AS350 B3e course · Power and systems
Oil, start and ignition
What keeps the engine alive, and how it wakes up
The essentials
The engine has its own oil system — tank, pump, filter and cooler — separate from the main gearbox's. Low oil pressure and chip detection are among its warnings.
On the Arriel 2D the FADEC runs the start: it engages the starter, schedules fuel and ignition, and watches for a hot or hung start. Your job is to monitor — Ng rising, light-off, TOT peaking and falling — and to stop the start if it isn't behaving.
The oil system
Oil is drawn from the tank by a pressure pump and passes through a filter before it enters the engine. It lubricates and cools the bearings and gears.
Scavenge pumps then collect it and send it back through a cooler to the tank. Chip detection sits on the return side, where oil coming off the bearings carries any metal with it.
Engine oil and main-gearbox oil are separate systems with separate warnings. Know which light belongs to which.
What the oil indications mean
- Oil pressure and oil temperature on the VEMD tell you the system is working; a low-pressure warning tells you it may not be.
- A chip warning means metal has reached a detector.
A single indication can be a sensor. The RFM tells you which other indications confirm a real problem and how urgently to land. Either way, an oil or chip indication is reported, not reset and forgotten.
How a chip detector works
An electrical chip detector is a magnet with two contacts. Ferrous particles collect on it; when enough bridge the gap, the circuit closes and the chip light comes on in the cockpit.
The Arriel 2 also has two mechanical magnetic plugs, on the accessory and reduction gearboxes, that maintenance pulls and inspects. What the debris means is maintenance's judgement, made against their manual — which is why a chip light ends in a log entry.
Source 3
Getting fuel to the burner
The airframe delivers fuel to the engine; engine-driven pumps raise its pressure; a metering unit decides how much reaches the injectors.
On the Arriel 2 aircraft the governor computes the fuel flow and drives the metering valve electrically. On the 2B, the twist grip also has a mechanical link to the metering unit — that is what makes manual backup possible.
On the B2's Arriel 1D1, the governing itself is hydromechanical, inside the fuel control unit.
The start, in principle
The starter-generator spins the gas generator through the accessory gearbox. At a set speed, fuel and ignition come on, the mixture lights, and TOT rises sharply — light-off.
The starter keeps assisting while the engine accelerates. At a set Ng it drops out, the ignition stops, and the engine is self-sustaining. The same machine then becomes the generator. On the Arriel 2B / 2B1 that happens at about 45 % Ng (training-manual figure).
The free turbine and rotor start turning as the gas flow builds — no clutch involved. The order and the limits you watch are in your RFM.
Hot and hung starts
A hot start is one where TOT exceeds its start limit — too much fuel for the airflow, or a weak battery turning the engine too slowly. A hung start is one where the engine lights but stops accelerating before it's self-sustaining.
The starter has to keep helping well past light-off; if it can't, the result is a hot or hung start. The FADEC guards against some of this, not all of it. A start with a weak battery is the classic case where watching TOT matters.
When it doesn't light
A wet start (or false start) is one where fuel goes in but doesn't light. The fuel pools in the combustion chamber and exhaust.
Try again without clearing it and the next light-off can burn all of it at once: a TOT spike, or flame from the exhaust. That is why a failed light-off is followed by ventilation, not an immediate second attempt.
Source 8
Clearing an aborted start
Ventilation (dry motoring) turns the gas generator on the starter with no fuel and no ignition. It blows unburnt fuel out after a failed start, and it pushes cool air through an engine whose TOT is still high from the last run.
On the Arriel 2 it has its own dry crank control. Whether a restart needs ventilation first, and for how long, is set by the RFM.
Why the starter has a duty cycle
The starter-generator draws a heavy current from the battery while it cranks, and it heats up. Repeated attempts in a row can overheat it, so there is a limit on consecutive starts or ventilations and a cooling time after them — Turbomeca limits an Arriel 2 dry crank to 20 seconds for exactly that reason.
The same attempts drain the battery, and a tired battery turns the engine slowly — the hot-start recipe. Two failed starts is a good moment to stop and think, not to try a third. The figures are in the RFM.
Shutdown and cooling
A turbine is stabilised at idle before it is shut off — Turbomeca gives 60 seconds for the Arriel 2B / 2B1. Stop it hot and the casing cools faster than the turbine wheels inside it; it can shrink onto them, and blades can rub or seize.
After shutdown, watch TOT fall. A TOT that rises again, or smoke and flame from the exhaust, points to fuel still burning — the RFM covers what to do.
What is a hung start?
The engine lights but hangs below self-sustaining speed. A hot start is the over-temperature case.
Which is a common cause of a hot start?
A slow-turning engine has too little airflow for the fuel it is given, so TOT climbs.
What is ventilation (dry motoring)?
Starter only, no fuel, no ignition — to clear fuel or cool a hot engine before a restart.
Why are engine chip detectors on the oil return side?
Scavenged oil has just passed the parts that wear, so it carries the evidence.
Sources
- Arriel 2D — Airbus H125 engine · Safran Helicopter Engines
- Aviation Investigation Report A04A0050 (AS350 B3) · Transportation Safety Board of Canada
- Arriel 2B/2B1 turboshaft engine — training manual · Turbomeca · Edition March 2003 (hosted by a flight school; facts cited only)
- Helicopter Flying Handbook (FAA-H-8083-21B) · FAA · Chapter 4, Helicopter Components, Sections, and Systems
- Helicopter Flying Handbook (FAA-H-8083-21B) · FAA · Chapter 11, Helicopter Emergencies and Hazards
- AS350B3 rolls — engine controls · Aerossurance
- Type-Certificate Data Sheet E.073, Arriel 1 series engines · EASA · Issue 05, 20 February 2025
- Aviation Maintenance Technician Handbook — Powerplant (FAA-H-8083-32B) · FAA · Ch. 5, Engine Starting Systems; Ch. 10, Turbine Engine Operation (p. 10-57)
- Information Notice 2976-I-76 · Airbus Helicopters · Revision 0, 23 February 2016
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.