BOMBARBUS C220 LIMITATIONS

  1. Maximum Ramp Weight MRW
    68 039  KG
  2. Maximum Takeoff Weight MTOW
    67 585 KG
  3. Maximum Landing Weight MLW
    57 833 KG
  4. Maximum Zero Fuel Weight MZFW
    55 111 KG
  5. MAX FLAP 1 SPEED
    230 KIAS
  6. MAX FLAP 2 SPEED
    210 KIAS
  7. MAX FLAP 3 SPEED
    210 KIAS
  8. MAX FLAP 4 SPEED
    190 KIAS
  9. MAX FLAP 5 SPEED
    170 KIAS
  10. MAX LANDING GEAR OPERATING SPEED VLO & VLE
    • Extension & VLE: 250 KIAS
    • Retraction: 220 KIAS
  11. TURBULENCE PENETRATION SPEED. (Moderate to Severe)
    • 10000 feet and below: 265 KIAS
    • Above 10000 feet: 280 KIAS / M.75, whichever is lower.
  12. MAX WINDSHIELD WIPER OPERATION
    250 KIAS
  13. TIRE LIMIT SPEED
    195 KNOTS ground speed
  14. MAX Airport P ALT for TO and Land
    8000 ft
  15. MAX operating ALT
    41 000 ft
  16. MAX TEMP FOR TO & LAND
    52.5 C
  17. MIN TEMP FOR TO & LAND
    -54 C
  18. COWL anti-ice must be used when:
    • On ground, ON with: OAT 10 C & blw and:
    • -Visible moisture present (FOG 1sm or blw).
    • -Operating on ground with contamination present.  WET not included. 
    • In flight, AUTO or ON with:
    • -TAT 10 C & blw with visible moisture, except when SAT -40 C or blw.
    • -When in icing conditions.
    • -When ICE is annunciated by the ice detection system.
  19. WING anti-ice must be used when:
    • For Take Off to ON: OAT 5 C & blw with:
    • -Visible moisture present (FOG 1sm or blw).
    • -On for Takeoff with contaminated runway.  WET not included. 

    • In flight, AUTO or ON with:
    • -Icing conditions: TAT 10 C or blw with visible moisture except when SAT is -40 or blw.
    • -When ICE is annunciated by the ice detection system.
    • -DO NOT HOLD WITH FLAPS/SLATS EXTENDED IN ICING CONDITIONS.
    • -WING ANTI-ICE MUST BE SELECTED OFF ABV 35000′.
    • -WING ANTI-ICE ON IS PROHIBITED WHEN TAT ABV 15C.
  20. Engine ICE shedding:
    • -When OAT 3C and blw with visible moisture present.
    • -N1 to 60% every 30 mins.
    • -First run up should be done ASAP. 
    • In flight: Increase thrust up to CLB thrust.
  21. Speed corrections for approach and landing in icing conditions with FLAP 5:
    Vref, Vac and Vga must be increased by 5 KIAS.
  22. Max Tailwind Conditions:
    • Takeoff: 15 knots.  Abv 10 knots, refer to SOP (High Wind Procedure).
    • Landing: 10 knots.  Abv 10 knots, refer to PERF section.
  23. Electronic Checklist ECL:
    The QRH must be used for Smoke/Fire/Fumes procedure.
  24. Air Conditioning:
    Do not operate PACKS with external AC source being used.
  25. Autopilot Engagement:
    • -Min height for engagement: 400 ft AGL.
    • -Min height for use: 80 ft AGL.
  26. Autoland:
    Autoland not approved for single engine.
  27. MAX SLATS/FLAPS ALT:
    20 000 ft
  28. FLIGHT SPOILERS:
    • -MIN height with flight spoilers manually extended: 500 ft AGL.
    • -MIN speed with flight spoilers manually extended: Vref +10 KIAS.
    • -Use of MAX spoilers is prohibited except in an emergency.
  29. MAX FUEL LOAD:
    • L & R main tank: 3050 KG / tank.
    • Center tank: 11300 KG.
    • Total: 17400 KG.
    • MAX imbalance: 363 KG.
    • MIN fuel for GA: 442 KG / wing.
  30. FUEL TEMPERATURE:
    • MAX bulk for starting and ops: 52,5 C.
    • Takeoff with bulk fuel T indications blw -37 C is prohibited.
  31. FUEL TRANSFER:
    Start left engine first if either wing tank abv 2830 KG.
  32. WHEEL BRAKE COOLING LIMITATIONS:
    MAX brake T for TO is 06 units.
  33. Data Link FANS-1/A+
    Use of FANS LOAD within 5 nm of sequencing a waypoint is prohibited.
  34. APU start:
    • -MIN oil T: -40C.
    • -Not more than 3 starts / starts attempts in 1 H.
    • -A 2 mins delay must be observed between start attempts.
  35. APU OPS:
    ALT limit for bleed extraction: 23000 ft.
  36. ENGINE OIL TEMP:
    • BLW -40 C: NO START.
    • BLW -6 C: IDLE.
    • BETWEEN -6 AND 21 C: MAX 30% N1.
    • FROM 21 C TO 49 C: MAX 50% N1.
    • 49 C AND ABV: NO LIMIT.
  37. AIRPLANE COLD SOAK:
    When A/C is cold soaked -20 C or blw for more than 8 H, cycle thrust reversers 2 times before takeoff on wet or contaminated runway.
  38. ENGINE CRANK
    After 3 start attempts, or 4 mins continuous cranking, 30 mins cooling is required.
  39. ENGINE SHUTDOWN
    Engine must be operated at or near idle (up to 40% N1) for at least 3 mins before shutdown.
  40. Engine MAX X-wind / tailwind limits:
    • -Starting and Ice Shedding: 43 knots x-wind.
    • -Starting and Ice Shedding: 18 knots tailwind.
  41. MAX X-WIND:
    • -TAKEOFF: 32 KTS
    • -LANDING: 29 KTS
  42. MAX depth of runway contaminants for Landing:
    • -Standing Water: 0,75 in / 19,1 mm
    • -Slush: 0,88 in / 22,4 mm
    • -Wet Snow: 0,88 in / 22,4 mm
    • -Dry Snow: 3,75 in / 95,3 mm
  43. MAX depth of runway contaminants for Takeoff:
    • -Standing Water: 0,50 in / 12,7 mm
    • -Slush: 0,60 in / 15,0 mm
    • -Wet Snow: 0,75 in / 19,1 mm
    • -Dry Snow: 3,0 in / 76,2 mm
  44. Wingspan
    115' 1" / 35,1 M
  45. Length
    127' / 38,7 M
  46. Height
    37' 9" / 11,5 M
  47. Min taxiway width for 180° turn.
    77' 1" / 23,5 M
  48. Turbulence Penetration Speed.
    • 265 KIAS blw 10000'
    • Lowest of 280 KIAS / M.75 abv 10000'
    • At high alt, maintain Mach between low and high speed buffet.
  49. Terrain colour on Map display.
    • From 500' blw to 2000' abv a/c alt: Yellow.
    • More than 2000' abv a/c alt: Red.
  50. Extended Overwater Ops
    • Approved in Benign Area of Ops.
    • Max diversion distance is 400 NM.
  51. Dimensions:
    • Wingspan:        115' 1" / 35,1 M
    • Length:             127' / 38,7 M
    • Height:              37' 9" / 11,5 M
  52. Structural Weight Limitations
    • Max Ramp Weight:          68039 KG
    • Max TO Weight:               67585 KG
    • Max Land Weight:            57833 KG
    • Max Zero Fuel Weight:     55111 KG
    • Min Flight Weight:            36287 KG
Author
Fredquatorze
ID
354034
Card Set
BOMBARBUS C220 LIMITATIONS
Description
Limitations for the Air Canada A220
Updated