Limitations

  1. Minimum crew
    Pilot; co-pilot
  2. MAXIMUM NUMBER OF SEATS
    MAXIMUM POB
    • 19 (2pilots; 1 attended;
    • 1 observer; 15 pax)
    • 17 persons
  3. Max.RampWeight
    LEGACY 600 S/N up to 591
    and Pre-Mod.
    SB 145LEG-28-0010
    22270kg
  4. MTOW
    LEGACY 600 S/N up to 591
    and Pre-Mod.
    SB 145LEG-28-0010
    22200kg
  5. MLW
    LEGACY 600 S/N 625 up to 591
    and Pre-Mod.
    SB 145LEG-28-0010
    Post-Mod. SB 145LEG-28-0010
    18500kg
  6. MZFW
    LEGACY 600 S/N 625 up to 591
    and Pre-Mod.
    SB 145LEG-28-0010
    Post-Mod. SB 145LEG-28-0010
    16000kg
  7. MLW
    Apt elev
    8500’-9500’
    18000kg
  8. MTOW
    LEGACY 600 S/N 625
    and on or
    Post-Mod. SB 145LEG-28-0010
    22500kg
  9. MRW
    LEGACY 600 S/N 625
    and on or
    Post-Mod. SB 145LEG-28-0010
    22570kg
  10. CG TO (22200)
    LEGACY 600 S/N UP TO 591
    AND PRE-MOD.
    SB 145LEG-28-0010
    • Forward 26,9%
    • Aft 35%
  11. CG LGN (18500)
    LEGACY 600 S/N 625 up to 591
    and Pre-Mod.
    SB 145LEG-28-0010
    Post-Mod. SB 145LEG-28-0010
    • Forward 19,3%
    • Aft 35%
  12. CG TO (22500)
    LEGACY 600 S/N 625
    AND ON OR POST-MOD.
    SB 145LEG-28-0010
    • Fwd 27,5%
    • Aft 35%
  13. Temperature
    FL390
    -65~ -21,5
  14. ISA
    +35
  15. Minimum TAT
    abv FL250
    -45
  16. Vlo for Retraction
    200kts
  17. Vlo for Extention
    250kts
  18. Vle
    250kts
  19. Vmo
    Up to 8000’
    250kts
  20. Vmo
    Fm 10000’
    Up to fl277
    320kts
  21. Mmo
    Fm fl277
    Up to fl390(410)
    0,8
  22. Va
    200kts
  23. Vfe
    Flaps 9
    250kts
  24. Vfe
    Flaps22
    200
  25. Vfe
    Flaps 45
    145kts
  26. MAXIMUM FLAP
    EXTENDED ALTITUDE
    20000’
  27. Maximum Airspeed after
    Takeoff/During Climb
    without Retrimming
    160kts
  28. Maximum Takeoff and
    Landing Tailwind Component
    10kts
  29. DIRECT VISION WINDOW
    Max speed
    140kts
  30. UNPRESSURIZED FLIGHT
    At max Altitude
    10000’
  31. TURBULENT AIR
    PENETRATION SPEED
    Abv 10000’
    250kts
  32. TURBULENT AIR
    PENETRATION SPEED
    At or Blw 10000’
    200kts
  33. Max cross wind
    Dry RW
    30kts
  34. Max cross wind
    Wet RW
    25kts
  35. Max cross wind
    Contaminated
    By compacted snow
    20kts
  36. Max cross wind
    Slush, standing water
    Loose snow
    15kt
  37. Max cross wind
    RW cnted by ICE
    10kts
  38. Load Factor
    Flaps 0
    • Posit 2,51g
    • Negat -1,00g
  39. Load Factor
    Flaps 9;22;45
    • Posit 2,0g
    • Negat 0g
  40. RW slope
    -2%~+2%
  41. WATER EQUIVALENT DEPTH
    • TO 8mm
    • LGN 20mm
  42. Inhibit EGPWS
    by TERRAIN SYS OVRD
    within 15nm if
    • The airport has no approved instrument approach procedure.
    • The airport is not included in the Allied Signal data base.
    • The longest runway is less than 1070 m (3500 ft) in length.
  43. Maximum Load
    on Main Generator
    400A
  44. Maximum Load
    on APU Generator
    • up to FL300 - 400A
    • abv FL300 - 300A
  45. Maximum Battery
    Temperature
    70
  46. Fuel Quantity
    LEGACY 600 S/N UP TO 591
    AND PRE-MOD.
    SB 145LEG-28-0010
    • Wing tank 2587kg(3198l)
    • Total 5174kg (6396l)
    • FUS:
    • FWD 800kg (1056l)
    • AFT 660kg (822l)
    • Total 1460kg (1878l)
  47. FUEL QUANTITY
    LEGACY 600 S/N 625
    and on or
    Post-Mod. SB 145LEG-28-0010
    • Wing tank 2587kg(3198l)
    • Total 5174kg (6396l)
    • FUS:
    • FWD 900kg (1112l)
    • AFT 670kg (822l)
    • Total 1570kg (1934l)
  48. FUEL IMBALANCE
    363kg
  49. UNUSABLE FUEL
    • WING TANK with pumps 18kg(22l)
    • WING TANK no pumps 163kg(203l)
    • FWD 11kg(13,5l)
    • AFT 14kg(17,5l)
  50. FUEL TANK TEMPERATURE
    • Minimum -45
    • Maximum 52
  51. APU T-62T-40C14
    • Alt for Start FL300
    • Ops Alt FL390
    • Rotor spd 108%(104% automatic off)
    • EGT Start 884
    • EGT Cont 680 (732 for 3sec; 717 for 5 min)
  52. Minimum battery
    temperature for APU start
    -20
  53. APU STARTER LIMITS
    • Btn 3 consecutive attempts 1 min off
    • Btn 2 series 30 min off
  54. PRESSURISATION
    AIRPLANES PRE-MOD.
    SB 145LEG-00-0007
    • Maximum differential pressure 8,1psi
    • Maximum differential overpressure 8,4psi
    • Maximum differential negative pressure -0,3psi
  55. PRESSURISATION
    AIRPLANES POST-MOD.
    SB 145LEG-00-0007
    • Maximum differential pressure 8,4psi
    • Maximum differential overpressure 8,6psi
    • Maximum differential negative pressure -0,3psi
Author
Mikle1185
ID
355224
Card Set
Limitations
Description
Updated