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GE 9662M78G08 General Parts
Catalogue listing: 9662M78G08 SHIELD, HEAT, TURBINE ENGINE
Product Overview
The reference 9662M78G08 from GE belongs to the general parts range and is listed in our records as “SHIELD, HEAT, TURBINE ENGINE”.
Everything shown for 9662M78G08 is taken from the GE catalogue row; no dimensions, materials or ratings have been added by AGO Aviation. 9662M78G08 is recorded by part number and component type only. Where a drawing or datasheet exists, it is requested from the manufacturer or matched against your removal record.
Turbine parts operate in the hot gas path and rotating section, where thermal cycling, oxidation and tip-clearance loss drive most replacement decisions. A part in the general parts range that looks similar can still differ at the interface, so the part number and source record are checked before anything is offered.
To progress GE 9662M78G08, send the part number, quantity, destination and any drawing or nameplate photo you already hold.
Catalogue Record
The original catalogue entry for 9662M78G08 reads: “SHIELD, HEAT, TURBINE ENGINE”. This wording is reproduced from the source listing and is not a substitute for the drawing or nameplate on your unit.
9662M78G08 is an alphanumeric reference of 10 characters.
Compatibility & Applications
- •Combustion inspections, hot gas path overhauls and turbine module repairs
- •Blade, nozzle, shroud and transition piece replacement programmes
- •Performance recovery, clearance restoration and outage spares planning
- •Existing GE installations that reference part number 9662M78G08
Inspection & Documentation
- •Dimensional and visual checks against the drawing, sample or OEM reference
- •Material, coating and hardness verification where the specification requires it
- •Photographic condition record and documentation review before dispatch
- •Final part-number and quantity check on 9662M78G08 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- •Cross-referencing for superseded or obsolete 9662M78G08 references
Part Number & Catalogue Reference
- Manufacturer
- GE
- Part number
- 9662M78G08
- Component type
- General Parts
- Catalogue title
- 9662M78G08 SHIELD, HEAT, TURBINE ENGINE
- Catalogue reference
- GE 9662M78G08
- Category
- Turbine Parts
GE 9662M78G08 is catalogued by AGO Aviation under General Parts within the turbine parts range. Quote part number 9662M78G08 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 | 9662M78G08 |
|---|---|
| Brand | GE |
| Category | Turbine Parts |
| Type | General Parts |
| Catalogue description | SHIELD, HEAT, TURBINE ENGINE |
| Condition | New / Refurbished on request |
| Availability | Quote on request |
Parts Enquiry
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9662M78G08 SHIELD, HEAT, TURBINE ENGINE
Part Number: 9662M78G08
Part Enquiry Help
Frequently Asked Questions
What is GE 9662M78G08?
GE 9662M78G08 is listed under Turbine Parts in the AGO Aviation catalogue, within the general parts range. It is identified in our records as "9662M78G08 SHIELD, HEAT, TURBINE ENGINE".
Can I request a quote for 9662M78G08?
Yes. Send your quantity, destination and any technical references through the enquiry form and our team will confirm availability, condition and pricing for GE 9662M78G08.
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 9662M78G08 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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