ANC13CA055
2013-06-11 · Juneau, Alaska, United States · None · 1 aircraft · Status: Completed
Airport PAJN
Current FAA registration · N1886P
- Make / Model
- PIPER PA-18A 150
- Year of manufacture
- 1955 · 58 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 1 seats · 1 engine
- Last airworthiness date
- 19930823
- ADS-B equipped
- Yes — Mode-S A1619C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot did not maintain directional control while attempting to recover from a bounced landing.
Factual narrative
The pilot stated that she was flying the airplane from the front seat, and the airplane owner (who is also a pilot) was in the rear seat. The pilot in the front seat turned final early to maintain aircraft separation and made a short and slightly steep final. She said she flared the airplane a little high and it bounced twice during the landing. During the second bounce, the pilot in the rear seat assisted the recovery by applying corrective input. The pilot in the front seat could not recall if she continued to apply control inputs or if the pilot in the rear seat had assumed the controls. Positive control transfer was not accomplished. The airplane subsequently ground looped to the right, substantially damaging the left wing when the wing tip struck the runway. The pilot reported no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot stated that she was flying the airplane from the front seat, and the airplane owner (who is also a pilot) was in the rear seat. The pilot in the front seat turned final early to maintain aircraft separation and made a short and slightly steep final approach. She said that while landing she flared the airplane a little high, and it bounced twice during the landing. During the second bounce, the pilot in the rear seat assisted the recovery by applying corrective input. The pilot in the front seat could not recall if she continued to apply control inputs or if the pilot in the rear seat had assumed the controls. Positive control transfer was not accomplished. The airplane ground looped to the right, substantially damaging the left wing when the wing tip struck the runway. The pilot reported no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2013_ANC13CA055.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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