AVIA 435 Quiz 3
AVIA 435 Quiz 3
- Takeoff with engine fuel feed temperature readouts below __________ degrees C is prohibited.
- DC BUS 2 is protected by __________?
- Pressing the EMER DEPR(ESS) switchlight on the Cabin Press Control Panel drives the outflow valves fully open and allows the cabin altitude to climb to (a maximum of) __________ feet.
- Which position of the Cargo Fan Switch maintains a suitable temperature for live cargo?
- According to the Originating Check, what is the correct switch positions for the left and right 14th stage SOVs on the BLEED AIR PANEL? (Ref: CR2 OM 2-3.4)
- Which circuit breaker panel is located behind the First Officer’s seat?
- How many nicad batteries are installed in the aft equipment bay?
- The STDBY (STBY) fan position on the ARINC Fan selector: (Ref: CR2 OM 11-7.4)
- Which of the following is required to be selected Off for takeoff?
- During normal operations, AC electrical power is provided by __________ AC generators.
- Fluid from three independent hydraulic systems powers:
- What is the maximum permissible individual loading on the APU generator at 37,000 feet?
- Which of the following statements is correct?
- Which of the following is/are true concerning the automatic thrust lever retard system?
- The normal source of DC power comes from __________ TRUs.
- What is the power source for the internal cabin reading lights? (Ref: CR2 OM 11-6.8)
- Which DC bus provides power to the aircraft navigation lights?
- Which of the following is/are true concerning the two pneumatic air conditioners (Packs) in the Environmental Control System? (Ref: CR2 OM 11-7.1)
- The APR system is armed for takeoff when:
- Where is the 14th stage isolation valve located? (Ref: CR2 OM 11-19.3)
- When no bleed air is provided or electrical power is lost, the 10th stage SOVs are
- In-flight, Hydraulic System 1 and 2 B pumps can manually be selected ON as long as:
- Where is the 10th stage isolation valve located?
- The maximum permissible fuel imbalance between the contents of the main left tank and the main right tank is __________ lbs.
- The cabin pressurization system must not be operated to __________ feet when the system is in the manual mode.
- Two __________ are installed in each wing leading edge to detect uncontrolled leakage of the anti-ice piccolo tubes.
- Which of the following is/are true concerning the Bleed Air Control Panel? (Ref: CR2 OM 11- 19.4)
- Inflight, which of the following statements is/are correct?
- During automatic powered crossflow, if a fuel imbalance of more than __________ exists between the fuel tanks, the fuel computer opens the crossflow valve associated with the low wing tank allowing fuel to flow to that wing tank.
- The 10th stage Bleed Air Leak Detection System uses a __________ overheat detection system.
- What is the in-flight maximum permissible continuous load on each Transformer Rectifier (TRU) is __________ amps.
- When the (either) wing tank quantity drops below __________, the fuel computer initiates fuel transfer from the center tank to the wing tank.
- In the AUTO mode the B pumps for Hydraulic Systems 1 and 2 will operate when:
- The high pressure used to create motive flow must be provided from the high pressure output developed from
- The maximum operating altitude single pack is __________ feet .
- In the Refueling/Defueling section, what does the acronym MLI stand for?
- The bleed air 10th stage valves must be __________.
- The APU battery is rated at 24 volts and __________ amp/hr.
- The 14th stage Bleed Air Leak Detection System uses a __________ overheat detection system.
- With the Engine Speed Switches selected ON, the switchover from N2 and N1 speed governing occurs above __________ N1.