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GE 114A6734P018 General Parts
Catalogue listing: PLATE, LOCK; DWG.: 114A6734P018;
Product Overview
Catalogued by AGO Aviation, GE 114A6734P018 sits under the general parts range under the label “PLATE, LOCK”.
This GE entry is short in the source data, which is normal for legacy turbine catalogues; the part number remains the primary identifier. No dimensional, material or rating data is held for 114A6734P018 beyond the component type, so the configuration is confirmed against the installed unit before an offer is made.
Turbine parts operate in the hot gas path and rotating section, where thermal cycling, oxidation and tip-clearance loss drive most replacement decisions. The useful comparison for a part in the general parts range is the original specification: mounting, connections, material and any certification called for by the plant.
AGO Aviation supplies worldwide against confirmed part numbers, so include 114A6734P018, the quantity and the destination port or site.
Catalogue Record
The original catalogue entry for 114A6734P018 reads: “PLATE, LOCK; DWG.: 114A6734P018”. This wording is reproduced from the source listing and is not a substitute for the drawing or nameplate on your unit.
114A6734P018 is an alphanumeric reference of 12 characters.
Compatibility & Applications
- •Rotor, casing and stationary component refurbishment
- •Outage kitting and long-lead spares provisioning
- •Combustion inspections, hot gas path overhauls and turbine module repairs
- •Existing GE installations that reference part number 114A6734P018
Inspection & Documentation
- •Serial and batch traceability review against the purchase record
- •Packaging and preservation checks for long-distance shipment
- •Dimensional and visual checks against the drawing, sample or OEM reference
- •Final part-number and quantity check on 114A6734P018 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- •Cross-referencing for superseded or obsolete 114A6734P018 references
Part Number & Catalogue Reference
- Manufacturer
- GE
- Part number
- 114A6734P018
- Component type
- General Parts
- Catalogue title
- PLATE, LOCK; DWG.: 114A6734P018;
- Catalogue reference
- GE 114A6734P018
- Category
- Turbine Parts
GE 114A6734P018 is catalogued by AGO Aviation under General Parts within the turbine parts range. Quote part number 114A6734P018 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 | 114A6734P018 |
|---|---|
| Brand | GE |
| Category | Turbine Parts |
| Type | General Parts |
| Catalogue description | PLATE, LOCK |
| Condition | New / Refurbished on request |
| Availability | Quote on request |
Parts Enquiry
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Complete the enquiry form below. Our team will review your requirement.
PLATE, LOCK; DWG.: 114A6734P018;
Part Number: 114A6734P018
Part Enquiry Help
Frequently Asked Questions
What is GE 114A6734P018?
GE 114A6734P018 is listed under Turbine Parts in the AGO Aviation catalogue, within the general parts range. It is identified in our records as "PLATE, LOCK; DWG.: 114A6734P018;".
Can I request a quote for 114A6734P018?
Yes. Send your quantity, destination and any technical references through the enquiry form and our team will confirm availability, condition and pricing for GE 114A6734P018.
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 114A6734P018 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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