SUPPLEMENTARY
PROCEDURES
NAVIGATION
AIRPLANE
OPERATIONS
MANUAL
1-02-80
Page
16
Code
02
REVISION 40
AOM-145/1114
The airplane is compliant with AC 90-100A (RNAV 1 and RNAV 2) and
with TGL-10 (P-RNAV and B-RNAV).
RNAV SPECIFICATIONS
Operation
Sensors that
may be used
Guidance
FAA
Guidance
EASA
RNAV 10
(RNP 10)
(1)
2 GNSS (2) Order
8400.12A
Order
8400.12A
RNAV 5
GNSS
DME/DME
VOR/DME
AC 90-96A
(3a)
AMC 20-4
(3b)
RNAV 2 GNSS (2) AC 90-100A -
RNAV 1 GNSS (2) AC 90-100A
TGL 10
(P-RNAV)
(1) Dual FMS is required.
(2) Off Line RAIM prediction is required.
(3a) According to AC 90-96A, the airplane should be considered
eligible for B-RNAV/RNAV 5 operations if the AFM shows the
appropriate instrument flight rules (IFR) navigation system installation
has received airworthiness approval in accordance with the current
edition of AC 20-130. According to AFM, the EMB-145 RNAV system
installation is compliant with AC 20-130A.
(3b) AMC 20-4 defines that installations in accordance with AC 20-
130() is an acceptable means of compliance for Basic RNAV systems,
with no further substantiation. According to AFM, the EMB-145 RNAV
system installation is compliant with AC 20-130A.
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