# NTSB NYC98LA015: Piper PA-32RT-300, N2200J, Scottsville, VA, October 20, 1997 - Type: NTSB accident investigation - Classification: Accident · No injuries · Limited investigation · Final report - Date: October 20, 1997, 10:46 local (14:46 UTC) - Place: Scottsville, VA - Coordinates: 37.790119, -78.490951 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=37.7901&lon=-78.4910&mi=10 - Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping) - Highest injury: No injuries - Injuries: 2 uninjured - Status: Completed, report April 15, 1999 - Report: Approved by Office Director - NTSB case key (mKey): 39492 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=NYC98LA015 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/39492/pdf - Page: https://openairdocs.org/ntsb/NYC98LA015 ## Probable cause improper engine operation by undetermined person(s) that initiated gauling on the connecting rod, and led to its subsequent failure. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of engine power(total) - mech failure/malf, cruise - normal - engine assembly,connecting rod - fatigue (cause) - powerplant controls - improper use of (cause) - engine assembly,connecting rod - failure,total - Forced landing, descent - emergency - On ground/water encounter with terrain/water, landing - roll - airport facilities,runway/landing area condition - hidden obstruction(s) ## Analysis The pilot leveled off at his cruise altitude of 6,500 feet, the engine started to vibrate, and oil was observed leaking from the engine cowling. The vibration and oil flow increased in intensity, and the pilot shut the engine off, and performed a forced landing to a field. During the ground roll, the airplane struck a berm about 2 feet high. Examination of the engine revealed the number 2 connecting rod had failed between the wrist pin hole and crankshaft yoke. Metallurgical examination of the fracture found fatigue, and evidence of gauling in the area of the connecting rod bolt holes. Gauling was also found on the number 6 connecting rod bolt holes. According engine manufacturer, gauling could occur from high loading such as produced during overspeed or excessive manifold pressure operation. The operator reported the airplane was flown by company pilots on charter flights, and was also a rental airplane. ## Factual narrative On October 20, 1997, about 1046 eastern daylight time, a Piper PA-32RT-300, N2200J, operated by Blue Ridge Air, was substantially damaged during a forced landing near Scottsville, Virginia. The certificated commercial pilot and passenger were not injured. Visual meteorological conditions prevailed for the charter flight that departed from Charlottesville, Virginia, about 1030. The flight was operated on a Visual Flight Rules (VFR) flight plan under 14 CFR Part 135, destined for Southern Pines, North Carolina. In the NTSB Pilot/Operator Aircraft Accident Report, the pilot stated: "...About 15 minutes into the flight, leveling off at a cruising altitude of 6,500 [feet] MSL. Severe engine vibration was noted along with oil leaking from the area of the oil door partially covering the windscreen." "An emergency was declared a decision to land off-airport was made. The single passenger on-board briefed, and a glide established...." In a follow-up telephone interview, the pilot reported that the departure and climb to cruise altitude were uneventful. As the airplane was leveled at 6,500 feet for cruise, the engine was vibrating more than normal, and oil was leaking from the area of the oil filler door on the engine cowling. The vibration continued, and increased in intensity, as did the amount of oil that was leaking from the engine cowling, and covering the windshield. A field was selected for a forced landing and the engine was secured, followed by shutting off the fuel and electrical power. On short final, a power line was observed and the pilot elected to go under it. After touchdown, the airplane struck a 2 foot high berm that had been obscured by vegetation, and not observed from the air. The nose and left main landing gear collapsed, and the airplane slide to stop. The occupants then exited the airplane. On-site examination of the airplane by an inspector from the Federal Aviation Administration (FAA) revealed two holes on the top of the engine case above the forward connecting rod. The Inspector reported that the forward connecting rod was separated from the crankshaft, and there was no evidence of distress on the forward connecting rod journal surface. The engine was disassembled on November 11, 1997. The number 2 connecting rod was broken mid-way between the crankshaft yoke and the piston wrist pin hole. Pieces of metal were found in the oil pump and oil screen. The number 2 and 6 connecting rods were forwarded to the Textron Lycoming Metallurgical Laboratory for further examination. According to their report # LN 11145, dated December 16, 1997: "...Examination of the [number 2] connecting rod fracture surface at the yoke revealed beach marks...initiating from the crankpin bore indicating the rod failed in fatigue and progressed toward the OD of the crankpin bore. The fatigue origin was too severely damaged to determine whether the fatigue initiated from a galled spot. However, galled spots were observed near the origin...Examination of the No.6 connecting rod crankpin bore also revealed galled spots in the vicinity of the connecting rod bolt hole areas...." According to Textron Lycoming Mandatory Service Bulletin No. 439A, Inspection of Connecting Rods for Fretting and/or Galling and Repair of Fretting: "...Galling...is caused by movement between the surfaces of the bearing insert and the connecting rod during periods of high loading such as is produced during overspeed or excessive manifold pressure operation...." According to the operator, the airplane was flown by company pilots on charter flights, and available to pilots at large as a rental airplane. ## Aircraft - Registration: [N2200J](https://openairdocs.org/aircraft/N2200J), registered now, S/N 32R7985041, built 1979 (OpenAirDocs) - Reported make and model: Piper PA-32RT-300 (PA-32RT-30) - Registry model: [Piper PA-32RT-300](https://openairdocs.org/model/piper-pa-32rt-300) (registry code 7103215) (OpenAirDocs) - Registry engine: [Lycoming IO-540 series](https://openairdocs.org/engine/lycoming-io-540-series) (registry code 41530, reciprocating) (OpenAirDocs) - Category: Airplane - Serial number: 32R-7985041 - Airframe hours: 3420 - Engines: Lycoming IO-540-K1G5D 300 horsepower reciprocating - Damage: Substantial damage - Flight: Part 135 - Operator: Blue Ridge Air - Registered owner: Sir Speedy Lancelot Lc - Airworthiness certificate: Standard, Normal - Last inspection: Annual, July 10, 1997, 90 hours before - Departed: CHO, CHARLOTTESVILLE, VA - Destination: SOP, SOUTHERN PINES, NC - Flight plan: VFR ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 31; flight engineer, commercial; airplane ratings: multi-engine land, single-engine land; instrument ratings: airplane; medical: class 2, valid medical--w/ waivers/lim; seat: left; flight hours: 5,800 total, 1,400 in this make and model, 5,740 as pilot in command, 150 in the last 90 days, 75 in the last 30 days ## Weather - Conditions: Visual (VMC), Day - Wind: calm - Visibility: 15 statute miles - Lowest ceiling: none - Temperature: 66 °F, dew point 43 °F - Altimeter: 30.00 inHg - Observed at: CHO, 4 nm away ## FAA reports on this event (1) The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs). - [Accident 19971020044769A](https://openairdocs.org/incident/19971020044769A), Oct 20, 1997: Piper PA32RT300, Scottsville, VA, Substantial damage. Engine vibration. Oil on windshield hit berm landing. Folded gear. Rod went thru case. Fretting galling present. ## Other investigations on N2200J (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ATL96LA045](https://openairdocs.org/ntsb/ATL96LA045), Feb 7, 1996: Piper PA-32-RT-300 (N2200J), Blountville, TN, substantial damage. Probable cause: Inadequate maintenance, and subsequent in-flight separation of the cowling, due to worn cowling components. From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.