LGAV 3110 Midterm Exam | Questions with complete solutions
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Course
LGAV 3110
Institution
LGAV 3110
LGAV 3110 Midterm Exam | Questions with complete solutions Equipment redundancy, LRUs, and MELs are designed to a. Stabilize the erratic nature of maintenance workload b. List the configuration differences between different aircraft c. Minimize maintenance delays d. A & B e. A & C DDG stands for ...
Equipment redundancy, LRUs, and MELs are designed to
a. Stabilize the erratic nature of maintenance workload
b. List the configuration differences between different aircraft
c. Minimize maintenance delays
d. A & B
e. A & C
DDG stands for
a. Designated Design Goals
b. Dispatch Deviation Guide
c. Deferral of Deteriorating Governors
d. Development of Destination Grounds
89% of aircraft components must be operated to failure before replacement or repair is
done. This results in the need for
a. Scheduled maintenance
b. Unscheduled maintenance
c. Unique equipment and components
d. Infant mortality
The design of aircraft systems or components is limited by
a. Physical entropy
b. Natural entropy
c. Man-made entropy
d. A & B
e. B & C
Maintenance can be scheduled daily, every flight, or every 100 cycles. A cycle is:
a. Revolutions per minute
b. An hour
c. Every time and engine is shut down
d. A takeoff and landing
Who determines which systems are not required to fly safely?
a. FAA
b. NTSB
, c. Mechanic
d. Pilot
The result of the MSG-3 analysis is published in the MRB (Maintenance Review Board)
report. This report
a. Is known by all U.S. carriers as the OAMP (On Aircraft Maintenance Planning)
document
b. Contains the initial scheduled maintenance program
c. Is used by U.S. certificated operators
d. B & C PAGE
Hard Time (HT), On-Condition (OC) and Condition Monitoring (CM) are failure
preventive processes
True
False
The _________approach to maintenance is primarily used by airlines for their new
aircraft
a. Process-oriented
b. Task-oriented
c. Maintenance Steering Group (MSG)
d. Mechanical Reliability Testing
Condition Monitoring (CM) monitors the _______ of the component
a. Condition
b. Failure/removal statistics
c. Reliability
d. Controllability
Which of the following is NOT a source of structural deterioration?
a. Environmental Deterioration
b. Accidental Damage
c. Fatigue Damage
d. Stress Damage
An aircraft operating in a humid environment may be subject to a maintenance task
more often than the MRB report indicates compared to operation in a dry climate.
True
False
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