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Accidents · NTSB WPR18FA035 · Final report

Cessna 152 accident near Tehachapi, California, November 20, 2017

On November 20, 2017 at about 1:56 am local time, a 1977 Cessna 152, registered N24987, was destroyed in an accident during maneuvering near Tehachapi, California (Tehachapi Municipal airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's loss of situational awareness shortly after takeoff over a sparsely lit area in dark night conditions, which resulted in a rapid descent to ground impact.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
November 20, 2017 · about 1:56 am local time
Place
Tehachapi, California · Tehachapi Municipal · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Cessna 152 NO SERIES, built 1977 · all 152s on the register
Registration
N24987 · no longer on the register · serial 15280496
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The private pilot departed on a personal flight in visual meteorological conditions during the early evening and flew to a nearby airport, where he parked the airplane and walked to a nearby restaurant. He returned to the airplane about an hour later, which was about 20 minutes after the end of civil twilight. Surveillance video captured the accident airplane depart the runway and enter a right traffic pattern, which was the opposite of the published left traffic pattern and took the airplane over unlit pasture and hills. The imagery then depicted the airplane enter a rapid descent on what appeared to be the right downwind leg of the traffic pattern. The airplane disappeared from view consistent with ground impact. The descent duration was about 7 seconds. The airplane impacted a pasture north of the airport. The debris field indicated that the airplane impacted the ground with a relatively shallow flight path angle, in a nose- and right-wing low attitude, with a significant amount of horizontal energy. All major airplane and engine components were identified in the wreckage, and no indications of any pre-impact mechanical deficiencies or failures were observed. The flaps were in the fully retracted position, which was the climb-cruise configuration, likely indicative that the pilot was not attempting a landing when the impact occurred. The undamaged condition of the artificial horizon gyro rotor and internal case suggested a possibility that the device was not operating, but the actual operating status of the instrument at the time of the accident could not be determined. Even if the artificial horizon was inoperative, external visual references should have been sufficient to enable the pilot, albeit possibly with some difficulty, to maintain the proper airplane attitude and flight path. Some fibrous lint-like material was found in the carburetor fuel inlet screen; the material was foreign to the airplane fuel system, but it was not determined when or by what means the lint was introduced into the system. The lint did not appear to have any adverse effect on engine operation; propeller damage was consistent with the engine developing significant power at the time of impact. Airplane fueling information and published performance data indicated that the airplane had sufficient fuel onboard for a return flight to the airport of origin. About 5 weeks before the accident, the pilot had completed a night flight in the accident airplane from his home airport to the accident airport and back, which indicated that he was at least somewhat familiar with the accident airport. The reason for the pilot's use of a right traffic pattern instead of the designated left traffic pattern for his departure could not be determined. Although the pilot had documented color vision deficiencies, this condition likely did not contribute to the accident sequence. The pilot had relatively limited total and night flying experience, and the night and local terrain were very dark. Given the signatures of engine power and lack of mechanical anomalies found during postaccident examination, it is not likely that the accident was the result of a loss of engine power. Further, correlation of debris field information with the descent angle depicted in the surveillance imagery frames indicated that the descent path was too shallow to be consistent with an aerodynamic stall. Additionally, the airplane's impact attitude and the distribution of the wreckage were inconsistent with a loss of control due to spatial disorientation. It is possible that the pilot lost his situational awareness while maneuvering onto the right downwind leg which resulted in the airplane descending rapidly to ground impact.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Loss of control in flight during maneuvering defining event
  2. Abrupt maneuver during maneuvering
  3. Collision with terrain or object (not controlled flight into terrain) during maneuvering

The NTSB's findings

  • cause Personnel issues › Psychological › Perception/orientation/illusion › Situational awareness › Pilot
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • cause Environmental issues › Conditions/weather/phenomena › Light condition › Dark › Effect on personnel
  • cause Environmental issues › Conditions/weather/phenomena › Light condition › Dark › Effect on operation

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 152 hours in all; 6 in the last 90 days; 3 in the last 30 days
  • Last flight review: August 22, 2017
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 11,168 hours
  • Last inspection: 100-hour inspection, September 29, 2017
  • Maximum gross weight: 1,669 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming O-235 SERIES (piston); 0 hours total

The flight

  • Departed from: TSP Tehachapi CA at 1:55 am
  • Flight plan: none

Weather at the time

  • Light: night, dark
  • Wind: from 320° at 3 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 50°F (10°C), dew point 32°F (0°C)
  • Altimeter: 30.12 inHg
  • Observation at 1:55 am from TSP

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

13 documents, released by the NTSB on October 30, 2019. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.