Aviation Crash Map

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
N364ST
Clemson, South Carolina, United States - No injuries -
18 Dec 2010 Piper PA-46-350P
N92358
Lake Elmo, Minnesota, United States Richard Davidson Minor injuries -
30 Dec 2010 Piper PA-46-310P
N9103N
Milaca, Minnesota, United States Teemark Corp Fatal 2
25 Apr 2010 Piper PA 46-350P
N46PT
Owensboro, Kentucky, United States T & K LLC No injuries -
24 Aug 2010 Piper PA-46-350P
N4167A
Greeley, Colorado, United States Williams Mirage LLC No injuries -
16 May 2010 Piper PA-46-350P
XBLTH
Clearwater, Florida, United States Ernesto Gonzalez Serious injuries -

All 284 records for this type

Other accidents in this area

Date Aircraft Location Operator Outcome Died
1 May 2010 Cessna 182T
N935FA
Parkersburg, West Virginia, United States Caylin LLC No injuries -
17 Oct 2010 Boeing PT17
N55464
Fayetteville, West Virginia, United States Carl Bailey No injuries -
10 Sep 2010 Cessna 150
N7922E
Fayetteville, West Virginia, United States - Serious injuries -
30 Oct 2010 MD Helicopters 369E
N765WH
Thomas, West Virginia, United States Winco Inc. Fatal 1
19 Jan 2010 Bombardier CL600
N246PS
Charleston, West Virginia, United States PSA Airlines Inc No injuries -
18 Sep 2010 Beechcraft 58
N86BR
Rainelle, West Virginia, United States Albatross Aircraft Sales Inc Minor injuries -

All 170,864 records in United States