Piper PA 46-350P N779MA
16 April 2010 · Parkersburg, West Virginia, United States · No injuries
Summary
On 16 April 2010 at about 19:20 local time, a Piper PA 46-350P registered N779MA, operated by P & C Aviation LLC, was involved in an accident near Parkersburg, West Virginia, United States. 2 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 19:20
- Classification
- Accident
- Location
- Parkersburg, West Virginia, United States
- Nearest airport
- Mid-Ohio Valley Regional (PKB)
- Coordinates
- 39.3453, -81.4392
- Aircraft
- Piper PA 46-350P
- Registration
- N779MA
- Category
- Airplane
- Engines
- 1
- Operator
- P & C Aviation LLC
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Business
- Phase of flight
- Not recorded
- Route
- Charlotte → Parkersburg
- Aircraft damage
- Substantial
- Weather
- VMC
- Light
- Day
- NTSB number
- ERA10LA237
People
Nobody was injured.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 2 | 0 | 0 | 0 | 2 |
Probable cause
The inadequate design of the engine mount by the manufacturer, resulting in collapse of the nose landing gear. Contributing to the accident was the failure of the operator to adhere to the manufacturer's suggested engine mount inspection schedule.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
During landing, the airplane veered hard to the right when the nose gear was lowered to the runway after touchdown. The pilot attempted to maintain directional control with rudder input, but the airplane veered to the right and departed the runway. Initial examination of the airplane at the site revealed that the nose landing gear had collapsed and the attachment components between the nose landing gear actuator and the engine mount were fractured. Each of the right and left two-piece attachment feet were fractured at the nose landing gear actuator attach location. Detailed examination of the right foot showed evidence of fatigue, which covered a 0.75-inch arc and approximately 0.04 inches of the 0.06-inch wall thickness of the foot. The left foot also showed evidence of fatigue, which covered a 0.35-inch arc and was approximately 0.03 inches deep. The manufacturer had issued a series of Service Bulletins (SB 1103, with subsequent revisions A, B, and C) for PA-46-350P models that required inspections for cracks in the engine mounts in the areas of the nose landing gear actuator attachment feet. Inspections were to take place at the next regularly scheduled maintenance event, and at each 100 hours time in service or annual inspection, whichever occurred first. Records showed that SB 1103B was accomplished on the accident airplane during an annual inspection in 2007, but records of subsequent annual inspections in 2008 and 2009 showed that SB1103 was not accomplished. Previous nose gear failures and runway excursions resulted in the redesign of the original engine mount due to compliance (flexibility) in the engine mount actuator attach feet structure. This compliance issue was sometimes exasperated at various speeds, resulting in a high speed shimmy effect and subsequent uncommanded left or right turn of the nose wheel during takeoff and/or landing. The new engine mount incorporates a one piece design at the actuator attach point, eliminating the two piece feet design. The one piece design provides a less compliant structure, which prevents relative motion between the two feet in the original engine mount design. The Federal Aviation Administration did not mandate the actions outlined in SB 1103B, but compliance could have alerted the operator of any problems because the SB inspection criteria called for examinations of the engine mount in the areas where the fatigue cracks were located. Replacement of the engine mount with the new design that had one-piece nose landing gear actuator attachment feet would have relieved the operator of the manufacturer's repetitive inspection requirement, but because the accident airplane still had the welded two-piece attachment feet it was subject to the repetitive inspection per the service bulletin.
Quoted verbatim from the NTSB record.
Other Piper PA-46 accidents
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 24 Apr 2010 | Piper PA 46-350P | Clemson, South Carolina, United States | - | No injuries | - |
| 18 Dec 2010 | Piper PA-46-350P | Lake Elmo, Minnesota, United States | Richard Davidson | Minor injuries | - |
| 30 Dec 2010 | Piper PA-46-310P | Milaca, Minnesota, United States | Teemark Corp | Fatal | 2 |
| 25 Apr 2010 | Piper PA 46-350P | Owensboro, Kentucky, United States | T & K LLC | No injuries | - |
| 24 Aug 2010 | Piper PA-46-350P | Greeley, Colorado, United States | Williams Mirage LLC | No injuries | - |
| 16 May 2010 | Piper PA-46-350P | Clearwater, Florida, United States | Ernesto Gonzalez | Serious injuries | - |
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 1 May 2010 | Cessna 182T | Parkersburg, West Virginia, United States | Caylin LLC | No injuries | - |
| 17 Oct 2010 | Boeing PT17 | Fayetteville, West Virginia, United States | Carl Bailey | No injuries | - |
| 10 Sep 2010 | Cessna 150 | Fayetteville, West Virginia, United States | - | Serious injuries | - |
| 30 Oct 2010 | MD Helicopters 369E | Thomas, West Virginia, United States | Winco Inc. | Fatal | 1 |
| 19 Jan 2010 | Bombardier CL600 | Charleston, West Virginia, United States | PSA Airlines Inc | No injuries | - |
| 18 Sep 2010 | Beechcraft 58 | Rainelle, West Virginia, United States | Albatross Aircraft Sales Inc | Minor injuries | - |