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… A , B , C , D , E SUBCHAPTER F - EQUIPMENT General 529.1301 Function and Installation Each item of … and signal. Electrical Systems and Equipment 529.1351 General (a) Electrical system capacity. The required … location. 529.1385 Position Light System Installation (a) General. Each part of each position light system shall meet …
43.407
… and changes to those type certificates, for transport category rotorcraft. (b) Transport category rotorcraft shall be certificated in accordance with … shall be met in order to comply with section 605.24(4) of the Canadian Aviation Regulations which requires the …
37.995
… operation. The powerplant take-off operation shall be limited by: (1) the maximum rotational speed which shall not … Continuous operation. The continuous operation shall be limited by: (1) the maximum rotational speed, which shall not … the 30-second OEI limit. (amended 1995/03/25) 529.1551 Oil Quantity Indicator Each oil quantity indicator shall be …
70.912
… directional control suddenly to the maximum deflection limited by the control stops or by the maximum pilot force … directional control suddenly to the maximum deflection limited by the control stops or by the maximum pilot force … Items of mass to be considered include, but are not limited to, rotors, transmission, and engines. The items of …
39.014
… no engine or fuel pump can draw fuel from more than one tank at a time; or (2) there are means to prevent introducing … (amended 1995/06/05) (a) Drop test requirements. Each tank, or the most critical tank, shall be drop-tested as follows: (amended 1995/06/05) …
44.252
… the flight deck pitch control in the initial direction, as limited by the control system stops, control surface stops, … as a function of time. In the initial direction, δ(t) is limited to . In the reverse direction, δ(t) may be truncated … investigated to find the critical response for each load quantity. (4) The design gust velocity must be: U ds = U ref …
45.631