Limitations - Required (#) Flashcards
Maximum Takeoff and Landing Tailwind Component?
10 knots
or
15 knots
What are the limitations for autopilot engagement? #
The autopilot must not be engaged below a minimum engage altitude of 200 feet AGL after takeoff.
[Model 787-8]Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 100 feet AGL.
Autoland capability may only be used for operations into runways at or below 8400 feet airport field elevation
Maximum Operating Altitude?
43,100 ft pressure altitude
Maximum Takeoff and Landing Altitude?
14,000 ft pressure altitude
but
Use high altitude airport operation procedures when operating above 8,000 feet pressure altitude
Maximum demonstrated crosswind?
Takeoff - 35 knots
Landing - 33 knots
Do not operate HF radios when \_\_\_\_\_\_\_\_? #
Refueling
Do not operate weather radar \_\_\_\_\_\_? (2) #
In a hangar
or
Within 50 feet (15.25 meters) of any fuel spill.
Prior to takeoff the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation?
75 feet
Maximum Taxi Weight?
-8
503,500 Pounds
228,383 Kilograms
-9
547,000 Pounds
248,115 Kilograms
The autopilot must not be engaged below a minimum engage altitude of? #
200 feet AGL after takeoff
Autoland capability may only be used for operations into runways at or below? #
8400 feet airport field elevation
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below? #
-8
100 feet AGL
-9
135 feet AGL
With LAND 2 or LAND 3 annunciated and glidepath angles greater than ____?, the autopilot must be disengaged below ________?
3.25 degrees
100 feet AGL
Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations? #
Headwind - 25 knots
Tailwind -15 knots
Crosswind - 20 knots
Maximum wind component speeds when landing weather minima are predicated on autoland operations? #
Headwind - 25 knots
Tailwind - 15 knots
Crosswind - 25 knots
The maximum glideslope angle is?
The minimum glideslope angle is?
#
- 25 degrees
2. 50 degrees
Autoland capability may be used with:
What flap settings?
How many engines?
20, 25, or 30
Both engines operative or with one engine inoperative
Oil temperature must be greater than _____? for engine start
#
-40° C
Dispatch prohibited (EEC)?
#
In alternate EEC mode (GE engines only)
Reverse thrust is prohibited when? (2)
#
In flight
Backing the airplane
If the airplane has been parked, un-powered, in an environment ,below _____? the temperature of the compartment air surrounding the engine fire extinguishing bottles must be warmed to ____? and maintained at this temperature for a minimum of ____? hours before engine start. Verify the appropriate warming procedure was accomplished, prior to engine start.
Below -40° F (-40°C)
- 10° F (-23° C) or greater
1. 5 hours
Maximum wind on the ground - (RR)
Limit engines to taxi power when ______? (2)
Do not run engines when _______?
With a tailwind component and total wind greater than 42 knots
or
For crosswinds greater than 45 knots
For winds greater than 65 knots
Maximum wind on the ground - GE Block 4 & PIP1 engines
Limit thrust to a setting normally used for taxi (45% N1) when? (2)
Limit engine thrust to idle when?
For crosswinds greater than 37 knots
With a tailwind component greater than 5 knots and winds greater than 34 knots
For winds greater than 55 knots
Maximum wind on the ground - PIP2 engines
Limit thrust to a setting normally used for taxi (45% N1) when? (2)
Limit engine thrust to idle when?
For crosswinds greater than 40 knots
With a tailwind component greater than 5 knots and winds greater than 35 knots
For winds greater than 55 knots
Maximum takeoff and landing tailwind component
[GE PIP2 engines]
10 knots
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. #
N/A
Do not extend flaps above?
20,000 feet
What is Turbulent air penetration speed? (2)
Turbulent air penetration speed (in severe turbulence) is defined as:
• 290 KIAS below 25,000 feet
• 310 KIAS/.84 Mach at and above 25,000 feet.
