A leading edge slot is basically a spanwise opening in the wing. The most simple flap is the plain flap. They accomplish this by increasing both the surface area and the camber of the wing by deploying outwards and drooping downwards. 4 Claims. EP 0 922 633 A2 2 . 1317(a). Unsourced material may be challenged and removed. ) Page OPR Phone E. Use of manual thrust is recommended as power changes will result in pitch changes. Control Surfaces. o. Federal Register/Vol. 51 No. Weight. The drives may be mechanically coupled to a rotational shaft, with a shaft brake arranged thereon. 88, No. " When the airfoil's at a low angle of attack, the stagnation point is on the leading edge. f. slats of a window blind. The structure of the flow field is calculated by iteratively coupling potential flow and boundary layer analysis. 3rd International Conference on Mechanical Engineering and Materials (ICMEM 2022) Journal of Physics: Conference Series 2437 (2023) 012119 IOP Publishing98F27508498000 – HOIST – REMOVAL/INSTALLATION FLAP SLAT. Download and share free MATLAB code, including functions, models, apps, support packages and toolboxesGet ready to crank up the heat with Quick Hit Platinum: Triple Blazing 7?s. 1. 5 DATCOM method for leading edge slats and flaps. 1301(a)(1), 25. You now have one flap extended but. note 1: note 2: 2. h. Krueger flaps, or Krüger flaps, are lift enhancement devices that may be fitted to the leading edge of an aircraft wing. This aerodynamic calculation is combined with a constrained function. And without a deep familiarity with the QRH, most guys fail to appreciate the failure’s impact on landing speeds, landing distance and the go-around. . Either AIRSPEED LOW or Flap Limit speed exceedences are likely. b. 3. The flaps are retracted first if both slat and flap retraction is required. i. We are making available to our customers a comprehensive one-stop solution in ensuring the right tooling equipment reaches you on time for your planned. 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. These differences are listed in Table 2. Flight Controls - Flaps and Slats. Classical leading-edge. l. 0 1 11 . 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°. j. . The use of active, internally blown high-lift flaps causes the reduction of the stall angle of attack, because of the strong suction peak generated at the leading-edge. © AIRBUS Operations S. This video begins with a quick review of slats (aka leading edge flap), both their purpose and basic theory, and then gives an XFOIL tutorial on how to add a. Camber includes how convex the upper part of the wing is, as well as the concavity of the lower half. 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. 5 m in length for the open test section. 1309(d), 25. BRIEF DESCRIPTION OF THE DRAWINGS. It does so by rotating. PDF | On Jun 15, 2020, Yang Zhang and others published Slat Noise Control Using a Slat Gap Filler | Find, read and cite all the research you need on ResearchGate1) difference between the reference attitude and the instantaneous attitude is high. Their main purpose is to allow the plane to fly at a higher angle compared to the relative wind; slats act to shift the oncoming air over the top surface of. Subchapter C. The longer B787-9 has nine settings, while the shorter 787-8 has six. Choudhari and ; David P. Airplane condition monitoring system (ACMS/printer)Since the extra cabin width benefits all classes of passenger seating, the extra space can go towards widening the aisles, the armrests, seat-pan in between the armrests, the centre console in Premium Economy – or a combination of these. 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. 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. Douglas, to compare, had no altitude. The B777 elevators are made from. consider a total flaps and slats fault (flap lever control sensor unit fault, for instance). Based on one type of aircraft SFCC design, the operation mode, redundancy. Below 20,000 feet - flaps speed limits are V speeds. Simulation of Flow over Double-Element Airfoil and Wind Tunnel Test for use in Vertical Axis Wind Turbine. In the mean time, PNF can calculate landing distance. d. 3 – Switch ALT FLAPS switch in ARM position. 3. When playing any online casino game for the first time, it is best to start simple and then progress to more complex versions. e. Flaps may be positioned in any of the six permanent detents in a 0 to 40-degree range by movement of the Flap/Slat Handle. d) All of the above are correct. g. Study with Quizlet and memorize flashcards containing terms like Operating Modes (PSA), Primary Mode, Secondary Mode and more. 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. The HI extraction of the aircraft control surface is usually based on multivariate statistical process control (MSPC). Table 2: CS100 and CS300 Major Differences ATA ATA 22 ATA 27 DIFFERENCES Software changes. An EICAS system will display engine parameters and, depending upon manufacturer and model, may display other information such as fuel quantity, cabin pressure or landing gear and flap/slat position. 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. Below 20,000 feet - flaps speed limits are V speeds. k. Categories. When extended they alter the airflow so the wing can produce more lift at lower speed. FAPCAT. AIAA P. This of course is NOT a good procedure and is not done like that on the real aircraft. At ASAP Aerospace, we are committed to making parts purchasing as simple as possible. 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. Plain flaps hinge to the back of the wing, and they pivot down when you extend them. Subsequently, during the appoach, the aircraft suffers a flap/hydraulic problem that prevents the leading edge slats from deploying. Additionally the left main gear will not lower and so a landing on one main gear and the nose gear is required. 5. BelArgUSA. Airborne vibration monitor (AVM) 777. eicas messages - read online for free. THE DESIGN and manufacture of the complete flap and slat operating systems and of the tailplane actuator for the A300B Airbus is being undertaken by H. Normal Procedure, of the Bombardier Global 5500 AFM, Publication No. 4% flights satisfy the stabilized approach criteriaProblems with KitchenAid French Door Refrigerator Doors. The extension and retraction follow a predefined schedule. Title 14. The FSEU is responsible for receiving input signals from the flight deck. , rm. Between position 5 and 20, the slats remain at the mid range and the flap indicator gives you the TE Flap position. surveillance track data and change in ground speed as a proxy for change in airspeed, showed that 52. The centralized control system includes a controller configured to receive a device signal and transmit a control signal, a communication bus connected to the controller being configured to transport the device signal and the control signal, a plurality of devices connected to. Air supply and cabin pressure controllers (ASCPC) 777. 1. The kind of method for. 1317(a). 137 Minneapolis, Minnesota 55401 RE: Slat-Flap Control Computer (SFCC); Aircraft Wing Slat/ Flap Positioning Device; Programmed Base for Electric Control; Navigational Instrument;. The numbers 1 and 2 are two sensors. Without them, flight simply couldn’t take place. 1) Plain Flaps. Flaps use Yellow & Green hydraulics. j. Chapter I. When I open or close the left side of the refrig door, the right side door got bounced open as well. You don't need flaps to land a plane. About Press Copyright Contact us Creators Advertise Developers Terms Privacy Policy & Safety How YouTube works Test new features NFL Sunday Ticket Press Copyright. g. FSEU. m. Boeing offers Aircraft Parts, Chemicals, Tools, and more. Top Porn Videos. Aerofly FS 4 is a highly realistic Flight Simulator for beginner, intermediate and professional flight sim pilots. White Technologies, the worldwide leader in the design and manufacture of flexible shafts and related assemblies, highlights bespoke flexible shaft solutions for aerospace applications. This video covers the evolution, operation and mechanics of the flaps, slats and the FSEU. Y. The inner is the inner flap that is close to the aircraft. 0 and is aimed to obtain lift force configuration when take off. k. If the pilot does not select configuration 0 after takeoff, the flaps retract automatically at 210 knots. A flap is a high-lift device used to reduce the. A clean configuration is a configuration where landing gear, flaps, slats, spoilers etc. For slats 2 and 3 (22º) the limit is 200 kt. This allows a steep angle of descent at slow airspeeds with but keeps the engines spooled up power. Two main geometrical. It seemed odd for the doors not to stay in place. Just for my own clarification. Slats will move from MID to EXT at approximately 14° flap. Ideally, this takes place before the flap makes physical contact with any other hardware, so nothing is damaged! Edit: Video of flaps being extended & retracted on the ground. j. note 1: note 2: 2. This paper describes a method to investigate the benefits of a continuously moving high-lift system for departure. Delivery: Stock: In stock. However the principle is air passing between the wing and the flap. g. Any slat angle above 18º and below or equal to 22º (positions 2 and 3) has the same limit (200 kt). So they just limit flaps operation to 20,000 maximum. Generally, a series of related aircraft uses the same wing: Take the A318, A319, A320 and A321: All use the same wing with the same airfoil, but the much lighter A318 can get away with single-slotted flaps while the heaviest, the A321, needs two flap sections for a double-slotted flap to tease out every bit of lift in order to keep the increase in take-off and approach speeds small. Before our approach, while manoeuvring towards the airport, or in a holding pattern. The dial-a-flap selector therefor has a yellow "do not use" band between 13 and 15 degrees. For slats 1 (18º) the limit is 230 kt. The applications range from simple force measurement solutions up to such cutting edge products as the Mars Exploration Rover Mission for. G'day, Mate!Welcome to The A320 Insider!First things first. . Slats have been around for over a century. Fourth St. c. The Cessna 210 is designed to be an efficient touring aircraft and so you can see by looking at the graph that the thinner airfoil is in fact more efficient than the CH-750 all the way up to a lift coefficient of 1. § 25. Two Slat/Flap Control Units (SFCUs) control the operation of the slats and flaps. White Aerospace Flexible Shafts support multiple applications for flight such as TRAS, Flap and Slat, and Variable Bleed Valve Systems. Avionteq offers both new and refurbished or used Astra 1125-27-50 Flap / Slat test adapter for sale or rent at most competitive price. aircraft is VH RMX at Perth 1996. 1316(a), 25. 5 ft. The overall shape, detent system design must conform. j. The free-field microphone sensitivity is 50 mV/Pa for high-precision aeroacoustic measurement. d. d. RE: Timing Of Flap/Slat Deployment #11074333. When on Go Around with Flaps Full, then Flaps 4 will be selected, but it has same slat/flap deployment as in Flaps 5 lever position. , rm. The Flap/Slat Control Lever in Fig. 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. The continuous. During take-off and climb, a typical airliner accelerates. j. 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. When on final, the usual flaps selection is Flaps 3 at GS intercept, next Flaps 5 before 1000' AGL. In this video we look at some secondary flight controls such as FLAPS; SLATS; SPOILERS and TABS. Approaching Green Dot, select flap 0 and MONITOR acceleration towards 230 compared to Slat retract speed. PE-2023-10] Petition for Exemption; Summary of Petition Received; The Boeing Company Before we dive in, it should be noted that the FAA recommends that while in the traffic pattern you do not extend the flaps while banking, in the event of an asymmetrical extension it may push you further into the turn. note 1: note 2: 2. A few systems can be onboard-loaded by inserting the medium into. The procedure gives the best and the most optimum deceleration rate on the approach. Development Timeline. , . ATA chapters makes it easy to categorize technical information and uniformity in presenting for All manufacturers of aircraft and its components. 5. 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. 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. . For Flap position 1, obviously the Slats are only devices to move. Partial – When reverse thrust is selected on at least one engine with the other at idle and one main landing gear strut is compressed. I'm actually shocked it was fixed so fast. The design of the detent system should be designed in combination withLeading-edge droop flap. This happens very often that you taxi in with the flaps extended. Above 20,000, should be a Mach number limit, but none are given. Maximum flaps are set only later in the approach when the plane has stabilized at the final approach speed. 25. MID - handle in FLAP 0° or 11°. 2008 alone (interestingly, all of the incidents were in Canada). h. Some aircraft also deploy Fowler flaps during takeoff if they don’t. . S. e. note 1: note 2: 2. FLAPS. Your decision now is which one do you need more. 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. The SLAT FLAP indicator on the display shows concurrent movement. RIB8 RIB9 RIB12 RIB13 RIB17 RIB18 1 1 1 1 1 (A/C 601-700 or A/C 6, 28-262) Figure 20: SLAT ACTUATOR FITTINGS - LOCATION Falcon 2000EX EASy Rev. Any overspeed aural Warning and VLS will be for the actual flap/slat. Stalling of an aircraft is the condition when an aircraft looses sufficient lift force. d. Government Publishing Office. Airplanes are transportation devices which are designed to move people and cargo from one place to another. The combination re-grouping all the correct state. Watch video Haydon Kerk Linear Rail Systems. 1316(a), 25. At that point the forward and rear stagnation points coalesce on the bottom of the cylinder. Boundary layer control devices for hi lift application feature various devices to maintain hi velocity in boundary layer and delay separation of the airfow. American Institute of Aeronautics and Astronautics 12700 Sunrise Valley Drive, Suite 200 Reston, VA 20191-5807 703. c. The usage of slats and flaps in airfoils may reduce the fuel consumption of airplanes and improve their performance as well. 3rd International Conference on Mechanical Engineering and Materials (ICMEM 2022) Journal of Physics: Conference Series 2437 (2023) 012119 IOP PublishingB737Theory. ( en noun ) A thin, narrow strip or bar of wood or metal. b. Our database of 85M lines of inventory includes parts like 5914868 SLAT FLAP CONTROL LEVER SFCL from multiple manufacturers EMBRAER, HAMILTON SUNSTRAND RHow the flap and slat operate on a Falcon 50. 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. Each system (green, blue and yellow) also has its own backup electrical pump which can supply pressure in the event of EDP failure or. Vote. Conventional flap and slat high-lift surfaces actuation systems in a commercial aircraft consist of actuators mechanically connected via a transmission. g. Flaps are designed so that when extended they not only provide higher lift but also have higher drag. This is your journey through the development process of Infinite Flight. The flap setting has an effect on the airplane's pitch angle. 5 inches (8. This is one reason why. 4) pressure altitude is high. 2. S. 0,00 DKK. 20,000 feet is an arbitrary limit. Manufacturer. 1) If you bring the flaps back to their last known good position, you might eliminate the asymmetric flap situation. So they just limit flaps operation to 20,000 maximum. 6. Airbus A320 Flight Control Tests-Flap Slat-Flap ve Slat Testleri-aircraftdocuments. Hinson Administrator Federal Aviation AdministrationNA 95-1210 B-1B FACT BOOK Table Of Contents - OPR LIST (cont. Flaps Asymmetry (Split Flaps) or Slats Asymmetry (Split Slats) Since a single actuator controls the flaps in the T-45C, a hydraulic failure can't cause split flaps. Software can be transferred into a software-loadable LRU using various equipment. 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. Unlike slats or droop flaps, the main wing upper surface and its nose is not changed. Why does E-Jet have this extra flaps lever position? Hi. . 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. For slats Full (27º) the limit is 177 kt. Combining several high lift devices on airplanes is a natural thing. AMT 280 Laboratory Airfoil Slat & Flap Effects • One of the ways to improve the versatility and flight characteristics of an airplane is to install wing flaps and slats. This is a scanned copy of a Lockheed L1011 flap and slat troubleshooting guide. It plays a vital role in the management and control of the aircraft’s flaps and slats, which are crucial for takeoff, landing, and other flight maneuvers. 8 other FSEU meanings. The system uses electrical power to move the surfaces. 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. c = Cruise airfoil angle of attack slat = Conventional slat deployment angle Krueger = Krueger ap deployment angle 1 = Cruise airfoil free stream angle of attack L B;scaled = L B;scaled;Conventional L B;scaled;Krueger gap = Chord-normalized slat or Krueger gap distance, x gap=c overlap = Chord-normalized slat or Krueger overlap distance, x. Boeing offers Aircraft Parts, Chemicals, Tools, and more. 슬랫은 비행기 날개의 앞쪽에 위치하고, 플랩은 날개 뒷쪽에 위치합니다. Slats slow or flaps slow message will display only durning operation. 264. The D5 aeroacoustic wind tunnel at Beihang University is a small-scale, closed-circuit wind tunnel with a closed test section of 1 m × 1 m × 2. general visual inspection of the wings overview of the job operation codes: 57-00-00-210-801. Casinos try to lower your bonus by making different games release different bonus amounts. Manager Customer/Technical Support. These airframe, engine and accessory. Recently some pilots in my company have "rediscovered" an old Boeing "approved" technique for resetting a leading (or trailing) edge slat (or flap) disagree. 5,=30 6,30 a 8 promoting premature growth of the mergrng wakes and shear layers from the three elements. The Flap/Slat Electronics Unit (FSEU) is a critical component of the Boeing 737 aircraft’s flight control system. Fly with complex airliners, helicopters, business jets, fighter jets and warbirds. Both the flaps and slats are operated by a flap/slat handle located on the right side of the control pedestal. Advanced Maintenance Techniques for the 757-300 The Boeing 757-300 airplane is the first major derivative in the 757 family. The most. 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. It doesn't take that long (or that much altitude), for an MD -83 to reach an airspeed of 192 knots. Answer: The slats on the leading edge of the wing allow the airplane to take off and land at lower speeds. 1c. To get this fixed detents, the "flap takeoff selector indicator" must be set to "STOW" position. view historical versions. The crews were trying to save the flap and slat motors from the desert heat and premature burnout. To do so, a simplified modular system is designed that aims to maintain the aircraft envelope, for safety reasons, changing the position of the flaps and slats of the plane. Fly with complex airliners, helicopters, business jets, fighter jets and warbirds. 73/Monday, April 17, 2023/Notices 23499 25. Seems like the turkey had some very sensitive quirks that made it a maintenance nightmare at times. b) TE asymmetry protection. The Flap/Slat Control Lever design is a complex process with multiple rounds of iteration and gradual progress. The model spans 9. a. Above 20,000, should be a Mach number limit, but none are given. 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. Aircraft communications addressing and reporting system (ACARS) 737-700/-800/-900, 747, 757, 767. 5 has 4 evenly divided card positions and 2 gate design. 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 stabilizer travel is +2. If you put the flap/ slat lever to 0 instantly the flaps retract and the slats accordingly. When a SLATS DRIVE failure occurs during takeoff – particularly at heavy weight – crew need to carefully consider continued flap retraction as an increasing minimum manoeuvre/stick shaker can combine with the flap/slat limit speed to leave the crew with no room to manoeuvre. Part Number GT415-5001-5 is a PDU, FLAP/SLAT manufactured or catalogued by Bombardier Learjet. Any slat angle above 18º and below or equal to 22º (positions 2 and 3) has the same limit (200 kt). 比较前缘襟翼和前缘缝翼：. It is the dark green solid part. 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. The droop flap is similar to the leading-edge slat and the Krueger flap, but with. @A320 AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING CONTENT CHG CODE LAST REVISION DATE Engine and Nacelle May 01/17 FIGURE Power Plant Handling - Major Dimensions - CFM56 SeriesNational Transportation Safety Board Washington, D. 1309(c), 25. B757 Leading Edge Slat Disagree Reset. The influence of the side cavities of. c. Photos. At 25 you then get Fully extended position on the Slats and TE Flap 25. Preparing for takeoff, the handles are moved to lock into the Dial-A-Flap detent and this extends both the slats and trailing. 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. 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. Today we will talk you through parts of a wing and give a detailed explanation of some technical terms too!What's This 'A' Check, 'C' Check Stuff? Aircraft inspections defined By Jack Hessburg April 2000 Jack Hessburg has over 40 years experience in aircraft maintenance. N & N AVIATION. The system uses electrical power to move the surfaces. Sign Up. Aviapool (Aviation Tool Pooling LLC) is a global company providing around the clock assistance for the planning, supply, and sourcing of tooling equipment to the commercial aviation marketplace. Ommitted the quotes on "1+0" :ok: but still 1+0=1 :oh:. e. In the B777 rudder system, the normal pressure for the rudder operation in flight is. l. If the pilot does not select configuration 0. FSEU is defined as Flap Slat Electronic Unit (aviation) somewhat frequently. Any slat angle below or equal to 18º (position 1) has the same limit (230 kt) even for just 1º. 672(c), 25. PN: 98D27803500000, 98D27803900000. Tech Log - Embraer 170/190 Flap/Slat issues - First time poster, and long time "lurker". 20. Compare the lift of the plain airfoil with that of the airfoil with flaps: the green line produces a certain lift at. 1309(b)(1), 25. Flader, Kenmore, Frank Lakowitz, N. In some aircraft, the slats are fixed, which opens up a slot. (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. The permanent coupling to the shafts makes the entire flap system move in unison, as do the slats. A few systems can be onboard-loaded by inserting the medium into. These airframe, engine and accessory parts are generally. All 737s from the 300 onward split the systems with. MULTI-ELEMENT AIRFOIL CONFIGURATIONS. The difference between h and h f represents the total flap deflection, which is denoted as y f. The leading edge slat is the most common leading edge device in wide use. Product No. 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. Flaps are devices on the leading (Krueger) and trailing edge which increase camber and the depth of the wing. Study Flaps & Slats(14) flashcards. a.