Aircraft Structures and Systems (230811 Questions)
Category A – Turbine Aeroplane Exams ( 108 questions 135 min),
Category B1 – Turbine Aeroplane Exams ( 140 questions 175 min),
Category A – Piston Aeroplane Exams ( 72 questions 90 min),
Category B1– Piston Aeroplane Exams ( 100 questions 125 min),
Category B3 – Piston Aeroplane Exams ( 60 questions 75 min),
Category A – Helicopter Aerodynamics Exams ( 100 questions 125 min),
Category B1– Helicopter Aerodynamics Exams ( 128 questions 160 min),
Category B2 – Aircraft Aerodynamics Exams ( 128 questions 180 min),
Chapter 01: Aircraft Structures (70 pages),
Chapter 02: Aerodynamics, Aircraft Assembly, and Rigging (70 pages),
Chapter 03: Aircraft Fabric Covering ( 24 pages),
Chapter 04: Aircraft Metal Structural Repair ( 114pages),
Chapter 05: Aircraft Welding ( 38 pages),
Chapter 06: Aircraft Wood and Structural Repair ( 28 pages),
Chapter 07: Advanced Composite Material ( 58 pages),
Chapter 08: Aircraft Painting and Finishing ( 22 pages),
Chapter 09: Aircraft Electrical System ( 106 pages),
Chapter 10: Aircraft Instrument Systems (86pages),
Chapter 11: Communication and Navigation (78 pages),
Chapter 12: Hydraulic and Pneumatic Power Systems (54 pages),
Chapter 13: Aircraft Landing Gear Systems (96 pages),
Chapter 14: Aircraft Fuel System (62 pages),
Chapter 15: Ice and Rain Protection (32 pages),
Chapter 16: Cabin Environmental Control Systems (62 pages),
Chapter 17: Fire Protection Systems (22 pages),
The system of a nacelle for the most part comprises of auxiliary individuals like those of the fuselage. The long way individuals, for example, longerons and stringers, consolidate with level/vertical individuals, for example, rings, formers, and bulkheads, to give the nacelle its shape and basic honesty. A firewall is consolidated to separate the motor compartment from the remainder of the airplane. This is essentially a tempered steel or titanium bulkhead that contains a fire in the bounds of the nacelle as opposed to letting it spread all through the airframe.
Motor mounts are additionally found in the nacelle. These are the auxiliary atherings to which the motor is affixed aircraft structures.
They are generally built from chrome/molybdenum steel tubing in light airplane and manufactured chrome/nickel/ molybdenum congregations in bigger airplane.
The outside of a nacelle is secured with a skin or fitted with a cowling which can be opened to get to the motor and parts inside. Both are typically made of sheet aluminum or then again magnesium combination with treated steel or titanium composites being utilized in high-temperature territories, for example, around the
exhaust exit. Despite the material utilized, the skin is ordinarily connected to the system with bolts aircraft structures.
Cowling alludes to the separable boards covering those zones into which access must be picked up routinely, for example, the motor what’s more, its adornments. It is intended to give a smooth wind current over the nacelle and to shield the motor from harm. Cowl boards are commonly made of aluminum combination development.
Be that as it may, hardened steel is regularly utilized as the internal skin toward the back of the force segment and for cowl folds and close to cowl fold openings. It is likewise utilized for oil cooler pipes. Cowl folds are moveable pieces of the nacelle cowling that open and close to control motor temperature.
There are numerous motor cowl structures. shows an detonated perspective on the bits of cowling for an on a level plane contradicted motor on a light airplane. It is appended to the nacelle by methods for screws as well as brisk discharge clasp. A few huge responding motors are encased by “orange strip” cowlings which give superb access to parts inside the nacelle. These cowl boards are appended to the forward firewall by mounts which additionally serve as pivots for opening the cowl. The lower cowl mounts are verified to the pivot sections by fast discharge pins. The side what’s more, top boards are held open by bars and the lower board is held in the vacant situation by a spring and a link. All of the cowling boards are secured in the shut situation by overcenter steel hooks which are verified in the shut position
by spring-stacked wellbeing gets aircraft structures.
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