6876865 Transition Assembly Liner
Part #: 6876865
$8,022.88
International Orders: import duties, VAT/GST and customs brokerage fees are not included in our prices or shipping charges and are paid by the recipient on delivery.
OVERVIEW
The purpose of the liner transition assembly, which is assembled on the downstream portion of the annular combustion chamber, serves to smoothly redirect the flow of high-pressure and high-temperature combustion gas into the turbine section, resulting in gas flow aligned with the direction of overall flow through the engine. The liner ensures a controlled and efficient flow of gas in the turbine section.
The liner is made of high-temperature-resistant material, which protects the underlying structure of the gas turbine. The transition liner undergoes heavy thermal stress while acting as a passage; thus, the design of the liner plays a crucial role in achieving optimal performance and efficiency in the turbine section. Part number 6876865 meets the exact design specifications and standards for easy drop-in replacements.
Alternate Part Numbers
Part number 6876865 has 3 known alternate, superseded or replacement part numbers. Search any of them, or call, text or WhatsApp +1 (954) 493-5088 for availability.
| Part Number | Manufacturer | Relationship | Notes |
|---|---|---|---|
| 6876865P | Pacific Sky Supply Inc | PMA Replacement | FAA-PMA eligibility: Rolls-Royce 501-D22A, -D22C; basis: identicality |
| 6876865TA | Extex Engineered Products Inc | PMA Replacement | FAA-PMA eligibility: Rolls-Royce 501-D22A, D22C; basis: identicality |
| T6876865 | Turbo Technologies LLC | PMA Replacement | FAA-PMA eligibility: Rolls-Royce 501-D22A, -D22C; basis: identicality |
Alternate and superseded part numbers are listed for reference from FAA PMA data, manufacturer cross-references and illustrated parts catalogs. Always confirm eligibility for your aircraft, engine and serial number before installation.
| Weight | 4.5 lbs |
|---|---|
| Dimensions | 13.5 × 7.3 × 7.3 in |
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