Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
94 Cards in this Set
- Front
- Back
Flight maneuvering load acceleration limits
-clean config -slats&flaps extended -slats extended & flaps retracted |
-1g ~ +2.5g
-0~+2g -0~+2g |
|
Max pax seats
|
180
|
|
Min flight crew
|
2
|
|
Max taxi weight
A320/320e |
77.4 /78.4 |
|
Max T/O weight A320/320e
|
77 /78
|
|
Max landing weight A320/320e
|
66
|
|
MZFW A320/320e
|
62.5
|
|
Minimum weight A320/320e
|
37.23
|
|
Max/Min TO & LDG alt
|
9200ft
|
|
RWY Slope
|
±2%
|
|
Nominal RWY width
|
45m
|
|
Max demonstrated Xwind
|
38kt gust included
|
|
Max tail wind for T/O
|
15kt |
|
Max tail wind for LDG
|
10kt
|
|
Max tail wind for auto land
|
10kt
|
|
Flap config for max tail wind
|
Flaps full
|
|
Max wind for pax door operation
|
65kt
|
|
Max wind for cargo door operation
|
40kt
(or 50kt, if the nose is oriented into the wind, or cargo door is on the leeward side) |
|
MMO
|
M0.82
|
|
VMO
|
350kt
|
|
Max tire speed
|
195kt
|
|
Windshield wiper speed
|
230kt
|
|
Cockpit window open
|
200kt
|
|
Taxi speed >76t
|
not more than 20kt during turn
|
|
Ram air inlet can be open if...
|
differential pressure is less than 1PSI
|
|
Do not use HP ground air-con unit when...
|
APU supplies bleed air to avoid SYS damage.
|
|
Max positive differential pressure
|
9PSI
|
|
Max negative differential pressure
|
-1PSI
|
|
Min height for use of AP on T/O with SRS mode
|
100ft AGL
|
|
Min height for use of AP in straight-in NPA
|
applicable MDA(MDH)
|
|
Min height for use of AP in straight-in LNAV/VNAV APPR
|
applicable DH
|
|
Min height for use of AP in circling APPR
|
applicable circling minimums -100ft
|
|
Min height for use of AP in ILS APR when CAT2 or CAT3 not displayed on FMA
|
160ft AGL
|
|
Min height for use of AP in PAR
|
250ft AGL
|
|
Min height for use of AP in GA
|
100ft AGL
|
|
Min height for use of AP in all other phases A320/321
|
500ft AGL
|
|
Use of AP/FD in "OP DES" or "DES" mode is not permitted below
|
not permitted in approach unless FCU alt is set to MDA(MDH) or 500ft whichever is highest
|
|
NAV mode may be used in terminal area, provided...
|
-GPS PRIMARY is avail
-HIGH accuracy and RNP is checked or entered on the MCDU -NAVAID raw data is monitored |
|
CAT Ⅱ MDH
|
100ft AGL
|
|
Auto APR without AUTO LAND disengage AP no later than...
|
80ft AGL
|
|
CAT Ⅲ SINGLE MDH
|
50ft
|
|
CAT Ⅲ DUAL MDH
with DH / without DH (a320) |
Alert height 100ft
MDH 20ft / Minimum RVR 75m |
|
Max head wind for CATⅡ or CATⅢ AUTO LAND & ROLL OUT
|
30kt
|
|
Max tail wind for CATⅡ or CATⅢ AUTO LAND & ROLL OUT
|
10kt
|
|
Max Xwind wind for CATⅡ or CATⅢ AUTO LAND & ROLL OUT
|
20kt
|
|
CATⅡ or CATⅢ AUTO LAND is approved in CONF...
|
CONF3 & CONF FULL
|
|
Max continuous load per GEN
|
100% (90KVA)
|
|
Max continuous load per TR
|
200A
|
|
Max operating alt with slats and /or flaps extended
|
20000ft
|
|
Max allowed wing fuel imbalance
INNER TANKS Tank fuel quantity -FULL a320 |
1500kg
|
|
Max allowed wing fuel imbalance
INNER TANKS Tank fuel quantity -4300kg a320 |
1600kg
|
|
Max allowed wing fuel imbalance
INNER TANKS Tank fuel quantity -2250kg a320 |
2250kg
|
|
Max allowed wing fuel imbalance
INNER TANKS Tank fuel quantity -below 2250kg |
no limit
|
|
Max allowed wing fuel imbalance
OUTER TANKS |
690kg
|
|
Min fuel quantity for T/O
|
1500kg
|
|
Normal HYD pressure
|
3000PSI ±200
|
|
max brake temp for T/O
|
fans off 300℃
|
|
AUTO BRAKE can be disengaged by...
|
-Pressing pushbutton of the armed mode, or
-Applying sufficient pressure to the brake pedals |
|
If one tire is deflated on one or more gears, taxi speed should be...
|
limited to 7kt when turning
|
|
If two tires are deflated on same main gear, taxi speed and nose wheel steering angle should be...
|
limited to 3kt and 30°
|
|
The nose steering angle when using handwheels
|
75°
|
|
The nose steering angle for towing and pushback
|
95°
|
|
The nose steering angle for Towbarless towing and pushback
|
85°
|
|
EGPWS enhanced function / GPWS predictive function should be inhibited when the A/C position is...
|
Less than 15nm from airfield
|
|
ISIS bug function must not be used when...
|
Both PFDs are lost
|
|
Min O2 pressure
|
Ref LIM 35 Oxygen(table)
|
|
APU
If LOW OIL LEVEL ECAM ADV is displayed... |
APU may be started and operated. MAINT action is Req within next 10hrs of APU ops
|
|
APU
Starter motor cycle |
after 3 motor duty cycles, wait for 60min
|
|
APU
Max N |
107%
|
|
APU
MAX EGT for start |
Below 35000ft 1090℃ Above 35000ft 1120℃ |
|
APU
Max EGT |
675℃ |
|
APU
ELEC PWR EXTRACTION at or below 25000ft ISA +35℃ and below |
90KVA
|
|
Engines
Time and Temp limit @TOGA a320 |
5min / 10min (engine failure)
950℃ |
|
Engines
Time and Temp limit @MCT a320 |
Unlimited
915℃ |
|
CFM56-5B
Temp limit @Starting a320 |
725℃
|
|
CFM56-5B
Max continuous Oil temp |
140℃
|
|
CFM56-5B
Min starting temp |
-40℃
|
|
Engines
Min oil quantity |
9.5qt +0.5qt/h
|
|
Engines
N1 max |
104%
|
|
Engines
N2 max |
105%
|
|
Engines
Starter limit |
-Max 2min of 4 consecutive cycles
-20s of Pause between start attempts -15min of cooling period -No engagement when N2 is above 20% |
|
Engines
Max Reverse Min speed |
70kt
|
|
Engines
Reduce thrust T/O Thrust reduction must not exceed ....% of full rated T/O thrust |
25%
|
|
Engines
FLEX temp must not be higher than |
ISA+53℃ (T MAX FLEX)
|
|
Engines
FLEX T/O is not permitted on |
contaminated RWY
|
|
What is the maximum operating altitude? |
39,800 |
|
What are the maximum speeds for each flap/slat config? |
As indicated on the cockpit placard |
|
What is the safety relief valve setting? |
8.6 psi |
|
What is the aircon limitation when using an LP ground unit? |
Do not use simultaneously with packs (to avoid chattering of the non return valve) |
|
What is the limitation regarding use of authothrust in selected or managed mode? |
None, use of auto thrust is approved with or without AP or FD in selected managed mode. |
|
what is the limitation regarding using NAV mode after take off? |
may be used provided FMGS runway updating has been checked. |
|
What is the limitation regarding obstacle clearance and constraints programmed into FMGS? |
Obstacle clearance and adherence remains the flight crew's responsibility. |
|
What is the limitation/precaution regarding the fuel, time predictions/performance information available through FMGC. |
This information is provided for advisory purposes only. |
|
What is the limitation regarding the use of NAV, or NAV and FINAL APP mode during instrument approaches? |
sawad hay 3alaik |