Fuel System Pressure: Piper 140'S Common Causes

what causes pressure in fuel system piper 140

The Piper Cherokee 140 is a popular aircraft that has been in production for over a decade, with more than 10,000 units built. While it is generally considered a safe and stable aircraft for instrument training, some pilots and owners have reported issues with low or high fuel pressure, which can cause power loss or reduction during flight. In this article, we will explore the potential causes of fuel pressure issues in the Piper Cherokee 140, including blocked vents, faulty fuel pumps, and the impact of temperature and fuel type. We will also discuss preventative measures and share insights from experienced pilots and mechanics on maintaining and troubleshooting the fuel system of this iconic aircraft.

shunfuel

Blocked vents

Blocked fuel vents can cause pressure issues in the fuel system of a Piper 140. The Piper 140 has two vents in each tank, and if both of these are plugged, it can cause problems. The first and most visible vent is a small tube under the wing at the outboard aft side of the fuel tank, near the jack points. This vent is cut at an angle facing forward to provide ram air pressure into the tank. The second vent is located in the fuel cap and is an orange rubber "umbrella" in the centre of the fuel cap, which covers the breather holes. If the umbrella is forced open by air pressure, it will allow air into the tank through the fuel cap.

One way to check for blocked vents is to use the blow technique. This involves blowing into the underwing line or a small tube connected to the vent. If you can hear and feel the tank expand, and then smell fuel vapours when you stop blowing, the vents are clear. If you can't blow into the tank, the line is likely plugged.

It's also important to consider other factors that can affect fuel pressure, such as temperature and altitude. Vapor lock can occur during hot weather, especially if auto fuel with ethanol is used. Additionally, changes in altitude can affect fuel pressure, as air pressure changes can impact the function of the vents.

If you suspect blocked vents or other fuel system issues, it is crucial to have a qualified mechanic inspect the aircraft before the next flight.

shunfuel

Faulty fuel pump

A faulty fuel pump can cause pressure issues in the fuel system of a Piper 140 aircraft. Fuel pumps play a critical role in ensuring a consistent and adequate fuel supply to the engine, and any malfunction can lead to significant performance issues.

One common issue with the Piper 140's fuel system is low fuel pressure, which can be caused by a faulty or failing fuel pump. This problem is often observed when the fuel tanks are full, with the pressure gauge reading significantly lower than normal levels. In some cases, turning on the electric pump can temporarily resolve the issue, bringing the pressure back up to acceptable levels. However, this may not always be effective, and it is crucial to address the underlying cause to prevent potential engine problems during flight.

The fuel pump's age and overall condition are essential factors to consider. Over time, fuel pumps can become worn or damaged, leading to reduced efficiency or, in some cases, complete failure. In the case of the Piper 140, the engine-driven fuel pump is a common culprit, especially if it has not been adequately maintained or replaced in many years. Operating the aircraft in hot weather can further exacerbate the issue, as higher temperatures can cause the fuel to turn into vapour, leading to a condition known as vapour lock, where the fuel pump is unable to draw fuel into the engine.

Additionally, fuel pump-related issues can also lead to sporadic high-pressure readings on the fuel pressure gauge. While this issue may not be directly related to the fuel pump, it is worth considering as part of the troubleshooting process. In some cases, the fuel pump may need to be replaced, especially if the problem persists despite other interventions.

To diagnose a faulty fuel pump, it is essential to inspect the pump and the entire fuel system for any signs of damage, leaks, or clogs. This may include checking fuel vents, hoses, and blast tubes for proper connectivity and functionality. If the fuel pump is suspected to be the root cause, it may be necessary to replace it with a new or properly functioning unit to restore the fuel system's normal operation and ensure the aircraft's overall performance and safety.

shunfuel

Blocked crankcase breather

A blocked crankcase breather can cause pressure issues in the fuel system of a Piper 140 aircraft. The crankcase breather tube plays a crucial role in maintaining appropriate pressure within the engine. When this tube is blocked, it can lead to a build-up of pressure in the crankcase, which in turn affects the fuel system.

The crankcase breather tube is responsible for venting excess pressure from the crankcase, ensuring that it remains at the optimal level. If the breather tube becomes blocked, the pressure has no means of escape, leading to a rise in pressure within the engine. This increased pressure can then impact the fuel system, causing fluctuations in fuel pressure and, in some cases, even resulting in fuel pump malfunction.

In a Piper 140, a blocked crankcase breather can lead to a range of issues, from erratic fuel pressure gauge readings to more serious problems such as reduced engine performance or rough running. The blockage prevents the crankcase from venting properly, leading to a build-up of pressure that can affect the entire engine system, including the fuel delivery.

To address this issue, it is essential to ensure that the crankcase breather tube is clear and functioning correctly. Regular inspection and maintenance of the breather tube are crucial to prevent blockages and maintain the integrity of the fuel system. Clearing any debris or build-up within the tube can help restore proper ventilation and alleviate the pressure within the crankcase.

Additionally, it is worth noting that the crankcase breather tube is just one component of the aircraft's ventilation system. Other factors, such as the condition of the fuel vents and the efficiency of the fuel pump, can also contribute to pressure fluctuations in the fuel system. Therefore, a comprehensive inspection and troubleshooting approach is necessary to identify and rectify the root cause of any pressure-related issues in the Piper 140's fuel system.

shunfuel

Faulty fuel selector

The fuel selector is an important component of the fuel system in a Piper 140 aircraft. A faulty fuel selector can cause issues with fuel pressure and engine performance. Here are some detailed paragraphs on the topic of "Faulty Fuel Selector" in relation to the Piper 140:

The Piper 140, also known as the Cherokee 140, is a popular aircraft model known for its reliability and performance. However, one issue that has been reported by some pilots and owners is the problem of faulty fuel selectors. The fuel selector is a critical component in the fuel system, allowing the pilot to choose between the left and right fuel tanks, and ensuring a consistent fuel supply to the engine.

The early models of the Piper 140, particularly the PA-28-140, were equipped with first-generation flat-plate fuel selectors. These older-style fuel selectors lacked safety features to prevent unintentional misalignment or over-rotation, which could result in the inadvertent selection of the off position. This meant that during flight, it was possible for the fuel supply to be cut off accidentally, leading to a loss of engine power. In some cases, pilots have reported that the fuel selector valve was found to be in an intermediate position between the left and right tank positions, resulting in fuel starvation and engine malfunction.

To address this safety concern, the Federal Aviation Administration (FAA) issued an Airworthiness Concern Sheet for the early Piper Cherokee and Arrow aircraft, including the PA-28-140. The FAA warned that the fuel selector arrangement in these aircraft did not include adequate protection against accidental selection of the off position. This issue was not limited to a single incident, and the FAA recognized the potential for widespread unsafe conditions. As a result, the FAA worked with Piper to mandate the upgrade from generation 2 fuel selectors to the improved generation 3 fuel selectors, which require extra effort to select the off position.

It is crucial for pilots of the Piper 140 to be aware of this potential issue and to ensure their aircraft has the latest generation of fuel selectors installed. Regular inspection and maintenance of the fuel system, including the fuel selector valve, are essential to mitigate the risk of fuel starvation and engine failure. Additionally, pilots should exercise caution when switching fuel tanks during critical phases of flight, as recommended by experienced Piper owners and pilots.

In conclusion, a faulty fuel selector in the Piper 140 can have significant consequences on the aircraft's performance and safety. It is important for owners and pilots to stay vigilant and proactive in addressing this issue by installing the recommended upgrades, conducting thorough inspections, and following best practices during flight operations.

shunfuel

Fuel contamination

Another cause of fuel contamination can be servicing the aircraft with improperly filtered fuel from small tanks or drums. It is crucial to ensure that the fuel is properly filtered to prevent contaminants from entering the fuel system. Additionally, storing aircraft with partially filled fuel tanks can also lead to fuel contamination. It is recommended to drain enough fuel from the fuel strainer to ensure that fuel is being drained from the tank, as water may remain at the bottom of the tank even after the drainage process.

Furthermore, a lack of proper maintenance can also contribute to fuel contamination. Regular maintenance checks and replacements of fuel system components are necessary to prevent corrosion and leaks. For example, the design and location of the battery box in the Piper PA-28-140 can lead to corrosion of the fuel line due to trapped water. It is essential to inspect this area during pre-purchase or pre-flight inspections and address any signs of corrosion or water intrusion.

In conclusion, fuel contamination in Piper PA-28-140 aircraft can have serious consequences, and it is crucial for pilots and mechanics to take preventive measures. By conducting thorough pre-flight inspections, properly draining fuel tanks, ensuring proper fuel filtration, and maintaining the fuel system, the risks of fuel contamination can be significantly reduced.

Frequently asked questions

There could be a number of reasons for low fuel pressure in your Piper 140. It could be due to inadequate venting, a faulty fuel pump, blocked crankcase breather, or a problem with the fuel selector. It is important to check for any leaks or clogs in the fuel system and ensure that the vents and fuel caps are clear.

High fuel pressure in your Piper 140 could be caused by a blockage in the crankcase breather, resulting in high crankcase pressure. It could also be due to vapor lock, especially if you are using auto fuel or fuel with a high Reid Vapor Pressure (RVP).

You can use the "blow" technique to check for vent blockages. Cover a small hole in the vent line and blow into the underwing line. If you are able to blow into the tank and hear the air leaving, then the vent is clear.

Fluctuations in fuel pressure and RPM could be due to a number of factors, including fuel type, temperature, and vapor lock. It is recommended to check for any leaks or restrictions in the fuel system and ensure that the fuel selector is in the correct position.

Written by
Reviewed by
Share this post
Print
Did this article help you?

Leave a comment