Appendix C to Part 135 - Helicopter Flight Recorder Specifications  


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  • Appendix C to Part 135 - Helicopter Flight Recorder Specifications

    Parameters Range Installed system1 minimum accuracy (to recovered data) Sampling interval (per second) Resolution3 read out
    Relative time (from recorded on prior to takeoff) 25 hr minimum ±0.125% per hour 1 1 sec.
    Indicated airspeed Vm in to VD (KIAS) (minimum airspeed signal attainable with installed pilot-static system) ±5% or ±10 kts., whichever is greater 1 1 kt.
    Altitude −1,000 ft. to 20,000 ft. pressure altitude ±100 to ±700 ft. (see Table 1, TSO C51-a) 1 25 to 150 ft.
    Magnetic heading 360° ±5° 1 1°.
    Vertical acceleration −3g to + 6g ±0.2g in addition to ±0.3g maximum datum 4 (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% 2 0.03g.
    Pitch attitude 100% of usable range ±2° 1 0.8°.
    Roll attitude ±60° or 100% of usable range, whichever is greater ±2° 1 0.8°.
    Altitude rate ±8,000 fpm ±10% Resolution 250 fpm below 12,000 ft. indicated 1 250 fpm below 12,000.
    Engine Power, Each Engine
    Main rotor speed Maximum range ±5% 1 1%2
    Free or power turbine Maximum range + 5% 1 1%2
    Engine torque Maximum range ±5% 1 1%2
    Flight Control - Hydraulic Pressure
    Primary (discrete) High/low 1
    Secondary - if applicable (discrete) High/low 1
    Radio transmitter keying (discrete) On/off 1
    Autopilot engaged (discrete) Engaged or disengaged 1
    SAS status - engaged (discrete) Engaged/disengaged 1
    SAS fault status (discrete) Fault/OK 1
    Flight Controls
    Collective4 Full range ±3% 2 1%2
    Pedal Position4 Full range ±3% 2 1%2
    Lat. Cyclic4 Full range ±3% 2 1%2
    Long. Cyclic4 Full range ±3% 2 1%2
    Controllable Stabilator Position4 Full range ±3% 2 1%2

    [Doc. No. 25530, 53 FR 26152, July 11, 1988; 53 FR 30906, Aug. 16, 1988, as amended by Amdt. 135-69, 62 FR 38397, July 17, 1997; Amdt. 135-113, 73 FR 12570, Mar. 7, 2008; 73 FR 15281, Mar. 21, 2008; Amdt. 135-121, 75 FR 17047, Apr. 5, 2010]