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Frontier Airlines - Flight Training 1/3/17 > Frontier Limitations A320/19/21 > Flashcards

Frontier Limitations A320/19/21 Flashcards

1
Q

LIMITATION Maximum # PAX Seats - A321 - A320

A

A321 - 240 A320 - 190

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2
Q

LIMITATION Flight Load Limits - Clean Configuration Slats and/or Flaps Extended

A

Clean Configuration = -1g to +2.5g Slats and/or Flaps Extended = 0g to +2g

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3
Q

Airport Operations - Runway Slope - Runway Altitude - Minimum Runway Width - Normal Runway Width

A

Runway Slope +/- 2º Runway Altitude 9,200’ Minimum Runway Width 148’/45m (A/C 227- 229, 601-699 100’/30m)

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4
Q

Max Tailwind for Takeoff / Max Tailwind for Landing

A

Takeoff : 15kt — (201-299, 301-399, 601-699)
Takeoff : 10kt — (701-799)

Landing : 10kt — All

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5
Q

Max Crosswind for Takeoff/Landing

A

Takeoff: 35kts Landing: 38kts

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6
Q

Max Wind for PAX Door Ops Max Wind for CARGO Door Ops

A

PAX Door Ops 65kt CARGO Door Ops 40kts/*50kts * if A/C nose into wind or door on leeward side * CARGO door must be closed prior to 65kts

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7
Q

Max Vmo/Mmo

A

350kt/.82 mach

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8
Q

Recommended Turbulent Air Penetration Speeds

A

A319/A320

Below FL200 250kt, FL200 to FL310 275kt, Above FL310 0.76 mach

A321

Below FL200 270kt, FL200 to FL310 300, Above FL310 0.76 mach

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9
Q

Maximum Flap/Slat Speeds Flaps 1 Maximum Flap/Slat Speeds Flaps 1 + F Maximum Flap/Slat Speeds Flaps 2 Maximum Flap/Slat Speeds Flaps 3 Maximum Flap/Slat Speeds Flaps Full (A319/A320)

A

Maximum Flap/Slat Speeds Flaps 1 = 230kt (220-FFP) Maximum Flap/Slat Speeds Flaps 1 + F = 215 kt (205-FFP) Maximum Flap/Slat Speeds Flaps 2 = 200kt (190-FFP) Maximum Flap/Slat Speeds Flaps 3 = 185kt (175-FFP) Maximum Flap/Slat Speeds Flaps Full = 177kt (167-FFP) (Note the Frontier Flap Procedures are VFE next -10 knots)

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10
Q

Maximum Flap/Slat Speeds Flaps 1 Maximum Flap/Slat Speeds Flaps 1 + F Maximum Flap/Slat Speeds Flaps 2 Maximum Flap/Slat Speeds Flaps 3 Maximum Flap/Slat Speeds Flaps Full (701-799)

A

Maximum Flap/Slat Speeds Flaps 1 = 235kt (225-FFP) Maximum Flap/Slat Speeds Flaps 1 + F = 225 kt (215-FFP) Maximum Flap/Slat Speeds Flaps 2 = 215kt (205-FFP) Maximum Flap/Slat Speeds Flaps 3 = 195kt (185-FFP) Maximum Flap/Slat Speeds Flaps Full = 190kt (180-FFP) (Note the Frontier Flap Procedures are VFE next - 10 knots)

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11
Q

Landing Gear Speeds Max. Speed with L/G Extended (VLE) Max. Speed to Extend L/G (VLO ext.) Max. Speed to Retract L/G (VLO ret.)

A

Max. Speed with L/G Extended (VLE) = 280 kt./.67 mach. Speed to Extend L/G (VLO ext.) = 250kt/.60 mach. Speed to Retract L/G (VLO ret.) = 220kt/.54 mach

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12
Q

Max Altitude Slats/Flaps

A

20,000’ MSL

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13
Q

Max Tire Speed

A

195kt Ground Speed

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14
Q

Max Speed Windshield Wiper Ops

A

230kt IAS

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15
Q

Max Speed Cockpit Window OPEN

A

200kt IAS

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16
Q

Taxi Speed (A320; A321) no more than _____ When greater than

A

20kt during a turn / 167,550lbs

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17
Q

Air Cond/Press/Vent Max. Positive Differential Pressure Max. Negative Differential Pressure Safety Relief Valve Setting

A

Max. Positive Differential Pressure = 9.0psi Max. Negative Differential Pressure = -1.0psi Safety Relief Valve Setting = 8.6psi

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18
Q

Avionics Ventilation Without a cooling system, A/C electrical should not be powered for more than ____ hours when OAT exceeds ____°

A

more than 2hours, > 49c

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19
Q

APU Ops. with LOW OIL LEVEL ECAM

A

10 hours Logbook entry NOT required

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20
Q

APU Starter Duty Cycle

A

After 3 starter motor duty cycles, wait 60 mins before a new start attempt.

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21
Q

APU Maximum N

A

107%

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22
Q

APU Maximum EGT (running)

A

675c

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23
Q

APU Maximum EGT for start (below 35,000’)

A

1090c

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24
Q

APU Maximum EGT for start (at or above 35,000’)

A

1120c

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25
Q

APU Max. Altitude APU start using normal electrics

A

39,000’ MSL

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26
Q

APU Max. Altitude APU Battery Start

A

25,000’ MSL

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27
Q

APU Max. Altitude APU Pneumatics (1 Pack w/ electrical)

A

22,500’ MSL

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28
Q

APU Max. Altitude APU Pneumatics (2 Packs w/ electrical)

A

15,000’ MSL

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29
Q

APU Max. Altitude for APU Assisted Engine Start

A

20,000’ MSL

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30
Q

Autopilot Engagement After Takeoff and Go-Around (if SRS is indicated) (SRS = Speed Ref System)

A

Takeoff: 100’ AGL and at least 5s after liftoff

GO-Around (If AP not already engaged) : 100’ AGL

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31
Q

Autopilot Engagement Enroute

A

900’ AGL

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32
Q

Autopilot Engagement RNAV VISUAL APPROACH

A

500’ AGL

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33
Q

Autopilot Engagement Non-Precision Approaches

A

DDA / DA

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34
Q

Autopilot Engagement Non-Autoland ILS with CAT 1 Displayed on FMA

A

160’ AGL

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35
Q

Autopilot Engagement Non-Autoland ILS with CAT 2/3 Displayed on FMA

A

80’ AGL

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36
Q

Autopilot Engagement Autoland ILS (1 or 2 Auto-Pilots)

A

ROLLOUT/Taxi Speed

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37
Q

Auto Flight Limitations Approach must be flown with A/P Engaged

(No longer a limitation ?)

A

Visibility less than 4000 RVR or 3/4 mi. ??

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38
Q

Auto Flight Limitations OPEN DES or DES not permitted

A

Inside FAF or 1000’ AGL on Visual Approach

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39
Q

Auto Flight Limitations Auto Land required when visibility is below

A

2400 RVR or 1/2 mi.

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40
Q

Auto Flight Limitations Minimum Runway Width for Autoland

A

148’/45m

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41
Q

Autolands Prohibited when braking action is less than

A

Medium

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42
Q

Autoland demonstrated for Airport Elevation at/below (205-299, 301-399, 601-699) / (701-799)

A

(9200) / (5750)

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43
Q

Autoland not allowed below ________ pressure alt.

A

-1000 PA

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44
Q

(205-299, 301-399, 701-799) / (601-699) Autoland Wind Restrictions Headwind Crosswind Tailwind Min/Max Wind Correction

A

(205-299, 301-399, 701-799) Headwind 30kt Crosswind 15kt Tailwind 10kt (601-699) Headwind 15kt Crosswind 10kt Tailwind 10kt Min/Max Wind Correction 5/15kt

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45
Q

Autobrake Requirements CAT III Autobrake Requirements - Runway Length less than ______ - Runway Length _____ or longer

A

Less than 8,000’ Medium 8,000’ or greater Low or Medium

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46
Q

Autoland Performance Limits Below 500’ AGL Glideslope Deviation Localizer Deviation Airspeed (vs target) Max Rate of Descent Airspeed not below Bank not to exceed Pitch

A

Glideslope Deviation < one dot
Localizer Deviation < ¼ dot
Airspeed ± 5 kts of target
Max Rate of Descent 1000’/min
Airspeed not below VLS
Bank not to exceed 7º
Pitch -2.5º to +10º

47
Q

Electrical Max. Continuous Load per Generator

A

100% (90 Kva)

48
Q

Electrical Max. Continuous Load per TR

49
Q

Electrical Max. Continuous Load APU Generator

50
Q

Electrical Batteries Rated @

51
Q

Electrical BAT 1 Static Inverter

52
Q

Electrical RAT/Emergency Generator

53
Q

Battery Min. Battery Voltage for APU Start

54
Q

Battery Time to Charge Batteries

A

20 minutes

55
Q

Battery Max. Battery Charge Current

56
Q

Battery When will the Battery Start Charging?

A

At / Blow 26.5 V

57
Q

Battery When does Battery Charging Stop?

A

4 A except in-flight or after APU start and 30 min.

58
Q

When is BAT 1 Static Inverter Active?

A

Batteries are only source of PWR and 1) Abov 50kts with BAT 1/2 PB set to ANY position. 2) Blow 50kts with BAT 1/2 PB set to AUTO position.

59
Q

RAT Extends with loss of which busses? Above what Speed? (RAM Air Turbine)

A

AC 1 and AC 2 100 kts

60
Q

Which Busses Remain Powered During RAT Extension?

A

AC Ess. via BAT 1 Static Inverter DC Ess. via BAT 2

61
Q

Which Buses Are Powered Once Emergency Power is Established?

A

AC Ess. and AC Ess. Shed DC Ess. and DC Ess. Shed via ESS. TR

62
Q

Minimum Speed for Emergency Generator Operation

63
Q

Which EIS Displays Remain Powered during RAT Extension?

A

Captain’s PFD and the EW Display

64
Q

RAT Extension How long to Couple/Extend?

A

8 SECONDS Book = 5-8 seconds

65
Q

Which Additional EIS Displays are Powered Once Emergency Power is Established?

A

Captain’s ND and MCDU

66
Q

Engine Thrust Setting/EGT Limits TakeOff and Go-Around MCT Starting (MAX Continuous Thrust)

A

TakeOff and Go-Around — 950ºC (1060º NEO) for 5 Minutes (10 min. w/Eng. Failure)
MCT — 915ºC (1025º NEO) - No Time Limit
Starting — 725º (NEO 750ºC Ground / 875º C In Flight)

67
Q

Engine Oil Max. Continuous Oil Temp. (205-299, 301-399, 701-799), (601-699)

A

140º C (205-299, 301-399, 701-799), 151º (601-699)

68
Q

Engine Oil Max. Transient Oil Temp. (15 minutes) (205-299, 301-399, 601-699)

A

155º C (205-299, 301-399, 601-699)

69
Q

Engine Oil Min. Starting Oil Temp

A

-40º C (All A/C)

70
Q

Engine Oil Min.Temp. for Takeoff (205-299, 301-399, 701-799) / (601-699)

A

19º C (205-299, 301-399, 701-799)

52º C (601-699)

71
Q

Engine Oil Minimum Oil Quantity (Qts)

A

(205-299, 701-799) 9.5qt + .5qt per every hour of estimated flight time.

(301-399) 9.0 qt + .5 qt per every hour of estimated flight time and not below 10.6 qt.

(601-699) OAT at or above -30 C: 14qt
OAT below -30 C: 16.5qt

72
Q

(205-299, 701-799) / ( 301-399) / (601-699) Engine Start Cycles How Many? Wait Period?

A

(205-299, 701-799) How Many — 4 Consecutive Cycles (three start attempts) 20 Sec Between Cycles for Starter Relubricaton. Wait Period — 15 min. after 4 Cycles. The starter must not be run when N2 is above 20%

(301-399) How Many — 3 Consecutive Cycles (three start attemtps) 60 Sec Between Cycles for Starter Relubrication Wait Period — 15 min. After 3 Cycles. The starter must not be run when N2 is above 63%

(601-699) How Many — 3 Consecutive Cycles (two stat attempts) 35 Sec Between Cycles for Starter Relubrication Wait Period — 15 min. After 3 Cycles. The starer must not be run when N2 is above 20%

73
Q

SOFT GO-AROUND (GA SOFT) is…

A

Prohibited

74
Q 
Maximum N1 (301-399), (205-299, 701-799), (601-699)
Maximum N2 (301-399), (205-299, 701-799), (601-699)
A

N1 — 101% (301-399), 104% (205-299, 701-799), 100-105% (601-699)
N2 — 116.5% (301-399), 105% (205-299, 701-799), 100-105% (601-699)

75
Q

(205-299, 701-799, 601-699) / (301-399) Do Not Engage Starter When N2 is above

A

(205-299, 601-699, 701-799) — 20%
(301-399) — 63%

76
Q

Crossbleed Engine Start during pushback operations is…

A

Prohibited

77
Q

Max. Reverse not be used below

78
Q

Reduced Thrust Not to Exceed ___% of Full Rated TakeOff Thrust.

79
Q

T MAX FLEX (ISA) (205-299, 301-399, 601-699, 701-799)

A

(601-699) ISA + 49c
(205-299) ISA + 53
(301-399) ISA + 55
(701-799) ISA + 43

80
Q

When would you not be allowed to use REDUCED THRUST on takeoff

A

MELsCOWSPERF25% MELS Contaminated / slippery OAT hotter than FLEX temp Windshear reports or in area Special departure procedures Performance will not allow 25% of reduced thrust exceeded.

81
Q

Speed brake limitation

A319 Aircraft and all NEO Aircraft

A

For approach, the use of speed brakes at or below 240 kt is not permitted if:

  • GWCG is above 35% or
  • In overweight landing conditions
82
Q

Fuel Temperature Limits Jet A

A

A GOOD rule of thumb -36+49 is exceed then a review book.. JetA = -36 / +54

83
Q

When using JP4 or JET B, Altitude must be limited to ________’ when wing fuel temp exceeds _____ at engine start

A

25,000 feet and 30c until the center tanks are empty.

84
Q

Minimum Fuel for TakeOff

A

3,300 lbs. - The “WING TK LO LVL” warning must not be displayed on ECAM

85
Q

Max. Allowable Wing Fuel Imbalance @ T/O All A320

A

Inner tanks - outer tanks balanced, Fuel in heavier tank - Full, Max imbalance - 1102 lbs.

Outer tanks (Inner tanks balanced) - 815 lbs

86
Q

Max. Allowable Fuel Imbalance @ T/O. All A321s

A

Fuel in heavier tank (FULL) - Max imbalance - 882

87
Q

Maximum Fuel Imbalance - In Flight and Landing All A320s

A

Inner tanks (Outer tanks balanced) - Full - 3306 lbs

Outer tanks (Inner tanks balanced - 1521 lbs

88
Q

Maximum Fuel Imbalance - In Flight and Landing- All A321s

A

Fuel in heavier tank (Full) - 2910 lbs

89
Q

Max. Hydraulic Pressure

90
Q

Max. Brake Temp. for TakeOff

A

300ºC (Brake Fans OFF)

91
Q

N1 Limit with Parking Brake ON

A

75% (Both Engines)

92
Q

Deflated Tire Taxi Speeds 1 Tire or less Per Gear, 2 Tires on Same Main - Zero on the Other

A

1 Tire or less Per Gear — 7 Kts when turning
2 Tires on Same Main - Zero on the Other — 3 Kts — NWS angle limit 30º

93
Q

Required Navigation Performance 10 (RNP-10)

Minimum navigation equipment required to enter RNAV 10 airspace:

A

Two FMGCs (or one FMGC and one BACK UP NAV)
Two MCDUs
Two IRS
Two NDs
One GPS if the flight time outside radio navaid coverage is longer than:

  • 6.2 hours from the time of IRS ground alignment or
  • 5.7 hours from the time of the last FM position update
94
Q

Crew Oxygen Bottle limits guarantee O2 – During Emergency Descent? Cruise at 10000 feet? (205-299, 701-799 / 301-399, 601-699) Provision with smoke? (ALL)

A

(205-299,701-799) During Emergency Descent = 13 Min Provision on NORMAL (ALL Crew)
During Cruise at 10,000 feet = 107 Min Provision on NORMAL (Two Crew)

(301-399, 601-699) During Emergency Descent = 15 Min Provision on NORMAL (ALL Crew)
During Cruise at 10,000 feet = 105 Min Provision on NORMAL (Two Crew)

or

With smoke at Cabin alt 8000 feet = 15 Min (100% oxygen ALL Crew)

95
Q

When would a diversion to a normal runway be recommended?

A

Loss of anything that might lead to a loss of directional control.

  • Rudder jam
  • Rudder pedal jam
  • Yaw damper system fault
  • Rudder travel Limit system fault
  • All failures leading to the loss of the nose wheel steering
96
Q

Minimum Flight Crew Oxygen @ 50º C (205-216, 228-232), (301-399, 601-699), (227, 233-238, 701-799)

A

Minimum Flight Crew Oxygen @ 50º C (A/C 201-216, 228-232) ROT - 600/800/1000 2 Pilots — 576 PSI (806) 2 Pilots + 1 JS — 744 PSI (1057) 2 Pilots + 2 JS — 933PSI (1339)

Minimum Flight Crew Oxygen @ 50º C (A/C 227, 233-238 and 701-799) ROT 900/1100/1400 2 Pilots — 806 PSI 2 Pilots + 1 JS — 1057 PSI 2 Pilots + 2 JS — 1339 PSI

Minimum Flight Crew Oxygen @ (A/C 301-399) ROT 600/800 CAPT —570 CAPT + 3rd Obs 800, FO — 570, FO + 4th Obs 800

97
Q

When calling the FAs in an emergency what is said.

A

Cabin Advisory or Emergency Preparation (EVAC or BRACE)

TEST
Type of EMER
Escape plan (EVAC/Wait)
Signals - Brace/Remain seated/Evacuate x3
Time remaining until landing

98
Q

How can you check your actual landing performance data

99
Q

Aircraft Dimensions A319/20/21

A 
A319/20/21
Length = 111/123/146ft
Wingspan = 111' 10"/ 117' 5" for sharklet
Tall = 38' 7"
100
Q

Wing turn A319/20

A

A319/20 68/75ft

101
Q

What are your Emergency Items Priority

A

MOEQ
Memory Items
OEB’s
ECAM
QRH

102
Q

Approach Category

A

(205-299, 301-399, 601-699) — Category C
(701-799) — Category D

103
Q

Max Crosswind for Landing

104
Q

Max Crosswind for Takeoff

105
Q

Max Tailwind for Takeoff/Landing

A

Takeoff: (205-299, 301-399, 601-699): 15kts
(701-799): 10kts
Landing All Aircraft: 10kts

106
Q

Icing Conditions (Definition)

A

Icing conditions may be expected when the OAT (on ground) or TAT (in flight) is at or below 10°C, and there is visible moisture in the air (such as clouds, fog with low visibility of one mile or less, rain, snow, sleet, ice crystals) or standing water, slush, ice or snow is present on the taxiways or runways.

107
Q

Slippery Runway (Definition)

A

A Runway that is considered to be more slippery than just a wet surface. This would be the result of freezing rain and/or freezing temperatures.

108
Q

Wet Runway (Definition)

A

A Runway that has a shinny appearance due to a thin layer of water less than 1/8” or 3mm covering 100% of the Runway surface. If there are any dry spots showing on a dying runway with no standing water, the runway is not considered to be wet.

109
Q

Contaminated Runway (Definition)

A

A Runway where more than 25% of the Runway length, within the wild h being used, is covered by standing water or slush more than 1/8” or 3mm deep, or that has an accumulation of snow or ice. A Runway may also be considered contaminated with less than 25% coverage if the contaminate is located prior to the midpoint of the runway.

110
Q

Minimum Oil Pressure

A

Minimum
(205-299, 701-799) 13 psi
(301-399) 17.4 psi
(601-699) 65 psi

111
Q

Contaminated Runway Crosswind Limitations

A

Runway Control/Braking Takeoff Crosswind Landing Crosswind
Condition Code Action Component Component

5 Good 35 38
4 Good to Medium 29 29
3 Medium 25 25
2 Medium to Poor 20 20
1 Poor 15 15
0 Nill Operations Prohibited

112
Q

Narrow Runway Crosswind Limitations

A

Runway Control/Braking Takeoff Crosswind Landing Crosswind
Condition Code Action Component Component

6 Dry 35 38
5 Good 33 33
4 Good to Medium 20 20
3 Medium 15 15
2 Medium to Poor 10 10
1 Poor 10 10
0 Nill Operations Prohibited

113
Q

Terrain Analysis Common

Aircraft Weights

A

A320ceo - 155,000 lbs

A320neo - 165,000 lbs

A321ceo - 167,000 lbs

A321NX - 193,000 lbs

114
Q

Stabilization Criteria (1000/500 ft AFE)

A

Steady rate of descent not to exceed 1,200 FPM (1,000 AFE)
On the correct lateral path (“Course”); (+/- one dot for ILS/LOC, 0.30NM
cross track for RNAV, or 1/2 dor for VOR) (1,000/500 AFE)
On correct vertical path (“Glidepath”); (+/- one dot) (1,000/500 AFE)
In the final landing configuration (Landing Gear and Flaps Extended) (1,000/500 AFE)
Absent any GPWS Warning and Cautions (1,000/500 AFE)
Steady rate of descent not to exceed 1,000 FPM (500 AFE)
Within -5 to +15 knots to target speed for approach (500 AFE)

Frontier Airlines - Flight Training 1/3/17 (7 decks)

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