C-5M PIQ Test 1 Review
2026-2027
Expert-Verified Questions and Answers
(With A+ Grades Guarantee)
,At 35C at sea level, each CF-6 Engine produces 51,250
___________ lb of static thrust
The max continuous trust of each engine is __________ lb 44,830 lb
The operating weight of the C-5M can vary between 375,000 - 425,000
_______ to ______ pounds
The definition of a heavyweight airplane is gross weights 635,850 lb
above normal landing weight of __________
C-5M Height minimum: 64' 9"
C-5M Height Maximum: 65' 1"
C-5M length: 247' 10"
C-5M Wing Span: 222' 9"
C-5M Stabilizer span: 68' 9"
How many total pallet positions are on the C-5M? 36
The flight deck and relief crew compartment will 20
accommodate _______ personnel
How many personnel can the troop compartment -75
accommodate? 73 pax + 2 loadmasters
Each ________ computer is linked to its corresponding VIA
AIU
VIA/AIU No. 1 is located in avionics bay number______ 4
VIA/AIU No. 2 is located in avionics bay number______ 3
, If both VIA/AIUs fail, a ___________ performs reduces backup integrating processor (BIP)
processing functions to provide essential flight information,
nav data, and engine instrumentation.
The _________ provides processing for basic get-home BIP
capability.
The BIP is located in avionics bay number ____ 4
How many remote interface units (RIUs) are on the C-5M? 6
(T/F) The BIP automatically takes over core processing if True
both VIA/AIUs fail
Two _____________ provide an interface between each bus system interface units (BSIUs)
VIA/AIU, various radios and airplane systems.
Using any MCDU, the BSIUs enable or disable power to: TACAN 1, TACAN 2, MMR 1, MMR 2, EGI 1, EGI 2, UHF 3, and the IFF
The VIA/AIUs contain 4 hardware components that are Line replaceable units (LRUs)
commonly called "black boxes". The dash -1 refers to them
as ____________
(T/F) If at least one VIA/AIU is operating, the core True
processing system will continue to function normally.
The LRUs of the pilot's VIA/AIU are: VIA computer number 1 and AIU number 1.
The ___________ is used to control and manage flight management system (FMS)
navigation, performance, and radio communications
functions.
The __________ enables datalink communications communications management function (CMF)
between onboard avionics and ground stations.
The mission processing system (MPS) in each VIA/AIU is - touchdown relays
programmed with an air/ground algorithm. The MPS - wheel spinup signals
algorithm senses the air/ground state based on air/ground - radar altimeters
sensing inputs from ________, _______, and ______
What are the 3 VIA/AIU failure modes? - Fail-safe
- Fail-passive
- Fail-operative
YELLOW: NO MATTER WHICH FAILURE MODE, THE CREW IS ALERTED FOR
ALL THREE TYPES
2026-2027
Expert-Verified Questions and Answers
(With A+ Grades Guarantee)
,At 35C at sea level, each CF-6 Engine produces 51,250
___________ lb of static thrust
The max continuous trust of each engine is __________ lb 44,830 lb
The operating weight of the C-5M can vary between 375,000 - 425,000
_______ to ______ pounds
The definition of a heavyweight airplane is gross weights 635,850 lb
above normal landing weight of __________
C-5M Height minimum: 64' 9"
C-5M Height Maximum: 65' 1"
C-5M length: 247' 10"
C-5M Wing Span: 222' 9"
C-5M Stabilizer span: 68' 9"
How many total pallet positions are on the C-5M? 36
The flight deck and relief crew compartment will 20
accommodate _______ personnel
How many personnel can the troop compartment -75
accommodate? 73 pax + 2 loadmasters
Each ________ computer is linked to its corresponding VIA
AIU
VIA/AIU No. 1 is located in avionics bay number______ 4
VIA/AIU No. 2 is located in avionics bay number______ 3
, If both VIA/AIUs fail, a ___________ performs reduces backup integrating processor (BIP)
processing functions to provide essential flight information,
nav data, and engine instrumentation.
The _________ provides processing for basic get-home BIP
capability.
The BIP is located in avionics bay number ____ 4
How many remote interface units (RIUs) are on the C-5M? 6
(T/F) The BIP automatically takes over core processing if True
both VIA/AIUs fail
Two _____________ provide an interface between each bus system interface units (BSIUs)
VIA/AIU, various radios and airplane systems.
Using any MCDU, the BSIUs enable or disable power to: TACAN 1, TACAN 2, MMR 1, MMR 2, EGI 1, EGI 2, UHF 3, and the IFF
The VIA/AIUs contain 4 hardware components that are Line replaceable units (LRUs)
commonly called "black boxes". The dash -1 refers to them
as ____________
(T/F) If at least one VIA/AIU is operating, the core True
processing system will continue to function normally.
The LRUs of the pilot's VIA/AIU are: VIA computer number 1 and AIU number 1.
The ___________ is used to control and manage flight management system (FMS)
navigation, performance, and radio communications
functions.
The __________ enables datalink communications communications management function (CMF)
between onboard avionics and ground stations.
The mission processing system (MPS) in each VIA/AIU is - touchdown relays
programmed with an air/ground algorithm. The MPS - wheel spinup signals
algorithm senses the air/ground state based on air/ground - radar altimeters
sensing inputs from ________, _______, and ______
What are the 3 VIA/AIU failure modes? - Fail-safe
- Fail-passive
- Fail-operative
YELLOW: NO MATTER WHICH FAILURE MODE, THE CREW IS ALERTED FOR
ALL THREE TYPES
