Limitations Set B (non-bold items) - Frontier Airbus A320

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danandana
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293616
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Limitations Set B (non-bold items) - Frontier Airbus A320
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2016-09-02 20:47:46
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Frontier Airbus A320 Limitations Set
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Frontier Airbus A320 Limitations (Set B) non-Bold items
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  1. WEIGHT: A319 regular
    (a) Max Taxi
    (b) Max Takeoff
    (c) Max Landing
    (d) Max Zero Fuel Weight
    • (a) 155,200
    • (b) 154,320
    • (c) 134,480
    • (d) 125,660
  2. WEIGHT: A319 IGW
    (a) Max Taxi
    (b) Max Takeoff
    (c) Max Landing
    (d) Max Zero Fuel Weight
    • (a) 167,320
    • (b) 166,440
    • (c) 137,780
    • (d) 128,960
  3. WEIGHT: A320 regular
    (a) Max Taxi
    (b) Max Takeoff
    (c) Max Landing
    (d) Max Zero Fuel Weight
    • (a) 170,630
    • (b) 169,750
    • (c) 142,190
    • (d) 134,480
  4. WEIGHT: A320 IGW
    (a) Max Taxi
    (b) Max Takeoff
    (c) Max Landing
    (d) Max Zero Fuel Weight
    • (a) 170,630
    • (b) 169,750
    • (c) 145,500
    • (d) 137,780
  5. WEIGHT: Maximum ZFW (Zero Fuel Weight): (FOM II 2.05 p1)
    A319
    A319 IGW
    A320
    A320 IGW
    • 125,669
    • 128,960
    • 134,480
    • 137,780
  6. Flt Maneuvering Load Acceleration Limits in CLEAN Config  FOM II, 2.05 p1
    -1g to +2.5g
  7. Flt Maneuvering Load Acceleration Limits w/Flaps and/or Slats extended  FOM II, 2.05 p1
    0g to +2g
  8. Maximum Runway Altitude   FOM II, 2.05.2
    9200'
  9. Minimum Runway Width   FOM II, 2.05.2
    100' (30m)

    100 feet (30 meters)
  10. Diversion to a normal runway is recommended in case of:   FOM II,  2.05.3
    • Rudder Jam
    • Rudder Pedal Jam
    • Yam damper fault
    • All failures leading to the loss of nose wheel steering
  11. PRESSURIZATION: Maximum Positive Differential (cabin) Pressure  FOM II,  2.10 p.1
    9.0 psi
  12. PRESSURIZATION: Maximum Negative Differential (cabin) pressure  FOM II, 2.10 p.1
    -1 psi
  13. PRESSURIZATION: Safety Relief Valve Setting  FOM II, 2.10 p.1
    8.6 psi
  14. Below what differential Pressure can the Ram Air Door be opened   FOM II, 2.10.1
    <1 psi. The door won't open, even if selected open, if greater than 1 psi
  15. AVIONICS VENTILLATION: FOM II, 2.10.1
    The airplane electrical system should not be powered for more than ____ (time) without a cooling system when the outside air temperature is above _____.
    • OAT 49o C = No Limitation
    • OAT 55o C = 2 hour limit
    • OAT 60o C = 1 hour limit
    • OAT 64o C = 1/2 hour limit
  16. APU Starter Duty Cycle  FOM II, 2.10.2

    how many cycles allowed?
    cool down period between each?
    cool down after a set of attempted starts?
    • 3 cycles at a time
    • 1 minute cool down between each start
    • 60 minutes after the 3 cycles
  17. APU Limits:   FOM II, 2.10.2

    Maximum N speed
    Maximum EGT
    Max EGT for start below 35,000'
    Max EGT for start above 35,000'
    • 107% max N speed
    • 675o C max EGT
    • 1090o C below 35,000'
    • 1120o C above 35,000'
  18. APU: Maximum Altitude for APU electrical & start.  FOM II, 2.10 p2
    39,000'
  19. APU: Maximum altitude for APU battery start  (FOM II, 2.10 p2)
    25,000'
  20. APU: Maximum Altitude for APU pneumatics (1 pack w/electrical)   FOM II, 2.10 p2
    22,500'
  21. APU: Maximum Altitude for APU assisted Engine Start ... FOM II, 2.10 p2
    20,000'
  22. APU: Maximum Altitude for APU pneumatics (2 packs w/electrical)  ..  FOM II, 2.10 p2
    15,000'
  23. APU: air bleed cannot be used for:  FOM II, 2.10 p2
    wing anti-ice
  24. With an inoperative engine, it is not permitted to use the autopilot to perform non-precision approaches in which modes?   FOM II, 2.10.3
    • FINAL APP
    • NAV V/S
    • NAV/FPA (not applicable on aircaft 205-216, 220, 223 & 227-232, and all A321)
    • Only the FD (Flight Director) use is authorized
  25. Auto land may be conducted when the following conditions are satisfied:   FOM II, 2.10.4
    • CAT II/III runway
    • CAT II/III aircraft
    • crew is CAT II/III trained
    • altitude below 9200' (A319, A320)
    • altitude below 5750' (A321)
    • appropriate ground facilities are operational
    • wind is within limits
    • braking action is fair or better

    • AUTOLAND:
    • NOT authorized on runways >100' wide
    • NOT allowed below -1000' pressure altitude
    • NOT authorized in Fairbanks on acft 203, 223, and 902-949
  26. AUTOLAND required:  (FOM II, 2.10 p4)
    AT or BELOW 2400 RVR or 1/2 mile
  27. AUTOLAND braking action must be:  (FOM II, 2.10 p4)
    Fair or Better
  28. Autobrakes (if available) are required for all Cat III approaches in which settings for what runway lengths?   FOM II, 2.10.4
    • runways less than 8000' - Medium
    • runways 8000' or longer - Low or Medium
  29. Performance Limits below 500'   FOM II, 2.10.5
    glideslope deviation
    localizer deviation
    airspeed limits
    max rate of descent (vertical speed)
    minimum airspeed
    maximum bank angle
    minimum & maximum pitch angle
    • Gildeslope Deviation..... < 1 dot
    • Localizer Deviation....... < 1/4 dot
    • Airspeed........... +/- 5 knots of target
    • Max rate of descent...... 1000 fpm
    • Airspeed not below.......VLS
    • Bank not to exceed.....7o
    • -2.5o </= Pitch </= 10o
    • ------------ END ----------------
  30. MAX continuous load per generator ___
    Max continuous load per TR ___
    FOM II, 2.10.6
    • 100% (90 kva)
    • 200 a
  31. ENGINE THRUST SETTINGS:
    ---------------------
    TOGA limit (normal) __/__ (time & temp)
    TOGA limit w/engine failure __/__ (time & temp)
    ---------------------
    MCT limit ____o C
    Starting limit ____o C
    FOM II,  2.10 p6
    • 5 minutes / 950o C
    • 10 minutes / 950o C
    • ---------------------
    • MCT 915o C
    • Starting 725o C
  32. Engine Oil limits    FOM II, 2.10.6

    Max continuous oil temp
    Max transient oil temp (15 minutes)
    Min starting oil temp
    Min oil temp for takeoff
    • 140o C - Max continuous oil temp
    • 155o C - Max transient oil temp (15 minutes)
    • -40o C - Min starting oil temp
    • -10o C - Min oil temp for takeoff
  33. Engine Starter Limitations  (FOM II, 2.10 p7)
    • 4 cycles, 2 minutes each, maximum
    • 20 seconds re-oiling between each start
    • after 4 cycles, 15 minutes cooling
    • do not engage starter above 20% N2
  34. (Big89) When can/can't you use Reduced Thrust (Flex)   FOM II, 2.10.7
    • "Mel's Cows Perform @ 25%
    • ------------------------
    • MEL's - permitted with inop item
    • Contaminated / slippery runways
    • OAT - not lower than flat rating temp or OAT
    • Windshear - suspected, reported or known
    • Special Departure procedure requires it
    • Performance does/does not allow it
    • @25% - reduction must not exceed 25% of full rated thrust
    •      Not >than ISA +60o C for A319
    •      Not >than ISA +53o C for A320
    •      Not >than ISA +43o C for A321
  35. Fuel Temperature Limits   FOM II, 2.10.8
    lowest temperature 
    highest temperature

    (most limiting - highest of the lows / lowest of the highs)
    • -36o C   (Jet A)
    • 49o C   (Jet B & JP 4)
  36. What is the density/weight of jet fuel?  (FOM II, 2.10 p8)
    6.551 lbs/gal
  37. FUEL IMBALANCE AT TAKEOFF for Inner Tanks (outer tanks balanced) for A319, A320
    FOM II,  2.10 p.9
    • 1100 lbs = short answer
    • -------------------------------------
    • in heavier tank:     max allowed imbalance:
    • Full                           1102 lbs
    • 6613 lbs                    2314 lbs
    • 3196 lbs                    3196 lbs
  38. FUEL IMBALANCE IN FLIGHT & AT LANDING for Inner Tanks (outer tanks balanced) for A319 & A320, FOM II p. 2.10.9
    • 3300 lbs = short answer
    • ---------------------------------
    • in heavier tank:      max allowed imbalance
    • Full                        3306 lbs
    • 9479 lbs                3527 lbs
    • 4960 lbs                4960 lbs
  39. FUEL IMBALANCE AT TAKEOFF for A321
    FOM II, 2.10.10
    • 800 = short answer
    • -----------------------------
    • Fuel Qty, heavier tank:      Max allwd imbal:
    • Full                                     882 lbs
    • 6614 lbs                              882 lbs
    • 1543 lbs                             1543 lbs
  40. FUEL IMBALANCE IN FLIGHT AND AT LANDING for A321, FOM II p. 2.10.10
    • 2900 lbs = short answer
    • --------------------------
    • Fuel in heavier tank ----- Max Imbalance
    • FULL                              2910 lbs
    • 8818 lbs                        3196 lbs
    • 5180 lbs                        5180 lbs
  41. MAX hydraulic pressure   FOM II, 2.10.9
    3200 psi
  42. RNP 10 Oceanic/Remote area operations approved with: ________     FOM II, 2.10.10
    • with GPS PRIMARY
    • without GPS PRIMARY for 6.2 hours following the loss of the second GPS
  43. Minimum Oxygen Pressures for 2/3/4 crew members  (@ 50 deg C)
    FOM II, 2.10.13

    (1) Acft 902-953, 201-219, 228-299
    (2) Acft 954, 220-227, all A321's
    (3) A320 NEO (pilot / pilot + jumpseater)

    (4) crew O2 bottle lasts ___ minutes
    FOM II,  2.10 p.11
    • (1) 600 / 800 / 1000
    • (2) 800 / 1100 / 1400
    • (3) 600 / 800

    • (4) Provides protection against smoke with 100% oxygen for all crew members during 15 minutes at 8000' cabin altitude
    • (worst-case #'s, based on 50o C temps)

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