NTSB CAROL · Event
Event WPR14CA120
Registry · N5626H
FAA Aircraft Registry record.
Make / Model
PIPER PA-16
Year of manufacture
1949 · 65 years old at event
Engine
LYCOMING 0-235 SERIES (115 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19560618
ADS-B equipped
Yes — Mode-S A7318A
Registrant of record
WHITMORE MARTHA J
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during landing roll. Contributing to the accident was the pilot's diverted attention and inadequate preflight inspection.
Factual narrative
The pilot reported that prior to the flight he removed an insulating blanket and heat source from the tailwheel equipped airplane, and conducted his preflight inspection. Following a normal engine run up, he initiated takeoff, where he thought the airplane seemed sluggish and that the rate of climb didn't feel normal. The pilot determined that the engine was not making full power, and decided to land at a nearby airport with a larger runway. Following an uneventful landing, the pilot diverted his attention to the engine instruments. Subsequently, the airplane swerved to the right, and the right main landing gear folded underneath the fuselage, which resulted in the right wing striking the ground. Postaccident examination of the airplane by the pilot revealed that the right wing spar was bent. The pilot added that he found an insulating cover over the carburetor air intake and that was the reason for the reduced power. The pilot reported that prior to the flight he removed an insulating blanket and heat source from the tailwheel equipped airplane, and conducted his preflight inspection. Following a normal engine run up, he initiated takeoff, where he thought the airplane seemed sluggish and that the rate of climb didn't feel normal. The pilot determined that the engine was not making full power, and decided to land at a nearby airport with a larger runway. Following an uneventful landing, the pilot diverted his attention to the engine instruments. Subsequently, the airplane swerved to the right, and the right main landing gear folded underneath the fuselage, which resulted in the right wing striking the ground. Postaccident examination of the airplane by the pilot revealed that the right wing spar was bent. The pilot added that he found an insulating cover over the carburetor air intake and that was the reason for the reduced power. 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
- F Personnel issues-Task performance-Inspection-Preflight inspection-Pilot - F
- F Personnel issues-Psychological-Attention/monitoring-Attention-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2014_WPR14CA120.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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