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progress test 163.pdf

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8 :58 AM Fri 16 Jun ~94% - F""(J A320 Progress Test - T X + i forms.office.com...

8 :58 AM Fri 16 Jun ~94% - F""(J A320 Progress Test - T X + i forms.office.com JFO 163 Hi, Hitesh. When you submit this form, the owner will see your name and email address. 1. The engine generators and APU generator are rated at _ _ KVA 0 50 0 70 0 90 0 110 2. The number 1 AC bus channel normally supplies power to _ _ and to the _ _ bus which supplies power to the ___ bus. Q TR2 / AC ESS SHED / DC ESS SHED Q TR1 / AC ESS SHED/ DC ESS Q TR1 / AC ESS / AC ESS SHED 8:58 AM Fri 16 Jun -:::-94%- F-r: A320 Progress Test - T X + i forms.office.com 3. When no other power is available in flight, the static inverter converts _ _ power to AC power for the bus; and ___ powers the _ _ _ bus. _ __ Q BAT1 DC/ AC ESS bus/ BAT2 / DC ESS Q BAT1 DC / AC ESS SHED/ BAT2 / DC ESS SHED Q BAT1 DC / AC ESS bus/ BAT2 / DC ESS SHED Q BAT1 DC / AC ESS bus/ DC ESS 4. The IDG Fault light indicates: Q An IDG oil over heat Q IDG low oil pressure. Q IDG low oil pressure or IDG oil overheat Q IDG has been disconnected 5. After landing, in the emergency electrical configuration : the batteries automatically connect to the nr. T h, - h n - n Ai:> Ar. i:,;:::i.;:.i:,95%) 8 :58 AM Fri 16 Jun ':::'94% -.-r: A320 Progress Test - T X + a forms.office.com 30. On ECAM's Cab. Press Page, the outflow valve indicator changes to amber if: Q It is fully open on the ground (>95%) Q It is open in flight (>95%) Q It is not fully open on the ground 31. Position of TRIM Air valves and HOT AIR pressure regulating valve are indicated on Q COND SD page. Q BLEED SD page Q COND & BLEED SD pages Q COND and CAB PRESS SD pages. 32. Two safety valves are provided such that Q Each safety valve avoids excessive positive and negative differential pressure. One safety valve avoids excessive positive differential pressure and another safety valve avoids excessive 0 ne ative differential press 8 :58 AM Fri 16 Jun ~94% - F-c A320 Progress Test - T X + i forms.office.com 32. Two safety valves are provided such that 0 Each safety valve avoids excessive positive and negative differential pressure. One safety valve avoids excessive positive differential pressure and another safety valve avoids excessive 0 negative differential pressure. 0 Both safety valves avoid excessive positive differential pressure only. 0 Both safety valves avoid excessive negative differential pressure only. 33. At what cabin altitude do you get an ECAM warning? 0 8,800 feet. Q 9,550 feet 0 14,000 feet. 34. With the engines off, if the AVAIL light is illuminated on both the APU START push button and the EXT PWR push button , what is the source of electrical power for the aircraft busses? 0 The aircraft batteries 8 :59 AM Fri 16 Jun ':::'94% - rr: A320 Progress Test - T X + i forms.office.com 34. With the engines off, if the AVAIL light is illuminated on both the APU START push button and the EXT PWR push button, what is the source of electrical power for the aircraft busses? 0 The aircraft batteries Q TheAPU. 0 External power. 35. What type of the Fuel is commonly used for our aircraft operation? Q JetA Q Jet A-1 Q JetB 36. What is the maximum altitude at which the APU may be started using the batteries only? 0 15, 000 ft 0 25 , 000 ft 0 39, 000 ft 8 :59 AM Fri 16 Jun -;:'94% - F""L, A320 Progress Test - T X + i forms.office.com ~ c!J 8 37. REV appears in green on ECAM when Q Only one reverser is deployed. Q On ground, the thrust reverser system is fully deployed Q In flight, the thrust reverser system is fully deployed Q Both B and C are correct. 38. During the second engine auto start, the PTU is Q. Inhibited. Q.Automatically tested. - Q.Automatically running. Q. Not available on ground. 39. In a managed DES mode, if aircraft is above profile , what is NTHR mode and what does A/P pitch channel control? Q THR IDLE and speed {IAS)11111ib~911111:l!lt:P~Plitlitsl!JIII~:sl!Jlil1!11!11&"'1i111111: s l ! J l i l - - - - - - - - - 8 :59 AM Fri 16 Jun ':::'94% - F"(J A320 Progress Test - T X + i forms.office.com 39. In a managed DES mode, if aircraft is above profile, what is A/THR mode and what does A/P pitch channel control? Q THR IDLE and speed {IAS} by AP Pitch channel Q SPEED and rate of descent by AP Pitch channel 0 THR IDLE and rate of descent by AP Pitch channel 40. Which of the followings is the GPWS Mode 1? Q Altitude loss after takeoff, or go-around. 0 Excessive terrain closure rate 0 Excessive rate of descent. 41. Both ECAM screens have failed. Is it possible to get E/WD indications? Q Yes, the E/WD is automatically transferred to one of the NDs. Q No. The E/WD is lost until the aircraft can be repaired. ( ) Yes , to get E/WD informatidll, It ii :ast 66 ii :a::aa119 aa::s:e:: ea to a: :e GI a:e 140.,. 8 :59 AM Fri 16 Jun '=::-94% - F-o A320 Progress Test - T X + i forms.office.com 41. Both ECAM screens have failed. Is it possible to get E/WD indications? Q Yes, the E/WD is automatically transferred to one of the NDs. Q No. The E/WD is lost until the aircraft can be repaired. Q Yes, to get E/WD information, it must be manually transferred to one of the NDs. Q Yes. E/WD information is automatically transferred to the the F/O's PFD in the event of an ECAM warning. 42. On the ground , CVR is stopped automatically ___ after the last engine shutdown. 0 Immediately 0 1 minute 0 3 minutes 0 5 minutes. 43. Mark the correct statements: Q You may fly with one engine in N1 mode and other engine in EPR Mode 8 :59 AM Fri 16 Jun '?94% - F-c A320 Progress Test - T X + i forms.office.com 43. Mark the correct statements: Q You may fly with one engine in N1 mode and other engine in EPR Mode Q You may fly one engine in Rated N1 mode and the other engine in Degraded N1 mode. Q Both are correct 44. In case of heavy rain which p/b is required to be pressed for "Operation in Heavy Rain on ground"? Q Extract to OVRD Q Blower to OVRD Q Blower and Extract to OVRD Q Ditching p/b to ON. 45. There is abnormal residual pressure in the cabin on touch-down when pressurization was controlled manually in flight. The aircraft will be automatically de-pressurized by opening the outflow valve, as soon as: Q All ADIRS indicate an airsµip?ii11i?M1d1111b1i11i1?111111la111111111111:11111111A A11111l111iCts....- - - - - - - - - - 8 :59 AM Fri 16 Jun -:::'94% - F"'(J A320 Progress Test - T X + i forms.office.com ~ c!J GJ 45. There is abnormal residual pressure in the cabin on touch-down when pressurization was controlled manually in flight. The aircraft will be automatically de-pressurized by opening the outflow valve, as soon as: Q All ADIRS indicate an airspeed below 100 kts Q Any one ADIRS indicate an airspeed below 100 kts Q On one engine is shutdown, Q Parking brakes are applied 46. Which of the following is NOT possible on ground? Q APU GEN powering AC BUS 1 and EXT PWR powering AC BUS 2. Q GEN 1 powering both AC BUS 1 and AC BUS 2. Q GEN 1 powering AC BUS 1 and APU GEN powering AC BUS 2. 47. The BAT FAULT light will illuminate when : Q Battery voltage is low 8 :59 AM Fri 16 Jun ':::-94% - F-c A320 Progress Test - T X + i forms.office.com 47. The BAT FAULT light will illuminate when: Q Battery voltage is low Q Charging current increases at an abnormal rate Q Charging current decreases at an abnormal rate. 48. If an engine fire is detected, when will the pedestal mounted red FIRE annunciator light extinguish? Q When the crew pushes the red MASTER WARN push button. Q After the fire getting extinguished. Q Only after the crew selects the adjacent ENG MASTER switch to off. 49. In case of Avionics Smoke, which page is displayed on S/D? A. Cruise page B. Air cond. page C. Pressurization page D. Elect page Enter your answer 8 :59 AM Fri 16 Jun ':::-94% -.-r-. A320 Progress Test - T X + i forms.office.com ~ c!J GJ 49. In case of Avionics Smoke, which page is displayed on S/D? A. Cruise page B. Air cond. page C. Pressurization page D. Elect page Enter your answer 50. Antiskid is deactivated below Q 20 kts Q 30 kts Q 40 kts Back Submit This content is created by the owner of the form. The data you submit will be sent to the form owner. Microsoft is not responsible for the privacy or security practices of its custom ; I I di g U f II I f II gl I9 password.

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aviation aircraft systems electrical engineering
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