# NTSB CHI98LA224: Piper PA-28-235, N8903W, Liberal, KS, June 27, 1998 - Type: NTSB accident investigation - Classification: Accident · Fatal · Limited investigation · Final report - Date: June 27, 1998, 09:59 local (14:59 UTC) - Place: Liberal, KS - Coordinates: 37.039981, -100.930831 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=37.0400&lon=-100.9308&mi=10 - Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping) - Highest injury: Fatal - Injuries: 1 fatal - Status: Completed, report February 15, 2001 - Report: Approved by Office Director - NTSB case key (mKey): 10938 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=CHI98LA224 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/10938/pdf - Page: https://openairdocs.org/ntsb/CHI98LA224 ## Probable cause the inadvertent stall, the pilot's inadequate preflight planning, which led to performing a takeoff with insufficient distance to clear the utility pole. A factor which contributed to this accident was the utility pole. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of control - in flight, takeoff - initial climb - stall - inadvertent, pilot in command (cause) - preflight planning/preparation - inadequate, pilot in command (cause) - altitude/clearance - not attained, pilot in command (cause) - In flight collision with object, descent - uncontrolled - object - utility pole (contributing factor) - In flight collision with terrain/water, descent - uncontrolled ## Analysis A witness watched the airplane as it was making its takeoff run from a dirt road. The airplane's tail seemed to strike the crest of a hill, but the airplane did not takeoff. Further down the road, the witness saw the airplane get airborne and begin a turn to the left. The airplane then descended rapidly and hit the ground left wing first. The witness said that the airplane seemed to be rolling and going inverted before it struck the ground. About three seconds after the airplane hit the ground, it burst into flames. The airplane came to rest 25 feet south of a severed power pole, which was approximately 1/2 mile from where the airplane began its takeoff run. Examination of wreckage revealed no anomalies. According to the Piper PA-28 Cherokee 235 'B' Pilot Operating Handbook Takeoff Distance versus Density Altitude Chart, the takeoff distance needed to clear a 50 foot obstacle, for a 2,900 pound gross weight airplane with a density altitude of 6,364 feet msl, is approximately 2,550 feet. ## Factual narrative On June 27, 1998, at 0959 central daylight time (cdt), a Piper PA-28-235, N8903W, operated by a private pilot, was destroyed when just after takeoff, the airplane departed controlled flight. The airplane subsequently struck a telephone pole and impacted the ground. A post-crash fire ensued. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under 14 CFR Part 91. There was no flight plan on file. The pilot was fatally injured. The local flight originated from a road, 15 miles north of Liberal, Kansas. A witness said that the pilot had landed his airplane on a county road near the witness' house to bid a concrete job for him and his wife. At the conclusion of their meeting, the pilot got back into his airplane and attempted to takeoff from the road. The witness said that as the airplane was making its run down the road away from him, he noticed that the airplane's tail seemed to strike the crest of a hill, but not takeoff. Further down the road, the witness said that the airplane got airborne and began to turn to the left. The airplane then descended rapidly and hit the ground left wing first. The witness said that the airplane seemed to be rolling and going inverted before it struck the ground. About three seconds after the airplane hit the ground, it burst into flames. A Federal Aviation Administration (FAA) inspector examined the wreckage at the site. The airplane's remains rested in a shallow ditch approximately 15 feet east of a north-south running dirt road, and 25 feet south of a severed power pole. The power pole, was approximately 1/2 mile from where the airplane began its takeoff run. The airplane's vertical stabilizer and rudder, and horizontal stabilator were found resting at the base of the severed power pole. The vertical stabilizer showed a 12-inch wide "C-shaped" dent in its right skin running vertically from the base of the stabilator to the top where the broken rotating beacon was. The tailcone was crushed and charred. The main wreckage laid on a burned grass, road-shoulder area approximately 30 feet long and 30 feet wide. Preceding the burned grass area were strikes in the road, approximately 8 to 10 inches apart, and perpendicular to the airplane's longitudinal orientation. The airplane's entire fuselage, including the cockpit area, instrument panel, and engine cowling, were consumed by fire. The left wing rested inverted, next to the wreckage on the east side of the fuselage. The fuel tank and inboard four feet of the wing was melted and consumed. The right wing rested next to the fuselage on the west side. It was charred and melted. The engine and propeller were broken off and resting south of the wreckage. The engine was charred and melted. The propeller showed torsional bending, chordwise scratches and tip curling. Flight control continuity was confirmed. Examination of the engine and other airplane systems revealed no anomalies. The results of FAA toxicology testing of specimens from the pilot revealed the following volatile concentrations: 49.00 milligrams per deciliter (mg/dL, mg/hg) Ethanol detected in heart fluid. 17 (mg/dL, mg/hg) Ethanol detected in lung fluid. 9 (mg/dL, mg/hg) N-Propanol detected in heart fluid. 3 (mg/dL, mg/hg) N-Propanol detected in lung fluid. 17 (mg/dL, mg/hg) Acetaldehyde detected in lung fluid. 16 (mg/dL, mg/hg) Acetaldehyde detected in heart fluid. 2 (mg/dL, mg/hg) N-Butanol detected in heart fluid. 82 (mg/dL, mg/hg) Methanol detected in heart fluid. 1 (mg/dL, mg/hg) Isobutanol detected in lung fluid. 4 (mg/dL, mg/hg) Isobutanol detected in heart fluid. The manager of the FAA Toxicology and Accident Research Laboratory stated that the concentrations of Ethanol, N-Propanol, Acetaldehyde, Methanol, and Isobutanol revealed were most characteristic of post-mortem putrefaction. According to the Piper PA-28 Cherokee 235 "B" Pilot Operating Handbook Takeoff Distance versus Density Altitude Chart, the takeoff distance needed to clear a 50 foot obstacle, for a 2,900 pound gross weight airplane with a density altitude of 6,364 feet mean sea level (msl), is approximately 2,550 feet. ## Aircraft - Registration: [N8903W](https://openairdocs.org/deregistered/N8903W-2003-11-17), registration cancelled 2003-11-17, S/N 28-10469, built 1964 (OpenAirDocs) - Reported make and model: Piper PA-28-235 - Registry model: [Piper PA-28-235](https://openairdocs.org/model/piper-pa-28-235) (registry code 7102810) (OpenAirDocs) - Registry engine: [Lycoming 0-540 series](https://openairdocs.org/engine/lycoming-0-540-series) (registry code 41532, reciprocating) (OpenAirDocs) - Category: Airplane - Serial number: 28-10469 - Engines: Lycoming O-540-B4 250 horsepower reciprocating - Damage: Destroyed - Fire: On-Ground - Flight: Personal, Part 91 - Registered owner: James A. & Colleen L. Harms - Airworthiness certificate: Standard, Normal ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 48; private; airplane ratings: multi-engine land, single-engine land; medical: class 3, valid medical--w/ waivers/lim; seat: left; toxicology performed; flight hours: 2,000 total ## Weather - Conditions: Visual (VMC), Day - Wind: 340° at 10 knots - Visibility: 10 statute miles - Lowest ceiling: none - Temperature: 97 °F, dew point 59 °F - Altimeter: 29.00 inHg - Observed at: GCK, 39 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 19980627015089A](https://openairdocs.org/incident/19980627015089A), Jun 27, 1998: Piper PA28235, Liberal, KS, Destroyed, 1 fatal. Acft had landed on a county road to make a survey, depart from road stalled and crashed while turning to avoid powe (.4)a witness watched the airplane as it… 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.