Federal Aviation Administration, DOT Pt. 135, App. F 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. Parameters Range Accuracy (sensor input) Seconds per sampling interval Resolution Remarks 56. Multi-function/ Engine Alerts Display format. Discrete(s) ......... ........................... 4 ........................ ........................... Discretes should show the display system status (e.g., off, normal, fail, and the identity of display pages for emergency procedures, need not be recorded. 57. Thrust comand 17. 58. Thrust target 59. Fuel quantity in CG trim tank. 60. Primary Navigation System Reference. Full Range ......... Section2% ................... 2 ........................ 2% of full range Full Range ......... Full Range ......... Section2% ................... Section5% ................... 4 ........................ (1 per 64 sec.) .. 2% of full range. 1% of full range. Discrete GPS, INS, VOR/ DME, MLS, Localizer Glideslope. Discrete - ice - or - no ice - . Discrete ............. ........................... 4 ........................ ........................... ........................... 4. ........................... 1. Discrete ............. ........................... 1. Discrete ............. ........................... 1. Discrete ............. ........................... 1. Full Range ......... 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. Discrete - 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. 61. Ice Detection 62. Engine warning each engine vibration. 63. Engine warning each engine over temp.. 64. Engine warning each engine oil pressure low. 65. Engine warning each engine over speed. 66. Yaw Trim Surface 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). As installed ........ Discrete - loss - or - normal - . Discrete - fail - or - normal - . ........................... 4. Section5% ................... 2 ........................ ........................... 1. ........................... 4. A suitable combination of discretes to determine the Primary Navigation System reference. To determine braking effort applied by pilots or by autobrakes. To determine braking applied by pilots. 100 psi. 533 VerDate Sep<11>2014 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00543 Fmt 8010 Sfmt 8002 Y:\SGML\247048.XXX 247048