6876865 Transition Assembly Liner
Part #: 6876865
$8,022.88
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Part number 6876865 has 3 known alternate, superseded or replacement part numbers.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Alternate and superseded part numbers are listed for reference from FAA PMA data, manufacturer cross-references and illustrated parts catalogs.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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