Various components and debris collected from the engine pertaining to the accidented aircraft were sent to the laboratory for analysis. Laboratory investigation showed evidences which suggest that the accident was caused due to bird hit. This conclusion was arrived at based on the nature of damages on the LPC rotor blades and the bird remains (feathers) found in the air-intake and by-pass ducts. A detailed account of the findings is summarized in this report
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
One 1st stage compressor blade and two turbine blades with suspected FOD were sent to the laboratory...
Findings of the analysis of a damaged first stage LP compressor rotor blade belonging to a SU-30 MKI...
Various components and debris collected from the engine pertaining to the accidented aircraft were s...
A few components of an accidented aircraft were examined. Examination revealed that the damages to t...
Four damaged components of an engine of a CAT-I accident aircraft were forwarded to the laboratory f...
A damaged LP compressor stage-1 blade of aircraft was analyzed. Laboratory investigation showed evid...
Evidences show that the damages on the airfoil were caused due to foreign object impact on the conca...
Damaged 1st stage compressor rotor blades of an aircraft were analyzed. Signatures on the leading ed...
Damaged components from the engine of a crashed aircraft were sent to the laboratory for analysis. O...
The aircraft met with an accident following reported oil splash on the windscreen of the cockpit and...
Damaged 1st stage compressor rotor blades of an aircraft were analyzed. Analysis revealed that the h...
11352552Final; May 1 981 - June 1983PDFTech ReportDOT/FAA/CT-84/13Tables (Data)William J. Hughes Tec...
Components of an aircraft which met with an accident immediately after take off were forwarded to th...
A few components retrieved from the wreckage of a helicopter were sent to the laboratory for investi...
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
One 1st stage compressor blade and two turbine blades with suspected FOD were sent to the laboratory...
Findings of the analysis of a damaged first stage LP compressor rotor blade belonging to a SU-30 MKI...
Various components and debris collected from the engine pertaining to the accidented aircraft were s...
A few components of an accidented aircraft were examined. Examination revealed that the damages to t...
Four damaged components of an engine of a CAT-I accident aircraft were forwarded to the laboratory f...
A damaged LP compressor stage-1 blade of aircraft was analyzed. Laboratory investigation showed evid...
Evidences show that the damages on the airfoil were caused due to foreign object impact on the conca...
Damaged 1st stage compressor rotor blades of an aircraft were analyzed. Signatures on the leading ed...
Damaged components from the engine of a crashed aircraft were sent to the laboratory for analysis. O...
The aircraft met with an accident following reported oil splash on the windscreen of the cockpit and...
Damaged 1st stage compressor rotor blades of an aircraft were analyzed. Analysis revealed that the h...
11352552Final; May 1 981 - June 1983PDFTech ReportDOT/FAA/CT-84/13Tables (Data)William J. Hughes Tec...
Components of an aircraft which met with an accident immediately after take off were forwarded to th...
A few components retrieved from the wreckage of a helicopter were sent to the laboratory for investi...
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
One 1st stage compressor blade and two turbine blades with suspected FOD were sent to the laboratory...
Findings of the analysis of a damaged first stage LP compressor rotor blade belonging to a SU-30 MKI...