- Date
- August 6, 2023, 20:00 local (Aug 7, 2023, 01:00 UTC)
- Place
- Holliday, TX · Grass field on private property
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Approach
- Aircraft
- N2005JTaylorcraft F21
- Defining event
- Approach-VFR pattern final: Unknown or undetermined
- Weather
- Visual (VMC) · Dusk
- Status
- Completed
- Report
- Approved by Office Director
- Investigation class
- Class 3
- NTSB office
- Central Region
- Parties
- FAA Lubbock FSDO
- FAA report
- 20230806010809A
- Case key
- 192814
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
A loss of engine power for reasons that could not be determined, which resulted in impact with terrain.
Findings · 2
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The pilot was landing the airplane at a private runway when he added additional engine power to clear trees and reach the runway. The pilot started to apply the throttle, but the airplane continued to sink. The pilot then applied full engine power to execute a go-around, but realized the engine was not producing power. The pilot observed that the engine did not stop operating but was not responsive to his throttle inputs. The pilot did not hear any abnormal noises from the engine, noting “[t]here were no coughing or sputtering noises to my recollection.” The left wing impacted a tree about 30 ft short of the runway and the airplane came to rest upright on a grass field. The pilot shut down the airplane and the two occupants egressed without further incident. The airplane sustained substantial damage to the fuselage and both wings. Postaccident examination of the airframe and engine found no mechanical anomalies. The pilot reported that the throttle cable might have been the potential cause for the lack of response from the engine, as there was a previous problem with the throttle cable “slipping.” During the postaccident examination, the throttle was found installed, intact, and there were no signs of any missing hardware. Although the pilot reported that he was not using carburetor heat on the approach, he indicated that on the final approach he was “carrying some power.” Additionally, the weather conditions at the time of the accident were not conducive to carburetor icing. Accordingly, the reason for the loss of engine power and the engine’s unresponsiveness to the pilot’s throttle inputs could not be determined.
Factual narrative
On August 6, 2023, about 2000 central daylight time, a Taylorcraft Aviation Corporation F21 airplane, N2005J, sustained substantial damage when it was involved in an accident near Holliday, Texas. The pilot and the passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot departed from a private grass airstrip near Holliday, Texas, for the local flight. While established on the approach to the airstrip, the pilot felt the airplane needed additional engine power to clear trees and reach the runway. The pilot started to apply the throttle, but the airplane continued to sink. The pilot then applied full engine power to execute a go-around but realized that the engine was not producing power. The pilot observed that the engine did not stop operating but was not responsive to his throttle inputs. The pilot did not hear any abnormal noises from the engine, noting “[t]here were no coughing or sputtering noises to my recollection.” The left wing impacted a tree about 30 ft short of the airstrip and the airplane came to rest upright on a grass field. The pilot shut down the airplane and the two occupants egressed without further incident. The airplane sustained substantial damage to the fuselage and both wings. Postaccident examination of the airframe revealed flight control continuity. The two wing fuel tanks were found intact. The wing tanks fed into a header tank, which appeared to be intact and full of fuel. Engine control continuity was established from the cockpit. Examination of the engine found no mechanical anomalies. The pilot reported that he was not using carburetor heat on the approach. He stated that he was on a mile final and was carrying some power. Comparison of the weather conditions at the time of the accident to the Federal Aviation Administration’s Special Airworthiness Information Bulletin CE-09-35 indicated that the conditions were not conducive to carburetor icing. The pilot reported that the throttle cable might have been the potential cause for the lack of response from the engine, as there was a previous problem with the throttle cable “slipping.” The throttle cable was adjusted by a mechanic on March 18, 2023, about four and a half months before the accident, and the pilot reported that the maintenance work corrected the slippage issue. During the postaccident examination, the throttle was found installed, intact, and there were no signs of any missing hardware. When the pilot purchased the airplane in September 2022, the most recent annual inspection had been completed in November 2011. A mechanic performed an annual inspection on the airframe and the engine on October 28, 2022.
Aircraft
- Registration
- N2005J
- Reported as
- Taylorcraft F21 (NO SERIES)
- Category
- Airplane
- Serial number
- F-1014
- Built
- 1981
- Airframe hours
- 1,388.77
- Engine
- Lycoming Engines O-235-L2C, 115 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Standard, Utility; Standard, Normal
- Last inspection
- Annual · October 28, 2022
- Departed
- Holliday, TX
- Equipment
- ADS-B
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 21
- Injuries
- None
- Certificate
- Commercial
- Airplane ratings
- Single-engine land
- Medical
- Class 1, Without waivers/limitations
- Last flight review
- May 2, 2023
- Seat
- Left
- Restraint
- 3-point
- Flight hours
- 535.4 total · 281.7 in this make and model · 454.6 as pilot in command · 100.1 in the last 90 days · 39.5 in the last 30 days
Weather
- Conditions
- Visual (VMC) · Dusk
- Wind
- 170° at 7 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- 11,000 ft broken
- Temperature
- 106 °F, dew point 59 °F
- Altimeter
- 29.86 inHg
- Observed at
- KCWC, 20 nm away
- METAR
- KCWC 070055Z AUTO 15006KT 10SM BKN110 41/15 A2986 RMK AO2 T04070146
Docket · 9
The files NTSB released with the investigation on April 18, 2024, on NTSB’s docket system: statements, records, photos and specialists’ reports. 40.9 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.
Other investigations on N2005J · 1
Matched to the same aircraft by N-number and date.