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

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1,135 questions · 1,938 answers · 463 members contributing

76 threads

11. Aeroplane aerodynamics, structures and systems
4 replies

A VOR radial is a magnetic bearing measured

  • outward from the station.
  • towards the station.
  • from the aircraft heading.
E

Edigno92 asked · 16 Jun 2014

Why isn't VOR ?

JD2016: It's a bad question. A radial is the magnetic bearing outbound from a VOR. So the 3rd answer is correct in so far as it is FROM but a "beacon" could be an NDB (non directional beacon) and it is VORs (the 2nd answer) that are relevant. The 150 VOR radial is QDR 150 - 150 degrees from that VOR - which is QDM 330 - i.e. you would have to fly a heading (assuming no wind) of 330 to fly to that VOR.

11. Aeroplane aerodynamics, structures and systems
2 replies

A structure that keeps carrying its loads through redundant members after one member fails is

  • fatigued.
  • safe-life.
  • failsafe.
M

matth asked · 9 Mar 2012

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

aerorodder1: A failure in the failsafe or (redundant) system. Fix ASAP!

11. Aeroplane aerodynamics, structures and systems
1 reply

The type of fluid in an oleo strut will depend upon

  • the type of seal material.
  • heat generated in operation of the system.
  • type of fluid most readily available.
T

Trevordodd asked · 21 May 2015

i thought the answer to this question was type of seal material, does anyone know why its heat generated in operation as the type of fluid may break the seal down.

aerorodder1: They don't design struts to use certain o-rings, they design it for strength and to find the appropriate fluids and corresponding compressibility/heat-factors. The compressibility of a fluid determines it heat factor...you could use water in a shock-strut but it wouldn't compress as much as hydraulic fluids do and wouldn't generate as much heat.

11. Aeroplane aerodynamics, structures and systems
4 replies

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.
D

dyane_july86 asked · 4 Nov 2013

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

PART66Online: Sure, depends on type. On airbus it is possible to make a printout of faulty reading, fsb and ns lamps via MCDU CFDS.

11. Aeroplane aerodynamics, structures and systems
1 reply

Upper surface wing skin is usually made from

  • 2024.
  • 7075.
  • 5056.
S

soonhchong asked · 23 May 2012

Jeppesen A&P Technician Airframe Textbook 2-8. commonly used in the construction of skins and rivets are 2017 and 2024.

PART66Online: Hello. Please, if it is not too hard for you, use "Report" function to report wrong questions and please, provide a screenshot of book or link or other proof, because I don't have this book and can't check are you right or not. Q&A section is for discussing, not for reporting. Thank you for your understanding and reports!

11. Aeroplane aerodynamics, structures and systems
3 replies

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.
M

matth asked · 9 Mar 2012

Stall Wedges are installed at the wing ROOT LEADING EDGE PLS CORRECT REF: scribd.com/doc/63481016/MODULE-11-COM...

PART66Online: Hope my project helps you. :) Project is very young and I'm everyday receiving some reports. Some of them are correct but some are because of lack of student's training. But anyway, only together we can make it better. It is not possible only by me. :) I have some plans and ideas how to improve functionality to get better training results, soon I'll introduce them. :)

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