Federal Aviation Administration, DOT

Section 135.152

(26) Radio altitude (when an information source is installed);
(27) Localizer deviation, MLS Azimuth;
(28) Glideslope deviation, MLS Elevation;
(29) Marker beacon passage;
(30) Master warning;
(31) Air/ground sensor (primary airplane system reference nose or main
gear);
(32) Angle of attack (when information source is installed);
(33) Hydraulic pressure low (each system);
(34) Ground speed (when an information source is installed);
(35) Ground proximity warning system;
(36) Landing gear position or landing
gear cockpit control selection;
(37) Drift angle (when an information
source is installed);
(38) Wind speed and direction (when
an information source is installed);
(39) Latitude and longitude (when an
information source is installed);
(40) Stick shaker/pusher (when an information source is installed);
(41) Windshear (when an information
source is installed);
(42) Throttle/power lever position;
(43) Additional engine parameters (as
designated in appendix F of this part);
(44) Traffic alert and collision avoidance system;
(45) DME 1 and 2 distances;
(46) Nav 1 and 2 selected frequency;
(47) Selected barometric setting
(when an information source is installed);
(48) Selected altitude (when an information source is installed);
(49) Selected speed (when an information source is installed);
(50) Selected mach (when an information source is installed);
(51) Selected vertical speed (when an
information source is installed);
(52) Selected heading (when an information source is installed);
(53) Selected flight path (when an information source is installed);
(54) Selected decision height (when
an information source is installed);
(55) EFIS display format;
(56) Multi-function/engine/alerts display format;
(57) Thrust command (when an information source is installed);

(58) Thrust target (when an information source is installed);
(59) Fuel quantity in CG trim tank
(when an information source is installed);
(60) Primary Navigation System Reference;
(61) Icing (when an information
source is installed);
(62) Engine warning each engine vibration (when an information source is
installed);
(63) Engine warning each engine over
temp. (when an information source is
installed);
(64) Engine warning each engine oil
pressure low (when an information
source is installed);
(65) Engine warning each engine over
speed (when an information source is
installed;
(66) Yaw trim surface position;
(67) Roll trim surface position;
(68) Brake pressure (selected system);
(69) Brake pedal application (left and
right);
(70) Yaw or sideslip angle (when an
information source is installed);
(71) Engine bleed valve position
(when an information source is installed);
(72) De-icing or anti-icing system selection (when an information source is
installed);
(73) Computed center of gravity
(when an information source is installed);
(74) AC electrical bus status;
(75) DC electrical bus status;
(76) APU bleed valve position (when
an information source is installed);
(77) Hydraulic pressure (each system);
(78) Loss of cabin pressure;
(79) Computer failure;
(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;
(83) Cockpit trim control input position - roll;
(84) Cockpit trim control input position - yaw;
(85) Trailing edge flap and cockpit
flap control position;
(86) Leading edge flap and cockpit
flap control position;

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