CH10 A320 Ice and Rain Protection Flashcards
ICE_001
Recall which areas of the wings and engines are provided ice protection.
Wings?
________ ___ slats (Slats _, _, and _).
ICE_001
Recall which areas of the wings and engines are provided ice protection.
Wings?
OUTBOARD three slats (Slats 3, 4, and 5).
ICE_001
Recall which areas of the wings and engines are provided ice protection.
Engines?
Engine _____ ______edge
ICE_001
Recall which areas of the wings and engines are provided ice protection.
Engines?
Engine nacelle leading edge
ICE_004
Recall whether an engine bleed valve must be open in order to use its respective engine anti-ice system:
______
Engine anti-ice is plumbed _______ from the ____-_____ compressor therefore, the engine’s bleed valve _____ _____ have to be _____ in order to use engine anti-ice.
ICE_004
Recall whether an engine bleed valve must be open in order to use its respective engine anti-ice system:
No.
Engine anti-ice is plumbed independently from the high-pressure compressor therefore, the engine’s bleed valve does not have to be open in order to use engine anti-ice.
ICE_005
Describe the indications when engine anti-ice is selected on.
▪ ____ (_____) illuminates on the respective ___ 1(2) pb.
▪ ____ ____ and _____ (____) appears on the ______ memo section.
ICE_005
Describe the indications when engine anti-ice is selected on.
▪ ON (blue) illuminates on the respective ENG 1(2) pb.
▪ ENG A.ICE and IGNITION (green) appears on the E/WD memo section.
ICE_006
Describe the indications of wing anti-ice being selected on.
▪ ____ (_____) illuminates on the WING pb.
▪ ______ ___ (____) appears on the _____ memo section.
▪ ____-____ (______) appears on each side of the ______ page.
▪ _____ ______ appear on each side of the BLEED page when the respective _____ _____ valve is open for that wing.
ICE_006
Describe the indications of wing anti-ice being selected on.
▪ ON (blue) illuminates on the WING pb.
▪ WING A. ICE (green) appears on the E/WD memo section.
▪ ANTI ICE (white) appears on each side of the BLEED page.
▪ Green arrows appear on each side of the BLEED page when the respective wing anti-ice valve is open for that wing.
ICE_009
Recall the meaning of the FAULT (amber) light in the WING and ENG 1(2) ANTI ICE pbs.
▪ Appears ______ during valve _______.
▪ Represents _____ between the _____ position and ______respective valve’s position.
▪ The FAULT light on the WING pb also indicates ____ ____ _____ pressure is being detected
▪ Appears momentarily during valve transition.
▪ Represents disagreement between the selected position and actual respective valve’s position.
▪ The FAULT light on the WING pb also indicates low bleed air pressure is being detected
ICE_010
Recall the operation of the Probe and Window heating system with the PROBE/WINDOW HEAT pb in AUTO (light out).
▪ On the ground, with at ____ _____ ____ running:
all _____ _____ windows/windshields,
_____ probes,
______ ports, and
_______ probes are
________ heated at a _____ heat level.
▪ Once airborne, heat levels are _____, and the _____ probes are heated.
ICE_010
Recall the operation of the Probe and Window heating system with the PROBE/WINDOW HEAT pb in AUTO (light out).
▪ On the ground, with at least one engine running:
all flight deck windows/windshields,
pitot probes,
static ports, and
AOA probes are
automatically heated at a low heat level.
▪ Once airborne, heat levels are increased, and the TAT probes are heated.
ICE_011
Recall the operation of the Probe and Window heating system with the PROBE/WINDOW HEAT pb selected ON.
▪ On the ground, with engines not running:
o all _____ _____ windows/windshields,
_____ probes,
____ ports, and
_____ probes are heated at a ____ heat level.
ICE_011
Recall the operation of the Probe and Window heating system with the PROBE/WINDOW HEAT pb selected ON.
▪ On the ground, with engines not running:
o all flight deck windows/windshields,
pitot probes,
static ports, and
AOA probes are heated at a low heat level.
EXTRA LMS ICE 02
Select the correct statement.
A Engine icing conditions exist when the TAT is 40 degrees C or below, and visible moisture in any form is present (clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals).
B Engine icing conditions exist when the OAT is 15 degrees C or below, and visible moisture in any form is present (clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals).
C Engine icing conditions exist when the OAT is 10 degrees C or below, and visible moisture in any form is present (clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals).
D Engine icing conditions exist when the TAT is 10 degrees C or below, and visible moisture in any form is present (clouds, fog with visibility of two miles or less, rain, snow, sleet, and ice crystals).
EXTRA LMS ICE 02
Select the correct statement.
A Engine icing conditions exist when the TAT is 40 degrees C or below, and visible moisture in any form is present (clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals).
B Engine icing conditions exist when the OAT is 15 degrees C or below, and visible moisture in any form is present (clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals).
C Engine icing conditions exist when the OAT is 10 degrees C or below, and visible moisture in any form is present (clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals).
D Engine icing conditions exist when the TAT is 10 degrees C or below, and visible moisture in any form is present (clouds, fog with visibility of two miles or less, rain, snow, sleet, and ice crystals).
C is correct.
EXTRA LMS ICE 07
What is the maximum speed for operating the windshield wipers?
EXTRA LMS ICE 07
What is the maximum speed for operating the windshield wipers?
230 knots
