439 

Federal Aviation Administration, DOT 

§ 135.152 

(26) Radio altitude (when an informa-

tion source is installed); 

(27) Localizer deviation, MLS Azi-

muth; 

(28) Glideslope deviation, MLS Ele-

vation; 

(29) Marker beacon passage; 
(30) Master warning; 
(31) Air/ground sensor (primary air-

plane system reference nose or main 
gear); 

(32) Angle of attack (when informa-

tion source is installed); 

(33) Hydraulic pressure low (each sys-

tem); 

(34) Ground speed (when an informa-

tion source is installed); 

(35) Ground proximity warning sys-

tem; 

(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 in-

formation 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 avoid-

ance system; 

(45) DME 1 and 2 distances; 
(46) Nav 1 and 2 selected frequency; 
(47) Selected barometric setting 

(when an information source is in-
stalled); 

(48) Selected altitude (when an infor-

mation source is installed); 

(49) Selected speed (when an informa-

tion source is installed); 

(50) Selected mach (when an informa-

tion source is installed); 

(51) Selected vertical speed (when an 

information source is installed); 

(52) Selected heading (when an infor-

mation source is installed); 

(53) Selected flight path (when an in-

formation source is installed); 

(54) Selected decision height (when 

an information source is installed); 

(55) EFIS display format; 
(56) Multi-function/engine/alerts dis-

play format; 

(57) Thrust command (when an infor-

mation source is installed); 

(58) Thrust target (when an informa-

tion source is installed); 

(59) Fuel quantity in CG trim tank 

(when an information source is in-
stalled); 

(60) Primary Navigation System Ref-

erence; 

(61) Icing (when an information 

source is installed); 

(62) Engine warning each engine vi-

bration (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 in-
stalled); 

(72) De-icing or anti-icing system se-

lection (when an information source is 
installed); 

(73) Computed center of gravity 

(when an information source is in-
stalled); 

(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 sys-

tem); 

(78) Loss of cabin pressure; 
(79) Computer failure; 
(80) Heads-up display (when an infor-

mation source is installed); 

(81) Para-visual display (when an in-

formation source is installed); 

(82) Cockpit trim control input posi-

tion—pitch; 

(83) Cockpit trim control input posi-

tion—roll; 

(84) Cockpit trim control input posi-

tion—yaw; 

(85) Trailing edge flap and cockpit 

flap control position; 

(86) Leading edge flap and cockpit 

flap control position; 

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