Gulf Union Ozone supplies OEM-equivalent gas turbine spare parts for power generation and process gas turbines operating across Saudi Arabia. Our portfolio covers the full hot-section and cold-section parts range for GE Frame 5, Frame 6B, Frame 7EA, LM2500, and LM6000; Solar Turbines Centaur 50/60 and Taurus 60/70; and Siemens SGT-200 and SGT-400 — the most widely deployed turbine models in Saudi Aramco gas plants, SEC power stations, SWCC desalination facilities, and industrial co-generation sites. Hot-section parts include combustion liners and flow sleeves in Hastelloy X and IN617, transition pieces in HA-188 cobalt alloy, first- and second-stage nozzle guide vane (NGV) segments in IN738 and Mar-M247 directionally solidified alloy with TBC coating where specified, and fuel nozzle assemblies for gas, liquid, and dual-fuel configurations. Cold-section parts include axial compressor rotor and stator blades in 17-4PH stainless steel and Ti 6Al-4V titanium, inlet guide vane actuators, brush seals, labyrinth seals, and honeycomb seal segments. Igniter plugs and high-energy surface-discharge igniters for all major OEMs are held in Jeddah warehouse for immediate dispatch during unplanned turbine shutdowns. All parts supplied with CMM dimensional inspection report and EN 10204 3.1 alloy chemistry certificate. ISO 9001:2015 certified. Saudi Aramco GIS approved. CR 4030570569.

Gulf Union Ozone supplies six gas turbine spare parts families covering hot-section combustion parts, rotating and stationary airfoils, sealing systems, and instrumentation consumables — all manufactured to OEM engineering drawings and alloy specifications for Saudi Arabia turbine fleets.
OEM-equivalent combustion chamber liners and flow sleeves in Hastelloy X and IN617 nickel superalloy for GE Frame 5, Frame 6B, Frame 7EA and Solar Centaur/Taurus turbines used at Saudi power and gas plants. Each liner is manufactured to OEM geometry with correctly dimensioned dilution holes, film-cooling holes, and aft-end seal slots. Supplied with dimensional inspection report (CMM data) and EN 10204 3.1 alloy chemistry certificate. TBC (thermal barrier coating) applied where required by OEM specification. Compatible with both gas and dual-fuel combustion systems. Critical high-cycle parts; Gulf Union Ozone recommends 10% safety stock at each Saudi plant for unplanned-outage coverage.
First- and second-stage NGV segments in IN738 and Mar-M247 directionally solidified alloy; TBC-coated where required by OEM specification; for hot-section replacements at Saudi Aramco and SEC gas turbine overhauls. NGV segments are the highest-temperature stationary airfoils in the gas turbine and are subject to oxidation, creep, and TBC spallation in Saudi Arabia's high-ambient-temperature operating environment. Gulf Union Ozone supplies both new and OEM-licensed repaired/re-coated NGV segments with full dimensional and coating thickness inspection records. Compatible with GE Frame 6B, Frame 7EA, LM2500, LM6000, and Siemens SGT-400 turbines.
Axial-flow compressor rotor and stator blades in 17-4PH stainless and titanium 6Al-4V for inlet stages; profile-ground and shot-peened per OEM tolerances for Saudi turbine fleet maintenance. Compressor blades are critical for turbine efficiency; erosion and corrosion from Saudi desert sand and coastal salt air accelerate blade degradation. Gulf Union Ozone supplies full-stage blade sets for GE Frame 5, Frame 6B, Frame 7EA, LM2500, and Solar Centaur 50 turbines, with profile-grinding certificates confirming chord, thickness, and leading-edge radius within OEM drawing tolerances. Inlet guide vane actuator assemblies also available.
Abradable brush seals, labyrinth seals and honeycomb seal segments for hot-section and compressor inter-stage sealing; reduce leakage losses by up to 2% turbine efficiency. Brush seals use Inconel 625 bristle packs for compressor discharge and turbine inter-stage positions; labyrinth seals in abradable aluminium-silicon alloy for large clearance control; honeycomb seal segments in SS 316L brazed construction for LM2500 and LM6000 compressor and turbine stages. All seals supplied with dimensional inspection records. Replacing worn seals at each major overhaul recovers measurable heat rate improvement in Saudi power plant gas turbines.
High-energy igniter plugs and surface-discharge igniters for GE, Siemens, Solar and Rolls-Royce turbines; rated for full diurnal temperature cycle in Saudi outdoor gas plants. Igniter plugs are consumable items replaced at every borescope inspection (typically every 4 000 fired hours) and must be held as critical spares to avoid delayed start-up. Gulf Union Ozone stocks high-energy igniter plugs (1–4 joule) and surface-discharge igniters in Jeddah warehouse for immediate dispatch. Ceramic insulator and nickel or platinum-iridium tip materials available. Fully compatible with OEM ignition exciter units.
Combustion transition ducts in HA-188 cobalt alloy and Hastelloy X; connect the combustion liner to the turbine first-stage nozzle; critical high-temperature parts requiring exact OEM geometry match. Transition pieces direct hot combustion gases from the can-annular combustors into the turbine nozzle and must maintain precise exit-plane geometry to ensure uniform temperature distribution across the NGV. Gulf Union Ozone supplies transition pieces for GE Frame 5, Frame 6B, and Frame 7EA turbines — the most common models in Saudi Arabia power and gas plants — with full CMM inspection and EN 10204 3.1 alloy certificates. TBC coating applied where OEM-specified.
All parts supplied with CMM dimensional inspection report and EN 10204 3.1 alloy chemistry certificate. Saudi Aramco GIS approved. ISO 9001:2015 (CR 4030570569). Stocked in Jeddah; fast dispatch across Saudi Arabia.
| Part | Compatible Turbine | Material | Stage / Location | Lead Time |
|---|---|---|---|---|
| Combustion Liner — GE Frame 5 | GE Frame 5 (MS5001) | Hastelloy X | Combustion Stage | 4–6 weeks |
| Combustion Liner — GE Frame 6B | GE Frame 6B (MS6001B) | Hastelloy X / IN617 | Combustion Stage | 4–6 weeks |
| Combustion Liner — GE Frame 7EA | GE Frame 7EA (MS7001EA) | Hastelloy X | Combustion Stage | 6–8 weeks |
| Combustion Liner — GE LM2500 | GE LM2500 / LM2500+ | Hastelloy X | Combustion Stage | 6–8 weeks |
| Combustion Liner — GE LM6000 | GE LM6000 PC/PD/PF | Hastelloy X | Combustion Stage | 6–8 weeks |
| Combustion Liner — Solar Centaur 50 | Solar Turbines Centaur 50 | Hastelloy X | Combustion Stage | 4–6 weeks |
| Combustion Liner — Solar Taurus 60/70 | Solar Turbines Taurus 60/70 | Hastelloy X | Combustion Stage | 6–8 weeks |
| Combustion Liner — Siemens SGT-200 | Siemens SGT-200 (Tornado) | Hastelloy X | Combustion Stage | 6–8 weeks |
| Combustion Liner — Siemens SGT-400 | Siemens SGT-400 | Hastelloy X | Combustion Stage | 6–8 weeks |
| Transition Piece — GE Frame 5/6B | GE Frame 5 / Frame 6B | HA-188 Cobalt Alloy | Combustion-to-Turbine Duct | 6–8 weeks |
| Transition Piece — GE Frame 7EA | GE Frame 7EA (MS7001EA) | Hastelloy X / HA-188 | Combustion-to-Turbine Duct | 8–10 weeks |
| NGV Segment Stage 1 — DS Alloy | GE Frame 6B / Frame 7EA / Siemens SGT | IN738 (Directionally Solidified) | First-Stage Turbine Nozzle | 8–12 weeks |
| NGV Segment Stage 2 — DS Alloy | GE Frame 6B / Frame 7EA | Mar-M247 DS Alloy | Second-Stage Turbine Nozzle | 8–12 weeks |
| Compressor Blade Stage 1–2 Rotor | GE Frame 5/6B / Solar Centaur 50 | 17-4PH Stainless Steel | Inlet Compressor Rotor | 6–8 weeks |
| Compressor Blade Stage 3–6 Rotor | GE Frame 6B / Frame 7EA | Ti 6Al-4V Titanium | Mid-Stage Compressor Rotor | 6–8 weeks |
| Compressor Stator Vane — Inlet Guide (IGV) | GE Frame 5/6B/7EA / Solar | 17-4PH Stainless Steel | Inlet Guide Vane Stage | 4–6 weeks |
| Compressor Stator Vane — Mid-Stage | GE Frame 6B / LM2500 | 17-4PH Stainless Steel | Mid-Compressor Stator | 6–8 weeks |
| Brush Seal — Compressor Exit | GE Frame 6B / Siemens SGT | Inconel 625 Bristle Pack | Compressor Discharge Seal | 4–6 weeks |
| Labyrinth Seal — Turbine Inter-Stage | GE Frame 5/6B/7EA | Abradable Al-Si Alloy | Turbine Inter-Stage | 4–6 weeks |
| Honeycomb Seal Segment | GE LM2500 / LM6000 | SS 316L Brazed Honeycomb | Compressor / Turbine Seal | 6–8 weeks |
| Igniter Plug — High-Energy | GE / Siemens / Solar / Rolls-Royce | Ceramic Insulator / Ni Electrode | Combustion Ignition | Ex-stock — 1 week |
| Igniter Plug — Surface Discharge | GE LM2500/LM6000 / Solar | Platinum-Iridium Tip | Combustion Ignition | Ex-stock — 1 week |
| Thermocouple Assembly — EGT | GE Frame 5/6B/7EA / Siemens | Type K / Type R Thermocouple | Exhaust Gas Temperature Measurement | Ex-stock — 1–2 weeks |
| Combustion Dynamics Pressure Sensor | GE Frame 7EA / Siemens SGT-400 | SS 316L Wetted Parts | Combustion Can Monitoring | 4–6 weeks |
| Fuel Nozzle — Gas (Dry Low NOx) | GE Frame 6B / Frame 7EA | SS 316L + Cobalt Hard-Face Tip | Fuel Injection Stage | 6–8 weeks |
| Fuel Nozzle — Dual-Fuel | GE Frame 7EA / Siemens SGT | SS 316L + Hastelloy X | Fuel Injection Stage | 6–8 weeks |
| Turbine Bearing — Journal | GE Frame 5/6B / Solar Centaur 50 | Babbitt-Lined Forged Steel | Rotor Journal Support | 4–6 weeks |
Parts manufactured to OEM engineering drawings and alloy specifications; dimensional and chemical inspection reports provided for Saudi Aramco turbine overhaul team verification. Every part ships with CMM data confirming critical features within OEM tolerances and EN 10204 3.1 alloy chemistry certificate against the required superalloy spec.
Gulf Union Ozone holds Saudi Aramco GIS supplier approval for gas turbine spare parts; parts accepted by Saudi Aramco's rotating equipment inspection team for GOSP and gas plant turbines. Full vendor qualification documentation available for EPC contractor and client engineering review.
Commonly replaced hot-section parts — igniters, thermocouples, fuel nozzle tips — held in Jeddah warehouse for fast delivery during unplanned shutdowns. Rapid dispatch to all Saudi regions including Jubail, Yanbu, Ras Tanura, Riyadh, and Jizan. ISO 9001:2015 certified (CR 4030570569).
Coordinates refurbishment of serviceable combustion liners and NGVs through accredited TBC re-coating facilities, reducing spare-parts cost for Saudi Aramco and SEC maintenance budgets. Written condition assessment and refurbishment cost comparison provided before ordering new parts.
Reciprocating, screw, and centrifugal air compressors and spares for Saudi Arabia oil & gas, petrochemical, and industrial facilities — including instrument air and process gas compression packages.
Shell-and-tube, plate, and air-cooled heat exchangers in carbon steel, SS 316L, and duplex stainless steel for turbine lube oil cooling, intercooling, and process heat recovery in Saudi industrial plants.
Pressure gauges, temperature transmitters, thermocouple elements, RTDs, and vibration monitoring instruments for gas turbine condition monitoring and Saudi Aramco DCS integration.
Gate, globe, check, ball, and butterfly valves in SS 316L, duplex SS, and carbon steel — API 600, API 602, ASME B16.34 — for turbine fuel gas, lube oil, and cooling water systems in Saudi Arabia.
Gulf Union Ozone sources gas turbine parts from manufacturers with active FAA Part 145 (or EASA Part 145) approvals or from OEM-licensed repair shops. Every part is shipped with a dimensional inspection report (CMM data) confirming that critical features (blade chord, trailing edge thickness, cooling hole diameters, pin boss geometry) are within OEM drawing tolerances. For Saudi Aramco turbines, we also provide the alloy chemistry certificate (EN 10204 3.1) against the required superalloy spec (e.g. IN738 per AMS 5891).
The highest-turnover hot-section parts on GE Frame 6B turbines in Saudi Arabia are (in order): combustion liners (typically replaced every 24 000 fired hours), transition pieces (same interval), first-stage NGV segments (replaced or repaired every 12 000–24 000 hours depending on firing temperature), fuel nozzle assemblies (inspected every 8 000 hours, replaced as needed) and igniter plugs (replaced at every inspection, typically 4 000 hours). Saudi dust and humidity accelerate oxidation and TBC spallation; Gulf Union Ozone recommends maintaining a 10% safety stock of each in the Saudi plant warehouse.
Yes. Gulf Union Ozone stocks and sources spare parts for Solar Turbines (a Caterpillar company) models including Centaur 50/60, Taurus 60/70 and Saturn 20/C28 — all widely used at Saudi Aramco gas-oil separation plants (GOSPs) and pipeline booster stations. Parts include combustion liners, IGV actuators, compressor blades, igniter plugs and fuel control valves. We also source Solar Turbines OEM parts through authorised distributors and can confirm availability within 48 hours of a request.
To get a fast quotation, provide: turbine OEM and model (e.g. GE Frame 6B), part name and OEM part number (if known), required quantity, inspection and certification requirements (CMM report, EN 10204 3.1 MTC, ASME, Saudi Aramco material standard), delivery location in Saudi Arabia, and required delivery date.
Recent Deliveries
CR 4030570569 | ISO 9001:2015 | Jeddah, Saudi Arabia — Saudi Aramco vendor compliance · SAEP-347 credentials
Technical content reviewed by Gulf Union Ozone's Engineering Team, Jeddah — 2026
Inventory updated: September 2026
Gulf Union Ozone Trading Co. supplies Gas Turbine Spare Parts to industrial customers across Saudi Arabia with delivery from our Jeddah warehouse — all products ship with original certificates and compliance documentation for Aramco, SABIC, and government projects.
Gas Turbine Spare Parts from Gulf Union Ozone serves Saudi Aramco operations, SABIC, SADARA, SEC utilities, NEOM mega-projects, and major industrial facilities across the Kingdom — our inventory covers the most common specifications and ratings.
Gulf Union Ozone stocks a comprehensive range of Gas Turbine Spare Parts — contact us for immediate availability confirmation and a competitive quotation with full compliance documentation and MTC traceability.
For urgent Gas Turbine Spare Parts procurement in Saudi Arabia, WhatsApp +966 55 098 8062 — our team confirms stock availability within the hour and provides competitive quotations with full compliance documentation for all industrial sectors.