Operating Limitations Flashcards
Runway Slope
+1.7% to -2.0%
Maximum Operating Altitude
37,000 feet
Maximum Takeoff and Landing Pressure Altitude
8,500 feet
Maximum Takeoff and Landing Tailwind Component
10 knots, or as permitted by Company Pages
Maneuvering Limit Load Factors
-Flaps/Slats retracted
+2.5g to -1.0g
Maneuvering Limit Load Factors
-Flaps/Slats extended
+2.0g to 0.0g
Wing landing light motors should be allowed to cool for
1 1/2 minutes after initial extension or retraction and 3 1/2 minutes after each subsequent extension or retraction.
Lamps should not be operated in still air for
over 10 minutes
Crosswind limit
38 knots for takeoff or landing, including gusts
Severe turbulence air penetration speed
275KIAS/.75M
Maximum Taxi Weight (MTW)
122,000#s
Maximum Take Off Weight (MTOW)
121,000#s
Maximum Landing Weight (MLW)
110,000#s
Maximum Zero Fuel Weight (MZFW)
100,500#s
Maximum cabin differential pressure is
7.86 psi
Maximum emergency relief pressure is
8.27 psi
For takeoff, the FLOW switch on the overhead panel must be in _____
NORM
Do not exceed _______ KIAS below _______ feet when windshield heat is inoperative on any windshield.
315 KIAS; 10,000 feet
Cracked captain, center, or first officer’s windshield operating limits below 10,000 feet:
Outer glass:
Inner glass:
Outer glass: 315 KIAS; Inner glass: 235 KIAS
Wing Ice:
Do not take off with “_________” alert displayed
WING ICE DETECTED
During takeoff, do not engage the _______ below ____ feet AGL
autopilot; 200’
Do not conduct an auto coupled (ILS or autoland) approach if ________ alert illuminates for longer than ___ seconds after airplane is stabilized and tracking glideslope.
STAB OUT OF TRIM; 3 sec
For non-ILS approaches, the autopilot must be disengaged no lower than the applicable minimums minus ___ feet.
50
Maximum allowable wind component for autoland operations:
Headwind:
Crosswind:
Tailwind:
25, 15, 10
Do not conduct autoland operations if:
- ALIGN mode is not annunciated on an FMA by 100 feet radio altitude.
- Any unusual control position or other abnormal conditions exist in the flight control system.
- RUDDER PWR OFF alert is displayed.
- Airport field elevation exceeds 8,000 feet MSL.
- Runway width is less than 145 feet
Engine Starter Duty Cycle: _____ start attempts, with a minimum of ___ seconds between attempts. Maximum duration of each attempt is __ minutes. Allow __ minutes cooling time before further start attempts are made.
Three; 15 seconds; 3; 15 minutes
Reduced thrust takeoffs are not authorized on runways contaminated with _____, _____, _____, _____, or _____.
standing water, loose snow, slush, compacted snow or wet ice.
APU AIR switch must be _____ for takeoff and in flight operations
OFF
APU starter motor duty cycle is limited to _____ consecutive start attempts. Wait ____ minutes prior to further start attempts.
three; 30
Speedbrakes may not be used with flaps extended beyond
20°
On the ground, the standby altimeter must be within +/- ____ feet of the Captain’s and First Officer’s altimeters
75
The maximum allowable on the ground altimeter reading differences at a known field elevation for RVSM operations are:
Captain & F/O: 60’
Captain or F/O & Field Elevation: 75’
Captain and F/O (In Flight): 200’
Do not operate the weather radar in a hangar or within ___ feet of any personnel or a fuel spill.
50’
After takeoff, _____ fuel shall be emptied prior to using _____ fuel.
center tank; main tank
Maximum permissible fuel imbalance is:
1500#’s
The maximum fuel temperature is ___ for types: Jet A, Jet A1, JP-5, JP-8.
54°C
The minimum fuel temperature is either the higher of the fuel freeze point, or the engine limits, as follows:
- -42°C for takeoff, climb, and go-around
* -48°C for flight above 15,000 feet
Prior to engine start on any flight where _____ tank fuel is present and will be needed for that route segment, the _____ tank fuel pumps must be individually checked to verify pump operation.
center; center
Do not reset any tripped _____ circuit breakers.
fuel pump
Maximum landing gear retraction speed is:
250 KIAS
Maximum landing gear extension speed is:
300 KIAS / 0.70M
The certified maximum tire speed rating is:
195 knots
Weather radar must be on for takeoff for _____ to be operable
predictive windshear
