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UF94200
EFFECTIVITY Page 27
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COCKPIT SLIDING WINDOWS DESCRIPTION/OPERATION
WINDOWS
One side window is provided on each side of the cockpit
beside the seats.
The cockpit sliding windows can only be operated from
the inside.
To open a window, push down the red indicator on top
of the opening handle.
Prior to closing, unlock the window by pulling the
locking pin.
TMUESFO01-T01 LEVEL 3
EFFECTIVITY 25-61-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 28
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COCKPIT SLIDING WINDOWS DESCRIPTION/OPERATION - WINDOWS
TMUESFO01-P01 LEVEL 3
EFFECTIVITY 25-61-00 Page 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
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TMUESFO01 LEVEL 3
EFFECTIVITY 25-61-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
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25 - EQUIPMENT/FURNISHINGS
25-61-00 COCKPIT ESCAPE ROPE
DESCRIPTION/OPERATION
CONTENTS:
Ropes
TMUESFP01 LEVEL 3
EFFECTIVITY 25-61-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
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COCKPIT ESCAPE ROPE DESCRIPTION/OPERATION
ROPES
Two ropes enable cockpit crew evacuation through the
sliding windows.
Two escape ropes are provided in stowage boxes located
over the sliding windows.
Pull the cover off the stowage box, grasp the handle
and throw it out.
Each rope can be used through either sliding window
in any normal or abnormal aircraft configuration.
TMUESFP01-T01 LEVEL 3
EFFECTIVITY 25-61-00 Page 2
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MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 32
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COCKPIT ESCAPE ROPE DESCRIPTION/OPERATION - ROPES
TMUESFP01-P01 LEVEL 3
EFFECTIVITY 25-61-00 Page 3
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUESFP01 LEVEL 3
EFFECTIVITY 25-61-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 34
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25 - EQUIPMENT/FURNISHINGS
25-11-00 COCKPIT COMPONENTS
CONTENTS:
Captain and First Officer Seats
Pilot Seat Harness
Sidestick Armrest
Third Occupant Seat
Fourth Occupant Seat
TMUESGA07 LEVEL 3
EFFECTIVITY 25-11-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 35
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COCKPIT COMPONENTS
CAPTAIN AND FIRST OFFICER SEATS
IDENTIFICATION
FIN: 3MS(CAPTAIN), 4MS(F/O)
LOCATION
ZONE: 211, 212
COMPONENT DESCRITION
All the manual controls must be operative for each
pilot.
Electrical controls are optionally installed and may
be inoperative.
PILOT SEAT HARNESS
IDENTIFICATION
FIN: 3MS(CAPTAIN), 4MS(F/O)
LOCATION
ZONE: 211, 212
COMPONENT DESCRITION
The aircraft may not leave an airport where repair or
replacements can be made.
SIDESTICK ARMREST
IDENTIFICATION
FIN: 3MS(CAPTAIN), 4MS(F/O)
LOCATION
ZONE: 211, 212
COMPONENT DESCRITION
The manual controls may be inoperative provided setting
is suitable for proper operation.
TMUESGA07-T01 LEVEL 3
EFFECTIVITY 25-11-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 36
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COCKPIT COMPONENTS-CAPTAIN AND FIRST OFFICER SEATS-PILOT SEAT HARNESS-SIDESTICK ARMREST
TMUESGA07-P01 LEVEL 3
EFFECTIVITY 25-11-00 Page 3
Oct 31/96
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MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 37
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THIRD OCCUPANT SEAT
IDENTIFICATION
FIN: 14MM
LOCATION
ZONE: 212
FOURTH OCCUPANT SEAT
IDENTIFICATION
FIN: 13MM
　
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