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Spirit Airlines - Study Guide (02/19/2025) > 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 SPEED 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
MAXIMUM SPEED WITH THE LANDING GEAR EXTENDED (VLE) *NOT BOLD*
280 KNOTS / MACH 0.67
26
MAXIMUM LANDING GEAR EXTENSION SPEED (VLO EXTENSION) *NOT BOLD*
250 KNOTS / MACH 0.60
27
MAXIMUM LANDING GEAR RETRACTION SPEED (VLO RETRACTION) *NOT BOLD*
220 KNOTS / MACH 0.54
28
MAXIMUM TIRE SPEED *NOT BOLD*
195 KNOTS GROUNDSPEED
29
APPLICABLE TO A320 CEO WHEN THE TAKEOFF WEIGHT IS HIGHER THAN (_____): CAUTION: DO NOT EXCEED A TAXI SPEED OF (_____) DURING A TURN.
167,550 POUNDS (76,000 KILOGRAMS) 20 KNOTS
30
MAXIMUM WINDSHIELD WIPER OPERATING SPEED
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.
31
MAXIMUM ALTITUDE LANDING GEAR MAY BE EXTENDED *NOT BOLD*
25,000 FEET
32
MAXIMUM LANDING WEIGHT A319 *NOT BOLD*
137,788 POUNDS
33
MAXIMUM LANDING WEIGHT A320 CEO *NOT BOLD*
145,505 POUNDS
34
MAXIMUM LANDING WEIGHT A320 NEO *NOT BOLD*
148,591 POUNDS
35
MAXIMUM LANDING WEIGHT A321 CEO *NOT BOLD*
171,519 POUNDS
36
MAXIMUM LANDING WEIGHT A321 NEO *NOT BOLD*
174,606 POUNDS
37
APU BLEED USE WITH AIR START UNIT
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
CABIN PRESSURE MAXIMUM POSITIVE DIFFERENTIAL PRESSURE *NOT BOLD*
9.0 PSI
39
CABIN PRESSURE MAXIMUM NEGATIVE DIFFERENTIAL PRESSURE *NOT BOLD*
-1.0 PSI
40
CABIN PRESSURE SAFETY RELIEF VALVE SETTING *NOT BOLD*
8.6 PSI
41
NOTE: THE RAM AIR INLET MUST ONLY BE OPENED WHEN THE CABIN DIFFERENTIAL PRESSURE IS LESS THAN (_____) *NOT BOLD*
+1 PSI (70 HPA).
42
PACKS USE WITH LP AIR CONDITIONING UNIT
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
MINIMUM USE HEIGHT FOR AUTOPILOT AT TAKEOFF
100 FEET AGL AND AT LEAST 5 SECONDS AFTER LIFTOFF
44
MINIMUM USE HEIGHT FOR AUTOPILOT IN APPROACH WITH F-G/S MODE
250 FEET AGL
45
MINIMUM USE HEIGHT FOR AUTOPILOT IN APPROACH WITH FINAL APP, V/S OR FPA MODE
250 FEET AGL
46
MINIMUM USE HEIGHT FOR AUTOPILOT IN CIRCLING APPROACH
600 FEET AGL
47
MINIMUM USE HEIGHT FOR AUTOPILOT ILS/MLS APPROACH WHEN CAT1 IS DISPLAYED ON THE FMA
160 FEET AGL
48
MINIMUM USE HEIGHT FOR AUTOPILOT ILS/MLS APPROACH WHEN CAT2 OR CAT3 SINGLE OR CAT3 DUAL IS DISPLAYED ON THE FMA
0 FEET AGL IF AUTOLAND
49
MINIMUM USE HEIGHT FOR AUTOPILOT LPV APPROACH (WITH SLS) WHEN APPR1 IS DISPLAYED ON THE FMA
160 FEET AGL
50
MINIMUM USE HEIGHT FOR AUTOPILOT AFTER A MANUAL GO-AROUND
100 FEET AGL
51
MINIMUM USE HEIGHT FOR AUTOPILOT IN ALL OTHER PHASES
500 FEET AGL (A319 / A320 CEO / A320 NEO) 900 FEET AGL (A321 CEO / A321 NEO)
52
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:
HIGHEST OF: MDA/MDH OR 500 FEET AGL (A319 / A320 CEO / A320 NEO) MDA/MDH OR 900 FEET AGL (A321 CEO / A321 NEO)
53
USE OF NAV MODE NAV MODE MAY BE USED IN THE TERMINAL AREA PROVIDED THAT: *NOT BOLD*
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
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*
FINAL APP NAV V/S NAV/FPA ONLY FD USE IS PERMITTED
55
APU START AFTER (_____) CONSECUTIVE APU START ATTEMPTS, THE FLIGHT CREW MUST WAIT (_____) MINUTES BEFORE A NEW START ATTEMPT.
3 CONSECUTIVE START ATTEMPTS 60 MINUTES
56
APPLICABLE TO A319 / A320 CEO THRUST SETTING / EGT LIMITS
TAKEOFF(1) AND GO-AROUND TIME LIMIT: 5 MINUTES (ALL ENGINES OPERATIVE) TIME LIMIT: 10 MINUTES (ONE ENGINE INOPERATIVE) EGT LIMIT: 635 DEGREES CELSIUS *NOT BOLD* MAXIMUM CONTINUOUS THRUST (MCT) TIME LIMIT: NOT LIMITED EGT LIMIT: 610 DEGREES CELSIUS *NOT BOLD* STARTING *NOT BOLD* TIME LIMIT: NOT LIMITED EGT LIMIT: 635 DEGREES CELSIUS (1) INCLUDES TOGA, FLEX AND DERATE THRUST MODES.
57
APPLICABLE TO A321 CEO THRUST SETTING / EGT LIMITS
TAKEOFF(1) AND GO-AROUND TIME LIMIT: 5 MINUTES (ALL ENGINES OPERATIVE) TIME LIMIT: 10 MINUTES (ONE ENGINE INOPERATIVE) EGT LIMIT: 650 DEGREES CELSIUS *NOT BOLD* MAXIMUM CONTINUOUS THRUST (MCT) TIME LIMIT: NOT LIMITED EGT LIMIT: 610 DEGREES CELSIUS *NOT BOLD* STARTING *NOT BOLD* TIME LIMIT: NOT LIMITED EGT LIMIT: 635 DEGREES CELSIUS (1) INCLUDES TOGA, FLEX AND DERATE THRUST MODES.
58
APPLICABLE TO A320 NEO / A321 NEO THRUST SETTING / EGT LIMITS
TAKEOFF(1) AND GO-AROUND TIME LIMIT: 5 MINUTES (ALL ENGINES OPERATIVE) TIME LIMIT: 10 MINUTES (ONE ENGINE INOPERATIVE) EGT LIMIT: 1,083 DEGREES CELSIUS *NOT BOLD* MAXIMUM CONTINUOUS THRUST (MCT) TIME LIMIT: NOT LIMITED EGT LIMIT: 1,043 DEGREES CELSIUS *NOT BOLD* STARTING *NOT BOLD* TIME LIMIT: NOT LIMITED EGT LIMIT: 1,083 DEGREES CELSIUS (1) INCLUDES TOGA, FLEX AND DERATE THRUST MODES.
59
APPLICABLE TO A319 / A320 CEO / A321 CEO MINIMUM OIL STARTING TEMPERATURE
-40 DEGREES CELSIUS
60
APPLICABLE TO A319 / A320 CEO / A321 CEO MINIMUM OIL TEMPERATURE BEFORE IDLE IS EXCEEDED
-10 DEGREES CELSIUS
61
APPLICABLE TO A319 / A320 CE0 / A321 CEO MINIMUM OIL TEMPERATURE BEFORE TAKEOFF *NOT BOLD*
50 DEGREES CELSIUS
62
APPLICABLE TO A319 / A320 CEO / A321 CEO MINIMUM OIL QUANTITY *NOT BOLD*
11 QUARTS + ESTIMATED CONSUMPTION AVERAGE ESTIMATED CONSUMPTION = 0.3 QUARTS/HOUR
63
APPLICABLE TO A319 / A320 CEO / A321 CEO MINIMUM OIL PRESSURE *NOT BOLD*
60 PSI
64
APPLICABLE TO A320 NEO / A321 NEO MINIMUM OIL STARTING TEMPERATURE *NOT BOLD*
-40 DEGREES CELSIUS
65
APPLICABLE TO A320 NEO / A321 NEO MINIMUM OIL TEMPERATURE BEFORE TAKEOFF *NOT BOLD*
52 DEGREES CELSIUS
66
APPLICABLE TO A320 NEO / A321 NEO MINIMUM OIL QUANTITY *NOT BOLD*
OAT AT OR ABOVE -30 DEGREES CELSIUS = 14 QUARTS OAT BELOW -30 DEGREES CELSIUS = 16.5 QUARTS
67
APPLICABLE TO A320 NEO / A321 NEO MINIMUM OIL PRESSURE *NOT BOLD*
65 PSI
68
APPLICABLE TO A319 / A320 CEO / A321 CEO STARTER *NOT BOLD*
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 4 MINUTES OF CONTINUOUS CRANK, OR 5 MINUTES OF CUMULATED CRANK FOR MANUAL START, DO NOT EXCEED THE TWO-MINUTE MAXIMUM CYCLE TIME THE STARTER MUST NOT BE RUN WHEN N2 IS ABOVE 10 % ON-GROUND AND 18 % IN-FLIGHT.
69
APPLICABLE TO A320 NEO / A321 NEO STARTER *NOT BOLD*
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
REVERSE THRUST
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
APPLICABLE TO A319 / A320 CEO / A320 NEO / A321 CEO / A321 NEO REDUCED THRUST TAKEOFF
FLEX TAKEOFF IS NOT PERMITTED ON CONTAMINATED RUNWAYS.
72
CROSSWIND OPERATION ON GROUND ENGINE START THE ENGINE IS ABLE TO START IN CROSSWIND UP TO (_____) KNOTS.
35 KNOTS
73
MAXIMUM OPERATING ALTITUDE WITH SLATS AND/OR FLAPS EXTENDED
20,000 FEET
74
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 (_____).
-34 DEGREES CELSIUS / -36 DEGREES CELSIUS
75
APPLICABLE TO A319 / A320 CEO / A320 NEO FUEL IMBALANCE AT TAKEOFF INNER TANKS (OUTER TANKS BALANCED)
TANK FUEL QUANTITY (HEAVIER TANK) FULL MAXIMUM ASYMMETRY 1,102 POUNDS (500 KILOGRAMS)
76
APPLICABLE TO A319 / A320 CEO / A320 NEO FUEL IMBALANCE IN FLIGHT AND AT LANDING INNER TANKS (OUTER TANKS BALANCED) *NOT BOLD*
TANK FUEL QUANTITY (HEAVIER TANK) FULL MAXIMUM ASYMMETRY 3,306 POUNDS (1,500 KILOGRAMS)
77
APPLICABLE TO A321 CEO / A321 NEO FUEL IMBALANCE AT TAKEOFF
TANK FUEL QUANTITY (HEAVIER TANK) FULL MAXIMUM ASYMMETRY 882 POUNDS (400 KILOGRAMS)
78
APPLICABLE TO A321 CEO / A321 NEO FUEL IMBALANCE IN FLIGHT AND AT LANDING *NOT BOLD*
TANK FUEL QUANTITY (HEAVIER TANK) FULL MAXIMUM ASYMMETRY 2,910 POUNDS (1,320 KILOGRAMS)
79
MINIMUM FUEL QUANTITY FOR TAKEOFF *NOT BOLD*
3,307 POUNDS (1,500 KILGRAMS) THE ECAM ALERTS THAT ARE RELATED TO FUEL LOW LEVEL IN THE WING TANKS (FUEL WING TK LO LVL, ETC.) MUST NOT APPEAR FOR TAKEOFF.
80
MAXIMUM BRAKE TEMPERATURE FOR TAKEOFF (BRAKE FANS OFF)
300 DEGREES CELSIUS
81
TOGA THRUST THE FLIGHT CREW MUST USE TOGA THRUST FOR TAKEOFF IF AT LEAST ONE OF THE FOLLOWING CONDITIONS APPLIES:
-ON **CONTAMINATED RUNWAYS** (LIMITATIONS) -FOR **KNOWN WINDSHEAR CONDITIONS** (AIRBUS TAKEOFF PERFORMANCE GUIDANCE AND COMPANY POLICY) -WHEN A **SPECIAL DEPARTURE PROCEDURE SPECIFIES FULL THRUST FOR TAKEOFF** (AERODATA REQUIREMENT) -WHEN A **DEFERRED MAINTENANCE ITEM PER THE MEL** REQUIRES FULL THRUST FOR TAKEOFF. -WHEN THE **FLEX TEMP IS WITHIN 10 DEGREES CELSIUS OF ACTUAL OAT**.

Spirit Airlines - Study Guide (02/19/2025) (3 decks)

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