If during a descent the pneumatic altimeter reading is constant the vertical

If during a descent the pneumatic altimeter reading

This preview shows page 47 - 49 out of 151 pages.

0294. If , during a descent ; the pneumatic altimeter reading is constant , the vertical speed indicator shows zero , the IAS is increasing , the most likely explanation is that ; a)the antenna of the radio altimeter is completely iced up. b)the static ports are completely blocked. c)the total pressure head is completely blocked. d)there is a leakage in the static pressure line. Answer ; b)the static ports are completely blocked. -----------------------------------------------------------------------------------------------------------------------------------------------------------------0295. If immediate crew awareness is required and subsequent crew action will be required , the flight warning system ( FWS ) generates ; -----------------------------------------------------------------------------------------------------------------------------------------------------------------0296. If immediate recognition and corective or compensatory action by the crew is required , the flight warning system ( FWS ) generates ; -----------------------------------------------------------------------------------------------------------------------------------------------------------------0297. If , in the event of a failure , the approach , flare and landing can be completed by the remaining part of the automatic system , such an automatic landing system is considered as ; -----------------------------------------------------------------------------------------------------------------------------------------------------------------0298. If , in the event of a failure , there is no significant out-of-trim condition or deviation of flight path or attitude but the landing is not completed atomatically , such an automatic landing system is considered as ; a)fail-passive. b)fail-safe. c)fail-operational. d)fail-redundant. Answer ; a)fail-passive. -----------------------------------------------------------------------------------------------------------------------------------------------------------------0299. If OAT decreases when at a constant Mach number ; ----------------------------------------------------------------------------------------------------------------------------------------------------------------- 0300. If OAT decreases when at a constant TAS ; a)Mach number remains constant. b)Mach number decreases. c)the difference between surrounding conditions and ISA must be known to deduce the Mach number variation. d) Mach number increases. Answer ; d) Mach number increases. -----------------------------------------------------------------------------------------------------------------------------------------------------------------
Background image
Ateş Murat Üstünbıçak , ATPL Instrumentation 48 0301. If OAT decreases whilst maintaining a constant CAS and flight level ; 0302. If OAT increases when at a constant Mach number ;
Background image
Image of page 49

  • Left Quote Icon

    Student Picture

  • Left Quote Icon

    Student Picture

  • Left Quote Icon

    Student Picture