Limitations Flashcards
Load limits clean - others
-1 to 2.5 g — 0 to 2g
Airports limits
- rnw slope
-rnw altitude
-nominal width
-minimal width
- 2%
-9200 ft (GEZX 14100ft )
-45 m
-30 m
Winds
-Crosswind
-tailwind t/o
-tailwind landing
-passenger and cargo door
-38 kts
-15
-10 (15 GEZX-FTXQ-GTCY )
-65 pax - 40 cargo (50 if nose up wind)
Cockpit window open
200
Flaps speed
-1
-1+f
-2
-3
-full
CEO
-235
-225
-215
-195
-190
Neo
-243
-225
-215
-195
-186
VMO/MMO
350 kts / 0.82 M
Landing Gear
-Extended
-extension
-retraction
-280 / 0.67
-250 / 0.60
-220 / 0.54
Max tire speed
195
VMCL
115 kts NEO
116 kts CEO
Wipers speed
230 kts
Weights
- max taxi
- max t/o
- max landing
-zero fuel
-min.
NEO
-97 400 kg
-97 000
-79 200
-75 600
-46 300
CEO
- 93 900Kg
- 93 500
- 77 800
- 73 800
- 47 500
With pax on , __ min max without air conditioning
20 min
Avionics ventilation
OAT + = 49 degre : no limit
+ 49 : see fcom
Cabin press
- max positive diff
- max negative diff
- safety valve
- 9.0 psi
- 1.0
- 8.6
Auto pilot min alt.
- for t/o
- In app with F-G/S
- In app with Final app , V/S or FPA
- In circling
- 100 ft agl and at lest 5s after liftoff
- 200 Ft
- 250 Ft
- 500 Ft cat C aircraft ( 600 ft for Cat D aircraft)
Auto pilot min alt.
- Ils CAT 1
-CAT 2 and 3
-LPV
- 160 Ft
- 0 ft if autoland ( 80 ft if manual)
- 160 ft
RNP accuracy with gps primary is:
En route :
In terminal :
In app:
- 1 nm with app on — 1 nm with app off an fd on — 1.1 nm with ap off and fd off
- 0.5 nm ‘’ — 0.51nm. ‘’ — 0.51 nm. ‘’
- 0.3 nm. ‘’ — 0.3 nm. ‘’ — 0.3 nm
ILS cat 2 decison height
100 ft
ILS CAT 3 fail passive ( single ) decison height
50 Ft
Min runway visual range for cat 3 dual
75 M
Max wind for Cat 2 and 3
CEO
Headwind : 40 kts for cat 2
30 kts for cat 3 and autoland
Tailwind: 10 kts
Crosswind : 25kts for cat 2
20 kts for cat 3 and autoland
NEO
Headwind : 15 kts
Crosswind : 10 kts
Tailwind : 10 kts
Autoland conditions
- conf 3 or conf full
- glide slope between - 2.5 and - 3.25 ( -3.15 CEO)
- airport elevation 9200 ft or below ( 5 750 Ft CEO )
-weight above 51 000 kg ( below max landing weight CEO)
-not below - 2000 ft press altitude ( - 1000 ft CEO) - auto rollout on one engine : no more idle thrust and wind not exceed max for roll out ( crosswind max 15 kts CEO)
APU starts limitations
Aftre 3 consecutive attemps , wait 60 min
Apu EGT
Start below 35 000
Start above 35 000
Running
- 1090
- 1120
- 675