...1. Flight Controls Purpose of flight controls: The purpose of a flight control system is transfer motion/force input from a pilot to a flight control surface. In a traditional aircraft, flight control systems are broken down by axis of control: pitch, roll and yaw. Flight control systems can be either reversible or irreversible. A reversible system is a flight control system where movement applied to the control surface moves the control in the flight compartment. A simple example is shown in Figure 1. Reversible flight control systems are used on smaller aircraft where the hinge moment (surface) loads are small enough that a mechanical linkage system is adequate. Another reversible flight control system is shown in Figure 2. This is a 2D representation of a system that shows some typical components in a reversible flight control system. The systems shown in Figures 1 and 2 both contain a cable system, however, reversible systems can also be designed using pushrods and bellcranks without cables. Figure 2 Reversible Flight Control System An irreversible system is a flight control system that utilizes powered controls so that movement of the surface will not move the control in the flight compartment. An example of an irreversible flight control system is shown in Figure 3. Figure 3 shows a mechanical system connected to a hydraulic actuator. The linkage positions the servo within the actuator that controls which side of the actuator sees high-pressure fluid and...
Words: 2918 - Pages: 12
...assignment I am going to discuss the construction and clarify the operation of a rod and a cable worked manual flying control system and for every system, expresses the motivation behind their real components. I will likewise clarify the operation of a hydraulically controlled aircraft rudder system and state the motivation behind each of the real components inside the system. I will likewise specify the operation of a hydraulically controlled aircraft trailing edge fold system and state the motivation behind each of the components inside the system. Index Cover Page | Page 1 | Introduction | Page 2 | Index | Page 3 | Task 1: Explain in detail the construction and operation manually operated flight control systems. And for each of this system explain the function of each of the components involved. | Page 4-6 | Task 2: Describe in detail the operation and state the function of the components involved in a hydraulically operated rudder system. | Page 6-10 | Task 3: Describe in detail the operation and state the function of the components involved in a hydraulically operated flap system. | Page 11-14 | Conclusion | Page 15 | Reference | Page 16 | Task 1:Explain in detail the construction and operation manually operated flight control systems. And for each of this system explain the function of each of the components involved. (Rod System: Construction: (It is developed from a light compound push-pull rods, backed by sitting still connections, bell cranks...
Words: 2055 - Pages: 9
...Abstract Aircraft design begins with dreams and design requirements, and eventually proceeds to detailed drawings of every part of the aircraft being fabricated. To the outside world, the disciplines of aerodynamics and structures often seem most important – they lead to the overall shaping of the aircraft and to the design of the parts that, when fabricated and assembled, comprise the physical geometry of the aircraft. These are obviously important, but without some other things inside, the aircraft could never fly. These ‘other things’ – more properly known as ‘aircraft subsystems’ or just ‘systems’ – play a crucial role in aircraft design and operation. Systems turn an aerodynamically shaped structure into a living, breathing, flying machine. Systems include flight control, hydraulics, electrical, pneumatic, fuel, environmental control, landing gear, and the evermore- capable avionics. In the early stages of conceptual or preliminary design the systems must be initially defined, and their impacts must be incorporated into design layouts, weight analyses, and performance calculations. Anyone seeking to become a good aircraft conceptual designer must learn about all types of systems. During detail design the systems are fully defined, including system architecture, functional analysis, component design, and safety and failure analysis. This is done by highly experienced systems specialists. Introduction Flight controls have advanced considerably throughout the years...
Words: 1122 - Pages: 5
...GENERAL PRINCIPAL When aircraft are flying at high speed, the aerodynamic forces acting on the control surface are such that it is not possible to move the surfaces without some form of assistance. This assistance can be provided in the form of hydraulic or electric power or a combination of both of the systems. This system is important for the aircraft to fly. . The purpose of the powered flight control unit fitted on the aircraft is to: 1) Aircraft speed and aerodynamic loads imposed on control surface too great for the pilot to overcome using manual force only. 2) Assist the pilot to overcome this load 3) No need for normal form of aerodynamic assistance, example: balance tab and spring balance tab EXPLAINATION OF POWERED FLIGHT CONTROL UNIT (PFCU) Figure 1: Powered Flight Control Unit System Drawing Artificial Feel With purely mechanical flight control systems, the aerodynamic forces on the control surfaces are transmitted through the mechanisms and are felt directly by the pilot, allowing tactile feedback of airspeed. With hydro mechanical flight control systems, however, the load on the surfaces cannot be felt and there is a risk of overstressing the aircraft through excessive control surface movement. To overcome this problem, artificial feel systems can be used. With total hydraulic or electric power moving the control surface, it becomes difficult for the pilot to gauge the amount of control movement required for any maneuver. This is because...
Words: 3655 - Pages: 15
...component balances within a specified range. If the control surface has either too much weight ahead of or behind the hinge line, the control surface may flutter during flight. In extreme cases, flutter causes oscillations that progressively increase in amplitude, which ultimately can cause the pilot to lose control of the aircraft or could cause a catastrophic structural failure. The balance check is done with the control surface remove from the aircraft and assembled as specified in the manufacturer’s instructions. Generally all the mounting hardware and components contained within the control surface should be installed in their relative positions. Once assembled, the control surface is placed on balancing madrels within a draft-free room. The mandrels are positioned under the hinge points in a way that allows the control surface to pivot freely without dragging or binding. A balance beam or jig is then installed to determine the moment arm required to balance the control surface. The beam consists a graduated measuring scale in which weight can be moved to bring the control surface to horizontally level position or other position specified by the manufacturer. Once in the proper position, the distance that the weight is located ahead of or behind the hinge line is recorded and checked against the manufacturer’s specification. If the moment arm exceeds the manufacturer’s specification, weight is added or removed from the control surface so that the balnce beam weight falls within...
Words: 2872 - Pages: 12
...\INING FLIGHT CONTROLS MANUAL 1.27.00 SEQ 001 P 1 ~S~O~~T~R FLIGHT CREW OPERATING CONTENTS I REV 36 27.00 27.10 CONTENTS DESCRIPTION - GENERAL - ARCHITECTURE NORMAL LAW GENERAL PITCH CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 LATERAL CONTROL LOAD ALLEVIATION FUNCTION (A320 ONLY) 7 SIDESLIP TARGET RECONFIGURATION CONTROL LAWS GENERAL FLIGHT CONTROLS LAW RECONFIGURATION ALTERNATE LAW ALTERNATE LAW WITHOUT REDUCED PROTECTION DIRECT LAW ABNORMAL ATTITUDE LAWS MECHANICAL BACKUP CONTROLS AND INDICATORS PEDESTAL LATERAL CONSOLES GLARESHIELD OVERHEAD PANEL SIDESTICK INDICATIONS ON PFD ECAM F/CTL PAGE ECAM WHEEL PAGE WARNINGS AND CAUTIONS - MEMO DISPLAY FLAPS AND SLATS - DESCRIPTION - CONTROLS AND INDICATORS - WARNINGS AND CAUTIONS 1 5 8 1 1 3 4 5 8 9 11 12 14 1 5 1 6 8 1 2 3 6 6 7 7 27.20 27.30 27.40 R 27.50 27.60 ELECTRICAL SUPPLY SIMU F.P.S.3 UP for training only STD 1.3.1 AlRBL"S TR.\INING FLIGHT CONTROLS MANUAL 1.27.10 SEQ 001 P 1 ~S~O~~T~R FLIGHT CREW OPERATING DESCRIPTION I REV 34 I GENERAL I The fly-by-wire system was designed and certified to render the new generation of aircraft even more safe, cost effective, and pleasant to fly. BASIC PRINCIPLE Flight control surfaces are all : - Electrically-controlled, and - Hydraulically-activated. The stabilizer and rudder can also be mechanically-controlled. Pilots use sidesticks to fly the aircraft in pitch and roll...
Words: 6391 - Pages: 26
...BOEING 737-300/400/500 Control Cables Rigging It is necessary to test the cycle of the control cables of a system after the replacement of the cable. I. Adjust the Control Cables II. Tighten the control cable of the system to two times the usual tension. III. Adjust the cable system. (Use the table below for the number of test cycles that are necessary for a system) Cable System | Number or Test Cycles At Twice Working Tension | Aileron | 20 | Elevator | 25 | Rudder | 25 | Tools Related - General Aileron | * Dial Indicator - Accurate to 0.001 inch * Spring Force Scale, Push Type - Capable of 5 +/- 0.2 pounds * Mounting Device (to hold the dial indicator) | Rudder | * Dial Indicator - 0.001 inch accuracy (Commercially available) * Push/Pull Scale - 0 to 25 lb capacity, 1/4 lb accuracy (commercially available) * Mounting Device (to hold the dial indicator) * Loading Block, 1/8 inch thick, 3 inches by 3 inches wood or fibreglass block with pad to prevent damage to the skin | Elevator | * Dial Indicator - Accurate to 0.001 inch * Spring Force Scale, Push Type - Capable of 15.0 +/-0.2 pounds * Mounting Device (to hold the dial indicator against the elevator tab) | Special Tools and Equipment Aileron Tab Alignment Protractor * to identify the aileron tab neutral position and movement Elevator Index Plate Rigging Beam * to install or adjust the elevator index plates RIGGING PROCEDURE Aileron Special...
Words: 1460 - Pages: 6
... Abstract The required 72 month inspection on our Gulfstream G IV is coming due in a few months. There are basically two options available to complete the inspection. We can perform the inspection in-house or we can outsource it. In our situation the main advantage of performing the inspection in-house is that we will have direct control over the inspection. While the main disadvantages are that we do not have the man-power or special tools that might be needed. The main advantages of outsourcing the inspection are that the inspection can be completed much faster by technicians that perform it regularly and have all of the special equipment necessary. Taking everything into consideration I recommend that we outsource the inspection. Should Pacific Jet outsource the 72 month inspection? This is the first 72 month inspection that our 135 charter company (Pacific Jet) has coming due. Since we are a small operation with only 3 aircraft and 4 maintenance technicians performing a 72 month inspection in-house will be a huge undertaking. The main items to consider are costs, aircraft downtime, and quality control issues. We have to decide if we want to perform this inspection in-house our outsource it. The airlines have been outsourcing maintenance for decades and have accelerated this outsourcing rapidly since 2001. In 2005, some airlines outsourced as much as 62 percent of their maintenance and that number continues to grow. While they have increased...
Words: 1523 - Pages: 7
...System THEORY | UAV for Disaster Surveillance | | | Arun Bhatta | S0254398 | | Contents Executive Summary 1 Introduction 2 System Test, Evaluation and Validation 2 Validation 3 Human Factor 3 Optimization in design and operation for reliability and maintainability 4 Reliability Assessment 5 Conclusion and Recommendation 5 Bibliography 7 Executive Summary There are several UAVs which are widely used in civil and military application. The continuous use of UAV has demanded a reliable and low cost UAV system. Since its use in increment it has undoubtedly raised the question about the reliability of these systems. Thus, requiring improvement in the modeling, testing and flight control for the small UAV’s. This reports aims to provide an integrated framework with systematic, schematic procedure so that the UAV can be synthesized and validate flight controllers. This approach will help FAA and EASA certification of UAV system very rapidly. The first part of this report provides a brief introduction regarding the failure of the components. The second part discusses about the System Test and validation of the UAV. The last part of the report analyzes the human factor issues involved in the UAV. Introduction The UAV is not a new concept as it was in the situation of First World War. The roles and responsibilities that it carries has increased its utilization in the field of defense, disaster surveillance etc. Increment in utilization has accompanied...
Words: 2630 - Pages: 11
...Reg. No. :RP-phvos | Aircraft Model Maintenance Check Sheet | Content Date | Station:MNL HUB | | | Arrival Flight No. : PR 143 | Time: 08:00 | A/C Type : L1P/S | Tech Log : AAC – 004 | Departure Flight No.PR 844 | Time: 12:00 | Task :Service Check | Title: 50 Hour Check | Applicability : Cessna Turbo Skylane JT-A | | | Aircraft : Cessna Turbo Skylane JT-A | Engine : SMASR305-230E-C1 | | | Aircraft Mechanic | PROPELLER | 1. Spinner – Check general condition and attachment | | 2. Propeller Blade – Inspect for crack, dent, nicks, scratches, erosion or other damages. | | ENGINE COMPARTMENT | 1. Engine Oil – drain oil sump and oil cooler. Check metal particles or foreign materials in filter, on sump drain plug, and on engine suction screen replaced filter, and refill for recommended grade aviation oil. | | 2. Induction of Air Filter – remove and clean. Inspect for damage and remove. | | 3. Cylinder, Oil Sump, Accessory Section and Front Crankshaft Seal – inspect for crankshaft evidence oil leakage. Check bolt and nut looseness and torque as necessary. Check crankcase seal breather line for obstruction security and general condition. | | 4. Intake and Exhaust System –inspect for crack and security special check in area of heat exchange, and inspect for leakage in intake manifold | | 5. Engine Control And linkage – Check general condition...
Words: 913 - Pages: 4
...handling, rental cars and tie-downs (storage of air craft) 2. Service and Parts – Headed by Carl Green and consisting of 6 mechanics. Quality was high but department was inefficient. 3. Flight Training – Managed by Roy Douglas and consisting of 7 instructor pilots and three dispatchers, operations generated revenue through flight training and the pilot shop which sold flight supplies. 4. Avionics - Had a single employee, Leon Praxis, who repaired radios and electronic navigational equipment. 5. Aircraft Sales – AirTex had been a dealer of Piper Aircraft. AirTex became unable to finance the aircraft, fired the salespeople and closed the department. 6. Accounting – Sarah Arthur who had worked for the previous owner for 20 years managed the accounting department. Sarah effectively managed the company in the absence of the owner and formally had no accounting training. The Challenges: Frank and Ted sought out to implement new management and control systems so that AirTex could become financially stable. Ted assumed operational...
Words: 557 - Pages: 3
...------------------------------------------------- LANDING GEAR SYSTEM Prepared by: KHALID WALI MOHAMMAD 53259209393 Date: OCTOBER 12, 2011 TABLE OF CONTENT: TOPIC | PAGE | INTRODUCTION | 2 | GULFSTREAM G200 LANDING GEAR SYSTEM (GENERAL, MAIN LG) | 3 | NOSE LANDING GEAR AND EMERGENCY GEAR EXTENSION | 5 | LANDING GEAR SYSTEM CONROLS AND INDICATORS | 7 | WHEEL AND BRAKES | 8 | ANTI SKID SYSTEM | 10 | NOSE WHEEL STEERING SYSTEM | 13 | AIR BRAKES | 14 | BOEING 747 LANDING GEAR SYSTEM (GENERAL, MAIN GEAR AND DOORS) | 15 | NOSE GEAR AND DOORS | 16 | LANDING GEAR EXTENSION AND RETRACTION, WHEEL AND BRAKES AND STEERING | 18 | POSITION AND WARNING | 19 | CONCLUSION AND REFERENCES | 20 | INTRODUCTION: The undercarriage or landing gear in aviation is the structure that supports an aircraft on the ground and allows it to taxi, takeoff and land. Typically wheels are used, but skids, skis, floats or a combination of these and other elements can be deployed, depending on the surface. Landing gear usually includes wheels equipped with shock absorbers for solid ground, but some aircraft are equipped with skis for snow or floats for water, and/or skids or pontoons(helicopters). The undercarriage is a relatively heavy part of the vehicle, it can be as much as 7% of the takeoff weight, but more typically is 4-5%. Gulfstream G200 Landing Gear System General The G200 has 4 main landing gear tires and two nose landing...
Words: 3824 - Pages: 16
...Airtex Aviation Case Study AirTex Aviation 1. Did AirTex need a new control system at the time of the takeover? * “The management system that was in place was one woman who magically kept everything in her head. There was limited and almost incomprehensible formal system.” Sarah Arthur, the company’s accountant, had complete autonomy over the company’s information, and she kept this information private. * AirTex was in need of a more formalized accounting system, since accounting was a central department of the company, and profitability was a key measure to ensure the success of the company at the time of the takeover. * Also, Ted and Frank had plans to dispose of Sarah Arthur, who was acting manager upon their arrival. However, given her central role within the company for 20 years, she possessed a plethora of information, which was undocumented and she retained in her head * AirTex should make an effort to document and provide proper procedure for all major processes. It will ensure that knowledge is not lost with the departure of key personnel. However, Ted and Frank should be cautious about “rubbing people the wrong way”, especially their employees who have worked at the company for 10+ years. These individuals will be the most resistant to change and will perceive Ted and Frank as new and disruptive. * Managers were unaware of their department’s profitability. It was kept very secretive by Sarah Arthur, the accountant. As a result, managers didn’t know how big...
Words: 1119 - Pages: 5
...AirTex Aviation 1. Did AirTex need a new control system at the time of the takeover? * “The management system that was in place was one woman who magically kept everything in her head. There was limited and almost incomprehensible formal system.” Sarah Arthur, the company’s accountant, had complete autonomy over the company’s information, and she kept this information private. * AirTex was in need of a more formalized accounting system, since accounting was a central department of the company, and profitability was a key measure to ensure the success of the company at the time of the takeover. * Also, Ted and Frank had plans to dispose of Sarah Arthur, who was acting manager upon their arrival. However, given her central role within the company for 20 years, she possessed a plethora of information, which was undocumented and she retained in her head * AirTex should make an effort to document and provide proper procedure for all major processes. It will ensure that knowledge is not lost with the departure of key personnel. However, Ted and Frank should be cautious about “rubbing people the wrong way”, especially their employees who have worked at the company for 10+ years. These individuals will be the most resistant to change and will perceive Ted and Frank as new and disruptive. * Managers were unaware of their department’s profitability. It was kept very secretive by Sarah Arthur, the accountant. As a result, managers didn’t know how big their...
Words: 1109 - Pages: 5
...vehicle. Their launch method is through an automated system called autopilot or by an operator located on the ground station. Aerial drones have many functions. These ranges from military operations, in civil applications such as firefighting, inspection of power lines among others. Mostly the drones are used in places where flying a manned craft is deemed dangerous. Other names used to refer to drones include model plans, unpiloted aerial vehicle...
Words: 1103 - Pages: 5