DSC Flashcards
Information Layers
L1: Need to know
L2: Nice to know
L3: Detailed information
PWS during T/O
Alerts inhibited from 100kt to 50ft
Reactive WS
Detected by the PRIM
T/O:
3s after L/O (or 50’) until 1300
LDG:
1300 to 50’
Only works with flaps/slats out.
TAWS has:
- GPWS with 5 basic modes
- TERR and OBST function
- TAWS Database
GPWS 5 Modes
STEPH
S ink Rate - > Pull Up T errain Closure - > Pull Up E rratic path after T/O or G/A P rotec. X Config (Too low gear, Flaps, TERR) H and flying the ILS "Glide Slope"
Flap Mode (4B) G/S Mode (5)
Fuel Transfer Sequence
After T/O LA to Outers
MT = from IMTO to Feeds
CG = from TT to IMF
LA from TT
LA from Outers
Which systems has ADV?
EPA!
Engine
Pressurization
APU
Speed brake auto retraction occurs in case of
- Alpha floor
- Low speed stability is active
- G/A
Once retracted they remain in that position until lever is first set in the retracted position for 5sec and then moved.
PFD pitch trim indications
Green band is the certified range of pitch trim positions, whatever the aircraft CG within the certified envelope. Ranges from 29% to 43% (5.8 nose up to 0.2 nose down)
Magenta bar is +/- 1.5 degrees from the optimum pitch trim position for the current GWCG (in degrees not %)