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Code · CFR · Title 14 — Aeronautics and Space · Part 194 — Special Federal Aviation Regulation No. 120—Powered-Lift: Pilot Certification and Training; Operations Requirements · § 194.310

§ 194.310. Powered-lift in vertical-lift flight mode, flight recorder specifications under part 91 of this chapter.

255 words·~1 min read·/us/cfr/t14/s§ 194.310·

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Table 1 to § 194.310 Parameters Range Installed system 1 minimum accuracy (to recovered data) Sampling interval (per second) Resolution 3 read out Relative Time (From Recorded on Prior to Takeoff)4 hr minimum±0.125% per hour11 sec. Indicated AirspeedVM in to VD
(KIAS)(minimum airspeed signal attainable with installed pilot-static system)±5% or ±10 kts., whichever is greater11 kt. Altitude−1,000 ft. to 20,000 ft. pressure altitude±100 to ±700 ft. (see Table 1, TSO C51-a)125 to 150 ft. Magnetic Heading360°±5°11° Vertical Acceleration−3g to + 6g±0.2g in addition to ±0.3g maximum datum4 (or 1 per second where peaks, ref. to 1g are recorded)0.05g. Longitudinal Acceleration±1.0g±1.5% max. range excluding datum error of ±5%20.03g. Pitch Attitude100% of usable range±2°10.8°. Roll Attitude±60 or 100% of usable range, whichever is greater±2°10.8°. Altitude Rate±8,000 fpm±10% Resolution 250 fpm below 12,000 ft. indicated1250 fpm below 12,000. Engine Power, Each Engine: Main Rotor SpeedMaximum Range±5%11%. 2 Free or Power TurbineMaximum Range±5%11%. 2 Engine TorqueMaximum Range±5%11%. 2 Flight Control Hydraulic Pressure: Primary (Discrete)High/Low1 Secondary—if applicable (Discrete)High/Low1 Radio Transmitter Keying (Discrete)On/Off1 Autopilot Engaged (Discrete)Engaged or Disengaged1 SAS Status-Engaged (Discrete)Engaged or Disengaged1 SAS Fault Status (Discrete)Fault/OK1 Flight Controls: Pilot Inputted—Primary Controls (I.E. Ascent, descent, acceleration, and deceleration, heading and directional control for all axis)Full range±3%21%. 2 Controllable Stabilator PositionFull range±3%21%. 2 1 When data sources are aircraft instruments (except altimeters) of acceptable quality to fly the aircraft the recording system excluding these sensors (but including all other characteristics of the recording system) shall contribute no more than half of the values in this column. 2 Percent of full range.
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