FLIGHT FINDINGSAVIATION OCCURRENCE MAP
Back to map

CEN10LA052 · Piper PA-34-200T

17 Nov 2009 · Saginaw, TX, United States

Piper PA-34-200T · Accident: system/component malfunction/failure (non-power) during initial climb

From Hicks Air Field (T67) to Arlington Municipal Airport (GKY)

Report a problem

Event

NTSB case
CEN10LA052
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
0 · 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 PA-34-200T

Aircraft type
Piper PA-34
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
N8297P
Operator
Glen R. Smith, Jr · private individual
Onboard fatalities
Unknown
Route
From Hicks Air Field (T67), Fort Worth, TXTo Arlington Municipal Airport (GKY), Arlington, TX
Aircraft age
Not recorded
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
Initial climb
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
System/component malfunction/failure (non-power)
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 systems

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

NTSB narrative

The pilot said that he took off and did not engage the autopilot, but did use the electric trim switch on the control yoke to establish a climb attitude after takeoff. When he activated the trim switch, the airplane "pitched down rapidly." Despite his application of full up elevator to arrest the descent, the airplane continued to descend. The pilot was forced to make a landing in an open field. During the ensuing forced landing, the airplane sustained substantial damage to both wings and fuselage. The pitch trim drum inner shaft was found to be in the full-nose-down position. Examination of the cockpit revealed all circuit breakers were closed and the master switch had been secured. The flight computer, trim servo, directional gyro, flight command indicator, pictorial navigation indicator, and control yoke were functionally tested and no defects were noted. The original control yoke trim switch had been replaced. The switch wiring was not the original wiring and did not correspond to the original color codes on the wires. The wire colors were written on pieces of masking tape which were wrapped around each corresponding wire. One of the wires was pinched and pressing on the switch wafer stack; according to a representative of the manufacturer the pinched wire pressing on the switch wafer stack could have resulted in a runaway trim condition.

Probable cause

The pilot's inability to maintain control of the airplane due to a pinched trim system wire that resulted in a runaway nose-down pitch trim.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CEN10LA052
Event ID
20091117X33933
Case number
CEN10LA052
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: 09c01fd46a95edc2a6110b872ee8702865dc9754d3cc06af2b6a419d4c6dbd0b; retrieved 2026-09-15T13:29:55.036Z.