Pt. 135, App. F 14 CFR Ch. I (1-1-19 Edition) The recorded values must meet the designated range, resolution and accuracy requirements during static and dynamic conditions. Dynamic condition means the parameter is experiencing change at the maximum rate attainable, including the maximum rate of reversal. All data recorded must be correlated in time to within one second. Range Accuracy (sensor input) Seconds per sampling interval 14a. Yaw control position(s) (nonfly-bywire) 5 18. Full Range ......... Section2Section unless higher accuracy uniquely required. 0.5 ..................... 0.3% of full range. 14b. Yaw control position(s) (flyby-wire) 18. Full Range ......... 0.5 ..................... 0.2% of full range. 15. Pitch control surface(s) position 6 18. Full Range ......... Section2Section unless higher accuracy uniquely required. Section2Section unless higher accuracy uniquely required. 0.5 or 0.25 for airplanes operated under Section 135.152(j).. 0.3% of full range. 16. Lateral control surface(s) position 7 18. Full Range ......... Section2Section unless higher accuracy uniquely required. 0.5 or 0.25 for airplanes operated under Section 135.152(j). 0.2% of full range. 17. Yaw control surface(s) position 8 18. Full Range ......... Section2Section unless higher accuracy uniquely required. 0.5 ..................... 0.2% of full range. 18. Lateral Acceleration. Section1g .................... 0.25 ................... 0.004g. 19. Pitch Trim Surface Position. Full Range ......... 1 ........................ 0.6% of full range 20. Trailing Edge Flap or Cockpit Control Selection 10. Full Range or Each Position (discrete). Section1.5% max. range excluding datum error of Section5%. Section3Section Unless Higher Accuracy Uniquely Required. Section3Section or as Pilot-s Indicator. 2 ........................ 0.5% of full range. 21. Leading Edge Flap or Cockpit Control Selection 11. Full Range or Each Discrete Position. 2 ........................ 0.5% of full range. 22. Each Thrust reverser Position (or equivalent for propeller airplane). Stowed, In Transit, and reverse (Discrete). Section3Section or as Pilot-s Indicator and sufficient to determine each discrete position. ........................... 1 (per engine ..... ........................... Parameters Resolution Remarks For airplanes that have a flight control breakaway capability that allows either pilot to operate the controls independently, record both control inputs. The control inputs may be sampled alternately once per second to produce the sampling of 0.5 or 0.25, as applicable. For airplanes fitted with multiple or split surfaces, a suitable combination of inputs is acceptable in lieu of recording each surface separately. The control surfaces may be sampled alternately to produce the sampling interval of 0.5 or 0.25, as applicable. A suitable combination of surface position sensors is acceptable in lieu of recording each surface separately. The control surfaces may be sampled alternately to produce the sampling interval of 0.5 or 0.25, as applicable. For airplanes with multiple or split surfaces, a suitable combination of surface position sensors is acceptable in lieu of recording each surface separately. The control surfaces may be sampled alternately to produce the sampling interval of 0.5. Flap position and cockpit control may each be sampled alternately at 4 second intervals, to give a data point every 2 seconds. Left and right sides, of flap position and cockpit control may each be sampled at 4 second intervals, so as to give a data point to every 2 seconds. Turbo-jet - 2 discretes enable the 3 states to be determined Turbo-prop - 1 discrete 530 VerDate Sep<11>2014 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00540 Fmt 8010 Sfmt 8002 Y:\SGML\247048.XXX 247048