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B-777 New Limitations

  1. LIMITATIONS 10.4  

    Takeoff, Landing and Enroute Operational Limits (AFM)

    Max. Operating Altitude:           ___ft 
    Max. TO / LDG Altitude:            ___ft
    Max. Alt. W/flaps or slats:         ___ft
    Operating Alt:    43,100' 

    TO/LDG Altitude:  8400'

    Flaps/Slats ext.:   20,000’
  2. LIMITATIONS 10.4
    Automatic Landings, Wind limitations:
    Max Headwind:

    Max Tailwind  (300ER):
    Max Tailwind  (200ER):

    Max Crosswind:
    Wx below 4000 and 3/4 vis:
    • Headwind:                     25 kts
    • Max Tailwind  (300ER):   15
    • Max Tailwind  (200ER):   10

    • Max Crosswind:              25kts
    • below 4000 and 3/4...     15kts
  3. LIMITATIONS 10.4   

    Peak wind value- except in an emergency:
    50 kts
  4. LIMITATIONS 10.4   
    MEMORY ITEM

    Max demonstrated crosswind:
    38 kts
  5. LIMITATIONS 10.4
    TAKEOFF CROSSWIND LIMITS


    Dry:
    Wet:
    Standing Water/Slush:
    Snow (Wet & Dry):
    Compacted Snow:
    Ice:
    • Dry                              38
    • Wet                              38
    • Standing Water/Slush.   25
    • Snow (Wet & Dry).        25
    • Compacted Snow.          20
    • Ice                               15
  6. LIMITATIONS 10.4
    LANDING CROSSWIND LIMITS

    Dry:
    Wet:
    Standing Water/Slush:
    Snow (Wet & Dry):
    Compacted Snow:
    Ice:
    • Dry                            38
    • Wet                            38
    • Standing Water/Slush  35
    • Snow (Wet & Dry).       25
    • Compacted Snow.        17
    • Ice.                             15
  7. LIMITATIONS 10.4
    LANDING CROSSWIND LIMITS

    Landing Only:  Reduce crosswind limits by ___ kts on wet or contaminated runways whenever asymmetric reverse thrust is used
    5 kts
  8. LIMITATIONS 10.4

    WIND LIMIATIONS:
    VISIBILITY LESS THAN 3/4 MILE
    MAX CROSSWIND:
    15KTS
  9. LIMITATIONS 10.5     NOTE:
    300ER

    For ground operations in tailwinds and crosswinds between 30-45kts, engine power should be limited to :      ____% N1
    70% N1
  10. LIMITATIONS 10.5 

    Reduce crosswind limits by ___knots on wet or contaminated runways whenever asymmetric reverse thrust is used.
    5 KNOTS
  11. LIMITATIONS 10.6  
    Landing Gear Operating (VLO / MLO) (AFM)


    Extension.   ____kts / ____ M. 

    Retraction.  ____ kts / ____M.
    Extension    270 kts / .82M

    Retraction    270 kts / .82M
  12. LIMITATIONS 10.7   

    Landing Gear Extended (VLE / MLE) (AFM)

    Extended: ____kts / ____ M.
    Extended    270 kts / .82M
  13. LIMITATIONS 10.7 
    NOTE:

    With flaps 25 and 30, positive limits vary linearly from +____ g at max landing weight to +____ g at maximum takeoff weight.
    from +2.0 g at max landing weight

    to +1.5 g at max takeoff weight.
  14. LIMITATIONS 10.3

    Flight Maneuvering Load Acceleration Limits (AFM)

    Flaps Up ...   +___g  to  -__g
    Flaps Down...+___g  to  ___g
    • +2.5g to  -1.0g
    • +2.0g to   0.0g
  15. LIMITATIONS 10.5   
    Airport Operations Limits
    Runway Slope:


    +___% to -___%
    +2.0% to -2.0%
  16. LIMITATIONS 10.4   
    MEMORY ITEM

    Maximum Wind Limits – Takeoff and Landing

    Tailwind: 300ER  ___ kts
                  200ER  ___kts

    Xwind (max demonstrated):
    • Tailwind:  300ER       15 kts
    •                200ER       10 kts
    • (May be further limited by performance requirements.)

    Crosswind (max demonstrated):  38 kts
  17. LIMITATIONS 10.8 

    Flap Placard Speeds  (300ER)

            (300ER)   
      1°    __ kts     
      5°    __ kts    
    15°    __ kts    
    20°    __ kts    
    25°    __ kts    
    30°    __ kts
    • 1     265 
    • 5     245 
    • 15   230 
    • 20   225 
    • 25   200
    • 30   180
  18. LIMITATIONS 10.8  

    Flap Placard Speeds:  (200ER)
      1°    __ kts    
      5°    __ kts    
    15°    __ kts    
    20°    __ kts    
    25°    __ kts    
    30°    __ kts    
    • 1     255 kts
    • 5     235 kts
    • 15   215 kts
    • 20   195 kts
    • 25   185 kts
    • 30   170 kts
  19. LIMITATIONS 10.8     MEMORY ITEM

    The turbulent air penetration speed (in severe turbulence) is defined as:

    1.) Below 25000':
    2.) 25,000 feet and above

    3.) Maintain a minimum speed of ___ knots above the minimum maneuvering speed (amber band) at all altitudes when the airspeed is below 0.82 Mach.
    • 1.)  270 knots below 25,000 feet
    • 2.)  280 knots or .82 Mach, whichever is lower

    3.)  15 knots above the minimum maneuvering speed (amber band) at all altitudes when the airspeed is below 0.82 Mach.
  20. LIMITATIONS 10.9    MEMORY ITEM
    Maximum Taxi Weights

    (300ER) ______    

    (200ER) ______     
    777,000 lbs

    650,000 lbs
  21. LIMITATIONS 10.9    MEMORY ITEM

    Maximum Takeoff Weights

    (300ER):     
    (200ER):
    • (300ER)   775,000 lbs
    • (200ER)   648,000 lbs
  22. LIMITATIONS 10.9    MEMORY ITEM
    Maximum Landing Weight

    (300ER)     
    (200ER) 
    • (300ER)     554,000 lbs    
    • (200ER)     460,000 lbs
  23. LIMITATIONS 10.9  
    Maximum Zero Fuel Weight

    (300ER)     
    (200ER) 
    • (300ER)    524,000 lbs   
    • (200ER)    430,000 lbs
  24. LIMITATIONS 10.9 

    Minimum Inflight Weight:

    (300ER)    
    (200ER) 

    (Does not include usable fuel)
    • (300ER)    305,500 lbs  
    • (200ER)    266,100 lbs

    (Does not include usable fuel)
  25. LIMITATIONS 10.9 

                            NOTES
    Maximum Landing Weight: 

    Landing at any weight that exceeds the
    Maximum Landing Weight is defined as a/an ___________landing.
    Overweight Landing
  26. LIMITATIONS 10.10    MEMORY ITEM
    Passenger Evacuation (AFM)

    Main door emergency power assist systems and emergency evacuation
    slide systems must be armed with the Mode Select Handles in the
    _________ position, prior to taxi, takeoff and landing whenever passengers
    are carried
    the ARMED position
  27. LIMITATIONS 10.10   MEMORY ITEM
    Passenger Evacuation (AFM)

    _________ are visible through windows in the doorway liners when the doors and slides are in the ARMED mode.
    Girt bar indication flags
  28. LIMITATIONS 10.9
    Aircraft Structure

    Ground wind limits for all doors:
    • ___ knots while opening or closing
    • ___ knots while open.
    40 knots

    65 knots
  29. LIMITATIONS 10.10
    Broadband Comm Switch (if installed) (AFM)

    During deicing/anti-icing procedures on the ground, the Broadband Comm
    switch must be in the ______position.
    • the Broadband Comm
    • switch must be in the OFF position.
  30. LIMITATIONS 10.9
    WLAN Use on Flightdeck (AFM)

    The use of WLAN on the flightdeck is ____.
    The use of WLAN on the flightdeck is prohibited
  31. LIMITATIONS 10.11  Cabin Pressurization (AFM)

    Maximum Cabin Differential Pressure:

    Maximum Allowable Cabin Pressure Differential for Takeoff and Landing:
    9.1 psi

    .11 psi
  32. LIMITATIONS 10.10  
    APU to Pack Operation (300ER)

    APU to pack takeoffs are prohibited at airport pressure altitudes above ____feet field elevation.
    above 6900 feet field elevation.
  33. LIMITATIONS 10.12   MEMORY ITEM
    Icing Conditions
    Ground and for Takeoff

    Icing conditions exist when OAT is 10°C (50°F) or below and:


    • Visible moisture in any form is present (such as clouds, fog with visibility one mile or less, rain, snow, sleet or ice crystals). 

    • When operating on ramps, taxiways, or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on the engines, nacelles, or engine sensor probes.
  34. LIMITATIONS 10.12   MEMORY ITEM
    Icing Conditions 

    Inflight
    Icing conditions exist when:
    • Indicated by the primary ice detection system, or 

    • TAT is 10°C (50°F) or below and visible moisture in any form is present (such as clouds, fog with visibility one mile or less, rain, snow, sleet or ice crystals).
  35. LIMITATIONS 10.13   MEMORY ITEM
    Minimum Altitude for Use of Autopilot

    Takeoff:
    200 feet AGL
  36. LIMITATIONS 10.13   MEMORY ITEM
    Minimum Altitude for Use of Autopilot (AFM)

    Coupled to ILS Glideslope and Localizer
     With LAND 2 or LAND 3 annunciated

    Without LAND 2 or LAND 3 annunciated
    With LAND 2 or LAND 3 annunciated.... None

    • Without LAND 2 or LAND 3 .............200 feet
  37. LIMITATIONS 10.13   MEMORY ITEM
    Minimum Altitude for Use of Autopilot (AFM)

    In Go-Around Mode:
    In Go-Around Mode .... None
  38. LIMITATIONS 10.13  
    Aileron Trim

    Use of aileron trim with the autopilot engaged is ____.
    Use of aileron trim with the autopilot engaged is prohibited
  39. LIMITATIONS 10.13
    Automatic Approach with Flaps 25 (AFM)

    Category II/III operations and autoland are/are not approved (Choose one) with flaps 25.
    are not approved with flaps 25.
  40. LIMITATIONS 10.13
    Non-AFM Operational Information

    Do not use FLCH (flight level change) on final approach below ____ft. AFE.
    below 1000 feet AFE.
  41. LIMITATIONS 10.13   MEMORY ITEM
    Automatic Landings

    Automatic landings can be made using flaps ________, with both engines operative or one engine inoperative.
    flaps 20 or 30
  42. LIMITATIONS 10.13   MEMORY ITEM
    Automatic Landings

    The autopilot flight director system
    (AFDS) autoland status annunciation must display ______.
    (AFM)
    LAND 2 or LAND 3.
  43. LIMITATIONS 10.13   MEMORY ITEM
    Automatic Landings

    Automatic landings cannot be made if the following EICAS messages are displayed:
    SLATS DRIVE (AFM), or

    PITCH UP AUTHORITY.
  44. LIMITATIONS 10.13  
    Automatic Landings

    Glideslope Angle (AFM)

    Maximum Glideslope angle:
    Minimum Glideslope Angle:
    • Maximum:  3.25°
    • Minimum:     2.5°
  45. LIMITATIONS 10.14
    COMMUNICATIONS

    Boom mics, if operative, must be used below _____feet
    18000'  (FL180)
  46. LIMITATIONS 10.14
    COMMUNICATIONS

    If one HF radio is selected for transmission, _________the other HF radio on all audio select panels to prevent audio interference.
    DESELECT the other HF radio
  47. LIMITATIONS 10.14

    All takeoff and go-around thrust ratings
    are limited to  ____  minutes duration.
    Five minutes.
  48. LIMITATIONS 10.15
    Reverse Thrust   (200ER)

    After a rejected takeoff (RTO) is performed, where thrust reversers were deployed, takeoff is prohibited until maintenance action is complete. (T or F)?
    TRUE
  49. LIMITATIONS 10.15 
    Reverse Thrust   (300ER)

    Position thrust reverse levers full down (forward thrust) only after engines have decelerated to:
    reverse idle
  50. LIMITATIONS 10.15
    APU (not an AFM)

    The APU’s start motors duty cycle for the electric starter motor and air turbine starter is:
    3 start attempts in a 60 minute period each.

    (one minute wait between starts, regardless of electric or air start)
  51. LIMITATIONS 10.15
    Engine Limit Display Markings

    Maximum and Minimum Limits:
    Maximum and Minimum Limits....... Red
  52. LIMITATIONS 10.15
    Engine Limit Display Markings

    Cautionary Limits:
    Cautionary Limits...... Amber
  53. LIMITATIONS 10.16

    During ground operations (including taxi-in and taxi-out) in icing conditions when the OAT is 3°C or below, the engine must be run up momentarily to a minimum of ____% N1 at intervals not to exceed ____minutes.
    50% N1  

    60 Minutes
  54. LIMITATIONS 10.16   MEMORY ITEM
    Oil System     (200ER)

    Oil Quantity: 

    Minimum prior to engine start (not an AFM)
    16 qts
  55. LIMITATIONS 10.16   MEMORY ITEM
    Oil System     (300ER)

    Oil Quantity
    Minimum prior to engine
    start (not an AFM):
    21 qts
  56. LIMITATIONS 10.16   
    Oil System     

    Oil Pressure
    Minimum (300ER)     ___psi
    Minimum (200ER)     ___psi
    • (300ER)       10 psi
    •  (200ER)      25 psi
  57. LIMITATIONS 10.16   (300ER)

              NOTE
    Temporary operation below
    10 psi during negative G
    operation is limited to:
    15 seconds maximum.
  58. LIMITATIONS 10.16 (300ER)

    Oil Temperature
    Max. for Continuous Operation:  __°C
    Max. for 15 minute limit:           __°C
    132 °C

    143 °C
  59. LIMITATIONS 10.16
    (200ER)
    Oil Temperature

    Min. for Engine Start :        __°C
    Min. for Takeoff Power:      __°C
    Max. for Cont. Operation:   __°C
    • -40 °C
    •   50 °C
    • 191 °C
  60. LIMITATIONS 10.18   

    Flight Controls
    Avoid _________, especially in combination
    with large changes in pitch, roll, or yaw.
    rapid and large alternating control inputs...

    (they may result in structural failure at any speed, including below VA.)
  61. LIMITATIONS 10.18
    Flight Control Mode (AFM)

    Takeoff is permitted only in the _____flight control mode.
    normal
  62. LIMITATIONS 10.19
    RVSM Operations

    Prior to takeoff the maximum allowable difference between captain’s or first officer’s altitude display and field elevation is ______feet.    
    75 feet
  63. LIMITATIONS 10.19
    RVSM Operations

    The standby altimeter (does / does not) meet altimeter accuracy requirements of
    RVSM airspace.  (Choose one)
    DOES NOT
  64. LIMITATIONS 10.19
    RVSM Operations

    The maximum allowable inflight difference between captain and first officer altitude displays for RVSM operations is _____ feet.
    200 FEET
  65. LIMITATIONS 10.19
    Ground Maneuver Camera System (300ER)

    The ground maneuver cameras (may /may not) be used during takeoff, approach, and landing.  (choose one)
    May not
  66. LIMITATIONS 10.21
    Tank Fuel Temperature

    Tank fuel temperature prior to takeoff must not be less than ___°C or ___°C above the fuel freeze point, whichever is higher.
    -40° C

       3° C
  67. LIMITATIONS 10.21
    Usable Fuel Tank Max. Quantities
    (300ER)

    Main L or R: ____ lbs
    Center:       ____ lbs
    • Main L or R:      69,000 lbs
    • Center:           182,800 lbs
  68. LIMITATIONS 10.21
    Usable Fuel Tank Max. Quantities
    (200ER)

    Main L or R:   _____ lbs
    Center:          _____ lbs
    • Main L or R:   64,100 lbs
    • Center:        174,900 lbs
  69. LIMITATIONS 10.21    MEMORY ITEM
    Fuel Loading

    Main tanks must be scheduled to be ____ if center tank fuel is loaded.
    FULL
  70. LIMITATIONS 10.21    
    Fuel Loading

    NOTE
    The center tank may contain up to _____pounds of fuel with less than full main tanks provided the weight of the fuel in the center tank plus the actual zero fuel weight does not exceed the _________ and the Center of Gravity limits are observed.
    3000 pounds

    Maximum Zero Fuel Weight,
  71. LIMITATIONS 10.22
    Fuel Imbalance Between Main Tanks

    (300ER)
    total main tank fuel >123,000 lbs.   ____ lbs
    total main tank fuel <  90,000 lbs    ____ lbs
    • 3000 lbs
    • 4000 lbs
  72. LIMITATIONS 10.22
    Fuel Imbalance Between Main Tanks

    (200ER)
    total main tank fuel >114,000 lbs.   ____ lbs
    total main tank fuel <  50,000 lbs    ____ lbs
    • 3000 lbs
    • 4000 lbs
  73. LIMITATIONS 10.22
    Refueling Operations

    Do not operate _____ radios during refueling operations. (not an AFM)
    HF radios
  74. END
Author
david130
ID
348567
Card Set
B-777 New Limitations
Description
B777
Updated

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