Document ID: chunk:federal_register_of_legislation:F2005B00951:body:0:p4
Version: federal_register_of_legislation:F2005B00951
Segment Type: other
Provision Reference: 
Character Range: 7512–10327

at sea level pressure altitude and a temperature of 15C; and shall be established under the following conditions:
 (a) maximum landing weight;
 (b) climb speed not to exceed the approach speed;
 (c) engine(s) operating within take-off power limitations;
 (d) landing gear extended;
 (e) wing flaps in the landing position, except that, if safe and rapid retraction to at least the take-off position is possible without causing excessive change in angle of attack or loss of altitude and without requiring exceptional piloting skill, the flaps may be retracted.

 (2) If compliance with the requirement in paragraph 3.8 (1) is conditional on wing flaps being retracted, a statement shall be included in the aeroplane flight manual detailing the procedure that shall be followed in the event of a baulked-landing manoeuvre.

 (3) It must be possible to make a safe transition to the en-route climb configuration and speed from the airspeed selected by the applicant under paragraph 3.9 (1) (b).
3.9 Landing

 (1) The landing distance shall be established and shall be the distance required to land and come to a full stop from a screen height of 50 feet above the landing surface, with:
 (a) wing flaps in the landing position; and
 (b) the aeroplane reaching the screen height at an approach speed of not less than 1.3 VSO.

 (2) The landing distance shall be that appropriate to a short dry grass surface.

 (3) It must be shown that a safe transition to the baulked landing conditions of paragraph 3.8 can be made from the conditions that exist at the 50 foot height point.
 (4) Landing charts, when included in the aeroplane flight manual, shall schedule distances established in accordance with the provisions of this paragraph, factored by 1.15.
3.10 Crosswind handling
A lateral wind velocity component at or below which it is safe to take-off and land shall be established.
3.11 Stall warning
There must be a clear and distinctive stall warning with wing flaps and landing gear in any normal position, in both straight and turning flight, sufficiently in advance of the stall to provide the pilot with adequate warning.
Note: The warning may be furnished either through inherent aerodynamic qualities of the aeroplane or by a device that will give clearly distinguishable indications under expected conditions of flight. However, a visual stall warning device that requires the attention of the crew within the cockpit is not acceptable by itself.
DESIGN AND CONSTRUCTION
3.12 Plastic, composite or fibre reinforced structural components shall be manufactured in accordance with specifications acceptable to CASA.
3.13 Wooden aeroplanes, in which the integrity of the primary structure depends on glued joints, shall not be assembled with acid catalysed phenolics and/or urea formaldehyde glues.
3.14 Cockpit