Design & Certification

Design Organisations / DOAs, Part 21, EMAR-21, DAOS, Aircraft Design, Aeronautical Engineering

Big Bustard Busts Blade: Propeller Blade Failure After Bird Strike

Accidents & Incidents, Airfields / Heliports / Helidecks, Design & Certification, Fixed Wing, Mining / Resource Sector, Safety Management

The SA CAA preliminary report confirms this J41 suffered a bird strike with what is “the world’s heaviest flying bird” species (up to 19 kg). Debris went through the cabin. Fortuitously the pax in that row had moved.

Big Bustard Busts Blade: Propeller Blade Failure After Bird Strike Read Post »

AD after Two Fatal Bell 430 Accidents: Main Rotor – Pitch Link Clevis Fractures Angola and South Africa

Accidents & Incidents, Design & Certification, Helicopters, Maintenance / Continuing Airworthiness / CAMOs, Offshore, Oil & Gas / IOGP / Energy, Safety Management, Special Mission Aircraft

AD issued to inspect the B430 main rotor pitch link clevis after the second of two accidents that cost the lives of 11 people.

AD after Two Fatal Bell 430 Accidents: Main Rotor – Pitch Link Clevis Fractures Angola and South Africa Read Post »

Military SAR H225M Caracal Double Hoist Fatality Accident

Accidents & Incidents, Crises / Emergency Response / SAR, Design & Certification, Helicopters, Human Factors / Performance, Maintenance / Continuing Airworthiness / CAMOs, Military / Defence, Safety Management, Special Mission Aircraft

BEA-E identify a range of possible factors for the jamming of a hoist and severing of the hoist cable during a military training exercise.

Military SAR H225M Caracal Double Hoist Fatality Accident Read Post »

The Curious Case of the Missing Shear Pin that Didn’t Shear: A Fatal Powerline Stringing Accident

Accidents & Incidents, Design & Certification, Helicopters, Human Factors / Performance, Maintenance / Continuing Airworthiness / CAMOs, Oil & Gas / IOGP / Energy, Safety Management, Special Mission Aircraft

A key component was never recovered, investigators seem to have misunderstood their own laboratory’s report on another and the NTSB conclusions omit to identify the evident failure of a shear pin to correctly perform its safety function as a factor.

The Curious Case of the Missing Shear Pin that Didn’t Shear: A Fatal Powerline Stringing Accident Read Post »

BEA Point to Inadequate Maintenance Data and Possible Non-Conforming Fasteners in ATR 42 Door Loss

Accidents & Incidents, Design & Certification, Fixed Wing, Maintenance / Continuing Airworthiness / CAMOs, Safety Management

At top of descent a 15 kg MLG door separated causing damage. Maintenance data “complex and contained error” and allowed “allowed nuts to be reused without checking their self-locking capability”.

BEA Point to Inadequate Maintenance Data and Possible Non-Conforming Fasteners in ATR 42 Door Loss Read Post »

RCAF Investigate Defect on Newly Delivered CH-148 Cyclone (S-92)

Accidents & Incidents, Design & Certification, Helicopters, Human Factors / Performance, Maintenance / Continuing Airworthiness / CAMOs, Military / Defence, Safety Management

Terminal wire lugs T1, T2 & T3 were found unsecured. T1 was missing its securing nut, washer and lockwasher but was still contacting its terminal stud. T2 & T3 were found hand tight.

RCAF Investigate Defect on Newly Delivered CH-148 Cyclone (S-92) Read Post »

Fatal US Helicopter Air Ambulance Accident: One Engine was Failing but Serviceable Engine Shutdown

Accidents & Incidents, Design & Certification, Helicopters, Human Factors / Performance, Safety Management, Special Mission Aircraft

PSM+ICR: A propulsion system malfunction (a failing No 2 engine) was followed by an inappropriate crew response (shutting down the No 1 engine). The NTSB show how the pilot may not have been familiar with how the helicopter’s displays respond in emergencies.

Fatal US Helicopter Air Ambulance Accident: One Engine was Failing but Serviceable Engine Shutdown Read Post »

Grand Canyon Air Tour Tragic Tailwind Landing Accident

Airfields / Heliports / Helidecks, Crises / Emergency Response / SAR, Design & Certification, Helicopters, Human Factors / Performance, Safety Management, Survivability / Ditching

A Loss of Control – Inflight during a downwind approach to a busy remote landing site. The helicopter crashed in a difficult to access gully and caught fire. It took almost 10 hours for survivors to reach hospital. Five of the 7 occupants died.

Grand Canyon Air Tour Tragic Tailwind Landing Accident Read Post »

NZ Firefighting AS350 Accident: Role Equipment Design Issues

Accidents & Incidents, Design & Certification, Helicopters, Regulation, Safety Management, Special Mission Aircraft

The sling for the underslung fire-fighting bucket contacted the tail rotor resulting in a loss of control. Investigators identified a vulnerability in the bucket’s design and shortcomings in promulgating essential design data to operators.

NZ Firefighting AS350 Accident: Role Equipment Design Issues Read Post »

Fire-Fighting AS350 Hydraulics Accident: Dormant Miswiring

Accidents & Incidents, Design & Certification, Helicopters, Human Factors / Performance, Maintenance / Continuing Airworthiness / CAMOs, Safety Management, Special Mission Aircraft

Hydraulics control system wiring had been misconnected 16 years earlier and repeatedly missed during checks. When inadvertently activated, the “HYD” cut-off caused the TR servo-valve compensator to make the aircraft uncontrollable say GPIAAF.

Fire-Fighting AS350 Hydraulics Accident: Dormant Miswiring Read Post »

Dash 8 Q400 Control Anomalies: 1 Worn Cable and 1 Mystery

Accidents & Incidents, Design & Certification, Fixed Wing, Human Factors / Performance, Maintenance / Continuing Airworthiness / CAMOs, Regulation, Safety Management

The AAIB identify weaknesses in maintenance practices relating to flying control cables, an unrelated anomaly that has occurred on a number of Q400s and a weakness in how the Q400 FDR processes data that has been solved only for US operators.

Dash 8 Q400 Control Anomalies: 1 Worn Cable and 1 Mystery Read Post »

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