Limitations Flashcards
Maximum Crosswind Takeoff
Runway Condition Wind LVP
6 33kts 5 25kts Same Values 4 20kts 3 17kts
Maximum Crosswind Landing
Runway Condition Wind LVP
6 33kts 5 33kts 15kts 4 33kts 3 25kts
Maximum Taxi Weight
187,333kgs
Maximum T/O Weight
186,880kgs
Maximum Landing Weight
147,871kgs
(MAFEV) LIMITATIONS
Turbulent Air
Severe turbulent air penetration speed is: 290 KIAS/.78 Mach, whichever is lower.
(MAFEV) LIMITATIONS
HF radios
Do not operate HF radios during refueling operations.
(MAFEV) LIMITATIONS
Weather radar
Avoid weather radar operation in a hangar
(MAFEV) LIMITATIONS
Aileron Trim
The use of aileron trim with the autopilot engaged is prohibited
(MAFEV) LIMITATIONS
Flight Level Change
Do not use FLCH on final approach below 1000 feet AFE
(MAFEV) LIMITATIONS
Autopilot After Takeoff
After takeoff, the autopilot must not be engaged below 200 feet AGL
(MAFEV) LIMITATIONS
Autopilot below 100ft
Do not use the autopilot below 100 ft. Radio Altitude at airport pressure altitudes above 8,400 ft
(MAFEV) LIMITATIONS
Flaps
The maximum altitude with flaps extended is 20,000 ft
(MAFEV) LIMITATIONS
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
(MAFEV) LIMITATIONS
Engine
Flight crew shall not blank engine vibration display during takeoff
(MAFEV) LIMITATIONS
Reverses
Reverse thrust is for ground use only
(MAFEV) LIMITATIONS
Tailwind
Maximum Takeoff and Landing Tailwind Component 15 knots
(MAFEV) LIMITATIONS
Wind speed for Autoland
Headwind 25kts
Crosswind 25kts
Tailwind 15kts
(MAFEV) LIMITATIONS
Wind speed CAT II/III
Headwind 25kts
Tailwind 10kts
Low Visiblity
(Captain Flying)
Taxi, takeoff, approach and landing with visibility less than 800 meters or RVR 550 meters must be performed by the Captain sitting in the LH seat
CAT II/III
Baro-altimeter
For CAT II/III approaches, Baro-altimeter Reference Bug must be set to zero
CAT II/III
In turbulence
CAT II/III approaches in windshear conditions or severe turbulence is prohibited
Airplane General
Runway Slope +- 2%
Max operating Altitude 43,100ft PA
Max T/O & Lndg Altitude 9,500ft PA
RVSM Altimeter Cross Check
In flight difference
The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation is 200 feet
RVSM Altimeter Cross Check
Field Elevation Max Diff Capt/FO & Field elev
Sea Level 40ft 75ft
5,000ft 45ft 75kt
10,000ft 50ft 75kt