WPR13CA097
2013-01-21 · Tucson, Arizona, United States · None · 1 aircraft · Status: Completed
Airport RYN
Current FAA registration · N223PE
- Make / Model
- CESSNA 140
- Year of manufacture
- 1946 · 67 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 20031216
- ADS-B equipped
- Yes — Mode-S A1ED70
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain directional control during the landing roll and his excessive application of brakes, which resulted in a noseover.
Factual narrative
The pilot stated that he was returning to the departure airport and completed a normal traffic pattern for the active runway. After touchdown, he attempted to hasten the landing roll and exit off the runway at the first turnoff to accommodate the airplane that was landing after him. The tail wheel and rudder began to shimmy and in response he manipulated the control wheel forward. He then applied brake pressure in an attempt to make the exit and the airplane lurched forward, coming to rest inverted on the runway. The wings, fuselage, and rudder were substantially damaged. The pilot stated that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. He additionally reported that he thought the accident may have been prevented if he increased his yearly flying time and flew with an instructor more frequently. The pilot stated that he was returning to the departure airport and completed a normal traffic pattern for the active runway. After touchdown, he attempted to hasten the landing roll and exit off the runway at the first turnoff to accommodate the airplane that was landing after him. The tailwheel and rudder began to shimmy and, in response, the pilot manipulated the control wheel forward. He then applied brake pressure in an attempt to make the exit, and the airplane lurched forward, coming to rest inverted on the runway. The wings, fuselage, and rudder were substantially damaged. The pilot stated that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. He additionally reported that he thought the accident may have been prevented if he increased his yearly flying time and flew with an instructor more frequently. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-(general)-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Aircraft-Aircraft systems-Landing gear system-Landing gear brakes system-Incorrect use/operation - C
Verbatim from NTSB's published report. Source file
NTSB_2013_WPR13CA097.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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