Airbus Flashcards
Vlo
Ext 250kts
Ret 220kts
Vle
280/m.67
Vfe 1
230kt
Vfe 1+f
215kts
Vfe 2
200kts
Vfe 3
185kts
Vfe full
177kts
Below 1000ft above TDZE and above DH or alert height a go-around must be performed in case of:
Alpha floor activation Loss of AP (cavalry charge) Downgrading of capability (triple click) Amber caution (single chime) Engine failure
Automatic landings, below 200ft, go around in case of:
AUTOLAND warning
FLARE does not come up on FMA.
If visual landing may be done manually
Stable approach criteria
A/C in landing config Target final App +10/-5kts Rate of descent less than 1200ft/min A/C within 1 dot GS/loc (ILS)/ correct flight path Bank angle less than 15
RAT supplies EMER GEN down to?
125kts approx
PTU comes on when?
Differential pressure > 500psi
RAT extension and coupling takes?
Approx 8 secs
Closed circuit config temp. Controlled by?
Passing air through skin heat exchanger
Lights available in EMER ELEC config?
RH dome, LH instrument panel, STBY compass/ice, torch
A319 min pitch for tailstrike wings level
13.9 degrees
One engine out AUTOLAND config?
3 or full
Flex corrections
A/ice on -5
Qnh reduction -1/2hPa
Emergency descent
Oxygen masks and establish comms Alt select - turn an pull Heading - pull (maybe turn) Speed - pull Mach/spd - push to select spd Check FMA's Speed breaks (consider, apply slowly)
PNF Seatbelts on Mode select IGN transponder 7700 Radio mayday Pax oxy on (cab alt > 14000)
PF refine
Then “My radios EM DES xlist”
Set QNH on standby
Level off alt
Remove masks - close left door
PA SCC to FD
Autopilot disengage at
More than 25 nose up (normal law)
Pitch trim wheel beyond a certain point
Fire pushbutton
Lp fuel valve, hydraulic fire shut off valve, eng bleed valve and pack flow control valve close
Fadec power cut and IDG deactivated
CRC cancelled and squibs armed
To release brakes after RTO
Disarm spoilers
ALD in QRG based on
Spoilers operating, no reverse thrust
Predictive windshear alerts inhibited
Above 100kts up to 50ft, below 50ft
Normal law protections:
Load factor limitation
+2.5 to -1g clean
+2 to 0 other
Pitch attitude protection
+30 or +25 (Full) reducing by 5 at low speed. -15.
Bank angle protection
Positive spiral static stability above 33 degrees.
Automatically reduces to 33 degrees
Max 67 deg
AP disconnect >45 degrees
High Speed Protection
Nose up order applied VMO+6/MMO+0.01 AP disco
High Angle of Attack (has priority)
Side stick commands angle of attack to alpha max, will return automatically to alpha prot if released. AP disconnect at alpha prot+1. To deactivate protection s/stick 8 degrees forward or .5 degree for 5 seconds less than alpha max.
Alpha floor. (Autothrust) lift off to 100 ft above landing
Alternate law protections
Load factor limitation
same as normal law (+-red. prot)
No pitch att prot
No bank angle prot
High Speed Stability (with red prot, lost with 3 ADR failure)
above Vmo/Mmo nose up demand, pilot can override. Aural overspeed remains.
Low Speed Stability (lost with 2 ADR failure)
active 5-10kts above SW speed, gentle progressive nose down introduced, keeps speed above VSW. Audio stall warning remains. Aircraft can stall. No Alpha floor.
Max flaps/slats alt
20000ft
All electric generators output power
90kVa