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Embraer 175 - Page 429

Embraer 175
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AIRPLANE
FLIGHT
MANUAL
APPENDIX 1
C
ONFIGURATION
DEVIATION LIST
ANAC APPROVED AP1-71
REVISION 14 code 01 Page 1
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
CONFIGURATION DEVIATION LIST
System & 1.
2. Number installed
Sequence ITEM 3. Number required for dispatch
Number 4. Remarks and/or exceptions
71 POWERPLANT
11-01 Inboard Nacelle
Strakes
2 1 One may be missing provided
the following performance
penalties are applied.
Takeoff
- Flaps retraction speed for
flaps 1 to 0 must be increased
in 10 kt.
- There are no obstacles in the
net Takeoff Flight Path above
Level Off Height.
Landing
- V
REF
is increased by 7 kt (flaps
FULL/ice condition) or by 3 kt
(all other conditions).
- A V
REF
Overspeed increment
of 7 kt (flaps FULL/ice
condition) or 3 kt (all other
conditions) must be
considered for CAFM
performance calculation.
- Landing climb weights are
reduced by 1472 lb (668 kg)
for flaps 5 or by 586 lb
(266 kg) for flaps FULL/no ice
condition or by 4475 lb
(2030 kg) for flaps FULL/ice
condition.
NOTE: - Items 57-20-01,
57-49-01 and 57-50-01
should not be missing
simultaneously with
inboard nacelle strake.
(Continued)

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