Source: https://www.law.cornell.edu/cfr/text/14/part-27/subpart-B
Timestamp: 2016-07-23 13:24:01
Document Index: 312975350

Matched Legal Cases: ['art 27', 'art 27', 'art 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27', '§ 27']

14 CFR Part 27, Subpart B - Flight | US Law | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 27 › Subpart B 14 CFR Part 27, Subpart B - Flight
§ 27.21 — Proof of compliance.
§ 27.25 — Weight limits.
§ 27.27 — Center of gravity limits.
§ 27.29 — Empty weight and corresponding center of gravity.
§ 27.31 — Removable ballast.
§ 27.33 — Main rotor speed and pitch limits.
§ 27.45 — General.
§ 27.49 — Performance at minimum operating speed.
§ 27.51 — Takeoff.
§ 27.65 — Climb: all engines operating.
§ 27.67 — Climb: one engine inoperative.
§ 27.71 — Autorotation performance.
§ 27.75 — Landing.
§ 27.87 — Height-speed envelope.
§ 27.141 — General.
§ 27.143 — Controllability and maneuverability.
§ 27.151 — Flight controls.
§ 27.161 — Trim control.
§ 27.171 — Stability: general.
§ 27.173 — Static longitudinal stability.
§ 27.175 — Demonstration of static longitudinal stability.
§ 27.177 — Static directional stability.
§ 27.231 — General.
§ 27.235 — Taxiing condition.
§ 27.239 — Spray characteristics.
§ 27.241 — Ground resonance.
§ 27.251 — Vibration.