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

Frontier Limitations A320/19/21 Flashcards

(114 cards)

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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
APU Max. Altitude APU start using normal electrics
39,000' MSL
26
APU Max. Altitude APU Battery Start
25,000' MSL
27
APU Max. Altitude APU Pneumatics (1 Pack w/ electrical)
22,500' MSL
28
APU Max. Altitude APU Pneumatics (2 Packs w/ electrical)
15,000' MSL
29
APU Max. Altitude for APU Assisted Engine Start
20,000' MSL
30
Autopilot Engagement After Takeoff and Go-Around (if SRS is indicated) (SRS = Speed Ref System)
Takeoff: 100' AGL and at least 5s after liftoff GO-Around (If AP not already engaged) : 100' AGL
31
Autopilot Engagement Enroute
900' AGL
32
Autopilot Engagement RNAV VISUAL APPROACH
500' AGL
33
Autopilot Engagement Non-Precision Approaches
DDA / DA
34
Autopilot Engagement Non-Autoland ILS with CAT 1 Displayed on FMA
160' AGL
35
Autopilot Engagement Non-Autoland ILS with CAT 2/3 Displayed on FMA
80' AGL
36
Autopilot Engagement Autoland ILS (1 or 2 Auto-Pilots)
ROLLOUT/Taxi Speed
37
Auto Flight Limitations Approach must be flown with A/P Engaged (No longer a limitation ?)
Visibility less than 4000 RVR or 3/4 mi. ??
38
Auto Flight Limitations OPEN DES or DES not permitted
Inside FAF or 1000' AGL on Visual Approach
39
Auto Flight Limitations Auto Land required when visibility is below
2400 RVR or 1/2 mi.
40
Auto Flight Limitations Minimum Runway Width for Autoland
148’/45m
41
Autolands Prohibited when braking action is less than
Medium
42
Autoland demonstrated for Airport Elevation at/below (205-299, 301-399, 601-699) / (701-799)
(9200) / (5750)
43
Autoland not allowed below ________ pressure alt.
-1000 PA
44
(205-299, 301-399, 701-799) / (601-699) Autoland Wind Restrictions Headwind Crosswind Tailwind Min/Max Wind Correction
(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
45
Autobrake Requirements CAT III Autobrake Requirements - Runway Length less than ______ - Runway Length _____ or longer
Less than 8,000' Medium 8,000' or greater Low or Medium
46
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
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
Electrical Max. Continuous Load per Generator
100% (90 Kva)
48
Electrical Max. Continuous Load per TR
200 amps
49
Electrical Max. Continuous Load APU Generator
90 Kva
50
Electrical Batteries Rated @
23 A-H
51
Electrical BAT 1 Static Inverter
1 Kva
52
Electrical RAT/Emergency Generator
5 Kva
53
Battery Min. Battery Voltage for APU Start
25.5 V
54
Battery Time to Charge Batteries
20 minutes
55
Battery Max. Battery Charge Current
60 A
56
Battery When will the Battery Start Charging?
At / Blow 26.5 V
57
Battery When does Battery Charging Stop?
4 A except in-flight or after APU start and 30 min.
58
When is BAT 1 Static Inverter Active?
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
RAT Extends with loss of which busses? Above what Speed? (RAM Air Turbine)
AC 1 and AC 2 100 kts
60
Which Busses Remain Powered During RAT Extension?
AC Ess. via BAT 1 Static Inverter DC Ess. via BAT 2
61
Which Buses Are Powered Once Emergency Power is Established?
AC Ess. and AC Ess. Shed DC Ess. and DC Ess. Shed via ESS. TR
62
Minimum Speed for Emergency Generator Operation
140 kts
63
Which EIS Displays Remain Powered during RAT Extension?
Captain's PFD and the EW Display
64
RAT Extension How long to Couple/Extend?
8 SECONDS Book = 5-8 seconds
65
Which Additional EIS Displays are Powered Once Emergency Power is Established?
Captain's ND and MCDU
66
Engine Thrust Setting/EGT Limits TakeOff and Go-Around MCT Starting (MAX Continuous Thrust)
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
Engine Oil Max. Continuous Oil Temp. (205-299, 301-399, 701-799), (601-699)
140º C (205-299, 301-399, 701-799), 151º (601-699)
68
Engine Oil Max. Transient Oil Temp. (15 minutes) (205-299, 301-399, 601-699)
155º C (205-299, 301-399, 601-699)
69
Engine Oil Min. Starting Oil Temp
-40º C (All A/C)
70
Engine Oil Min.Temp. for Takeoff (205-299, 301-399, 701-799) / (601-699)
19º C (205-299, 301-399, 701-799) 52º C (601-699)
71
Engine Oil Minimum Oil Quantity (Qts)
(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
(205-299, 701-799) / ( 301-399) / (601-699) Engine Start Cycles How Many? Wait Period?
(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
SOFT GO-AROUND (GA SOFT) is...
Prohibited
74
``` Maximum N1 (301-399), (205-299, 701-799), (601-699) Maximum N2 (301-399), (205-299, 701-799), (601-699) ```
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
(205-299, 701-799, 601-699) / (301-399) Do Not Engage Starter When N2 is above
(205-299, 601-699, 701-799) --- 20% (301-399) --- 63%
76
Crossbleed Engine Start during pushback operations is...
Prohibited
77
Max. Reverse not be used below
70Kts
78
Reduced Thrust Not to Exceed \_\_\_% of Full Rated TakeOff Thrust.
25%
79
T MAX FLEX (ISA) (205-299, 301-399, 601-699, 701-799)
(601-699) ISA + 49c (205-299) ISA + 53 (301-399) ISA + 55 (701-799) ISA + 43
80
When would you not be allowed to use REDUCED THRUST on takeoff
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
Speed brake limitation A319 Aircraft and all NEO Aircraft
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
Fuel Temperature Limits Jet A
A GOOD rule of thumb -36+49 is exceed then a review book.. JetA = -36 / +54
83
When using JP4 or JET B, Altitude must be limited to \_\_\_\_\_\_\_\_' when wing fuel temp exceeds _____ at engine start
25,000 feet and 30c until the center tanks are empty.
84
Minimum Fuel for TakeOff
3,300 lbs. - The "WING TK LO LVL" warning must not be displayed on ECAM
85
Max. Allowable Wing Fuel Imbalance @ T/O All A320
Inner tanks - outer tanks balanced, Fuel in heavier tank - Full, Max imbalance - 1102 lbs. Outer tanks (Inner tanks balanced) - 815 lbs
86
Max. Allowable Fuel Imbalance @ T/O. All A321s
Fuel in heavier tank (FULL) - Max imbalance - 882
87
Maximum Fuel Imbalance - In Flight and Landing All A320s
Inner tanks (Outer tanks balanced) - Full - 3306 lbs Outer tanks (Inner tanks balanced - 1521 lbs
88
Maximum Fuel Imbalance - In Flight and Landing- All A321s
Fuel in heavier tank (Full) - 2910 lbs
89
Max. Hydraulic Pressure
3,200 PSI
90
Max. Brake Temp. for TakeOff
300ºC (Brake Fans OFF)
91
N1 Limit with Parking Brake ON
75% (Both Engines)
92
Deflated Tire Taxi Speeds 1 Tire or less Per Gear, 2 Tires on Same Main - Zero on the Other
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
Required Navigation Performance 10 (RNP-10) Minimum navigation equipment required to enter RNAV 10 airspace:
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
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)
(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
When would a diversion to a normal runway be recommended?
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
Minimum Flight Crew Oxygen @ 50º C (205-216, 228-232), (301-399, 601-699), (227, 233-238, 701-799)
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
When calling the FAs in an emergency what is said.
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
How can you check your actual landing performance data
AWP QRH
99
Aircraft Dimensions A319/20/21
``` A319/20/21 Length = 111/123/146ft Wingspan = 111' 10"/ 117' 5" for sharklet Tall = 38' 7" ```
100
Wing turn A319/20
A319/20 68/75ft
101
What are your Emergency Items Priority
MOEQ Memory Items OEB's ECAM QRH
102
Approach Category
(205-299, 301-399, 601-699) --- Category C (701-799) --- Category D
103
Max Crosswind for Landing
38kts
104
Max Crosswind for Takeoff
35kts
105
Max Tailwind for Takeoff/Landing
Takeoff: (205-299, 301-399, 601-699): 15kts (701-799): 10kts Landing All Aircraft: 10kts
106
Icing Conditions (Definition)
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
Slippery Runway (Definition)
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
Wet Runway (Definition)
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
Contaminated Runway (Definition)
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
Minimum Oil Pressure
Minimum (205-299, 701-799) 13 psi (301-399) 17.4 psi (601-699) 65 psi
111
Contaminated Runway Crosswind Limitations
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
Narrow Runway Crosswind Limitations
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
Terrain Analysis Common Aircraft Weights
A320ceo - 155,000 lbs A320neo - 165,000 lbs A321ceo - 167,000 lbs A321NX - 193,000 lbs
114
Stabilization Criteria (1000/500 ft AFE)
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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