The Austart ATS103 turbine air starter is a heavy-duty compressed air-powered cranking system designed for consistent, reliable engine starting across the most demanding industrial environments. Rated to a maximum of 150 psi with a standard operating pressure of 100 psi, the ATS103 converts compressed air into high cranking torque through a precision turbine rotor and a three-planet epicyclic gear reduction, delivering that torque to the engine flywheel ring gear via an SAE 3 flanged nose assembly fitted with a pre-engaged pneumatic piston drive. Engineered as three independently serviceable sub-assemblies — nose, motor, and silencer — the ATS103 is purpose-built for spark-free starting duty in mining, oil and gas, marine, and stationary power generation applications where electrical starting systems are impractical or present unacceptable ignition risk.
The Austart ATS103 turbine air starter is a heavy-duty pneumatically driven cranking system that routes compressed air through a precision turbine rotor, then steps that high-speed rotation through a three-planet epicyclic gear reduction to deliver the sustained torque needed to crank large diesel and gas engines reliably across extreme operating environments. A pre-engaged pneumatic piston drive mechanism ensures the pinion is fully meshed with the engine flywheel ring gear before the turbine reaches cranking speed, providing a positive and controlled start cycle every time. Built as three independently serviceable sub-assemblies — nose, motor, and silencer — and entirely spark-free in operation, the ATS103 is engineered for applications where consistent starting performance and long service life matter as much as safety compliance.
Specifications listed below apply to the standard Austart ATS103 turbine air starter. Dimensional data is sourced from the official installation and maintenance documentation. Pinion and flange configurations are available in multiple options — contact us with your engine details for the correct part number.
| Parameter | Specification |
|---|---|
| Starter Type | Turbine Air Starter (Pneumatic) |
| Drive Mechanism | Pre-Engaged Pneumatic Piston Drive |
| Standard Operating Pressure | 100 psi |
| Maximum Operating Pressure | 150 psi |
| Control Port Size (Inlet & Outlet) | 1/4" NPT |
| Minimum Supply Hose I.D. (up to 15 ft / 5 m) | 1-1/2" (40 mm) |
| Minimum Supply Hose I.D. (over 15 ft / 5 m) | 2" (50 mm) |
| Control Line Size | Minimum 1/4" (6 mm) O.D. |
| Overall Length | 16.242" (412.5 mm) |
| Flange to Pinion Distance | 5.750" (146.1 mm) |
| Motor Housing Diameter | Ø 3.623" (92.0 mm) |
| Flange Standard | SAE 3 |
| Mounting Hole Pattern | 3 holes · Ø 0.656" (16.7 mm) · equally spaced at 120° |
| Pinion Rest Position | Flange-to-Ring-Gear (FRG) spacing less 1/8" (3 mm) |
| Pinion Options (Right-Hand) | 9TH 3MOD · 10TH 8/10 · 11TH 6/8 · 12TH 8/10 |
| Pinion Options (Left-Hand) | 9TH 3MOD · 10TH 8/10 · 11TH 6/8 · 12TH 8/10 |
| Y Strainer (Required) | 100 mesh · 1-1/2" BSP |
| Relay Valve (Required) | RV1500 · 1-1/2" NPT (mounted directly upstream via Y strainer) |
| Turbine Rotor Nut Torque | 25–30 ft lb (30–40 Nm) |
| Re-start Delay | Minimum 15 seconds between start attempts |
| Special Options Available | Threaded exhaust outlets · Alternate pinion tooth counts and modules · Left-hand pinion configurations · Mining-grade housing options |
| Warranty | 12 months from date of purchase (first user) |
When the operator activates the SC25 starter control button at the instrument panel or control station, a pneumatic control signal travels through the 1/4-inch control line to the RV1500 relay valve installed upstream of the starter. The relay valve opens, allowing high-pressure compressed air from the air receiver to flow through the 100-mesh Y strainer, which captures particulate contamination before it can reach the starter's precision internal components. Filtered supply air then enters the ATS103 turbine housing through the main inlet port and acts on the blades of the turbine rotor, spinning it rapidly under the force of the expanding compressed air.
Simultaneously, a portion of the supply air acts on the piston assembly within the nose housing, driving the piston forward along the bearing housing and pushing the drive assembly — and the pinion attached to it — outward into positive mesh with the engine flywheel ring gear. This pre-engagement occurs before the turbine reaches cranking speed, ensuring every tooth on the pinion is fully loaded and in contact with the ring gear by the time maximum cranking torque arrives. The turbine's high-speed rotational output passes through the rotor shaft into the nose assembly's three-planet epicyclic gear reduction, which steps the speed down and multiplies torque to the level required to turn over a large, high-compression diesel or gas engine.
Once the engine fires and accelerates beyond the cranking speed, the operator releases the control button. The relay valve closes, cutting the compressed air supply, and the turbine decelerates. The spring within the nose assembly retracts the piston and drive assembly, withdrawing the pinion cleanly from the ring gear as drive torque falls. Exhaust air from the turbine passes through the integrated silencer assembly — the foam insert and stacked sleeve arrangement progressively reducing discharge noise before air exits to atmosphere. A mandatory 15-second pause between consecutive start attempts ensures both the ATS103 and the engine have fully stopped rotating before re-engagement, protecting the drive components from impact damage.
The ATS103 is rated to a maximum supply pressure of 150 psi. The standard recommended operating pressure is 100 psi, which delivers optimal cranking torque while keeping all internal components within their design load limits. Operating at pressures approaching the 150 psi ceiling should be reserved for applications with a genuine high-compression starting requirement and must not become the routine operating condition. The air receiver supplying the ATS103 must be manufactured to an applicable pressure vessel code such as AS1210 or an equivalent recognised standard.
The ATS103 uses a pre-engaged pneumatic piston drive. When the start cycle is initiated, compressed air simultaneously powers the turbine and acts on an internal piston that pushes the pinion into positive mesh with the engine ring gear before the turbine reaches cranking speed. This contrasts with an inertia drive, where the pinion is extended by centrifugal force as the output shaft accelerates — a mechanism that relies on sufficient rotational speed to achieve engagement. The pre-engaged drive ensures full tooth contact at the moment of peak cranking torque, providing a more controlled and consistent start cycle, particularly on large engines and in applications where reliable engagement on every attempt is critical.
The ATS103 is built to the SAE 3 flywheel housing standard, with three equally spaced bolt holes of Ø 0.656 inch (16.7 mm) at 120-degree spacing. SAE 3 is a widely used flange standard across large heavy-duty diesel and gas engines in mining, marine propulsion, oil and gas compression, and stationary power generation. Multiple pinion configurations in both right-hand and left-hand variants — covering 9-tooth, 10-tooth, 11-tooth, and 12-tooth options across standard pitch and module specifications — are available to match different ring gear designs. Please provide your engine make, model, and ring gear specification so the correct full part number can be confirmed for your application.
The ATS103 installation requires a 100-mesh Y strainer fitted upstream in the main supply line, with the RV1500 relay valve (1-1/2 inch NPT) connected directly to the strainer outlet via a short nipple. The Y strainer protects both the relay valve seat and the starter's precision turbine and drive components from particulate contamination that can accumulate in the air receiver over time. A minimum 1/4-inch (6 mm) O.D. control line connects the SC25 starter control button to both the relay valve and the starter control inlet port. Fitting the Y strainer is a mandatory requirement of the product warranty and must not be omitted from the installation.
A minimum interval of 15 seconds is required between consecutive start attempts. This pause allows the ATS103 turbine rotor, output drive assembly, and the engine itself to come to a complete standstill before the control is re-activated. Attempting to initiate a new start cycle while any of these components are still rotating can cause significant impact damage to the pinion teeth, flywheel ring gear, and the internal piston and drive mechanism — damage that is excluded from warranty coverage. Always confirm visually that all rotating components have fully stopped before initiating the next start attempt.
Yes. The connection between the ATS103 motor housing and nose assembly allows the housing to be repositioned to a different angular orientation without complete disassembly of the unit. This makes it practical to redirect the air supply inlet and control ports to the most convenient angle for hose or pipework routing — a significant advantage in engine compartments where access is restricted from certain directions or where the starter must be installed in a non-standard orientation. Always follow the installation manual's procedure and torque specifications when repositioning the housing to ensure a sealed and correctly loaded joint.
Our engineers will confirm the correct ATS103 flange code, pinion configuration, and system components — including relay valve, Y strainer sizing, and air supply line requirements — and provide full technical documentation and a competitive quote tailored to your engine and application.