DGCA Technical General: Landing Gear, Wheels & Brakes Questions
148 exam-style Landing Gear, Wheels & Brakes questions for the DGCA Technical Generalpaper (CPL & ATPL). The first 12 are free below with answers and explanations — sign up free to practise all of them with progress tracking.
- Q1
In the following diagram the landing gear arrangements shown are: 1. 2. 3. 4.
- A Fork cantilever levered tandem
- B Cantilever dual fork tandem
- CCantilever fork half fork dual wheel
- D Half fork dual wheel cantilever fork
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Correct answer: C. Cantilever fork half fork dual wheel
The four undercarriage arrangements illustrated are, in order, cantilever, fork, half fork and dual wheel: a cantilever leg carries the wheel on a stub axle from a single rigid member, a fork straddles the wheel supporting the axle on both sides, a half fork supports the axle from one side only, and the dual-wheel unit mounts two wheels on a common axle.
- Q2
Torque links on an undercarriage come under most stress when
- A During crosswind landings
- BDuring pushback
- CMaking tight turns when taxying
- DAfter take-off
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Correct answer: C. Making tight turns when taxying
The torque links (scissor links) hold the two halves of the oleo strut in rotational alignment, so they are loaded most heavily when the wheel is being turned relative to the strut, as in tight turns while taxiing. That twisting is exactly what the links are designed to resist.
- Q3
The advantages of tubeless tyres include? 1.The tube cannot rotate within the tyre. 2.The tyre cannot rotate relative to the wheel. 3.The tyre will deflate if there is excessive creep. 4.They are more easily fitted to wheels. 5.The valves cannot be sheared off by excessive braking.
- A 1,2,3,4,5.
- B 1,2,4,5.
- C1,3,4,5.
- D 1,5.
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Correct answer: D. 1,5.
With no inner tube there is nothing to chafe or rotate inside the cover, and there is no separate tube valve that creep could shear off. However, the tyre itself can still creep on the rim, creep does not deflate a tubeless tyre, and they are not notably easier to fit.
- Q4
How is gear retraction prevented on the ground?
- A A warning sign on the lever.
- B An aural warning system.
- CIsolation of hydraulic power when on the ground.
- D Microswitches.
Show answer
Correct answer: D. Microswitches.
Microswitches operated by the compression of the landing gear legs, the weight-on-wheels or squat switches, signal that the aircraft is on the ground and prevent the retraction circuit from operating. A ground lock solenoid typically blocks the selector until the aircraft is airborne.
- Q5
Oil is used in an oleo strut to:
- Asupport the weight of the alrcraft
- Blimit the speed of extension and compression of the strut
- C limit the speed of compression of the strut
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Correct answer: B. limit the speed of extension and compression of the strut
The oil in an oleo strut is forced through restrictor orifices, damping movement in both directions so that neither compression on touchdown nor extension (recoil) happens too quickly; it is the compressed gas charge, not the oil, that actually supports the aircraft's weight.
- Q6
Thermal plugs?
- ARelease brake pressure to prevent overheating of brakes.
- BRelease excessive tyre pressures to prevent wheel/tyre explosions.
- CHeat up the hydraulic fluid to working temperature.
- D Active brake cooling fans at some pre-determined temperature.
Show answer
Correct answer: B. Release excessive tyre pressures to prevent wheel/tyre explosions.
Thermal plugs in the wheel rim melt at a set temperature when brake heat soaks into the wheel, releasing the tyre pressure in a controlled way. This prevents the overheated wheel and tyre assembly from exploding.
- Q7
390.Creep (slippage):
- A can damage the braking system
- Bcan be measured by painting marks on the tyre and wheel rim
- Cmay cause excess wear
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Correct answer: B. can be measured by painting marks on the tyre and wheel rim
Creep is the slow rotation of the tyre relative to its wheel rim; aligned paint marks applied across the tyre and rim make any relative movement immediately visible on inspection so excessive creep can be caught before it tears out the inflation valve.
- Q8
Fusible plugs react to?
- A High pressures.
- B High temperatures.
- C Low pressures.
- D Low temperatures.
Show answer
Correct answer: B. High temperatures.
Fusible plugs have a core of low melting point alloy that melts when the wheel reaches a dangerously high temperature, deflating the tyre safely. They respond purely to temperature, not to pressure.
- Q9
What does three green lights represent when the landing gear is selected down
- A The gear is down
- BThe gear is down and locked
- C The gear and doors are down and locked
- D The gear is travelling between up and down
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Correct answer: B. The gear is down and locked
Three green lights confirm the gear is down and locked, each light being triggered by the down-lock microswitch on its respective leg. A leg that is merely down but not locked will not illuminate its green light, so the greens indicate more than just gear position.
- Q10
Shimmy is a potentially damaging oscillation that occurs when?
- A Landing gear is retracted.
- BLanding gear is extended.
- C Moving at low speeds on the ground.
- D Moving at high speeds on the ground.
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Correct answer: D. Moving at high speeds on the ground.
Shimmy is a rapid, potentially damaging oscillation of a wheel about its vertical axis that develops when moving at high speed on the ground. It is countered by torque links, shimmy dampers and correct tyre pressures.
- Q11
238.The most likely cause of brake fade is
- Aoil or grease on the brake drums
- Bworn stators
- Cthe brake pads overheating
Show answer
Correct answer: C. the brake pads overheating
Brake fade occurs when the friction pads overheat: at high temperature the coefficient of friction falls sharply, so braking effectiveness fades away even though pedal pressure is maintained.
- Q12
The majority of modern transport aircraft use …….brake units?
- A Drum.
- B Multi drum.
- C Disc.
- DMulti disc.
Show answer
Correct answer: D. Multi disc.
Modern transport aircraft use multi-disc brake units, in which alternating rotor and stator discs are squeezed together by hydraulic pistons. Multiple friction surfaces provide the large braking capacity needed in a compact wheel space.
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