Limitations Flashcards
Unpressurized Flight
Max. Alt. for Operation after an in flight depressurization is 10,000ft. MSL unless MEA or other constraints require a higher altitude.
Max Operating Speed Vmo/Mmo
320/.78
Max. Operating KIAS 8,000 to 10,000 MSL Vmo
Red Line,
(Do not deliberately exceed Vmo/Mmo in any regime of flight (climb, cruise or descent), Vmo/Mmo increases linearly from 250kts at 8,000 to 320 kts at 10,000)
Max Operating KIAS up to 8,000 MSL Vmo
250
Max Turb. Penetration Vb/Mb
250/.63 which ever is lower,
Max landing gear extension Vloe
250
Maximum Maneuvering Va
200,
Full application of rudder and ailerons, and maneuvers involving angle of attack near stall, must be confined to speed below Va
Va Limits Rudder caution
A full or nearly full rudder deflection in one direction followed by a full or nearly full deflection in the other direction, even at speeds below the Va, can dramatically increase the risk of structural failure of the vertical stabilizer or the rudder.
Flaps 45 speed caution
- Can momentary airspeed excursion that are due to wind gust or turbulence are allowed up to 155kts with no crew or mx action required.
- Can not steady state operation over 145kts is not allowed and must be entered into the AML.
Max landing gear extended Vle
250
Max landing gear retraction Vlor
200
Flap Speeds
9, 250
18, 200.
22, 200
45, 145
Max Wiper Operation
160
Max Operating Alt
37,000ft
Landing Pressure Alt Min and Max for Takeoff and Landing
Min -1000
Max 8,000
Min Takeoff and landing Temp
-40C SAT
Limits if below -40c SAT
The aircraft may not takeoff without further mx inspeciton
TAT limits in cruise flight above 25,000ft
-45c
Icing Definition on the ground for takeoff
- Icing conditions exist when the OAT is 10°C or below and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain,
snow, sleet and ice crystals) - Icing conditions also exist when the OAT is 10°C or below when operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes
Ground Icing Caution
Do not rely on visual icing evidence or ice detector actuation to turn on the Anti-icing System. Use the temperature and visual moisture criteria as specified above. Delaying the use of the Anti-icing System until
ice build-up is visible from the cockpit may result in ice ingestion and possible engine damage or flameout
In Flight Icing definition
Icing conditions may exist whenever the Total Air Temperature (TAT), is 10°C or below and visible moisture in any form is present (such as clouds, fog with
visibility of one mile or less, rain, snow, sleet and ice crystals).
IN flight ice Caution
Not withstanding ice detector monitoring, the crew remains responsible of monitoring potential icing condition and for manual activation of the ice protection system if icing condition are present and the ice detection is not activating the ice protection.
Min Temp for Manual anti-icing ops
-40c
Max temp for manual anti icing ops
10c
Use what temp reedout for ground or air for anti icing ops
Ground SAT
Air TAT
Auto anti icing system temp limits
none
Contaminated runways def.
A runway is considered “Contaminated” when more than 25% of the required field length, within the width being used, is covered by: • More than 1/8th inch (3 mm.) of: — standing water, — slush or — wet snow. • More than 3/4 inches (19 mm.) of dry snow. • Compacted snow • Ice
Auto Pilot Limits (max engage and min disengagement)
Min engagement 500 AGL
Min disengagement, Instrument app, MDA/DA/DH, Vis traffic pattern alt (1500AGL)
Auto Pilot Go around Single eng operaiton
Prohibited
Yaw damper operation is not authorized for:
- Takeoff to 500AGL
2. Landing
Apu Starter Limits
Between 3 Consecutive attempts 1 min off
Between 2 series of 3 consecutive attempts 30min off
AHARS
The Aircraft must not be moved when the AHRS is in the initialization mode until all attitude and heading information presented on the PFD is displayed
Engine Cool Down after landing or High Power runs
1 min at idle or taxi thrust before shutdown
Engine Oil Level
8 quarts before start
Or 7 quarts after engine start
Engine warm up prior to takeoff
4 mins for cold eng
2 Mins for warm
Note: eng is cold if it has been shutdown for more than 90 min
Prior to increasing N2 more than 83%, Engine oil temp must be
min of 40c
Note: acceptable to run the engine for at least 8 min to get this temp and ensure the oil temp is in the green arc before advancing the thrust lever for takeoff.
T/O-1 (A1), T/O RSV (A1/3) (5 Min Limit) ITT N1 N2
ITT 948 N1 100 N2 57-102.4
T/0-1 (A1/3), T/O (A1/3) (5 Min limit) ITT N1 N2
ITT 929 N1 100 N2 57-102.4
Alt T/O-1 (5 min limit) ITT N1 N2
ITT 917 N1 100 N2 57-102.4
Max Continuous ITT N1 N2
ITT 901 N1 100 N2 57-102.4
Max Engine Start ITT
800
Engine Oil PSI limits
- Amber rage up to 115 psi for 5 min in all thrust modes
- 115 to 155psi only for 2 mins
- total time for all 5 mins
- Red range not authorized, and exceed must be monitored and logging in AML
Min oil temperature for starting
-40c
Min oil temp for takeoff
+40c, if less than preform eng warm up procedure.
Starter Limits
Starting or Dry Motoring . . . Up to 5 min. ON, 5 min. OFF
OR
First to Fourth Cycles . . . . . . . . . . . .. 1 min. ON, 1 min. OFF
Following Cycles . . . . . . . . . . . . . . .. 1 min. ON, 5 min. OFF
Max Flap extension Altitude
20,000 MSL
Pitch Trim Limits
Max airspeed after takeoff during climb without re-trimming is 160kias
Holding Configuration
- Landing gear and flaps are up,
2. Min airspeed in icing condition is 200kias
Use of Thrust Reverser
Intended for use during rejected takeoff or landing, after initiating reverse thrust, a full stop must be made
Using max reverse thrust must be Used:
— Whenever its use will prevent a runway excursion.
— When landing on runways with “Medium” or “Poor” braking action, unless the appropriate landing distance penalty [Flip Cards] is applied.
Using Idle revers may be used:
— Dry runways 9,000 ft. or shorter usable length (LDA)
— Non-dry runways where braking action is “Good”
Thrust reverser is prohibited:
— Power-back operations
— Taxi operations
— Thrust levers stabilized in any intermediate position between IDLE reverse and MAXIMUM reverse.
Max Demonstrated Crosswind and Tailwind
30kts for crosswinds 10kts for tailwind
Max Turb penetration Vb speed below 10000
200
Section of the Autopilot App Mode Limitation
-app mode selection during localizer capture is allowed only when aircraft is inbound.
