Limitations Flashcards
Maximum Takeoff and Landing Tailwind
Component
15 knots
Maximum Operating Altitude
43,100 ft pressure altitude
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.
The maximum demonstrated crosswind for takeoff is __knots and for landing is
__knots.
(-8) takeoff is 40 knots and for landing is 37 knots.
(-9) takeoff is 33 knots and for landing is 40 knots.
Do not ____ when refueling.
Do not operate HF radios when refueling.
Avoid weather radar operation
in a hangar, or within 50 feet (15.25 meters) of fueling operations or a fuel spill.
When personnel are within the area normally
enclosed by the aircraft nose radome.
Flight Management System - VNAV Temperature Compensation
Instrument approach operations are prohibited, unless altitude corrections are applied to all published procedure altitudes when the temperature at the landing elevation is below the minimum temperature on the approach chart, or below 0 degrees Celsius if no minimum temperature is on the approach chart. Warning: Below these temperatures, use of published procedure altitudes does not assure obstacle clearance.
Officer’s altitude display and field elevation is
75 feet.
Main door emergency power assists and evacuation slide systems
must be armed with the door mode select levers in the automatic position and the electronically dimmable door windows must be in the clear state prior to taxi, takeoff and landing whenever passengers are carried.
Maximum Taxi Weight
Maximum Takeoff Weight
(-8) 503,500 Pounds 502,500 Pounds
(-9) 563,000 Pounds 561,500 Pounds
Maximum Landing Weight
(-8) 380,000 Pounds
(-9) 425,000 Pounds
Maximum Zero Fuel Weight
(-8) 355,000 Pounds
(-9) 400,000 Pounds
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 _____ feet airport field elevation.
8400
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below ______.
the autopilot must be disengaged below 135 feet AGL.
With LAND 2 or LAND 3 annunciated and glidepath 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
disengaged no later than 50 feet below DH/MDA.
Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:
Headwind 25 knots
Tailwind 15 knots
Crosswind 15 knots
Maximum wind component speeds when performing autoland operations (may be limited by visibility or runway condition):
Headwind 25 knots
Tailwind 15 knots
Crosswind 25 knots
The maximum glide slope angle is ___ degrees
The minimum glide slope angle is ___ degrees
The maximum glide slope angle is 3.25 degrees
The minimum glide slope angle is 2.5 degrees
Autoland capability may be used with flaps ___ Engines _____
Autoland capability may be used with flaps 20, 25, or 30, with both engines operative or with one engine inoperative.
The autopilot flight director system (AFDS) autoland status annunciation must have LAND 2 or LAND 3 displayed.
Do not use FLCH on final approach below
1,000 feet AFE or on any approach past the FAF.
Oil temperature must be greater than ___° C for engine start.
greater than -40° C for engine start.
Reverse Thrust Limitations
Intentional selection of reverse thrust in flight is prohibited.
Backing the airplane with use of reverse thrust is prohibited.
Ground wind operating envelope:
- for crosswinds greater than 35 knots, limit thrust to a setting normally used for taxi (45% N1).
- with a tailwind component greater than 5 knots and winds greater than 35 knots, limit thrust to a setting normally used for taxi (45% N1).
- for winds greater than 55 knots, limit engine thrust to idle.
The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is ____ feet.
for RVSM operations is 200 feet.
The maximum altitude with flaps extended is
20,000 feet.
In-flight tank fuel temperature must be maintained
must be maintained at least 3° C above the freezing
point of the fuel being used.
Fuel Loading if center tank fuel is loaded.
Main tanks must be scheduled to be full
Note: The center tank may contain up to 22000 pounds of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed.
Dimensions
-8 Length 186 Feet 1 Inch
Wingspan 197 Feet 3 Inches
Tail 55 Feet 6 Inches
-9 Length 206 Feet 1 Inch
Wingspan 197 Feet 3 Inches
Tail 55 Feet 10 Inches
Minimum pavement width for 180o turn:
- 8 138 Feet 4 Inches (42.2 Meters).
- 9 154 Feet 0 Inches (47.0 Meters).
