LearJet Training Resources
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Part 135 Training Resources
1.
The basic navigation system on the Lear 35 (FC200) consists of the
A.
pitot static system and ram air temperature gauge
B.
pitot static system and air data sensor, and the ram air temperature gauge
C.
air data sensor, air data computer, static system drains, and the pitot gauge
D.
pitot static system and air data sensor, and the absolute temperature gauge
2.
The normal (FC200) static system provides
A.
independent yet connected sources of static pressure to the pilot's instruments
B.
independent sources of dynamic pressure to the pilot and co-pilot's instruments
C.
independent and connected sources of pitot and static pressure to the pilot and co-pilot's instruments
D.
independent sources of static pressure to the pilot and co-pilot's instruments
3.
When the alternate static source valve (FC200) is positioned to OPEN
A.
the pilot's instruments are connected to an alternate port inside the unpressurized nose section
B.
the co-pilot's instruments are connected to an alternate port inside the unpressurized nose section
C.
the pilot's instruments are connected to an alternate port inside the pressurized nose section
D.
the co-pilot's instruments are connected to an alternate port inside the pressurized nose section
4.
The static port toggle switch (FC530) is normally set to the
A.
left (captain's) position except in the event one of the pitot-static heads becomes inoperable or unreliable.
B.
both position except in the event one of the ADI or RMI heads becomes inoperable or unreliable.
C.
both position except in the event one of the pitot-static heads becomes inoperable or unreliable.
D.
right (co-pillot's) position except in the event one of the pitot-static heads becomes inoperable or unreliable.
5.
A separate unheated static port is flush mounted on the right side of the nose section (FC530)
A.
to provide static pressure to the pressurization control module
B.
to provide static pressure to standby static system source selector
C.
to provide a separate source of static pressure to the secondary static system source selector
D.
to provide a standby source of static pressure to the secondary static system source selector
6.
The air data sensor provides air data to the autopilot computer
A.
and to the air data computer
B.
and to the altitude hold computer
C.
and to the Mach trim warning system
D.
and to the Mach trim computer
7.
The Static Port switch (FC530) is in the L position
A.
static pressure is provided to the left systems only from the two static ports on the left pitot static head
B.
static pressure is provided to the right systems only from the two static ports on the right pitot static head
C.
static pressure is provided to all user systems only from the two static ports on the left pitot static head
D.
static pressure is provided to all user systems from the static ports in the unpressurized nose compartment
8.
In the event of electrical failure (FC530)
A.
all static port shutoff valves will be closed regardless of the STATIC PORT switch position
B.
all static port shutoff valves will be open regardless of the STATIC PORT switch position
C.
only the pilot's (left side) static port shutoff valves will be open
D.
only the co-pilot's (right side) static port shutoff valves will be open
9.
FC530 Static ports for flight instruments are located
A.
in the pitot static heads
B.
in the unpressurized nose section
C.
flush mounted on the left and right sides of the nose section
D.
on both sides of the aft fuselage
10.
FC530 The pilot controls the static pressure source for the pilot's flight instruments
A.
mechanically with the static port switch
B.
electrically with the static port switch
C.
electrically with the alternate static source switch
D.
mechanically with the alternate static source switch
This is the end of the test. When you have completed all the questions and reviewed your answers, press the button below to grade the test.