# Accident 20021009033659A: Beech A200, Cleveland, OH, October 9, 2002

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: October 9, 2002, 14:30 local time
- Place: Cleveland, OH
- Airport: Burke Lakefront
- Damage: Minor damage
- Operating rules: General operating rules (Part 91)
- Location: 41.5175° N, 81.6833° W: From the FAA
- Nearby events: https://openairdocs.org/map.md?lat=41.5175&lon=-81.6833&mi=10
- Aircraft: N200NG (not matched to a registry record)
- Reported make and model: BEECH A200
- Fatal injuries: 0
- NTSB investigation: [NTSB IAD03TA003](https://openairdocs.org/ntsb/IAD03TA003) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20021009033659A

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(-23) AFTER T/O ON 24R THE RIGHT MAIN GEAR WOULD NOT COMPLETELY RETRACT. A LOW FLY BY WAS PERFORMED AND THE TOWER VERIFIED THE RIGHT GEAR WAS NOT FULLY EXTENDED. PILOT TRIED TO CYCLE THE GEAR, BUT STILL SHOWED AN UNSAFE CONDITION ON THE RIGHT MAIN GEAR. THE PILOT CYCLED THE GEAR CB AND THEN PERFORMED THE EMERGENCY GEAR EXTENSION PROCEDURE. THE RIGHT MAIN GEAR STILL INDICATED AN UNSAFE CONDITION. THE PILOT DECLARED AN EMERGENCY AND THEN LANDED THE AIRCRAFT ON RWY 24R. AT TOUCH DOWN THE CO-PILOT SHUT DOWN BOTH ENGINES. THE RIGHT MAIN GEAR COMPLETELY COLLAPSED AFTER LANDING AND THE AIRCRAFT SKIDDED OFF THE RIGHT SIDE OF THE RUNWAY HITTING PART OF THE VASI SYSTEM WITH THE RIGHT WING. DAMAGE TO THE AIRCRAFT APPEARED TO BE MINOR.

## The NTSB's investigation of this event (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB IAD03TA003](https://openairdocs.org/ntsb/IAD03TA003), Oct 9, 2002: Beech A200 (N200NG), Cleveland, OH, substantial damage. Probable cause: Inadequate operating clearance between the ring gear and pinion gear during the manufacturing process resulting in the failure of the landing gear actuator gear ring.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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