Skip to content

Atlas / NTSB / GAA15CA273

NTSB CAROL · Event

Event GAA15CA273

2015-09-19 Marshfield, Massachusetts, United States Airport · GHG None 1 aircraft Status: Completed

Registry · N6932K

FAA Aircraft Registry record.

Make / Model

PIPER PA-20

Year of manufacture

1950 · 65 years old at event

Engine

LYCOMING 0-290 SERIES (140 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19560505

ADS-B equipped

Yes — Mode-S A93883

Registrant of record

HODGE TYLER

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's loss of directional control during the landing roll, which resulted in a ground loop and impact with terrain.

Factual narrative

The pilot of the tailwheel-equipped airplane reported that on final approach, he realized he was above the normal glide path and performed a forward slip to lose altitude. At the conclusion of the slip, the airplane had a higher than normal approach airspeed. The pilot planned to make a wheel landing and when the airplane touched down, it landed hard, and bounced twice. The pilot then decided to alter his landing to a three point landing after the bounce. At touchdown the airplane "fishtailed" and started to veer left. The pilot was unable to correct the veer with control inputs, the airplane continued off the runway to the left and ground looped. The airplane sustained substantial damage to the right wing, elevator, horizontal stabilizer, and fuselage. The pilot reported no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot of the tailwheel-equipped airplane reported that on final approach, he realized he was above the normal glide path and performed a forward slip to lose altitude. At the conclusion of the slip, the airplane had a higher than normal approach airspeed. The pilot planned to make a wheel landing and when the airplane touched down, it landed hard, and bounced twice. The pilot then decided to alter his landing to a three point landing after the bounce. At touchdown the airplane "fishtailed" and started to veer left. The pilot was unable to correct the veer with control inputs, the airplane continued off the runway to the left and ground looped. The airplane sustained substantial damage to the right wing, elevator, horizontal stabilizer, and fuselage. The pilot reported no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C

Verbatim from NTSB's published report. Source file NTSB_2015_GAA15CA273.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.