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Spirit Study Guide > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

0
Q

Wingspans NON SHARKLET

A

111’ 10”

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1
Q

Wingspans SHARKLET 320/321

A

117’ 5”

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3
Q

Max Landing Weight 319 N502NK THRU N534NK

A

137,788

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4
Q

Max Certified Altitude

A

FL398

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4
Q

Max Landing Weight 320 N601NK THRU N617NK

A

145,505

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5
Q

Max Landing Weight 321

A

171,519

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7
Q

Applicable to N502NK THRU N672NK

  • Runway Slope
  • Max Runway Altitude
  • Normal Runway Width
  • Max demonstrated crosswind
A

Applicable to N502NK THRU N672NK

  • Runway Slope ……………………… +/- 2%
  • Max Runway Altitude ……………. 9200
  • Normal Runway Width ………….. 148 (see note)
  • 38 kt (gust included)

NOTE: Narrow runway ops procedures up to 98 ft

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8
Q

Applicable to N502NK THRU N672NK
Wind for takeoff and landing

Max demonstrated cross wind …..
Max Tailwind - Takeoff ………………
Max Tailwind - Landing ……………..

A

Applicable to N502NK THRU N672NK
Max demonstrated cross wind ……………..38 knots
Max Tailwind - Takeoff …………………………15 knots
Max Tailwind - Landing ……………………….. 10 knots

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8
Q 
Landing Gear Speed Limitations
Max Extended 
Max Extension 
Max Retraction 
Max Altitude to Extend
A 
Max Extended (VLE) ............................. 280 kts/M.67
Max Extension (VLO Extension) ........... 250 kts
Max Retraction (VLO Retraction) ......... 220 kts
Max Altitude to Extend ......................... FL250
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9
Q

Max Speed - Windshield Wipers

A

230 kts

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10
Q 
Landing Gear Speed Limitations
Max Extended 
Max Extension 
Max Retraction 
Max Altitude to Extend
Brakes maximum temperature for takeoff
A 
Max Extended (VLE) ............................. 280 kts/M.67
Max Extension (VLO Extension) ........... 250 kts
Max Retraction (VLO Retraction) ......... 220 kts
Max Altitude to Extend ......................... FL250
Brake fans (if installed) off...............300° C
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11
Q

Max Taxi Speed in a Turn (320/321)

A

Taxi Weight higher than 167,550, do not exceed 20 kts

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12
Q

Air Conditioning with LP Ground Unit

A

Do not use A/C from Ground Unit and PACKS simultaneously to avoid chattering of non-return valves

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13
Q

A/C with HP Ground Unit

A

Do not use HP Ground Unit when the APU is supplying bleed air. This avoids bleed system damage

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14
Q

AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot

Takeoff with SRS mode

A

100 ft AGL

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15
Q

Cabin Pressure

Max positive
Max negative
Safety relief valve setting

A

Max positive ………………. 9.0 psi

Max negative ……………… -1.0 psi

8.6 psi

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16
Q

AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot

Straight-in non-precision approach

A

Applicable Minimum

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17
Q

AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot

Circling Approach

A

Applicable Circling Minimums - 100 ft

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18
Q

AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot

ILS approach when CAT2 or CAT3 is not displayed on the FMA

A

160 ft AGL

19
Q

AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot

Go-Around (AP or FD engagement)

A

100 ft AGL

20
Q

AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot

All other phases

A

500 ft AGL (A319/A320)

900 ft AGL (A321)

21
Q

AUTO PILOT FUNCTION
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 500 ft (A319/A320)
Minimum or 900 ft (A321)

22
Q

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

A
  • GPS PRIMARY is available, or
  • HIGH accuracy is displayed, and the appropriate
    RNP is checked or entered on the MCDU, or
  • NAVAID raw data is monitored.
23
Q

Non-Precision Approaches with Engine-Out

A

A319/A321

If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes: FINAL APP, NAV V/S, NAV/FPA.

Only FD use is permitted

24
Q

Max operating altitude with slats and/or flaps extended

A

20,000 ft

26
Q

FUEL IMBALANCE - N618NK thru N649NK, N901NK thru N905NK

Fuel imbalance at TAKE OFF

Inner Tanks (Outer Tanks Balanced)
Tank Fuel Quantity (Heavier Tank)…
Maximum Allowed Imbalance…

A

Tank Fuel Quantity (Heavier Tank)…Full

Maximum Allowed Imbalance…1,102 lbs

26
Q

FUEL IMBALANCE - N587NK thru N588NK

Fuel imbalance IN FLIGHT and AT LANDING

Wing Tanks
Tank Fuel Quantity (Heavier Tank)…
Maximum Allowed Imbalance…

A

Tank Fuel Quantity (Heavier Tank)…Full

Maximum Allowed Imbalance…2,910 lbs

27
Q

FUEL IMBALANCE - N618NK thru N649NK, N901NK thru N905NK

Fuel imbalance IN FLIGHT and AT LANDING

Inner Tanks (Outer Tanks Balanced)
Tank Fuel Quantity (Heavier Tank)…
Maximum Allowed Imbalance…

A

Tank Fuel Quantity (Heavier Tank)…Full

Maximum Allowed Imbalance…3,306 lbs

28
Q

FUEL IMBALANCE - N657NK thru N672NK

Fuel imbalance at TAKE OFF

Wing Tanks
Tank Fuel Quantity (Heavier Tank)…
Maximum Allowed Imbalance…

A

Tank Fuel Quantity (Heavier Tank)…Full

Maximum Allowed Imbalance…882 lbs

29
Q

Maximum brake temperature for takeoff (brake fans off)

A

300°C

30
Q

APU Bleed Extraction/Max Altitude

A

APU Operating 2 PACKS …………… 15,000 ft
APU Operating 1PACK ……………… 20,000 ft

APU Bleed Extraction is not permitted for Wing Anti Ice

30
Q

APU Starter duty cycles

A

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

31
Q

APU Starting Max Altitude

A

Battery Power …………. 25,000 ft

Normal A/C Power …… 41,000 ft

33
Q

OIL

Oil Temperature
Minimum starting temperature…
Minimum prior to exceeding idle…

Oil quantity
Minimum oil quantity…

A

Minimum starting temperature… -40°C
Minimum prior to exceeding idle… -10°C

11 qts + est. consumption (-0.3 qt/hr)

34
Q

OIL
Applicable to N502NK thru N672NK

OIL TEMPERATURE
Minimum starting temperature…
Minimum prior to exceeding idle…
Minimum oil pressure

Oil quantity
Minimum oil quantity…

A

Minimum starting temperature… -40°C
Minimum prior to exceeding idle… -10°C
Minimum oil pressure ….. 60 psi

11 qts + est. consumption (-0.3 qt/hr)

35
Q

STARTER
Applicable to N502NK Thru N672NK

Engine Starter Cycles

Cranking…
Engagement ground/air…

A

3 consecutive cycles:

  • 2 cycles of 2 minutes each,
  • 3rd cycle of 1 minute.

Pause between start attempts: 15 seconds.
Cooling period, following 3 start attempts or 4 minutes of
continuous cranking: 30 minutes

No engagement of starter when N2 is above 10% on ground or 18% in flight

36
Q

REDUCED THRUST TAKE OFF

A

Take off at reduced thrust is not permitted on contaminated runways

37
Q

REVERSE THRUST

Maximum reserve should not be used below…

Applicable to N502NK thru N534NK and N601NK thru N646NK

Maximum reverse should not be used when…

A

…70 knots

…Airspeed indication starts to fluctuate

Idle reverse is permitted down to aircraft stop

38
Q

Max Landing Weight 320 Neo N901NK THRU N905NK

A

148,591 lb

39
Q

CROSSWIND OPERATION ON GROUND
Applicable to N502NK thru N672NK

-STARTING

A

This engine is capable of starting in crosswinds up to 35 knots

40
Q

Airport Operations and Wind Limitations
Applicable to Neo N901NK THRU N905NK

  • Runway slope
  • Runway altitude
  • Nominal runway width
  • Max certified crosswind for takeoff
  • Max demonstrated crosswind for landing
  • Max tailwind for takeoff
  • Max tailwind for landing
  • Max wind for passenger door operation

Note: Maximum tailwind for automatic landing and rollout remains 10 kt

A
  • +/- 2%
  • 6,000 ft
  • 45 m (148 ft)
  • 35 kt (gust included)
  • 38 kt (gust included)
  • 15 kt
  • 10 kt
  • 65 kt
41
Q

Maximum Wind Conditions for CAT II or CAT III Automatic Approach, Landing, and Roll Out

Applicable to (Neo) N901NK THRU N905NK

  • Headwind
  • Cross wind
  • Tail wind
A

Maximum Wind Conditions for CAT II or CAT III Automatic Approach, Landing, and Roll Out

Applicable to (Neo) N901NK THRU N905NK

  • 20 kt
  • 5 kt
  • 15 kt
42
Q

Fuel Temperatures

A

Fuel Temperatures

For Jet A only, it TAT reaches -34° C, monitor on FUEL SD page that fuel temperature remains higher than -36° C

43
Q

Power Plant - Thrust Setting/EGT Limits
Applicable to N901NK Thru N905NK (Neo)

Starting -
T/O & G/A (A320 Neo) -
T/O & G/A (A320 Neo) -
MCT -

A

Starting .……………………………… No Limit 1018° C
T/O & G/A ………………….. 1083° pC
(5 min 2ENG/10 min 1EO)
(5 min 2ENG/10 min 1EO) only in case of engine failure
MCT ………………………………………………. 1043° C

44
Q

OIL
Applicable to N901NK thru N905NK

OIL TEMPERATURE
Minimum starting temperature…
Minimum oil pressure
Maximum oil pressure

A

Minimum starting temperature… -40° C
Minimum oil pressure….. 65 psi
Maximum oil pressure

45
Q

STARTER
Applicable to N901NK Thru N905NK (Neo)

Engine Starter Cycles

Cranking…

Starter engagement ground/air…

A

3 consecutive start attempts, 35 s between each cycle

After 3 cycles, or after 15 min of continuous or cumulative cranking:
A 15 min cooling period is necessary before a new start motoring cycle is attempted.

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

46
Q

CROSSWIND OPERATION
Applicable to N901NK thru N905NK

Takeoff

A

Engine crosswind limited at takeoff: 35 kt (gust included)

Spirit Study Guide (3 decks)

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