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SYLLABI
EFC2R\FAILURE\F2FBSGD
F2 FBS SESSION GUIDE (END)
04 - SESSION GUIDE (END)
7 : Alternate / Direct law. Demonstrate for Trainee 1 and Trainee 2 :
- Stability in pitch : accelerate to 300 kts, observe autotrim.
- Loss of stability in roll with higher roll rate : turn with 45° of bank.
- Reduce speed and establish the aircraft in landing configuration : show that at
landing gear extension the alternate law switches to direct law : use of manual trim.
Transfer controls to Trainee 2. Repeat starting from direct law in landing configuration.
Then accelerate and clean up the aircraft.
Demonstrate alternate law.
Do not spend too much time for this demonstration. Both alternate / direct laws will be
studied in a FFS session.
- Restore ADR 1 + 2 fault. Trainee 1 as PF.
9, 14 : For Trainee 1 :
Insert B reservoir OVHT. When the status page has been cleared, insert a G reservoir
LO LVL.
When the malfunction becomes active (B RSVR OVHT) insert B electrical pump fault
in addition and keep both malfunctions as well active till next landing in order to avoid a
system restore.
For Trainee 2 :
Insert Y reservoir LO LVL : when the status page has been cleared, insert a G reservoir
LO LVL.
17 : Smoke associated with fuel vapors is coming from cabin to the cockpit : this will lead to
select two packs off and conduct to initiate a high speed descent.
20 : The trainee will insert a short F-PLN : direct to GAI.
Emphasize :
- Use of RMP1 for APPR NAVAID.
- Fuel gravity feeding.
- Use of QRH for equipment list.
Freeze the simulator for ECAM actions. Release for approach activation.
INSTRUCTOR ONLY INSTRUCTOR ONLY
2.02.05
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Page 6B
REV 23 JUL 99
R
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A319/A320/A321
FLIGHT CREW TRAINING MANUAL
REGULAR COURSE
ABNORMAL/EMERGENCY COURSE
SYLLABI
EFC2R\FAILURE\F2FBSGD
F3 FFS TAKE-OFF DATA
INIT PAGE ATIS
CO RTE FROM/TO TRIP DIST RWY ............... 15 R
LFBO/LFPO 345 NM WIND ............. 100°/12 kt
ALTN/CO RTE CRZ WIND VISI ................ 6 km
240° / 30 kt CEILING ........ SCT 400 ft
FLT NBR ALTN TEMP.............. 1°C
[Airline ID] 303 EDDF DEW POINT ... -3°C
LAT LONG ALTN DIST QNH ............... 1003 hPa/29.62 inHg
4338.1N 00122.1E 295 NM QFE ............... 985 hPa/29.08 inHg
COST INDEX FL to ALTN RWY COND ... WET
30 240 Observations : ________________
CRZ FL/TEMP TROPO ________________
FL 350 / -52°C ________________
________________
INIT NEXT PAGE PERF PAGE T/O FLAPS NOTE :
ZFCG/ZFW IAE CFM 2 F/PLN :
28.8%-54 t
28.8%-118 800 lb
V1 LFBO 15 R
T/O C.G. FISTO SID
VR 27.5% UT 210 - LMG
UT 258 - MORIK
V2 TOGA UT 158 - AMB
BLOCK NO STAR
12 t
26400 lb
FLEX FLEX VIA EPR
LFPO ILS 26
DRT DRT
2.02.05
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Page 7
REV 23 JUL 99
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
REGULAR COURSE
ABNORMAL/EMERGENCY COURSE
SYLLABI
EFC2R\FAILURE\F3FFS
MALFUNC
REF. - F3 FFS -
TRAINEE 2
1 - TRANSIT COCKPIT PREPARATION
INIT T/O
2 - ENGINE FAIL AT V2 (NO DAMAGE) | AP | FD | ATHR | | |
3 - ENGINE RELIGHT | AP | FD | ATHR | | |
4 - RADAR VECTORS | AP | FD | ATHR | | |
5 - ILS APPROACH | | FD | ATHR | | |
6 - GO AROUND - ENGINE FAIL (DAMAGE) | | FD | ATHR | | |
7 - RADAR VECTORS | AP | FD | ATHR | | |
8 - ILS APPROACH - ENGINE OUT | | FD | ATHR | | |
9 - LANDING - ENGINE OUT (OVERWEIGHT) - Restore | | FD | ATHR | | |
INIT T/O
10 - ENGINE FAIL AT V1 (CROSSWIND) | AP | FD | ATHR | | |
11 - RADAR VECTORS | AP | FD | ATHR | | |
12 - NON PRECISION APPROACH - ENGINE OUT | AP | | ATHR | | FPD |
13 - LANDING - ENGINE OUT (CROSSWIND) - Restore | | | ATHR | FPV | |
INIT T/O
14 - TAKE-OFF
15 - VISUAL PATTERN
16 - VISUAL APPROACH - NO SLATS/NO FLAPS
17 - LANDING - NO SLATS/NO FLAPS - Restore | | | | FPV | |
IF 2 CAPTAIN CREW OR 2 FIRST OFFICER CREW : CHANGE SEATS BEFORE BEGINNING THE "TRAINEE 1" STAGE
TRAINEE 1
INIT T/O
18 - ENGINE FAIL AT V2 (NO DAMAGE) | AP | FD | ATHR | | |
19 - ENGINE RELIGHT | AP | FD | ATHR | | |
20 - RADAR VECTORS | AP | FD | ATHR | | |
21 - ILS APPROACH | | FD | ATHR | | |
22 - GO AROUND - ENGINE FAIL (DAMAGE) | | FD | ATHR | | |
23 - RADAR VECTORS | AP | FD | ATHR | | |
24 - ILS APPROACH - ENGINE OUT | | FD | ATHR | | |
25 - LANDING - ENGINE OUT (OVERWEIGHT) - Restore | | FD | ATHR | | |
INIT T/O
26 - ENGINE FAIL AT V1 (CROSSWIND) | AP | FD | ATHR | | |
27 - RADAR VECTORS | AP | FD | ATHR | | |
　
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