. j. The impact of curved Gurney flaps on the performance of a 660 kW V47 horizontal axis wind turbine (HAWT) is analyzed in this study. The flaps are retracted first if both slat and flap retraction is required. The flaps and slats move along metal tracks built into the wings. Partial – When reverse thrust is selected on at least one engine with the other at idle and one main landing gear strut is compressed. FSEU - Finance Sector Employees Union. 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. Buy, sell, trade-in or rent Astra 1125-27-50 Flap / Slat Test Panel. If you like what we're doing here, please help us by supporting our efforts!That means, before you. A bit of digging into the 7Z9363 accident investigation has brought up some interesting information regarding the DC-9-80 ("MD-80")'s flap system:. There are actually many parts to a wing. He is recently. ) Page OPR Phone E. Top Porn Videos. 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. The theoretical maximum lift of a cylinder is 4π. k. When the airplane is taking off, the flaps help to produce more lift. However Slats at the 3 index indicates maximum slat deflection ( I. So they just limit flaps operation to 20,000 maximum. a. This invention relates to hydraulic control systems and is particularly concerned with systems An object of the invention is to provide a. 407,894. 슬랫은 비행기 날개의 앞쪽에 위치하고, 플랩은 날개 뒷쪽에 위치합니다. Subchapter C. Delivery: Stock: In stock. FSEU - Flap Slats Electronics Unit. In smaller planes (GA sized stuff) there are 2 basic flap mechanisms, electric and mechanical. g. It does so by rotating. Krueger flaps deployed from the leading edge of a Boeing 747 (top left and right in photo). N & N AVIATION. 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. Hobson Ltd (now absorbed within the Hydro‐mechanical Products Group of the newly formed Company, Lucas Aerospace Ltd). 8 other FSEU meanings. 21/APR/2023Jetblue A220 performing flight from Phoenix to Boston was descending when the pilots reported they had just received a Caution Message due to a fl. Two Slat/Flap Control Units (SFCUs) control the operation of the slats and flaps. 2) If you bring the flaps back to their last known good position, you may do more damage to the plane, and affect other flight controls, like your ailerons. 1. Two main geometrical. You do need flaps to land at the slowest possible airspeed. September 2019 NASA/CR−2019-220403 This paper describes a method to investigate the benefits of a continuously moving high-lift system for departure. At ASAP Aerospace, we are committed to making parts purchasing as simple as possible. MULTI-ELEMENT AIRFOIL CONFIGURATIONS. Plain flaps hinge to the back of the wing, and they pivot down when you extend them. 5 ft. The skin is reinforced graphite/epoxy bonded to a core of Nomex honeycomb. FSEU. 1317(a). When extended they alter the airflow so the wing can produce more lift at lower speed. Choose from millions of XXX videos and sex pics that stream quickly in HD format. The controls are very sensitive at high speeds. 다만 항공업계에서 업무 편의상 (?) 슬랫을 "앞쪽 플랩"으로 언급하기도 합니다. Chapter I. Title 14 was last amended 10/27/2023. The applications range from simple force measurement solutions up to such cutting edge products as the Mars Exploration Rover Mission for. A flap is a high-lift device used to reduce the. A. TABLE OF CONTENTS 10−00−1. o. (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. 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 continuous moving system adapts the slat/flap setting. Their purpose is to increase lift during low speed operations such as takeoff, initial climb, approach and landing. 20,000 feet is an arbitrary limit. 73/Monday, April 17, 2023/Notices 23499 25. 1) Plain Flaps. in I Tolj, MV Reddy & A Syaifudin (eds), Recent Advances in Mechanical Engineering - Select Proceedings of ICOME 2021. + 3. The leading edge slat is analogous to the slotted trailing edge. Approaching Green Dot, select flap 0 and MONITOR acceleration towards 230 compared to Slat retract speed. BY 113312 - Wed Jul 21, 2021 10:52 am. The most simple flap is the plain flap. 20594 embry-riddl e aeronautical university library 3200 n. CHAPTER 10 Page. The flaps and slats move along metal tracks built into the wings. ALT. 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. 2008 alone (interestingly, all of the incidents were in Canada). The drives may be mechanically coupled to a rotational shaft, with a shaft brake arranged thereon. If the pilot does not select configuration 0 after takeoff, the flaps retract automatically at 210 knots. Re: SOP flap/slat movement on the DC-10 #22883687. On the DC-10, the flap and slat handles are mechanically linked. 1) If you bring the flaps back to their last known good position, you might eliminate the asymmetric flap situation. The drives may be mechanically coupled to a rotational shaft, with a shaft brake arranged thereon. If you put the flap/ slat lever to 0 instantly the flaps retract and the slats accordingly. from 1+F to 1 (slats only). 81-01357. BY 113312 - Wed Jul 21, 2021 10:52 am. Slats have been around for over a century. A few systems can be onboard-loaded by inserting the medium into. Our database of 85M lines of inventory includes parts like 5912847 FLAP/SLAT PSU POSITION SENSOR from multiple manufacturers EMBRAER, HAMILTON SUNSTRAND R1 . 5. c. 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. , Ulica Crvenog kriza 33, 10000 Zagreb, CroatiaOfficial Publications from the U. CONF 1 is used in-flight and is slats only. Subpart D. C. 1c. Below 20,000 feet - flaps speed limits are V speeds. Choose category you like and enjoy. Discover the growing collection of high quality Most Relevant XXX movies and clips. Aftermarket Aircraft Part. Maximum flaps are set only later in the approach when the plane has stabilized at the final approach speed. 600pix. l. Analysis was done in Ansys 14. Slats are extendable, high lift devices on the leading edge of the wings of some fixed wing aircraft. Fly with complex airliners, helicopters, business jets, fighter jets and warbirds. 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. The function of wing tip brake to hold and stop rotation of flap/slat transmission shaft when slat/flap control computer sense asymmetry, uncommanded or runways condition of flap/slat. Billing Code 4910-13-P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration [Summary Notice No. Before our approach, while manoeuvring towards the airport, or in a holding pattern. m. a. The early breed of slow commercial airliners did not require high-lift systems because their wing loadings were low and their speed ratios between cruise and low speed (takeoff and landing) were. Krueger flaps, or Krüger flaps, are lift enhancement devices that may be fitted to the leading edge of an aircraft wing. P. For slats 2 and 3 (22º) the limit is 200 kt. During take-off and climb, a typical airliner accelerates. 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. 75001. this is speculation, but if you ask why we lower gear between F2 and F3, I think Koyovis is getting quite close to the potential answer:. Each SFCU controls and monitors the slats and flaps independently of the other unit. Muscle flaps are commonly used to eradicate infection, fill defects following trauma or. 2. The procedure is based on a multiobjective genetic algorithm; two flow solvers have been coupled with the genetic algorithm: a viscous–inviscid interaction method, based on an Euler flow solver and an integral boundary layer routine,. 14. The flap disconnection detection system detects the connection failure and suppresses the flap operation to prevent further damage. Based on one type of aircraft SFCC design, the operation mode, redundancy. Slats will move from MID to EXT at approximately 14° flap. general visual inspection of the wings overview of the job operation codes: 57-00-00-210-801. 1. In this study, a multi-element aerofoil including NACA2415 aerofoil with NACA22 leading-edge slat is experimentally and computationally investigated at a transitional Reynolds number of 2×10 5. 20. Above 20,000, should be a Mach number limit, but none are given. 13, 2023 (88 FR 2286). Next. Flaps are devices on the leading (Krueger) and trailing edge which increase camber and the depth of the wing. Y. 027_004 SEP 01, 2021 Obsolete RevisionAbstract. 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°. Camber includes how convex the upper part of the wing is, as well as the concavity of the lower half. c. Pivoting the leading edge of the slat and the trailing edge of the flap downward increases. 6 in. Free porn videos sorted by categories - Fapality. As you can see below, it pushes the slat closed. 264. Slats are extendable, meaning they can extend out in front of the wings. Figure 3 shows the combined effect of using a lower takeoff flap setting and flying profile 2,I saw on the latest update for the 737 this was fixed. Seems like the turkey had some very sensitive quirks that made it a maintenance nightmare at times. A certain flap setting may help to minimize the tailstrike risk. 60 seconds. Part 25. Hello fellow pilots. The overall shape, detent system design must conform to the pilot’s control habits, have good control comfort and accessibility, the shape of the knob is smooth, easy to identify, simple, smooth and accurate operation. . Dimensions. Approaching Green Dot, select flap 0 and MONITOR acceleration towards 230 compared to Slat retract speed. Any slat angle above 18º and below or equal to 22º (positions 2 and 3) has the same limit (200 kt). Aero quArterly qtr_04 | 08 28 they use 3 to 4 percent less fuel than when flying profile 1. d. 3 at a stall. In Direct Law, deflection of the control surfaces is a linear function of deflection of the side-stick and trimming must be done manually. Heavy weight, allow the aircraft to accelerate normally towards 'S' speed which will possibly result in auto-flap retraction i. The structure of the flow field is calculated by iteratively coupling potential flow and boundary layer analysis. Airbus A380 approaching to land, with deployed droops visible between the fuselage and the inner engines. Our database of 85M lines of inventory includes parts like 285A1200-1 FLAP/SLAT ELECTRONIC UNIT from multiple manufacturers BAE SYSTEMS, BAE SYSTEMS CONTROLSIt really depends on the amount of overspeed. o. When the FLAP legend appears in cyan on the upper ECAM display what is indicated? Flaps/slats in transit. The LE slats are at the retracted position when the flap lever is in 0 detent, at the 1st EXTEND position when the flap. FSEU - Flap/Slat Electronic Unit. f. It also provides detailed. The Cessna focuses on an efficient cruise at the expense of short field performance. c. "consider a total flaps and slats fault (flap lever control sensor unit fault, for instance). To get this fixed detents, the "flap takeoff selector indicator" must be set to "STOW" position. Four-reel, six-reel, seven-reel, and other slots are pretty much nonexistent in physical. f. , Model BD-700-1A10 and BD-700-1A11 airplanes. If you are coming in hot, just set them to 35 and let them extend on their own. ATA chapters makes it easy to categorize technical information and uniformity in presenting for All manufacturers of aircraft and its components. Flat terrain at the other end of the runway means that you won't require the full go-around performance, big hill at the end of the runway and you may decide that the extra 10 or so knots on landing is worth it to preserve that go-around. S. g. "Flap" aeronautics –. In this video we look at some secondary flight controls such as FLAPS; SLATS; SPOILERS and TABS. 1) Plain Flaps. The present problem simulates the airflow around the aircraft wing with a flap and slat, using ANSYS Fluent software. When the lever is moved, the number becomes cyan indicating that the flaps/slats are in transit and when they have reached the selected position the number becomes green. Increasing the angle of attack from 8 to 16 results in much higher values of suction pressure on the upper surface, especially in the vicinity of the slat and wing leading edges, resulting in higher lift. Aircraft wings are a feat of modern engineering. The flap disconnection detection system detects the connection failure and suppresses the flap operation to prevent further damage. Combining several high lift devices on airplanes is a natural thing. A drive station includes two drives connected via drive transmissions to one or more flaps or slats of a flap/slat group. Each configuration has a reference speed: Green Dot, S speed, F speed. Results of power up test or reset: Pass: Fault clears. pdf), Text File (. The retraction sequence for the flaps and slats are; first the. Compared with the CLEAN-SC method, the L 1 / 2-DAMAS method has higher spatial resolution. d. note 1: note 2: 2. The SLAT FLAP indicator on the display shows concurrent movement. The numbers 1 and 2 are two sensors. a. Tale. from 1+F to 1 (slats only). i. So they just limit flaps operation to 20,000 maximum. . com; Aviotools d. 701. At 25 you then get Fully extended position on the Slats and TE Flap 25. This allows a steep angle of descent at slow airspeeds with but keeps the engines spooled up power. This proposed AD was prompted by a report that in case of a flap, slat, or slat-flap failure in flight, resetting the slat flap control unit (SFCU) to clear the. The Flap Slat Electronic Unit (FSEU) protects all lift devices against an uncommanded motion, to prevent worsening aerodynamic conditions by uncontrolled movement. "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 Air. In stock. The numbers 1 and 2 are two sensors. b. k. 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. The leading-edge droop flap is a device on the leading edge of aircraft wings designed to improve airflow at high angles of attack. 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. 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. A flap is a high-lift device used to reduce the stalling speed of an aircraft wing at a given weight. Avionteq offers both new and refurbished or used Astra 1125-27-50 Flap / Slat test adapter for sale or rent at most competitive price. The influence of the side cavities of. Pressing this button simulates the application of takeoff-power, thus triggering a warning if the flaps are not. Above 20,000, should be a Mach number limit, but none are given. com; Aviotools d. TRIM SYSTEM HORIZONTAL STABILIZER TRIM SYSTEMS General The variable incidence horizontal stabilizer serves for longitudinal (pitch) aircraft trim. o. 701. Le mot FAPSLAT vaut zéro au scrabble. The leading-edge droop flap is a device on the leading edge of aircraft wings designed to improve airflow at high angles of attack. The work was also to distinguish between NACA 2410 using and without flap and slat in term of lift and drag coefficient quality. This aerodynamic calculation is combined with a constrained function. Accident Prevention Vol. The slats have three positions. Part-span flap/part-span slat wing geometry. i. The Green, Blue and Yellow hydraulic systems each have their own resevoir and are supplied with a normal system pressure of 3000psi by engine driven pumps (EDPs). Rhodes 797-2973 B-1B Operational Inspections / Evaluations E-2 R. Flaps 25 or 30 or. 1+F is a configuration with slats at the default position for the flap selector at "1" but with additional flaps extended (10°). . 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. Slat and flap motion is sequenced such that slats extend first and flap retracts first when the motion command requires both surfaces to move. 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). . FlightDetent. The skew sensor detects that this sort of misalignment is starting to happen, and causes the flap drive to stop. 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. The Flap/Slat Control Lever in Fig. If the pilot does not select configuration 0 after takeoff, the flaps retract automatically at 210 knots. The slat is permanently e…Trailing edge flaps extended on the right on a typical airliner (an Airbus A310-300). The design of the detent system should be designed in combination withLeading-edge droop flap. Below 20,000 feet - flaps speed limits are V speeds. Manager Customer/Technical Support. There were 109 passengers and nine crew members on board. Subpart D. B737-800 Aircraft Maintenance Always Refer to Current and Updated Manuals while working on Aircraft. The combination re-grouping all the correct state. The construction of the control surfaces is similar to that of the stabilizers; however, the movable surfaces usually are somewhat lighter in construction. Title 14. 4 Claims. 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. slats of a window blind. You can reduce speed right away to VLS and set the lever to conf 2 and 3 at VFE next -5 kt. Meelan M. Clean vs Dirty Landings. 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. 60 Related: 067317 CLA-2:CO:R:C:G 087979 JAS District Director of Customs 110 S. On 10/17/2011 at 12:33 PM, sheepfu said: The MD-11 will auto extend flaps when the speed allows. Although flaps and slats can be controlled independently from each other in old type. DeveLopment of a FOWLER Flap System for A High Performance General Aviation Airfoil. These control surfaces used during take-off and landing are not used during cruise flight because they create induced drag. Depends, really and it’s very subjective from pilot to airline procedures… For me personally, I always retract my flaps during take off when my airspeed has reached the S speed on the PFD airspeed indicator. This page shows the parts of an airplane and their functions. e. Apparentemente uguali ai plain flap, hanno come caratteristica, quando estesi, di creare tra bordo d'uscita dell'ala e bordo d'attacco dell'ipersostentatore una fessura di forma ben determinata, che consente un passaggio di flusso ventrale, dotato di maggior energia, sul dorso dell'ipersostentatore. Slats and Flaps Control System § B1_B2 - Free download as PDF File (. Federal Register/Vol. 1, 1+F, 2, 3 and FULL refer to the level at which the flaps are currently deployed: Thanks for clear answer, it helps a lot!Study with Quizlet and memorize flashcards containing terms like When selecting the flap lever to 1 after the flaps have been at CONF 2 or higher, what setting will the flaps and slats go to?, What is the normal flap setting for a go-around?, How are the flaps and slats affected if only GREEN hydraulic system pressure available? and more. 2, and it is a compromise replace the original I-beam track [26]. Avherald reports 13 incidents (appended below) since Nov. #Ansys #Aerodynamics #CFD #Fluent #AirfoilRESOURCES:Airfoils: TIMESTAMPS:Airfoil Basics (Parameters):. Description of Relief Sought: The Boeing Company is petitioning for a temporary exemption from the affected sections of 14 CFR. We are doing this by making aviation hardware such as GT415-5300-3 immediately available to each of our customers through simple, convenient business exchanges. The usage of slats and flaps in airfoils may reduce the fuel consumption of airplanes and improve their performance as well. 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. 4. The longer B787-9 has nine settings, while the shorter 787-8 has six. The Flap/Slat Control Lever in Fig. It involves selecting and then deselecting the appropriate (or both) Alternate Flap Switches and thereby resetting the timer on the motor and. The spring-loaded slat lies flush with the wing leading edge, held in place by the force of the air acting on them. i. 1309(b)(1), 25. d. You now have one flap extended but. The design of high safety and reliability slat flap control computer (SFCC) has become the main objective of flight control development. Ommitted the quotes on "1+0" :ok: but still 1+0=1 :oh:. h. d. SPEED LIMITS MINIMUM CONTROL SPEEDS • VMCL – 108 Knots for BLY and BLZ and 113 Knots for others. j. The part on the leading edge is called a slat , while the part on the trailing edge is called a flap. When a G150 has been exposed to precipitation or high humidity followed by exposure to freezing temperature at altitude The early breed of slow commercial airliners did not require high-lift systems because their wing loadings were low and their speed ratios between cruise and low speed (takeoff and landing) were. Instead, a portion of the lower wing is rotated out in front of the main wing. Inspection after Flap & Slat Extension at more than the Flap & Slat Limiting Speed - Read online for free. 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. The S809 airfoil has been chosen in the present study since it is one of the most suitable sections for small scale wind turbine. Ipersostentatore a fessura o slotted flap. CONF 1 is used in-flight and is slats only. 1cm) and has a chord of 3. 1309(c), 25. Fix slot. We then “dirty-up” by selecting sequential flap/slat selections, as ATC reduce our speeds for traffic spacing. com. h. FSEU - Flap Slat Electronic Unit. The V1, VR, and V2 numbers all make sense to me, however, I was surprised to see the speed for retracting the flaps as being only 5 knots faster than V2, as well as the speed for retracting the slats as being only 43 knots faster than V2 . Flaps primary fail would mean the flaps are now electric but the slats are still hydraulic?Abstract and Figures. That's because as air moves over the wing, it loses energy and starts to separate from the wing. Posted October 28, 2011. The maximum C L obtained will also vary after long operational hours of aircraft when surface smoothness deteriorates and impacts the boundary layer transitions on wing. b. The free-field microphone sensitivity is 50 mV/Pa for high-precision aeroacoustic measurement. at a prescrib ed set of (x; y) co ordinates mak es this setup ideal for the surrogate metho ds describ ed next. When dealing with the LE slat problem, the QRH says to deploy. Title 14. Sometimes referred to as Handley-Page slats. : 9014. These differences are listed in Table 2. 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. The slat/flap setting is configured stepwise after the acceleration altitude is reached. Depending on speed and other factors, split flaps can edge the nose of the plane either up or down, and they became very popular in the 1930s. 5 inches (8. This will be symbolic, since nothing happens. The device can be used with any electrical actuator providing the operating current is less than 8 amps at 12 volts. When the B777 reverts to secondary mode for the Flaps and Slats is it just in the electric mode for the item that has failed? i. The airplane shown on this slide is a turbine-powered airliner which has been. Certificates. Precision Manuals Development Group. At 30 position the TE Flaps move to the primary landing position. 比较前缘襟翼和前缘缝翼：. In addition, no single failure in the mechanism prevents the flight. b. Wing tip brake (WTB) work similar to pressure off brake (POB). Flaps use Yellow & Green hydraulics. m. Not an Airbus pilot, but I am certain the explanation is same as for Boeings. You don't need flaps to land a plane. Slat and flap motion is sequenced such that slats extend first and flap retracts first when the motion command requires both surfaces to move. e. There are seven slat/flap control lever positions. pb93-910408 ntsb/aar-93/07 national \ transportation safety board washington, d. As I remember the story, there was a belief that the 727 was more stable at altitude if flaps were put in trail. 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. Note: In the case of go-around with CONF FULL selected, the L/G NOT. are retracted. For slats 2 and 3 (22º) the limit is 200 kt. We then “dirty-up” by selecting sequential flap/slat selections, as ATC reduce our speeds for traffic spacing. Subchapter C. P10-0090002: LEADING EDGE FLAP/SLAT ANNUNCIATOR. This Video contains Maintenance TIPS on Trailing Edge Fl. o. The impact of curved Gurney flaps on the performance of a 660 kW V47 horizontal axis wind turbine (HAWT) is analyzed in this study. d) All of the above are correct. This paper presents an intelligent system, based on fuzzy logic, to automate the action of a pilot in a commercial airplane in the different phases of a flight. With flaps 1 already set, your S speed (minimum maneuvering speed with flaps 1) will be at like 185 knots (aircraft weight at about 63 tonnes), which is pretty close to 200 knots. f. Guide transmissions are connected to the shaft and to respective flaps or slats of the flap/slat group. PETITION FOR EXEMPTION Docket No. Probably lots of things on the web about it. d. view historical versions. You can reduce speed right away to VLS and set the lever to conf 2 and 3 at VFE next -5 kt.