JAR OPS 1 regulation
List of paremeters to be recorded by Aeroplanes with a maximum take-off mass of greater than 5700kg, first issued with an individual Certificate of Airworthiness (either in a JAA Member State or elsewhere) on or after 1 April 1998. (From Appendix 1 to JAR-OPS 1.715)
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| - Time or relative time count
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| - Manual radio transmission keying
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| - Propulsive thrust/power on each engine and cockpit thrust/power lever position if applicable
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| - Trailing edge flap or cockpit control selection
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| - Leading edge flap or cockpit control selection
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| - Ground spoiler position and/or speed brake selection
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| - Total or outside air temperature
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| - Autopilot, autothrottle and AFCS mode and engagement status
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| - Longitudinal acceleration (Body axis)
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Additional parameters for aeroplanes with a maximum certificated take-off mass over 27000kg
| - Primary flight controls - Control surface position and/or pilot input (pitch, roll, yaw)
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| - Vertical beam deviation (ILS Glide path or MLS Elevation)
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| - Horizontal beam deviation (ILS Localiser or MLS Azimuth)
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| - Navigation receiver frequency (recommended)
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| - DME distance (recommended)
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| - Landing gear squat switch status or air/ground status
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| - Ground proximity Warning System
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| - Low pressure warning (hydraulic and pneumatic power)
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| - Landing gear or gear selector position
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Aeroplanes equipped with electronic display systems
| - Selected barometric setting (each pilot station)
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| - Multi function/engine/alerts display format
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