A discussion on PT6 engine STCs
By Joe Escobar
The Pratt & Whitney PT6 engine is in wide use today. Since its introduction in 1964, the PT6 family of engines has achieved more than 247 million flying hours. As with any engine, there are costs associated with scheduled and unscheduled maintenance of the engine. The most expensive part of PT6 engine ownership can be the engine overhaul. Because of this, some owners and operators are looking at ways to extend their overhaul intervals. We will look at one option available to do just that.
There are basically four choices when it comes to your PT6 engine overhaul:
- Overhaul the engines at the P&WC recommended hours
- Request a recommendation from P&WC to extend TBO
- Develop a maintenance program
- Use an FAA STC to extend TBO
In this article, we will focus on the fourth option - using an STC to extend the engine TBO.
Using an FAA STC to extend TBO
For mechanics that aren't familiar with a TBO extension STC, it can seem like an odd concept. Most STCs we are familiar with involve a change to the aircraft or engine - installing a Raisbeck wing locker on a King Air for example.
But a TBO extension STC is a little different. Maintenance On Reliable Engines (MORE) has developed an STC for an engine maintenance regimen designed for PT6 engines. It states that its STC is designed to extend life, reliability, safety, and reduce the cost of operation and ownership. But what is unique is that there are no actual changes to the engine. The program revolves around a change in inspection intervals and maintenance requirements.
How it works
In the most basic sense, the MORE STC is an aggressive inspection system. The STC increases the frequency and thoroughness of routine engine inspections. The purpose is to find problems in their early stages. These problems then can be corrected promptly. This early correction of engine problems leads to an increase in the engine overhaul interval. The five main elements of the MORE STC are:
Required inspections. An initial inspection is performed. This establishes an initial baseline and shows the present condition of the engine. An FAA Form 337 is required to incorporate the STC along with a notice to the FAA informing them that the engine will be using the STC for the maintenance of the engine per FAR 91.409. If the aircraft is transferred to another owner, a notice to the FAA is required at the same time the new owner registers the aircraft.
Engine performance information. Performed at regular intervals, engine performance monitoring allows you to remain informed if an engine needs a repair. It evaluates the efficiency of the engine on a scheduled basis and is able to detect gradual changes over that time that will help pinpoint problems while the corrective actions are small and less expensive.
Oil and oil filter analysis. These are performed at scheduled time intervals. Oil and filter analysis can help users detect excessive wear of components and can provide early warnings of impending failure of engine parts. Sampling and filter analysis is performed using the MORE company's filter analysis tool kit and oil sampling kit. Debris is removed from the oil filter and analyzed. The filter is then cleaned in accordance with the P&WC manual.
Engine vibration analysis. Propellers are balanced on a regular basis. Vibration analysis is performed and charted on cards. Specific speeds and RPMs are then reviewed and identified to the corresponding speeds of critical parts in the engine. Readings are compared from one inspection to the next and any changes are noted and corrected. This can help reduce deterioration or rotating parts that can be caused by excessive vibration.
Borescope inspections. Periodic borescope inspections of the internal parts of the engine hot section and compressor are used to identify engine problems in their early stages and to enable corrective action. Borescope inspection of internal parts without the need to disassemble the engine allows for the hot section to operate "on condition."
PT6 engines that are maintained under the MORE Instructions for Continued Airworthiness are separated into modules for record keeping purposes. This is due to the fact that experience has shown that certain portions of the engine need inspection/repair more often than others. Separating the engine into modules allows each module to be repaired or overhauled when necessary. If the remainder of the engine is operating normally, this allows the remainder of the engine to remain in service until there is a reason for it to be repaired or overhauled. The modules in the MORE Instructions for Continued Airworthiness are:
Changes in SB 14003 that affect 1900 operators.
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