15* Autopilot/auto A suitable 1 throttle/AFCS mode and combination of engagement status discretes 16 Longitudinal acceleration +/-1 g 0.25 ±0.015 g excluding a 0.004 g (Note 3) datum error of ±0.05 g 17 Lateral acceleration ±1 g 0.25 ±0.015 g excluding 0.004 g (Note 3) a datum error of ±0.05 g 18 Pilot input and/or control Full range ±0.25 ±2˚ unless higher 0.2% of full surface position-primary accuracy uniquely range or as controls (pitch, roll, yaw) required installed (Note 5) (Note 6) 19 Pitch trim position Full range 1 ±3% unless higher 0.3% of full accuracy range or as uniquely required installed 20* Radio altitude– -6 m to 750 m 1 ±0.6 m (±2 ft) or 0.3 m (1 ft) (–20 ft to 2 500 ft) ±3% whichever is below 150 m greater below 150 m (500 ft); 0.3 m (500 ft) and ±5% (1 ft) + 0.5% of above 150 m (500 ft) full range above 150 m (500 ft) 21* Vertical beam deviation Signal range 1 ±3% 0.3% of full (ILS/GPS/GLS glide range path, MLS elevation, IRNAV/IAN vertical deviation) 22* Horizontal beam Signal range 1 ±3% 0.3% of full deviation (ILS/GPS/GLS range localizer, MLS azimuth, lateral deviation) 23 Marker beacon passage Discrete 1 24 Master warning Discrete 1 25 NAV receiver frequency Full range 4 As installed selection (Note 7) 26* DME 1 and 2 distance 0 370 km 4 As installed 1852 m – (includes Distance to (0-200 NM) (1 NM) runway threshold (GLS) and Distance to missed approach (IRNAV/IAN) (Notes 7 and 8 27 Air/ground status Discrete 1 28* GPWS/TAWS/GCAS Discrete 1 status (selection of terrain display mode including pop-up display status) and (Terrain alerts, both cautions and warnings, and
15* Autopilot/auto throttle/AFCS mode and engagement status A suitable combination of discretes 1 16 Longitudinal acceleration (Note 3) +/-1 g 0.25 ±0.015 g excluding a datum error of ±0.05 g 0.004 g 17 Lateral acceleration (Note 3) ±1 g 0.25 ±0.015 g excluding a datum error of ±0.05 g 0.004 g 18 Pilot input and/or control surface position-primary controls (pitch, roll, yaw) (Note 5) (Note 6) Full range ±0.25 ±2˚ unless higher accuracy uniquely required 0.2% of full range or as installed 19 Pitch trim position Full range 1 ±3% unless higher accuracy uniquely required 0.3% of full range or as installed 20* Radio altitude– -6 m to 750 m (–20 ft to 2 500 ft) 1 ±0.6 m (±2 ft) or ±3% whichever is greater below 150 m (500 ft) and ±5% above 150 m (500 ft) 0.3 m (1 ft) below 150 m (500 ft); 0.3 m (1 ft) + 0.5% of full range above 150 m (500 ft) 21* Vertical beam deviation (ILS/GPS/GLS glide path, MLS elevation, IRNAV/IAN vertical deviation) Signal range 1 ±3% 0.3% of full range 22* Horizontal beam deviation (ILS/GPS/GLS localizer, MLS azimuth, lateral deviation) Signal range 1 ±3% 0.3% of full range 23 Marker beacon passage Discrete 1 24 Master warning Discrete 1 25 NAV receiver frequency selection (Note 7) Full range 4 As installed 26* DME 1 and 2 distance (includes Distance to runway threshold (GLS) and Distance to missed approach (IRNAV/IAN) (Notes 7 and 8 0 – 370 km (0-200 NM) 4 As installed 1852 m (1 NM) 27 Air/ground status Discrete 1 28* GPWS/TAWS/GCAS status (selection of terrain display mode including pop-up display status) and (Terrain alerts, both cautions and warnings, and Discrete 1
07_MCAR_Part-7_and_IS_V2.8.docx