# NTSB FTW02LA022: Bellanca 17-30A, N614CJ, Clarendon, TX, October 27, 2001 - Type: NTSB accident investigation - Classification: Accident · No injuries · Limited investigation · Final report - Date: October 26, 2001, 20:45 local (Oct 27, 2001, 01:45 UTC) - Place: Clarendon, TX - Coordinates: 34.879444, -100.906669 - Nearby events: https://openairdocs.org/map.md?lat=34.8794&lon=-100.9067&mi=10 - Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping) - Highest injury: No injuries - Injuries: 2 uninjured - Status: Completed, report July 2, 2002 - Report: Approved by Office Director - Parties: Federal Aviation Administration - NTSB case key (mKey): 53669 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=FTW02LA022 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/53669/pdf - Page: https://openairdocs.org/ntsb/FTW02LA022 ## Probable cause the loss of engine power for undetermined reasons. Contributing factors to the accident were the dark night light conditions and the lack of suitable terrain for the forced landing. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of engine power, takeoff - initial climb - reason for occurrence undetermined (cause) - Forced landing, emergency landing after takeoff - In flight collision with terrain/water, landing - flare/touchdown - light condition - dark night (contributing factor) - terrain condition - ravine - terrain condition - rough/uneven - terrain condition - none suitable (contributing factor) ## Analysis The airplane departed for a night cross-country flight, and while climbing through 500 feet agl, the pilot heard a popping sound, which was followed by a complete loss of engine power. The pilot turned on the fuel boost pump and attempted to restart the engine; however, he was not successful. The pilot stated that when the engine lost power the fuel selector was in the right tank position. A forced landing was then executed to an area of rough terrain south of the departure airport. The aircraft came to rest upright in a ravine. Examination of the airplane revealed the left fuel tank was empty, the right fuel tank was full, and the fuselage (header) tank contained 7 gallons of fuel. The fuel selector was found selected to the right tank position. The engine was examined and test run, and no anomalies were noted that would preclude operation of the engine. The reason for the loss of engine power was not determined. ## Factual narrative On October 26, 2001, approximately 2045 central daylight time, a Bellanca 17-30A single-engine airplane, N614CJ, was substantially damaged during a forced landing following a loss of engine power near Clarendon, Texas. The private pilot and the sole passenger were not injured. The airplane was registered to a private individual and operated by the pilot. Night visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The cross-country flight originated from the Clarendon Municipal Airport, Clarendon, Texas, at 2040, with a destination of Plainview, Texas. According to the pilot, the airplane departed the Clarendon Municipal Airport, and climbing through 500 feet in dark, night conditions, he heard a "popping" sound. The engine "hesitated and then returned to normal for only a brief moment before it quit completely." When the engine lost power, the fuel selector was in the right tank position. He then initiated emergency procedures by turning the boost pump on and attempting to restart the engine, which proved unsuccessful. The pilot turned the airplane back toward the departure airport. Subsequently, he determined that he would not be able to "make the airport," and landed the airplane in an area of rough terrain approximately 3 miles south of the departure airport. The aircraft came to rest upright, on a slope in a ravine. An FAA inspector, who responded to the accident site, reported that the right wing sustained structural damage to its front spar, ribs, and leading edge. The left horizontal stabilizer strut was damaged and the landing gear was found separated from the aircraft. All three propeller blades exhibited chord-wise scratching. Two of the propeller blades were bent aft, one of which was bent aft 80-degrees at its root. The outboard portion of one propeller blade was curled aft. The left fuel tank contained no visible fuel and the left wing fuel system was not compromised. The right fuel tank was "completely full" of fuel and the fuselage (header) tank contained approximately 7 gallons of fuel. The fuel selector was selected to the right tank position. The IO-520-K engine was examined and test run by the FAA inspector and a representative of Teledyne Continental Motors. The engine was observed to be intact and crankshaft continuity was confirmed between the propeller and the accessory drive gears. A compression check was performed and the following values were recorded: 70/80, 59/80, 60/80, 24/80, 65/80, and 64/80. The engine was test run using fuel from the fuselage tank. The engine ran for 15 minutes, during which a magneto check was performed and no anomalies were noted. The engine was then run for an additional five minutes using fuel from an outside source. The engine was run at idle, cruise and takeoff power settings, and no anomalies were noted. ## Aircraft - Registration: [N614CJ](https://openairdocs.org/deregistered/N614CJ-2017-05-23), registration cancelled 2017-05-23, S/N 74-30636, built 1973 (OpenAirDocs) - Reported make and model: Bellanca 17-30A - Registry model: [Bellanca 17-30A](https://openairdocs.org/model/bellanca-17-30a) (registry code 1220433) (OpenAirDocs) - Registry engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032, reciprocating) (OpenAirDocs) - Category: Airplane - Serial number: 74-30636 - Airframe hours: 2244.18 - Engines: Continental IO-520 K(1) 300 horsepower reciprocating - Damage: Substantial damage - Flight: Personal, Part 91 - Operator: David L. Williams - Registered owner: Jimmy E. Lofton - Airworthiness certificate: Standard, Normal - Last inspection: Annual, January 22, 2001, 96.48 hours before - Departed: E34, Clarendon, TX - Destination: PVW, Plainview, TX - Airport: E34, Clarendon Municipal Airport ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 29; injuries: none; private; airplane ratings: single-engine land, multi-engine land; medical: class 3, valid medical--no waivers/lim.; last flight review February 28, 2000; seat: left; flight hours: 850 total, 269 in this make and model, 781 as pilot in command, 20 in the last 90 days, 8 in the last 30 days ## Weather - Conditions: Visual (VMC), Night/dark - Visibility: 10 statute miles - Lowest ceiling: none ## 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 20011026029969A](https://openairdocs.org/incident/20011026029969A), Oct 26, 2001: Blanca 1730A, Clarendon, TX, No damage. (-23) Engine lost power during climb out from Clarendon airport. Pilot could not recover the engine and made a forced landing at night in a ravine 3 miles… 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.