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. Parameters Range Accuracy (sensor input) Seconds per sampling interval Resolution 36. Landing Gear Position or Landing gear cockpit control selection. 37. Drift Angle 15 38. Wind Speed and Direction. 39. Latitude and Longitude. Discrete ............. ........................... 4 ........................ ........................... As installed ........ As installed ........ As installed ........ As installed ........ 4 ........................ 4 0.1Section 1 knot, and 1.0Section. As installed ........ As installed ........ 4 ........................ 0.002Section, or as installed. 40. Stick shaker and pusher activation. 41. Windshear Detection. 42. Throttle/power lever position 16. Discrete(s) - on - or - off - . ........................... 1 ........................ ........................... Discrete - warning - or - off - . Full Range ......... ........................... 1. Section2% ................... 1 for each lever 2% of full range 43. Additional Engine Parameters. As installed ........ As installed ........ Each engine each second. 2% of full range 44. Traffic Alert and Collision Avoidance System (TCAS). Discretes ........... As installed ........ 1 ........................ ........................... 45. DME 1 and 2 Distance. 46. Nav 1 and 2 Selected Frequency. 47. Selected barometric setting. 48. Selected altitude. 49. Selected speed. 50. Selected Mach. 51. Selected vertical speed. 52. Selected heading. 53. Selected flight path. 54. Selected decision height. 55. EFIS display format. 0-200 NM; ........ As installed ........ 4 ........................ 1 NM ................. Full range .......... As installed ........ 4 ........................ ........................... Full Range ......... Section5% ................... (1 per 64 sec.) .. Full Range ......... Section5% ................... 1 ........................ 0.2% of full range. 100 ft. Full Range ......... Section5% ................... 1 ........................ 1 knot. Full Range ......... Section5% ................... 1 ........................ .01. Full Range ......... Section5% ................... 1 ........................ 100 ft./min. Full Range ......... Section5% ................... 1 ........................ 1Section. Full Range ......... Section5% ................... 1 ........................ 1Section. Full Range ......... Section5% ................... 64 ...................... 1 ft. Discrete(s) ......... ........................... 4 ........................ ........................... Remarks A suitable combination of discretes should be recorded. Provided by the Primary Navigation System Reference. Where capacity permits latitude/longitude resolution should be 0.0002Section. A suitable combination of discretes to determine activation. For airplanes with non-mechanically linked cockpit engine controls. Where capacity permits, the preferred priority is indicated vibration level, N2, EGT, Fuel Flow, Fuel Cutoff lever position and N3, unless engine manufacturer recommends otherwise. A suitable combination of discretes should be recorded to determine the status of - Combined Control, Vertical Control, Up Advisory, and down advisory. (ref. ARINC Characteristic 735 Attachment 6E, TCAS VERTICAL RA DATA OUTPUT WORD.) 1 mile. Sufficient to determine selected frequency. Discretes should show the display system status (e.g., off, normal, fail, composite, sector, plan, nav aids, weather radar, range, copy. 532 VerDate Sep<11>2014 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00542 Fmt 8010 Sfmt 8002 Y:\SGML\247048.XXX 247048