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MIA03CA129 · Robinson R22 BETA

16 Jun 2003 · Kissimmee, FL, United States

Orlando Flight Training Robinson R22 BETA · Accident: loss of control in flight en route

From Kissimmee Gateway Airport (KISM) to Kissimmee Gateway Airport (KISM)

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Event

NTSB case
MIA03CA129
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

Robinson R22 BETA

Aircraft type
Robinson R22
Category
Helicopter
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
N7185K
Onboard fatalities
Unknown
Route
From Kissimmee Gateway Airport (KISM)To Kissimmee Gateway Airport (KISM)
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
En route · descent
First occurrenceThe 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
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Stall/spin
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

  • Pilot in command(cfi) › Supervision, inadequate

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

NTSB narrative

The CFI stated that his student was having difficulty performing hovering auto-rotations, and they were practicing the maneuver. After about 4 executions of the maneuver, while hovering about 2 feet above the ground at the practice area, the student applied left anti-torque pedal instead of right input when he reduced engine power to begin the maneuver. The CFI later reported he had his right foot over the right anti-torque pedal to confirm correct input by the student, but he was unable to prevent or correct the incorrect input from the student as quickly as he should have done. The helicopter started to spin to the left and while descending, the aft portion of the left skid dug in to the soft soil and the helicopter stopped spinning immediately. A vibration followed the landing; he disengaged the clutch and secured the engine then exited the helicopter. Post accident inspection of the helicopter by him revealed the tail boom was substantially damaged. The student pilot stated that he was practicing the autorotation maneuver at the practice area with his flight instructor. On his third or fourth attempt of performing the maneuver, the helicopter spun to the left and contacted the ground. His instructor later told him that he applied left anti-torque pedal instead of right pedal causing the helicopter to spin to the left at an unusual rate in autorotation.

Probable cause

The inadequate supervision by flight instructor for his failure to prevent incorrect anti-torque pedal input by the student resulting in the helicopter yawing at touchdown. A factor in the accident was the incorrect anti-torque pedal input by the student pilot while performing a practice auto-rotative landing procedure from a hover.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record MIA03CA129
Event ID
20030808X01292
Case number
MIA03CA129
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
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. 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: 88585a99c51f38e2b49c37be202979ec77d02fc31c614bd8cc7152a3b3f25b76; retrieved 2026-09-22T09:08:20.499Z.