Modulo A
Modulo A
PARTE D. CAPACITACIÓN
ENTRENAMIENTO PERIÓDICO A340 Apéndice EDICIÓN IV PÁGINA
1/15
MÓDULO A D 28/03/2025
TRAINING SESSION A
PILOT’S NAME: DATE:
CAPT. ☐ FO. ☐ SIM TYPE AND PLACE:
BRIEFING ROOM
Review Technical: Fuel leak / Stall recovery
Review CRM: Problem solving / Decision making
00.15
CRUISE
ATA 26 AFT CRG SMOKE.
DESCENT TO....
PROVIDE RADAR VECTOR TO FINAL
PASSING 2000FT :
CONTACT DEPARTURE ON...
CLIMB:
CB AVOIDANCE / MODERATE TURBULENCE -
01.40 INTRODUCE WIND / TEMP CHANGE
00.25
RETURN TO LEMD
PROCEED DIRECT TO .... AND CONTACT APP
OVERWEIGHT LANDING
GO AROUND
SET CAVOK
ON FINAL
02.05 WIND .../ ... RWY ... CLEAR TO LAND
00.10
02.15 BREAK
00.20 POS INIT: HOLDING POINT (or TO POS ) RWY 36L - ENGINES RUNNING
WX INIT: 040/15KT 9999 BKN 010 OVC025 25/18 QNH 1019 / RWY DRY
ACFT INIT : ZFW :150T FUEL:60T ZFWCG: 30.2
CONF2 // FLEX 52 // V1= 146 // VR=156 // V2=161
ACFT INIT : ZFW :220T FUEL:20T ZFWCG:29.0 if STD
CONF2 // FLEX 72 // V1= 130 // VR=139 // V2=149 Crew:
ATC CLEARANCE: SID PINAR - RBO / CLIMB INITIALY 7000FT CM2
TAKE OFF:
ENGINE FAILURE BETWEEN V1 AND V2 -
ATA 70 ENGINE FLAME OUT WITH DAMAGE
VISUAL CIRCUIT -
00.20 POS INIT: HOLDING POINT (or TO POS ) RWY 36L - ENGINES RUNNING
WX INIT: 040/15 9999 BKN 010 OVC025 25/18 QNH 1013 / RWY DRY
ACFT INIT : ZFW :170T FUEL:60T ZFWCG:30.0
CONF2 // FLEX 51 // V1 = 146 // VR=156 // V2=161 if STD
ACFT INIT : ZFW :220T FUEL:20T ZFWCG:29.0 Crew:
CONF2 // FLEX 72 // V1= 130 // VR=139 // V2=149 CM1
ATC CLEARANCE: SID PINAR CLIMB INITIALY 7000FT
-
TAKE OFF: ENGINE FAILURE BETWEEN V1 AND V2 if NON
ATA 70 ENGINE COMPRESSOR STALL (NORMAL PARAMETERS: STALL DOES NOT RECUR) STD
Crew:
CM1
RADAR VECTORS
or
ASK CREW TO DISENGAGE AP 1+2 AND FD1+2
ILS APPROACH RAW DATA LEMD 32R CM2
03.10 (1)
00.10
RUNWAY OCCUPIED -
GO AROUND NO AP IF RH
SET CAVOK QUAL
CREW:
CM2 (2)
VISUAL CIRCUIT
03.20 LANDING
00.10 POS INIT: HOLDING POINT (or TO POS ) RWY 36L - ENGINES RUNNING
ATC CLEARANCE: SID PINAR CLIMB INITIALLY 7000FT
TAKE OFF: ENGINE FIRE BEFORE V1 - REJECTED TAKE OFF CM1
ATA 70 ENGINE UNEXTINGUISHABLE FIRE ARM AT 110ktS
03.30 EMERGENCY EVACUATION
00.15
CM1 OR
EXTRA TIME AVAILABLE FOR ADDITIONAL EXERCISES
CM2
03.45
(1)(2) See notes on first page
Establish the aircraft in a visual circuit, flying downwind, abeam the runway 32R in CONF 1 /
with all systems in normal configuration to commence the standard visual circuit. Perform a
visual pattern and configure the aircraft following the Standard Operating Procedure (SOP).
Set the aircraft in Alternate Law (ATA 27 DEMONSTRATION OF ALTERNATE LAW) When
commencing the base turn, request the trainee to reduce thrust to idle, maintain the circuit CM2
altitude and continue the approach visually.
As soon as any stall indications are recognized (e.g. aural warning, buffet, etc.) the trainee
must apply the actions as stated in FCOM / QRH.
After recovery from the stall, stop the exercise.
Continue to configure the aircraft.
04.00
PERSONAL COMPETENCES S US
Cooperation
Leadership and managerial skills
Situation awareness
Decision-making
NOTE: NO BRIEFING REQUIRED FOR THE LOFT MALFUNCTIONS.
S: Satisfactory SB: Satisfactory after Briefing US: UnSatisfactory
REMARKS:
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
……………………………………………………………………………………………………………………………………
CHECKING SESSION A
PILOT’S NAME: DATE:
CAPT. ☐ FO. ☐ SIM TYPE AND PLACE:
BRIEFING ROOM
Review Technical: Use of radar / Crosswind conditions
Review CRM: Communication
00.05 POS INIT: HOLDING POINT (or TO POS ) RWY 36L - ENGINES RUNNING
WX INIT: 050/15KT 3000 OVC005 25/18 1019 / RWY DRY
ACFT INIT : ZFW :170T FUEL:60T ZFWCG:30.0
CONF 2 // FLEX 52// V1 = 146// VR=156// V2=161
ACFT INIT : ZFW :220T FUEL:20T ZFWCG:29.0
CONF 2 // FLEX 72// V1 = 130// VR=139// V2=149
01.15 ATC CLEARANCE:SAU1P CLIMB INITIALLY 4000FT
00.25 TAKE-OFF ENGINE FAILURE BETWEEN V1 AND V2
ATA 70 ENGINE FLAME OUT WITH DAMAGE if STD
Crew:
RADAR VECTORS CM1
ASK CREW TO DISENGAGE AP 1+2 (FD AVAILABLE) ON INTCP HDG (1)
ILS APPROACH LEMD 32R ONE ENGINE OUT NO AP
-
SET OVC 000
GO AROUND ONE ENGINE OUT NO AP
if NON
AP 1+2 AVAILABLE AFTER CLEAN UP
STD
RADAR VECTORS Crew:
FOR THE NON PRECISION APPROACH SET CONDITIONS OVC AT MDA+100' CM1
NON PRECISION APPROACH VOR LEMD 32R ONE ENGINE OUT or
01.40 LANDING ONE ENGINE OUT CM2
00.05 IF NON STANDARD CREW (2)
POS INIT: HOLDING POINT (or TO POS ) RWY 36L - ENGINES RUNNING
ATC CLEARANCE: SAU1P CLIMB INITIALY 7000FT
TAKE OFF
ENGINE FAILURE BEFORE V1
ATA 70: ENGINE FLAME NO DAMAGE ARM AT 100 kts
01.45 REJECTED TAKE OFF
(1)(2) See notes on first page.
RETURN TO LEMD
ADHERENCE TO ARRIVAL ROUTES AND ATC INSTRUCTIONS:
CONTACT AQUITAINE APP
IN CONTACT WITH APP
ENTER RUDBI HOLDING (OPTIONAL) RWY 32R IN USE CONTINUE DESCENT TO
5000FT QNH...
SET WIND 340/15 G25KT
ILS APPROACH LEMD 32R + CIRCLING 14L
WHEN READY FOR APPROACH
CLEARED FOR ... APPROACH RWY ... REPORT ESTABLISHED ON ...
ESTABLISHED ON FINAL
CONTACT TOWER ON ...
WITH TOWER
02.30 WIND .../ ... RWY ... CLEAR TO LAND
(1)(2) See notes on first page.
RADAR VECTORS -
ASK CREW TO DISENGAGE AP 1+2 (FD AVAILABLE) ON INTCP HDG
ILS APPROACH LEMD 32R ONE ENGINE OUT NO AP if NON
STD
SET OVC 000 Crew:
GO AROUND ONE ENGINE OUT NO AP CM1
AP 1 + 2 AVAILABLE AFTER CLEAN UP or
CM2
RADAR VECTORS (2)
FOR THE NON-PRECISION APPROACH SET CONDITIONS OVC AT MDA+100'
NON PRECISION APPROACH LOC LEMD 32R ONE ENGINE OUT
TAKE OFF:
ENGINE FAILURE BEFORE V1
IF NON STANDARD CREW DO LVO PART EXCEPT EMERGENCY EVACUATION (SET ENGINE EXTINGUISHABLE FIRE AT 110
kts FOR REJECTED TAKE OFF) THEN SWAP SEATS AND DO ALL LVO EXERCISES AS DESCRIBED BELOW
00.05 POS INIT: HOLDING POINT (or TO POS ) RWY 18R - ENGINES RUNNING
WX INIT: 200/5KT 300 OVC001 05/03 1013 / RWY WET
ACFT INIT : ZFW:170T FUEL:60T ZFWCG:30.0
CONF2 // FLEX 51 // V1 = 146 // VR=156 // V2=161
ACFT INIT : ZFW:220T FUEL:20T ZFWCG:29.0
CONF2 // FLEX 72 // V1 = 130 // VR=139 // V2=149 if STD
03.05 ATC CLEARANCE: SID RWY HDG CLIMB INITIALLY 7000FT Crew:
00.25 CM1
TAKE OFF:
(1)
LOW VISIBILITY OPERATION
GO AROUND if NON
ATA 27 : PRIM 3 FAULT STD
RADAR VECTORS / SET WEATHER = MINIMA Crew:
ILS APPROACH LEMD 32R CAT II/III CM1
03.30 LANDING or
00.05 CM2
(2)
POS INIT: HOLDING POINT (or TO POS ) RWY 18R - ENGINES RUNNING
ATC CLEARANCE: SID RWY HDG CLIMB INITIALY 7000FT
EMERGENCY EVACUATION
03.35
REMARKS:
………………………………………………………………………………………………………………………………….
………………………………………………………………………………………………………………………………….
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………
…………………………………………………………………………………………………………………………………