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Accidents · NTSB CEN20LA082 · Final report

Cessna 560 accident near Aledo, Texas, February 12, 2020

On February 12, 2020 at about 9:27 pm local time, a 2004 Cessna 560, registered N654CE, was substantially damaged in an accident during enroute near Aledo, Texas. It was an executive or corporate flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The in-flight separation of the upper and lower right engine cowlings for reasons that could not be determined based on available evidence.

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

What the record shows

Date
February 12, 2020 · about 9:27 pm local time
Place
Aledo, Texas · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Cessna 560 ENCORE, built 2004 · all 560s on the register
Registration
N654CE · no longer on the register · serial 5600654
Damage
Substantial damage
Flight
Executive or corporate flight · general aviation rules (Part 91)

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

The air transport pilot of the twin-engine jet heard a "loud crashing noise" followed by a "turbulent air sound." The pilot reported everything checked out normal except the "turbulent air sound," which was exacerbated with rudder movement. The flight diverted and continued to a normal landing. A postflight inspection revealed the upper and lower cowlings for the No. 2 (right) engine were missing. A portion of the separated cowlings was found wrapped around the inboard section of the right horizontal stabilizer. Another portion of the separated cowlings impacted the area between the leading edge of the vertical stabilizer and the top of the fuselage, resulting in substantial damage. The remaining pieces of the separated cowlings have not been recovered. On-scene examination revealed that receptacle 29, at the forward inboard side of the lower cowl door, was missing its stud, snap ring, and grommet and that receptacles 26 and 28 were missing their grommets and snap rings but had retained their studs. All other receptacles had retained their attachment hardware. Receptacle 29 was visually examined for indications of damage or wear and the locking features on the backside of the cup were compared against an exemplar cup. There were no apparent indications of damage or wear that could have contributed to the stud cross-pin pulling out or rotating out of the locked position. The fracture surfaces on the two cowl pieces were examined for indications of fatigue, but none were found. The most likely cause of the cowl door departure is that either the stud at receptacle 29 was left unlocked when the cowl door was attached, or an oversized stud was used at receptacle 29 that was able to rotate from the locked to unlocked position. Without the stud to examine and additional on-wing testing, it cannot be determined whether the stud at that location was a longer grip-length stud or if spontaneous unlocking of a longer grip-length stud is an actual possibility. The reason for the separation of the cowlings could not be determined because the stud in question was not recovered.

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. Part(s) separation from AC during enroute defining event
  2. Attempted remediation/recovery during enroute
  3. Off-field or emergency landing during enroute
  4. Unknown or undetermined during enroute

The NTSB's findings

  • Aircraft › Aircraft power plant › Power plant › Engine cowling system › Unknown/Not determined
  • Aircraft › Aircraft power plant › Power plant › Engine cowling system › Failure
  • Aircraft › Fluids/misc hardware › Misc hardware › Fasteners › Unknown/Not determined

Pilot

  • Certificate: airline transport pilot, flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 6,151 hours in all; 753 in this make and model; 103 in the last 90 days; 42 in the last 30 days; 5,870 as pilot in command; 799 on instruments
  • Last flight review: June 14, 2019
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 3,666.3 hours
  • Last inspection: approved inspection programme, December 17, 2019
  • Maximum gross weight: 16,630 lb
  • Seats: 11
  • Landing gear: retractable
  • Engine 1: Pratt & Whitney Canada PW535A (turbofan); 3,666 hours total
  • Engine 2: Pratt & Whitney Canada PW535A (turbofan); 3,666 hours total
  • Operator: Sc Cole Aviation, LLC

The flight

  • Departed from: DAL Dallas TX at 9:17 pm
  • Destination: MAF Midland TX
  • Flight plan: IFR

Weather at the time

  • Light: daylight
  • Wind: from 270° at 11 knots
  • Visibility: 7 statute miles
  • Sky: overcast at 2,200 ft
  • Temperature: 48°F (9°C), dew point 41°F (5°C)
  • Altimeter: 29.85 inHg
  • Observation at 2:52 pm from KNFW

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

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

8 documents, released by the NTSB on May 10, 2022. 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.