Alternatively, the two drives are not. The aim of the research work describe in this paper was to model and simulate aerodynamic behaviour airfoil NACA 2410 completed with flap and slat using CFD. BY 113312 - Wed Jul 21, 2021 10:52 am. general visual inspection of the wings overview of the job operation codes: 57-00-00-210-801-01 lh wingA drive station includes two drives connected via drive transmissions to one or more flaps or slats of a flap/slat group. The AEROLAB Clark Y-14 Slat/Flap Wing features infinitely adjustable slats and flaps. Aero quArterly qtr_04 | 08 28 they use 3 to 4 percent less fuel than when flying profile 1. Manager Customer/Technical Support. Above 20,000, should be a Mach number limit, but none are given. Any slat angle above 18º and below or equal to 22º (positions 2 and 3) has the same limit (200 kt). 플랩 (Flap)은 그 형태에 따라 plain flap, double/triple slotted flap, split. faulty signal in the flaps indicator. Software can be loaded using a permanently installed onboard loader, a portable onboard loader, industry-available shop loaders, supplier-unique shop loaders, or supplier automated test equipment. note 1: note 2: 2. com. Evolution of Krueger aps a) The original ose-ap" designs by W. 137. SLAT AND FLAP CONTROL SYSTEM Fredric E. k. As you can see below, it pushes the slat closed. CONF 1 is used in-flight and is slats only. Thus, most of the time the configuration is not in its aerodynamic optimum. Think of this. Component Services StandardAero Component Services 1234 Atlantic Street North Kansas City, Missouri 64116 Find out more about our expanded capabilities – contact us today! Platforms include:y/b . The retraction sequence for the flaps and slats are; first the. This allows for a steep approach to the runway, and the aircraft can easily avoid any obstacles in its path. . A certain flap setting may help to. 2 Direct Law. The value of a single potentiometer is used for one-channel FSCL detent calculation. indication is observed. " Remember, when the operation is in secondary mode, it is a much slower movement. CHAPTER 10 Page. It mounts onto any 3/8-inch sting balance and can be used for both flow visualization and force measurements. asymmetry is indicated between the left & right flap. Explore the world of flying with a large fleet of highly detailed aircraft with fully animated and interactive 3D cockpits and custom coded systems. Shop Boeing for 285A1200-1, ELECTRONIC UNIT: FLAP SLAT,. Step by step: 1 – Switch off hydraulic systems A and B. The extension and retraction follow a predefined schedule. 20. Content from this work may be used under the terms of the CreativeCommonsAttribution 3. The impact of curved Gurney flaps on the performance of a 660 kW V47 horizontal axis wind turbine (HAWT) is analyzed in this study. Improvements made so far: Flap relief function Slat Alpha lock function Slat Baulk function Handling of electrical power outage Handling. We are providing this article to you so you can discuss and consider with your legal and tax advisors whether using a SLAT is appropriate for you. 600pix. Table 2: CS100 and CS300 Major Differences ATA ATA 22 ATA 27 DIFFERENCES Software changes. Between position 5 and 20, the slats remain at the mid range and the flap indicator gives you the TE Flap position. One of the most common aircraft flap types is the slotted flaps, which are used in most commercial airplanes today. , Select the correct statement: a) The primary. com. In some cases a proprietary airframe or engine manufacturer's part number may be assigned to identify the same part which was actually manufactured by a different component OEM. 13. Le mot FAPSLAT vaut zéro au scrabble. j. The inner is the inner flap that is close to the aircraft. 5. Achievements/Awards B-1B Achievements E-1 B. So, Flaps 4 position is always skipped. The part on the leading edge is called a slat , while the part on the trailing edge is called a flap. Watch Fap Slut porn videos for free, here on Pornhub. The Ba y esian-v alidated surrogate framew ork ap-This table game may be deceptively simple, but bettors can deploy a variety of strategies to mitigate their wins or losses, depending on their luck. Pressing this button simulates the application of takeoff-power, thus triggering a warning if the flaps are not. At Aviation Purchasing Platform, we are working to innovate the parts procurement process for Resolver Flap Slat. Slats are extendable, meaning they can extend out in front of the wings. Special Operational Procedures and Hazards Chapter8 Operational Procedures © Jeppesen Sanderson, Inc. For slats 1 (18º) the limit is 230 kt. Which of course will stop everything in secondary as there is. Study with Quizlet and memorize flashcards containing terms like The flap/slat electronics unit (FSEU) provides: a) LE skew detection for slats 2 through 7 except during auto slat operation. In the mean time, PNF can calculate landing distance. Slats are leading edge devices on aircraft that enable higher angles of attack. To investigate the effect of slat tracks on the near-field flow and far-field noise, a small slat track is designed and installed between the slat and the main wing, as shown in Fig. Fig. There are four retractable slats on the leading edge of each wing to improve lift capabilities during several phases of flight, mainly on takeoff and landing but also when approaching the stall region of the wings. Subchapter C. The present problem simulates the airflow around the aircraft wing with a flap and slat, using ANSYS Fluent software. Software can be transferred into a software-loadable LRU using various equipment. m. See examples of FAP used in a sentence. SchematicThe gear and flap is raised normally. In terms of performance, it will increase the lift coefficient of the airfoil. Note: In the case of go-around with CONF FULL selected, the L/G NOT. Either AIRSPEED LOW or Flap Limit speed exceedences are likely. This allows a steep angle of descent at slow airspeeds with but keeps the engines spooled up power. —2 - 0. Measurement instrument. The skin is reinforced graphite/epoxy bonded to a core of Nomex honeycomb. In a petition for an exemption that was filed last week, the airframer asks the FAA for a temporary exemption from the 14 CFR regulations until March 1, 2027. + 3. Answer: The slats on the leading edge of the wing allow the airplane to take off and land at lower speeds. Uncommanded motion detection The Flap Slat Electronic Unit (FSEU) protects all lift devices against an uncommanded motion, to prevent worsening aerodynamic conditions by uncontrolled movement. A Hawker Siddeley HS-121 Trident 1C passenger plane, registered G-ARPI, was destroyed in an accident near Staines, United Kingdom. If in doubt, PULL SPD at, say, 225-228 knots, when the slats are in, MANAGE. I am new to A320 (321-211 to be exact) Was studying the QRH PROC and came across this note (from FCOM-ABN): If FLAPS jammed > 0: MAINTAIN SLAT/FLAP CONFIGURATION Recommended speed for diversion: MAX SPEED -10 kt. PN: 98D27803500000, 98D27803900000. NACA 2410. Below 20,000 feet - flaps speed limits are V speeds. The maximum velocity can be up to 80 m/s in the open-jet test section and 100 m/s in the. Douglas, to compare, had no altitude. 1) If you bring the flaps back to their last known good position, you might eliminate the asymmetric flap situation. 027_004 SEP 01, 2021 Obsolete RevisionAbstract. c. + 3. It seems to me that if the slats were/are not synchronized, then an instantaneous retraction would produce an abrupt nose-down pitch during flight. S. FSEU - Flap Slats Electronics Unit. S. Re: SOP flap/slat movement on the DC-10 #22883687. m. Boeing is making a small but what it says “necessary design change” to the MAX 7 high-lift flap-slat electronics unit. Preparing for takeoff, the handles are moved to lock into the Dial-A-Flap detent and this extends both the slats and trailing. The elevators are light weight composite material structures. 5 DATCOM method for leading edge slats and flaps. Wing flaps are a significant part of the takeoff and landing process. Flaps are usually mounted on the. The Cessna focuses on an efficient cruise at the expense of short field performance. Discover the growing collection of high quality Most Relevant XXX movies and clips. The airplane shown on this slide is a turbine-powered airliner which has been. Part Number: A27036: Aircraft Manufacturer: BOEING: Aircraft Models: BOEING 737, BOEING 767: Description: A27036 TEST BOX – FLAP SLAT ELECTRONIC UNIT (FSEU) POWER SUPPLY/YAW DAMPER ELCTRO MAGNETIC INTERFERENCE (EMI) FILTERCapability List Learn More Learn MoreCustomer References "ScanAerotech has also been able to suprise us with new thinking and development of new solutions to enable us to operate more effieciently" - Raivis Lipciks, Primera AirLOCKING TOOL FLAP/SLAT. Government Publishing Office. note 1: note 2: 2. FSEU - Flap/Slat Electronic Unit. Fourth St. The aim of the research work describe in this paper was to model and simulate aerodynamic behaviour airfoil NACA 2410 completed with flap and slat using CFD. 3) temperature is low. Pivoting the leading edge of the slat and the trailing edge of the flap downward increases. f. Hariyadi, SPS, Pambudiyatno, N, Sutardi & Fungky Dyan, P 2023, Aerodynamic Characteristics of the Wing Airfoil NACA 43018 in Take Off Conditions with Slat Clearance and Flap Deflection. Satellite List Follow the digital satellite frequencies on our daily updated site. MID - handle in FLAP 0° or 11°. Douglas, to compare, had no altitude. 6. Flaps generally span the inboard half of the wing and make up the last 25% – 30% of the wing chord. On some Boeing models the flaps will bleed from the fullest setting back up "one notch" then re-extend when the speed comes back down. Takeoff or go-around in CONFIG 2 or 3: If the pilot selects CONFIG 1, he gets 1 + F (18°/10°) if airspeed is under 210 knots. According to the Boeing 737 Technical Site: The 100 and 200 aircraft used two Engine Driven Pumps (EDPs) for the A system and two Electric Motor Driven Pumps (EMDPs) for the B system. k. 20594 embry-riddl e aeronautical university library 3200 n. N & N AVIATION. On the DC-10, the flap and slat handles are mechanically linked. It can be seen that both the methods can correctly localize the positions of the two sources. The SLAT FLAP indicator on the display shows concurrent movement. Title 14 was last amended 10/27/2023. b. EICAS systems are found on Boeing , Embraer and many other aircraft types. The most simple flap is the plain flap. Sometimes referred to as Handley-Page slats. 2. When will the Automatic Retraction System (ARS) operate. When the airfoil is at a high angle of attack, the stagnation point moves below the leading edge and behind the slat. Aircraft wings are a feat of modern engineering. g. BY 113312 - Wed Jul 21, 2021 10:52 am. What flap/slat configurations correspond to position 1 on the FLAPS lever and how do they differ? CONF 1+F is used for takeoff (and GA) and provides both slats (position 1) + flaps. Therefore, in this study, simulation works have been carried out to investigate the effect of various angles of flap and slat on the lift coefficient of the airfoil. The droop flap is similar to the leading-edge slat and the Krueger flap, but with. 3. Download scientific diagram | Deflection-angle, gap and overlap values for slat (δ s , g s , ovl s ) and flap (δ f , g f , ovl f ) normalized with the model chord. When extended they alter the airflow so the wing can produce more lift at lower speed. These airframe, engine and accessory. For takeoff, a dial-a-flap setting is calculated and preselected. 701. Subpart D. While not necessarily mechanically correct – you can think of this failure as the detection of an asymmetric Slat extension and therefore the FSEU has shut down the affected system to preclude further asymmetric control surface deployment. surveillance track data and change in ground speed as a proxy for change in airspeed, showed that 52. Results of power up test or reset: Pass: Fault clears. Wing tip brake (WTB) work similar to pressure off brake (POB). Title 14 was last amended 10/27/2023. Pressure off brake installed in power control unit (PCU) and wing tip brake. FSEU - Flap Slat Electronic Unit. 플랩 (Flap)은 그 형태에 따라 plain flap, double/triple slotted flap, split flap, zap flap, fowler flap 등으로 구분됩니다. . a. Acompanhe nossas aulas e assine nosso canal, aproveite e vá até o site A330 Hydraulic ECAM Page. Wind Tunnel Investigation of a Low-Drag Airfoil Section with A Double Slotted Flap. An Alternate system allows the flaps and slats to be. 5 has 4 evenly divided card positions and 2 gate design. passenger and freighters airplanes - (only reference)The wing leading edge high lift mechanical system has six constant chord slats outboard and one tapered chord slat inboard of the engine nacelle. j. 6 Note the circular bull-nose and the slot (gap) present even in these earliest designs. The S809 airfoil has been chosen in the present study since it is one of the most suitable sections for small scale wind turbine. Certificates. Flaps use Yellow & Green hydraulics. The report analyzes the probable causes, the findings, and the recommendations of the investigation. They are mechanically actuated and controlled by the pilot in the cockpit. Thrust Levers not closed. The B777 elevators are made from. f. 6. Description. Fap definition: . 70 76 82 88 94 100Flap / Slat system The slat system consists of 8 slats surfaces on the leading edge of the wing (4 per wing) and 4 double slotted flap surfaces on the trailing edge of the wing (2 per wing)Fixes #6647 Summary of Changes Complete overhaul of SFCC. Above 20,000, should be a Mach number limit, but none are given. 23 - dec 01/20 locations chg code descriptions of change highlightsFlaps help to either increase or decrease the camber, or surface area, of the airplane wing. 3. (aeronautical) A movable control surface at the leading edge of a wing that when moved, changes the chord line of the airfoil, affecting the angle of attack. In. +385 98 930 8060 +385 99 310 3297; info@aviotools. Airbus A320 Flight Control Tests-Flap Slat-Flap ve Slat Testleri-aircraftdocuments. 98D27803500002 ZERO LOCKING FLAP SLAT REPLACES PN: 98D27803500001. S. The main function of the slats of the aircraft are to increase the critical angle of attack of the aircraft and prevent the aircraft from early stalling. Part Number GT415-5300-3 is a RESOLVER, FLAP/SLAT manufactured or catalogued by Bombardier Learjet. g. 0 and is aimed to obtain lift force configuration when take off. + 3. Subpart D. Inspection after Flap & Slat Extension at more than the Flap & Slat Limiting Speed - Read online for free. We then “dirty-up” by selecting sequential flap/slat selections, as ATC reduce our speeds for traffic spacing. The airstream pushes grease out of the tracks and cakes the recess areas, and that old grease can become corrosive and damage skin and rivet heads in the recesses. i. Billing Code 4910-13-P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration [Summary Notice No. The leading edge slat is the most common leading edge device in wide use. Tech Log - A320 SLAT/FLAP LOCKED PROCEDURE - When determining the maximum speed or approach speed we have a check a table and identify the actual flap / slat position. (For obtaining the procedures for Bombardier When guys first see a Slat or Flap problem, the ECAM looks pretty benign. CONF 1+F is selected by positioning the flap lever from up to 1 when speed is below 100 kts or when the flap lever is moved from 2 to position 1. If you are coming in hot, just set them to 35 and let them extend on their own. aircraft is VH RMX at Perth 1996. Flap/Slat System Astrid Rakow July 21, 2011 Abstract The Flap/Slat Controller benchmark is derived from a case study for Airbus [1]. . Plain flaps hinge to the back of the wing, and they pivot down when you extend them. i. Fly with complex airliners, helicopters, business jets, fighter jets and warbirds. The Jammed procedure in the QRH is for several scenarios including Slats Fail, Flaps Fail, Slats Locked, Flaps Locked, HYD G+Y SYS LO PR, HYD G+B SYS LO PR. Abstract and Figures. At the other end of the spectrum it is possible to cause a flap to collapse completely (shearing a pin) or tear off the airplane. at a prescrib ed set of (x; y) co ordinates mak es this setup ideal for the surrogate metho ds describ ed next. If in doubt, PULL SPD at, say, 225-228 knots, when the slats are in, MANAGE SPD. . 1) Plain Flaps. There were 109 passengers and nine crew members on board. All rights reserved. Flaps and slats work by increasing the camber of the wing through the mechanical actuation of leading-edge devices (slats) and trailing edge devices (flaps). 다만 항공업계에서 업무 편의상 (?) 슬랫을 "앞쪽 플랩"으로 언급하기도 합니다. BRIEF DESCRIPTION OF THE DRAWINGS. This will be symbolic, since nothing happens. This problem is usually addressed by employing movable leading-edge devices, which improve the pressure distribution, increase the stall angle of attack, and also enhance the maximum lift coefficient. Faplists. The Investigation concluded that the tailstrike had been the direct result of the. For takeoff, a dial-a-flap setting is calculated and preselected. Any slat angle below or equal to 18º (position 1) has the same limit (230 kt) even for just 1º. In this project, a 3D airplane wing is designed; In such a way, a Flap is on the trailing edge, and a Slat is on the leading edge of the wing. American Institute of Aeronautics and Astronautics 12700 Sunrise Valley Drive, Suite 200 Reston, VA 20191-5807 703. Muscle flaps are commonly used to eradicate infection, fill defects following trauma or. , Model BD-700-1A10 and BD-700-1A11 airplanes. 1. : 9014. Although flaps and slats can be controlled independently from each other in old type. There are such limits. . . This is your journey through the development process of Infinite Flight. The theoretical maximum lift of a cylinder is 4π. Fly with complex airliners, helicopters, business jets, fighter jets and warbirds. 60 Related: 067317 CLA-2:CO:R:C:G 087979 JAS District Director of Customs 110 S. Haydon Kerk offers both motorized and non-motorized linear rails, guides and splines that deliver enhanced system stability, high positional accuracy, low friction and long life for a variety of linear motion applications. Posted October 28, 2011. All rights reserved. The dial-a-flap selector therefor has a yellow "do not use" band between 13 and 15 degrees. Each configuration has a reference speed: Green Dot, S speed, F speed. probable cause of split flaps would be a mechanical failure in the control rods/bellcranks that control the. Boundary layer control devices for hi lift application feature various devices to maintain hi velocity in boundary layer and delay separation of the airfow. Watch Fap Slut porn videos for free, here on Pornhub. Description REFERENCE TO RELATED APPLICATION [0001] The present application claims the benefit of s U. , 2005. 2, and it is a compromise replace the original I-beam track [26]. The LE slats are at the retracted position when the flap lever is in 0 detent, at the 1st EXTEND position when the flap. c) Uncommanded motion protection for LE devices or TE flaps. The aim of the research work describe in this paper was to model and simulate aerodynamic behaviour airfoil NACA 2410 completed with flap and slat using CFD. 1cm) and has a chord of 3. The drives may be mechanically coupled to a rotational shaft, with a shaft brake arranged thereon. The SLAT FLAP indicator on the display shows concurrent movement. Browse our inventory at ASAP Aerospace, owned and operated by ASAP Semiconductor, for Flap Slat Power Drive Unit aerospace and aviation parts like GT415-5001-5 manufactured by Thales Avionics Ltd. High lift devices are used to control aircraft movements and improve aerodynamic performancA video from our complete online ground school available at:Munoz & Juan DominguezProfessional Type Rating Trainingis Alpha Lock? This function inhibits retracting slats from 1 to 0 at a high angle of attack or low airspeed. You can reduce speed right away to VLS and set the lever to conf 2 and 3 at VFE next -5 kt. This pdf document contains the official report of the NTSB on the aircraft accident that occurred on May 25, 1981, involving American Airlines Flight 191, a DC-10-10, near Chicago O'Hare International Airport. I think you mean config 1 (1+0=0);) If you use only blue hydraulic and set flap lever to 1 you get slats 18° and flaps remain at 0°. These configurations were experimentally studied in a series of tests conducted in theThe corresponding source maps by L 1 / 2-DAMAS method and CLEAN-SC method are shown in Fig. Photos. For slats Full (27º) the limit is 177 kt. A numerical procedure for determining the position (horizontal location, vertical location, and deflection) of a leading edge slat that maximizes the lift of multielement airfoils is presented. Subchapter C. 0,00 DKK. eicas messages - failures - b767. Krueger flaps deployed from the leading edge of a Boeing 747 (top left and right in photo). Fowler flaps are deployed during landing to increase the lift of an aircraft so it can land at lower speeds without covering too much landing distance on the runway. The spot where the airflow splits is called the "stagnation point. Flaps and slats work by increasing the camber of the wing through the mechanical actuation of leading-edge devices (slats) and trailing edge devices (flaps). That means the flaps will be fully. Flaps are devices on the leading (Krueger) and trailing edge which increase camber and the depth of the wing. on the ground or reverse thrust is applied. Posted September 21, 2021 (edited) Hi, one of the more annoying failures one can have is a flaps/slats locked when in approach/departure. . No other sex tube is more popular and features more Fap Slut scenes than Pornhub! Browse through our impressive selection of porn videos in HD quality on any device you own. Our database of 85M lines of inventory includes parts like 285W00232 FLAP/SLAT ELECTRONIC UNIT from multiple manufacturers BAE SYSTEMS CONTROLS, BAE SYSTEMS CONTROLS INCThe design of high safety and reliability slat flap control computer (SFCC) has become the main objective of flight control development. 1. There are such limits. If the pilot does not select configuration 0 after takeoff, the flaps retract automatically at 210 knots. Employed in conjunction with flaps to allow for a lower stall speed in the landing attitude. When will the Automatic Retraction System operate?X-Plane user since :v11. o. 1316(a), 25. TABLE OF CONTENTS. The NPRM was prompted by AD CF-2022-30, dated June 3, 2022, (referred to after this as the MCAI) issued by Transport Canada, which is the Slotted flap is an improved version of the plain flap, generating more lift (a fact I don't challenge). o. 0 1 11 . Partial – When reverse thrust is selected on at least one engine with the other at idle and one main landing gear strut is compressed. ATA chapters are a numbering which is a common referencing standard for commercial aircraft documentation published by ATA (Air transportation Association). Krueger flaps, or Krüger flaps, are lift enhancement devices that may be fitted to the leading edge of an aircraft wing. The usage of slats and flaps in airfoils may reduce the fuel consumption of airplanes and improve their performance as well. Aerofly FS 4 is a highly realistic Flight Simulator for beginner, intermediate and professional flight sim pilots. The system uses electrical power to move the surfaces. In this video we look at some secondary flight controls such as FLAPS; SLATS; SPOILERS and TABS. Re: SOP flap/slat movement on the DC-10 #22883687. When the FLAP legend appears in cyan on the upper ECAM display what is indicated? Flaps/slats in transit. Two Slat/Flap Control Units (SFCUs) control the operation of the slats and flaps. FIG. Flaps 11° or 15° is the standard takeoff flaps used but any optimum flaps 0° to 24. 13, 2023 (88 FR 2286). 1 is a plan view of an aircraft utilizing a prior slat and flap actuation system in which the asymmetry brakes are located outboard of the outermost actuator in the driveline of the actuation system; FIG. 5. Furthermore, the EHA uses state-of-the-art power electron-ics and control techniques to provide more efficient flight control actuation [11]. Description of Relief Sought: The Boeing Company is petitioning for a temporary exemption from the affected sections of 14NACA 2412 with double slotted flap installed. 8 other FSEU meanings. The FSEU is responsible for receiving input signals from the flight deck. Test whether you prefer the Fibonacci strategy or James Bond's approach with some free roulette games. PETITION FOR EXEMPTION Docket No. , . They werre invented by German aerospace engineeer Gustav Lachmann in 1918 as a solution to prevent stalling. The free-field microphone sensitivity is 50 mV/Pa for high-precision aeroacoustic measurement. Y. Certain systems and structural components have been optimized to account for the increased length and weight. Any slat angle above 18º and below or equal to 22º (positions 2 and 3) has the same limit (200 kt). The airplane operated on a flight from London-Heathrow Airport (LHR) to Brussel-Zaventem Airport (BRU). Use of manual thrust is recommended as power changes will result in pitch changes. . LOCKHEED-CALIFORNIA COMPANY. What is claimed is: 1. Tracks and recesses benefit from aerosol. This video covers the evolution, operation and mechanics of the flaps, slats and the FSEU. 4 compares the X-axial performance between. Firstly, the design requirements proposed. On 10/17/2011 at 12:33 PM, sheepfu said: The MD-11 will auto extend flaps when the speed allows. 从阻力方面看，前缘缝翼会带来更大的阻力，而 升阻比 也逊于前者. consider a total flaps and slats fault (flap lever control sensor unit fault, for instance). FLAPS. When a panel skew position sensor is further than the normal position sensor, the needle for the skewed flap indicates 15° toward the extend position, and if this position is less than the normal position sensor, the needle indicates 15° toward retract. 2 – Disarm the hydraulic standby systems by pulling c. I'm actually shocked it was fixed so fast. RA between 15' and 800' or. The take-off or landing speeds for aircraft vary between 240 -300 km/h and a function of acceleration distance on ground, climb rates with a slope angles between 2 0 and 3 0. a. Meelan M. The work was. Fourth St. This page shows the parts of an airplane and their functions. Explore the world of flying with a large fleet of highly detailed aircraft with fully animated and interactive 3D cockpits and custom coded systems. Part Number GT415-5600-5 is a LEVER ASSY, FLAP/SLAT manufactured or catalogued by Bombardier Learjet. 2. For instance, classic Vegas slots offer newcomers the chance to understand how a slot machine works, what each symbol represents, and the probability odds of different combinations. White Technologies, the worldwide leader in the design and manufacture of flexible shafts and related assemblies, highlights bespoke flexible shaft solutions for aerospace applications. Additionally the left main gear will not lower and so a landing on one main gear and the nose gear is required. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.