AS350 B3e course · Rotors and flight controls
Main-rotor blades
Composite blades, and what they tell you
The essentials
The Astar has three composite main-rotor blades. They are light, damage-tolerant and long lived, but they are not indestructible: leading-edge erosion, impact damage and skin damage all matter.
Blade track and balance are set by maintenance with adjustments on the blades and pitch links. A change in vibration is information — something has changed, and it should be reported.
How a composite blade is built
The Astar's blades are glass fibre and epoxy: a spar of wound glass rovings carries the loads, a light foam core fills the section behind it, and the whole is wrapped in a composite skin. A metal strip protects the leading edge from erosion.
Damage limits — how deep a dent, how long a crack — are set by maintenance documentation, not by eye.
Source 1
The leading edge
On the Astar the erosion strip is stainless steel, bonded to the blade. It takes the sand, rain and grit so the composite behind it doesn't.
The bond matters as much as the strip. EASA AD 2022-0246 followed reports of the strip debonding on certain blade part numbers, which unbalanced the rotor and produced high vibration; it requires repeated tap inspections. It lists the earlier variants (B, BA, BB, B1, B2, D) and AS355s — whether it applies is a blade part-number question for maintenance.
Damage on the walkaround
Run your eye and hand along each blade:
- leading edge — erosion through the strip, dents, lifting at the ends of the strip
- skin — cracks, dents, soft spots, blisters, paint cracking in a line
- tip and trailing edge — impact marks, split trailing edge, a bent trim tab
- root — the attachment bolts and the area where the blade meets the sleeve
Then compare all three. A blade that looks different from the other two is the thing to report.
Track, balance and trim tabs
For a smooth ride all three blades must fly in the same plane (track) and the rotor must be balanced around the mast. Maintenance measures both with track-and-balance equipment and corrects them — typically with pitch-link length, the small trim tabs on the trailing edge, and balance weights.
Tabs are set with tools, to measured values. A bent tab changes the track — check them on the walkaround, and never adjust one by hand.
Reading vibration
The handbook groups vibration by frequency. Low-frequency vibration — near main-rotor speed; a blade out of track or balance gives one beat per revolution — comes from the main rotor: track, balance, a damaged blade, worn bearings or dampers. Medium frequencies come from things like cooling fans, accessories and the driveline. High-frequency vibration points to the engine or the tail rotor.
A new vibration in flight is a reason to slow down and land to have it looked at, not to press on to see if it goes away.
Source 5
Describing it to maintenance
What helps the engineer most is a good description:
- frequency — a slow beat you could count, a buzz, or a high-pitched tingle
- direction — up-and-down (vertical) or side-to-side (lateral)
- when — on the ground, in the hover, at a particular speed, in turns
- what changed — recent maintenance, a blade change, a bird strike, a hard landing
The handbook stresses direction — up and down, fore and aft, side to side — and whether it's in the controls or the airframe: that's what lets maintenance tell track from balance. Some vibration is part of any rotor's normal character; what matters is a change.
Why slow blades sail
At flight rpm, centrifugal force holds the blades stiffly out. At low rpm it is a fraction of that, while a gust still acts with full force on blades that are flexible and long. A gust or an updraft under one side lifts the blades there and drives them down on the other — towards the tail boom.
The handbook pairs the gust with the controls: a control that moves, or sits out of position, tilts the slow disc before the wind does anything — one reason the controls are frictioned and the pilot stays on them. Rooftops, buildings and ridges make the worst gusts.
Source 4
A new one-per-revolution vertical vibration appears. Where is it most likely to come from?
Low-frequency vibration — near main-rotor speed, one beat per revolution for a blade out of track or balance — points to the main rotor.
You notice a trim tab bent on the walkaround. What do you do?
Report it. Tabs are set with tools to correct track; a bent one changes it, and adjusting it is a maintenance task.
What two conditions turn up in tail-boom strikes during start?
Slow blades have little centrifugal stiffness. A control out of position and a gust together can tilt the slow disc and drive a blade down onto the boom.
What is the leading-edge strip on an Astar main-rotor blade made of?
Stainless steel, bonded on. A debonding strip unbalances the rotor — the subject of EASA AD 2022-0246 on certain blades.
Sources
- Aérospatiale AS 350B Écureuil — in depth · Heli Archive
- Helicopter Flying Handbook (FAA-H-8083-21B) · FAA · Chapter 4, Helicopter Components, Sections, and Systems
- Airworthiness Directive 2022-0246 (main rotor blade leading-edge protection) · EASA · Issued 12 December 2022; applicability and reason
- Helicopter Flying Handbook (FAA-H-8083-21B) · FAA · Chapter 8, Ground Procedures and Flight Preparations
- Helicopter Flying Handbook (FAA-H-8083-21B) · FAA · Chapter 11, Helicopter Emergencies and Hazards
- Helicopter Flying Handbook (FAA-H-8083-21B) · FAA · Chapter 2, Aerodynamics of Flight
- AS350B2 accident after vibration from unrecorded maintenance · Aerossurance
Educational only. Not approved training material, and never a substitute for the Rotorcraft Flight Manual, an instructor, or your operator's procedures. Figures marked as manufacturer data or test results are not limitations. This content is a draft and has not yet been reviewed by an instructor.