Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 2068

b) when the parameters of altitude and airspeed are provided by sensors that are dedicated to the FDR system, there should be a re-calibration performed as recommended by the sensor manufacturer, or at least every two years. 2007/70/II. szám Annex 6 — Operation of Aircraft Part I 1/11/01 ATT D-4 Table D-1 Parameters for Flight Data Recorders Serial number Parameter Measurement range Recording interval (seconds) Accuracy limits (sensor input compared to FDR read-out) Time (UTC when available, otherwise elapsed time) 24 hours ±0.125% per hour Pressure-altitude –300 m (–1 000 ft) to maximum certificated altitude of aircraft +1 500 m (+5 000 ft) ±30 m to ±200 m (±100 ft to ±700 ft) Indicated airspeed 95 km/h (50 kt) to max VSo (Note 1) VSo to 1.2 VD (Note 2) ±5% ±3% Heading 360° ±2° Normal acceleration –3 g to +6 g 0.125 ±1% of maximum range excluding datum error of ±5% Pitch attitude ±75° ±2° Roll attitude ±180° ±2° Radio transmission keying On-off (one discrete) Power on each engine (Note 3) Full range 1 (per engine) ±2% Trailing edge flap or cockpit control selection Full range or each discrete position ±5% or as pilot’s indicator Leading edge flap or cockpit control selection Full range or each discrete position ±5% or as pilot’s indicator Thrust reverser position Stowed, in transit, and reverse 1 (per engine) Ground spoiler/speed brake selection Full range or each discrete position ±2% unless higher accuracy uniquely required Outside air temperature Sensor range ±2°C Autopilot/auto throttle/AFCS mode and engagement status A suitable combination of discretes Note.— The preceding 15 parameters satisfy the requirements for a Type II FDR. Longitudinal acceleration ±1 g 0.25 ±1.5% max range excluding datum error of ±5% Lateral acceleration ±1 g 0.25 ±1.5% max range excluding datum error of ±5% Pilot input and/or control surface position-primary controls (pitch, roll, yaw) (Note 4) Full range ±2° unless higher accuracy uniquely required 2007/70/II. szám Attachment D Annex 6 — Operation of Aircraft ATT D-5 1/11/01 Notes.—

Source: https://magyarkozlony.hu/hivatalos-lapok/4c6310a937d14bac566ee9c9d944896656c292dd/dokumentumok/5a6ac3c6db12e692ae41096677ad5f072d2cc9f3/letoltes