آزمون فنی و نگهداری هواپیما (Part-66)
بانک سؤالات ماژولهای Part-66 برای مجوزهای B1.1 و B2 سازمان هواپیمایی کشوری؛ با زمان و نمرهی قبولی آزمون واقعی و کارنامهای که دقیقاً نشان میدهد در کدام مبحث باید بیشتر بخوانید.
ماژولهای هر مجوز
ماژولهایی که برای هر مجوز باید بگذرانید؛ ماژولهای مشترک فقط یک بار امتحان داده میشوند.
بانک سؤالات ماژولهای فنی و نگهداری
سؤالات هر ماژول بر اساس سرفصلهای رسمی مبحثبندی شدهاند تا بتوانید دقیق تمرین کنید.
سؤالات نمونهی هر ماژول
با سطح و شکل سؤالات آشنا شوید. پاسخ و توضیح هر سؤال را با «نمایش پاسخ» ببینید.
1.Locus points plotted equidistant from a central points represent.
- Acircumference.
- Bdiameter.
- Cradius.
Answer: A
Description: Locus is the line scribed by points moving equidistant from a point - in this case it will scribe the circumference of a circle.
2.What is the Lowest Common Multiple of 5; 12; 20.
- A60.
- B120.
- C5.
Answer: A
Description: The lowest common multiple is the lowest number each number will divide into exactly. In this case the required number is 60.
3.In the following equation what is the y-intercept? 4y = 2x + 8.
- A2.
- B4.
- C8.
Answer: A
Description: First get rid of the 4 from RHS (divide all by 4) y = 0.5x + 2. Intercept with y-axis is when x = 0. So put x = 0 and what is left? (remember that 0.5 x 0 = 0).
1.Refractive index is.
- Athe speed of light in the medium divided by the speed of light in air.
- Bthe speed of light in air divided by the speed of light in the medium.
- Cthe speed of light in air multiplied by the speed of light in the medium.
Answer: C
Description: Introduction to Fiber Optics by John Crisp page 11.
2.The Steam Point of water is.
- A0 Kelvin.
- B373 Kelvin.
- C273 Kelvin.
Answer: B
Description: K = C + 273.
3.The number of radians in a semi circle are.
- Aexactly 3.
- Bπ.
- C2π.
Answer: B
Description: full circle = 2π radians, so a semicircle = π radians = 3.142.
1.What polarity do interpoles take in a DC motor?.
- AEither, provided they lay on the MNA.
- BThe same as the next main pole ahead in the direction of rotation.
- CThe same as the next main pole behind in the direction of rotation.
Answer: C
Description: The interpole must pull back the magnetic field. In a motor, the magnetic field deflects in the opposite direction to the armature.
2.The unit of energy is the.
- AJoule.
- BWatt.
- CCoulomb.
Answer: A
Description: Energy is measured in Joules.
3.In a purely resistive AC circuit, the current vector is.
- A+90° out of phase with the voltage vector.
- Bin phase with the voltage vector.
- C-90° out of phase with the voltage vector.
Answer: B
Description: Purely resistive - current and voltage must be in phase.
1.In a control synchro the stator current ceases to flow when.
- Athe CT rotor is at null.
- Bwhen power is removed.
- Cwhen the two rotors are aligned.
Answer: B
Description: In a control synchro, the stator is supplied with current at all times, whatever the transformer rotor position.
2.The voltage drop of a silicon diode is.
- A1 V.
- B0.7 V.
- C0.3 V.
Answer: B
Description: Aircraft Electricity and Electronics 5th Edition Eismin Page 111.
3.A differential synchro.
- Acan be used as either a transmitter or a receiver.
- Bcan only be used as a receiver.
- Ccan only be used as a transmitter.
Answer: A
Description: The TDX is a transmitter, the TDR is a receiver.
1.ARINC 629, aperiodic mode is used.
- Afor landing and approach operation.
- Bfor normal operation.
- Cfor database loads.
Answer: C
Description: B777 MM 23-91-00 pg 41. Periodic mode is for normal operation. Aperiodic mode is for non- normal operation and large information transfer such as database loads and operating software loads.
2.As a minimum requirement, when must a cockpit voice recorder start recording?.
- AFrom the start of the aircraft take off run.
- BAfter take off when airborne.
- COn first engine start.
Answer: C
Description: CAP 393 Section I Para 53, OR answer a by JAR OPS Para 1.700 ©.
3.In a computer memory device, which one of these has the slowest access time?.
- Afloppy disk.
- Bmagnetic tape.
- C8mm video tape.
Answer: B
Description: 8mm video tape is not (and never has been) a computer memory device.
1.What is the colour of an AN steel flared-tube fitting?.
- ABlack.
- BRed.
- CBlue.
Answer: A
Description: Steel AN fittings are black, aluminium AN fittings are blue.
2.Malleable materials are.
- Aeasy to forge.
- Beasy to cast.
- Chighly ductile.
Answer: A
Description: Malleability does not necessarily mean ductility.
3.The first step for the coaxial cable to attach to the end fitting is.
- Ause a tooling hold between the assembly and cable.
- Bthe outer covering is cut back to expose the braided outer conductors.
- Cback-off the insulator and connect with conductor.
Answer: B
Description: Aircraft Electrical Systems 3rd edition by EHJ Pallet; Chap 4 pg 87.
1.HIRF interference occurs when.
- Ain use on mid frequencies.
- Bin use on low frequencies.
- Cin use on all frequencies.
Answer: C
Description: HIRF is a problem from 10kHz - 18GHz (Civil-40 GHz Military) Understanding HIRF By Gerald L. Fuller.
2.The three electrical checks carried out on aircraft are (1) continuity (2) bonding (3) insulation. What is the order in which they are executed?.
- A2-3-1.
- B1-2-3.
- C2-1-3.
Answer: C
Description: Bonding - Continuity, Insulation, Function.
3.When using a heat shrink gun, what should the temperature of the gun be set to?.
- A100° below the heat shrink temperature.
- B15° below the heat shrink temperature.
- C100° above the heat shrink temperature.
Answer: C
Description: A trick question. The 'Heat shrink temperature' is the normal 'room' temperature of about 20- 25°C. Most heat shrink materials shrink at around 125°C.
1.Stability of an aircraft is.
- Athe tendency of the aircraft to return to its original trimmed position after having been displaced.
- Bthe tendency of the aircraft to stall at low airspeed.
- Cthe ability of the aircraft to rotate about an axis.
Answer: A
Description: Stability is the tendency for the aircraft to return to its original position after being displaced.
2.As the angle of attack decreases, what happens to the centre of pressure?
- AIt moves rearwards.
- BCentre of pressure is not affected by angle of attack decrease.
- CIt moves forward.
Answer: A
Description: The centre of pressure moves FORWARDS with an INCREASE in angle of attack. Therefore it moves REARWARDS with a DECREASE in angle of attack.
3.In the ISA the sea level pressure is taken to be.
- A14 PSI.
- B1013.2 mb.
- C1.013 mb.
Answer: B
Description: 1013.2 millibars.
1.A perforated ear drum could occur if.
- Ayou were subjected to intermittent noise above 25 kHz.
- Byou blew your nose excessively.
- Cyou were subjected to continuous noise below 8 kHz.
Answer: C
Description: Normal audible range is 20 - 20,000 Hz (CAP 715 Ch.5 Para.1.1). 8 kHz is high frequency. Anything below that can cause damage if sound level is too high.
2.What meal is most recommended after a long shift?.
- AHigh carbohydrates.
- BLow carbohydrates.
- CHigh protein.
Answer: A
Description: Carbohydrates replace blood sugar levels most quickly.
3.In a discussion, the person who is most likely to be agreed with is.
- Athe person who repeats the point most times.
- Bthe most argumentative person.
- Cthe person with the highest status.
Answer: C
Description: No reference found in CAP 715 or 716, but this is one of the problems found with pilots 'steep cockpit status gradient'.
1.Flying under A conditions is carried out by aircraft in the.
- Aproto-modified Group.
- Bvariant Group.
- Cseries aircraft group.
Answer: C
Description: A conditions is generally for the series aircraft.
2.Which of the following does not require a Noise Certificate?.
- AA helicopter under 5700 kg.
- BA small business jet aircraft.
- CA fixed wing aircraft under 2730 kg.
Answer: B
Description: Air Navigation (Noise Certification) Order 1990.
3.A Part-145 approval covers.
- Abase maintenance.
- Bthe major part of the organisation.
- Conly line maintenance.
Answer: A
Description: The part-145 organisation covers ALL of the organisation, and not only line maintenance.
1.How is a serrated rod ice detector bench tested?.
- AScrewdriver torque test.
- BBy a motor load test.
- CMotor test and go/no-go gap measurement.
Answer: A
Description: Retard rotation [of the detector] with slight thumb pressure using a torque screwdriver.' Ref: CAIPs AL/11-6.
2.A fire that can be put out by a crew member in a cargo bay is in a.
- Aclass A compensation.
- Bclass D compensation.
- Cclass B compensation.
Answer: C
Description: Transport Category Aircraft Systems Page 9-3 and JAR 25.857.
3.In a pneumatic system, the maintainer valve will be fitted in supply lines to.
- Aessential equipment.
- Ball equipment.
- Cnon-essential equipment.
Answer: C
Description: CAIPs AL/3-22. Maintainer valves work in same way as those in hydraulic systems (hence the reference). Although they protect the flow to the essential systems, they do so by being situated in the non- essential lines, and closing off if the pressure drops.
1.When OAT increases, what happens to an helicopter operating ceiling?.
- ADecrease.
- BIncrease.
- CNo effect.
Answer: A
Description: As temperature increases, density decreases and aircraft performance decreases.
2.ATA Zone 100 is.
- Aupper fuselage.
- Blower fuselage.
- CWing.
Answer: B
Description: ATA Zone 100 is lower fuselage (below floor).
3.A direct reading Bourdon gauge has a restriction in the inlet. This is to.
- Aprevent FOD ingestion.
- Bdampen sudden pressure changes.
- Callow for calibration.
Answer: B
Description: The restriction is to damp out surges in pressure.
1.During aerobatic maneuvers, what prevents fuel from spilling out of fuel tank vents?
- ABooster pump differential pressure.
- BBaffle plates in tanks.
- CFloat operated valves.
Answer: C
Description: Float operated valves allow the vent lines to vent both ways if there is no fuel on the float, but will `shut when the float is lifted by fuel.
2.To prevent compressor surge and overheating of the combustion chamber due to over fueling
- Aa barometric unit is fitted.
- Ba throttle unit is fitted.
- Can acceleration control unit is fitted.
Answer: C
Description: The acceleration unit automatically limits the rate of increase of fuel flow until sufficient air is passing through the engine.
3.The end fittings on a fuel non-return valve are normally of different sizes to.
- Aprevent incorrect installation.
- Bfacilitate bleeding the system.
- Callow a full fuel flow through the valve.
Answer: A
Description: Also known as check valves, NRV's have different end fittings and sometimes an arrow showing direction of flow embossed on the casing.
1.When a fire extinguisher is discharged the immediate action is.
- Aoperate engine to idle.
- Bclean with cold water.
- Cclean with hot water.
Answer: C
Description: When the extinguishant is introduced into the gas path hot water should be used. Jeppesen Gas Turbine Powerplants Page 13-8 refers.
2.The term Pb means.
- Aburner pressure measured at the diffuser case.
- Bburner pressure measured at the NGV.
- Cburner pressure measured at the combustion chamber.
Answer: C
Description: Burner pressure is the static pressure in the combustor can, used in some systems to regulate fuel flow.
3.What must not be used during an engine compressor wash?.
- AChlorine.
- BDesalinization solution.
- CCrushed almond.
Answer: A
Description: By elimination b is correct. Crushed almond and desalination solutions are accepted compressor wash applications.
1.In blade station numbering the stations nearest the hub are.
- Adatum.
- Bhighest.
- Clowest.
Answer: C
Description: Blade stations are measured in inches-from the hub.
2.Adjustments to a variable pitch propeller are.
- Amade in the air using the synchronizer.
- Bmade on the ground with the engine stationary.
- Cmade on the ground with the engine running.
Answer: B
Description: Governor spring pressure may be adjusted but only with the engine stationary!!.
3.In a single acting propeller, blade angle is increased by.
- Acounterweights and a feathering spring.
- BCTM.
- Coil pressure.
Answer: A
Description: Oil pressure turns the prop to fine. If the oil pressure is released by the CSU the spring and counterweights drive the prop to feather.
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