1 - Air Conditioning, Pressureisation & Ventilation Flashcards
- (DSC-21-10) Hot air fault light illuminates on the air conditioning panel.
(a) The hot air press. reg. valve opens and the trim air valves close.
(b) The hot air press. reg. valve closes and the trim air valves open.
(c) The hot air press. reg. valve closes and the trim air valves close.
(d) The hot air press. reg. valve opens and the trim air valves open.
(c) The hot air press. reg. valve closes and the trim air valves close.
- (DSC-21-10) In case of zone controller primary and secondary channel failure, what temperatures are maintained by pack one and pack two;
(a) 15 deg.c. both.
(b) 25 deg.c. both.
(c) 20 deg.c. pack 1, 10 deg.c. pack 2.
(d) 24 deg.c. pack 1, 15 deg.c. pack 2.
(c) 20 deg.c. pack 1, 10 deg.c. pack 2.
- (DCS-21-30) In normal flight in closed circuit configuration, the avionics ventilation system controls the temperature of the cooling air by;
(a) Adding air-conditioned air to the flow.
(b) Extracting air overboard.
(c) Adding avionics bay air.
(d) Passing air through a skin heat exchanger.
(d) Passing air through a skin heat exchanger.
- (DSC-21-10) To enable Ram air to the mixer until, the Ram air switch should be used;
(a) At any time.
(b) Only when diff. Press. Is less then 1 psi.
(c) When press. Is greater then 1 psi.diff.
(d) Only after outflow valve is fully opened.
(b) Only when diff. Press. Is less then 1 psi.
- (DSC-21-10) Pack controller, primary channel failure;
(a) The secondary computer operates as a back up mode and regulation is not optimised.
(b) The secondary computer takes over (all functions as normal).
(c) Pack is lost.
(d) Pack outlet temp. Is controlled at 15 deg.c.
(a) The secondary computer operates as a back up mode and regulation is not optimised.
- (DSC-21-10) Pack controller, secondary channel failure;
(a) No effect on pack regulation back up mode is lost.
(b) Pack is lost.
(c) No effect (all modes still available).
(d) Pack outlet temp. Is controlled at 15 deg.c.
(a) No effect on pack regulation back up mode is lost.
- (DSC-21-10) Pack controller, primary and secondary channel failure;
(a) Pack outlet temp. Is controlled at 5˚C to 30˚C in a maximum of 6 minutes by the anti-ice valve.
(b) The pack is closed.
(c) The packs deliver a fixed temperature of 20 deg.c.
(d) Both packs are controlled to 24 deg.c.
(a) Pack outlet temp. Is controlled at 5˚C to 30˚C in a maximum of 6 minutes by the anti-ice valve.
- (DSC-21-10) Hot air press. reg. valve failed open;
(a) Optimised regulation is lost.
(b) The temperature stays at the value selected when the failure occurred.
(c) No effect.
(d) Cabin temperature will be controlled at the upper limit 30 deg.c.
(c) No effect
- (DSC-21-10) Bleed air supplied from the APU (apu bleed valve open), the pack flow is automatically selected;
(a) High.
(b) Normal.
(c) Low.
(d) Econ. flow.
(a) High.
- (DSC-21-10) Trim air valve, each one optimizes the temperature by;
(a) Adding hot air.
(b) Adding fresh air.
(c) Modulation of pack flow.
(d) Adding recirculated air.
(a) Adding hot air.
- (DSC-21-10) Hot air pressure regulating valve;
(a) Regulates the pressure of hot air tapped upstream of the packs.
(b) Is spring loaded open in the absence of air.
(c) Opens automatically in case of duct overheat.
(d) Opens automatically if the cockpit trim air valve fails.
(a) Regulates the pressure of hot air tapped upstream of the packs.
- (DSC-21-10) Pack flow control valve;
(a) Is pneumatically operated and electrically controlled.
(b) Electrically operated and pneumatically controlled.
(c) Opens automatically during engine starting.
(d) Is spring loaded to open.
(a) Is pneumatically operated and electrically controlled.
- (DSC-21-10) The temperature selectors are located in;
(a) The cockpit.
(b) The cabin.
(c) The avionics bay.
(d) Only on the CIDS panel at the fwd. attendant station.
(a) The cockpit.
- (DSC-21-10) Pack flow may be selected from;
(a) The cockpit.
(b) The cabin.
(c) The avionics bay.
(d) Only the CIDS panel at the fwd. attendant station.
a) The cockpit
- (DSC-21-10) Engine pressure demand, when the cooling demand in one zone cannot be satisfied, if bleed pressure is low;
(a) The minimum idle must be increased manually.
(b) The minimum idle is increased automatically.
(c) In any case, flight idle is sufficient.
(d) The APU must be used to supply additional air.
(b) The minimum idle is increased automatically.
- (LIM-21-21-20) What is the Norm. Max. cabin altitude;
(a) 8,000 ft.
(b) 9,550 +/- 350 ft.
(c) 14,000 ft.
(d) 800 ft.
(a) 8,000 ft.
- (LIM-21-21-20) What is the Max. negative Diff. pressure for the cabin;
(a) 0 psi.
(b) -1 psi.
(c) -2 psi.
(d) -8.6 psi.
(b) -1 psi
- (LIM-21-21-10) Is it permissible to use simultaneously packs and Lp ground unit during long stops in a hot airfield;
(a) Yes.
(b) No.
(c) Yes, if external temperature is greater than 50 deg.c.
(d) Yes, provided the airflow supplied by the ground cart is less than 1.2 kg/s.
(b) No.
- (DSC-21-10) Trim air valves are modulated by;
(a) The zone controller.
(b) Anti-ice valve.
(c) Hot air pressure regulating valve.
(d) The pack controller.
(a) The zone controller.
- (DSC-21-10) The mixing unit is connected to;
(a) Packs, Cabin air, emergency ram air inlet and Lp ground connector.
(b) Packs, emergency ram air inlet and Lp ground connector.
(c) Packs and cabin air.
(d) Pack 1 and pack 2 only.
(a) Packs, Cabin air, emergency ram air inlet and Lp ground connector.
- (DSC-21-10) Once set to ‘ON’ the air conditioning packs operate;
(a) Automatically and independently of each other.
(b) Normally, but the output of one affects the other.
(c) Automatically, pack one as a master, pack two as a slave.
(d) Automatically, pack two as a master, pack one as a slave.
(a) Automatically and independently of each other.
- (DSC-21-10) Emergency ram air inlet, when set to ‘ON’ the ram air valve will open and supply airflow;
(a) In any case.
(b) Diff. press. < 1 psi. and ditching not selected.
(c) Provided ditching is not selected.
(d) Provided ditching is selected.
(b) Diff. press. < 1 psi. and ditching not selected.