200 Limitations Flashcards
Maximum Ramp Weight
53250
Maximum Takeoff Weight
53000
Maximum Landing Weight
47000
Maximum Zero Fuel Weight
44000
Minimum Flight Weight
30000
Maximum Tailwind component for takeoff and landing
PIC- 10kts
SIC- 10kts
Maximum Crosswind component for takeoff and landing.
27kts
Maximum Crosswind component for takeoff and landing on a contaminated runway
15
Maximum Pressure Altitude for Takeoff and Landing
10,000ft
Maximum Operating Altitude
37,000ft
Maximum Operating Altitude- single pack
25,000ft
Maximum ambient air temperature for takeoff and landing
ISA +35
Minimum ambient temperature for takeoff
-40C
Cowl Anti-Ice System- Ground ops
The COWL ANTI-ICE system must be ON when:
- The OAT is 10C or below and visible moisture in any form is present.
- The OAT is 10C or below when operating on runways, ramps, or taxiways where surface snow, ice, standing water, or slush is present.
Cowl Anti-ice system- flight ops
The COWL ANTI-ICE system must be ON when:
- in icing conditions, or
- ICE is annunciated by the ice detection system.
Wing Anti-ice system- Ground operations
- The wing anti-ice system must be selected ON during final taxi prior to takeoff if the OAT is 5C or below, unless Type II, III or IV anti-icing fluids have been applied. During single engine taxi operations, final taxi is defined as that period after second engine is started.
- L Wing A/I caution messages may be posted during taxi but must be verified out and Wing A/ICE ON advisory message posted prior to take-off. If wing anti-ice is not required for take-off it should be selected OFF just prior to takeoff.
- To prevent wing contamination from reverse jet blast, operating the thrust reversers during taxi operations on wet and contaminated surfaces should be avoided.
Wing anti-ice system- ground ops cont.
- The wing anti-ice system must be selected and confirmed ON for take-off when, the OAT is 5C or below and:
- Visible moisture in any form is present below 400ft AGL, or
- the runway is wet or contaminated, or
- in the presence of any precipitation - When Type II, III, or IV anti-icing fluids have been applied, the wing anti ice system must only be selected ON just prior to thrust increase for takeoff.
Wing Anti-Ice system- Flight ops
The wing anti-ice system must be ON:
- When ICE is annunciated by the ice detection system, or
- When in icing conditions and the Airspeed is less than 230kts.
Vfe Flaps 8
230kts
Vfe Flaps 20
230kts
Vfe Flaps 30
185kts
Vfe Flaps 45
170kts
Vfo Flaps 8
200kts
Vfo Flaps 20
200kts
Vfo Flaps 30
185kts
Vfo Flaps 45
170kts
Vle
250kts
Vlo retract
200kts
Vlo extend
250kts
Maximum Tire speed
182kts
Maximum turbulent air penetration speed
280kts or .75
Maximum wiper speed
220kts
Minimum Operating Limit 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.
Airplane Cold-soaked
Before the first flight of the day, when the airplane is cold-soaked at an ambient temperature of -30C or below for more than 8 hours:
- The engines must be motored for 60 seconds and the fan rotation must be verified before an engine start is initiated.
- Reverse thrusters must be actuated until the deploy and stow cycles are less than 5 seconds.
Continuous Ignition
Continuous Ignition must be used during the following:
- Takeoff and landings on contaminated runways
- Takeoff with high cross-wind components (>27kts company)
- Flight through moderate or heavier intensity rain
- Flight through moderate or heavier intensity turbulence
- Flight in the vicinity of thunderstorms
Engine operation at or near the shaker and pusher settings is predicated on an operable auto-ignition system.
Starter Limits
The starter must not be used if indicated N2 rpm exceeds 55%
Engine Start limits
1st attempt- 1 minute ON 10 seconds off
2nd attempt- 1 minute ON 10 seconds off
3rd etc..- 1 minute ON 5 minutes off
ITT limits for start
ITT must be 120C or less for all ground starts.
ITT must be 90C or less for all air starts.
Dry Motoring Cycle
The dry motoring cycle (with thrust levers at SHUT OFF) may be used for engine ground starts and engine air starts.
Dry Motoring limits
1st attempt- 90 seconds ON 5 minutes OFF
2nd and subsequent- 30 seconds ON 5 minutes OFF
Reduced Thrust Takeoff
Reduced Thrust Takeoff cannot be used:
- If normal takeoff fan speed is less the 85% N1
- With an engine that cannot achieve available full thrust rating
- If the wing and/or cowl anti-icing bleeds are in use
- On runways contaminated with standing water, slush, snow, or ice
- When warnings of wind shear or downdrafts have been forecast
- Special Departure Procedures specifies full thrust for takeoff
- Antiskid inoperative
- The reduced engine thrust procedure may be used on wet runways provided that wet runway performance data is used
- If the reduced thrust can be used, the fan speed for reduced engine thrust must not be lower then 85% N1
- In determining the assume temperature, when the reduced engine thrust take-off procedure is used, the take-off performance data for APR OFF must always be utilized.
Max fuel imbalance
The maximum permissible fuel imbalance between the contents of the left main and the right main tank is 800lbs.
Unusable fuel
Fuel remaining in a tank when the appropriate fuel quantity indicator reads zero is not usable.
Center Fuel tank limits
Take-off with a fuel load in excess of 500lbs in the center tank is not permitted unless each main tank is above 4400lbs.
APU Starting limits
Minimum ambient temperature for starting a cold soaked APU on the ground is -40C
APU starts on Battery
1- 30 seconds ON 2 minutes OFF
2- 30 seconds ON 20 minutes OFF
3- 30 seconds ON 2 minutes OFF
4- 30 seconds ON 40 minutes OFF
APU start limits using DC ground power
1- 15 seconds ON. 2 minutes OFF
2- 15 seconds ON. 20 minutes OFF
3- 15 seconds ON. 2 minutes OFF
4- 15 seconds ON. 40 minutes OFF
Maximum Differential Pressures
Positive 8.7psi
Negative -0.5psi
During ground maneuvering 0.1psi
During initial landing 1.0psi
The aircraft must be completely depressurized prior to opening any doors.
Cabin pressurization must not be operated to -1500ft when the system is in manual mode.
When the low pressure air ground connection is used, the Passenger Door must be OPEN.
DC system limits
To protect flight compartment CRT displays, the maximum permissible time for ground operations with DC power is only 5 minutes.
Wheel Brake Cooling limits
Brake cooling time must be observed between a landing or a low energy rejected takeoff (RTO) and a subsequent takeoff to ensure that sufficient brake energy is available to bring the airplane to a complete stop if the subsequent takeoff is rejected.
Flap Limits
Enroute use of Flaps is prohibited.
Flight with Flaps extended at altitudes above 15000ft is prohibited.
Flight Spoiler limits
Flight spoilers must not be extended in flight below an altitude of 1000ft AGL
To ensure adequate maneuver margins, flight spoilers must not be extended in flight at air speeds below the recommended approach speed plus 17kts.
Thrust Reversers
Thrust reversers are approved for ground use only.
The thrust reversers are intended for use during full stop landings. Do not attempt a go-around maneuver after deployment of the thrust reversers.
Takeoff with any of the following thrust reverser lights on, icons, or EICAS messages displayed is prohibited:
- THRUST REVERSER UNLK light
- REV icon N1 gauge
- L or R REV UNLOCKED caution message
During landing, application of maximum reverse thrust is not permitted at air speeds below 60kts. Below 60kts, reverse thrust must be at idle.
During preflight checks of the thrust reversers with the airplane stationary, reverse thrust must be limited to reverse idle.
Taxi lights
Taxi lights must be switched OFF whenever the aircraft is stationary in excess of 10 minutes.
Automatic Flight Control System
Use of DES submode (Flight director or autopilot coupled), During approach is not permitted.
Operation with the autopilot engage is prohibited at altitudes below 600 feet AGL, except when performing the following:
- For visual and non-precision approaches, the minimum autopilot use height is 400ft AGL.
- For precision approaches (ILS), the minimum autopilot use height is 80ft AGL.
The ADC source coupled to the active autopilot must be the same as that coupled to the ATC transponder during flight in RVSM airspace.
