# NTSB LAX99LA062: Beech C23, N2313L, Furnace Creek, CA, December 31, 1998 - Type: NTSB accident investigation - Classification: Accident · Minor injuries · Limited investigation · Final report - Date: December 30, 1998, 16:30 local (Dec 31, 1998, 00:30 UTC) - Place: Furnace Creek, CA - Coordinates: 36.599418, -116.829559 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=36.5994&lon=-116.8296&mi=10 - Phase of flight: [Takeoff](https://openairdocs.org/ntsb-phases/300) (OpenAirDocs' grouping) - Highest injury: Minor injuries - Injuries: 2 minor - Status: Completed, report March 31, 2000 - Report: Approved by Office Director - NTSB case key (mKey): 45529 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=LAX99LA062 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/45529/pdf - Page: https://openairdocs.org/ntsb/LAX99LA062 ## Probable cause The pilot's inadequate preflight inspection when he failed to remove the gust lock from the flight controls. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of control - on ground/water, takeoff - roll/run - flight control,gust lock - not removed (cause) - aircraft preflight - inadequate, pilot in command (cause) - Overrun, takeoff - roll/run - aborted takeoff - not performed, pilot in command (contributing factor) - On ground/water encounter with terrain/water, takeoff - roll/run - landing gear,nose gear - separation ## Analysis The private pilot/ owner and his daughter had arrived at Furnace Creek after departing Lancaster earlier that morning. They toured Death Valley National Park for several hours and were preparing to return home. The pilot conducted his preflight check in the tie down area. After back taxiing on the runway and aligning the aircraft for takeoff, he became concerned that he would not be able to see approaching aircraft while he conducted his takeoff checklist. He decided to maintain his position but would expedite without using the written checklist from the glove compartment. He performed his run-up and completed the checks from memory. He announced his departure on Unicom, added full power, and began the takeoff roll. He estimated rotation speed (65 mph) was reached approximately 2/3 of the way down the runway. As he started to pull on the control yoke, he realized the gust lock pin was still in the locked position. He felt that he could not abort the takeoff at this point without departing the end of the runway at a high rate of speed. He attempted to remove the gust lock, which required him to depress a button on the bottom of the pin while pulling down on the shaft. As he was struggling with the pin, the aircraft overran the runway. The nose gear dug into the dirt and was sheared off. He estimated the aircraft came to rest 30-50 yards past the end of the runway. As he secured the cockpit the pilot noticed the key was sheared off, the throttle was pulled out and the shaft was bent down. He also noted that the control lock was on the floor with a broken piece of its neoprene housing. The pilot exited the aircraft behind his daughter. ## Factual narrative On December 30, 1998, about 1630 hours Pacific standard time, a Beech C23, N2313L, sustained substantial damage when it collided with terrain during a takeoff overrun from the Furnace Creek, California, airport. The private pilot/owner and his passenger both received minor injuries. The aircraft departed Lancaster, California, at 1000 for the flight to Furnace Creek. The personal flight was conducted under the provisions of 14 CFR Part 91. After touring Death Valley National Park, the pilot/owner and his daughter were departing for Lancaster when the accident occurred. Visual meteorological conditions prevailed and no flight plan was filed. The pilot stated he performed his preflight in the tie down area. There was no wind so he elected to use runway 15. After checking visually and with Unicom, the pilot proceeded to back taxi on the runway to the departure end since Furnace Creek has no taxiway. He lined up in position for takeoff to conduct his takeoff checklist. He stated he became concerned that he could not see approaching traffic while he was pointed in this direction and considered repositioning so that he could. He maintained this position but decided to forego pulling the written checklist from the glove compartment and did the checklist by memory. After completing his run-up and checks, he announced his departure on Unicom, added full power, and began the takeoff roll. He estimated rotation speed (65 mph) was reached approximately 2/3 of the way down the runway. As he started to pull on the control yoke, he realized the gust lock pin was still in the locked position. He felt that he could not abort the takeoff at this point without departing the end of the runway at a high rate of speed. He attempted to remove the gust lock, which required him to depress a button on the bottom of the pin while pulling down on the shaft. As he was struggling with the pin, the aircraft overran the runway. The nose gear dug into the dirt and was sheared off. He estimated the aircraft came to rest 30-50 yards past the end of the runway. The pilot turned off the magnetos and fuel. He noticed that the key was sheared off and that the throttle was pulled out and bent down sharply. Lying on the floor was the gust lock pin and a broken part of its neoprene housing. Fuel was flowing down the right wing as the pilot followed his daughter out of the aircraft. ## Aircraft - Registration: [N2313L](https://openairdocs.org/deregistered/N2313L-2000-09-15), registration cancelled 2000-09-15, S/N M-139 (OpenAirDocs) - Reported make and model: Beech C23 - Registry model: [Beech 23](https://openairdocs.org/model/beech-23) (registry code 1151202) (OpenAirDocs) - Category: Airplane - Serial number: M139 - Airframe hours: 3000 - Engines: Lycoming O-320-D2B 160 horsepower reciprocating - Damage: Substantial damage - Flight: Personal, Part 91 - Registered owner: Harold Underwood - Airworthiness certificate: Standard, Normal - Last inspection: Annual, September 1, 1998, 12 hours before - Departed: L06 - Destination: WJF, LANCASTER, CA - Airport: L06, Furnace Creek, runway 15, 3,065 × 70 ft, asphalt ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 67; private; airplane ratings: single-engine land; instrument ratings: airplane; medical: class 3, valid medical--w/ waivers/lim; seat: left; flight hours: 1,921 total, 758 in this make and model, 1,921 as pilot in command, 30 in the last 90 days, 10 in the last 30 days, 2 in the last 24 hours ## Weather - Conditions: Visual (VMC), Day - Wind: calm - Visibility: 50 statute miles - Lowest ceiling: none - Temperature: 64 °F ## 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 19981230034409A](https://openairdocs.org/incident/19981230034409A), Dec 30, 1998: Beech C23, Death Valley, CA, Substantial damage. (.19)On December 30, 1998, about 1630 hours pacific standard time, a Beech C23, N2313L, sustained substantial damage when it collided with terrian during a… 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.