Civil Aviation Order 20.7.1B - Aeroplane weight & performance limitations - Aeroplanes above 5 700kg - All operations (turbine & piston-engined) (02/12/2004) (Cth)

Civil Aviation Order 20.7.1B – Aeroplane weight and performance limitations – specified aeroplanes above 5 700 kg, or 2 722 kg if driven by 2 or more jet engines – all operations as amended

made under subregulation 235 (2) of the Civil Aviation Regulations 1988. This compilation was prepared on 28 May 2014 taking into account amendments up to Civil Aviation Order 20.7.1B Amendment Instrument 2014 (No. 1). Prepared by the Legislative Drafting Section, Legal Branch, Legal Services Division, Civil Aviation Safety Authority, Canberra.

Contents Page

2...Application........................................................ 3...Definitions........................................................ 4...Take-off weight limitations............................................. 5...Landing weight limitations............................................. 6...Accelerate-stop and take-off distance required.............................. 7...Take-off climb performance............................................ 8...En-route climb performance............................................ 9...Approach climb performance........................................... 10..Landing climb performance............................................ 11..Landing distance required............................................. 12..Obstacle clearance requirements........................................ 12A.Alternative take-off area requirements.................................... 14..Aeroplane configuration and procedures................................... Notes to Civil Aviation Order 20.7.1B.....................................

Section 20.7.1B Civil Aviation Order 20.7.1B – Aeroplane weight and performance limitations – specified aeroplanes above 5 700 kg, or 2 722 kg if driven by 2 or more jet engines – all operations