Limitations Flashcards
What is Max Ramp Weight?
18,078 pounds
8200 kg
Max TO Weight
17,968 lbs
8,150 kg
Max Landing weight
16,865 lbs
7,650 kg
Max zero fuel weight
13,999 lbs
6,350
V LO
V LE
250 KIAS
V MC
For takeoff with takeoff flaps
97 KIAS
V MC
For landing with landing flaps
No Icing Conditions
91 KIAS
V MC
For landing with landing flaps in Icing Conditions
95 KIAS
Operating Maneuvering Speed
V O
205 KIAS
Max Flap Extended Speeds
V FE
Flap 1 180 KIAS
Flap 2 170 KIAS
Flap 3 170 KIAS
Flap full 160 KIAS
Max Altitude for Flaps Extended
18,000 ft
Max Tire Ground Speed
182 knots
Runway slope
Type surface
-2% to +2%
Paved
Load factor limit flaps up
3.00 g
Load factor limit flaps down
1,2,3 and full
2.00 g
Baggage Loading
LH forward cabinet - 44 lb (20kg)
Lab cabinet - 33 lb (15kg)
Aft baggage - 463 lb (210kg)
Forward baggage - 110 lb (50kg)
Refreshments - 71 lb (32kg)
Side stowage - 36 lb (16.5kg)
Max takeoff and landing tailwind component
10 knots
Max crosswind component allowed to apply static takeoff power
18 knots
Hydraulic system accumulator pre-charge check interval
15 consecutive calendar days or before the next flight, whichever occurs last
Stall warning and protection system must be tested
Prior to each flight
What are the prohibitions associated with the use of the SVS?
Use of the SVS as primary information to base decisions and/or plan maneuvers, to navigate, or to avoid terrain, obstacles, or traffic is prohibited
Minimum battery voltage for start
24V
Minimum GPU voltage required for battery charging
27V
Max generator load on ground
330 amps each
Max generator load in flight
390 amps each
Max useable fuel per tank
FAA 399.4 Gal (2,676 lbs)
ANAC/EASA - 1,512 L (1,214 kg)
Unusable fuel per tank
FAA - 3.75 US Gal (25.13 lbs)
ANAC/EASA - 14 L (11kg)
Max fuel capacity
FAA - 806.2 US Gal (5,401 lbs)
ANAC/EASA - 3,052 L (2,450 Kg)
Max fuel imbalance
FAA - 33 US Gal (220 lbs)
ANAC/EASA - 125 L (100kg)
Min fuel tank temperature
-37 C
Max fuel tank temperature on the ground
52 C
Can be exceeded up to 80 C in flight
Position of fuel xfeed during takeoff and landing
OFF
Max thrust operating limits
Max Thrust: 10 minutes
Max ITT: 725 C
N2: 101 %
N1: 100 %
Oil pressure: 45-160
Oil temperature: 10-132.2 C
Takeoff operating limits:
Thrust: 5 minutes
Max ITT: 700
N2: 101%
N1: 100%
Oil Pressure: 45-160
Oil Temperature: 10-132.2 C
Max ITT for max continuous thrust and max climb thrust
680 C
Ground idle operating limits
N2: 55.1% (OEI)
51.2% (AEO)
Oil pressure: 25-160
Oil temperature: -40-132.2C
Flight idle operating limits
N2: 55.1%
Oil pressure 25-160
Engine start operating limits
Time: 5 seconds
ITT MAX: 765 C
Oil Temperature: -40 C
Transient operating limits 20 seconds
ITT: 765
N2: 103
N1: 102
Oil pressure: 0-20
Transient limits 200 seconds
Max Oil Temperature 140.5
Transient limits 400 seconds
Oil pressure 20-270
Starter limit motoring attempt cool down times:
1st: 60 seconds
2nd: 60 seconds
3rd: 15 minutes
4th: 30 minutes
Air conditioning
For operation on ground the GPU must be used or one engine must be turned on.
Pressurization (PSI)
Max differential: 9.4
Max diff over pressure: 9.6
Max diff negative pressure: -0.3
Max diff T.O. + L. 0.2
When must the crew activate the ice and rain protection system?
When icing conditions exist or are anticipated as per section 3 Normal Proceedures.
Define “when icing conditions exist or are anticipated “.
1). Whenever the SAT on the ground or for takeoff, or TAT in flight, is 10C or below and visible moisture in any form is present. (Clouds, fig, vis 1 mi or less, ice, standing water or slush)
Operating in icing conditions
Max altitude for T.O. + L: 10,000 ft
Min. airspeed gear + flaps up:
Wing and stabilizer anti-ice inhibited or armed 165 KIAS
Wing and stabilizer anti-ice uninhibited
150 KIAS
What I the limitation regarding contaminated aircraft surfaces?
Takeoff is prohibited with frost (polished or not), ice, snow or slush adhering to wings, control surfaces , engine inlets, or other control surfaces.
In what environmental condition is flight prohibited?
Flight in freezing drizzle or freezing rain is prohibited.
The pilot must immediately exit the freezing rain or freezing drizzle by changing altitude or course.
What are the limitations regarding use of the autopilot in icing conditions?
Autopilot use is prohibited in the following conditions:
1) . Severe icing
2) . Unusual control force or control deflection, or unusually large control forces to move flight controls when the the autopilot is disconnected.
3) . Indications of frequent autopilot re-trimming during straight and level flight.
When must the wing inspection light be operative?
Prior to flight into known or forecast icing conditions, at night.
Autopilot/Yaw Damper Limitations
Min. Engagement Height (2 engine): 600 ft.
Min. Engagement Height ( 1 engine): 1,000 ft.
Min. Use Height (2 engine): 195 ft
Min. Use Height (1 engine): 220 ft
Altitude loss (maneuvering/cruise): 160 ft
Yaw damper airspeed is limited to 180 KIAS if in icing conditions.
