BOMBARBUS C220 LIMITATIONS

  1. Maximum Ramp Weight MRW
    • 101-124: 68 039  KG
    • 125-133: 70 307 KG
  2. Maximum Takeoff Weight MTOW
    • 101-124: 67 585 KG
    • 125-133: 69 853 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. MAX WINDSHIELD WIPER OPERATION
    250 KIAS
  12. TIRE LIMIT SPEED
    195 KNOTS ground speed
  13. MAX Airport P ALT for TO and Land
    10 000 ft
  14. MAX operating ALT
    41 000 ft
  15. MAX TEMP FOR TO & LAND
    52.5 C
  16. MIN TEMP FOR TO & LAND
    -54 C
  17. 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.
  18. 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.
  19. 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.
  20. Speed corrections for approach and landing in icing conditions with FLAP 5:
    Vref, Vac and Vga must be increased by 5 KIAS.
  21. 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.
  22. Electronic Checklist ECL:
    The QRH must be used for Smoke/Fire/Fumes procedure.
  23. Air Conditioning:
    Do not operate PACKS with external AC source being used.
  24. Autopilot Engagement:
    • -Min height for engagement: 400 ft AGL.
    • -Min height for use: 80 ft AGL.
  25. Autoland:
    Autoland not approved for single engine.
  26. MAX SLATS/FLAPS ALT:
    20 000 ft
  27. 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.
  28. MAX FUEL LOAD:
    • L & R main tank: 3050 KG / tank.
    • Center tank: 11300 KG.
    • Total: 17400 KG.
    • MAX imbalance: 454 KG.
    • MIN fuel for GA: 442 KG / wing. Max 10° Nose Up.
  29. FUEL TEMPERATURE:
    • MAX bulk for starting and ops: 52,5 C.
    • Takeoff with bulk fuel T indications blw -37 C is prohibited.
  30. FUEL CROSSFLOW
    Manual transfer and gravity crossflow must be off for Take-off.
  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. 1-AIRPLANE COLD SOAK:
    2-OPS OF THRUST REVERSER IN COLD WEATHER:
    • 1-Found in LIMITATIONS-GERNERAL Cold Weather Operations.
    • 2-Found in LIMITATIONS-POWER PLANT.
  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. Wingspan
    115' 1" / 35,1 M
  43. Length
    127' / 38,7 M
  44. Height
    37' 9" / 11,5 M
  45. Min taxiway width for 180° turn.
    77' 1" / 23,5 M
  46. 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.
  47. Terrain colour on Map display.
    • From 500' blw to 2000' abv a/c alt: Yellow.
    • More than 2000' abv a/c alt: Red.
  48. Extended Overwater Ops and ETOPS
    • Approved for 75 mins ETOPS in Canadian domestic airspace and Benign Area of Ops.
    • Overwater flight legs to remain 400 NM of a suitable landing site.
    • Approved one engine inop cruise speed is 310 KIAS.
    • 60 mins: 390 NM
    • 75 mins: 481 NM
  49. Dimensions:
    • Wingspan:        115' 1" / 35,1 M
    • Length:             127' / 38,7 M
    • Height:              37' 9" / 11,5 M
  50. Structural Weight Limitations
    • Max Ramp Weight:          68 039 KG / 70 307 KG
    • Max TO Weight:               67 585 KG / 69 853 KG
    • Max Land Weight:            57 833 KG
    • Max Zero Fuel Weight:     55 111 KG
    • Min Flight Weight:            36 287 KG
Author
Fredquatorze
ID
354034
Card Set
BOMBARBUS C220 LIMITATIONS
Description
Limitations for the Air Canada A220
Updated