Text in force at CAR3R-8: from CAR3R-0, effective 15 May 1956. OCR text
specified in §3.75 lies beyond (a) the extremes selected by the applicant, or (b) the extremes for which the structure has been proven, or (c) the extremes for which compliance with all functional requirements were demonstrated, loading instructions shall be provided in the Airplane Flight Manual as specified in § 3.777-3.780. PERFORMANCE REQUIREMENTS GENERAL §3.80 Alternate performance requirements. The provisions of §§ 3.84, 3.85, 3.86, and 3.112 (a) (2) (ii) shall not be applicable to airplanes having a maximum certificated take-off weight of 6,000 pounds or less. In lieu thereof, such airplanes shall comply with the provisions of §§ 3.84a, 3.85a, 3.87, and 3.112 (c).