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TRAINEE 2
INIT T/O
20 - TAKE-OFF - ALPHA LOCK (DEMO) | | FD | ATHR | | |
21 - RADAR VECTORS | | FD | ATHR | | |
22 - ILS APPROACH | | FD | | | |
23 - LANDING
INIT T/O
24 - TAKE-OFF | | FD | ATHR | | |
25 - VISUAL PATTERN | | | ATHR | FPV | |
26 - REJECTED LANDING AT 30 FT | | | ATHR | | |
27 - VISUAL PATTERN | | | | FPV | |
28 - LOW ENERGY WARNING | | | | FPV | |
29 - LANDING (SIDESTEP)
INIT T/O
30 - TAKE-OFF | | FD | ATHR | | |
31 - RADAR VECTORS | AP | FD | ATHR | | |
32 - NON PRECISION APPROACH | AP | | ATHR | FPV | FPD |
33 - LANDING
34 - 180° TURN ON RUNWAY
IF TIME PERMITS :
35 - VISUAL APPROACH
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REV 23 JUL 99
R
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A319/A320/A321
FLIGHT CREW TRAINING MANUAL
REGULAR COURSE
NORMAL COURSE SYLLABI
EFC2R\NORMAL\N3FFS
N3 FFS SESSION GUIDE
01 - SESSION OBJECTIVE
· Introduction to the normal law protection
· Introduction to aircraft handling characteristics.
02 - TRAINING TOPICS
A. REVIEW
· ILS and non precision approaches.
B. INTRODUCE
· Simulator and installation safety.
· Flap auto retraction function
· Normal law - protections
· Low energy warning
· 180° turn on runway
· Slats / Alpha-speed lock function
· Visual pattern - landing
· CRM briefing : situational awareness - preventing (if not previously debriefed).
03 - SESSION PROFICIENCY CRITERIA
· Understanding of normal law protections and flap auto retraction system.
· Ability to perform :
- Standard ILS approach within tolerances (SOP, ILS approach)
- Standard Non precision approach
· Ability to apply correct landing technique.
04 - SESSION GUIDE
Eng V1 VR V2 Flex
CFM 124 134 134 52
IAE 124 134 134 57
INSTRUCTOR ONLY INSTRUCTOR ONLY
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REV 22 OCT 98
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
REGULAR COURSE
NORMAL COURSE SYLLABI
EFC2R\NORMAL\N3FFSGD
N3 FFS SESSION GUIDE (END)
04 - SESSION GUIDE (END)
1 : Instructor should encourage the crew to save time during transit cockpit preparation.
3 : When flaps at 1 + F do not retract further, observe flaps auto retraction at 210 kt.
5 : Accelerate to 300 kt, then demonstrate :
Roll :
- Stability up to 33° of bank.
- Need of back stick pressure with bank angle above 33°.
- Max bank angle : 67° (load factor).
Pitch attitude : 30° (25°) up, 15° down, in clean configuration.
High speed : VMO only
- VMO + 6 : warning pitch up load factor.
- In dynamic : VMO + 16 or 30 kt.
- Bank angle limitation : 45°.
- Positive spiral stability.
High angle of attack :
- Alpha prot.
- Alpha floor.
- Alpha Max.
- Bank angle limitation 45°.
CFIT : one emergency pull up.
Trainee 1 then Trainee 2 performs the normal law demonstration.
Trainee 1 resumes control at the end of the demonstration.
11, 26 : Demonstrate the need for increased back pressure on the side stick to achieve the
required pitch attitude (flare law).
Perform go around at low altitude (30 ft) - Rejected landing (JAR requirement).
13, 28 : Extend downwind, set conf 2 and demonstrate low energy warning (Speed - Speed -
Speed), by turning to base leg with nose up (manual thrust).
When final turn complete, ATC orders a runway change.
"Cleared to land on RWY 15 L (or 33 R)". Aircraft must be stabilized at 500 ft AGL.
17, 32 : VOR or NDB approach, managed or selected at trainee discretion.
20 : At ACC ALT, retract F1 then adjust pitch + 20°.
When speed is less than 148 kt retract flap to 0.
Observe Alpha Lock on ECAM Flap indicator.
Resume normal pitch and observe flap retraction when protection is removed.
INSTRUCTOR ONLY INSTRUCTOR ONLY
2.02.04
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REV 23 JUL 99
R
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A319/A320/A321
FLIGHT CREW TRAINING MANUAL
REGULAR COURSE
NORMAL COURSE SYLLABI
EFC2R\NORMAL\N3FFSGD
N4 FFS TAKE-OFF DATA
INIT PAGE ATIS
CO RTE FROM/TO TRIP DIST RWY ............... 15 R
TLSLHR1 LFBO/EGLL 519 NM WIND ............. 060°/10 kt
ALTN/CO RTE CRZ WIND VISI ................
090°/35 kt CEILING ........ CAVOK
FLT NBR ALTN TEMP.............. 14°C
[Airline ID] 204 EINN DEW POINT ... 10°C
LAT LONG ALTN DIST QNH ............... 1003 hPa/29.62 inHg
4338.1N 00122.1E 330 NM QFE ............... 985 hPa/29.08 inHg
COST INDEX FL to ALTN RWY COND ... DRY
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Airbus.Flight.Crew.Training.Manual空客机组训练手册1(99)
