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WPR26LA028 · Cessna 305 C

18 Oct 2025 · Phoenix, AZ, United States

Cessna 305 C · Accident: loss of control on ground during landing

From Grapevine Airstrip (88AZ) to an unrecorded destination

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Event

NTSB case
WPR26LA028
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
Event fatalities
Unknown
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

Cessna 305 C

Aircraft type
Cessna 305
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
N4584N
Operator
Unknown
Onboard fatalities
Unknown
Route
From Grapevine Airstrip (88AZ), Roosevelt, AZTo not recorded
Aircraft age
About 68 years (built 1957)
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
Landing
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 on ground
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
  • Aircraft › Aircraft systems

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The pilot taxied the tailwheel airplane to the departure end of the runway, made a tight left turn to reverse direction on the runway for take-off, then applied hard-right tailwheel input to stop the turn and straighten the airplane. Once airborne, he realized the airplane yawed significantly to the right and the right rudder pedal seemed to be stuck. This condition required continuous full-left rudder control input to maintain coordinated flight. Upon reaching the destination airport, he communicated with the local air traffic controller and requested the largest runway out of concern the tailwheel might be stuck in an offset position and create a loss of directional control during landing. After touchdown the airplane ground looped to the left, resulting in substantial damage to the right wing, horizontal stabilizer, and tail cone. After exiting the airplane, he observed the steering arm was stuck in the full-right position. Photos taken by the pilot immediately after the accident showed both tailwheel steering springs/chains were under tension, and the tailwheel was offset to the left. With the assistance of others, the pilot picked up the airplane’s tail and kicked the steering arm loose, after which he was able to taxi the airplane to its hangar.

The pilot shipped the tailwheel assembly to the NTSB, where an examination of the components was conducted. The overall condition of the assembly was consistent with a worn tailwheel locking/steering mechanism with an increased likelihood of unreliable lock engagement/disengagement and accelerated wear.

The tailwheel assembly was replaced at an unknown date and the maintenance records did not contain any maintenance history of the tailwheel.

Probable cause

A worn tailwheel steering mechanism, which resulted in a locked tailwheel and a ground loop during a landing roll.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR26LA028
Event ID
20251021201901
Case number
WPR26LA028
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, coordinates, cause areas. 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: e54de8c0ff930589db22f1419f30e26a59bd997cc61e62eef161eb57bd51c34e; retrieved 2026-09-16T20:29:44.713Z.