What are the zones in the aircraft?
LocationZones:
100 UpperHalfofFuselage.
200 LowerHalfofFuselage.
300 Empennage.
400 PowerplantandNacelleStruts.
500 LeftWing.
600 RightWing.
700 LandingGearandLandingGearDoors.
800 Doors.
100 LowerHalfofFuselage.
200 Empennage.
300 UpperHalfofFuselage.
400 PowerplantandNacelleStruts.
500 LeftWing.
600 RightWing.
700 LandingGearandLandingGearDoors.
800 Doors.
100 LowerHalfofFuselage.
200 UpperHalfofFuselage.
300 Empennage.
400 PowerplantandNacelleStruts.
500 LeftWing.
600 RightWing.
700 LandingGearandLandingGearDoors.
800 Doors.
. What are the models of B737 NG? B737-500
B737-600
B737-700
B737-800
B737-600
B737-700
B737-800
B737-900
B737-300
B737-400
B737-500
B737-600
. What is a body station? BS, В STA, or STA
Body (Fuselage) Station. A plane that is perpendicular to the fuselage
centerline. It is measured from a point 130.00 inches forward of the
nose.
BS, В STA, or TTA
Body (Fuselage) Station. A plane that is perpendicular to the fuselage
centerline. It is measured from a point 140.00 inches forward of the
nose.
BS, В STA, or STA
Body (Fuselage) Station. A plane that is perpendicular to the fuselage
centerline. It is measured from a point 130.00 inches forward of the
tai
. Which are the principal and auxiliary points of jacking? Main points:
Wings jacking points C and D
Aft body jacking point A
Auxiliary points:
Fwd body jacking point D
Point E (Nose)
Point F (Landing Gear)
Main points:
Wings jacking points A and E
Aft body jacking point C
Auxiliary points:
Fwd body jacking point D
Point E (Nose)
Point F (Landing Gear)
Main points:
Wings jacking points A and B
Aft body jacking point C
Auxiliary points:
Fwd body jacking point D
Point E (Nose)
Point F (Landing Gear)
. Where is located p6 and p18 panels?
p18 is located behind the first officer's seat
p6 is located behind the captain's seat
p18 is located behind the first officer's seat
p16 is located behind the captain's seat
p6 is located behind the first officer's seat
p18 is located behind the captain's seat
. The maximum angle of the nose steering is? 78 Degrees 87 Degrees 79 Degrees. How many times the standby electricalpower system
supplies AC and DC power to heelectrical network of
the aircraft?
30 minutes of AC and DC power to systems
necessary to maintain safe flight
30 hours of AC and DC power to systems
necessary to maintain safe flight
30 seconds of AC and DC power to systems
necessary to maintain safe flight
. What is the function of TRU? Transformer Rectifier Units (TRUs)
convert the 115V dc to 28V ac
Transformer Rectifier Units (TRUs)
convert the 115V ac to 28V dc
Transformer Rectifier Units (TRUs)
convert the 28V ac to 115V dc
. Where is located the external power connection? Is located on the right side of the fuselage, near the nose. Is located on the left side of the fuselage, near the nose. Is located on the right side of the fuselage, far the nose. What is the function of the Static Inverter? The static inverter supplies a one phase, converter 115v dc to 28v ac output to the AC standby bus
The static inverter supplies a one phase, converter 28v ac to 115v dc output to the AC standby bus
The static inverter supplies a one phase, converter 28v dc to 115v ac output to the AC standby bus
. What type of alert does the Fire and overheat detection
System provide to alert the lght crew?
Visual (fire warning) and aural indications (bell) Touch and aural indications Visual . Where are located the engine and APU fire control panel? Is in the right main wheel well, on the aft Bulkhead.P18 Is in the left main wheel well, on the aft Bulkhead.P28 Is in the right main wheel well, on the aft Bulkhead.P28. What is the function of Nitrogen Generator system? The nitrogen is to push out the oxygen from the center fuel tank The nitrogen is to push out the oxygen from the 1 fuel tank The nitrogen is to push out the oxygen from the 2 fuel tank. How many fuel tanks are installed in the aircraft 3 Fuel Capacity
Main tank 1 (8630lbs-3915kg)
Main tank 2 (8630lbs-3915kg)
Center tank (28803lbs-13065kg)
3 Fuel Capacity
Main tank A (8630lbs-3915kg)
Main tank B (8630lbs-3915kg)
Center tank (28803lbs-13065kg)
3 Fuel Capacity
Main tank 1 (8630lbs-3915kg)
Main tank 2 (8630lbs-3915kg)
Main tank 3 (28803lbs-13065kg)
. What is the function of spar valve battery? The engine fuel spar valve battery makes sure that the engine fuel feed system some has power to open the engine fuel spar valve The engine fuel spar valve battery makes sure that the engine fuel feed system always The engine fuel spar valve battery makes sure that the engine fuel feed system always has power to close the engine fuel spar valve. What is the function of wáter scavenge ejector pumps? The water scavenge jet pumps remove water from the low points of each tank to prevent corrosion.
The water scavenge jet pumps remove water from the low points of tank 1 to prevent corrosion.
The water scavenge jet pumps remove water from the low points of center to prevent corrosion.
. during refueling procedures of the main tanks and center tank the blue valve position lights come on when the refuling shutoff valve selenoid have power when the refuling shut on valve selenoid have power when the refuling shutoff valve selenoid not power. How many fuels measuring stick are installed in the aircraft and what is the function? (5) installed in center tank (8)main tank 1 and 2, total 21 (4) installed in center tank (6)main tank 1 and 2, total 16 (4) installed in center tank (4)main tank 1 and 2, total 12. Which are the threemain Hydraulic Systems? System A, B, and C Hidraulic Sys. System A, B, and STANBY System A, B, and STANBY Hidraulic Sys. What is the function of PTU? Hydraulic Power Transfer Unit (PTU) System
The PTU system is a hydraulic motor-pump assembly that supplies alternative pressure to leading edge flaps and slats and auto slat the system is located on system B on the right side of the plane.
Hydraulic Power Transfer Unit (PTU) System
The PTU system is a hydraulic motor-pump assembly that supplies alternative pressure to leading edge flaps and slats and auto slat the system is located on system A on the right side of the plane.
Hydraulic Power Transfer Unit (PTU) System
The PTU system is a hydraulic motor-pump assembly that supplies alternative pressure to leading edge flaps and slats and auto slat the system is located on system B on the left side of the plane.
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