Welcome Back

Sign in to your PART66Online account

or use email
Forgot password?

Don't have an account? Register here

11. Aeroplane aerodynamics, structures and systems - Q&A

74 questions found

Module 11. Aeroplane aerodynamics, structures and systems

Emergency floor lighting system is inoperative, then

  • the aircraft is allowed to fly empty to a main base.
  • the aircraft is not allowed to fly until repaired.
  • the aircraft is allowed to fly in daylight conditions only.
avtaar23 asking:

any evidence?

Module 11. Aeroplane aerodynamics, structures and systems

How are passenger reading lights normally tested?

  • By using a READ LIGHT TEST switch on the cabin attendant panel.
  • Each one is switched on individually at passenger panel.
  • By using a READ LIGHT TEST switch at any passenger panel.
dyane_july86 asking:

Y? Based on aircraft I work . Its answer should be B

Module 11. Aeroplane aerodynamics, structures and systems

When air is pressurized, the oxygen content

  • increases.
  • remains constant.
  • decreases.
chesters1234 asking:

why?

Module 11. Aeroplane aerodynamics, structures and systems

If an accumulator loses air pressure there will be

  • rapid fluctuations of instruments.
  • rapid depressurisation of system.
  • pump cavitation.
paulhb1972 asking:

Accumulators in instruments?? pfcu's maybe?

Module 11. Aeroplane aerodynamics, structures and systems

Buckling in a semi-monocoque structure is prevented by

  • bulkheads.
  • stringers.
  • longerons.
paulhb1972 asking:

Are all 3 not correct?

Module 11. Aeroplane aerodynamics, structures and systems

Before checking the SG of a battery recently removed from an aircraft

  • take the temperature of the electrolyte.
  • carry out a capacity test.
  • allow to stabilise for one hour.
paulhb1972 asking:

I have had this question elsewhere and the answer was to let it stand for an hour!?

Module 11. Aeroplane aerodynamics, structures and systems

What colour is the strobe light on the PORT wing?

  • White.
  • Green.
  • Red.
hongyanhong asking:

why not red?

Module 11. Aeroplane aerodynamics, structures and systems

As fuel level increases, system capacitance

  • no change.
  • decreases.
  • increases.
haridass asking:

i dun gt this point...cn u explain briefly?

Module 11. Aeroplane aerodynamics, structures and systems

A cockpit check on the engine firewire system is a

  • continuity check.
  • calibration check.
  • function check.
subh1985ch asking:

is this answer is correct bcoz i have study somewhere that firewire check is a check for continuity of the loop..........please can anyone help me regarding it........
thanks guys.....

Module 11. Aeroplane aerodynamics, structures and systems

Inwards relief valves usually open at a negative differential pressure not exceeding

  • 0.16 p.s.i.
  • 1.2 p.s.i.
  • 0.5 p.s.i.
simontay asking:

I thought it should be 0.5 psi

Module 11. Aeroplane aerodynamics, structures and systems

111.2 MHz is

  • VHF.
  • VOR.
  • ILS.
mladjo20 asking:

VOR frequency 112-118 MHz
ILS frequency 108-112 MHz(all odd frequencies).
so,the only correct answer must be VHF(108-136 MHz).

Module 11. Aeroplane aerodynamics, structures and systems

Upper surface wing skin is usually made from

  • 2024.
  • 7075.
  • 5056.
soonhchong asking:

Jeppesen A&P Technician Airframe Textbook 2-8.

commonly used in the construction of skins and rivets are 2017 and 2024.

Module 11. Aeroplane aerodynamics, structures and systems

The equalizing coils on voltage regulators will

  • have current passing through them from the higher loaded generator to the lower.
  • have current passing through them only when the generators are not paralleled.
  • be connected to each other when the generators are paralleled.
soonhchong asking:

Aircraft Electricity and Electronics Thomas Eismin 5th Edition page 200.

Module 11. Aeroplane aerodynamics, structures and systems

In typical vapour cycle system, the sub-cooler

  • cools the vapour further to prevent slugging.
  • is a heat exchanger to superheat the vapour.
  • delivers extra cooling effect when the aircraft is on ground.
soonhchong asking:

option 1 is the most correct answer?!

http://navyaviation.tpub.com/14020/css/14020_106.htm

Module 11. Aeroplane aerodynamics, structures and systems

In a Turn and Slip indicator, the effect of increasing the rotor speed would be

  • it would have no effect.
  • it would under read.
  • it would over read.
harbhla asking:

MAY BE IT IS WRONG SINCE MORE SPEED MEANS MORE FORCE IS REQUIRED TO MOVE SO UNDERREAD

Module 11. Aeroplane aerodynamics, structures and systems

Laser gyros have

  • no rotating parts.
  • moving parts.
  • a spinning rotor.
harbhla asking:

may be it is wrong ,since nothing moves except beam of light which is weightless

Module 11. Aeroplane aerodynamics, structures and systems

On large aircraft, braked wheel assemblies are normally inflated with

  • nitrogen.
  • nitrogen and not more than 5% of air.
  • an argon and CO2 mixture.
soonhchong asking:

refer to JAR 25.733 Tyres (e)

tyres mounted on brakedwheels must be inflated with dry nitrogen or other gases shown to be inert so that the gas mixture inthe tyre does not contain oxygen in excess of 5% by volume..
nitrogen and not more than 5% of air, will be more correct?

Module 11. Aeroplane aerodynamics, structures and systems

The life of an aircraft oxygen cylinder is

  • 4 years.
  • 10 years.
  • 2 years.
soonhchong asking:

As i know the oxygen cylinder are removed for overhaul and tested is every 4 year
so life of an aircraft oxygen cylinder is 4 years also?! or 5 years will be the most correct answer?

Module 11. Aeroplane aerodynamics, structures and systems

What is the principle of an O2 generator?

  • Sodium chlorate and iron mixed by an electronic detonator.
  • Sodium chlorate and iron using a mechanical detonator producing O2 when mixed with air.
  • Sodium chloride and iron mixed by an electronic detonator.
soonhchong asking:

iron mixed by an electronic detonator or iron using a mechanical detonator?!

refer to CAIPs AL/3-25 3.5.1

Module 11. Aeroplane aerodynamics, structures and systems

Floor proximity lighting is a mandatory requirement and each light should be spaced

  • at 70 inch intervals.
  • at 60 inch intervals.
  • at 40 inch intervals.
soonhchong asking:

the answer suppose be 'at 40 inch intervals'
refer to CAAIPs Leaflet 5-11 2.7.1

Module 11. Aeroplane aerodynamics, structures and systems

During flap down selection in a continuous straight and level flight at constant IAS and weight

  • the lift coefficient and the drag coefficient increase.
  • the stall speed increases.
  • the centre of pressure moves aft, lift coefficient and the drag coefficient increase.
matth asking:

Center of pressure moves AFT but LIFT COEFFICENT AND DRAG INCREASE TOO

Module 11. Aeroplane aerodynamics, structures and systems

What external warning is there for an APU fire?

  • Aural.
  • Red light.
  • Both aural and a red light.
matth asking:

Never seen RED light outside Aircraft. AURAL sign OK

Module 11. Aeroplane aerodynamics, structures and systems

If a redundant structure fails it becomes

  • fatigued
  • safe-life
  • failsafe
matth asking:

The answer is FAILSAFE due to if a structure fail other structure (redundant) carry the load.
Safe life depend on LIFE of component. After FH or FC must be replaced... means that the component must be replaced BEFORE FAIL

Module 11. Aeroplane aerodynamics, structures and systems

To ensure that a wing stalls at the root first, stall wedges are

  • installed on the wing leading edge at the wing tip.
  • installed on the wing leading edge at the wing root.
  • installed at the wing trailing edge at the wing root.
matth asking:

Stall Wedges are installed at the wing ROOT LEADING EDGE PLS CORRECT

REF: http://www.scribd.com/doc/63481016/MODULE-11-COMPLETE

We use essential cookies to keep you signed in, plus anonymous analytics to understand how the site is used. Cookie-based analytics is set only with your consent. See our Privacy & Cookie Policy.