Limitations Flashcards
Runway Slope
+/- 2%
Maximum Takeoff and Landing Tailwind Component
Boeing - 15 kts
Kalitta - 10 kts
– The capability of the airplane has been satisfactorily demonstrated for takeoff and landings with tailwinds up to 15 knots. This does not constitute operational approval to conduct takeoffs and landings with tailwind components in excess of 10 knots.
Maximum Operating Altitude
43,100 feet pressure altitude
Maximum Takeoff and Landing Altitude
8,400 feet pressure altitude (Basic)
9,800 feet pressure altitude (Optional)
Door Mounted Power Assists and Escape Slides
Door Marked ARMED/DISARMED
Main door emergency power assist and evacuation slide systems must be armed with mode select handle in the ARMED position prior to taxi, takeoff and landing whenever passengers are carried.
Door Mounted Power Assists and Escape Slides
Door Marked AUTO/MANUAL
Main door emergency power assist and evacuation slide systems must be armed with mode select handle in the AUTOMATIC position prior to taxi, takeoff and landing whenever passengers are carried.
Maximum demonstrated takeoff and landing crosswind
38 kts
Severe turbulent air penetration speed
- 270 kts < 25,000 ft
- 280 kts <> 0.82M =< 25,000 ft
- if <0.82M, MMS+15kts
DO NOT operate HF radios…
during refueling operations
Do not operate the weather radar…
- in a hangar
- within 50ft of fueling operations or spills
- when personnel are within the area normally enclosed by the aircraft nose radome
Max difference between CA or FO altitude display and field elevation
75 ft
Max Taxi Weight
768,000 lbs
Max Takeoff Weight
766,000 lbs
Max Landing Weight
575,000 lbs
Max Zero Fuel Weight
547,000 lbs
DO NOT use the autopilot below 100ft radio altitude at…
airport field elevations above 8,400ft
After T/O, A/P must not be engaged…
Below 200 ft AGL
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below…
200 ft AGL
Max wind when ldg wx min are predicated on autoland
- Headwind
- Crosswind (Cat II/III and other)
- Tailwind
25 kts - Headwind
10 kts/15 kts - Tailwind
25 kts - Other
Max/Min glideslope when ldg wx min are predicated on autoland
Max - 3.25 deg
Min - 2.5 deg
Do not use FLCH below…
1000 ft AFE
Max fuel tank temp
49oC
Reverse thrust prohibited (2)
- Intentional in flight selection
- Backing the airplane
For ground operation (exclusive of takeoff) in tailwinds and crosswinds between 30 and 45 knots…
engine power should be limited to a maximum of 70% N1. Avoid thrust levels above that required for normal taxi operation in all tailwinds and crosswinds greater than 45 knots.
APU’s starter motors duty cycle for the electric starter motor and air turbine starter
3 starts attempts in a 60 minute period each
Flight control rapid & large alternating control inputs…
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.
Max flap extension altitude
20,000 ft
The ground maneuver cameras should not be used during…
takeoff, approach, and landing.
ADIRU alignment must not be attempted at latitudes greater than…
78 degrees, 14.75 minutes.
Minimum Oxygen pressure CREW
1,100 psi for dispatch
- 4 crew
- 180 min diversion time
Minimum Oxygen pressure SUPERNUMERARY
1,300 psi for dispatch
- 5 supernumeraries
- 180 min diversion time
Minimum Oxygen pressure for Portable bottles
1,200 psi for dispatch
Flap Limits
- 1
- 5
- 15
- 20
- 25
- 30
Flaps: 265 - 1 245 - 5 230 - 15 225 - 20 200 - 25 180 - 30
