FCC 2 (22-48) Exam Questions And Answers
Latest 2025
Q22-'Left side functions', in general terms, are controlled by the
Flight Control Computers (FCCs):
A-1 and 3.
-1 and 4.
-2 and 4. -
correct answer ✅A-1 and 3
Q23-The Flight Control Computers (FCCs) receive their power
supplies from:
-AC Busbars XP1 and XP2.
-Essential DC Busbars PP3 and PP4.
-Non-essential DC Busbar PP1 and AC Busbar XP3. -
correct answer ✅Essential DC Busbars PP3 and PP4.
Q24-The functions of the Flight Control Computer (FCC) do NOT
include:
, FCC 2 (22-48) Exam Questions And Answers
Latest 2025
-Bus Controller Interface control of ADT, SSICA, IMU and Digital
Engine Control and management Unit
(DECMU).
B-Remote Terminal Interface with the Attack and Utilities Control
System (UCS) buses.
-Flight Control Law Computation. -
correct answer ✅B-Remote Terminal Interface with the Attack and
Utilities Control System (UCS) buses.
Q25-The FCS Sensor that is NOT synchronised to the Flight Control
Computer via Intra-Channel
synchronisation is the
Air Data Transducer (ADT).
Stick Sensor Interface Control Assembly (SSICA).
C-Inertial Measurement Unit (IMU). -
correct answer ✅
Latest 2025
Q22-'Left side functions', in general terms, are controlled by the
Flight Control Computers (FCCs):
A-1 and 3.
-1 and 4.
-2 and 4. -
correct answer ✅A-1 and 3
Q23-The Flight Control Computers (FCCs) receive their power
supplies from:
-AC Busbars XP1 and XP2.
-Essential DC Busbars PP3 and PP4.
-Non-essential DC Busbar PP1 and AC Busbar XP3. -
correct answer ✅Essential DC Busbars PP3 and PP4.
Q24-The functions of the Flight Control Computer (FCC) do NOT
include:
, FCC 2 (22-48) Exam Questions And Answers
Latest 2025
-Bus Controller Interface control of ADT, SSICA, IMU and Digital
Engine Control and management Unit
(DECMU).
B-Remote Terminal Interface with the Attack and Utilities Control
System (UCS) buses.
-Flight Control Law Computation. -
correct answer ✅B-Remote Terminal Interface with the Attack and
Utilities Control System (UCS) buses.
Q25-The FCS Sensor that is NOT synchronised to the Flight Control
Computer via Intra-Channel
synchronisation is the
Air Data Transducer (ADT).
Stick Sensor Interface Control Assembly (SSICA).
C-Inertial Measurement Unit (IMU). -
correct answer ✅