# NTSB CHI02LA150: Piper PA-24-250, N5360P, Sparta, IL, May 31, 2002 - Type: NTSB accident investigation - Classification: Accident · No injuries · Limited investigation · Final report - Date: May 31, 2002, 17:30 local (22:30 UTC) - Place: Sparta, IL - Coordinates: 38.149002, -89.709281 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=38.1490&lon=-89.7093&mi=10 - Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping) - Highest injury: No injuries - Injuries: 4 uninjured - Status: Completed, report April 18, 2003 - Report: Approved by Office Director - Parties: Federal Aviation Administration - NTSB case key (mKey): 54858 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=CHI02LA150 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/54858/pdf - NTSB docket: https://data.ntsb.gov/Docket?ProjectID=54858 - Page: https://openairdocs.org/ntsb/CHI02LA150 ## Probable cause The total loss of engine power due to a separated cylinder and the failure of the pilot to perform a precautionary landing at the nearest suitable airport when the engine had a partial loss of engine power. The failure of the aircraft owners to perform an engine overhaul and the unsuitable terrain encountered during the emergency landing were contributing factors. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of engine power(partial) - mech failure/malf, cruise - precautionary landing - not performed, pilot in command (cause) - maintenance,overhaul - not performed, owner/builder (cause) - Loss of engine power(total) - mech failure/malf, emergency descent/landing - engine assembly,cylinder - separation (cause) - Forced landing, emergency descent/landing - Gear collapsed, emergency landing - unsuitable terrain or takeoff/landing/taxi area - encountered, pilot in command (contributing factor) ## Analysis The airplane was substantially damaged when the gear collapsed during a forced landing due to a total loss of engine power. The airplane was directly over the Festus Memorial Airport (FES), Festus, Missouri when the engine started to run rough. The pilot decided to return to the Sparta Community-Hunter Field Airport (SAR), Sparta, Illinois, approximately 35 nautical miles (nm) from FES. The engine experienced a total loss of engine power approximately eight nm from SAR and the pilot executed an emergency landing on a wheat field. The number five cylinder was found to have separated from the engine. The last major overhaul on the engine was conducted on November 1, 1988 and the engine had accumulated 526 hours since the overhaul. The engine manufacturer recommends the engine be overhauled every 12 years even if the engine does not meet the time between overhaul hours. ## Factual narrative On May 31, 2002, at 1730 central daylight time, a Piper PA-24-250, N5360P, piloted by a private pilot, was substantially damaged when the landing gear collapsed during a forced landing on a wheat field following a total loss of engine power. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operated under the provisions of 14 CFR Part 91 and was not on a flight plan. The pilot and three passengers were uninjured. The flight originated from the Sparta Community-Hunter Field Airport (SAR), Sparta, Illinois at 1700 and was en route to the Eldon Model Airpark Airport, Eldon, Missouri. A witness reported that he observed the accident airplane during run-up and he stated that the airplane was idling very well prior to departure. The pilot stated in his written statement that 15 minutes after departing SAR, at 6,500 feet, the engine, "...acted over-lean adjustments didn't seem to help. I then turned around to return to SAR. Lost electronics after turn around near Red Bud IL. I was holding 6,500 over Red Bud IL. Engine started running worst. But was still running somewhat. Over Ballwin IL I was down to around 4,000 ft. [and] preparing for landing and thought I located a good field, I then engaged landing gear manually, turned fuel off, master-switched to off and landed safely, however landing gear collapsed." The pilot reported that when the engine started to run rough, the airplane was over the Festus Memorial Airport (FES), Festus, Missouri. FES is served by runway 18/36 (2,202 feet by 49 feet, asphalt) and is approximately 35 nautical miles to the west of SAR. The Federal Aviation Administration inspector's examination of the Lycoming O-540-AID5 engine, serial number L-3749-40, revealed that the number five cylinder had separated from the engine, and the number two cylinder was loose. The number five cylinder's studs had remaining threads while the number two cylinder's studs were sheared. The number three cylinder was replaced during its last annual inspection on October 5, 2001. No recorded maintenance on the number five cylinder had been done since the engine was installed on the accident airplane five years prior to the accident. Torque checks on all the cylinder studs were found to be within tolerances four years prior to the accident. The engine was last overhauled on November 1, 1988 and installed on the accident airplane approximately 10 years later with an accumulated time of approximately 100 hours since overhaul. At the time of the accident, the engine had a total of 526 hours since overhaul. According to the Textron Lycoming Service Instruction number 1009AQ, Recommended Time Between Overhaul Periods: "Engine deterioration in the form of corrosion (rust) and the drying out and hardening of composition materials such as gaskets, seals, flexible houses and fuel pump diaphragms can occur if an engine is out of service for an extended period of time. Due to the loss of a protective oil film after an extended period of inactivity, abnormal wear on soft metal bearing surfaces can occur during engine start. Therefore, all engines that do not accumulate the hourly period of time between overhauls specified in this publication are recommended to be overhauled in the twelfth year." ## Aircraft - Registration: [N5360P](https://openairdocs.org/aircraft/N5360P), registered now, S/N 24-409, built 1958 (OpenAirDocs) - Reported make and model: Piper PA-24-250 - Registry model: [Piper PA-24-250](https://openairdocs.org/model/piper-pa-24-250) (registry code 7102404) (OpenAirDocs) - Registry engine: [Lycoming 0-540 series](https://openairdocs.org/engine/lycoming-0-540-series) (registry code 41532, reciprocating) (OpenAirDocs) - Category: Airplane - Serial number: 24-409 - Airframe hours: 2720 - Engines: Lycoming O-540-AID5 250 horsepower reciprocating - Damage: Substantial damage - Flight: Personal, Part 91 - Registered owner: Allen W. Brand - Airworthiness certificate: Standard, Normal - Last inspection: Annual, November 5, 2001, 30 hours before - Departed: SAR, Sparta, IL - Destination: H79, Eldon, MO - Flight plan: Unknown - Airport: SAR, Sparta Community-Hunter Field ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 45; injuries: none; private; airplane ratings: single-engine land; medical: class 3, valid medical--w/ waivers/lim; last flight review June 1, 2001; seat: left; flight hours: 323 total, 120 in this make and model, 262 as pilot in command, 5 in the last 90 days, 4 in the last 30 days, 1 in the last 24 hours ## Weather - Conditions: Visual (VMC), Day - Wind: 220° at 6 knots - Visibility: 10 statute miles - Lowest ceiling: none - Temperature: 90 °F, dew point 63 °F - Altimeter: 29.82 inHg - Observed at: SAR, 8 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 20020531017529A](https://openairdocs.org/incident/20020531017529A), May 31, 2002: Piper PA24250, Baldwin, IL, Substantial damage. (.19) On may 31, 2002, at 1730 central daylight time, a Piper PA-24-250, N5360P, piloted by a private pilot, was substantially damaged during a forced landing… ## Docket (3 files) The files NTSB released with the investigation on February 14, 2003, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=54858. 693 KB in all. - Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1 (item 1, .PDF, 336 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40439814&FileExtension=.PDF&FileName=Pilot%2FOperator%20Aircraft%20Accident%20Report,%20NTSB%20Form%206120.1-Redacted.PDF - Record of Interview (item 2, .PDF, 43 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40439815&FileExtension=.PDF&FileName=Record%20of%20Interview-Redacted.PDF - Textron Lycoming Service Instruction (item 3, .PDF, 314 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40175906&FileExtension=.PDF&FileName=Textron%20Lycoming%20Service%20Instruction-Master.PDF 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.