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Airbus limitations > Airbus 319/320 limitations > Flashcards

Airbus 319/320 limitations Flashcards

0
Q

Max passenger seats
A321
A320
A319

A

– Maximum number of passenger seats: 230 (A321)
– Maximum number of passenger seats: 190 (A320)
– Maximum number of passenger seats: 150 (A319)

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1
Q

Flight maneuvering load limits

A

Clean configuration ……-1 g to +2.5 g

Slats and/or flaps extended ….. 0 g to +2 g

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2
Q

Runway slope (mean)
Min runway length
Min runway width
Max runway alt

A

+- 2%
Minimum runway length 5000 ft
Minimum runway width 100 ft
Runway altitude 9200 ft

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3
Q

Normal runway width

Narrow runway width

A

Normal is considered 150ft or wider (45 meters which is actually 148 feet)
Narrow runway is less than 150ft wide (45 meters /148 feet)

Normal runways needed for

  • rudder jam
  • rudder pedal jam
  • yaw damper fault
  • and all failures leading to the loss of nose wheel steering
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4
Q

Max crosswinds takeoff and landing on contaminated runways

A

Contaminated runway max cross wind is 10kts (gusts included) takeoff and landing

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5
Q

Wind for passenger door operation

A

Max wind pax door operation is 65kts
Cargo door operation max wind is 40kts if nose oriented into wind
50kts if cargo door is leeward side of wind

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6
Q

Max speed Vmo /Mmo

A

Vmo 350kts / Mmo .82 Mach

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7
Q

SEVERE TURBULENCE AIR PENETRATION
FL200 and below
Above FL200 through FL310
Above FL310

A

FL200 and below …. 250kts
Above FL200 through FL310….275kts
Above FL310 ….. 0.76Mach

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8
Q

Gear down speeds
VLE
VLO EXTENSION
VLO RETRACTION

MAX ALTITUDE FOR GEAR EXTENSION

A

VLE … 280kts/ 0.67 Mach
VLO extension 250kts
VLO RETRACTION … 220kts
Max Altitude gear may be extended … 25000ft

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9
Q

MAX FLAPS/SLATS SPEEDS
A319-320
A321

A

A319-A320 A321
Slat 1 =230 KIAS Slats1=235 KIAS
1+f)= 215 KIAS (1+F)=225
Config 2= 200 KIAS Config 2 = 215
Config 3=184 KIAS Config 3= 195
Config Full =177 KIAS Config Full=190

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10
Q

MAX TIRE SPEED (ground speed)

A

195 KTS

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11
Q

WINDSHIELD WIPER SPEED

A

230 KTS

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12
Q

COCKPIT WINDOW SPEED

A

200 KTS

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13
Q

MAX TAXI SPEED (A320)

A

When taxi weight is higher than 167550 lbs DO NOT EXCEED TAXI SPEED OF 20 KTS during a turn

30 knots Max taxi speed

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14
Q

MAXIMUM OPERATING ALTITUDE WITH FLAPS and/or SLATS EXTENDED

A

20000 feet

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15
Q

CABIN PRESSURES
MAX POSITIVE DIFFERENTIAL PRESSURE
MAX NEGATIVE DIFFERENTIAL PRESSURE

A

Max pos diff 8.6 psi ( safety relief valve setting) however
9.0 is max pos diff
Max negative diff -1.0 psi

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16
Q

RAM INLET DOOR

A

If differential pressure is greater than 1.0 psi, the check valve located downstream will not open even if the ram air door has been selected open.

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17
Q

AIR CONDITIONING WITH LP GROUND UNIT

A

Do not use conditioned air simultaneously from packs and LP ground unit (to avoid chattering of the non return valves)

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18
Q

AIR CONDITIONING WITH HP GROUND UNIT

A

An external hp source may be used for air conditioning provided air supply is confirmed to be free from oil contamination. Do not use HP ground unit when APU supplies bleed air to avoid bleed system damage.

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19
Q

AVIONICS VENTILATION
THE AIRPLANE ELECTRICAL SYSTEM SHOULD NOT BE POWERED FOR MORE THAN ——– WITHOUT A COOLING SYSTEM WHEN THE OUTSIDE TEMPERATURE EXCEEDS———.

A

2 hours

49*C

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20
Q

APU may be started and operated even if —————advisory is displayed. Maintenance action is required within the next———— hours of operation.
Logbook entry is NOT required after receiving this advisory message. Contact MCC

A

the LOW OIL LEVEL ECAM advisory

Maintenance required within the next 10 hours of operation

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21
Q

After ——– motor start duty cycles of the APU , each separated by ———-cool down. Wait ——minutes before attempting three more cycles.

A

3 motor duty cycles with one minute cool down in between each . Wait 60 minutes before attempting three more cycles.

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22
Q

Maximum N on APU

A

107%

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23
Q

MAXIMUM APU EGT

A

675*C

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24
Q

Maximum APU IGT for start ( below 35,000 feet)

A

1090*C

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25
Q

Maximum APU EGT for start ( above 35,000 feet)

A

1120* C

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26
Q

Maximum altitude for APU electrical and start

A

39,000 feet

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27
Q

Maximum altitude for APU battery start

A

25,000 feet

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28
Q

Maximum altitude for APU pneumatics ( 1 pack w/ electrical)

A

22,500 feet

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29
Q

Maximum altitude for APU assisted engine start

A

20,000 feet

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30
Q

Maximum altitude for APU Pneumatics (2 packs w/ electrical)

A

15,000 feet

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31
Q

APU air bleed extraction for wing anti-ice

A

NOT PERMITTED

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32
Q

Autopilot engagement after take-off/go around (if SRS is indicated)

A

100 feet AGL

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33
Q

Autopilot engagement Enroute

A

500 feet AGL A319 & A320

900 feet AGL in A321

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34
Q

Autopilot engagement Non-Precision Approaches

A

May be engaged until reaching DDA/DA

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35
Q

Autopilot engagement Non-autoland ILS Approach with CAT-I displayed on FMA

A

160 feet AGL

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36
Q

Autopilot engagement Non-autoland ILS approach with CAT 2/3 displayed on FMA

A

80 feet AGL

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37
Q

AUTOPILOT ENGAGEMENT WITH AUTO-LAND ILS Approach (one or two autopilots)

A

Rollout /taxi speed

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38
Q

When visibility is less than ——– RVR or —–SM , the approach must be flown with

A

If the visibility is less than 4000 RVR or 3/4sm autopilot(s) must be engaged if operable.

39
Q

The use of the —- or the —– in ——- —- or —- mode is not permitted inside the FAF or below 1000 feet AGL on a visual approach

A

Use of AP or FLIGHT DIRECTOR prohibited in OPEN DES or DES mode inside FAF or below 1000 feet AGL on a visual approach.

40
Q

The use of ———- is approved with or without AP/FD in selected or managed mode

A

Auto thrust

41
Q

Derived decision altitude for a MDA

A

(Monkey do add)

Must add 50 feet to the published MDA

42
Q

NAV, NAV & APP NAV and FINAL APP mode may be used for —, — , —-, or —– approaches but not for —–, —–, or —- approaches.

A

May be used on VOR, VOR/DME or RNAV (including GPS or RNAV(GNSS)) approaches

May not be used for ILS , LOC , or LDA Approaches

43
Q

GPS RNP NAV accuracy demonstrated

A

Autopilot on
En route is 1nm
Terminal area is 0.5nm
Approach is 0.3 nm

Autopilot off and FD on in NAV
Enroute 1nm
Terminal area 0.51nm
Approach 0.3 nm

44
Q

Autoland limitations

A

Must be preformed by the captain
Autoland approved for CONF3 and CONF FULL.
CONF FULL is recommended for all autolands to maximize forward slant range visibility

45
Q

Single engine non-precision approaches the autopilot is not permitted in the following modes

A

FINAL APP, NAV V/S, NAV/FPA ( not applicable on a/c 205-216 , 220)
Only the FD is authorized

46
Q

AUTOLANDS may be conducted when what conditions are satisfied

A 
CAT II/III runway
CAT II/III  aircraft
Crews CAT II/III trained
Appropriate ground facilities are operational
Wind within limits
Braking action is fair or better
47
Q

AUTOLAND REQUIRED WHEN

A

THE REQUIREMENTS FOR AUTOLAND ARE SATISFIED AND THE ATIS reported RVR visibility is at or below 2400 RVR or 1/2 statute mile the approach briefed and flown as a CAT II OR CAT III autoland except as noted

Note if any of the CAT II/III REQUIREMENTS ARE NOT MET, AND CAT I or better weather conditions prevail upon arrival at the airport, the crew may brief and fly the approach to current CAT I minimums as stated in FOM I, chapter 20 with a manual landing

48
Q

AUTOLAND PROHIBITED if braking action is

A

Less than Fair

49
Q

AUTOLANDS not authorized if runway is less than

A

100 feet wide

Not authorized in FAIRBANKS ALASKA on aircraft 203, 803, and ,902-943

50
Q

AUTOBRAKES are required (if available) for all

A

CAT III APPROACHES

  • runways less than 8000 ft - medium setting
  • runways 8000 ft or longer -low or medium setting
51
Q

CAT II APPROACHES MUST

A

Minimum decision height 100ft AGL

At least one auto pilot must be engaged in APPR mode and CAT2, CAT 3 SINGLE, or CAT 3 DUAL displayed on the FMA

52
Q 
CATIIIA 
FAIL PASSIVE ( CAT 3 SINGLE)  decision height 50ft AGL .
A

FAIL PASSIVE :At least one autopilot engaged in APPR mode and CAT3 SINGLE displayed on the FMA. A/THR must be used in selected or managed speed.

Fail operational (CAT 3 DUAL) Alert height 100ft AGL . Two autopilots engaged in APPR mode and CAT 3 DUAL displayed on FMA. A/THR must be used in selected or managed speed.

53
Q

CAT IIIB

A

Alert height 100ft AGL
Two autopilots engaged in APPR mode and CAT3 DUAL displayed on FMA.
A/THR must be used in selected or managed speed

54
Q

AUTOLAND WIND RESTRICTIONS

A

30kts headwind (20 in NEO)
15kts crosswind
10kts tailwind (5 in NEO)
Wind correction : Vapp=VLs +wind correction
Minimum/maximum wind correction : 5kts/15kts

55
Q

AUTOLAND PERFORMANCE LIMITS (below 500ft)

A 
Glide slope deviation < one dot
Localizer deviation <1/4 dot
Airspeed +-5 knots of target
Max rate of descent 1000fpm
Airspeed not below VLs
Bank not to exceed 7* degrees
-2.5* <=pitch<=10*
56
Q

SINGLE ENGINE AUTOLAND

A

Are approved by the AFM . Although Frontier Airlines limitations prohibit the initiation of single engine AUTOLAND approaches , the flight crew may use emergency authority if it is determined to be the safest course of action.

57
Q

Single engine autolands on A320
Configuration
Single engine autolands on A319

A

Are only approved in the CONFIG FULL on A 320
And CONFIG 3 or CONFIG full on the A319
However remember frontier prohibits single engine autolands unless exercising emergency authority and considered the safest course of action

58
Q

Cargo loads

A

May not be higher than the mark in cargo bay approximately 2 inches below top of cargo pits to ensure proper functionality of the smoke detectors

59
Q

MAX Continuous load per generator

A

100% (90kVa)

60
Q

MAX Continuous load per transforming reducer (TR)

A

200Amps

61
Q

Electrical outlets

A

Must not be used during takeoff or landing and the rear 115V 400hz outlet on the rear circuit breaker panel should never be used for charging PEDS( including EFBs) as it could pose. Fire risk.

62
Q

ENGINE THRUST SETTINGS EGT LIMITS
Takeoff and GO AROUND
MCT
STARTING

A

Takeoff and go around 5 minutes at 950*C or 10 minutes (only in case of engine failure)

MCT unlimited time at 915*C

Starting 725*C

63
Q

MAX CONTINUOUS OIL TEMP

A

140*C

64
Q

MAXIMUM transient oil temperature (15minutes)

A

155*C

65
Q

MINIMUM Starting oil temperature

A

-40*C

66
Q

Minimum oil temperature for takeoff

A

19*C (new updated number)

67
Q

Minimum oil quantity

A

11 quarts plus .5 quarts per hour of estimated flight time

68
Q

RPM MAXIMUM N1

A

104% in A320 and A321

101% in A320 NEO

69
Q

MAXIMUM N2

A

105% except

NEO is 116.5%

70
Q

Starter limitations

A

4 consecutive cycles, each of 2 minutes duration, maximum
20 seconds between cycles to allow for starter lubrication (60secs between starts and limited to 3 cycles in NEO )
After 4 cycles, 15 minutes to allow starter to cool before attempting a new start or motoring
Do not engage the starter when N2 is above 20% (above 59% in NEO)

71
Q

Reverse thrust

A

Prohibited selecting in flight
Prohibited from using reverse thrust to back the aircraft
Maximum reverse should not be used below 70kias (idle reverse is allowed down to aircraft stop)
Except in an emergency, reverse thrust is not authorized to reduce taxi speed

72
Q

Certified fuel types

A

JET A ,JET A1, NO.3JET, JET B, JP4, JP5, JP8, RT, or TSA-1

73
Q

Fuel temperature limits
Minimums
Maximums all but JETB and JP4
Maximum JETB and JP4

A 
JetA1/JP8/ no.3JET.         MINIMUM FUEL TEMP -43*C
JET A Minimum fuel temp -36*C( for JET A only, it TAT reaches -34*C, monitor on ECAM FUEL page that fuel temp remains higher than -36*C)
JP5 -42*C min
RT -45*C min 
TS-1 -45*C min
JET B -46*C min
MAX TEMP for all 54*C except
JET B and JP4 which max temp is 49*C
74
Q

Restricted altitude when using JP4 or JET B if wing fuel temperature exceeds 30*C at engine start

A

Restricted to 25,000 ft until center fuel tank is empty

75
Q

APPROXIMATE USEABLE FUEL WEIGHT AND VOLUME

A

Inner wing tanks = 6924x2 liters or 1829x2 gallons or 11982x2 lbs
Outer wing tanks = 880x2liters or 232x2gallons or 1520x2 lbs
Center tank = 8250 liters or 2180 gallons or 14281 lbs

Total
=23858 liters
=6302 gallons
=41285 lbs

76
Q

Max hydraulic pressure

Normal hydraulic pressure

A

3200psi

Normal hydraulic pressure is 3000 psi for all systems unless blue on ram air turbine which in that case is 2500psi

77
Q

Hydraulic fluid quantity

A

In the green band

78
Q

Maximum brake temperature for takeoff

A

300*C

79
Q

Parking brake caution

A

Do not set N1 above 75% on both engines with the parking brake on.

80
Q

Reduced thrust take offs
A319
A320

A

Thrust reduction not to exceed 25% of full rated takeoff thrust.
A319 flex temperature must not be higher than (T MAX THRUST) ISA+60C
320 flex temperature must not be higher than (T MAX THRUST) ISA+53C
Assumed temperature must not be lower than the flat rating temp or the actual OAT.
Not allowed from slippery or contaminated runway
Or if wind-shear is predicted or present including wind-shear alert

81
Q

Minimum fuel for takeoff

A

3300 lbs and the WING TK LO LVL warning must not be displayed on the ECAM

82
Q

Max fuel imbalances

A

Inner/outer tank imbalances
When heavier tank full Max imbalance
Full. 3305/1102lbs
9480/6613lbs 3520/2310lbs
4960/3196 lbs. 4960/3195* lbs
*All numbers with * are for shark-let takeoff performance aircraft

Outer tanks max imbalance 1520/815* lbs

83
Q

Center fuel tanks

A

Must be emptied first followed by the wing tanks

Takeoff on center tank prohibited. ( engines 1 and 2 must be completely segregated for takeoff (cross feed valve closed)

84
Q

Taxi with deflated tires

A

One deflated tire on one or more gears(max 3) then taxi speed limited to 7 knots in the turns.
If 2 tires deflated on same side (other main gear tires not being deflated) then taxi speed limited to 3 knots and nose wheel steering angle not to exceed 30 degrees

Taxi should only be done if absolutely necessary and all other means of moving the aircraft have been exhausted

85
Q

When both PFDs are lost the ——- must not be used

A

ISIS Bugs function

86
Q

A320 dimensions
Wingspan
Length
Height

A

Wingspan 112 feet
Length 123 feet
Height 38’ 7”

87
Q

A319 dimensions
Wingspan
Length
Height

A

Wingspan 112’
Length 111’
Height 38’ 7”

88
Q

A321 Dimensions
Length
Wingspan
Height

A

A321
Length 146 ft (23’ longer than A-320)
Wingspan 111’10”
Height 39’11”

89
Q

Fire push button does what 8 things

21212

A 
Silences repetitive chime
Arms the squibs
Hyd fire shut off valve closes
Shuts LP fuel valve to associated engine
FADEC power supply is removed and turns off IDG return fuel (thru FADEC )
Shuts off associated generator
Engine bleed valve closes
Pack flow valve closes
90
Q

APU fire shut off push button does what 7 things

20212

A 
Continuous chime is silenced
Halon bottle Squibb is armed
Squibb light illuminates
APU LP fuel valve closes
APU fuel pump shuts off (shutting down APU)
APU bleed valve closes
APU generator is deactivated
91
Q

Airbus 320 engine

A

CFM56-5B4

92
Q

Alpha lock speeds

A

The alpha/speed lock function is activated when:
1. Alpha exceeds 8.6 or
2. Airspeed falls below 148 knots
Results of alpha/speed lock function: Retraction from position 1 to position 0 is
inhibited.
Inhibition removed when:
1. Alpha falls below 7.6 or
2. Speed exceeds 154 knots.
Alpha/speed lock function not active if:
1. Alpha exceeds 8.6 or airspeed falls below 148 knots after pilot has moved the flap
lever to 0; or
2. Aircraft is on ground with speed less than 60 knots.

93
Q

Engine
Max N1
Max N2

A

N1 104%

N2 105%

94
Q

When is PTU inhibited?

A
  • When parking brake is set with only one engine master in on position .
  • When nose wheel steering disconnect pin is installed and only one engine master is on.
  • When PTU switch is off
  • during cargo door operation ( continues approx 40 sec after door operation)
95
Q

Alpha lock

A

This function inhibits slat retraction at high angles of attack and low speeds.
The SFCCs use corrected angle-of-attack (alpha) or airspeed information from the air
data inertial reference units (ADIRUs) to key the inhibition of slat retraction.
If alpha exceeds 8.5 (8° on A321) or the airspeed falls below 148 knots (165 knots
on A321), retraction from position 1 to position 0 is inhibited. The inhibition is
removed when alpha falls below 7.6 (7.1° on A321) or when the speed exceeds 154
knots (171 knots on A321).
This function is not active if:
– Alpha exceeds 8.5 (8° on A321) or the airspeed falls below 148 (165 knots on
A321) knots after the pilot has moved the lever to 0.
– The aircraft is on the ground with its speed less than 60 knots.

Airbus limitations (2 decks)

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