Embraer 175 - Autopilot; Navigation;Communication Equipment; Inertial Reference System

AIRPLANE
FLIGHT
MANUAL
LIMITATIONS
ANAC APPROVED
2-56
AUTOPILOT
- Minimum Engagement Height ................................................ 400 ft
- Minimum Use Height .............................................................. 50 ft
NAVIGATION/COMMUNICATION EQUIPMENT
- TAS, TAT and SAT information are only valid above 60 KIAS.
- While transmitting in VHF1 the standby magnetic compass indication
is not valid.
- Baro altim
eter minimums must be used for all Cat I approaches.
- Back course approaches using IESS is prohibited.
- The ACARS is limited to the transmission and receipt of messages
that w
ill not create an unsafe condition if the message is improperly
received, unless they are verified per approved operational
procedures.
- For airplanes Post-Mod. SB 170-34-0035 (ADS-B Out) or equipped
wi
th an equivalent modification factory incorporated, the ADS-B Out
system complies with AMC 20-24 and was implemented according to
DO-260A, change 1 and change 2.
- For airplanes Post-Mod SB 170-34-0034 (ADS-B Out) or equipped
wi
th an equivalent modification factory incorporated, the installed
ADS-B Out system has been shown to meet the equipment
requirements of 14 CFR § 91.227.
INERTIAL REFERENCE SYSTEM
- The airplanes may be operated within the North and South magnetic
polar cut-out regions specified in the table below, but IRS magnetic
heading and track angle magnetic data will not be available.
MAGNETIC
CUT-OUT
REGIONS
LATITUDE LONGITUDE
Between 73.125°N
and 82°N
Between 80°W and
130°W
North
North of 82°N Between 0° and 180°W/E
(Continued on the next page)
AFM-1385
REVISION 12 code 01 Page 1