Embraer 190 - Page 359

AIRPLANE
FLIGHT
MANUAL
SUPPLEMENT 1
COMPUTERIZED AFM
ANAC APPROVED S1-05
REVISION 12 code 06 Page 1
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1912
LIMITATIONS
CAFM-195-FAA-002
CAFM-195-FAA-002 is constituted by specific Software Module part
numbers and Engine Database to allow performance calculations for
airplanes with the following configuration:
− EMBRAER 195 airplanes.
− CF34-10E6A1 engines.
WARNING: • CAFM VERSION MUST BE IN ACCORDANCE WITH
AIRPLANE CONFIGURATION.
• VERSIONS NOT PRESENTED IN THIS
SUPPLEMENT ARE AUTOMATICALLY
CANCELLED AND MUST NOT BE USED.
• THE CAFM CG ENVELOPE OPTION MUST
ALWAYS BE SET TO STANDARD, UNLESS
OTHERWISE STATED IN THE AFM LIMITATIONS
SECTION.
• THE CAFM TIRES MODEL OPTION MUST ALWAYS
BE SET TO BIAS. THE RADIAL OPTION MUST BE
SET ONLY WHEN OPERATING IN ACCORDANCE
WITH THE LIMITATIONS AND PROCEDURES
DESCRIBED IN SUPPLEMENT 11 RADIAL TIRES
PERFORMANCE.
• AIRPLANES PRE-MOD. SB 190-31-0015 (LOAD
21.2) MUST SELECT FIXED V
2
/V
S
OPTION AND
MUST USE ON
E OF THE FOLLOWING VALUES:
FLAPS POSITION
1 2 3 4
V
2
/V
S
1.18 1.17 1.17 1.21
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