Memory Items Flashcards
The maximum altitude with flaps extended is___
20,000 feet
APU to pack takeoffs are prohibited at airport altitudes above ____.
6,900 feet
Do not use FLCH on final approach below ___
1,000 feet AFE
Maximum landing weight
575,000 lbs
260,815 kgs
FIRE ENG L, R
Fire is detected in the engine
1) A/T ARM switch ( affected side) - Confirm - OFF
2) Thrust lever (affected side) - Confirm - Idle
3) FUEL CONTROL switch (affected side) - Confirm - CUTOFF
4) Engine fire switch (affected side) - Confirm - Pull
5) If the FIRE ENG message stays shown:
Engine fire switch (affected side) - Rotate to the stop and hold for 1 second
If after 30 seconds the FIRE ENG message stays shown:
Engine fire switch (affected side) - Rotate to the other stop and hold for 1 second
Maximum zero fuel weight
547,000 lbs
248,115 kgs
ENG SVR DAMAGE / SEP L, R
One or more of these occur:
• Airframe vibration with abnormal engine indications
• Engine separation
1) A/T ARM switch (affected side) - Confirm - OFF
2) Thrust lever (affected side) - Confirm - Idle
3) FUEL CONTROL switch (affected side) - Confirm - CUTOFF
4) Engine fire switch (affected side) - Confirm - Pull
Max takeoff and landing tailwind component
10 knots
Do not use the autopilot below ___ RA at airport pressure altitudes above ____
100 feet / 8500 feet
Max glide slope angle with autoland
3.25°
AIRSPEED UNRELIABLE
Airspeed or Mach indications are suspected to be unreliable.
1) Autopilot disengage switch - Push
2) A/T ARM switches (both) - OFF
3) F/D switches (both) - OFF
4) Set the following gear up pitch attitude and thrust:
Flaps extended - 10° and 85% N1
Flaps up - 4° and 70% N1
Do not operate the ____ in a hangar or within ____ of any fuel spill.
Weather radar / 50 feet (15.25 meters)
ABORTED ENGINE START L, R
During a ground start, an abort start condition occurs
1) FUEL CONTROL switch (affected side) - CUTOFF
Do not operate ___ during refueling operations
HF radios
The maximum demonstrated takeoff and landing crosswind
38 knots
ENG LIM / SURGE / STALL L, R
One or more of these occur:
• Engine indications are abnormal
• Engine indications are quickly nearing or showing and exceedance
• Abnormal engine noises are heard, possibly with airframe vibration
• There is no response to thrust lever movement or the response is abnormal
• Flames in the engine inlet or exhaust are reported
1) A/T ARM switch (affected side) - Confirm - OFF
2) Thrust Lever (affected side) - Confirm - Retard until engine indications stay within limits or the thrust lever is at idle
Max winds with auto land operations:
Headwind
Tailwind
Crosswind
Crosswind CAT II/CAT III
Headwind 25 knots
Tailwind 10 knots
Crosswind 25 knots
Crosswind CAT II / CAT III 15 knots
Ground wind limits for doors:
Opening or closing
While open
40 knots opening or closing
65 knots while open
CABIN ALTITUDE
Cabin Altitude is excessive
1) Don the oxygen masks
2) Establish crew communications
3) Check the cabin altitude and rate
4) If the cabin altitude is uncontrollable:
SUPRNMRY OXYGEN switch - Push to ON and hold for 1 second
Without delay, descend to the lowest safe altitude or 10,000’, whichever is higher
To descend:
Move the thrust levers to idle
Extend the speed brakes
If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads
Descend at Vmo/Mmo
DUAL ENG FAIL/STALL
Engine Speed for both engines is below idle.
1) FUEL CONTROL switches (both) - CUTOFF, then RUN
2) RAM AIR TURBINE switch - Push and hold for 1 second
Maintain a minimum speed of ______ above the minimum maneuvering speed at all times when airspeed is below _____
15 knots / 0.82 Mach
The autopilot must not be engaged below a minimum engaged altitude of _____ after takeoff.
200 feet AGL
Min glide slope angle with autoland
2.5°
Maximum takeoff weight
N774SA, N775SA: 766,000 lbs
N714SA, N777SA/N778SA: 766,800 lbs / 347,451 kgs
Maximum taxi weight
N774SA, N775SA: 768,000 lbs
N714SA, N777SA/N778LA: 768,800 lbs / 348,358 kgs
Turbulent air and penetration speed (in severe turbulence) is defined as:
270 knots below 25,000 feet
280 knots or 0.82 Mach whichever is lower at 25,000 feet and above
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below ____.
200 feet AGL
Prohibited maneuvers
Intentional selection of reverse thrust in flight
Backing the airplane with the use of reverse thrust
Avoid ___ and ___ 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 ___ speed, including below ___.
Rapid / large alternating / any / Va
ENGINE AUTOSTART L, R
During a ground start, one of these occurs:
• AUTOSTART did not start the engine
• Fuel Control switch is in RUN at low engine RPM with the autostart switch OFF
FUEL CONTOL switch (affected side) - CUTOFF
STABILIZER
One of these occurs:
• Stabilizer movement without a signal to trim
• The stabilizer is failed
1) STAB cutout switches (both) - CUTOUT
2) Do not exceed the current airspeed
Max Runway slope?
+/- 2°
Max T/O and landing altitude?
9,800’ pressure altitude
Max field elevation?
9,650’
APU starter motor duty cycle?
Time between starts?
3 starts in a 60 min period
1min wait between each start (electric and air turbine)
