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Limitations > General > Flashcards

General Flashcards

1
Q

Max runway altitude

A

9200 ft

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2
Q

Minimum Runway width

A

100ft/30m A/C 227, 228, 229

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3
Q

Maximum crosswind demonstrated for landing (Normal runway)

A

38kts

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4
Q

Maximum demonstrated crosswind for takeoff

A

35kts

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5
Q

Maximum tailwind for takeoff (201-299, 301-399, 601-699)

A

15kts

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6
Q

Maximum tailwind for landing (All)

A

10kts

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7
Q

What is the difference between a normal and a narrow runway

A

Normal runway = at least 150ft/45m wide

Narrow runway = less then 150ft/45m wide

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8
Q

Maximum demonstrated crosswind for T/O landing (Narrow runway) Dry

A

35kts (Gusts included)

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9
Q

Above what speed do you look up max crosswind on contaminated runway (Normal runway)

A

15kts (Gusts included)

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10
Q

Above what speed do you look up max crosswind on contaminated runway (Narrow runway)

A

10kts (Gusts included)

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11
Q

Max wind for passenger door operation

A

65kts

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12
Q

Max wind for cargo door operation

A

40 kt/*50 kt
* If the aircraft nose is oriented into the wind, or if the cargo door is on the leeward side of the aircraft, operation of the cargo door is permitted in winds up to 50 knots. If wind speed begins to exceed these limitations, the cargo door must be closed before the wind speed exceeds 65 kts.

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13
Q

Maximum VMO/MMO

A

350 kt/.82 mach

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14
Q

SEVERE TURBULENT AIR PENETRATION

SPEED - FL200 and below

A

319/320 — 250kts

321 — 270kts

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15
Q

SEVERE TURBULENT AIR PENETRATION

SPEED - Above FL200 through FL310

A

319/320 — 275 kts

321 — 300 kts

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16
Q

SEVERE TURBULENT AIR PENETRATION

SPEED - Above FL 310

A

.76 Mach

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17
Q

MAXIMUM FLAPS/SLATS SPEEDS

A

Lever Ind Placarded
Position - Flaps - on ECAM -Speeds*(319/320) - (321)
1 0 1 230 235
1 10 1 + F 215 225
2 15 2 200 215
3 20 3 185 195
FULL 40 FULL 177 190

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18
Q

Maximum speed with landing gear extended (VLE)

A

280kts/.67 Mach

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19
Q

Maximum speed at which the landing gear may be extended

Vlo extension

A

250kts

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20
Q

Maximum speed at which the landing gear may be retracted

Vlo retraction

A

220kts

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21
Q

Maximum altitude at which the landing gear may be extended

A

25,000 ft

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22
Q

Maximum Tire Speed (ground speed)

A

195 kts

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23
Q

Maximum speed for use of windshield wipers

A

230 kts

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24
Q

Maximum speed for opening cockpit window

A

200 kts

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25
Q

When the taxi weight is higher than 167,550 lbs do not exceed a taxi speed of…

A

20kts

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26
Q

Max operating altitude with slats and/or flaps extended

A

20,000 ft

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27
Q

Max positive and negative differential pressure

Safety relief valve setting

A

Pos - 9.0 psi
Negative - -1 psi

Safety valve setting - 8.6 psi

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28
Q

APU starter cranking limits

A

After three consecutive APU start attempts, wait 60 min before a new start attempt.

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29
Q

APU Max N

A

107%

NOTE: The APU automatically shuts down at 107% N speed (ECAM display)

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30
Q

APU Maximum EGT

A

675* C

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31
Q

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

A

1090* C

32
Q

APU Maximum EGT for start (above 35,000 feet)

A

1120* C

33
Q

Maximum altitude for APU start using normal electrics & APU operation

A

39,000 ft

34
Q

Maximum altitude for APU battery restart

A

25,000 ft

35
Q

Maximum altitude for APU pneumatics (1 pack w/electrical)

A

22,500 ft

36
Q

Maximum altitude for APU to assist engine start

A

20,000 ft

37
Q

Maximum altitude for APU pneumatics (2 packs w/electrical)

A

15,000 ft

38
Q

APU Air bleed extraction for wing anti-ice is not permitted

A

…

39
Q

Min autopilot altitude - After Takeoff/Go-Around (If SRS is indicated)

A

100 AGL (and at least 5 s after liftoff for takeoff)

40
Q

Min autopilot altitude - Enroute

A

900 AGL

41
Q

Min autopilot altitude - Non-Precision Approaches

A

DDA/DA

42
Q

Min autopilot altitude - Non-Autoland ILS Approach with CAT 1 displayed on FMA

A

160 AGL

43
Q

Min autopilot altitude - Non-Autoland ILS Approach with CAT 2/3 displayed on FMA

A

80 AGL

44
Q

Min autopilot altitude - Autoland ILS Approach (one or two autopilots)

A

Rollout/Taxi speed

45
Q

When visibility is less than 4000 RVR or 3/4, the approach must be flown with:

A

the autopilot(s) engaged if operable.

46
Q

The use of AP or FD in OPEN DES or DES mode is not permitted:

A

inside the FAF or below 1000 ft AGL on a visual approach.

47
Q

When are auto lands prohibited

A

Autolands are prohibited if braking action is reported less than medium.

48
Q

For autolanding, the surface wind conditions are limited to:

A

A/C 205-299, 301-399, 701-799 A/C 601-699

 30        knots of headwind                                                           15     Knots of headwind
 15         knots of crosswind                                                          10     Knots of crosswind
 10         knots of tailwind                                                              10     Knots of tailwind
                           Wind Correction: Vls + wind correction  5 to 15 kts
49
Q

MAX continuous load per generator

A

100% (90 kVA)

50
Q

MAX continuous load per TR

A

200 Amps

51
Q

Maximum continuous oil temperature (A/C 205-299, 301-399, & 701-799)

A

140* C

52
Q

Maximum transient oil temperature (15 minutes) (A/C 205-299, 301-399, & 701-799)

A

155* C

53
Q

Minimum starting oil temperature (All A/C)

A

A319/320/321 -40* C

54
Q

Minimum oil temperature for takeoff

A/C 205-299, 301-399, & 701-799 ___

A/C 601-699 ___

A

A/C 205-299, 301-399, & 701-799 19* C

A/C 601-699 52* C

55
Q

Engine oil quantity
(A/C 205-299 & 701-799)
(A/C 301-399)
(A/C 601-699)

A

A/C 205-299 & 701-799 — 9.5 qt + .5 qt per every hour of estimated flight time

A/C 301-399 — 9.0 qt + .5 qt per every hour of estimated flight time and not below 10.6 qt (1)

A/C 601-699 — OAT at or above -30* C 14 qt
OAT below -30* C 16.5 qt

56
Q

THRUST SETTING/EGT LIMITS - TAKEOFF and GO-AROUND

A

5 min. (Both engines) / EGT limit 950* C (301-399 - 1060C) (601-699 - 1083 C)
10 min. (Only in case of engine failure) / EGT limit 950* C (301-399 - 1060C) (601-699 - 1083 C)

57
Q

THRUST SETTING/EGT LIMITS - MCT

A

Unlimited / EGT Limit 915* C

58
Q

THRUST SETTING/EGT LIMITS - Starting

A

EGT limit 725* C

59
Q

Maximum N1

CEO aircraft
301-399
601-699

A

CEO - 104%
301-399 - 101%
601-699 - Normal ops 100% - Permitted 105%

60
Q

Maximum N2

CEO aircraft
301-399
601-699

A

CEO - 105%
301-399 - 116.5%
601-699 - Normal ops 100% - Permitted 105%

61
Q

Engine starter limitations (A319/320/321) (Not 301-399 or 601-699)

A

– A standard automatic start that includes up to three start attempts, is considered one cycle
– 20 seconds between cycles to allow for starter relubrication.
– After four cycles, 15 minutes to allow starter to cool before
attempting a new start or motoring.
– Do not engage the starter when the N2 is above 20%.

62
Q

Reverse Thrust Limitations

A

– Selecting reverse thrust in flight is prohibited.
– Backing the aircraft with reverse thrust is not permitted.
– Maximum reverse should not be used below 70 knots (Idle reverse is
allowed down to aircraft stop).
– Except in an emergency, reverse thrust is not authorized to reduce
taxi speed.

63
Q

Takeoff at reduced thrust is prohibited:

A
  • on slippery or contaminated runways;
  • when suspected, reported or known wind shear is present (e.g., predictive wind shear alerts, or ATC-Issued wind shear alerts for the departure runway or departure path);
  • when a Special Departure Procedure specifies full thrust for takeoff.
64
Q

Fuel temperature limits

A

Anything hotter then 49* C or colder then -36* C you would look in the book to determine if it’s ok.

65
Q

MAXIMUM ALLOWED WING FUEL IMBALANCE - Full

A

1102 lbs — A319/320/320NEO

882 lbs — A321

66
Q

MAX hydraulic pressure

A

3200 lbs

67
Q

Maximum brake temperature for takeoff

A

300* C

68
Q

Runway slope (mean)

A

+/- 2%

69
Q

Max tailwind for takeoff (321)

A

10kts

70
Q

Engine starter limitations (A/C 301-399)

A

A standard start that includes up to three start attempts, is considered one cycle
A 60 sec pause is required between successive cycles
A 15min cooling period is required subsequent to three failed cycles.
No started engagement above 63% N2

71
Q

Maximum N1 (A/C 301-399)

A

101%

72
Q

Maximum N2 (A/C 301-399)

A

116.50%

73
Q

Minimum oil pressure

A

60 PSI

74
Q

Minimum fuel for T/O

A

3300lbs

75
Q

Maximum starter reengagement RPM
301-399 ___
205-299, 701-799, 601-699 ___

A

301-399 — 59% N2

205-299, 701-799, 601-699 — 20% N2

76
Q

Maximum Engine Oil Temperature (A/C 601-699)

A

151* C

77
Q

Engine starter limitations (A/C 601-699)

A

A standard start that includes up to two start attempts, is considered one cycle
A 35 sec pause is required between successive cycles
A 15 min cooling period is required subsequent to three failed cycles.
No started engagement above 20% N2

Limitations (1 decks)

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