Spirit MQF 25r6 > 0-LIMITATIONS (GENERAL) (12) > Flashcards

0-LIMITATIONS (GENERAL) (12) Flashcards

250320 (109 cards)

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1
Q

MANEUVERING LOAD ACCELERATION LIMITS - CLEAN

A

-1 g to +2.5 g

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2
Q

MANEUVERING LOAD ACCELERATION LIMITS - OTHER

A

0 g to +2 g

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3
Q

KIND OF OPERATIONS

A

‐ VFR
- IFR
‐ Extended overwater flight

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4
Q

MINIMUM FLIGHT CREW

A

2 pilots

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5
Q

WINGSPANS (Original Fence-tip)

A

111 feet, 10 inches

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6
Q

320 - TAILSTRIKE PITCH ATTITUDE - L/G EXTENDED

A

13.5°

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7
Q

320N - TAILSTRIKE PITCH ATTITUDE - L/G EXTENDED

A

13.7°

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8
Q

321 - TAILSTRIKE PITCH ATTITUDE - L/G EXTENDED

A

11.2°

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9
Q

ENVIRONMENTAL ENVELOPE - NEO (PW) T/O & LANDING

A

ISA +40C
MAX 9200ft
MIN -2000ft

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10
Q

ENVIRONMENTAL ENVELOPE - CEO (IAE) T/O & LANDING

A

ISA +40C
MAX 9200ft
MIN -1000ft

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11
Q

MEAN RUNWAY SLOPE

A

±2 %

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12
Q

MAX RUNWAY ALTITUDE

A

9200 ft

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13
Q

Nominal runway width

A

45 m (148 ft)

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14
Q

Minimal runway width

A

30 m (99 ft)

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15
Q

Maximum wind for passenger door operation

A

65 kt

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16
Q

Maximum wind for FWD and AFT cargo door operation

A

40 kt,
(or 50 kt, if the aircraft nose is into the wind, or if the cargo doors are on the downwind side)

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17
Q

The FWD and AFT cargo doors must be closed before the wind speed exceeds

A

65 kt

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18
Q

Max Recommended Crosswind for RCR - Good / 5

A

38 kts

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19
Q

Max Recommended Crosswind for RCR - Good-to-Medium / 4

A

29 kts

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20
Q

Max Recommended Crosswind for RCR - Medium / 3

A

25 kts

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21
Q

Max Recommended Crosswind for RCR - Medium-to-Poor / 2

A

20 kts

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22
Q

Max Recommended Crosswind for RCR - Poor / 1

A

15 kts

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23
Q

Takeoff is not recommended on the following runway conditions:

A

‐ Water on top of Compacted Snow

‐ Dry Snow or Wet Snow over Ice

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24
Q

Takeoff is not permitted on the following runway conditions:

A

Wet ice

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25
COCKPIT WINDOW OPEN MAXIMUM SPEED
200 kts
26
MAXIMUM FLAPS/SLATS SPEEDS = 320
Lever | Display | Max Speed |Phase 0 | 0 | VMO / MMO | CRUISE 1 | 1 | 230 kt | HOLDING | 1 + F | 215 kt | TAKEOFF 2 | 2 | 200 kt | TO/APP 3 | 3 | 185 kt | TO/APP/LAND F | FULL | 177 kt |LANDING
27
MAXIMUM FLAPS/SLATS SPEEDS = 321 C
Lever | Display | Max Speed |Phase 0 | 0 | VMO / MMO | CRUISE 1 | 1 | 235 kt | HOLDING | 1 + F | 225 kt | TAKEOFF 2 | 2 | 215 kt | TO/APP 3 | 3 | 195 kt | TO/APP/LAND F | FULL | 190 kt |LANDING
28
MAXIMUM FLAPS/SLATS SPEEDS = 321 N
Lever | Display | Max Speed |Phase 0 | 0 | VMO / MMO | CRUISE 1 | 1 | 243 kt | HOLDING | 1 + F | 225 kt | TAKEOFF 2 | 2 | 215 kt | TO/APP 3 | 3 | 195 kt | TO/APP/LAND F | FULL | 186 kt |LANDING
29
MAXIMUM OPERATING SPEED
VMO = 350 kt MMO = M 0.82
30
Maximum speed with the landing gear extended (VLE)
280 kt /M 0.67
31
Maximum speed at which the landing gear may be extended (VLO extension)
250 kt /M 0.60
32
Maximum speed at which the landing gear may be retracted (VLO retraction)
220 kt /M 0.54
33
Maximum TIRE ground speed
195 kt
34
MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 320C
109 kt
35
MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 320N
116 kt
36
MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 321C
114 kt
37
MINIMUM CONTROL SPEED FOR LANDING (VMCL) - 321N
115 kt
38
MINIMUM CONTROL SPEED ADJUSTMENT FOR NARROW RUNWAYS
WIDTH | +VMCG 98 ft | +2.5 kt 114 ft | +1.5 kt 131 ft | +0 kt
39
When is an immediate landing at weight above maximum landing weight is permitted, provided the pilot follows the overweight landing procedure.
In exceptional cases of in-flight turn back or diversion.
40
MAX LANDING WEIGHT - 319
137,788 lbs
41
MAX LANDING WEIGHT - 320C
145,505 lbs
42
MAX LANDING WEIGHT - 320N
148,591 lbs
43
MAX LANDING WEIGHT - 321C
171,519 lbs
44
MAX LANDING WEIGHT - 321N
174,606 lbs
45
With passengers on board, it is not recommended to exceed _____ without air conditioning supply. The lack of fresh air supply will significantly reduce the cabin’s air quality.
_20 min_
46
AVIONICS VENTILATION During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows:
While OAT is less than 49 °C, there is no limit. Otherwise, check the FCOM for appropriate time limits. FCOM > LIMITATION - AVIONICS VENTILATION
47
CABIN Maximum positive differential pressure
9.0 PSI
48
CABIN Maximum negative differential pressure
-1.0 PSI
49
CABIN Safety relief valve setting
8.6 PSI
50
The ram air inlet must only be opened when the cabin differential pressure is less than
+1 PSI (70 hPa).
51
FMGS lateral and vertical navigation is certified for:
‐ After takeoff, en route, and terminal area operations ‐ Navigation within RNAV/RNP airspace - Instrument approach procedures (except ILS & FLS finals) ‐ Missed approach procedures.
52
If GPS PRIMARY LOST is displayed on the ND and MCDU, the navigation accuracy remains sufficient for RNP operations provided that. . .
. . . the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.
53
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.
54
Min Decision Height ILS CAT 2
100 ft AGL, with at least one autopilot engaged and CAT 2, CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA. For manual landing, AP should be disconnected no later than 80 ft AGL.
55
Min Decision Height SA CAT 2
100 ft AGL, with at least one autopilot engaged and CAT 2, CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.
56
Min Decision Height ILS CAT 3 SINGLE (PASSIVE)
50 ft AGL, with at least one autopilot & A/THR engaged and CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.
57
Min Decision Height ILS CAT 3 DUAL (OPERATIONAL)
0 ft AGL (NODA). Alert height of "100 ft" AGL, with at least one autopilot & A/THR engaged and CAT 3 DUAL must be displayed on the FMA.
58
Minimum Runway Visual Range for CAT III without DH:
300 RVR
59
320C - CAT II and CAT III fail passive auto-land are approved in CONFIG _____
CONFIG FULL only
60
319 / 320N / 321 / 321N CAT II and CAT III fail passive auto-land are approved in CONFIG ____
CONFIG 3 and FULL
61
320C AUTOLAND Restrictions - Max Glideslope & Airport Elevation
Glideslope = -3.15 degree Elevation = At/below 6500 ft
62
321C AUTOLAND Restrictions - Max Glideslope & Airport Elevation
Glideslope = -3.15 degree Elevation = At/below 5750 ft
63
320N / 321N AUTOLAND Restrictions - Max Glideslope & Airport Elevation
Glideslope = -3.25 degree Elevation = At/below 9200 ft (901-905 = < 5750ft)
64
During refuel/defuel procedures, APU starts or shutdown are. . .
. . . permitted unless: ‐ If the APU failed to start or following an automatic APU shutdown, do not start the APU ‐ If a fuel spill occurs, perform a normal APU shutdown.
65
APU BLEED Max altitude to assist engine start
20,000 ft
66
APU BLEED Max altitude for single pack operation
20,000 ft for a few (22,500 ft for most. Check LIM-APU-OPEV)
67
APU BLEED Max altitude for dual pack operation
15,000 ft
68
APU BLEED Use of APU bleed air for wing anti-ice. . .
. . . is not permitted.
69
The use of Wi-Fi devices within the flight compartment (cockpit) is. . .
is prohibited when engines are operating for the purpose of flight unless the following condition is met: * Additional FAA certification of the wireless devices to be used on the flight deck is obtained.
70
ENGINE EGT LIMITS - 319 / 320 Starting, Takeoff & Go-Around
635 °C
71
ENGINE EGT LIMITS - 321 Starting
635 °C
72
ENGINE EGT LIMITS - 321 Takeoff & Go-Around
650 °C
73
ENGINE EGT LIMITS - 319 / 320 / 321 Maximum Continuous Thrust (MCT)
610 °C
74
ENGINE EGT LIMITS - 320N / 321N Starting, Takeoff & Go-Around
1083 °C
75
ENGINE EGT LIMITS - 320N / 321N Maximum Continuous Thrust (MCT)
1043 °C
76
ENGINE OIL TEMP - 319 / 320 / 321 Max continuous
155 °C 165 °C transient (15 min)
77
ENGINE OIL TEMP - 319 / 320 / 321 Min before takeoff
50 °C
78
ENGINE OIL QUANTITY - 319 / 320 / 321 Min Oil Quantity
11 qt + 0.3 qt/hr
79
ENGINE OIL PRESSURE - 319 / 320 / 321 Min Oil Pressure
60 PSI
80
ENGINE OIL TEMP - 320N / 321N Max Continuous
151 °C
81
ENGINE OIL TEMP - 320N / 321N Min Starting
-40 °C
82
ENGINE OIL TEMP- 320N / 321N Min before takeoff
52 °C
83
ENGINE OIL QUANTITY 320N / 321N Min Oil Quantity
14 qt when OAT => -30 °C 16.5 qt when OAT < -30 °C
84
ENGINE OIL PRESSURE - 320N / 321N Min Oil Pressure
65 PSI
85
ENGINE OIL PRESSURE - 320N / 321N Max Oil Pressure
270 PSI
86
ENGINE STARTER CYCLE - 320N / 321N
‐ A standard automatic start that includes up to two start attempts, is considered one cycle ‐ For ground starts (automatic or manual), a 35 s pause is required between successive cycles ‐ A 15 min cooling period is required, subsequent to three failed cycles, or 15 min of continuous or cumulated crank ‐ The starter must not be run when N2 is above 20 %.
87
ENGINE STARTER CYCLE - 319 / 320 / 321 IAE2500
‐ A standard automatic start that includes only one start attempt, is considered one cycle ‐ For ground starts (automatic or manual), a 15 s pause is required between successive cycles ‐ A 30 min cooling period is required, subsequent to three failed cycles, or 4 min of continuous crank, or 5 min 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.
88
USE OF REVERSE THRUST
Selection of the reverse thrust is prohibited in flight. Backing the aircraft with reverse thrust is not permitted.
89
The use of GA SOFT mode is ___________ with one engine inoperative.
_ PROHIBITED _
90
FUEL IMBALANCE AT TAKEOFF - 319 / 320 *Inner* Tanks (outer balanced)
Heavier | Max Tank | Asymmetry ------------+---------------- 6613 | 2314 3196 | 3196
91
FUEL IMBALANCE AT TAKEOFF - 319 / 320 *Outer* Tanks (inner balanced) MAX
815 lbs
92
FUEL IMBALANCE INFLIGHT & LANDING - 319 / 320 Inner Tanks (outer balanced)
Heavier | Max Tank | Asymmetry ------------+---------------- FULL | 3306 9479 | 3527 4960 | 4960
93
FUEL IMBALANCE AT TAKEOFF - 321
Heavier | Max Tank | Asymmetry ------------+---------------- 6614 | 882 1543 | 1543
94
FUEL IMBALANCE INFLIGHT & LANDING - 321
Heavier | Max Tank | Asymmetry ------------+---------------- FULL | 2910 8818 | 3196 5180 | 5180
95
MINIMUM FUEL QUANTITY FOR TAKEOFF
3307 lbs - 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.
96
DEFINITION OF ICING CONDITIONS
‐ Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is at or below 10 °C and visible moisture in any form is present (such as clouds, fog with visibility of 1 sm or less, rain, snow, sleet or ice crystals). ‐ Icing conditions also exist when the OAT on the ground and for takeoff is at or below 10 °C and operating on ramps, taxiways or runways where surface snow, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes.
97
DEFINITION OF SEVERE ICE ACCRETION
Ice accretion is considered severe when the ice accumulation on the airframe reaches approximately 5 mm (0.2 in) thick or more.
98
DEFINITION OF THIN HOARFROST
Thin hoarfrost is typically a white crystalline deposit which usually develops uniformly on exposed surfaces on cold and cloudless nights. It is so thin that surface features (lines or markings) can be distinguished beneath it.
99
The flight crew should _____ use the rain repellent in the case of moderate to heavy rain.
The flight crew should ONLY use the rain repellent in the case of moderate to heavy rain.
100
The braking system _____ designed to hold the aircraft in a stationary position when a high thrust level is applied on at least one engine.
_IS NOT_ During ground procedures that require a thrust increase with braking, the flight crew must ensure that the aircraft remains stationary, and must be ready to immediately retard the thrust levers to IDLE.
101
MAXIMUM NWS ANGLE
+/- 85° L/R
102
MAX TAXI SPEED WITH DEFLATED/DAMAGED TIRES = 1 TIRE PER GEAR:
7 KTS
103
MAX TAXI SPEED WITH DEFLATED/DAMAGED TIRES = 2 TIRES ON SAME GEAR:
3 KTS
104
MAX NWS ANGEL WITH DEFLATED/DAMAGED TIRES:
30°
105
FLS function is certified for ...
RNAV, RNAV (GNSS), GPS, VOR to LNAV/VNAV or LNAV only minima
106
SLS function is certified for ...
RNAV (GNSS) to LPV or LP minima
107
MAX HEADWIND FOR ILS CAT 2 or CAT 3
30 kt
108
MAX TAILWIND FOR ILS CAT 2 or CAT 3
10 kt
109
MAX CROSSWIND FOR ILS CAT 2 or CAT 3
15 kt
Spirit MQF 25r6
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