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        <title><![CDATA[Haytham Aly — AviationNuggets]]></title>
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        <lastBuildDate>Fri, 03 Jul 2020 00:00:00 +0000</lastBuildDate>

                    <item>
                <title><![CDATA[Differences between internal and external hydraulic leaks]]></title>
                <link>https://aviationnuggets.com/blog/differences-between-internal-and-external-hydraulic-leaks?utm_source=rss&amp;utm_medium=feed</link>
                <guid isPermaLink="false">urn:uuid:f29cb233-9e66-49fa-b2cd-83274adb37fa</guid>
                <description><![CDATA[in this article, we clarify the difference between external and internal hydraulic leaks]]></description>
                                <content:encoded><![CDATA[<p style="text-align:center;"></p>
<p>in this article, we clarify the difference between external and internal hydraulic leaks</p>
<h1><strong>External leak </strong></h1>
<p>External hydraulic fluid leakage is the most recognizable type of leakage. Even the untrained eye can easily spot a broken hose spewing oil like a Texas geyser. These types of leaks will typically be repaired quickly, because the equipment, production line or process will quickly come to a halt if the problem is ignored.</p>
<h2><strong>External leaks will results:</strong></h2>
<ol>
<li>in a loss of system pressure,</li>
<li>loss of fluid,</li>
<li>a rise in the temperature of the remaining fluid</li>
<li>and cause a possible fire risk.</li>
</ol>
<h1><strong>Internal leaks:</strong></h1>
<p>Internal planned leakage is typically small orifices or pathways that allow the hydraulic fluid from a higher pressurized zone of a system to travel into a lower pressurized zone to lubricate, clean and cool a specific component or area. These planned internal leaks do not allow the fluid to exit the hydraulic circuit, so there is no visual indication of its presence. The most common cause of excessive internal leakage is wear of component surfaces during normal operation.</p>
<p>The vast majority of hydraulic systems in operation today have leaks - leaks that are planned. They are designed with a specific function in mind, and in many cases, are documented by the original equipment manufacturer (OEM) as the amount of acceptable leakage under normal operating conditions.</p>
<p>Leakage can also result from poor system design, incorrect component selection, and poor quality control tolerances during the manufacturing of a component, and incorrect overhaul of rebuilt components.</p>
<p>System performance, reliability, and increased operating temperatures are the first visual signs of excessive internal leakage.</p>
<ol>
<li>happens from high pressure to low,</li>
<li>causes a drop in system pressure,</li>
<li>more activity of pressure regulating or cut-out valves</li>
<li>and a rise in system temperature.</li>
<li>Internal leaks cause a rise in fluid<br />temperature</li>
</ol>
<p> </p>
<p>Detection and quantification of the fluid consumption is the first step in external leak control. Up-to-date reservoir management records must be maintained to determine when by whom and how much fluid was required to top-up a reservoir. These records should be used along with visual inspections to determine the location and the leak rate of any detected anomalies.</p>
<h2><strong>References:</strong></h2>
<ul>
<li>1.Photo by <a href="https://unsplash.com/@fatgar?utm_source=unsplash&amp;utm_medium=referral&amp;utm_content=creditCopyText">Fatima Garcia</a> on <a href="https://unsplash.com/s/photos/plane-servicing?utm_source=unsplash&amp;utm_medium=referral&amp;utm_content=creditCopyText">Unsplash</a></li>
<li>A320 Maintenance Manual</li>
</ul>]]></content:encoded>
                                
                <dc:creator><![CDATA[Haytham Aly]]></dc:creator>
                <pubDate>Fri, 03 Jul 2020 00:00:00 +0000</pubDate>
                <atom:updated>2020-07-03T00:00:00+00:00</atom:updated>
                                                <category><![CDATA[Aviation Maintenance & Engineering]]></category>
                                <category><![CDATA[Featured]]></category>
                            </item>
                    <item>
                <title><![CDATA[Avoiding Fuel Spills on A320 Family Aircraft]]></title>
                <link>https://aviationnuggets.com/blog/avoiding-fuel-spills-on-a320-family-aircraft?utm_source=rss&amp;utm_medium=feed</link>
                <guid isPermaLink="false">urn:uuid:3688fac6-c5ba-4a56-afa3-3993021cc9cf</guid>
                <description><![CDATA[Cases of fuel spillage have been reported to Airbus on A320 family aircraft equipped with fuel transfer jet-pumps in the center tank.
This article recalls the protections available against tank overf]]></description>
                                <content:encoded><![CDATA[<p></p>
<h1><strong>Introduction</strong></h1>
<p>Cases of fuel spillage have been reported to Airbus on A320 family aircraft equipped with fuel transfer jet-pumps in the center tank.</p>
<p>This article recalls the protections available against tank overfill. It explains why fuel spillage happened on the reported events and provides recommendations on how to avoid it.</p>
<h1><strong>OVERFILL AND OVERFLOW PROTECTION AND MONITORING</strong></h1>
<p>Fuel tanks on Airbus aircraft are designed so that fuel spills into the vent tank through their vent line in the event of a tank overfill. Each vent tank is equipped with a NACA duct where fuel can flow out and onto the ground if the vent tank is full.</p>
<h1><strong>Refuel valves automatic closure</strong></h1>
<p>On A320 family aircraft, the refuel valve for a fuel tank will automatically close when the targeted fuel quantity is reached, or fuel is detected by the high-level sensor fitted in the tank during refueling.</p>
<p>Protection is available to prevent fuel spill incidents from Airbus aircraft during refueling. Sensors fitted to the center tank and wing tanks will automatically close the refuel valves to stop the refueling operation, preventing overfill. Fuel spills are avoided if these protections are operating correctly and this should be checked by a quick test just before refueling the aircraft.</p>
<p>Fuel spillages were reported to Airbus on A320 family aircraft fitted with transfer jet pumps where the fuel transfer mode selection was mistakenly left in MANUAL. Ensuring that the FUEL MODE SELector is set to AUTO before refueling the aircraft will avoid a fuel spill incident.</p>
<h1><strong>WHAT TO DO IN THE CASE OF A FUEL SPILLAGE?</strong></h1>
<p>In the event of fuel spillage, Airbus recommends the following actions:</p>
<ol>
<li>Perform TSM Task “Refuel - Fuel Spillage From NACA Vent During Refuel’ to identify the root cause of the spillage</li>
<li>Notify Airbus about the fuel spillage event and provide the following information:<br />                a. Fuel Spillage Sheet (available in the TSM task)<br />                b. Fault Reports<br />                c. Shop Reports of replaced components if any, including Part Number and Serial Number.</li>
</ol>]]></content:encoded>
                                
                <dc:creator><![CDATA[Haytham Aly]]></dc:creator>
                <pubDate>Fri, 17 Apr 2020 00:00:00 +0000</pubDate>
                <atom:updated>2020-04-17T00:00:00+00:00</atom:updated>
                                                <category><![CDATA[Aviation Maintenance & Engineering]]></category>
                                <category><![CDATA[Aviation Safety]]></category>
                                <category><![CDATA[Aviation Tecnology]]></category>
                            </item>
                    <item>
                <title><![CDATA[Difference between Engine and the tailpipe fire]]></title>
                <link>https://aviationnuggets.com/blog/difference-between-engine-and-the-tailpipe-fire?utm_source=rss&amp;utm_medium=feed</link>
                <guid isPermaLink="false">urn:uuid:3e4fae8a-0e0b-4f79-bac6-5cc1e0d75de0</guid>
                <description><![CDATA[brief about the two types of fire that may affect the aircraft turbofan engines, for pilots and engineers, Engine fire is an external one, also called...]]></description>
                                <content:encoded><![CDATA[<div>
<div>
<p></p>
</div>
<div>The above video contain brief about the two types of fire that may affect the aircraft turbofan engines, for pilots and engineers, Engine fire is an external one, also called a nacelle fire, but the tailpipe fire is an internal fire or core fire as the fire is developing within the combustion chamber or in the aft turbine race, the difference between the engine fire and the tailpipe fire is very important as to know how to extinguish them during engine run up procedures , they are totally different , their procedures to extinguish are totally different, as there is a different in location between them, also the fire bottles available for each engine are only for the engine fire, again, engine fire is an external fire or a nacelle fire, but the tailpipe fire is an internal fire or a core fire, this is applicable to all turbofan engines whatever the manufacturer , this is for all GE, pratt, V2500 , CFM, Trent, Rolls Royce , this video is an aviation training solution for the benefits of all pilots and aircraft maintenance engineers, technicians and mechanics as pilots and engineers may have panic during a fire events during engine running and they mistakenly distinguish this type of fire and may apply the wrong procedures and this is horrific, a tailpipe fire if not extinguished within minimum delay it may transfer to an engine fire.</div>
</div>
<div> </div>
<h3>References:</h3>
<ol>
<li>                                                         <strong>Airbus Safety first magazine</strong></li>
</ol>
<blockquote>
<h1>FOR TRAINING PURPOSE ONLY</h1>
</blockquote>]]></content:encoded>
                                
                <dc:creator><![CDATA[Haytham Aly]]></dc:creator>
                <pubDate>Fri, 22 Nov 2019 00:00:00 +0000</pubDate>
                <atom:updated>2019-11-22T00:00:00+00:00</atom:updated>
                                                <category><![CDATA[Aviation Maintenance & Engineering]]></category>
                                <category><![CDATA[Aircraft Pilots]]></category>
                                <category><![CDATA[Aviation Safety]]></category>
                            </item>
                    <item>
                <title><![CDATA[Aircraft Jacking]]></title>
                <link>https://aviationnuggets.com/blog/aircraft-jacking?utm_source=rss&amp;utm_medium=feed</link>
                <guid isPermaLink="false">urn:uuid:bf85883e-f955-48c9-af33-2732cb71257f</guid>
                <description><![CDATA[Each aircraft type has a specific jacking procedures stated in the Aircraft Maintenance Manual AMM ,here in this blog tried summarize the concept of the ...]]></description>
                                <content:encoded><![CDATA[<div>
<div>Each aircraft type has a specific jacking procedures stated in the <em><strong>Aircraft Maintenance Manual AMM</strong></em>  Chapter 07,here in this blog tried summarize the concept of the aircraft jacking procedure.</div>
</div>
<div> </div>
<div>
<h5><strong>Why aircraft jacking ?</strong></h5>
<ul>
<li>Perform maintenance require lifting (jacking)- for example : change tire,brake unit... .</li>
<li>Landing gear extension retraction test.</li>
<li>Place the aircraft into rigging position.</li>
<li>Aircraft weighing and CG calculations.</li>
</ul>
<h5><strong>Where is the ideal place to jack an aircraft ?</strong></h5>
<p>To know where is the ideal place for lifting the aircraft let us ask ourselves what are the requirements for lifting the aircraft with respect to the place?</p>
<ul>
<li>Leveled place.</li>
<li>Place well protected from the wind.</li>
</ul>
<p>always the appropriate place for such procedure is the maintenance hangar .</p>

<h5><strong>Jacking safety precautions :</strong></h5>
<div><strong>MAKE SURE THAT THE AIRCRAFT IS STABLE AND THAT THE WEIGHT IS APPLIED EQUALLY ON EACH SIDE OF THE AIRCRAFT CENTER LINE.</strong></div>
</div>
<div> </div>
<div><strong>BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.</strong></div>
<div> </div>
<div><strong>WHEN YOU DO THE LEVELING/LIFTING OR LOWERING OF THE AIRCRAFT, MAKE SURE THAT: </strong></div>
<ul>
<li><strong> YOU USE THE CORRECT LIFTING/LOWERING EQUIPMENT FOR THE CONDITIONS </strong></li>
<li><strong> THE PERSONS WHO OPERATE THE LIFTING/LOWERING EQUIPMENT HAVE THE CORRECT TRAINING AND KNOWLEDGE </strong></li>
<li><strong> THE NECESSARY SAFETY AREA IS IDENTIFIED </strong></li>
<li><strong> THERE ARE NO UNWANTED PERSONS OR EQUIPMENT IN THIS AREA </strong></li>
<li><strong> THERE IS NO WORK IN PROGRESS ON THE AIRCRAFT. IF YOU DO NOT OBEY THESE PRECAUTIONS, INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT CAN OCCUR.</strong></li>
</ul>
<p> </p>
<p><strong>MAKE SURE THAT THE LOAD ON THE JACKS IS NOT MORE THAN THE MAXIMUM LOAD SPECIFIED IN THIS PROCEDURE.</strong></p>
<p> </p>
<p><strong>MAKE SURE THAT THE WEIGHT OF THE AIRCRAFT IS NOT MORE THAN THE MAXIMUM WEIGHT SPECIFIED IN THIS PROCEDURE.</strong></p>
<p> </p>
<p><strong>OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING AND RUBBER GLOVES.</strong></p>]]></content:encoded>
                                
                <dc:creator><![CDATA[Haytham Aly]]></dc:creator>
                <pubDate>Sun, 04 Nov 2018 00:00:00 +0000</pubDate>
                <atom:updated>2018-11-04T00:00:00+00:00</atom:updated>
                                                <category><![CDATA[Aviation Maintenance & Engineering]]></category>
                                <category><![CDATA[Featured]]></category>
                                <category><![CDATA[Aviation Tecnology]]></category>
                            </item>
                    <item>
                <title><![CDATA[What is Aircraft Fire Extinguisher Agent?]]></title>
                <link>https://aviationnuggets.com/blog/what-is-aircraft-fire-extinguisher-agent?utm_source=rss&amp;utm_medium=feed</link>
                <guid isPermaLink="false">urn:uuid:de5a4d74-1c64-45b3-b4f7-0b2f61fa6c59</guid>
                <description><![CDATA[Halon gas is the aviation fire extinguisher agent leader , used for suppression fire in many aircraft components such as the engines, APU...]]></description>
                                <content:encoded><![CDATA[<p></p>
<h3>What is agent used inside fire extinguisher in the aviation ?</h3>
<p><em><strong>Halon gas</strong></em> is the aviation fire extinguisher agent leader , used for suppression fire in many aircraft components such as the engines, APU (auxiliary power units) , cargo compartments and you can find it even in the handheld fire extinguisher bottles through the cabin and the flight deck compartments, tell now the aviation industry can not find a replacement for the halon gas because the regulation insist on a very restricted characteristics, all the civil aircraft including Boeing, airbus are using the halon gas for the fire bottles as a suppression agent for fighting the abnormal fire situations , engines may suffer a nacelle fire so the halon gas must be submitted to extinguish such fire, halon gas is good for all types of fire.</p>
<h3>Why " Hallon Gas" ?</h3>
<ul>
<li>Will not damage engine parts (no negative impact on the engine).</li>
<li>Very dry gas.</li>
<li>Non corrosive.</li>
<li>Not conductive.</li>
<li>Leave no residue.</li>
<li>So effective in small quantities (reliable and effective ).</li>
<li>Effective even in high altitudes .</li>
<li>compatible with wide range of material and equipment include : electronics - fluids - composites - metals</li>
</ul>
<h3>Types &amp; Usage :</h3>
<ul>
<li><em><strong>Hallon 1301</strong> </em>used for Engine - APU - cargo compartment - lavatory.</li>
<li><em><strong>Hallon 1211</strong></em> used for cabin - flight deck - accessible cargo compartment -crew rest compartment - handheld fire extinguisher .</li>
</ul>
<h4>References :</h4>
<blockquote>
<h1>FOR TRAINING PURPOSE ONLY</h1>
</blockquote>]]></content:encoded>
                                
                <dc:creator><![CDATA[Haytham Aly]]></dc:creator>
                <pubDate>Sun, 07 Oct 2018 00:00:00 +0000</pubDate>
                <atom:updated>2018-10-07T00:00:00+00:00</atom:updated>
                                                <category><![CDATA[Aviation Maintenance & Engineering]]></category>
                                <category><![CDATA[Aviation Safety]]></category>
                                <category><![CDATA[Aviation Tecnology]]></category>
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