR) issued 5 minutes prior to the accident indicated a temperature of 62.6 degrees Fahrenheit, a dewpoint of 59 degrees Fahrenheit, and a relative humidity of 88 percent. According to a carburetor icing probability chart, these conditions are conducive for serious icing at glide power.
The airplane incurred damage to the vertical stabilizer during the accident sequence. The pilot reported that aside from the engine not immediately responding to his throttle control, there were no pre impact mechanical malfunctions or failures.
About This NTSB Record
This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.