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CEN17FA196 · Piper J3C 65

24 May 2017 · Chetek, WI, United States

Piper J3C 65 · Accident: loss of control in flight while maneuvering

From Chetek, WI to Chetek, WI

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Event

NTSB case
CEN17FA196
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
1 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Piper J3C 65

Aircraft type
Piper J3
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N35132
Operator
Unknown
Onboard fatalities
Unknown
Route
From Chetek, WITo Chetek, WI
Aircraft age
About 76 years (built 1941)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Maneuvering
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of control in flight
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Aircraft › Aircraft oper/perf/capability
  • Personnel issues › Task performance

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

The private pilot and the passenger were on a local flight in the airplane; the pilot was seated in the rear seat and the passenger was in the front seat. Several witnesses, located west of the accident location, observed the airplane flying low, heading north, just west of a river. After overflying several people on a pond, the airplane continued to the north briefly and then started a right turn. The nose of the airplane dropped, and the airplane descended rapidly below the tree line. The passenger stated that the airplane started to turn and then went straight down. The airplane impacted the river and came to rest in the water. The passenger, who was seated in the front seat, did not recall exiting the airplane but did recall being underwater, surfacing, and swimming to the bank of the river. The pilot, who was seated in the rear seat, was ejected from the airplane and found face down in the water when first responders arrived.

Examination of the airplane indicated that it impacted the river in about a 45° nose-down attitude. No evidence was found of any preimpact mechanical malfunctions or failures with the airframe, flight controls, engine, or related systems that would have precluded normal operation. Witness statements, the passenger's statement, and the damage to the airplane are consistent with an aerodynamic stall followed by an uncontrolled descent and impact with the river.

An examination of the lap belts and shoulder harnesses in the airplane revealed that the front and rear lap belts were buckled; the front and rear shoulder harness straps were not attached to the buckles; and one side of each lap belt was not attached to its mounting bracket. For the rear seat, the left mounting bracket for the lap belt had failed in overload likely during the impact sequence. For the front seat, the left-side webbing of the lap belt was found not attached to the mounting bracket, and the right-side webbing of the lap belt was found knotted to the mounting bracket, which was an improper method for attaching the belt to the bracket. The pilot had fastened the lap belt for the passenger before the flight; had the webbing not been secured at that time, it is likely that the passenger and the pilot would have noted that fact. Therefore, it is likely that the left-side webbing was also knotted to the wire bracket and came undone during the impact sequence.

Based on the passenger's statement that he was not wearing a shoulder harness, the inflight video taken by the passenger, and the postaccident finding that the front and rear seat shoulder harness straps were not attached to the buckled lap belts, it is apparent that neither the pilot nor the passenger were using the shoulder harness portions of their restraint system at the time of the accident. The damage to the airplane, the location of the pilot following the accident, and the injuries to both the pilot and the passenger are consistent with the pilot being ejected forward, into the back of the front seat, and then likely out the front windscreen of the airplane. The passenger's facial injuries were consistent with the passenger impacting the airplane's instrument panel.

Investigators were unable to determine what method, if any, was used to approve the installation of the shoulder harness. It is unknown if the seatbelts and shoulder harnesses installed were part of a properly certified restrain system. Without the method of certification or approval of the restraint system, investigators were further unable to determine what role the failure to use the restraint system played in the pilot's ejection, mitigation of the pilot's injuries, and protection from injuries for the front seat occupant. However, both occupants likely would have benefited from the use of a properly certificated and installed four-point restraint system in this accident.

Probable cause

The pilot's failure to maintain control of the airplane while flying at a low altitude, which resulted in the airplane exceeding the critical angle of attack and a subsequent aerodynamic stall.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CEN17FA196
Event ID
20170524X33247
Case number
CEN17FA196
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 595a911bc9da25b81becaf4ecd7434b8c6022a0932b1d1f5eba9012fc31601d7; retrieved 2026-09-15T06:02:52.496Z.