FORM NO ENG / TS / A320 /001
ISSUE
PAGE : 1/9
: 04 JUN/2013
REVISION : 17
A320 MAINTENANCE LINE CHECK LIST
TRANSIT CHECK
NOTE
1)
Check to be accomplished before EACH FLIGHT at
all TRANSIT STOPS.
2) The performance of following maintenance line
checks does not prevent the accomplishment of
flight crew checks and tests as recommended by
the airline approved FLIGHT CREW OPERATING
MANUAL (FCOM).
STATION
P AGE EFFE C T IVITY
DATE
Page No Revision
A/C REGISTRATION
FLIGHT NO:
ARR
:.........................
DEP
:.........................
01
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04
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06
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17
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17
Issue
04/ JUN2013
04/ JUN2013
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A320- Maintenance Line Check Lists
FORM NO ; ENG / TS/ A320 / 001
REV :17
TRANSIT CHECK
FIG
ITEM
A/C REG :
ISSUE: 04 JUN 2013
DATE :
PAGE: 2 /9
DESCRIPTION
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A320- Maintenance Line Check Lists
FORM NO ; ENG / TS/ A320 / 001
REV :17
TRANSIT CHECK
FIG
A/C REG :
ISSUE: 04
DATE :
PAGE: 3/9
ITEM
1.0
JUN2013
DESCRIPTION
ARRIVAL PRELIMINARY ITEMS
1.1
Check ramp area is clear of debris
1.2
Install wheel chocks
1.3
Install nose and main landing gear safety pins if work requirements
require the use of safety pins or aircraft towing is expected
1.4
Place the towing lever in the “Tow position” and install pin for push
1.5
If the aircraft electrical network is not energized perform a safety
check to ensure proper position of controls and switches before
energizing the electrical network
1.6
Energize the aircraft electrical network
1.7
a) Review technical log book and undertake corrective actions as
required.
b) Review Deferred Defect recording and Cabin Log and action
accordingly.
c) If transit time is greater than six (06) hours,
review deferred defects record sheet log and raise continuation
work sheet for all open defects and action accordingly.
3
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A320- Maintenance Line Check Lists
FORM NO ; ENG / TS/ A320 / 001
REV :17
TRANSIT CHECK
FIG
ITEM
1.8
A/C REG :
ISSUE: 04
DATE :
PAGE: 4/9
JUN2013
DESCRIPTION
Check Engine oil quantity (ECAM LOWER DISPLAY ENGINE
PAGE) within 30 minutes after Engine shut-down:
If indication is below minimum check Engine
oil level at tank sight-glass ,top-up as required NO. 1 ENGINE
with OIL and record uplift(s) in journey log
book as well.
NO. 2 ENGINE
“ WARNING” Do not remove the oil tank cap for five minutes after
Engine stops to permit the pressure in the oil tank to decrease.
NOTE: If the access panel is opened for oil filing. Check Pop out
Indicates of Electric Master Chip Detector (ABK/ABM/ABN/ABO
ABP/ only)
(a) Select Hydraulic page on lower ECAM and check that
green/blue/yellow hydraulic system quantity levels are in normal
operating range, and that “Reservoir low air press” messages are
not displayed.
1.9
NOTE: If under MEL, the APU is to be used for the duration of the
following flight.
Check APU OIL LEVEL at sight glass. Service as required.
Note amount of oil uplifted in the journey log book
1.10
Print post flight and attach to main base copy of journey log
(CMB only)
1.11
If the aircraft layover is more than 4 hours depressurize the potable
water system i.a.w. AMM
1.12
Review ECAM Class 1 Warning/caution and action accordingly
1.13
If transit time is greater than six (06) hours
(a)Pull all bellow mentioned circuit breakers
PANEL 49VU FIN 3DA1 LOCATION D02
PANEL 122VU FIN 3DA2 LOCATION Y14
PANEL 122VU FIN 3DA3 LOCATION Z16
PANEL 122VU FIN 5DA1 LOCATION Z13
PANEL 122VU FIN 5DA2 LOCATION Y11
PANEL 122VU FIN 5DA3 LOCATION Z14
(b) Install Pitot Covers and Static blanks
(c) Install glare shield panel insulation blanket
(d) Install O/W Exit Warning Placards
(e) Install the Ram Air Turbine Safety Device
(Refer MM Task 29-22-00-491-001)
(f) Install Main Landing gear pins
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A320- Maintenance Line Check Lists
FORM NO ; ENG / TS/ A320 / 001
REV : 17
TRANSIT CHECK
FIG
3,11,16
A/C REG :
ISSUE: 04
DATE :
PAGE: 5/9
ITEM
JUN 2013
DESCRIPTION
1.14
Check and record seal serial no. of the CD pouch, located in the
cockpit coat stowage
S/No……………
1.15
Intentionally left blank
1.16
NOTE: TO BE ACCOMPLISHED PRIOR TO THE FIRST FLIGHT OF
THE DAY-FROM MAIN BASE
On panel 25VU, section EXT LT, perform operational test on
Navigation Lights, Landing Lights, Runway Turnoff Lights, Taxi and
Take-Off Lights, Logo Lights, Anti-collision/Strobe Lights, Wing and
Engine Scan Lights
1.17
Intentionally left blank
1.18
Follow cold weather maintenance procedures as per AMM 12-31-00
PB 001 if:
Outside air temperature (OAT) is less than 0 deg.C and aircraft is not
electrically powered.
2.0
EXTERNAL CHECKS
2.1
Carry out an aircraft walk around for evidence of obvious damages
which may have occurred during the last flight or during the landing
and taxi phases:
(a) Impact/F.O.D.
(b) Fluid leakage
(c) Missing or loose parts
(d) Missing overpressure discharge discs
(e) Fuselage tail skin for damage of ground contact during take off
(f) Obstruction of inlet/outlets
2.2
Check brake units for evidence of overheating or leaks on MLG and
NLG shock absorber for normal extension, wheels for condition, tires
for wear, damage and evidence of under-inflation
2.3
Intentionally left blank
2.4
Check the integrity of the FSK seal
TECH
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A320- Maintenance Line Check Lists
FORM NO ; ENG / TS/ A320 / 001
REV :17
TRANSIT CHECK
FIG
7,8,11
16,19,
20
1,4
A/C REG :
ISSUE: 04
DATE :
PAGE: 6/9
ITEM
JUN 2013
DESCRIPTION
2.5
Intentionally left blank
2.6
Before starting engine, ensure all plug and cover assemblies are
removed and check engine intake/pylon exhaust areas for signs of
damage or leaks and cowlings for security
2.7
Static ports, all probes and sensors: Ensure covers/blanks are
removed prior to flight departure
2.8
Close all bellow mentioned circuit breakers
PANEL 49VU FIN 3DA1 LOCATION D02
PANEL 122VU FIN 3DA2 LOCATION Y14
PANEL 122VU FIN 3DA3 LOCATION Z16
PANEL 122VU FIN 5DA1 LOCATION Z13
PANEL 122VU FIN 5DA2 LOCATION Y11
PANEL 122VU FIN 5DA3 LOCATION Z14
3.0
REFUELING
3.1
Obtain water free fuel samples form bowser or “Refueling trucks” prior
to refueling
3.2
Refuel aircraft up to required dispatch quantity and record
uplift/content in journey log book
3.3
Ensure refuel coupling caps are in place secured
3.4
Ensure fuel magnetic level indicators are retracted and secured
4.0
WATER/WATER SERVICING
4.1
Ensure servicing of potable water system is carried out and water
servicing access door is closed and secured
4.2
Service toilets as required
TECH
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A320- Maintenance Line Check Lists
FORM NO ; ENG / TS/ A320 / 001
REV : 17
TRANSIT CHECK
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DATE :
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ITEM
DESCRIPTION
4.3
(APPILICABLE FOR EVERY TRANSIT THROUGH BASE STATION)
(a) Drain the waste tanks in order to ensure that the tanks are empty,
the outside of the waste drain hose shall be touched by hand to
verify that the fluid flow has stopped before beginning tank
rinsing process
(b) After draining wit the waste drain valves in the open position the
waste tank rinsing system shall be connected to the toilet service
vehicle, having the following requirements.
(c) Pressure 2.4 bars (35-50 psi) Flow rate: Stable at 38.0 L (10.04
Usg) per minutes Volume to be delivered. Approx 20L (5.3 Usg)
close the drain valve after rinsing and add 01 sachet (each 8
grams) of deodorant Celeste Sani-Pack AMS 1476 into each
toilet bowl flush once before departure to deodorize the system
(AMM 12-16-38)
5.0
OXYGEN
5.1
Check crew oxygen bottle pressure in “DOOR/OXY” page as follows:
Line Station : Between 900-1850 PSI (70ºF)
CMB
: Between 1200-1850 PSI (70ºF)
NOTE
: Above pressure applicable for Transit check only
5.2
Ensure the “REGUL LOPR” message is not displayed on the
“DOOR/OXY” page
6.0
INTERIOR CLEANING
6.1
Ensure all smoke detector inlet ducts are free from any blockage
6.2
Ensure general cleaning in flight and passenger compartments,
service centers and lavatories are carried out
6.3
Intentionally left blank
JUN 2013
TECH
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A320- Maintenance Line Check Lists
FORM NO ; ENG / TS/ A320 / 001
REV :17
TRANSIT CHECK
FIG
3,11
16
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ISSUE: 04
DATE :
PAGE: 8/9
ITEM
JUN 2013
DESCRIPTION
7.0
FINAL ITEMS
7.1
Endorse and sign off corrective actions in Technical log book
7.2
(a) Remove main landing gear safety pins (if installed)
(b) Remove Rat Safety Service
7.3
Ensure aircraft is released by an authorized individual and the
applicable maintenance duly certified in the Technical log book
7.4
Carry out a final aircraft walk around:
(a) Ensure all cabin doors, cargo compartment doors and service
Panels are properly closed and secured
(b) Ensure no damage has been caused by ground equipment for
During or baggage loading
ALL
7.5
Intentionally left blank
7.6
Normalize the cold weather preventive procedures as per
AMM 12-31-00 PB 001 if cold weather procedures were done
8.0
DEPARTURE PROCEDURE
8.1
If insect presence is evident in the vicinity of the aircraft, within 15
minutes prior to departure visually inspect Pitot probes and Static
ports to detect any blockage as far as visible
Ten minutes prior to departure, the Departure Engineer will establish
intercom contact with flight deck and maintain contact until departure
clearance is given
8.2
8.3
If push back or towing departure required:
(a) Ensure ground towing control is set to the “TOWING”
position on the nose steering deactivation box and lock the lever
with safety pin
(b) Connect bar to the NLG towing attachment
NOTE: ENSURE TOWING ANGLE IS NOT EXCEEDED DURING
TOWING/ PUSHBACK
8.4
If APU is fully operative, remove GPU/Air-con unit/Air Start unit
TECH
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A320- Maintenance Line Check Lists
FORM NO ; ENG / TS/ A320 / 001
REV :17
TRANSIT CHECK
FIG
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DATE :
PAGE: 9/9
ITEM
TECH
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DESCRIPTION
8.5
Ensure all ground equipment removed and is clear of aircraft except
GPU, ACU, ASU as required
8.6
Inform flight crew that aircraft is clear to start engines
8.7
After engine start, remove all ground equipment as soon as flight
crew acknowledge that it is no longer required
8.8
When Cockpit crew request pushback
(a) Remove wheel chocks
(b) Request cockpit crew to release parking brake and await
confirmation that brakes are OFF from captain
(c) Signal tractor driver to commence pushback/towing indication
direction of turn if required
On completion of pushback, request cockpit crew to set parking
brakes and await confirmation that brakes are ‘ON’
8.9
8.10
Position wheel chock at nose wheels and remove towbar, form the
nose landing gear towing attachment, and move the tractor away.
8.11
Before aircraft taxi out for departure:
(a) Remove nose landing gear safety pin
(b) Remove safety pin of the nose wheel steering deactivation box
and make sure the towing control lever return to the normal
position
Remove Nose Wheel chocks and move to the left or right hand
wingtip and indicate aircraft is clear to taxi
8.12
JUN 2013
LAE
SIG
THE PERSON/S SIGNING IN LAE’S SIG. COLUMN CERTIFIES AS FOLLOWS
CAASL
I HEREBY CERTIFY THAT THE INSPECTION/ OVERHAUL / REPAIR / REPLACEMENT / MODIFICATION
SPECIFIED ABOVE HAVE BEEN CARRIED OUT IN ACCORDANCE WITH THE REQUIREMENT OF THE SRI
LANKA AIR NAVIGATION REGULATIONS.
DATE COMPLETED : ..................................
LAE SIGNATURE : .................................
TIME COMPLETED : ..................................
LIC / APP NO
: .................................