MENU
EN
IT
ES
DE
FR
PL
CZ
NL
HU
RS
EN ATPL Operational Procedures Questions in English
Practise Operational Procedures
A water fire-extinguisher (straight jet) can be used on a fire of: 1 - solids (fabric, carpet,...). 2 - liquids (ether, gasoline,...). 3 - gas. 4 - metals (sodium,...). The combination regrouping all the correct statements is:
For an internal engine tailpipe fire during ground start or shutdown, when the aircraft’s approved procedure calls for ventilation with fuel and ignition off, which action provides that ventilation?
Which of the following extinguisher types are rated for ordinary Class A fires? 1. Water. 2. Carbon dioxide. 3. Multipurpose (ABC-rated) dry chemical. 4. Halon 1211.
During an explosive decompression at flight level 370 (FL 370), your first action will be:
Refer to figure op2. If cabin pressure altitude is 14,000 ft and the cabin-to-ambient pressure differential is 3 psi, what aircraft pressure altitude is closest to the ISA pressure calculation?
When taking off behind a heavy aeroplane with a crosswind from the left, which relative flight path is preferable for wake avoidance when permitted by ATC and aircraft performance?
When the standard category-based time wake minima are applied to an instrument arrival, a LIGHT aeroplane (7,000 kg or less) follows a MEDIUM aeroplane on approach to landing. With no visual-approach exception or alternative approved wake scheme, what minimum time separation applies?
Under the standard time-based wake minima in AMC2–AMC3 ATS.TR.220, excluding VFR and visual-approach exceptions and alternative approved schemes, which listed case requires 3 minutes?
What transponder code should be used to provide recognition of an aircraft which is being subjected to unlawful interference:
From the following list: 1. Fuel jettisoning system and its operation are free from fire hazard 2. The fuel discharges clear of any part of the aeroplane 3. Fuel fumes do not enter any part of the aeroplane 4. The jettisoning operation does not adversely affect the controllability of the aeroplane. Which of the above are requirements that must be shown to exist during fuel jettisoning tests:
