Propeller Blade Separation Causes Severe Damage to Beechcraft 95-B55

Casualties unknown • RECIFE, PE, BR

A propeller blade detached from a Beechcraft 95-B55 during takeoff at Recife International Airport, causing significant engine and airframe damage.

What happened

On May 28, 2008, a Beechcraft 95-B5 and PT-DRI was performing a domestic flight from Recife (SBRF) to Maceió (SBMO) carrying one pilot and three passengers. Shortly after takeoff, once the landing gear had been retracted, the aircraft experienced a violent impact and intense vibration. The pilot immediately extended the landing gear and performed an emergency return to the runway, landing successfully.

The separation of a blade from the right engine propeller caused severe damage to the propeller hub, the engine mount, and the nose landing gear fairing. Despite the severe damage to the aircraft, all four occupants escaped without injury.

The investigation

CENIPA investigators examined the wreckage and the maintenance history of the aircraft. Technical analysis by the Aeronautical Institute of Aerospace (IAE) revealed that the propeller hub showed signs of cracks and oxidation. The investigation determined that the failure was caused by a fatigue mechanism originating in the threads of both the blade and its housing.

Investigators found that during the previous 1,500-hour overhaul, the propeller blades were not secured with the correct torque. Furthermore, the mandatory use of "Red Dye"—a specialized oil used to detect cracks during inspections—was omitted during the overhaul. Because this dye was missing, subsequent 100-hour inspections failed to detect the developing cracks in the hub.

Findings

  • Improper maintenance torque: The blades of the right engine were secured with incorrect torque, initiating the fatigue process.
  • Failure to use inspection dye: The omission of Red Dye during the overhaul prevented the detection of cracks during routine inspections.
  • Inadequate maintenance supervision: The maintenance facility failed to properly supervise the overhaul process.
  • Training deficiencies: There was evidence of inadequate training or difficulty in interpreting technical publications by the mechanics involved in the overhaul.

Safety action

CENIPA issued several safety recommendations, including:

  • A recommendation for the maintenance facility to provide theoretical retraining for mechanics regarding technical publications and inspection procedures.
  • A recommendation for ANAC to evaluate the implementation of standardized training programs for maintenance organizations and to increase oversight of maintenance workshops to ensure compliance with manufacturer specifications.

Probable cause

The propeller blade separation was caused by fatigue and subsequent hub collapse, resulting from improper torque applied during a previous overhaul and the failure to use specialized dye to detect cracks during subsequent inspections.

Frequently asked questions

What happened in the 2008-05-28 aircraft accident near RECIFE, PE, BR?

A propeller blade detached from a Beechcraft 95-B55 during takeoff at Recife International Airport, causing significant engine and airframe damage.

What aircraft was involved and where did it happen?

The accident on 2008-05-28 involved a aircraft, registration PTDRI, at RECIFE, PE, BR.

What was the probable cause of the accident?

The propeller blade separation was caused by fatigue and subsequent hub collapse, resulting from improper torque applied during a previous overhaul and the failure to use specialized dye to detect cracks during subsequent inspections.

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