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TCAS II Questions with 100% Correct Answers | Verified | Latest Update 2024, Complete Solutions
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TCAS II Questions with 100% Correct Answers | Verified | Latest Update 2024, Complete Solutions
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TCASII
1
.
Disregarding
RA
information
may
result
in:
Safe
vertical
separation
may
be
lost.
Excessive
altitude
excursions.
ATC
unknowingly
issuing
instructions
contrary
to
the
RA.
All
of
the
answers
are
correct.
-
ANS-All
of
the
answers
are
correct.
1
.
Flying
with
inoperative
TCAS
II
is
permitted.
True;
however
the
fault
must
be
rectified
within
3
days.
True;
provided
it
is
done
in
accordance
with
the
applicable
MEL
provisions.
False;
only
aircraft
with
TCAS
I
may
fly
when
the
system
is
inoperative.
False;
TCAS
must
be
operative
if
it
is
installed.
-
ANS-True;
provided
it
is
done
in
accordance
with
the
applicable
MEL
provisions.
1
.
If
the
input
from
the
aircraft's
transponder
fails:
RAs
will
be
inhibited.
TCAS
will
automatically
fail.
TAs
and
RAs
will
be
inhibited.
TCAS
visual
display
will
fail
and
pilots
must
rely
solely
on
TCAS
aural
annunciations.
-
ANS-TCAS
will
automatically
fail.
1
.
TCAS
II
version
7.1:
Is
the
commercially
available
implementation
of
ACAS
II.
All
answers
are
correct.
Is
mandated
by
ICAO. Is
an
airborne
collision
avoidance
system.
-
ANS-All
answers
are
correct.
1
.
Traffic
advisories:
Alert
the
pilot
of
the
presence
of
another
aircraft
that
may
become
a
threat.
Coordinate
between
TCAS
equipped
aircraft.
Provide
information
to
pilots
on
how
to
modify
or
regulate
vertical
speed
to
avoid
a
potential
mid-air
collision.
All
of
the
answers
are
correct.
-
ANS-Alert
the
pilot
of
the
presence
of
another
aircraft
that
may
become
a
threat.
10
.
A
corrective
RA
will
advise
the
pilot
to:
Any
of
these.
Deviate
from
current
vertical
speed.
Maintain
existing
descent
rate.
Maintain
existing
climb
rate.
-
ANS-Any
of
these
10
.
TCAS
is
designed
to
provide
collision
avoidance
for
aircraft
closing
horizontally
up
to
1200
kts.
and
vertically
up
to:
7,000
fpm.
12,000
fpm.
10,000
fpm.
5,000
fpm.
-
ANS-10,000
fpm.
10
.
TCAS
is
recommended
for:
Only
Part
135
aircraft.
Turbine
powered
aircraft
with
a
maximum
takeoff
weight
over
5,700
kg
or
authorized
to
carry
more
than
10
passengers.
Aircraft
with
a
maximum
takeoff
weight
over
5,700
kg
or
authorized
to
carry
more
than
19
passengers.
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