Part 107 Loading and Performance
Loading and performance questions test aircraft limits, center of gravity, payload, battery endurance, density altitude, obstacle clearance, and manufacturer data.
How to study FAA Part 107
Build each answer around remote PIC responsibility: verify the rule, check airspace authorization, read weather and charts, preserve battery and performance margin, brief the crew, and stop the operation when the risk picture changes.
Core concepts
Concept 1
Part 107 Loading and Performance questions reward the answer that follows the official rule source, safety duty, and practical work sequence.
Exam cue: Identify the system, hazard, tool, code rule, or licensing duty being tested.
Concept 2
The strongest answer controls the hazard before continuing work, testing equipment, or documenting completion.
Exam cue: Check inspection, isolation, measurement, documentation, and environmental requirements.
Concept 3
Eliminate answers that ignore inspection, code clearance, environmental controls, lockout, labeling, or qualification limits.
Exam cue: Choose the safe compliant answer before the fastest production answer.
Risk pitfalls and guardrails
Treating local, state, and federal rules as interchangeable.
Guardrail: Avoid answers that skip inspection, ignore the code source, energize unsafe equipment, vent regulated material, or treat local rules as optional.
Skipping required inspection, isolation, documentation, or recovery steps.
Guardrail: Avoid answers that skip inspection, ignore the code source, energize unsafe equipment, vent regulated material, or treat local rules as optional.
Choosing a convenient answer that exceeds the worker's qualification or equipment rating.
Guardrail: Avoid answers that skip inspection, ignore the code source, energize unsafe equipment, vent regulated material, or treat local rules as optional.
Memory anchors
Weight Limit
A small UAS operation must respect aircraft weight and configuration limits.
Center Of Gravity
Improper CG can reduce stability, controllability, and recovery margin.
Payload Secure
Payload must be attached so it does not shift, detach, or create controllability hazards.
Battery Planning
Battery reserves must cover the mission, contingency, return, wind, temperature, and landing margin.
Performance Data
Use manufacturer performance data and limitations before assuming climb, range, or endurance.
Temperature Effect
Cold can reduce battery output, while heat can reduce electronics and motor reliability.
Obstacle Clearance
Launch and recovery planning must account for wires, trees, structures, terrain, and people.
Lost Link
Lost-link or return-to-home settings must fit airspace, obstacles, and mission geometry.
Propeller Condition
Damaged propellers can create vibration, reduced lift, and loss of control.
No Overload Shortcut
A mission objective never justifies exceeding aircraft, payload, or battery limits.
Checkpoint rule
Do the check-up only after you can summarize each concept in one sentence and identify one dangerous pitfall from memory.
Knowledge Check (after reading)
Short check-up to confirm understanding of this module.
Check-up Questions
A drone weighs 12 pounds empty and has a maximum approved operating weight of 18 pounds. The camera mount weighs 1.5 pounds. What maximum camera weight remains?
A small UAS weighs 52 pounds with its normal battery. A 2-pound sensor and 1.5-pound bracket are added. Can it remain within the Part 107 small-aircraft definition?
Answer all questions to submit.
Next step personalized recommendations
Continue learning
Move forward only after this module is stable.
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