Limitations -8 (# items) + Nice to Know Flashcards
Runway slope
+/- 2%
(#) Maximum Takeoff and Landing Tailwind
Component
15 knots
Maximum Operating Altitude
43.100ft pressure altitude
Maximum Takeoff and Landing Altitude
14.000ft pressure altitude
(#) Do not operate HF radios ________.
when refueling
Verify that an operational check of the Flight Deck Access System has been accomplished according to approved procedures once _________.
each flight day
The maximum demonstrated crosswind for takeoff is _______ (gust included),
40 knots
The maximum demonstrated crosswind component for landing is ______ (gust
included).
37 knots
(#) Severe turbulent air penetration speed (in severe turbulence) is defined as:
- 290 KIAS below 25,000 feet
- 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet.
(#) Avoid _______________ in a hangar.
weather radar operation
Prior to takeoff the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation is _______.
75 feet
Maximum Taxi Weight
228.383kg
Maximum Takeoff Weight
227.930kg
Maximum Landing Weight
172.365kg
Maximum Zero Fuel Weight
161.025kg
(#) The autopilot must not be engaged below a minimum engage altitude of ______________ after takeoff.
200 feet AGL
(#) Autoland capability may only be used for operations into runways ________________ airport field elevation.
at or below 8400 feet
(#) Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below ____________.
100 feet AGL
(#) With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below __________.
100 feet AGL
If the glidepath angle for approach is greater than 3.77 degrees, the autopilot must be disengaged ________________.
no later than 50 feet below DH/MDA
Low Visibility (HUD) Takeoff
(#) Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations (headwind, crosswind, tailwind):
Headwind: 25 knots
Crosswind: 20 knots
Tailwind: 15 knots
Automatic Landing
(#) Maximum wind component speeds when landing weather minima are predicated on autoland and CAT II/III operations (headwind, crosswind, tailwind):
Headwind: 25 knots
Crosswind: 25 knots
Tailwind: 10 knots
Automatic Landing
For USA operations the Crosswind component is reduced to ________.
15 knots
(#) The maximum glideslope angle is ____ degrees.
3.25
(#) The minimum glideslope angle is _____ degrees.
2.5
Autoland capability may be used with flaps _________ with both engines operative or with one engine inoperative.
20, 25, or 30
(#) Do not use FLCH on final approach _______.
below 1,000 feet AFE
(#) Oil temperature must be greater than ______ for engine start.
-40° C
(#) What AFM Limitations should we observe regarding the use of thrust reversers?
- Intentional selection of reverse thrust in flight is prohibited.
- Backing the airplane with use of reverse thrust is prohibited.
(#) What AFM Limitation should we observe regarding the use of flight controls?
Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA.
The maximum altitude with flaps extended is _______.
20.000 feet
Maximum tank fuel temperature at takeoff is _______ for Jet A, Jet A-1, JP-5, JP-8 or TS-1.
49° C (120° F)
Tank fuel temperature prior to takeoff must not be less than _______.
-29° C (-20° F)
In-flight tank fuel temperature must be
maintained ___________________ of the fuel being used.
at least -42° C, as well as 3° C
above the freezing point
Before Takeoff Procedure
Engine warm up requirements:
Run the engines for at least _____ minutes.
5
Before Takeoff Procedure
Engine warm up requirements:
Engine oil temperature must be _________ before takeoff.
above the lower amber band
After Landing Procedure
Engine cooldown recommendations:
Run the engines for at least _____ minutes
5
Flap placard speeds
1 - 250kt
5 - 230kt
15 - 215kt
20 - 210kt
25 - 180kt
30 - 170kt
Minimum pavement width for a 180-degree turn
42,2 meters
Principal dimensions (length, height, wingspan)
Length: 56,7 m
Height: 16,9 m
Wingspan: 60,1 m
Thrust Rating Rolls-Royce Trent 1000G
67.300 pounds BET
