Limitations Flashcards

1
Q

Max Crosswind Takeoff ___
Max Crosswind Landing ___
Max Tailwind Takeoff 320/321NEO____
321___
Max Tailwind Landing 320/321___

A

Max Crosswind Takeoff 35(gust included)

Max Crosswind Landing 38(gust included)

Max Tailwind Takeoff(320/321NEO) 15 (gust included)
(321CEO) 10 (gust included)

Max Tailwind Landing(320/321) 10 (gust included)

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2
Q

Narrow Runway
Minimum runway width

A

<150’ 45M wide
100’ (227-229) (601-699) /148’ all other

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3
Q

Autoland Wind Restrictions
A/C 213-299, 301-399, 701-799, A/C 601-699
-Headwind____
-Crosswind____
-Tailwind____

A

A/C 213-299, 301-399, 701-799
Headwind 30
Crosswind 15
Tailwind 10

A/C 601-699
Headwind 15
Crosswind 10
Tailwind 10

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4
Q

Autoland
-Prohibited With Breaking Action

A

Autoland
-Prohibited With Breaking Action < MEDIUM

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5
Q

Autopilot Engagement
-After Takeoff/ Go Around With SRS____
-Enroute____
-RNAV Visual
-Non Percision Approach____/____
-Non Autoland Cat I FMA____
-Non Autoland Cat II III FMA____
-Go Around____
-Autoland____

Autoland Required:
Visibility_____/_____

A

Autopilot Engagement
-After Takeoff/ Go Around
With SRS 100’ &at least 5sec after T O
-Enroute 900’
-RNAV Visual 500’
-Non Percision Approach DDA/DA
-Non Autoland Cat I FMA 160’
-Non Autoland Cat II III FMA 80’
-Autoland Rollout/Taxi Speed

Autoland Required:
RVR/visibility is at or below CAT I published minimums

(Notes)

Autoland Required: If the requirements for an autoland are satisfied and the ATIS
reported RVR/visibility is at or below CAT I published minimums, the approach
must be briefed and flown as a CAT II or CAT III autoland except as noted below.
NOTE: If any of the CAT II/III requirements cannot be met, and CAT I or
greater weather conditions are reported and prevail upon arrival at the
airport, the crew may brief and fly the approach to CAT I minimums and a
manual landing.

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7
Q

Severe Turbulence Penetration Speed
-FL____ and Below____
-FL____ and FL____/____
-FL____ and Above____

A

Severe Turbulence Penetration Speed
-FL 200 and Below 250Kts (270Kts,321)
-FL200 and FL310 275Kts (300Kts, 321)
-FL310 and Above .76Mach

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8
Q

Reduced Thrust Prohibited
1____
2.____
3.____

A
  1. Slippery / Contaminated Runway
  2. Suspected / Reported / Indicated Windshear
    (Including Windshear Ahead)
  3. Special Departure Procedures Require TOGA
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9
Q

Speed Limitations
-Max VMO/MMO____/____
-Max Tier Speed____
-Max Tier Speed In a Turn____/____
-Max Cockpit Window Speed____
-Max Flaps 1+F Speed____/____
-Max Flap/Slat Altitude____
-VLO REC/EXT____/____
-Max Wiper Speed____
-VLE____/____

A

Speed Limitations
-Max VMO/MMO 350Kts/M.82
-Max Tier Speed 195Kts
-Max Tier Speed In a
Turn 320/321 167550Lbs/20Kts
-Max Cockpit Window
Speed 200Kts
-Max Flaps 1+F Speed 215Kts/321 225Kts
-Max Flap/Slat Altitude FL200
-VLO REC/EXT 220Kts/250Kts(FL250)
-Max Wiper Speed 230Kts
-VLE 280Kts/M.67

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10
Q

Engine Stabilization Time
-Before Takeoff/After Landing____

A

Engine Stabilization Time:

-Before Takeoff: 320 NIO 3Min
320/321 CEO 2Min
321NEO 5Min (after 2hrs) otherwise 2Min

-After Landing 3Min

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14
Q

Engine
-Start EGT Limit____
-TOGA Time Limit____Engine Out____
-Minimum Oil Temp Takeoff____
-Minimum Oil NEO & CEO____+____

A

Engine
-Start EGT Limit 725deg
-TOGA Time Limit 5min
Engine Out 10min
-Minimum Oil Temp Takeoff 19c 321(NIO) 52C(ecam)
-Minimum Oil
NEO9.0+.5qts hour(10.6min)
CEO 9.5+.5qts hour
321(NEO) 14qts at or >-30
321(NEO) 16.5qts <-30

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15
Q

APPROACH CATEGORY

A

A320 Category C (A321NIO)

A321(CEO) Category D

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16
Q

Maximum altitude for APU battery start

A

FL250(emergency electrical)
FL390 normal electric

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17
Q

Must use Autopilot When

Autoland Required When

A

MUST USE AUTOPILOT:
When visibility is less than 4000 RVR or 3/4, the approach must be flown with the autopilot(s) engaged if operable.

AUTOLAND REQUIRED:
ATIS reported RVR/visibility at or below CAT I Minimums

Furthermore, to minimize the chances of a go around, Frontier policy is to set up and brief for an autoland IF
the reported RVR/visibility is at or below 1/2 mile or 2400 RVR AND all of the requirements for an autoland
can be met (environmental, aircraft approach capability, ground equipment, etc.), the approach will be
briefed and flown as a CAT II or CAT III autoland.

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18
Q

Wind limit:
PASSENGER DOOR OPERATION

CARGO DOOR OPERATIONS

A

PASSENGER DOOR OPERATION 65kts

CARGO DOOR OPERATIONS 40/50kts

(50kts depending on nose into wind or Door on downwind(leeward) side. If winds pick up must be closed by 65kts)

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19
Q

WING SPAN
Sharklet Wing Tip
Normal Wing Tip

TAIL HEIGHT

LENGTH
320
321

A

WING SPAN
Sharklet Wing Tip 117’ 5”
Normal Wing Tip 111’ 10”

TAIL HEIGHT 38’ 7”

LENGTH
320 123, 3”
321 146’

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20
Q

Approach Category

A

A320/321(NEO) C

A321(CEO) only D

21
Q

Stabilized Approach Policy

A

Stabilization Criteria:
1000 ft AFE
-Steady rate of descent not to exceed 1,200 FPM
-On the correct lateral path (“Course”); (± one dot for ILS/LOC,
0.30 NM cross track for RNAV, or 1/2 dot for VOR)*
-On the correct vertical path (“Glidepath”); (± one dot)*
-In the final landing configuration (Landing Gear and Flaps Extended)
-Absent any GPWS Warnings and Cautions

500ft AFE
-Steady rate of descent not to exceed 1,000
-Within -5 to +15 knots of target speed for approach
-Landing checklist complete
-Thrust Stabilized

22
Q

NEO Aircraft
Speed break Limits on approach

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

23
Q

Speed Break Limitation

A

NEO
On approach below 240kts
-Overweight Landing
-GWCG is above 35%

24
Q

NON PRECISION APPROACHES WITH ENGINE-OUT​

A

A/C 701-712: flight director only(non precision) “NO AUTOPILOT”

25
Q

WIND-SHEER

A

WX RADAR: (predictive)
T O-100kts
-5NM ahead
-40deg ahead
~inhibited from 100kts to 50’
-approach caution
~370’-50’
-inhibited below 50’

FAC: (reactive)
-at least config 1
T O
~3 sec after lift off
~1300’ RA
Landing
~1300’ RA
to
~50’ RA

26
Q

Approach Categories (FAA)
Category A:
Category B:
Category C:
Category D:
Category E:

A

Approach Categories (FAA)
Category A: Speed 90 knots or less.
Category B: Between 91 and 120 knots.
Category C: Between 121 and 140 knots.
Category D: Between 141 knots and 165 knots.
Category E: Speed 166 knots or more.

27
Q

LOAD FACTOR

A

Normal and alternate law
+2.5 to -1g clean
+2.0 to 0g dirty (slats/flaps)

28
Q

PITCH PROTECTION

A

Normal law only

30 to -15deg flaps 0 to 3
25 to -15deg flaps full

29
Q

BANK PROTECTION

A

Normal law
0 to 33deg (auto pitch trim)
33 to 67deg (auto turn co-ordination)

Alternate law
>45deg “BANK BANK”

30
Q

HIGH SPEED PROTECTION

A

Normal Law
350/.82M
Positive static stability to 0
Vmo + 4 “OVERSPEED”
Vmo + 6 40deg bank protection
Vmo + 15 auto pilot disconnect
Vmo + 16 pitch 0

Alternate/Direct
Vmo + 4 “OVERSPEED”

31
Q

AOA PROTECTION

A

Normal Law. Alternate law/Direct Law
Vls. Low Speed Stability
Aprot Vls
Afloor Vsw +10 “STALL STALL
Amax