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CLEAN CONFIGURATION : 4-2.5gtO-1 g g\i-gkFI CONFIGURATION : + 2 g to I g
HOLDING
(SLATS EXTENDED)
D. Operating performance limitations :
(7) Environmental envelope
I
0
0 - U
0
.o
N0
0
I U 0
U Y
Y0
m
(2) Airport Operation limitations
RUNWAY SLOPE (MEAN) . . . . . . . . . . . f 2 %
Runway altitude ................... 8500 ft
WIND :
.TAIL WlND COMPONENT (TAKE-OFF AND . LANDING). .................... 1Okt . CROSS WIND (TAKE OFF AND LANDING) : R ...
maximum demonstrated on dry and wet R 2 )
runway,, ...................... 32kt R x *...
Max wind for passenger and cargo doors
operation ........................ 60kt
Mod : 7007 or (Mod : 7007/PW 4158)
us
@A30@600
FUQHT CREW OPERATINO MANUAL I
1. SYMBOLOGY AND DEFINITIONS
PROCEDURES AND TECHNIQUES 1 2.02.01
GENERAL PAGE 1 I
OPERATING SPEEDS
- vs
................. ........... .................................................................................... ............................_............................................................ ........................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................................... ........ ...........................................................................................-.-............. ......... ................................................. ..... ...................................................................................................................................................................................................................................................................................................................................................................................................................................................................... .................................................................................................................................................................................................................................................... .................................................................................................................................................................................................................................. ...................................................................... .... ... ....... ...... .
' ............................................................................................................................................................... .. ....................................................
. , R -VMCG
R
R
R
R - v1
- VR
- v2
- VMCA
- F
.-:. , .
: Minimum stalling s eed for a specified
configuration, It is a tnction of the aircraft
weight and altitude.
: Minimum control speed on round at which
Primary flight controls only, in case of a sudden.
ailure of the critical engine (the other engine
remaining at takeoff power).
: Speed at which the pilot can make the decision,
following failure of critical engine :
either to continue take-off
or to stop the aircraft.
Represented by u 1 m on airspeed scale (or V1
value when out of range).
: Speed at which rotation is initiated to reach V2
at an altitude of 35 feet.
: Take-off safety speed reached before the
altitude 35 feet with one engine failed.
Represented by the SPEED SELECT symbol on
airspeed scale as any speed selected on FCU.
: Minimum control speed In flight at which
aircraft can be controlled with 5" max bank, in
　
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