Pt. 125, App. E 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. Accuracy (sensor input) Seconds per sampling interval ........................... 1 ........................ ........................... 1 ........................ Section3% Unless Higher Accuracy Uniquely Required. Section3% Unless Higher Accuracy Uniquely Required. Section5% ................... 2 ........................ 0.3% of full range.. 2 ........................ 0.3% of full range.. 1 ........................ ........................... Discrete or Analog - applied - or - off - . Full Range ......... Section5% (Analog) .... 1 ........................ ........................... Section5% ................... 1 ........................ 0,5Section. ................... Decrete - open - or - closed - . Discrete - on - or - off - . ........................... 4 ........................ ........................... ........................... 4 ........................ ........................... Full Range ......... Section5% ................... (1 per 64 sec.) .. 1% of full range. Discrete - power - or - off - . Discrete - power - or - off - . Discrete - open - or - closed. Full range .......... ........................... 4 ........................ ........................... Each bus. ........................... 4 ........................ ........................... Each bus. Parameters Range 64. Engine warnDiscrete ............. ing each engine oil pressure low. 65. Engine warnDiscrete ............. ing each engine over speed. 66. Yaw Trim Sur- Full Range ......... face Position. 67. Roll Trim Surface Position. Full Range ......... 68. Brake Pressure (left and right). 69. Brake Pedal Application (left and right). 70. Yaw or sideslip angle. 71. Engine bleed valve position. 72. De-icing or anti-icing system selection. 73. Computed center of gravity. 74. AC electrical bus status. 75. DC electrical bus status. 76. APU bleed valve position. 77. Hydraulic Pressure (each system). 78. Loss of cabin pressure. 79. Computer failure (critical flight and engine control systems). 80. Heads-up display (when an information source is installed). 81. Para-visual display (when an information source is installed). 82. Cockpit trim control input position - pitch. As installed ........ 83. Cockpit trim control input position - roll. Resolution ........................... 4. ....................... Section5% ................... 2 ........................ Discrete - loss - or - normal - . Discrete - fail - or - normal - . ........................... 1. ....................... ........................... 4. ....................... Discrete(s) - on - or - off - . ........................... 4. ....................... Discrete(s) - on - or - off - . ........................... 1. ....................... Full Range ......... Section5% ................... 1 ........................ 0.2% of full range. Full Range ......... Section5% ................... 1 ........................ 0.7% of full range. Remarks To determine braking effort applied by pilots or by autobrakes. To determine braking applied by pilots. 100 psi. Where mechanical means for control inputs are not available, cockpit display trim positions should be recorded. Where mechanical means for control inputs are not available, cockpit display trim position should be recorded. 376 VerDate Sep<11>2014 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00386 Fmt 8010 Sfmt 8002 Y:\SGML\247048.XXX 247048