AIRPLANE
OPERATIONS
MANUAL
LIMITATIONS
REVISION 41
1-01-82
Page
1
Code
02
Copyright © by Embraer. Refer to cover page for details.
HGS OPERATION
SYSTEM CAPABILITY LIMITATIONS
DEMONSTRATED MINIMUM VISIBILITY TAKEOFF LIMITS
Runway Visual Range (RVR)........................................ 75 m
DEMONSTRATED MINIMUM AIII MODE LIMITS
Decision Height (DH).................................................... 50 ft
Runway Visual Range (RVR)........................................ 180 m
WIND COMPONENTS
For Low Visibility Takeoff operations the following wind components
must not be exceeded:
Headwind................................................................. 25 kt
Tailwind.................................................................... 10 kt
Crosswind................................................................ 15 kt
For AIII mode operations the following wind components must not be
exceeded:
Headwind................................................................. 25 kt
Tailwind.................................................................... 10 kt
Crosswind................................................................ 15 kt
AIII mode operations initiated with one engine inoperative has been
demonstrated and following wind components must not be exceeded:
Headwind................................................................. 25 kt
Tailwind.................................................................... 10 kt
Crosswind................................................................ 11 kt
NOTE: The maximum wind limits listed above include gusts.