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even including below VA.
ROUGH AIR PENETRATION SPEED (VRA)
VRA.................................................................................................. 265 KIAS/0.75 MI
MAXIMUM LANDING GEAR OPERATING SPEED — RETRACTION
VLO RET...................................................................................... 200 KIAS
MAXIMUM LANDING GEAR OPERATING SPEED — EXTENSION
VLO EXT...................................................................................... 250 KIAS
MAXIMUM LANDING GEAR EXTENDED SPEED (VLE)
VLE .............................................................................................250 KIAS
MAXIMUM FLAP EXTENDED SPEED (VFE)
VFE
- Flaps 10 ................................................................................ 210 KIAS
- Flaps 20 ................................................................................ 210 KIAS
- Flaps 30 ................................................................................ 175 KIAS
(METRIC) LIMITATIONS
02-03-02 Airplane Flight Manual DOT Approved Feb 02/2005
CSP 100-1 REV 2
(Metric)
SPEED LIMITATIONS (Cont)
MINIMUM OPERATING SPEED
Intentional speed reduction below the onset of stall warning, as defined by
stick shaker operation, is prohibited unless a lower speed is specifically authorized
for flight test or training operations.
TIRE SPEED
Maximum tire speed (ground speed) ....................................................182 kts.
AIRSPEED/MACH LIMITATIONS
(PRIMARY PITOT-STATIC SYSTEM)
Figure 02-03-01
SPDENV_BD100_10FEB04
100 125 150 175 200 225 250 275 300 325 350
INDICATED AIRSPEED − KNOTS
0
5
10
15
20
25
30
35
40
45
50
PRESSURE ALTITUDE − 1000 FEET
24000
28500
33750
38850
Mmo = 0.83
Vmo
MAXIMUM ALTITUDE
VA FOR WEIGHT − LB
NOTE:
1.0 lb = 0.4536 kg
LIMITATIONS
DOT Approved Jul 31/2006 Airplane Flight Manual 02-03-03
REV 6 CSP 100-1
OPERATIONAL LIMITATIONS
TAKEOFF AND LANDING
Maximum takeoff and landing pressure altitude..........................10 000 ft
Maximum tailwind component .........................................................10 kts
Takeoffs and Landings are limited to paved runways.
The maximum runway slopes approved for takeoff and landing are +2% uphill
and -2% downhill.
For aircraft on the State Aviation Administration of Ukraine (SAAU) registry:
MAXIMUM CROSSWIND COMPONENT - DRY RUNWAYS
The maximum crosswind component for takeoff is 28 knots (14 meters/sec).
The maximum crosswind component for landing is 24 knots (12 meters/sec).
MAXIMUM CROSSWIND COMPONENT - WET RUNWAYS
The maximum crosswind component for takeoff and landing on a wet runway
with water depth no more than 3.00 mm (0.125 inch) is defined in the following
table for different values of the coefficient of friction:
1. Operation on runways with a coefficient of friction less than 0.3 is
prohibited.
MAXIMUM CROSSWIND COMPONENT -
CONTAMINATED RUNWAYS
1. The maximum crosswind component for takeoff and landing on a
contaminated runway is 10 knots (5 meters/sec).
2. Operation on runways with a coefficient of friction less than 0.3 is
prohibited.
Reported Runway
Coefficient of Friction
Maximum Crosswind
Component
0.3 (poor braking) 10 knots (5 meters/sec)
0.4 (average braking) 15 knots (8 meters/sec)
0.5 (good braking, equivalent to dry) Takeoff - 28 knots (14 meters/sec)
Landing - 24 knots (12 meters/sec)
EFFECTIVITY
LIMITATIONS
02-03-04 Airplane Flight Manual DOT Approved Jul 31/2006
CSP 100-1 REV 6
OPERATIONAL LIMITATIONS (Cont)
TAKEOFF AND LANDING (Cont)
COLD WEATHER OPERATIONS
1. Takeoff is prohibited with frost, ice, snow, or slush adhering to any
critical surface (wings, horizontal stabilizer, vertical stabilizer, control
surfaces, engine inlets, and upper surface of the fuselage).
WARNING: Even small amounts of frost, ice, snow or slush on the wing
leading edges and forward upper wing surface may adversely
change the stall speeds, stall characteristics, and the protection
provided by the stall protection system, which may result
in loss of control on takeoff.
(Continued)
For aircraft on the Russian Federation (RF) and Commonwealth of
Independent States (CIS) countries’ registry:
MAXIMUM CROSSWIND COMPONENT - DRY RUNWAYS
The maximum crosswind component for takeoff is 28 knots (14 meters/sec).
The maximum crosswind component for landing is 24 knots (12 meters/sec).
MAXIMUM CROSSWIND COMPONENT - WET RUNWAYS
　
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