Piper PA28R accident near Daytona Beach, FL

On April 4, 2018, a Piper PA28R (airplane) was involved in an accident near Daytona Beach, FL. 2 people died. Damage to the aircraft: destroyed.

Date

April 4, 2018

Place

Daytona Beach, FL

Aircraft

Piper PA28R · Airplane

Injuries

2 fatal, 0 serious, 0 minor

Damage

Destroyed

Position

29.159°N, 81.085°W

NTSB ID

20180404X13226

Official records · ERA18FA120

• Public docket: reports, statements and exhibits from the investigation

Air traffic control records

• Dab Air Traffic Control Communications Transcript Excerpt (Courtesy Of FAA): Transcript (PDF), on ntsb.gov

NTSB summary

HISTORY OF FLIGHTOn April 4, 2018, about 0953 eastern daylight time, a Piper PA-28R-201, N106ER, collided with terrain following an in-flight separation of the left wing near the wing root during climb after a touch-and-go maneuver at Daytona Beach International Airport (DAB), Daytona Beach, Florida. The airline transport pilot and private pilot were fatally injured, and the airplane was destroyed. The airplane was registered to and operated by Embry-Riddle Aeronautical University (ERAU) under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91 as an instructional flight. Day visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed for the local flight. The private pilot was conducting a practical test to obtain a commercial pilot certificate with an airplane single-engine land rating, and the airline transport pilot was acting as a designated pilot examiner (DPE). Radar and voice communication data provided by the Federal Aviation Administration (FAA) and automatic-dependent surveillance broadcast (ADS-B) data provided by the operator revealed that the private pilot began the training flight by departing runway 25L about 0927. The airplane then turned southbound and climbed to about 3,000 ft mean sea level (msl) at a groundspeed of 100 knots. The airplane flew about 14 miles to the south of DAB, and several climbing and descending turns occurred between 1,300 and 3,000 ft. About 0940 the airplane leveled off at an altitude about 2,200 ft and airspeed of 112 knots on an easterly ground track before turning northbo

Probable cause

Extensive fatigue cracking in the left-wing main spar lower cap and doublers, which resulted in the in-flight separation of the left wing. The fatigue cracks initiated and grew to a critical size due to flight and ground loads associated with flight-training involving flight-training maneuvers, significant operation at low altitudes and frequent landing cycles. Previously established inspection cr

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Source: NTSB aviation accident database (US government, public domain). Findings may be preliminary or later revised by the NTSB. Not a complete global record.