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240°/35 kt CEILING ........ 600 ft
FLT NBR ALTN TEMP.............. 30°C
[Airline ID] 404 LFBO DEW POINT ... 25°C
LAT LONG ALTN DIST QNH ............... 1010 hPa/29.83 inHg
4338.1N 00122.1E 176 NM QFE ............... 992 hPa/29.25 inHg
COST INDEX FL to ALTN RWY COND ... DRY
30 220 Observations : ________________
CRZ FL/TEMP TROPO ________________
FL 230 / -25°C 36090 ________________
________________
INIT NEXT PAGE PERF PAGE T/O FLAPS NOTE :
ZFCG/ZFW IAE CFM F/PLN :
28.4%-48 t
28.4%-105 600 lb
V1 LFBO 33 L
T/O C.G. AFRIC DEP
VR 26.6% G393 - FJR
G6 - VARES
V2 TOGA VARES ARRIVAL
BLOCK LFML 14 L
10 t
22 000 lb
FLEX FLEX
DRT DRT
2.02.05
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A319/A320/A321
FLIGHT CREW TRAINING MANUAL
REGULAR COURSE
ABNORMAL/EMERGENCY COURSE
SYLLABI
EFC2R\FAILURE\F6FFS
MALFUNC
REF.
- F6 FFS -
SKILL TEST
TRAINEE 1
1 - TRANSIT COCKPIT PREPARATION (B)
2 - BEFORE START
3 - ENGINE START - MANUAL OR CROSS BLEED OR HOT START OR VALVE FAULT
4 - AFTER ENGINE START
5 - TAXI OUT
6 - TAKE-OFF - SID - ADR FAULT | AP | FD | ATHR | | |
7 - RETURN TO DEPARTURE | AP | FD | ATHR | | |
8 - ILS APPROACH | | FD | ATHR | | |
9 - GO AROUND - ENGINE FAIL | | FD | ATHR | | |
10 - RADAR VECTORS | AP | FD | ATHR | | |
11 - ILS APPROACH - ENGINE OUT | | FD | ATHR | | |
12 - LANDING - ENGINE OUT - Restore
INIT T/O
13 - ENGINE FAIL AT V1 | AP | FD | ATHR | | |
14 - ENGINE RELIGHT | AP | FD | ATHR | | |
15 - RADAR VECTORS | AP | FD | ATHR | | |
16 - NON PRECISION APPROACH | AP | FD | ATHR | | FPD |
17 - CIRCLING | | | ATHR | FPV | |
18 - LANDING
INIT T/O
19 - TAKE-OFF | AP | FD | ATHR | | |
20 - RADAR VECTORS | AP | FD | ATHR | | |
21 - G + B SYS LO PR OR G + Y SYS LO PR | | FD | ATHR | | |
22 - VISUAL APPROACH - DIRECT LAW - NO SLATS OR NO FLAPS | | | ATHR | FPV | |
23 - LANDING - DIRECT LAW - NO SLATS OR NO FLAPS - Restore
IF 2 CAPTAIN CREW OR 2 FIRST OFFICER CREW :
INIT T/O
24 - ENGINE FAIL BEFORE V1
25 - REJECTED TAKE-OFF
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R
R
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
REGULAR COURSE
ABNORMAL/EMERGENCY COURSE
SYLLABI
EFC2R\FAILURE\F6FFS
MALFUNC
REF.
- F6 FFS (END) -
SKILL TEST
TRAINEE 2
INIT T/O
26 - TAKE-OFF - WINDSHEAR | | FD | ATHR | | |
27 - RADAR VECTORS - STAR | AP | FD | ATHR | | |
28 - ILS APPROACH | | FD | ATHR | | |
29 - GO AROUND - ENGINE FAIL | | FD | ATHR | | |
30 - RADAR VECTORS | AP | FD | ATHR | | |
31 - ILS APPROACH - ENGINE OUT | | FD | ATHR | | |
32 - LANDING - ENGINE OUT - Restore
INIT T/O
33 - ENGINE FAIL AT V1 | AP | FD | ATHR | | |
34 - ENGINE RELIGHT | AP | FD | ATHR | | |
35 - RADAR VECTORS | AP | FD | ATHR | | |
36 - NON PRECISION APPROACH | AP | FD | ATHR | | FPD |
37 - CIRCLING | | | ATHR | FPV | |
38 - LANDING
INIT T/O
39 - TAKE-OFF | AP | FD | ATHR | | |
40 - RADAR VECTORS | AP | FD | ATHR | | |
41 - DUAL ADR FAULT OR DUAL IR FAULT OR DUAL RA FAULT | | | | FPV | |
42 - VISUAL APPROACH - DIRECT LAW | | | | FPV | |
SINGLE ADR OR SINGLE IR OR NO RA
43 - LANDING - DIRECT LAW - SINGLE ADR OR SINGLE IR OR NO RA - Restore
INIT T/O
44 - TAKE-OFF - ENGINE FIRE BEFORE V1
45 - REJECTED TAKE-OFF
46 - EMER EVAC
IF 2 CAPTAIN CREW OR 2 FIRST OFFICER CREW : CHANGE SEATS AT ITEM 26
2.02.05 R
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REV 23 JUL 99
R
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
REGULAR COURSE
ABNORMAL/EMERGENCY COURSE
SYLLABI
EFC2R\FAILURE\F6FFS
F6 FFS SESSION GUIDE
01 - SESSION OBJECTIVE
· Evaluation of the ability to operate the aircraft in normal and abnormal operations according
to standard requirements.
02 - TRAINING TOPICS
· Suggested briefing :
- "The evaluation will consist of a series of exercises : before each take-off I will brief you
on what is expected. When released, follow the departure clearance and deal with any
problems or emergencies as they occur using the procedures and techniques learnt
during the training course.
- You should use Airbus standard procedures or your own company procedures if different.
- You will be responsible for liaison with ATC, safe operation and navigation of the aircraft.
Make sure that you correctly understand ATC instructions. During the flight, it will be
necessary for me to initialize the simulator in order to carry out exercises ; I will inform
　
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