# NTSB ATL00FA019: Bellanca BL-17-30A, N8821V, Monteagle, TN, January 1, 2000 - Type: NTSB accident investigation - Classification: Accident · Fatal · Field investigation · Final report - Date: January 1, 2000, 13:02 local (19:02 UTC) - Place: Monteagle, TN - Coordinates: 35.239204, -85.839973 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=35.2392&lon=-85.8400&mi=10 - Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping) - Highest injury: Fatal - Injuries: 2 fatal - Status: Completed, report April 19, 2001 - Report: Approved by Office Director - NTSB case key (mKey): 48389 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=ATL00FA019 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/48389/pdf - NTSB docket: https://data.ntsb.gov/Docket?ProjectID=48389 - Page: https://openairdocs.org/ntsb/ATL00FA019 ## Probable cause The pilot's failure to adequately evaluate weather conditions that resulted in the continuation of visual flight into instrument weather conditions and the subsequent collision with trees. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - In flight encounter with weather, cruise - weather condition - low ceiling (cause) - vfr flight into imc - continued, pilot in command (cause) - preflight planning/preparation - inadequate, pilot in command (cause) - In flight collision with object, cruise - object - tree(s) ## Analysis Circumstances of the history of flight are not known. The intended route of flight was not determined, a review of the Federal Aviation Administration Flight service system failed to disclose that the pilot had received a pre-flight weather briefing for the intended flight. The flight was first heard only seconds before the airplane collided with trees. Subsequent to the collision, smoke was sighted in the vicinity of the accident site. Upon arriving at the accident site, rescue personnel noticed that fog and low clouds were about 20 feet above the ground, and the mountain top was obscured. Examination of the engine and airframe failed to disclose a mechanical malfunction or the failure of related component assemblies. ## Factual narrative HISTORY OF FLIGHT On January 1, 2000, at 1302 central standard time, a Bellanca BL-17-30A, N8821V, collided with trees and burst into flames in a heavily wooded area near Monteagle, Tennessee. The personal flight was operated by the pilot under the provisions of Title 14 CFR Part 91 with no flight plan filed. Instrument weather conditions prevailed at the time of the accident. The airplane was destroyed; the private pilot and his passenger were fatally injured. According to the initial report from local law enforcement authorities, the flight departed Asheville, North Carolina, at an undetermined time, and the exact route of flight was not known. Reportedly, the pilot and his passenger spent the evening prior to the accident at a local hotel in Asheville, North Carolina. Circumstances of the history of flight are also not known. The flight departed Asheville, North Carolina, at an undetermined time on the morning of the accident. The intended route of flight was not determined, a review of the Federal Aviation Administration Flight service system failed to disclose that the pilot had received a pre-flight weather briefing for the intended flight. The flight was first heard only seconds before the airplane collided with trees. According to a witness near the accident site, he heard the airplane overhead followed by a high revving engine sound and the sound of the airplane colliding with trees. Another witness reported hearing an explosion during the sequence of events. Subsequent to the collision, smoke was sighted in the vicinity of the accident site. Within minutes of the collision, emergency response personnel from surrounding counties were on site. According to Monteagle Chief of Police, upon arriving at the accident site, he noticed that fog and low clouds were about 20 feet above the ground, and the mountain top was obscured. PERSONNEL INFORMATION The pilot held a private pilot certificate with airplane single-engine land, and instrument ratings. A review of pilot information from the Federal Aviation Administration (FAA), his total flight time was 400 hours but the approximately flying time in the Bellanca BL-17-30A was not determined. The pilot held a current third class medical certificate, dated August 10, 1999, valid with no waivers or limitations. AIRCRAFT INFORMATION The four place Bellanca BL-17-30A airplane, N8821V, was owned and operated by the pilot. N8821V was powered by a fuel injected, 300 horse power Continental Motors IO-520-K engine. A review of the airplane maintenance logbooks showed that the last annual inspection was completed on July 28, 1999. The airframe tachometer was not recovered at the accident site, however, according to the airframe maintenance logbook the last entry was recorded on December 24 1999, at 1916.5 hours. METEOROLOGICAL INFORMATION A review of weather data from reporting facilities in the vicinity of the accident site showed the following observations: The Chattanooga 1353 weather observation reported broken clouds at 300 feet with 1.75 miles visibility: the altimeter setting was 30.15 inches of mercury. The winds were light and variable. The area forecast for middle Tennessee at the approximate time of the accident called for broken cloud conditions between 2000 and 3000 feet, and visibility under the cloud layer between 3 and 5 miles. Marginal visual flight rule weather conditions were also forecasted for middle Tennessee. A review of the FAA flight service files failed to show that the pilot had received a preflight or inflight weather briefing. WRECKAGE AND IMPACT INFORMATION Examination of the accident site disclosed that wreckage debris was scattered over an area approximately 800 feet long and 60 feet wide. Wreckage debris was orientated on a northwesterly magnetic heading. Several freshly broken trees were scattered along the wreckage path. Fire damage was confined to the last third of the wreckage path. The main wreckage, which consisted of the cockpit and center section of the airframe, was heavily fire damaged. Further examination of the airframe disclosed that the airplane rested inverted at the accident site. Several pieces of the airframe including engine cowling were torn from the airplane and were scattered throughout the length of the wreckage path. Other wreckage debris was lodged in trees along the wreckage path. The engine assembly was located approximately 100 feet northwest of the main wreckage. Examination of the engine assembly revealed that many externally installed components were torn from their normally installed positions. Further examination of the engine showed a large hole on the top and front portions of engine case halves. The three propeller blades separated from the engine assembly. One propeller blade rested 48 feet northwest of the main wreckage the second and third propeller blades remained attached to the hub assembly and was 39 feet east of the main wreckage. Examination of the propeller blades showed twisting and chordwise scraping on each blade. The examination of the engine failed to disclose a system malfunction or a component failure. Examination of the remainder of the airframe also failed to disclose a mechanical malfunction or the failure of related component assemblies. MEDICAL AND PATHOLOGICAL INFORMATION On January 3, 2000, a limited postmortem examination of the pilot was performed by Dr. Charles Harlan at the office of the Forensic Pathology Association in Nashville, Tennessee, The toxicology examinations were performed by the FAA Toxicology and Accident Research Laboratory, Oklahoma City, Oklahoma. The tests were negative for carbon monoxide, cyanide, drugs and alcohol. ADDITIONAL INFORMATION The airplane wreckage was released on August 30, 2000 to Mr. Kevin Twist, an insurance adjuster, Atlanta, Georgia. ## Aircraft - Registration: [N8821V](https://openairdocs.org/deregistered/N8821V-2000-07-24), registration cancelled 2000-07-24, S/N 30345 (OpenAirDocs) - Reported make and model: Bellanca BL-17-30A - Registry model: [Bellanca 17-30A](https://openairdocs.org/model/bellanca-17-30a) (registry code 1220433) (OpenAirDocs) - Category: Airplane - Serial number: 30345 - Airframe hours: 1888 - Engines: Continental IO-520-K 300 horsepower reciprocating - Damage: Destroyed - Fire: On-Ground - Flight: Personal, Part 91 - Registered owner: John R. Jackson - Airworthiness certificate: Standard, Normal - Last inspection: Annual, July 28, 1999, 26 hours before - Departed: AVL, ASHEVILLE, NC - Destination: JACKSON, IN ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 56; private; airplane ratings: single-engine land; instrument ratings: airplane; medical: class 3, valid medical--no waivers/lim.; seat: left; toxicology performed; flight hours: 400 total ## Weather - Conditions: Instrument (IMC), Day - Visibility: 1.75 statute miles - Lowest ceiling: 300 ft broken - Temperature: 55 °F, dew point 55 °F - Altimeter: 30.00 inHg - Observed at: CHA, 30 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 20000101008419A](https://openairdocs.org/incident/20000101008419A), Jan 1, 2000: Blanca 1730A, Monteagle, TN, Destroyed, 2 fatal. (-23) See attached narrative NTSB#ATLOOFA019 (.4) the four place Bellanca BL-17-30A airplane, N8821V, was owned and operated by the pilot. N8821V was powered… ## Docket (17 files) The files NTSB released with the investigation on March 6, 2001, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=48389. 3.3 MB in all. - Supplement A (item 1, .PDF, 257 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133764&FileExtension=.PDF&FileName=Supplement%20A-Master.PDF - Supplement S (item 2, .PDF, 58 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133765&FileExtension=.PDF&FileName=Supplement%20S-Master.PDF - Witness Statements (item 3, .PDF, 326 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40437834&FileExtension=.PDF&FileName=Witness%20Statements-Redacted.PDF - Weather Reports and Records (item 4, .PDF, 977 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40437835&FileExtension=.PDF&FileName=Weather%20Reports%20and%20Records-Redacted.PDF - Statement of Party Representatives to NTSB Investigation (item 5, .PDF, 124 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40437837&FileExtension=.PDF&FileName=Statement%20of%20Party%20Representatives%20to%20NTSB%20Investigation-Redacted.PDF - Release of Aircraft Wreckage, NTSB Form 6120.15 (item 6, .PDF, 56 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40437838&FileExtension=.PDF&FileName=Release%20of%20Aircraft%20Wreckage,%20NTSB%20Form%206120.15-Redacted.PDF - Toxicological Report (item 7, .PDF, 142 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133770&FileExtension=.PDF&FileName=Toxicological%20Report-Master.PDF - Wreckage Diagram (item 8, .PDF, 123 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133771&FileExtension=.PDF&FileName=Wreckage%20Diagram-Master.PDF - 1. View of wreckage path-note swath through trees (item 9, .PDF, 71 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133772&FileExtension=.PDF&FileName=1.%20View%20of%20wreckage%20path-note%20swath%20through%20trees-Master.PDF - 2. Propeller hub with one blade attached (item 10, .PDF, 62 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133773&FileExtension=.PDF&FileName=2.%20Propeller%20hub%20with%20one%20blade%20attached-Master.PDF - 3. Main wreckage-center section, note extensive fire damage (item 11, .PDF, 55 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133774&FileExtension=.PDF&FileName=3.%20Main%20wreckage-center%20section,%20note%20extensive%20fire%20damage-Master.PDF - 4. Engine and propeller blade (item 12, .PDF, 69 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133775&FileExtension=.PDF&FileName=4.%20Engine%20and%20propeller%20blade-Master.PDF - 5. Engine assembly (item 13, .PDF, 61 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133776&FileExtension=.PDF&FileName=5.%20Engine%20assembly-Master.PDF - 6. Magneto assembly torn from engine (item 14, .PDF, 59 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133777&FileExtension=.PDF&FileName=6.%20Magneto%20assembly%20torn%20from%20engine-Master.PDF - 7. Freshly cut tree branch at accident site (item 15, .PDF, 46 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133778&FileExtension=.PDF&FileName=7.%20Freshly%20cut%20tree%20branch%20at%20accident%20site-Master.PDF - Supplement B (item 16, .PDF, 368 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40133779&FileExtension=.PDF&FileName=Supplement%20B-Master.PDF - Airframe and Maintenance Log Books (item 17, .PDF, 473 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40437839&FileExtension=.PDF&FileName=Airframe%20and%20Maintenance%20Log%20Books-Redacted.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.