One of our operators shared the following information after one of their pilots had a linear actuator failure while fighting fires in...

Over the years I have seen this many times. The fuel lines that go up the back wall of the hell hole from the boost pumps to the main...

The Tail Rotor Pitch Change has the short manual inspection criteria for the pitch change housing ( Quill ) 204-010-775-3 and the Pitch...

The purpose of the synchronized elevators is to increase the fore/aft cg range by lowering the tail as the aircraft accelerated. They did...

This a photo of a T1 sensing unit removed from a Fuel Control. These should NEVER be removed from a Fuel Control they are calibrated...

If you are operating the Centrisep Inlet Particle Separator on your aircraft and having to do engine washes often, check the drain valve...

Over the years Hydraulic lines and fittings in the Huey have been changed, chaffed, removed and reinstalled, even become bent over time....

Where the Pilot and Co-Pilot shoulder harness connects to the inertia reel strap, it should be attached with a clevis bolt, also known as...

The picture above shows that the retainer for both the upper and lower vertical fin hinge pin was installed incorrectly. The photo of...