Operating Limitations Flashcards
Max operating Altitude
FL 410
Max Air Temp for TO and Landing
ISA +35C, +50C, 122F
Min. Temp approved for TO
-40C, -40F
When the ambient temp. Is -30C (-22F) or below for engine start
The Engine must be motored for 60 seconds, and the fan must rotate before engine start is initiated
For TO or landing on runways covered with standing water, slush or snow, or icing conditions..
Both igniters on both engines must be on continuously
Maximum runway slopes for take off and landing
+2% uphill
-2% down hill
Max tailwind component for take off and landing
10 knots
Maximum occupancy, including no more than 19 passengers, must not exceed the lesser of the following
22, or the # of seats for which takeoff and landing accommodation is provided.
Rotation rates should not exceed
3° per second
Pitch trim must be set according to
Aircraft computed center of gravity
Take off it’s trend initial target for rotation is
10°
Max Press. Altitude for TO and Landing
10,000 ft.
Engine cowl anti-ice system must be on when (Flight and Ground)
OAT is 10°C (50°F) or below and visible moisture in any form is present (such as fog with vis. Of 1 mi. Or less, rain, snow, sleet and ice crystals).
Also, when those same temps are present when operating on runways or taxiways where surface contamination is present.
The engine cowl anti-ice system must be on
At or above FL 220:
- When ice is indicated by ice detection system
- When in icing conditions if an ice detector has failed.
Below FL 220:
- When in icing conditions
- When ice is detected by the ice detection system
Wing anti-ice system. Ground operations.
Must be on for final taxi prior to TO. IF OAT is 5°C ( 41°F) or below, unless type 2,3, or 4 fluids have been applied.
Single engine taxi operations are prohibited in these conditions.
Icing conditions exist on the ground when
OAT is 5°C (41°F) or below and
- visible moisture in any form is present below 400 feet AGL
- the runway is wet or contaminated
- in the presence of any precipitation
L Heat or R Heat may go out during taxi, but..
Must be verified on prior to take off.
If wing anti-ice is not required for TO. It should be selected off just prior to take off
Wing anti-ice system must be selected and confirmed on for take off when
The OAT is 5°C (41°F) or below and moisture is present
If wing anti-ice is selected on for take off, what also must be selected on?
Cowl anti-ice must also be selected on
When type 2,3, or 4 anti-ice fluids have been applied, the wing anti-ice system must..
Only be selected and confirmed on just prior to thrust increase for take off
Icing conditions exist in flight at…
A TAT of 10°c (50°F) or below and visible moisture encountered, except when the SAT is -40°C. (40°F)
Supercooled large droplet icing (SLD)
Wing anti-ice and Cowl anti-ice must be on, leave icing conditions when side window icing occurs
Take off is permitted with frost adhering to
- The upper surface of the fuselage
- The underside of the wing, that is caused by cold soaked fuel
In addition to a visual check, a tactile check of the wing leading edge wing upper surface and wing rear upper surface is required during walk around when
The outside air temperature is 5°C (41°F) or less
- The wing fuel temperature is 0° C or less
- The atmospheric conditions have been conducive to frost formation