Wednesday, March 1, 2023

Pc9 Aircraft

Pc9 Aircraft

Pc9 Aircraft - The Pilatus PC-9M is a single engine, advanced military training aircraft designed and built by Pilatus Aircraft Limited, Switzerland. The aircraft is manufactured principally to meet the requirements of the Swiss Air Force (SAF), the Royal Australian Air Force (RAAF), the Royal Saudi Air Force (RSAF) and the Royal Thai Air Force (RTAF). The aircraft was derived from its predecessor Pilatus PC-7 turbo trainer aircraft.

The PC-9M is an advanced version of PC-9. The variant boasts wide dorsal fins to enhance longitudinal stability, stall strips, a new engine and propeller controls. The PC-9 Mk2 is an improved version of PC-9M. The improved variant is developed by Pilatus and Beechcraft for the US. It was re-named as T-6A Texan II.

Pc9 Aircraft

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The cockpit of PC-9M is upgraded with primary flight display (PFD) and multi function display (MFD), both of which provide clear visibility and display flight information. Engine monitoring, aircraft configuration, pressurisation, and environmental controls are available in the cockpit.

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The PC-9M can climb at the rate of 19.7m/s. The maximum and cruise speeds of the aircraft are 593km/h and 552km/h respectively. The stall speed is 143km/h. The range of the aircraft is 1,593km and service ceiling is 11,580m. The maximum endurance is 4 hours 30 minutes. The aircraft weighs around 1,781kg and the maximum take-off weight is 2,350kg.

The PC-9M is powered by a single Pratt & Whitney Canada PT6A-62 turboprop engine and a Hartzell four blade propeller made of aluminium. The engine can generate 857kW of power. The propeller rotates at a constant speed of 2,000 rpm.

Pilatus Air Support

The PC-9M is equipped with advanced Visual Flight Rules (VFR) and Instrument Flight Rules (IFR) avionics suite for navigation, communication and identification. The avionics suite installed in the cockpit includes electronics flight instrumentation system (EFIS), Head Up Display (HUD), On-board Oxygen Generating System (OBOGS) and anti-G system.

The PC-9M has six under wing hard-points (three on each wing). These hard-points are fitted with two Rocket Pods, FN LAU 7 folding fin aerial rockets and two FN heavy machine guns (HMG). Each gun can fire 250 rounds of ammunitions.

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Pilatus Pc-M Orders And Deliveries

The development of PC-9 began in 1982 to replace the ageing PC-7 fleet. Few aerodynamic changes were made to the PC-7 during 1982 and 1983. The maiden flight of PC-9 was completed on 7 May 1984. The aircraft was first certified in September 1985. It entered into service in 2004.

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An epicyclic speed reduction gearbox installed in the engine reduces propeller noise by optimising output speed. The engine is also equipped with multi-stage axial and single-stage centrifugal compressor, reverse flow combustor and a single-stage compressor turbine.

In 1997, Croatia signed a contract with the RAAF for supplying three second-hand PC-9M aircraft. Slovenia ordered nine aircraft in December 1997. Oman procured 12 aircraft in January 1999. Ireland ordered eight aircraft in January 2003. Bulgaria acquired 12 aircraft in 2004. Mexico was the last customer to receive two aircraft in September 2006.

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Pinnacle Aircraft Engines

Pinnacle Aircraft Engines

Pinnacle Aircraft Engines - A key driver of this action is reports of two engine seizures on the ground and one in-flight loss of engine oil pressure. It goes without saying that one incident at altitude is one too many.

There is no airborne AAA to come to your rescue. It is important to note that the mandatory service bulletin identifies crankshaft assemblies with fewer than 200 operating hours, while the "AD requires compliance for all affected engines, regardless of operating hours."

Pinnacle Aircraft Engines

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The AD supersedes the service bulletin. The crankshaft counterweight setup includes the counterweight assemblies, pins, plates, and clips. The counterweights have a bushing installed that fits precisely with the pins, which are short squat steel dowels.

Incorrect Installation Of Counterweight Clips

Plates cover the pin, and clips hold the entire thing in place. A new ownership team that includes J.D. Kuti as vice president of operations and chief inspector, along with Todd LaVelle and Aron Stefanides, bought the business in July 2019. As a Part 145 repair station, Pinnacle now does work for other customers including major overhauls and repairs.

Its engines are built to new limits using Superior Air Parts cylinders. Kuti said the company prefers Superior cylinders because of their advanced manufacturing techniques and their warranty period—37 months, which is longer than almost any other cylinder manufacturer.

The AD explicitly states, "before further flight." Citing such low time on the crankshafts suffering failures and the gravity of what could happen should the counterweight depart, the FAA shortened the time-to-market for this AD and reduced the period for public comment.

One should go into an overhaul expecting a few "extras" such as that. Royal Aircraft informed me that the propeller shop was recommending the prop governor be overhauled as well. As it turned out, the cost of the overhaul rivaled the price of a new McCauley governor, so I went with new.

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Affected Continental Aircraft Engines

Kuti walked me through the process, which includes a detailed inspection and photo session as the engine is uncrated. They then tear the engine down, using more photos to document the condition. The engine is cleaned using a baking soda blast system rather than plastic or glass media used by some other shops.

The baking soda, Kuti said, is harmless and breaks down easily should anyone find its way into any nooks and crannies. The parts to potentially be reused then go through an extensive nondestructive testing and measurements process to determine whether they still meet new limits.

Crankshafts go out to a vendor for regrinding if necessary. All bushings are honed in house because they believe they get better quality control that way. The test flights and subsequent break-in period show an incredibly smooth and fast engine.

Flat out it moves the old A36 airframe along at 178 to 180 knots true airspeed. At 75 percent it is typically 172 to 175 KTAS. The FAA Advisory Circular AC No. 20-103 “Aircraft Engine Crankshaft Failure” describes the function of aircraft engine counterweights in detail.

Crankshaft Counterweight Function

According to this AC, aircraft engineers design counterweights to position themselves by the inertia forces generated during crankshaft rotation, and effectively absorb and dampen crankshaft vibration. So, with the airplane going into the shop for a period of weeks to repair the wing skin, I decided to use the downtime to get the engine and propeller overhauls done, too.

Royal Aircraft Services in Hagerstown, Maryland, was one of the shops recommended by my insurance company for the wing repair. Royal has experience swapping engines in and out for overhauls as well, so in addition to a quote on the wing repair, I asked for one for the engine swap, propeller overhaul, new engine mounts, new baffling, and a number of other accessories that

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go with such a job. Please make sure that Javascript and cookies are enabled on your browser and that you are not blocking them from loading. With oil analysis trend monitoring, frequent compression checks, and digital borescopes, I still had confidence in the engine, but I knew I was on borrowed time.

I expected the engine would talk to me before it had a catastrophic failure—wear metals in the oil trending up, declining cylinder compressions, or visual indications inside the cylinders would be a harbinger of a problem.

I had already scoped out Pinnacle Aircraft Engines in Silverhill, Alabama, as the shop to do the engine overhaul. Pinnacle developed a good reputation for overhauls when its only customers were Nantucket Airlines and Cape Air.

Kuti said when it was torn down, my engine looked much as he would expect of a big-bore Continental run to TBO and beyond. The lifters had some spalling; the oil cooler was rejected because of a crack;

and the starter adapter shaft and gear were worn beyond limits—all common findings. However, one important and expensive part did not pass muster: the crankcase. After cleaning and upon inspection, Pinnacle discovered a crack that was not repairable.

Cha ching! An overhauled case added $6,500 to the bill. The original was a "heavy" case—as opposed to earlier models with thinner cases. The thicker, heavier cases were introduced to reduce cracking, but Kuti says they see a fair amount of cracking of heavy cases.

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It may be too much of a good thing, he suggests: the heavier cases don't flex under stress, which may lead to cracks. Nevertheless, that is still the recommended case. At first glance, the counterweight clips appear to be nothing more than a souped-up snap ring you can get at ACE Hardware.

They are not. Continental manufactures counterweight clips to precision measurements, and they are not to be interchanged with something that looks pretty close. The AD states that this unsafe condition will likely exist on affected engines.

That means you need to check it out if you have one. This is not a time to second-guess the feds. ADs are mandatory. This notice applies to Continental 360, 470, 520, 520, and 550 series engines manufactured between June 1, 2021, and February 7, 2023.

I caught up with JD Kuti, owner of Pinnacle Aircraft Engines in Silverhill, Alabama. He offered only one word when I asked about the call volume concerning the Continental crankshaft AD: 'crazy.' Because of the volume of aircraft affected, working through them all will take time.

After about 18 hours of flying with mineral oil, I changed it out for regular ashless dispersant oil and am on my way to what I hope is another couple of thousands of hours of trouble-free flying.

What concerned me more than the engine was the propeller. It was overhauled in 2002 as well as now, millions of revolutions and 18 years later, it was still working hard with almost no way to tell whether it was about to give out.

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And, as with the engine, I had pushed well beyond the recommended propeller TBO of 2,000 hours or six years, whichever comes first. It is imperative to keep aircraft crankshaft counterweights functioning correctly. Understanding how counterweights work is the first step in properly maintaining them.

Aircraft engine installations that incorporate counterweights are typically more complex, more powerful, and require advanced skills to fly and maintain than those on entry-level aircraft. If there's one must-do with an engine overhaul, it is replacement of the engine mounts.

I knew that when it was overhauled in 2002, but the shop that did that installation convinced me that the old mounts were in good condition and didn't need to be changed. Clearly, 18 years later, they had failed and caused damage.

Fortunately, I had been planning and saving for the overhaul of the Continental IO-550-B in my Beechcraft Bonanza A36 ever since the Hobbs meter turned over the first hour on the last engine overhaul way back in 2002—when Crocs and iPods were all

the rage. That engine served me well, surpassing the 1,700-hour recommended time between overhaul by nearly 600 hours and still going strong enough. Owners often complain that big-bore Continentals frequently need a top overhaul somewhere in the middle, but this one soldiered on without a blink, asking only for the replacement of one exhaust valve a few years ago.

Pinnacle's engine test cell is more sophisticated than many in that it includes a downdraft cooling system which closely mimics the baffling system installed in an airframe. This improved airflow plus a water misting system means they can run the highly instrumented engines longer on the dynamometer without fear of overheating.

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Kuti said my engine did so well in the dyno that they ran it for an extra hour to conduct their regular calibration processes. "We can see crankcase pressures drop off while on the dyno," Kuti said, indicating that rings are often seated during that initial run, which means much of the break-in process is complete before the engine leaves the test cell.

New and reusable parts come together in the rebuild room where all of the parts are measured again. Pinnacle uses a buddy system for the reassembly process. One technician does the build; another checks the work.

With the engine out of the airframe, Royal technicians noted that the engine mounts had sagged enough over the years to allow the engine to damage the nose bowl inner panels—wearing holes through in a couple of places and causing a crack.

Because of the complex shape, they could not be repaired with doublers. New panels were ordered. The old baffling was just that. Rather than piece it back together, I sprung for a new D'Shannon Aviation baffle cooling kit.

I have to say, it looks great; fits super tight; and appears to be doing a good job of cooling the engine. The bulletin includes specifics, such as part and serial numbers. For the complete list of suspect engines, refer to Appendix 1 on page 9 of MSB23-01.

Appendix 2 on page 39 contains a table listing the crankshaft part and serial numbers. The table lists the engine serial number and the crankshaft serial number.

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Part 25 Aircraft

Part 25 Aircraft

Part 25 Aircraft - Using the wave pool ensured consistent conditions and enabled accurate comparisons and measurements. With the wave machine cranked up to give its most aggressive waves, one Raft Rat with extensive sailing experience noted, “the waves are a whole lot more realistic than I expected, it really is like being in the ocean.”

Subsequent open-ocean testing of many of the same life rafts previously tested in the wave pool have proven the results are accurate and scalable. We had a wide range of body types, sizes and weights, which served to show up some deficiencies we might have otherwise not noticed.

Part 25 Aircraft

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These volunteers came from throughout the U.S. and one survival instructor even came from Norway. Two couples who attended did so expressly to finalize their decision for a life raft purchase. Pragmatism aside, it's simply not prudent to travel over any significant body of water out of gliding distance from land without a life raft of some sort on board.

Hostile Environment

To do so is foolhardy, especially so if you are flying over colder waters. There is no question that the odds are in your favor if you ditch (see Equipped To Survive's “Ditching Myths Torpedoed!”), but carrying survival equipment is all about improving the odds.

There are plenty of stories of those who have survived a ditching in open water without a raft, just wearing a life vest or sometimes nothing at all to keep them afloat. Some of their stories are told on Equipped To Survive: Lessons Learned: True Life Ditching Experiences.

They were very, very lucky. Ask any of them and most will tell you so. What you don't hear about very often, for obvious reasons, are those few who don't return to tell a tale of survival against the odds.

The manufacturer is supposed to prove to the FAA that the raft meets the agency's criteria before TSO approval is granted by the FAA. It is supposed to be a rigorous examination and series of tests and generally speaking, no significant leeway is supposed to be allowed from the TSO requirements unless the applicant can convince the FAA that its design results in an equivalent level of safety.

You Can Indeed Put A Price On Human Life

Remember that point as it is important later on. We've all heard the old saw that "you can't put a price on human life." We'd like to think that was true, but there are significant, potentially life-and-death differences between the various rafts offered.

Similarly, price certainly seems to have some correlation with life-saving capability, although high price alone is no guarantee of performance. I've seen many high-priced rafts that I cannot recommend. Because the differences in price can be significant, and the differences in capability generally not very obvious, many pilots and operators often opt for the least expensive product, perhaps not realizing the tradeoffs they are making in safety.

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Often, the only goal is to meet regulatory requirements at the lowest possible price and weight, as shortsighted as that attitude may be. Safety never enters into the equation. There has been considerable confusion among many raft purchasers and users about what is required and what is approved.

This has often been aided and abetted by misleading nomenclature and, in a few instances, by patently misleading advertising by some manufacturers. To no one's great surprise, the FAA itself has not been clear on these questions at times.

What Is Required? Confusion Reigns…

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, and 737 Classic series aircraft. I asked the FAA, but they could only point me to an older Advisory Circular (AC 91-38A) which says “The liferaft requirements of Section 91.189(b)(2) (ed. – now 91.509) may be met by using:

(1) Liferafts approved under FAR 37, Section 37.122, and marked TSO-C12c. (2) Liferafts approved under FAR 37, Section 37.176, and marked TSO-C70″ (emphasis added). However, the AC is just that – advisory in nature. Note also the word "may."

Approved rafts, required under these FARs, must be manufactured by an FAA-certified manufacturer in accordance with designs approved by the FAA to meet the standards of the applicable TSO, in this case TSO C70a or its predecessor, TSO C70 or C12a (although C12a

…Type Confusion…

is largely irrelevant at this point as far as general aviation rafts are concerned). The TSO stipulates the minimum design criteria and materials and performance specifications that must be met as well as some minimal raft equipment that must be included.

A pilot who really wants a TSO'd raft, even if they aren't legally required to have it, and just figure they want one that the government has blessed, can often be bamboozled. To say nothing of those who are required to have a TSO'd raft and the appropriate equipment - they have also been known to purchase the wrong raft, much to their chagrin when the mistake is caught on an FAA inspection.

Ecfr :: 14 Cfr Part 25 -- Airworthiness Standards: Transport Category  Airplanes (Far Part 25)

With FAA "encouragement" a few years ago, Eastern Aero Marine (EAM), who makes both types of rafts, changed its nomenclature to eliminate the confusion, no longer referring to the optional equipment kits for their non-TSO'd rafts by the

FAR Part reference. But wait; we're not finished. There’s also FAR 25.1415 (b), which requires that “each life raft … must be approved.” So, regardless of what operations are being carried out, even under Part 91, transport category aircraft, which these days includes many bizjets, must use approved life rafts.

Testing And Evaluation

I also recognize that ultimate safety and performance may not be the sole consideration for a purchaser. Weight, size and price are also legitimate concerns and entirely appropriate as long as the purchaser is cognizant of the compromises that may be involved in overall performance and safety.

There will always be a range of products that are acceptable to a range of users who have different priorities. After completing the wave pool tests, the rafts were moved to a warehouse where we meticulously detailed each life raft, measuring them, taking gigabytes of digital photos and making notes of design features and equipment – ​​both good and bad.

Sea anchor/drogue effectiveness, manual inflation pump tests and other equipment tests were also conducted. Each Survival Equipment Pack (SEP) was opened and the contents analyzed and photographed, and where appropriate, tested. Equipped to Survive conducted in-water tests of aviation and marine life rafts in January 2000. This was the third of a series of similar evaluations of aviation life rafts we've run since 1994. The results reported here represent a compilation of these tests.

The airworthiness standards outlined in CFR Part 25 apply to aircraft in the transport category. The term "transport," widely used by aviation regulatory bodies in the U.S., Canada, and Europe, is typically used to describe large civil airplanes or helicopters.

What Types Of Aircraft Are Certified Under Cfr Part ?

Under the FAA's regulations, transport category aircraft can fall into one of two categories: jets with at least 10 seats or a maximum takeoff weight (MTOW) above 12,500 pounds; or propeller aircraft with either more than 19 seats or an MTOW above 19,000 pounds.

Transport category aircraft are designed and certified under CFR Part 25 and Part 26, while transport category helicopters fall under Part 29. Requirements (i.e., what type of raft (“approved” or not specified) and what minimum equipment for the raft must be on the aircraft) are dealt with in the FARs dealing with equipment for “extended over water operations” (FARs 91.509 and 135.167

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for example). Each subpart has a list of required raft equipment that differs from one to the other. With the foregoing as preamble, I hope I've laid the regulatory and features-related groundwork involving aviation life rafts for the remaining three parts of this series.

In subsequent installments, we'll look at the various features and equipment available from each manufacturer and then dive in for some in-depth examinations of single- and double-tube rafts. We'll wind up Part Four with some specific product- and manufacturer-related conclusions.

A Necessary Nuisance?

By then, you'll know exactly what to look for in an aviation life raft and, hopefully, won't get that sinking feeling if you ever have to use one. Secure .gov websites use HTTPS A lock ( LockA locked padlock ) or https:// means you've safely connected to the .gov website.

Share sensitive information only on official, secure websites. Part 91.509, “Survival equipment for over water operations,” is part of Subpart F dealing only with Large (over 12,500 pounds MGTOW) and Turbine-Powered (jet or turboprop) Multiengine Aircraft.

This does not cover your Cessna 182 or any other light GA aircraft, single or twin. FAR 91.509(b)(2) requires only that “Enough life rafts…” be aboard: There is no mention of “approved” life rafts. This is a real sore point for some folks, like those manufacturing TSO'd rafts, who insist that the raft must be TSO'd.

We tested the rafts in a wave pool, which made for a realistic test of the rafts' capabilities. As before, by the end of the test our volunteers, referring to themselves as “Raft Rats,” were beaten up, bruised and exhausted.

…Testing The Rafts…

And wet. The United States Coast Guard sent two representatives, the Coast Guard's senior rescue swimmer, Master Chief Keith Jensen, and Lieutenant Commander Paul Steward from the Office of Search And Rescue at USCG Headquarters, both to participate and observe.

LCDR Steward noted that "these tests offer a unique opportunity to further our knowledge of recreational marine and general aviation life raft features and performance which can be extremely valuable information when conducting search and rescue operations."

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In addition to setting forth general regulations, CFR Part 25 includes “subparts” spanning flight, structure, design and construction, power plant, equipment, operating limits, and electrical wiring. In all, CFR Part 25 features more than 1,800 individual regulations (read the full text here).

If you're seeking a quick primer, it's most important to understand the topic areas covered, which we've outlined below with hyperlinks to each subsection. Want more confusion? Try to figure out how many life rafts are required on board your bizjet.

What Regulations Are Set Forth In Cfr Part ?

Under FARs Part 91 Subpart F and Part 135 you only required to have “enough approved life rafts of a rated capacity and buoyancy to accommodate the occupants of the aircraft.” In Part Two, AVweb will present a "Life Raft Primer" - what features and equipment you should look for in a life raft.

Don't miss it! As long as "better than nothing" is an acceptable standard of safety for you and your passengers, you can probably get by with any of the rafts which I've otherwise found unacceptable or marginal, with the caveat noted above.

The fact remains that in most cases, they will save your life. Most, but not all. It's simply a matter of risk management - and occasionally of playing the odds. From regularly scheduled air carriers to manned free balloons and drones, the Federal Aviation Administration (FAA) regulates the activity of a wide variety of aircraft in order to ensure safe skies.

These Federal Aviation Regulations, called FARs, are part of Title 14 of the Code of Federal Regulations (CFR). As an operator, you must adhere to airworthiness standards as dictated by your part number under 14 CFR.

…And How Many?

From this I conclude that there is no regulatory basis for requiring a TSO'd raft for Part 91 operations. Further support to that interpretation is given because Part 135.167(b) says "Enough approved life rafts..." This FAR clearly requires an approved raft - it must be TSO'd.

The result is a typical FAA muddle; your best bet, if it's a concern, may be to get the FAA to issue you a written ruling, possibly avoiding problems over interpretation later on. That is not to say that all bizjet manufacturers operate in such a manner, but if you happen to be in the market for one, you might ask what raft is included.

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That may tell you something about the manufacturer's real attitude towards your safety; a view beyond their marketing hype. In addition to the righting, boarding, stability and general performance tests, the Tempe Fire Department provided a hydrant and hose to test the effectiveness of the life raft's canopies in protecting survivors in extreme weather conditions.

The screams of volunteers emanating from inside the life rafts provided quick, eloquent testimony to any deficiencies that let in the cold water. For those operations which require a life raft pursuant to the FARs, a life raft of the appropriate type must be available and it must be equipped with all the applicable equipment listed in the FARs.

Far Vs …

In other words, a Part 135 operator needs an approved (TSO'd) raft equipped with the minimum equipment listed in 135.167(b)(3). Probably the most notable change between TSO C70 and TSO C70a involves the design of single tube rafts and the effects of a deflated cell.

The older version has no requirement that the occupants be kept out of the water if a cell is lost, the newer version does. This would be a significant point if any of the rafts actually met this standard, which they don't in my opinion.

Part 121 carriers, for example, are regularly scheduled air carriers such as large U.S. airlines, cargo operators, and regional air carriers. Part 91 carriers are private operators, while foreign air carriers and foreign registered operators of U.S.

aircraft fall into Part 129. On-demand and commuter operators adhere to regulations under Part 135. Aircraft certified under 14 CFR Part 25 must comply with the airworthiness standards for airplanes in the transport category. The effort to reduce weight on some rafts was obvious, sometimes painfully so with significant decreases in safety and performance.

Hypocritical Biz-Jet Manufacturers?

We were taken back by Air Cruisers' Al Wigert's explanation that the corporate air raft makers' number one priority was reduced weight, followed by price. When we asked where the performance stood, he told us it came after those.

He explained that while that "wouldn't be the priority (ranking) of the crews" who might someday have to depend upon the rafts, that is "clearly the priority of the (corporate aircraft) manufacturers" who are their primary customers.

A global aviation leader, AerSale specializes in the sale, lease, and exchange of used aircraft, engines, and components, in addition to providing a broad range of maintenance, repair, and overhaul (MRO) services and engineering services for commercial and governmental aircraft

and components. AerSale also offers asset management services to owners of end-of-life aircraft and engine portfolios. Headquartered in Coral Gables, Florida, AerSale maintains offices and operations in the United States, Europe, and Asia. For more information on how AerSale can exceed your MRO requirements and keep your aviation assets functional and profitable from first flight to final flight, visit www.aersale.com or contact us.

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