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Spirit Airlines - Study Guide (02/23/2024) > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

CLEAN CONFIGURATION

NOT BOLD

A

-1 G TO +2.5 G

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2
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

OTHER CONFIGURATIONS

NOT BOLD

A

0 G TO +2 G

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3
Q

KIND OF OPERATIONS

NOT BOLD

A

TRANSPORT CATEGORY (PASSENGERS AND FREIGHT)

DAY AND NIGHT

VFR AND IFR

EXTENDED OVERWATER FLIGHT

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4
Q

MINIMUM FLIGHT CREW

NOT BOLD

A

2 PILOTS

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5
Q

WINGSPANS

A319 / A320 CEO (NON SHARKLET)

NOT BOLD

A

111 FEET, 10 INCHES

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6
Q

WINGSPANS

A320 CEO SHARKLET / A320 NEO SHARKLET / A321 CEO SHARKLET / A321 NEO SHARKLET

A

117 FEET, 5 INCHES

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7
Q

GROUND CLEARANCE TABLE
(TAILSTRIKE PITCH ATTITUDE)

A319

A

L/G STRUTS COMPRESSED

13.9 DEGREES

L/G STRUTS EXTENDED NOT BOLD

15.5 DEGREES

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8
Q

GROUND CLEARANCE TABLE
(TAILSTRIKE PITCH ATTITUDE)

A320 CEO

A

L/G STRUTS COMPRESSED

11.7 DEGREES

L/G STRUTS EXTENDED NOT BOLD

13.5 DEGREES

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9
Q

GROUND CLEARANCE TABLE
(TAILSTRIKE PITCH ATTITUDE)

A320 NEO

A

L/G STRUTS COMPRESSED

11.7 DEGREES

L/G STRUTS EXTENDED NOT BOLD

13.7 DEGREES

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10
Q

GROUND CLEARANCE TABLE
(TAILSTRIKE PITCH ATTITUDE)

A321 CEO / A321 NEO

A

L/G STRUTS COMPRESSED

9.7 DEGREES

L/G STRUTS EXTENDED NOT BOLD

11.2 DEGREES

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11
Q

MAXIMUM CERTIFIED ALTITUDE

A

FL398

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12
Q

RUNWAY SLOPE (MEAN)

NOT BOLD

A

+/- 2 %

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13
Q

RUNWAY ALTITUDE

NOT BOLD

A

9,200 FEET

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14
Q

NOMINAL RUNWAY WIDTH

NOT BOLD

A

45 METERS (148 FEET)

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15
Q

MINIMAL RUNWAY WIDTH

NOT BOLD

A

30 METERS (99 FEET)

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16
Q

MAXIMUM DEMONSTRATED CROSSWIND

TAKEOFF AND LANDING

A

38 KNOTS (GUST INCLUDED)

NOTE:

-THE MAXIMUM DEMONSTRATED CROSSWIND VALUE IS NOT AN AIRPLANE FLIGHT MANUAL (AFM) LIMITATION : IT IS THE MAXIMUM CROSSWIND CONDITION EXPERIENCED DURING THE AIRCRAFT CERTIFICATION CAMPAIGN.

-SPIRIT AIRLINES HAS ADOPTED THIS MAXIMUM DEMONSTRATED VALUE OF 38 KNOTS AS A LIMITATION FOR SPIRIT FLIGHT CREWS FOR TAKEOFF AND LANDING.

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17
Q

MAXIMUM TAILWIND FOR TAKEOFF

A

15 KNOTS

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18
Q

MAXIMUM TAILWIND FOR LANDING

A

10 KNOTS

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19
Q

MAXIMUM WIND FOR PASSENGER DOOR OPERATION

NOT BOLD

A

65 KNOTS

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20
Q

MAXIMUM WIND FOR FWD AND AFT CARGO DOOR OPERATION

NOT BOLD

A

40 KNOTS

(OR 50 KNOTS, IF THE AIRCRAFT NOSE IS INTO THE WIND, OR THE FWD AND AFT CARGO DOORS ARE ON THE LEEWARD SIDE.)

THE FWD AND AFT CARGO DOORS MUST BE CLOSED BEFORE THE WIND EXCEEDS 65 KNOTS

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21
Q

TAKEOFF LIMITATIONS ON CONTAMINATED RUNWAYS

TAKEOFF IS NOT RECOMMENDED ON THE FOLLOWING RUNWAY CONDITIONS:

NOT BOLD

A

WATER ON TOP OF COMPACTED SNOW

DRY SNOW OR WET SNOW OVER ICE

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22
Q

TAKEOFF LIMITATIONS ON CONTAMINATED RUNWAYS

TAKEOFF IS NOT PERMITTED ON THE FOLLOWING RUNWAY CONDITIONS:

NOT BOLD

A

WET ICE

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23
Q

MAXIMUM COCKPIT WINDOW OPEN SPEED

NOT BOLD

A

200 KNOTS

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24
Q

MAXIMUM OPERATING SPEED VMO/MMO

NOT BOLD

A

VMO - 350 KNOTS

MMO - MACH 0.82

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25
Q

MAXIMUM SPEED WITH LANDING GEAR EXTENDED (VLE)

NOT BOLD

A

280 KNOTS / MACH 0.67

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26
Q

MAXIMUM LANDING GEAR EXTENSION SPEED (VLO EXTENSION)

NOT BOLD

A

250 KNOTS / MACH 0.60

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27
Q

MAXIMUM LANDING GEAR RETRACTION SPEED (VLO RETRACTION)

NOT BOLD

A

220 KNOTS / MACH 0.54

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28
Q

MAXIMUM TIRE SPEED

NOT BOLD

A

195 KNOTS GROUNDSPEED

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29
Q

APPLICABLE TO A320 CEO

WHEN THE TAKEOFF WEIGHT IS HIGHER THAN (_____):

CAUTION: DO NOT EXCEED A TAXI SPEED OF (_____) DURING A TURN.

A

167,550 POUNDS (76,000 KILOGRAMS) / 20 KNOTS

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30
Q

MAXIMUM WINDSHIELD WIPER OPERATING SPEED

A

230 KNOTS

NOTE: THIS LIMITATION IS APPLICABLE WHEN THE WIPERS ARE SWEEPING. IT IS NOT APPLICABLE IF THE WIPERS ARE NOT SWEEPING FOR ANY REASONS.

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31
Q

MAXIMUM ALTITUDE LANDING GEAR MAY BE EXTENDED

A

25,000 FEET

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32
Q

MAXIMUM LANDING WEIGHT

A319

NOT BOLD

A

137,788 POUNDS

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33
Q

MAXIMUM LANDING WEIGHT

A320 CEO

NOT BOLD

A

145,505 POUNDS

34
Q

MAXIMUM LANDING WEIGHT

A320 NEO

NOT BOLD

A

148,591 POUNDS

35
Q

MAXIMUM LANDING WEIGHT

A321 CEO

NOT BOLD

A

171,519 POUNDS

36
Q

MAXIMUM LANDING WEIGHT

A321 NEO

NOT BOLD

A

174,606 POUNDS

37
Q

APU BLEED USE WITH AIR START UNIT

A

THE FLIGHT CREW MUST NOT USE BLEED AIR FROM THE APU BLEED AND FROM THE HP AIR START UNIT AT THE SAME TIME, TO PREVENT ANY ADVERSE EFFECT ON THE BLEED AIR SYSTEM.

38
Q

CABIN PRESSURE

MAXIMUM POSITIVE DIFFERENTIAL PRESSURE

NOT BOLD

A

9.0 PSI

39
Q

CABIN PRESSURE

MAXIMUM NEGATIVE DIFFERENTIAL PRESSURE

NOT BOLD

A

-1.0 PSI

40
Q

CABIN PRESSURE

SAFETY RELIEF VALVE SETTING

NOT BOLD

A

8.6 PSI

41
Q

NOTE: THE RAM AIR INLET MUST ONLY BE OPENED WHEN THE CABIN DIFFERENTIAL PRESSURE IS LESS THAN (_____)

NOT BOLD

A

+1 PSI

42
Q

PACKS USE WITH LP AIR CONDITIONING UNIT

A

THE FLIGHT CREW MUST NOT USE CONDITIONED AIR FROM THE PACKS AND FROM THE LP AIR CONDITIONING UNIT AT THE SAME TIME, TO PREVENT ANY ADVERSE EFFECT ON THE AIR CONDITIONING SYSTEM.

43
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

AT TAKEOFF

A

100 FEET AGL AND AT LEAST 5 SECONDS AFTER TAKEOFF

44
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

IN APPROACH WITH F-G/S MODE

A

250 FEET AGL

45
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

IN APPROACH WITH FINAL APP, V/S OR FPA MODE

A

250 FEET AGL

46
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

IN CIRCLING APPROACH

A

600 FEET AGL

47
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

ILS/MLS APPROACH WHEN CAT1 IS DISPLAYED ON THE FMA

A

160 FEET AGL

48
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

ILS/MLS APPROACH WHEN CAT2 OR CAT3 SINGLE OR CAT3 DUAL IS DISPLAYED ON THE FMA

A

0 FEET AGL IF AUTOLAND

49
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

LPV APPROACH (WITH SLS) WHEN APPR1 IS DISPLAYED ON THE FMA

A

160 FEET AGL

50
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

AFTER A MANUAL GO-AROUND

A

100 FEET AGL

51
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

IN ALL OTHER PHASES

A

500 FEET AGL (A319 / A320 CEO / A320 NEO)

900 FEET AGL (A321 CEO / A321 NEO)

52
Q

MINIMUM USE HEIGHT FOR AUTOPILOT

THE AP OR FD IN OP DES OR DES MODE CAN BE USED IN APPROACH. HOWEVER, ITS USE IS ONLY PERMITTED IF THE FCU SELECTED ALTITUDE IS SET TO, OR ABOVE, THE HIGHER OF THE TWO:

A

HIGHEST OF:

MDA/MDH OR 500 FEET AGL (A319 / A320 CEO / A320 NEO)

MDA/MDH OR 900 FEET AGL (A321 CEO / A321 NEO)

53
Q

USE OF NAV MODE

NAV MODE MAY BE USED IN THE TERMINAL AREA PROVIDED THAT:

NOT BOLD

A

GPS PRIMARY IS AVAILABLE, OR

THE APPROPRIATE RNP IS CHECKED OR ENTERED ON THE MCDU, AND HIGH ACCURACY IS DISPLAYED, OR

FMS NAVIGATION IS CROSSCHECKED WITH NAVAID RAW DATA.

54
Q

APPLICABLE TO A319 / A321 CEO

IF ONE ENGINE IS INOPERATIVE, IT IS NOT PERMITTED TO USE THE AUTOPILOT TO PERFORM NPAS IN THE FOLLOWING MODES:

NOT BOLD

A

FINAL APP

NAV V/S

NAV/FPA

ONLY FD USE IS PERMITTED

55
Q

APU START

A

AFTER THREE CONSECUTIVE APU START ATTEMPTS, THE FLIGHT CREW MUST WAIT 60 MINUTES BEFORE A NEW START ATTEMPT.

56
Q

APPLICABLE TO A319 / A320 CEO

THRUST SETTING / EGT LIMITS

A

TAKEOFF(1) AND GO-AROUND

5 MINUTES (ALL ENGINES OPERATIVE)
10 MINUTES (ONE ENGINE INOPERATIVE)
635 DEGREES CELSIUS

MAXIMUM CONTINUOUS THRUST (MCT)

NOT LIMITED
610 DEGREES CELSIUS

STARTING NOT BOLD

NOT LIMITED
635 DEGREES CELSIUS

(1) INCLUDES TOGA, FLEX AND DERATE THRUST MODES.

57
Q

APPLICABLE TO A321 CEO

THRUST SETTING / EGT LIMITS

A

TAKEOFF(1) AND GO-AROUND

5 MINUTES (ALL ENGINES OPERATIVE)
10 MINUTES (ONE ENGINE INOPERATIVE)
650 DEGREES CELSIUS

MAXIMUM CONTINUOUS THRUST (MCT)

NOT LIMITED
610 DEGREES CELSIUS

STARTING NOT BOLD

NOT LIMITED
635 DEGREES CELSIUS

(1) INCLUDES TOGA, FLEX AND DERATE THRUST MODES.

58
Q

APPLICABLE TO A320 NEO / A321 NEO

THRUST SETTING / EGT LIMITS

A

TAKEOFF(1) AND GO-AROUND

5 MINUTES (ALL ENGINES OPERATIVE)
10 MINUTES (ONE ENGINE INOPERATIVE)
1,083 DEGREES CELSIUS

MAXIMUM CONTINUOUS THRUST (MCT)

NOT LIMITED
1,043 DEGREES CELSIUS

STARTING NOT BOLD

NOT LIMITED
1,083 DEGREES CELSIUS

(1) INCLUDES TOGA, FLEX AND DERATE THRUST MODES.

59
Q

APPLICABLE TO A319 / A320 CEO / A321 CEO

MINIMUM OIL STARTING TEMPERATURE

A

-40 DEGREES CELSIUS

60
Q

APPLICABLE TO A319 / A320 CEO / A321 CEO

MINIMUM OIL TEMPERATURE BEFORE IDLE IS EXCEEDED

A

-10 DEGREES CELSIUS

61
Q

APPLICABLE TO A319 / A320 CE0 / A321 CEO

MINIMUM OIL TEMPERATURE BEFORE TAKEOFF

NOT BOLD

A

50 DEGREES CELSIUS

62
Q

APPLICABLE TO A319 / A320 CEO / A321 CEO

MINIMUM OIL QUANTITY

NOT BOLD

A

11 QUARTS + ESTIMATED CONSUMPTION
AVERAGE ESTIMATED CONSUMPTION = 0.3 QUARTS/HOUR

63
Q

APPLICABLE TO A319 / A320 CEO / A321 CEO

MINIMUM OIL PRESSURE

NOT BOLD

A

60 PSI

64
Q

APPLICABLE TO A320 NEO / A321 NEO

MINIMUM OIL STARTING TEMPERATURE

NOT BOLD

A

-40 DEGREES CELSIUS

65
Q

APPLICABLE TO A320 NEO / A321 NEO

MINIMUM OIL TEMPERATURE BEFORE TAKEOFF

NOT BOLD

A

52 DEGREES CELSIUS

66
Q

APPLICABLE TO A320 NEO / A321 NEO

MINIMUM OIL QUANTITY

NOT BOLD

A

OAT AT OR ABOVE -30 DEGREES CELSIUS = 14 QUARTS

OAT BELOW -30 DEGREES CELSIUS = 16.5 QUARTS

67
Q

APPLICABLE TO A320 NEO / A321 NEO

MINIMUM OIL PRESSURE

NOT BOLD

A

65 PSI

68
Q

APPLICABLE TO A319 / A320 CEO / A321 CEO

STARTER

NOT BOLD

A

A STANDARD AUTOMATIC START THAT INCLUDES ONLY ONE START ATTEMPT, IS CONSIDERED ONE CYCLE

FOR GROUND STARTS (AUTOMATIC OR MANUAL), A 15 SECOND PAUSE IS REQUIRED BETWEEN SUCCESSIVE CYCLES

A 30 MINUTE COOLING PERIOD IS REQUIRED, SUBSEQUENT TO THREE FAILED CYCLES OR 5 MINUTES OF CONTINUOUS CRANK

FOR MANUAL START, OBSERVE A TWO-MINUTE MAXIMUM CYCLE TIME

FOR CRANK, OBSERVE A 5 MINUTE MAXIMUM CYCLE TIME

THE STARTER MUST NOT BE RUN WHEN N2 IS ABOVE 10 % ON-GROUND AND 18 % IN-FLIGHT.

69
Q

APPLICABLE TO A320 NEO / A321 NEO

STARTER

NOT BOLD

A

A STANDARD AUTOMATIC START THAT INCLUDES UP TO TWO START ATTEMPTS, IS CONSIDERED ONE CYCLE

FOR GROUND STARTS (AUTOMATIC OR MANUAL), A 35 SECOND PAUSE IS REQUIRED BETWEEN SUCCESSIVE CYCLES

A 15 MINUTE COOLING PERIOD IS REQUIRED, SUBSEQUENT TO THREE FAILED CYCLES, OR 15 MINUTES OF CONTINUOUS OR CUMULATED CRANK

THE STARTER MUST NOT BE RUN WITH N2 IS ABOVE 20 %.

70
Q

REVERSE THRUST

A

MAXIMUM REVERSE SHOULD NOT BE USED BELOW 70 KNOTS. IDLE REVERSE IS PERMITTED DOWN TO AIRCRAFT STOP.

SELECTION OF THE REVERSE THRUST IS PROHIBITED IN FLIGHT. NOT BOLD

BACKING THE AIRCRAFT WITH REVERSE THRUST IS NOT PERMITTED. NOT BOLD

71
Q

APPLICABLE TO A319 / A320 CEO / A320 NEO / A321 CEO / A321 NEO

REDUCED THRUST TAKEOFF

A

FLEX TAKEOFF IS NOT PERMITTED ON CONTAMINATED RUNWAYS.

72
Q

CROSSWIND OPERATION ON GROUND

ENGINE START

A

THE ENGINE IS ABLE TO START IN CROSSWIND UP TO 35 KNOTS.

73
Q

MAXIMUM OPERATING ALTITUDE WITH SLATS AND/OR FLAPS EXTENDED

A

20,000 FEET

74
Q

FUEL TEMPERATURE

(1) FOR JET A ONLY, IF TAT REACHES (_____), MONITOR THE FUEL TEMPERATURE ON THE FUEL SD PAGE, TO ENSURE THAT IT REMAINS ABOVE (_____).

A

-34 DEGREES CELSIUS / -36 DEGREES CELSIUS

75
Q

APPLICABLE TO A319 / A320 CEO / A320 NEO

FUEL IMBALANCE AT TAKEOFF

INNER TANKS (OUTER TANKS BALANCED)

A

TANK FUEL QUANTITY
(HEAVIER TANK)

FULL

MAXIMUM ASYMMETRY

1,102 POUNDS (500 KILOGRAMS)

76
Q

APPLICABLE TO A319 / A320 CEO / A320 NEO

FUEL IMBALANCE IN FLIGHT AND AT LANDING

INNER TANKS (OUTER TANKS BALANCED)

NOT BOLD

A

TANK FUEL QUANTITY
(HEAVIER TANK)

FULL

MAXIMUM ASYMMETRY

3,306 POUNDS (1,500 KILOGRAMS)

77
Q

APPLICABLE TO A321 CEO / A321 NEO

FUEL IMBALANCE AT TAKEOFF

A

TANK FUEL QUANTITY
(HEAVIER TANK)

FULL

MAXIMUM ASYMMETRY

882 POUNDS (400 KILOGRAMS)

78
Q

APPLICABLE TO A321 CEO / A321 NEO

FUEL IMBALANCE IN FLIGHT AND AT LANDING

NOT BOLD

A

TANK FUEL QUANTITY
(HEAVIER TANK)

FULL

MAXIMUM ASYMMETRY

2,910 POUNDS (1,320 KILOGRAMS)

79
Q

MINIMUM FUEL QUANTITY FOR TAKEOFF

NOT BOLD

A

3,307 POUNDS (1,500 KILGRAMS)

80
Q

MAXIMUM BRAKE TEMPERATURE FOR TAKEOFF
(BRAKE FANS OFF)

A

300 DEGREES CELSIUS

Spirit Airlines - Study Guide (02/23/2024) (3 decks)

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