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Embraer EMB145 - Page 168

Embraer EMB145
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AIRPLANE
OPERATIONS
MANUAL
LIMITATIONS
FAA
REVISION 40
1-01-60
Page
5
Code
02
AOM-145/1114
RNP-10 - REQUIRED NAVIGATION PERFORMANCE
The dual FMZ2000 installation with dual Global Positioning System
(GPS) sensors as installed has been found to comply with the
requirements of FAA Order 8400.12A, as amended, as a primary
means of navigation with no time limitation, when used in
conjunction with Honeywell Off Line RAIM prediction program.
The dual FMZ2000 installation with dual Inertial Reference
Systems (IRS) as installed has been found to comply with the
requirements of FAA Order 8400.12A, as amended, as a primary
means of navigation for flights up to 6.2 hours after the system is
placed in the navigation mode.
The dual FMZ2000 installation with dual Global Positioning System
(GPS) sensors and dual Inertial Reference Systems (IRS) as
installed has been found to comply with the requirements of FAA
Order 8400.12A, as amended, as a primary means of navigation
with no time limitation.
ENROUTE AND TERMINAL
In accordance with AC 20-130A and TSO C129a C1 provided it is
receiving usable signals from:
One VOR/DME or multiple DME's;
GPS.

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