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GE X10620ZC-11 General Parts
Catalogue listing: X10620ZC-11 PB/SW
Product Overview
GE X10620ZC-11 is part of the general parts range under the label “PB/SW GE X10620ZC-11” and is quoted against the exact part number.
The source entry for X10620ZC-11 is kept intact below so engineers can compare it with the drawing, nameplate or removal record. Because the legacy catalogue carries no additional data for X10620ZC-11, the enquiry is checked against the existing item rather than assumed from a similar-looking listing.
Turbine parts operate in the hot gas path and rotating section, where thermal cycling, oxidation and tip-clearance loss drive most replacement decisions. Replacement decisions in the general parts range usually start with the installed reference, the overhaul scope and the lead time available before the next outage.
The next step is a part-number check: send X10620ZC-11 with the installed configuration and our sourcing team will respond with options.
Catalogue Record
The original catalogue entry for X10620ZC-11 reads: “PB/SW GE X10620ZC-11”. This wording is reproduced from the source listing and is not a substitute for the drawing or nameplate on your unit.
X10620ZC-11 is an alphanumeric reference of 11 characters arranged in 2 hyphen-separated groups.
Compatibility & Applications
- •Outage kitting and long-lead spares provisioning
- •Combustion inspections, hot gas path overhauls and turbine module repairs
- •Blade, nozzle, shroud and transition piece replacement programmes
- •Existing GE installations that reference part number X10620ZC-11
Inspection & Documentation
- •Photographic condition record and documentation review before dispatch
- •Serial and batch traceability review against the purchase record
- •Packaging and preservation checks for long-distance shipment
- •Final part-number and quantity check on X10620ZC-11 before dispatch
Why source this part from AGO Aviation
- •Part-number verification against the exact GE general parts configuration
- •New, refurbished and as-removed options confirmed before quotation
- •Worldwide delivery with export documentation available on request
- •Cross-referencing for superseded or obsolete X10620ZC-11 references
Part Number & Catalogue Reference
- Manufacturer
- GE
- Part number
- X10620ZC-11
- Component type
- General Parts
- Catalogue title
- X10620ZC-11 PB/SW
- Catalogue reference
- GE X10620ZC-11
- Category
- Turbine Parts
GE X10620ZC-11 is catalogued by AGO Aviation under General Parts within the turbine parts range. Quote part number X10620ZC-11 in your enquiry so our sourcing team can confirm the exact GE configuration. The catalogue currently lists 25665 parts in Turbine Parts and 37106 products from GE.
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Technical Information
Product Specifications
Product identification and technical details.
| Part Number | X10620ZC-11 |
|---|---|
| Brand | GE |
| Category | Turbine Parts |
| Type | General Parts |
| Catalogue description | PB/SW GE X10620ZC-11 |
| Condition | New / Refurbished on request |
| Availability | Quote on request |
Parts Enquiry
Request a Quote
Complete the enquiry form below. Our team will review your requirement.
X10620ZC-11 PB/SW
Part Number: X10620ZC-11
Part Enquiry Help
Frequently Asked Questions
What is GE X10620ZC-11?
GE X10620ZC-11 is listed under Turbine Parts in the AGO Aviation catalogue, within the general parts range. It is identified in our records as "X10620ZC-11 PB/SW".
Can I request a quote for X10620ZC-11?
Yes. Send your quantity, destination and any technical references through the enquiry form and our team will confirm availability, condition and pricing for GE X10620ZC-11.
Does AGO Aviation supply GE spare parts worldwide?
Yes. AGO Aviation supplies gas turbine and industrial spare parts to power plants, oil and gas facilities and EPC contractors worldwide. Quote part number X10620ZC-11 when you contact us.
Platform Support
Gas turbine platform guides
Confirm the machine family and the part groups normally sourced for it. These guides are a starting point; exact fitment is verified against your part number and unit details.
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