CIRCULAR OPERATIVA Nº 028 / 2009 DIRECCIÓN DE OPERACIONES / LAN ARGENTINA S.A.
DE :
COMANDANTES
PRIMEROS OFICIALES
OFICINAS
A‐320
B‐767
A‐320
B‐767
GOV
CCV
A :
XX
‐‐
XX
‐‐
XX
‐‐
Nº ÚLTIMA CIRCULAR
027/009
027/009
027/009
027/009
027/009
027/009
DIA
MES
AÑO
02
06
2009
INCLUSIÓN MOE SI
‐‐
NO
XX
REF: Revisión N° 9 al Operational Procedures Knowledge Test para la Flota A‐320 (FAM).
A.‐ Con el propósito de actualizar el OPKT, considerando nueva información de Airbus respecto de limitaciones y procedimientos de acción inmediata, se deberán considerar los siguientes aspectos que cambian en el nuevo test. 1) Se elimina la restricción adicional de un máximo de 10 kts. de viento de cola sobre 9200 ft., quedando como única restricción un máximo de 15 kts. de viento de cola tanto para el despegue como aterrizaje. Lo anterior se basa en la información contenida en los AFM (suplemento), manual que tiene preponderancia sobre los FCOM. Este último manual en lo relacionado a esta información será actualizado por Airbus a la brevedad. 2) Conforme a lo indicado en FCOM 3 (3.02.01) el procedimiento “Smoke/Fumes/Avncs Smoke” se retira de aquellos considerados como Memory Item. 3) Se incorpora como Memory Item el procedimiento Pilot Incapacitation, para lo cual y conforme a lo estandarizado en LAN, el aviso a la tripulación de cabina será “TRIPULACIÓN, ATTENTION CREW, ATTENTION CREW, JEFE(A) DE SERVICIO ABORDO AL COCKPIT” en reemplazo de lo actualmente publicado en FCOM 3 (3.02.80) ATTENTION, PURSER TO COCKPIT PLEASE. Este cambio será incorporado en la revisión N° 12 del Airline Policy. B.‐ Adjunto a esta circular encontrarán dos formatos (en blanco y con respuestas) del nuevo OPKT para la Flota A‐320 (Fam). Esta nueva revisión entra en vigencia a contar del 02 de junio y será aplicable a todos los cursos y entrenamientos de vuelo periódicos (Recurrent).
GERENCIA DE FLOTA A320. Página 1 de 1
Auto flight
on takeoff with SRS mode
Ice & Rain Protection
a
WINDSHEAR AHEAD
.
• When airborne
NOTE: Predictive wind shear alerts are inhibited above 100 knots until 50 feet.
A318/319/320 OPERATIONAL PROCEDURES KNOWLEDGE TEST (para curso y recurrent)
Maximum average estimated oil consumption
Minimum oil quantity on ground before engine start
OIL QUANTITY IAE
Rev.9 / Mayo 11 ’09
por Jefes de Flota
Apply precautionary measures as indicated in the Supp. Techniques 3.04.09
W/S AHEAD amber
to minimize the loss of heigh, increase this pitch attitude
2. If the FD is not available, use a pitch initial attitude up to 17.5°. If necessary
Note: 1. If engaged, the autopilot disengaged when α. is greater than α. Prot.
This includes de use of full backstick, if required
Minimum oil quantity on ground before engine start
Note: If a positive verification is made that not hazard exist, the warning may be Considered cautionary
-
Maximum average estimated oil consumption
.
“WINDSHEAR
%
Page 1
.
. Landing: Associated with aural synthetic voice “GO AROUND, WINDSHEAR AHEAD”
-
. take off run • During
Takeoff: Associated with aural synthetic voice AHEAD, WINDSHEAR AHEAD” • Before take off
W/S AHEAD red
-
Porcentaje:
EMERGENCY MEMORY ITEMS PART
firma inst.
OIL QUANTITY P&W
Non Precision Approaches whith engine-out If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes: _____ ____, ___ _____ , ____ __________. Only FD use is permitted.
Maximum speed at which windshield wipers may be used:
ATA - 30
All other phases
Straight-in non precision approach Minimum height Circling approach for use of ILS app. with CAT I displayed on FMA autopilot: Go-around (AP or FD engagement)
ATA - 22
Maximum tailwind for takeoff and landing
Airport Operations
I I.
Nombre y Apellido
__________
Nombre:_________________________________________________Fecha:___ / ____ / 2_____
Lugar:__________________ Instructor:_____________________________
Cpt. F.O.
(para curso y recurrent)
OPERATIONAL PROCEDURES KNOWLEDGE TEST
I. OPERATING LIMITATIONS PART
Instrucción de Vuelo
A318/319/320
.
-
.
-
.
.
-
A318/319/320 OPERATIONAL PROCEDURES KNOWLEDGE TEST (para curso y recurrent)
.
-
Resolution advisory : All “CLIMB” and “DESCEND” or “MAINTAIN VERTICAL SPEED MAINTAIN” or “ADJUST VERTICAL SPEED ADJUST” or “MONITOR VERTICAL SPEED” type messages
.
-
TCAS WARNINGS
. .
-
• Above THRUST RED ALT & Above FL 100………………..
• Above THRUST RED ALT & Below FL 100 ………………..
. -PITCH/THRUST : • Below THRUST RED ALT……………………………………..
-
MEMORY ITEMS :
.
-
UNRELIABLE SPEED INDIC/ADR CHECK PROC
.
-
Pull up to full backstick and maintain
.
Simultaneously : -
“PULL UP” - “TERRAIN TERRAIN PULL UP” - “TERRAIN AHEAD PULL UP” - “OBSTACLE AHEAD PULL UP”
EGPWS ALERTS
-
-
-
EMER DESCENT
Rev.9 / Mayo 11 ’09
por Jefes de Flota
Descend with the autopilot engaged: • Turn the ALT selector knob and pull. • Turn the HDG selector knob and pull. • Adjust the target SPD/MACH. Use of the autopilot is also permitted in EXPEDITE mode
IMMEDIATE ACTIONS
-
• IF STILL NO BRAKING:
-
Page 2
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. .
.
.
.
.
.
-
.
.
.
.
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-
-
-
• IF NO BRAKING AVAILABLE:
-
• IF AUTOBRAKE IS SELECTED:
LOSS OF BRAKING
. . ..
-
Airborne, initial climb or landing
-
CREW INCAPACITATION
Rev.9 / Mayo 11 ’09
por Jefes de Flota
Page 3
If a cockpit crew member becomes _______________, the remaining crew member must call a cabin attendant __ ____ _ ____________. The best way to request assistance from the cabin crew, is by means of the passenger address system : “____________, ____________ _______, __________ ________ ________ __ _____________ ___________ ____ _________”. The purser or any other cabin attendant must proceed to the cockpit immediately. The cabin attendant must then: - tighten and manually lock the shoulder hardness of the incapacitated crew member ; - push the seat completely aft ; - recline the seat back It take two people to remove the dead weight of an unconscious body from a seat without endangering any controls and switches. If it is not possible to remove the body, one cabin attendant must remain in the cockpit to take care of and observe the incapacited crew member. In coordination with the purser : - request assistance from any medically ________ __________ - check if a type qualified ___________ _______ is on board to replace the incapacitated crew member.
A318/319/320 OPERATIONAL PROCEDURES KNOWLEDGE TEST (para curso y recurrent)
- RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF SHEAR
- CLOSELY MONITOR FLIGHT PATH AND SPEED
- DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF SHEAR
to minimize the loss of heigh, increase this pitch attitude
2. If the FD is not available, use a pitch initial attitude up to 17.5°. If necessary
Note: 1. If engaged, the autopilot disengaged when α. is greater than α. Prot.
This includes de use of full backstick, if required
. . -_______________________________________________.
.
-
At take off: • If before V1 The takeoff should be rejected only if significant airspeed variations occur below indicated V1 and the pilot decides that there is sufficient runway remaining to stop the airplane. • If after V1
WINDSHEAR
Ice & Rain Protection 230 KTS
500 ft AGL
11 qt + estimated consumption 0.3 qt/h
8.7 qt + estimated consumption 0.4 qt/h
A318/319/320 OPERATIONAL PROCEDURES KNOWLEDGE TEST (para curso y recurrent)
Maximum average estimated oil consumption
Minimum oil quantity on ground before engine start
OIL QUANTITY IAE
Maximum average estimated oil consumption
Minimum oil quantity on ground before engine start
OIL QUANTITY P&W
Non Precision Approaches whith engine-out If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes: _____Final APP____, ____NAV V/S____, ____NAV/ FPA____. Only FD use is permitted.
Maximum speed at which windshield wipers may be used:
ATA - 30
All other phases
MDA or MDH MDA - 100 ft or MDH - 100 ft 160 ft AGL
Straight-in non precision approach Minimum height Circling approach for use of ILS app. with CAT I displayed on FMA autopilot: Go-around (AP or FD engagement)
100 ft AGL
100 ft AGL
Auto flight
15 KTS
on takeoff with SRS mode
ATA - 22
Maximum tailwind for takeoff and landing
Airport Operations
firma inst.
a
Porcentaje:
“WINDSHEAR
%
Rev.9 / Mayo 18 ’09
por Jefes de Flota
Apply precautionary measures as indicated in the Supp. Techniques 3.04.09
W/S AHEAD amber
to minimize the loss of heigh, increase this pitch attitude
2. If the FD is not available, use a pitch initial attitude up to 17.5°. If necessary
Note: 1. If engaged, the autopilot disengaged when α. is greater than α. Prot.
This includes de use of full backstick, if required
Page 1
- GO-AROUND………………………………………PERFORM
Note: If a positive verification is made that not hazard exist, the warning may be Considered cautionary
- THR LEVERS.….….………….……...………….………TOGA . - SRS ORDERS…...………………….……...………..FOLLOW . Landing: Associated with aural synthetic voice “GO AROUND, WINDSHEAR AHEAD”
• When airborne
NOTE: Predictive wind shear alerts are inhibited above 100 knots until 50 feet.
- Reject takeoff
- Delay takeoff, or select the most favorable runway . take off run • During
Takeoff: Associated with aural synthetic voice AHEAD, WINDSHEAR AHEAD” • Before take off
WINDSHEAR AHEAD
EMERGENCY MEMORY ITEMS PART
W/S AHEAD red
I I.
Nombre y Apellido
__________
Nombre:_______________________________________________ Fecha:____ / ____ / 2_____
Lugar:__________________ Instructor:_____________________________
Cpt. F.O.
(para curso y recurrent)
OPERATIONAL PROCEDURES KNOWLEDGE TEST
I. OPERATING LIMITATIONS PART
Instrucción de Vuelo
A318/319/320
A318/319/320 OPERATIONAL PROCEDURES KNOWLEDGE TEST (para curso y recurrent)
- BOTH FDs….………………....……….…………………...OFF
- AP (if engaged)..................………..….…….……….......OFF
Resolution advisory : All “CLIMB” and “DESCEND” or “MAINTAIN VERTICAL SPEED MAINTAIN” or “ADJUST VERTICAL SPEED ADJUST” or “MONITOR VERTICAL SPEED” type messages
TCAS WARNINGS
- L/G………...……….…………..…………..…..……….…….UP
- FLAPS .……………...…......MAINTAIN CURRENT CONFIG - SPEEDBRAKES.....………............…CHECK RETRACTED
• Above THRUST RED ALT & Above FL 100……….5°/CLB
• Above THRUST RED ALT & Below FL 100………10°/CLB
- A/THR .…………….…………..……………..……………. OFF -PITCH/THRUST : • Below THRUST RED ALT……………………......15°/TOGA
- AP/FD …………….………..….………...….…...………... OFF
MEMORY ITEMS :
UNRELIABLE SPEED INDIC/ADR CHECK PROC
Rev.9 / Mayo 18 ’09
por Jefes de Flota
Page 2
- SIGNS………………………………………………………...ON - THR LEVERS (if A/THR not engaged).….....…….......IDLE - SPD BRK.….…………………………...………………...FULL.
Descend with the autopilot engaged: • Turn the ALT selector knob and pull. • Turn the HDG selector knob and pull. • Adjust the target SPD/MACH. Use of the autopilot is also permitted in EXPEDITE mode
- CREW OXY MASKS.….…………………………………...ON
IMMEDIATE ACTIONS
EMER DESCENT
APLICATIONS
- PARKING BRAKE.……………..SHORT AND SUCCESIVE
• IF STILL NO BRAKING:
- MAX BRK PR.……………..…...........………………1000 PSI
- BRAKE PEDALS.…………….…….…………..……...PRESS
- SPEEDBRAKE lever…..……............CHECK RETRACTED
- BANK.…………………..……....WINGS LEVEL or ADJUST
- A/SKID & N/W STRG.………..……..…………..………...OFF
- BRAKE PEDALS..………….……...…………..…..RELEASE
- REV.…………………..…..….…………………..….……..MAX
• IF NO BRAKING AVAILABLE:
- BRAKE PEDALS..……….……………….……..……..PRESS
• IF AUTOBRAKE IS SELECTED:
LOSS OF BRAKING
- THRUST LEVERS…….…….....…...….……………….TOGA
Pull up to full backstick and maintain
- PITCH…………………...….…….…..……………….PULL UP
Simultaneously : - AP….……….….………………...………….…………..…..OFF
“PULL UP” - “TERRAIN TERRAIN PULL UP” - “TERRAIN AHEAD PULL UP” - “OBSTACLE AHEAD PULL UP”
EGPWS ALERTS
CREW INCAPACITATION
Rev.9 / Mayo 18 ’09
por Jefes de Flota
Page 3
If a cockpit crew member becomes incapacitated, the remaining crew member must call a cabin attendant as soon as practicable. The best way to request assistance from the cabin crew, is by means of the passenger address system : “TRIPULACIÓN, ATTENTION CREW, ATTENTION CREW, JEFE (A) DE SERVICIO ABORDO AL COCKPIT”. The purser or any other cabin attendant must proceed to the cockpit immediately. The cabin attendant must then: - tighten and manually lock the shoulder hardness of the incapacitated crew member ; - push the seat completely aft ; - recline the seat back It take two people to remove the dead weight of an unconscious body from a seat without endangering any controls and switches. If it is not possible to remove the body, one cabin attendant must remain in the cockpit to take care of and observe the incapacited crew member. In coordination with the purser : - request assistance from any medically qualified passanger - check if a type qualified company pilot is on board to replace the incapacitated crew member.
A318/319/320 OPERATIONAL PROCEDURES KNOWLEDGE TEST (para curso y recurrent)
.
- RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF SHEAR
- CLOSELY MONITOR FLIGHT PATH AND SPEED
- DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF SHEAR
to minimize the loss of heigh, increase this pitch attitude
2. If the FD is not available, use a pitch initial attitude up to 17.5°. If necessary
Note: 1. If engaged, the autopilot disengaged when α. is greater than α. Prot.
This includes de use of full backstick, if required
- THR LEVERS AT TOGA……………..…SET OR CONFIRM . - AP (if engage)…………………………………………....KEEP . - SRS ORDERS………………………………………..FOLLOW
- SRS ORDERS...………………………..…….….…..FOLLOW Airborne, initial climb or landing
- REACHING VR..………….…...………..……..….….ROTATE
- THR LEVERS..……..……….………….………………..TOGA
At take off: • If before V1 The takeoff should be rejected only if significant airspeed variations occur below indicated V1 and the pilot decides that there is sufficient runway remaining to stop the airplane. • If after V1
WINDSHEAR
