A320 Limitations Flashcards

1
Q

MANEUVERING LOAD LIMITS(G’s)

A

Clean config — -1G to + 2.5G

Other config — 0G to +2G

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2
Q

Environmental envelope

A

Max alt 39800 ft

Max alt for T/o/ Lnd — 9200ft to -2000ft

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3
Q

RUNWAY SLOPE

A

+/- 2%

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4
Q

WIND LIMITATIONS (sop)

A
X wind T/o —      28 kts
X wind Ldg—-     28 kts
Xwind f/o. —-       14 kts
Tailwind  T/o + Ldg—    15 kts
Wind for T/o —-    50 kts
HWind for Auto land —   30 kts
X w Auto Lnd No autom roll out -  20 kts (chk ac)
X w Auto Lnd autom roll out -  15/20 (chk ac).
TL wind Auto Lnd   —-     10 kts
Wind oper doors —.  65 kts.
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5
Q

Max cockpit window open spd

A

Max —. 200 kts

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6
Q

FLAPS/SLATS SPDS VTA 321

A

Fl 1 — 235 kts. VTA A321 CEO CFM
Fl 2 — 215 kts
Fl 3 — 195 kts
Fl full — 190kts.

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7
Q

VMO/MMO

A

VMO — 350 kts

MMO — M 0.82

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8
Q

Max Spds Lndg gear

A

Max Spd w Lnd gear exten(vle) - 280k/m0.67

Max spd at which Lnd g may be extended —250kt
Gear locked.- 260 +~ 5 kt
(Vlo)250k/m0.60

Max spd at which Lnd g may be retr —
(Vlo) 220knots/m0.54

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9
Q

MAX TIRE SPD

A

Max Grnd spd —. 195 kts.

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10
Q

Min cntr spd for Landing

A

VMCL. — 113 kts

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11
Q

Max taxi spd > 76000 kg

A

20 kts hka

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12
Q

Wipers max oper spd

A

230 kts

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13
Q
WEIGHT LIMITATIONS A321 ceo vta
M TAXI
M TO WT
M LND WT
MZFW
MIN WT
A
A320:
Max taxi wt —     93900 kg
MTOW.      ——    93500 kg
MLW.         —-      77800 kg
MZFW.        —      73800 kg
Min wt.       —      47500 kg
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14
Q

Max pos diff pressure
Max neg diff press
Safety relief valve setting

A

Max pos diff press —- 9.0 psi
Max neg diff press —- -1.0 psi
Safety relief v setting—. 8.6 psi

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15
Q

Max cabin alt
Cab Alt Warn
Maxnorm cab alt

A

Max cab Alt. —- 14.000 ft
Cab Alt warn —- 9550 ft +/- 350
Max norm cab Alt — 8000 ft

Max diff pr + safety v tolerance =+/- 7 hpa
(0.1psi)

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16
Q

AP MIN/max alt

A
To —-   100 ft or min 5 sec after to
Appr —- G/S.  160 ft
Final app/ vs or fpa. 250 ft
Circling —-   600ft (D)
Cat 1 — 200/160 ft
Cat 2 — 100 ft
Cat 3 A — 50 ft
Cat 3 B — 0 ft
17
Q

Glide slope angle

A

Between -2.5 and 3.15•
<2500 ft

18
Q

APU MAX ROTOR SPD N
Max Egt Apu start <35000 ft
Max Egt Apu start >35000 ft
Max Egt Apu running

A

Max N spd. — 107%
Max Egt start <35000 ft - 1090c
Max Egt start >35000 ft - 1120c
Max Egt Apu running — 675c

19
Q

APU BLEED:
MAX ALT START ASSIST
MAX ALT AIR CON+ pres -1 pack
Max Alt aircon+ press -2 packs

A

Max Alt start assist. - 20000ft

Max Alt aircon+ pres 1 pck- 22500ft

Max Alt aircon+ press 2 pck - 15000ft.

Apu bleed for wing ai not permitted

20
Q

THR/EGT LIMITS ENGINES

Time/Temp

A

TO/GA ALL ENG - 5 min 950c
OneENG - 10 min 950c
MCT NO LIM. 915c
STARTING. GRND/AIR. 725c

21
Q

ENGINES
MAX N1
MAX N2

A

Max N1 — 104%

Max N2 — 105%

22
Q

ENG CONT OIL TEMP:

MAX TRANSIENT
MIN STARTING TEMP
Min BEFORE TAKEOFF

A

Max cont temp. — 140c
Max trans (15 min) —. 155c
Min start temp. — -40c
Min temp before T/0 —. -10c

23
Q

OIL QUANTITY

A

AT OR ABOVE. — 9.5 qrt

Estm consumption — 0.5 qrt/hr

24
Q

OIL PRESS MINIMUM

A

13 Psi

25
Q

ENG STARTER LIM

A

3 Start attemps autom= one cycle

Grn autom/man , a 20 sec pause btw cycles

A 15 min cooling after 4 failed cycles

Starter must not run when N2>20%

26
Q

MAX OPER FLAPS SLAT EXTENDED ALT:

A

20000ft

27
Q

MIN FUEL QUANT FOR T/O

A

1500 kg

NO “Fuel Wing Tk Lo LvL” dur T/O

28
Q

BRAKE TEMP MAX FOR T/O
Brk fan off
Brk fan on

A

(Brake fans off). 300c

Brk fan on. 150c

29
Q

MAX NOSEWHEEL STEERING degrees tiller

A

+/- 85* tiller

95 towing

30
Q

MAX TAXI SPD DEFLATED TIRES

A

1 Tire per gear deflated —. 7 kts

2 Tires defl same gear(max 1 main gear). — 3 kts

Max nosewh steering angle defl tires —. 30*

31
Q

MIN OXIGEN PRESSURE

A

At Temp 30c. — need. Min 708psi (use average 850psi)
2 crew + 1 observer

On grnd. Ref Temp= oat+Ckp t/ 2

32
Q

Oxygen AND TIME DURATION:
Emerg descent
Cruise
Smoke

A

EMERGENCY DESCENT - 22 min

CRUISE AT 8000 ft — 98 min

SMOKE 100%Oxigen at 8000 ft. — 15 min

33
Q

ICE ACCRETION SEVERE ?

MAX ALLOWED UNDER WING ?

A

5 mm (0.2 in) SEVERE

3mm max underwing allowed.

34
Q

MAX FUEL DIFF BTW UPLIFT
AND CALCULATED UPLIFT.

TAKE OFF WEIGHT MAX DIFF OR
NEW FLIGHT PLAN (CFP).

A

A321. Diff >5% manual check must be performed (Vta)

TO WT DIFF WITH CFP MAX 3000 kg

35
Q

LMC WEIGHT CHANGE MAX (HKA)

A

MAX BELOW OR EQUAL TO

500 KG hka

36
Q

NORM HYDR PRESSURE

A

3000 psi (+- 200 psi)