Lear 40/45 Limitations

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Pilot
ID:
57278
Filename:
Lear 40/45 Limitations
Updated:
2011-03-15 13:03:41
Tags:
Lear Learjet Lear45 Lear40 LJ45 LJ40
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Description:
Lear 40/45 Ops Limitations
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  1. Icing conditions exist when OAT on ground & for takeoff is __°C (__°F) or below, or SAT in flight is __°C (__°F) to -__°C (__°F), and visible moisture in any form is present.
    • 10°C (50°F)
    • 10°C (50°F)
    • -40°C (-40°F)
  2. LR45 Max Ramp Weight
    21,750 lbs
  3. LR45 Max Certified Takeoff Weight
    21,500 lbs
  4. LR45 Minimum Flight Weight
    14,000 lbs
  5. LR45 Max Zero Fuel Weight
    16,500 lbs
  6. LR45 Max Certified Landing Weight
    19,200 lbs
  7. LR40 Max Ramp Weight
    21,250 lbs
  8. LR40 Max Certified Takeoff Weight
    21,000 lbs
  9. LR40 Minimum Flight Weight
    13,500 lbs
  10. LR40 Max Zero Fuel Weight
    16,000 lbs
  11. LR40 Max Certified Landing Weight
    19,200 lbs
  12. VMO
    330 KIAS
  13. MMO Primary Display
    • with Mach Trim Operative - .81MI
    • with Mach Trim Inop & A/P engaged - .81MI
    • with Mach Trim Inop & A/P disengaged
    • - 23,400 to 42,000 feet - .76-.78 MI
    • - Above 42,000 feet - .78 MI
  14. VMO Standby Instruments
    325 KIAS
  15. MMO Standby Instruments
    .75 MI
  16. VLO
    200 KIAS
  17. VLE
    260 KIAS
  18. VFE
    • Flaps 8°......250 KIAS
    • Flaps 20°....200 KIAS
    • Flaps 40°....150 KIAS
  19. Turbulent Penetration
    Lowest of .75 M or 230
  20. Vmcg
    • Rudder Boost On, APR On.....102 KIAS
    • Rudder Boost On, APR Off....100 KIAS
  21. Max Takeoff Pressure Altitude
    14,000 feet
  22. Max Takeoff Tailwind Component
    • Aircraft not modified by SB 45-72-1...10 kts
    • Aircraft modified by SB 45-72-1:
    • - 12,000 feet and below...10 kts
    • - Above 12,000 feet.........0 kts
  23. Max En Route Pressure Altitude
    51,000 feet
  24. Max En Route Fuel Load Imbalance
    • 45-002 thru 45-258 and 45-260 not modified by SB 45-28-8...Wings balanced w/in 500 lbs
    • 45-259, 45-261 thru 45-200 and prior modified by SB 45-28-8...Wings balanced w/in 200 lbs
  25. Max Landing Pressure Altitude
    14,000 feet
  26. Max Landing Tailwind Component
    10 kts
  27. Runway Conditions
    • Landing is limited to paved runways
    • Runway Water...3/4 inch (19mm)
  28. Landing Pressurization
    Cabin not pressurized
  29. Max Fuel Load Imbalance for Landing
    Wings balanced within 200 lbs
  30. EICAS Landing Requirements
    SUMRY or FLT page
  31. A minimum of __ minutes must elapse between landing touchdown and selection of takeoff thrust for next takeoff. This does not prohibit touch-and-go landings.
    15 minutes
  32. EICAS or MFD __ or __ page must be selected for takeoff and landing.
    SUMRY or FLT
  33. Do not extend flaps above __ feet.
    18,000 feet
  34. Do not extend gear above __ feet.
    18,000 feet
  35. No __ maneuvers, including __ are approved. Intentional stalls are prohibited above __ feet.
    • Aerobatic
    • Spins
    • 18,000 feet
  36. Autopilot must be __ for takeoff and landing.
    Off
  37. Do not intentionally __ the autopilot
    Overpower
  38. Autopilot Minimum Use Height:
    - Climb, En Route or Descent __ feet AGL
    - Approach __ feet AGL
    • Climb, En Route or Descent...500 feet AGL
    • Approach............................200 feet AGL
  39. Autopilot and Flight Director are approved for __ approaches.
    Cat 1
  40. Starter cooling periods between consecutive uses:
    • After Start Attempt 1; 1 Minute
    • After Start Attempt 2; 2 Minutes
    • After Start Attempt 3; 30 Minutes
  41. ITT Limit APR
    • AR: 963°C
    • BR: 1013°C
  42. ITT Limit T/O
    • AR: 941°C
    • BR: 991°C
  43. ITT Limit MCT
    • AR: 916°C
    • BR: 991°C
  44. ITT Limit MCR
    • AR: 900°C
    • BR: 974°C
  45. ITT Limit Start
    • AR: 941°C
    • BR: 991°C
  46. Tire Limiting Speed (Ground Speed)... __ kts
    165 kts
  47. Do not takeoff or land with wing fuel imbalance greater than __ lbs.
    200 lbs
  48. APU Generator Limits
    Continuous- __ amps
    300 amps
  49. Fuels approved for the main aircraft engines are also approved for the __
    APU
  50. Delta P Pressurization Limits..... __
    +9.9 psid to -0.5 psid
  51. Do not __ with the cabin pressurized.
    Land
  52. Operating the APU during __ refueling is prohibited.
    Gravity Fill
  53. Operating the APU during fluid de-icing/anti-icing is __ .
    Prohibited
  54. Do not takeoff with an -APU FAIL- amber CAS illuminated. In the event the APU automatically shuts down due to and APU failure, a visual inspection of the unit must be conducted prior to __ .
    Flight
  55. HI FLOW must be __ with takeoff power selected , or for landing, anti-icing operations and flight above 30,000 feet.
    Off
  56. ENG Sync must be __ for takeoff, landing and single-engine operation.
    Off
  57. The max amperage from an external power source must be limited to __ amps.
    1,500 amps
  58. Generator output is limited as follows:
    -- Continuous - __ amps
    -- Transient - Higher transient loads for cross-starts and battery charging are __ .
    • 300 amps
    • Authorized
  59. Crew and pax O2 masks are not approved for use above __ feet cabin altitude. Prolonged operation of pax O2 masks above __ feet cabin altitude is not recommended.
    • 40,000 feet
    • 25,000 feet
  60. Rudder boost must be __ for takeoff.
    On
  61. Do not extend spoilers with flaps __ while airborne, except as specified in EMERGENCY and/or ABNORMAL PROCEDURES.
    Extended
  62. Autospoilers must be __ for takeoff and landing, except do not __ autospoilers for training maneuvers where engine failure will be simulated above V1 speed or for touch-and-go landings.
    • Armed
    • Arm
  63. __ __ use Thrust Reversers for backing up aircraft.
    Do not
  64. TR circuit breaker must __ be intentionally pulled in flight, except as specified in QRH.
    Not
  65. Thrust Reverser must not be used for __ __ __ landings.
    touch-and-go
  66. Max reverse thrust usable at speeds down to __ KIAS.
    40 KIAS
  67. Thrust Reversers limited to __ when in MANual mode.
    Idle

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