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Limitations Flashcards

1
Q

Max Landing Gear Extension Altitude

A

FL250

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2
Q

Landing Gear Max Speeds (RET, EXT, Vle)

A

Vlo RET - 220
Vlo EXT - 250
Vle - 280/.67 M

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3
Q

Turbulent Penetration Speed - abv FL200 to FL310

A

275 kts

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4
Q

Max Flaps/Slats Speeds - 319/320

A 
1 - 230 kts
1 + F - 215 kts
2 - 200 kts
3 - 185 kts
FULL - 177 kts
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5
Q

Takeoff w/ Center Tank Fuel Requirement

A

Takeoff with center tank fuel supplying the engines is PROHIBITED

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6
Q

Max Brake Temp for Takeoff (brake fans off)

A

300˚ C

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7
Q

Avionics Ventilaiton Limits

A

the AC electrical system should not be powered for MORE THAN 2 HOURS w/o a cooling system when the OAT is above 49˚ C

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8
Q

When is Autoland required?

A
  • required below CAT I mins
  • to minimize chances of GA, Frontier policy is to set up and brief for an auto land IF
    • below 1/2 SM and 2400 RVR
    • all requirements for autoland are met (environmental, AC approach capability, ground equip., etc)
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9
Q

Engine Starter Duty Cycles - 320NEO

A

Start Cycle Off
1 60 sec
2 60 sec
3 15 min

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10
Q

AP Min Engagement Height - Autoland Approach

A

Rollout/Taxi Speed

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11
Q

Environmental Envelope/Max Altitude

A

FL390

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12
Q

Reduced Thrust T/O Prohibited (MCOWSP@)

A
  • MEL prevents it
  • Contaminated/slippery runway
  • OAT > Flex
  • Windshear
  • Special Departure Procedure
  • Perfromance does not allow it
  • @ 25% reduction exceeded
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13
Q

Max Engine EGT Starting - 320NEO (Ground/Flight)

A

On Ground - 750˚ C

Inflight - 875˚ C

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14
Q

AP Min Engagement Height - Non-Precision Approach

A

DDA/DA

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15
Q

Max Flaps/Slats Speeds - 321

A 
1 - 235 kts
1 + F - 225 kts
2 - 215 kts
3 - 195 kts
FULL - 190 kts
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16
Q

AP Min Engagement Height - Non-Autoland ILS w/ CAT 2/3 FMA

A

80’ AGL

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17
Q

Max Tire Speed

A

195 kts

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18
Q

Min Fuel Req for T/O

A

3,300 lbs

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19
Q

APU Max Altitudes - for APU start using normal electrics

A

FL390

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20
Q

Flight Maneuvering Load Limits

A
  • Clean = -1.0g to 2.5g
  • Slats = 0g to 2.0g
  • Slats and Flaps = 0g to 2.0g
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21
Q

Pressurization - Cabin Diff for Safety Relief Valve

A

8.6 PSI

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22
Q

Max Flaps/Slats Altitude

A

FL200

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23
Q

Max Windshield Wiper Operations

A

230 KIAS

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24
Q

APU Max Altitudes - 2 pack operation w/ electrical

A

15,000’

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25
Autoland Max Winds - 320/320NEO/321
HW - 30 kts XW - 15 kts TW - 10 kts
26
APU Max Altitudes - For APU start using battery only
FL250
27
Stabilized Approach Policy
@ 1,000' 1. VSI not to exceed 1200 FPM 2. Correct Lateral Path (ILS +/- 1 Dot, RNAV .3 NM, VOR 1/2 Dot) 3. Correct Vertical Path (+/- 1 Dot) 4. Final Landing Config 5. No GPWS Warning/Cautions @500' 5. Steady Rate of Descent no more than 1,000 FPM 6. Within -5 to +15 kts of target airspeed
28
Max TR Load Continuous per TR
200 amps
29
AP Min Engagement Height - RNAV Visual Approach
500' AGL
30
Min Engine Oil Temp for Takeoff
19˚ C
31
AC System Parameters - w/ LP Ground Unit
do not use conditioned air simultaneously form packs and LP ground unit ( to avoid chattering of the non return valves)
32
Engine Reverse Thrust Limits (4)
1. selecting rev thr in flight is prohibited 2. backing the AC w/ rev thr is not permitted 3. max rev will not be used below 70 kts (idle rev thr is allowed down to AC stop) 4. except in emergency, rev thr is not authorized to reduce taxi speed
33
APU Max Altitudes - for engine start
FL200
34
Max Crosswind 319/320/321 T/O and Land
``` T/O = 35 kts Land = 38 kts ```
35
Max Generator Continuous Load Per Generator
100% (90 kVA)
36
Min Engine Oil Pressure
17.4 PSI
37
Runway Limits - Max Slope - Max Altitude - Min Width
- Max Slope = +/- 2% - Max Altitude = 9,200' - Min Width = 100'/30m
38
Max Landing Weights
A319................................134,480 (134,000) A319 IGW.......................137,780 (137,000) A320...............................142,190 (142,000) A320IGW.......................145,500 (145,000) A320NEO.......................148,590 (148,000) A321................................171,520 (171,000)
39
Turbulent Penetration Speed - FL200 and below
250 kts
40
Max Operating HYD Pressure
3,200 PSI
41
Max Thrust Time Limit for T/O and GA
2 Eng - 5 min | 1 Eng - 10 min
42
Ram Air Inlet Limitation
only open if differential pressure is lower 1 PSI
43
Max Engine EGT Starting - 319/320/321
725˚ C
44
AP Min Engagement Height - After T/O if SRS indicated
100' AGL
45
Vmo/Mmo
350/.82 M
46
APU Starter Duty Cycle Time Limits
B/w each start attempt - 1 minute | After 3 attempts - 60 minutes
47
Max Taxi Speed
320/321 = 20 kts during a turn @ 167,550 lbs
48
Min Engine Oil Temp for Starting
``` 320NEO = -29˚ C 319/320/321 = -40˚ C ```
49
AC System Parameters - w/ HP Ground Unit
and external HP source may be used for air conditioning provided the air supply is confirmed to be free from oil contamination. DO NOT USE HP ground unit when APU supplies bleed air to avoid bleed system damage.
50
Max Cockpit Window Speed
200 KIAS
51
AP Min Engagement Height - Enroute
900' AGL
52
Narrow Runway Operations
- Autoland not authorized - Divert to normal width rwy if: 1. rudder jam 2. rudder pedal jam 3. yaw damper fault 4. no NWS 5. any wheel brake inop
53
Approach Category
``` 319/320 = C 321 = D ```
54
Engine Starter Duty Cycles - 319/320/321
``` Start Cycle Off 1 20 sec 2 20 sec 3 20 sec 4 15 min ```
55
Turbulent Penetration Speed - abv FL310
.76 M
56
AP Min Engagement Height - Go-Around w/ SRS indicated
100' AGL
57
AP Min Engagement Height - Non-Autoland ILS w/ CAT I FMA
160' AGL
58
Pax Door Wind Limits
- PAX Max Wind - 65 kts - Cargo Door - 40/50 - if the AC nose door is oriented into the wind, or if the cargo door is on the leeward side of the AC, operation of the cargo door is permitted in winds up to 50 kts, if wind speed begins to exceed these limitations, the cargo door must be closed before the wind speed exceeds 65 kts
59
APU Max Altitudes - 1 pack operation w/ electrical
FL225
60
Max Tailwind 319/320 T/O and Land
``` T/O = 15 kts Land = 10 kts ```
61
Max Tailwind 321 T/O and Land
``` T/O = 10 kts Land = 10 kts ```
62
Autoland Max Winds - 319
HW - 20 kts XW - 15 kts TW - 5 kts

Limitations - BS (1 decks)

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