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Load factor in a 60-degree bank

Remote Pilot (Part 107) practice question 7 of 25 on Loading and Performance. ACS element UA.IV.A.K1 · difficulty: recall. Want to answer it in a timed quiz? Use the Remote Pilot (Part 107) practice mode.

Question bank updated 2026-09-22

QUESTIONIn a coordinated, constant-altitude turn at a 60° bank, what is the load factor on any aircraft?

  1. A1.5 Gs
  2. B5.76 Gs
  3. C2 Gs
Show the answer and explanation

Correct answer: C. 2 Gs

  • A — incorrect No 1.5-G figure is given for a 60° bank; the guide states 2 Gs.
  • B — incorrect 5.76 Gs is the load factor the guide gives for an 80° bank, not 60°.
  • C — correct The guide states that the load factor for any aircraft in a coordinated level turn at 60° bank is 2 Gs.

BACKGROUND

In a coordinated, constant-altitude turn, the load factor results from two forces: centrifugal force and weight. The Remote Pilot study guide notes that the load factor increases at a terrific rate once the bank exceeds 45° or 50°. At a 60° bank the load factor in a coordinated level turn is 2 Gs, and at an 80° bank it is 5.76 Gs. The wing must produce lift equal to these load factors if altitude is to be maintained.

STUDY TIP

Memorize the two anchor values: 60° gives 2 Gs and 80° gives 5.76 Gs.

KEY POINTS

  • Load factor in a level turn comes from centrifugal force plus weight.
  • A 60° bank produces 2 Gs.
  • An 80° bank produces 5.76 Gs.

SOURCES

  • remote_pilot_study_guide.txt ch4 "Load Factors in Steep Turns"
Practice the Remote Pilot (Part 107) test →Timed 60-question exam, by ACS area, or review your misses. Free.
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SkyDrill is not affiliated with the FAA. This is an original practice item based on 14 CFR part 107, 14 CFR part 89, and the FAA Remote Pilot – Small UAS Study Guide (FAA-G-8082-22). Regulations and handbooks are revised; confirm details against the current edition.