...* A. * * An approach path for an aircraft landing is shown in the figure and satisfies the following conditions: * (i) The cruising altitude is h when descent starts at a horizontal distance L from touch- down at the origin. (Note: in this coordinate system, the direction of flight is from right to left or in the negative –x direction). (ii) The pilot must maintain a constant horizontal speed v throughout the descent.(Note: speed is the absolute value of velocity. In this instance the velocity will be negative, however, the speed will be a positive number of the same magnitude). (iii) The absolute value of the vertical acceleration should not exceed a constant k (which is much less than the acceleration due to gravity). * ------------------------------------------------- * * 1. Find a cubic polynomial that satisfies condition (i) by imposing suitable conditions on and at the start of descent and touchdown. * Solution: Assume the cubic polynomial function is P(x)= ax3 + bx2 + cx + d According to the graph, We know P(0) = 0, P'(0) = 0, P(L) = h, P'(L) = 0 The original equation is P(x)= ax3 + bx2 + cx + d P(0) = 0, so plug in zero for x. You will find that d = 0. Simplify the equation to P(x)= ax3 + bx2 + cx Find the derivative of P(X), which is 3ax2 + 2bx + c P’(0) = 0, so plug in zero for x. We found that c =0 Simplify the equation to P’(X) = 3ax2 + 2bx Plug in P'(L) = 0 We get the equation of 3aL2+ 2bL= 0 ① Plug in P(L) = h We get the equation...
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...Boeing’s ‘Dreamliner’ – an Operations Nightmare 1 a) Boeing is the world’s largest aerospace company and leading manufacturer of commercial jetliners and defence, space and security systems. Boeing’s products and services include commercial and military aircraft. It also includes satellites, weapons electronic and defence systems. 1 b) There are many issues Boeing had faced in introducing new technology to its ‘Dreamliner’ plane. Firstly, they had ditched the more traditional hydraulic systems for the landing gear and had gone for electric systems instead, and because of this, Boeing had left themselves working with something less familiar than the traditional landing gear to work with, therefore increasing the risks of the 787 plane and its landing. Although the technological leap was always likely to cause teething issues, it worsened when they decided to bring a high percentage of their plane parts from outside contractors. Again, by introducing new, foreign technology to its Dreamliner plane, Boeing had faced more issues than they would have because not only did it take longer for them to get the parts (delayed by 3 years) but it had also led to the parts not even fitting together properly, which causes even more delay and money to ‘fix’ the parts in order for them to somehow fit. 2 a) The use of sub-contracting may have been an unwise decision in the case of the Boeing Dreamliner because sub-contracting means employing a firm outside one’s company to do the work...
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...Conclusion We have learned from this Rotational Energy experiment that rotational energy is pretty powerful. We learned how to actually calculate and configure our own values for rotational energy rather than collecting them from a problem in the book, and actually use them to achieve our purpose of landing the ball into the cup. We did not achieve our purpose, but we did get pretty close in a couple of our tries. This experiment showed us how rotational energy worked and how it can account for many things. We had to calculate multiple things to find the rotational energy and then find the distance at which we need to place the cup. We needed to know the height of not only the table but the ramps as well. We needed to calculate exactly where the ball would land after it left the ramps and was in free fall to the floor. That is where we should place the cup so that the ball will land in the cup. Our calculations we not 100% correct as we did not make it into the cup. Some of the uncertainties that could have accounted for us not making the ball into the cup would be incorrect measurements. We could have accidently misread some of our measurements. Also we did not account for the height of the cup, so where the ball would normally land it would miss the cup because the cup’s opening was too high. Also we did not account for friction in our calculations, so that could have caused some caused some calculations to be slightly off. Also the wooden balls may not have been perfectly...
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...3.3 Airport Slots Connectivity, especially through hub operations, would depend largely on the allocation of airport slots for connecting flights. The number of airports that use full capacity of their slots are increasing in recent years. These airports are called Level 3 airports. Operators should not misuse their airport slots like different time or different way. If operator complies with its slots, the slot cannot be confiscated. Slots can be exchanged or transferred between airlines. Slot allocation is independent from bilateral air service agreements. Most countries use IATA Worldwide Slot Guidelines (WSG) as standard. Because of the physical capacity of airports airport slot system is needed for sure, but it’s affecting the air transportation market in a bad way, some operators adopt practices that decrease the efficiency of this process. Because slots are so valuable, some companies overbid, return the slots late or under-utilize just enough to keep the slot so that it can be sold for a higher price. The studies about increasing the efficiency of slot allocation is not enough to conclude a solution. There is a need for the international aviation community to standardize the slot allocation procedures and work together for better policies. ATC slots are different than airport slots and they are not predefined, they should also comply with airport slots, so that scheduled times can be met. Some studies has had conclusions to solve the issues of the airport slot allocation...
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...that happened in 1997 at Newark International Airport in New Jersey. The paper will address the causes of the accidents, the findings of the investigation carried out after the accident, recommendations after the investigation as well as the measures taken to make sure that accidents of this type do not happen again. Aviation Safety FedEx Express Flight 14 This scheduled cargo flight was going to Newark International Airport, New Jersey from the Ted Stevens Anchorage International Airport in Anchorage, Alaska. It crashed when trying to make a safe landing on July 31, 1997. The pilots thought that the plane would have little stopping distance after landing, which made them think of landing early on the runway. Misinterpretation of runway data was the main cause of the crash (Dismukes, Berman & Loukopoulos, 2012). The pilots were aware that the plane had problems with its auto-breaks because they failed to initiate during landing, which also contributed to their hasty decision to land the craft earlier than expected. The problem arose at the commencement of the flare phase. The MD-11 touched down and rolled, which continued until the spars of the right wing broke. The craft crashed on the runway on its back and it was on fire. Luckily, none of the crewmembers suffered any injuries. The National Transportation Safety Board conducted an investigation on the causes of both the...
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...part a) and part b), do you believe PPP is a potential solution (by reducing the arrival rates during periods where demand is much higher) to reduce the costs of over scheduling? QUESTION 2 Once you read the Delay at Logan Airport case it is clear that peak periods exist for a reason. That is, they are not random fluctuations but rather a result of passenger’s desires for landings and takeoffs at certain times of the day. Therefore airlines will shift flights to different periods only if the costs of incurring peak charges outweigh the costs (in terms of lost revenue and customer dissatisfaction) of shifting flights to off-peak periods. Continue to assume that planes fly with 35% of passenger seats empty (that is, 65% load factor) and also assume that per passenger revenue for different aircraft sizes are as follows; $230 for a turboprop airplane with 15 seats; $154 for a regional jet with 50 seats; $402 for a jet with 150 seats. a) ( ) Which airplane types would feel a significant economic impact by peak-period landing fee of $150? What about $200 fee? What about $250 fee? b) ( ) Assume that $150 landing fee is sufficient to reduce the peak period demand to 55 planes per hour, similarly with $200 fee...
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...Case Analysis 4: FedEx Express MD-10 Landing Gear Failure Karreem L. Lisbon Embry-Riddle University This paper will cover information on a FedEx Express MD-10 Landing Gear Failure. Specifically, research and information pertaining to the accident that occurred on October 28, 2016. Additionally, information will be analyzed and presented on the primary cause of the accident. The research for the paper will be conducted through the use of the world-wide web and the Hunt Library. FedEx Express flight 910, a Boeing MD-10-10F (registration N370FE) experienced a left main landing gear collapse and subsequent fire in the left wing after landing on Runway 10L at Fort Lauderdale–Hollywood International Airport, Fort Lauderdale, Florida, Oct. 28, about 5:51 p.m. EDT. The airplane came to rest on the side of Runway 10L. The two flight crew members evacuated the airplane via the cockpit window and were not injured. The airplane was substantially damaged. The cargo flight originated from Memphis International Airport, Memphis, Tennessee,(Knudson, 2016)....
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...Embry-Riddle University Nigeria Airways Flight 2120 Nationair DC-8 Flight 2120 took the lives of 247 passengers and 14 crew members; 261 in all; during takeoff on July 11, 1991. The jet was owned by Canadian airline Nolisair, and was being operated by a Nigerian company to transport Nigerian pilgrims in and out of Mecca. The DC- 8 caught fire during take-off from Abdulaziz International Airport, Jeddah, Saudi Arabia. Pilots noticed problems during early stages of take-off and only made it 671 meters in elevation before attempting to turn around for a emergency landing. It was too late; the under inflated tires had overheated began to catch fire. The fire grew and blew out the hydraulics which made the emergency landing impossible. This was the worst wreck a DC-8 had ever experienced and has held the record for many years following. The NTSB concluded that the fire could have been handled by leaving the landing gear extended and away from the plane. Although the pilots failed to make the right decision, and added just one more human error to the equation, it was the obvious neglect by the maintenance team that caused this horrific accident. There are many human factors which played a vital role in the crash. The maintenance team failed to inflate the #2 and #4 main gear tires after recognizing the pressure during the pre-flight. An attempt to inflate the tires failed because there was no nitrogen available at the location. Further investigation shows later that the maintenance...
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...TABLE OF CONTENTS LIST OF FIGURES ................................................................................................................. ii LIST OF TABLES ................................................................................................................... ii ABSTRACT............................................................................................................................ iii CHAPTER 1: INTRODUCTION ............................................................................................ 1 1.1. 1.2. 1.3. 1.4. Introductory of the Title ........................................................................................... 1 Objective and Purpose ............................................................................................. 2 Problem Statement and Problem Solving ................................................................ 3 Limitation of the Project .......................................................................................... 4 CHAPTER 2: LITERITURE REVIEW ................................................................................... 5 2.1. 2.2. Research Theory, Ideology and Concept ................................................................. 5 Previous Research and Proposed Project Comparison........................................... 11 CHAPTER 3: METHODOLOGY ......................................................................................... 12 3.1.0 3.2.0. 3.2.1. 3.2.2. 3...
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...General description: beechcraft-model c50 twin bonanza is a six-place, low-wing, all-metal monoplane with tricycle landing gear. It is powered by two Lycoming go 480-f6 engines, each rated at 275 horsepower for take-off. The engines have reduction gearing to the propeller shafts and drive beach craft model 279 full-feathering, constant-speed propellers with aluminum blades. This is intended to be a guide for some of the procedures for this specific aircraft. Servicing fuel tanks- the airplane fuel system should be serviced with 30/87 octane fuel. The fuel system is suitable for aromatic fuels. Fuel system access doors are of the flush type and are located on the upper surface of each outboard wing panel and each side of the wing center section. Expanding-type filler caps with neoprene seals are used on each filler opening. The fuel tanks are not interconnected and each tank must be serviced separately. Hoisting airplane the aircraft may be hoisted for mantenance or parts replacement through the use of a three-cable sling attached to the hoisting lugs and eyebolt. A minimum overhead clearance of 12 feet 6 inches and a hoist of at least 3 tons capacity is required .To hoist engine remove the propeller and cowling and attaching a hoist to the engine lifting eyes provided on top of engine. Jacking provision is made for a three-point jack-pad system the two aft pads are located on the center section rear spar in board of each nacelle(a streamlined housing or tank on the outside of...
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...Vo - lan - tor (vo-lan'ter) n. A vertical takeoff and landing aircraft that is capable of flying in a quick, nimble, and agile manner. --intr. & tr.v. -tored, -toring, tors. To go or carry by volantor. [Lat. volare, to fly. Fr. volant, to move in a nimble and agile manner] The Skycar is capable of vertical take-off and landing (VTOL) similar to a helicopter and flies from point of departure to destination much like an airplane. However, the Skycar has been designed to also travel at low speed for short distances on the ground like an automobile. It has fold-up wings which make it narrow enough to be useable on roadways. All this and, incredibly, it's easy to fly! Actually we believe that most of "flying" will be done by the on-board systems. The aircraft is controlled by the pilot providing inputs for direction, speed and altitude through the simple controls and the on-board systems interpret these inputs to do the flying...it is called a "fly by wire" system. Therefore operating a Skycar, while very easy, could be done by someone with little training or flight experience, but will, at least initially, require a private pilot's license until the ease of operation and safety are thoroughly demonstrated. The Moller Skycar is a volantor capable of these remarkable capabilities through the use of latest proprietary technologies developed by Moller International. Favorable power to weight ratio is the basic qualification for VTOL. However, in order to create a safe, environmentally...
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...Current situation Delays are a very important issue at Boston’s Logan Airport, the fifth most delayed airport in the United States. Approximately 4.75% of total flights at Logan Airport are delayed and with total annual operations projected to increase over the next 15 years, it is important to address this issue today. Delay costs, which include operational and human costs, prove to be extensive and therefore a solution has to be found to ensure the survival of Logan airport. The major causes of these delays include the adverse weather conditions as well as the fact that demand tends to be clustered at certain periods of the day. There are several approaches that can be taken to conquer this delay problem. The first option, which has been determined to be the best alternative, is to build another runway. This would ensure at least two operating runways at all times, regardless of weather conditions. The second option proposed for dealing with the delay issue is that of peak period pricing (PPP), which entails increasing airline fees during periods of high demand in order to spread the demand for flights more evenly throughout the day. Problem analysis Weather is the foremost cause of delays in the case of Logan Airport. The airport’s operational capacity is significantly impacted by these adverse weather conditions (declining from approximately 120 operations per hour in normal conditions to approximately 80 operations per hour). In some cases, entire runways must be...
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...I had always wanted to kickflip it. So we both decided that we would both try it first on the 6th there before we started trying our checks on the 6th there, we took a glance at the Aged and sized it up and compared the two sets. The eight stair and 6 that have the same length and height stairs but was only two longer so it'll only added about a foot extra and length and maybe half a foot in height. We both began talking to each other about how we have both skated bigger things and we had always wanted to learn these tricks for a while. After we got done sizing up the age there we walked over to the six and began to warm up on it. The first tricks I like to try when I'm skating asset is an ollie which is basically just jumping down and landing on the board. That was the easy part me and my friend meet you both did that first try and then we were onto the next one. The first couple tries were pretty wild, I would either take out my board as soon as I jumped just jump off my board or just not even commit as a whole. But as the sun begin to go down I knew my time was coming close to an end. I would have to hurry up and land it before dark is once it gets dark out you can't see your board under you. After about 5 tries of not getting even close I put a hundred and 10% to it and try my very hardest. I landed on it but cannot roll away I would then try a few more times and get closer and closer by the try the same goes for my friend. Once I had landed it my buddy landed it within a...
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...has 72 planes within it and when you click on each manufacturer it brings up all the models that they have specifications on. You can explore all the different models from each manufacturer. When you click on a specific company it comes up with a brief history on them and how the company got started. When you click on a specific model of plane they also give you a brief history on the plane and how it originated. They also include a few color photos, both inside and outside the plane. The performance specifications that they give all include horsepower, top speed, cruising speed, stall speed, gross weight, empty weight, fuel capacity and range. They also include ground rolls both normal and over a 50ft obstacle for both takeoff and landing. The information also includes the rate of climb and the ceiling for the aircraft. The one thing that I didn’t really like about this website is that it is mostly privately flown aircraft and not commercial liners. Other than that this website has a world of information on planes from Cessna to...
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...Chastin Seeby PRAV 495 Aviation Professionalism 2/8/2015 14 CFR 91.175 The regulation 14 CFR 91.175 refers to takeoffs and landing under IFR conditions. This regulation is meant to pilots and their passengers safe during instrument flight, but this can only happen if the regulation is understood. There was a recent crash on a localizer DME approach where the aircraft descended to MDA and reported that he had the approach lights in sight. The pilot immediately after he reported that he had the approach lights in sight descended to 100 feet above touchdown zone elevation and struck a rising tree covered hill a few miles from the end of the runway. This crash was the cause of not fully understanding the regulation and all that it says. In section (c), Operation below DH/DA or MDA, subsection (1) states that: The aircraft is continuously in a position from which a decent to a landing on the intended runway can be made at a normal rate of decent using normal maneuvers… The aircraft did not follow that particular part of the regulation. It is extremely important to remember that no pilot without meeting 3 things. The first has been mentioned above, the second states that: The flight visibility cannot be less than the visibility prescribed in the standard instrument approach being used And the third is that part that most instrument rated know verbatim, and it states: (3) Except for a Category II or Category III approach where any necessary visual reference...
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