Add to ORKGA cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze the cause of failure. Investigation revealed that the tube of the leg sub-assembly had failed by fatigue. The fatigue was of low cycle – high stress type. Misalignment of the sliding tube sub-assembly appears to be the most probable reason for fatigue crack initiation
Fractographic study confirmed that the ventral fin axle has failed by reverse bending fatigue. The f...
Fractographic study confirmed that the ventral fin axle has failed by reverse bending fatigue. The f...
Laboratory investigation showed that damages to the tail strut assembly of a helicopter were caused ...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
A starboard outrigger strut assembly of an aircraft that cracked during taxiing was sent to the labo...
A starboard outrigger strut assembly of an aircraft that cracked during taxiing was sent to the labo...
A cracked pipe assembly of hydraulic system-II of an aircraft was forwarded to this laboratory for e...
Support assembly of a fractured tail under carriage a helicopter was sent to the laboratory for anal...
Support assembly of a fractured tail under carriage a helicopter was sent to the laboratory for anal...
Damaged components of the Nose landing gear strut assembly of an aircraft were analyzed. Evidences s...
Damaged components of the Nose landing gear strut assembly of an aircraft were analyzed. Evidences s...
A fractured drain pipe-port installed in an aircraft was forwarded to the laboratory for analyzing m...
A fractured drain pipe-port installed in an aircraft was forwarded to the laboratory for analyzing m...
From the failure pattern, it appears most probable that the main fitting subassembly of the main lan...
From the failure pattern, it appears most probable that the main fitting subassembly of the main lan...
Fractographic study confirmed that the ventral fin axle has failed by reverse bending fatigue. The f...
Fractographic study confirmed that the ventral fin axle has failed by reverse bending fatigue. The f...
Laboratory investigation showed that damages to the tail strut assembly of a helicopter were caused ...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
A starboard outrigger strut assembly of an aircraft that cracked during taxiing was sent to the labo...
A starboard outrigger strut assembly of an aircraft that cracked during taxiing was sent to the labo...
A cracked pipe assembly of hydraulic system-II of an aircraft was forwarded to this laboratory for e...
Support assembly of a fractured tail under carriage a helicopter was sent to the laboratory for anal...
Support assembly of a fractured tail under carriage a helicopter was sent to the laboratory for anal...
Damaged components of the Nose landing gear strut assembly of an aircraft were analyzed. Evidences s...
Damaged components of the Nose landing gear strut assembly of an aircraft were analyzed. Evidences s...
A fractured drain pipe-port installed in an aircraft was forwarded to the laboratory for analyzing m...
A fractured drain pipe-port installed in an aircraft was forwarded to the laboratory for analyzing m...
From the failure pattern, it appears most probable that the main fitting subassembly of the main lan...
From the failure pattern, it appears most probable that the main fitting subassembly of the main lan...
Fractographic study confirmed that the ventral fin axle has failed by reverse bending fatigue. The f...
Fractographic study confirmed that the ventral fin axle has failed by reverse bending fatigue. The f...
Laboratory investigation showed that damages to the tail strut assembly of a helicopter were caused ...