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Spirit > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Landing Weight

502NK-536NK

A

137,788 lbs

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2
Q

Max Landing Weight

601NK-650NK

A

145,505 lbs

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3
Q

Max Landing Weight

901NK-905NK

A

148,591 lbs

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4
Q

Max Landing Weight

587NK, 588NK, 657NK-683NK

A

171,519 lbs

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5
Q

Max Altitude

A

FL 398

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6
Q

Runway Slope (mean)

A

+/-2%

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7
Q

Runway Altitude

All except 535NK, 536NK

A

9,200 ft

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8
Q

Nominal Runway Width

A

45m (148ft)

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9
Q

Max X-wind Landing

A

38 kt (gust included)

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10
Q

Max Tailwind for Takeoff

A

15 kt

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11
Q

Max Tailwind for Landing

A

10 kt

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12
Q

Max Wind for Passenger Door Operation

A

65 kt

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13
Q

Max Crosswind for Takeoff

901NK-905NK

A

35 kt (gust included)

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14
Q

Vle

A

280kt/M.67

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15
Q

Vlo Extension

A

250kt/M.60

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16
Q

Vlo Retraction

A

220kt/M.54

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17
Q

Max Altitude Landing Gear May Be Extended

A

25,000ft

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18
Q

Windshield Wipers Max Speed

A

230kt

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19
Q

When Taxi Weight Higher than 167,550 lb, taxi speed in a turn
587NK, 588NK, 601NK-905NK

A

20kt

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20
Q

Do not use conditioned air simultaneously from…(to avoid any adverse effects on the air conditioning system)

A

PACKS and LP ground unit

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21
Q

Do not use….when the APU supplies bleed air to avoid any adverse effects to the bleed system

A

HP ground unit

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22
Q

Max positive differential pressure

A

9.0 psi

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23
Q

Max negative differential pressure

A

-1.0 psi

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24
Q

Minimum Height for use of Autopilot

Takeoff with SRS mode

A

100 ft AGL

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25
Q

Minimum Height for use of Autopilot

Straight-in non-precision approach

A

Applicable Minimum

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26
Q

Minimum Height for use of Autopilot

Circling Approach

A

Applicable Circling Minimums -100 ft

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27
Q

Minimum Height for use of Autopilot

ILS Approach when CAT 2 or CAT 3 is not displayed on the FMA

A

160ft AGL

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28
Q

Minimum Height for use of Autopilot

Go-Around (AP or FD engagement)

A

100ft AGL

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29
Q

Minimum Height for Use of Autopilot

All Other Phases

A 
500ft AGL (A319/A320)
900ft AGL (A321)
30
Q

Minimum Height for use of Autopilot

Use of the AP or FD in OPEN DES or DES mode is not permitted in Approach, unless the FCU Altitude is set at or above:

A

Highest of:
Minimum or 500ft (A319/A320)
Minimum or 900ft (A321)

31
Q

NAV mode may be used in the terminal area, provided:

A
  • GPS PRIMARY is available
  • HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or
  • FMS navigation is cross-checked with NAVAID raw data
32
Q

If one engine is inoperative, it is not permitted to use the Autopilot to perform NPAs in the following modes:

A

FINAL APP, NAV V/S, NAV/FPA

Only FD use is permitted

33
Q 
Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out
All Engines Operative(AEO)
And 
One Engine Inoperative (OEI)
N502NK-N536NK
A

(AEO)
Headwind - 20kt
Tailwind - 5kt
Crosswind - 15kt

(OEI)
Headwind - 15kt
Tailwind - 5kt
Crosswind - 10kt

34
Q

Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out
All Engines Operative(AEO)
N601NK-N683NK, N587NK, N588NK

A

Headwind - 30kt
Tailwind - 10kt
Crosswind - 15kt

35
Q

Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out
All Engines Operative(AEO)
N901NK-N905NK

A

Headwind - 20kt
Tailwind - 5kt
Crosswind - 15kt

36
Q

Max operating Altitude with slats and/or flaps extended

A

20,000ft

37
Q

Max Fuel Imbalance at Takeoff, Inner Tanks

502NK-536NK, 601NK-650NK, 901NK-905NK

A

1,102 lb

38
Q

Max Fuel Imbalance In Flight and At Landing, Inner Tanks

502NK-536NK, 601NK-650NK, 901NK-905NK

A

3,306 lb

39
Q

Max Fuel Imbalance in Flight and At Landing

587NK, 588NK, 657NK-683NK

A

2,910 lb

40
Q

Max Fuel Imbalance at Takeoff

657NK-683NK

A

882 lb

41
Q

Max brake temperature for Takeoff (brake fans off)

A

300 C

42
Q

APU Starter duty cycles

A

After 3 starter motor duty cycles, wait 60 min before attempting 3 more cycles

43
Q

EGT limits
Takeoff and Go Around
502NK-536NK, 601NK-650NK

A

5 min, 635 C

10 min, 635 C only in case of engine failure

44
Q

EGT limits
MCT
502NK-536NK, 601NK-650NK
587NK, 588NK, 657NK-683NK

A

Unlimited 610 C

45
Q

EGT limits
Starting
502NK-536NK, 601NK-650NK
587NK, 588NK, 657NK-683NK

A

635 C

46
Q

EGT limits
Takeoff and Go Around
901NK-905NK

A

5 min, 1,083 C

10 min, 1,083 C only in case of engine failure

47
Q

EGT limits
MCT
901NK-905NK

A

Unlimited, 1,043 C

48
Q

EGT limits
Starting
901NK-905NK

A

1,083 C

49
Q

EGT limits
Takeoff and Go Around
587NK, 588NK, 657NK-683NK

A

5 min, 650 C

10 min, 650 C only in case of engine failure

50
Q

Minimum Oil Temperature prior to exceeding idle

502NK-683NK

A

-10 C

51
Q

Minimum Oil Temperature for Starting

502NK-683NK

A

-40 C

52
Q

Minimum Oil Pressure

901NK-905NK

A

65 psi

53
Q

Stater Cycles

502NK-683NK

A

3 consecutive cycles, for manual start, observe a 2 min max start cycle time
Pause 15s between starts
Cooling period, following 3 start attempts or 5 min of continuous cranking wait 30 min

No running engagement if the starter, when N2 is above 10% on ground, or 18% in Flight

54
Q

Starter Cycles

901NK-905NK

A

3 consecutive start attempts, 35s in between each cycle
After 3 cycles, or 15 min of continuous or cumulative cranking: 15 min cooling period

No running engagement of the starter, when N2 is above 20%

55
Q

Maximum reverse should not be used below

A 
70 kt
(Idle reverse is permitted down to aircraft stop)
56
Q

Takeoff on contaminated runway

A

Reduced thrust takeoff is not permitted on contaminated runways

57
Q

Max Crosswind for engine start

A

35kt

58
Q

Vmo/Mmo

A

350kts/M.82

59
Q

Max Tire Ground Speed

A

195 kts

60
Q

Cockpit Window Open Max Speed

A

200 kt

61
Q

Max Continuous Load per Generator

A

100%

90KVA

62
Q

Max Continuous Load per TR

A

200 A

63
Q

For JET A only, if TAT reaches…,monitor the FUEL SD page that the fuel temp remains higher than…

A

-34C, -36C

64
Q

Minimum Fuel Quantity for Takeoff

A

3,307 lb and the WING TK LO LVL warning must not be displayed on the ECAM

65
Q

Fuel Management, tanks must be emptied in the following order:
N502NK-N536NK, N601NK-N628NK

A

Center tank then wing tanks

Takeoff on center tank is prohibited

66
Q

Hydraulic normal operating pressure

A

3,000psi +/- 200

67
Q

Taxi with deflated Tires

If one tire is deflated on one or more gears( maximum of 3 tires) Speed should be limited to

A

7kts

68
Q

Taxi with deflated Tires
If two tires are deflated in the same main gear(the other main gear tires not being deflated) Speed should be limited to…and nose wheel steering angle limited to…

A

3kt and 30*

69
Q

Nosewheel steering limits with hand wheels and for towing and pushback

A

75* when using hand wheels

95* for towing and pushback

70
Q

Tail Strike Pitch Attitude
A319
(Struts Compressed)

A

13.9*

71
Q

Tail Strike Pitch Attitude
A320
(Struts Compressed)

A

11.7*

72
Q

Tail Strike Pitch Attitude
A321
(Struts Compressed)

A

9.7*

Spirit (4 decks)

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