No fatalities

Precautionary Landing with Nose Gear Retracted After Propeller Control Cable Interference

Conséquences et dommages, FR

On May 25, 2011, a Piper PA 28 was involved in an aviation accident near Conséquences et dommages, FR. No fatalities were reported. Investigators recorded the probable cause as: incorrect positioning of the propeller control cable during engine reassembly. This summary draws on records from the French Bureau d'Enquêtes et d'Analyses (BEA); 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe French Bureau d'Enquêtes et d'Analyses (BEA)Primary reportUpdated 2026-10-18Data APIEditorial standards

On 25 May 2011, a Piper PA-28 (F-GFIT) made a precautionary landing at Aix-les-Milles with the nose gear not down due to a propeller control cable interfering with the nose gear compass. The aircraft slid on its nose, causing damage.

Accident Details

On Wednesday, 25 May 2011, at 15:15 local time, a private Piper PA-28 aircraft, registration F-GFIT, was on approach to runway 15 at Aix-les-Milles aerodrome (Bouches-du-Rhône, France). The pilot, who had departed from Cassagnes Begonhes (Aveyron), lowered the landing gear but noticed that the green indicator light for the nose gear did not illuminate. After two flypasts, the air traffic controller confirmed that the nose wheel was not extended. The pilot decided to perform a precautionary landing.

Landing Sequence

During the landing roll, the pilot attempted to stop the engine but was unsuccessful. The propeller struck the runway, and the aircraft slid on its nose, resulting in damage to the aircraft.

Examination Findings

Inspection of the aircraft revealed that the propeller control cable was interfering with the nose gear compass, preventing the nose gear from deploying fully.

Maintenance Background

On 26 March 2011, during a flight near Rodez, the pilot had diverted to Cassagnes following an engine failure. The engine was removed and repaired on site. The mechanic who performed the work explained that during reassembly, the propeller control cable was likely moved downward to facilitate access to other engine components. Subsequently, the cable was not repositioned, and the final inspection did not detect the anomaly. The manufacturer's documentation does not require the cable to be secured to the engine mount. The accident flight was the first since the maintenance intervention.

Conclusion

The accident was caused by the incorrect positioning of the propeller control cable during engine reassembly. The precautionary landing executed by the pilot helped to limit the damage to the aircraft.

Probable cause

incorrect positioning of the propeller control cable during engine reassembly

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Frequently asked questions

What happened in the 25 May 2011 Piper PA 28 accident near Conséquences et dommages, FR?

On 25 May 2011, a Piper PA-28 (F-GFIT) made a precautionary landing at Aix-les-Milles with the nose gear not down due to a propeller control cable interfering with the nose gear compass. The aircraft slid on its nose, causing damage.

Were there any fatalities in the 25 May 2011 Piper PA 28 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 25 May 2011 involved a Piper PA 28, at Conséquences et dommages, FR.

What was the probable cause of the accident?

incorrect positioning of the propeller control cable during engine reassembly