7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
1/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:1 of 19
FORM NO.IGO/E&M/A320/LO/41A
A/C REG. ______________ DATE: ______________ STATION: ________________
WORK ORDER NO.______________ STAMP (PLANNING DEPT.) _____________
CHECKED BY:
DIVISION NAME DATE SIGNATURE
TECH RECORDS
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
2/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:2 of 19
FORM NO.IGO/E&M/A320/LO/41A
INSTRUCTIONS TO THE CERTIFYING STAFF
1.
ENSURE THAT YOU HAVE REQUIRED TOOLS, EQUIPMENT, SPARES AND TECHNICAL LITERATURE PRIOR TO COMMENCEMENT OF
MAINTENANCE TASK.
2. ALL WARNINGS, CAUTIONS DETAILED IN THE REFERENCE TECHNICAL LITERATURE SHALL BE ADHERED TO WHILE PERFORMING
THE RESPECTIVE MAINTENANCE TASK.
3. CARRY OUT FUNCTIONAL TEST OF ALL SYSTEMS THAT WERE DISTURBED DURING THE COURSE OF INSPECTION AND MAINTAIN
RECORDS.
4. RAISE A MAINTENANCE WORK ORDER FOR ANY ABNORMAL FINDINGS OBSERVED WHILE PERFORMING THE INSPECTION
SCHEDULE.
5. WHENEVER AN AREA IS OPENED, INSPECT THE ADJACENT STRUCTURE/COMPONENT ALSO, AND RECORD ABNORMALITY IF
NOTICED, IN A SEPARATE MAINTENANCE WORK ORDER.
6. INSPECTION DATA SHOULD BE RECORDED BY CERTIFYING STAFF AS PER TASK CARD/ WORK ORDER DETAILS (IF APPLICABLE).
7. WHENEVER VALUES ARE TO BE CHECKED THE SAME ARE TO BE RECORDED AGAINST THE CORRESPONDING INSPECTION ITEM.
8. CERTIFY EACH MAINTENANCE STEP IN THE SCHEDULE/WORK ORDER AFTER ITS COMPLETION WITH TIME AND DATE.
9.
WHILE CARRYING OUT THE INSPECTION IN OPEN AIR ENSURE THE WEATHER AND ENVIRONMENT IS CONDUCIVE TO CARRY OUTTHE INSPECTION PROPERLY.
10.ALWAYS USE CALIBRATED MEASURING INSTRUMENTS/EQUIPMENTS.
11.ENSURE THAT THE COMPONENT HAS APPROPRIATE SERVICEABLE TAG BEFORE INSTALLING ON THE AIRCRAFT.
12.REVIEW THE AIRCRAFT TECH LOG / CABIN DEFECT LOG FOR ANY PILOT / CABIN CREW DEFECT REPORTS. TAKE APPROPRIATE
RECTIFICATION ACTIONS.
13.REFER ADD/CDD PAGES OF TECH LOG FOR ANY DEFFERED DEFECT AND TAKE APPROPRIATE ACTION.
14.THE TERM INSPECTION/CHECK WHEREVER USED IN THIS SCHEDULE MEANS THAT THE ITEM HAS TO BE CHECKED FOR
SECURITY, CLEANLINESS, CORROSION, DETERIORATION, WEAR, CRACKS, DENTS, SCORES, CUTS, DISTORTION VISUAL EVIDENCE
OF BOWING, OVERHEATING, FREEDOM FROM OBSTRUCTION, LEAKS, LOCKING AND ANY OTHER DAMAGE.
15.THE CMR TASKS ARE MARKED AS (CMR).
16.THE ALS TASKS ARE MARKED AS (ALI).
17.THE CERTIFYING STAFF SIGNING THE CRS SHOULD ENSURE THAT ALL THE TASKS IN THE SCHEDULE ARE SIGNED OFF AND SHOULD
SIGN AND STAMP ON THE COLUMN PROVIDED AT THE BOTTOM OF EACH PAGE OF THE SCHEDULE.
DEFINITIONS:1. AIRWORTHINESS LIMITATION SECTION (ALS): ALS IS THE REPOSITORY FOR STAND-ALONE DOCUMENTS THAT CONSTITUTES
INSTRUCTIONS FOR CONTINUOUS AIRWORTHINESS. THE TASKS FROM ALS ARE INCLUDED IN THE MAINTENANCE PROGRAM AS
AIRWORTHINESS LIMITATION ITEM (ALI). IT COMPRISES OF DAMAGE TOLERANT AIRWORTHINESS LIMITATION ITEMS (DT ALI),
CERTIFICATION MAINTENANCE REQUIREMENTS (CMR) TASK ARISING FROM SYSTEM SAFETY ASSESSMENT WHICH ARE
ASSOCIATED WITH MOST SIGNIFICANT FAILURE CONDITIONS, AGEING SYSTEMS MAINTENANCE (ASM) & FUEL AIRWORTHINESS
LIMITATIONS (FAL).
2. EXTENDED DIVERSION TIME OPERATIONS (EDTO): THE EXTENDED DIVERSION TIME OPERATIONS (EDTO) IS AN OPERATION BY
AN AIRPLANE WITH TWO OR MORE TURBINE ENGINES WHERE THE DIVERSION TIME TO AN EN-ROUTE ALTERNATE AERODROME
IS GREATER THAN 60 MINUTES.
3. ELECTRICAL WIRING INTERCONNECTION SYSTEM (EWIS): EWIS RELATED TASKS COMPRISE OF THE ATA 20 TASKS, THE
LIGHTNING / HIGH INTENSITY RADIATED FIELDS (L/HIRF) TASKS AND ALL ZONAL INSPECTIONS IDENTIFIED EXCEPT THOSE
ASSOCIATED WITH MAJOR EXTERNAL ZONES (100, 200, 300 ETC). THESE TASKS ARE IDENTIFIED BY (EWIS) IN PARENTHESIS
FOLLOWING THE TASK DESCRIPTION.4. DETAILED INSPECTION (DI): AN INTENSIVE EXAMINATION OF A SPECIFIC ITEM, INSTALLATION OR ASSEMBLY TO DETECT
DAMAGE, FAILURE OR IRREGULARITY. AVAILABLE LIGHTING IS NORMALLY SUPPLEMENTED WITH A DIRECT SOURCE OF GOOD
LIGHTING AT AN INTENSITY DEEMED APPROPRIATE. INSPECTION AIDS SUCH AS MIRRORS, MAGNIFYING LENSES ETC MAY BE
NECESSARY. SURFACE CLEANING AND ELABORATE ACCESS PROCEDURES MAY BE REQUIRED.
5. GENERAL VISUAL INSPECTION (GVI):A VISUAL EXAMINATION OF AN INTERIOR OR EXTERIOR AREA, INSTALLATION OR ASSEMBLY
TO DETECT OBVIOUS DAMAGE, FAILURE OR IRREGULARITY. THIS LEVEL OF INSPECTION IS MADE FROM WITHIN TOUCHING
DISTANCE UNLESS OTHERWISE SPECIFIED. A MIRROR MAY BE NECESSARY TO ENSURE VISUAL ACCESS TO ALL SURFACES IN THE
INSPECTION AREA. THIS LEVEL OF INSPECTION IS MADE UNDER NORMALLY AVAILABLE LIGHTING CONDITIONS SUCH AS
DAYLIGHT, FLASHLIGHT OR DROP-LIGHT AND MAY REQUIRE REMOVAL OR OPENING OF ACCESS PANELS OR DOORS. STANDS,
LADDERS OR PLATFORMS MAY BE REQUIRED TO GAIN PROXIMITY TO THE AREA BEING CHECKED.
6. VISUAL CHECK (VC):AN OBSERVATION TO DETERMINE THAT AN ITEM IS FULFILLING ITS INTENDED PURPOSE. DOES NOT REQUIRE
QUANTITATIVE TOLERANCES. THIS IS A FAILURE FINDING TASK.
7. OPERATIONAL CHECK (OP):A TASK TO DETERMINE THAT AN ITEM IS FULFILLING ITS INTENDED PURPOSE. DO NOT REQUIRE
QUANTITATIVE TOLERANCES. THIS IS A FAILURE FINDING TASK.
8. FUNCTIONAL TEST (FU):A QUANTITATIVE CHECK TO DETERMINE IF ONE OR MORE FUNCTIONS OF A SYSTEM/SUB-SYSTEM OR
COMPONENT PERFORMS, WITHIN SPECIFIED LIMITS. THIS TASK MAY CALL FOR THE USE OF SPECIAL TEST EQUIPMENT.
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
3/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:3 of 19
FORM NO.IGO/E&M/A320/LO/41A
MANPOWER DETAILS
CERTIFYING STAFF
SN NAMELIC/APP./AUTH.
STAMPCAT
SHORT
SIGN.
SIGNATURE WITH
DATE
1
2
3
4
5
6
TECHNICIANS
SN NAME EMP. ID SHORT SIGN.SIGNATURE WITH
DATE
1
2
3
4
5
6
7
8
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
4/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY: IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:4 of 19
FORM NO.IGO/E&M/A320/LO/41A
A/C REG.: ______________ DATE: _______________ STATION: _______________
TOTAL NUMBER OF WORK ORDERS PERFORMED (SCHEDULED & UNSCHEDULED)
FLIGHT REPORT
DATE OF FLIGHT FLIGHT NO.
SECTOR FLOWN TIME IN AIRNO. OF
LDGS.
OIL UPLIFT (QTS.)
FROM TO AIRBORNE TOUCH DOWN IN AIR ENG 1 ENG 2 APU
TOTAL
PREVIOUS DAY RECORD CURRENT DAY RECORD TOTAL NOTE: THIS FLIGHT TIME LOG IS TO BE FILLED AND CERTIFIED BY THE APPROVED/AUTHORISED PERSON
A/C FLIGHT HRS.
A/C LANDINGS DATE TIMESIGN
(CERTIFYING STAFF)
APP. / AUTH.
STAMPCAT
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
5/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:5 of 19
FORM NO.IGO/E&M/A320/LO/41A
LIST OF REQUIRED TOOLS/EQUIPMENTS/CONSUMABLES
SN NOMENCLATURE PART NUMBER / SPECIFICATION QTY
1 SUITABLE ACCESS PLATFORMS NOT SPECIFIC AS REQUIRED
2 WARNING NOTICES NOT SPECIFIC AS REQUIRED
3 SAFETY BARRIER NOT SPECIFIC AS REQUIRED
4 CIRCUIT BREAKER SAFETY CLIP NOT SPECIFIC AS REQUIRED
5 LINT-FREE CLOTH NOT SPECIFIC AS REQUIRED
6 SPONGE NOT SPECIFIC AS REQUIRED
7 BRUSH - BRISTLED, SOFT NOT SPECIFIC AS REQUIRED
8 GLOVES - RUBBER NOT SPECIFIC AS REQUIRED
9 GOGGLES - PROTECTIVE NOT SPECIFIC AS REQUIRED
10 TYRE PRESSURE GAUGE NOT SPECIFIC 1
11 METALLIC CONTAINER NOT SPECIFIC AS REQUIRED
12 PIN-SAFETY (TOWING PIN) D23156000 1
13 GROUND SAFETY LOCK OF NLG DOWNLOCK D23080000 1
14 GROUND LOCK SLEEVE OF MLG DOWNLOCK460007280/
DRT689232
15 ENGINE OILMIL PRF 23699/
V10-077AS REQUIRED
16 HYDRAULIC FLUID SKYDROL LD4CML REF : 02-003D OR 02-506
AS REQUIRED
17 MINERAL HYDRAULIC FLUID MIL PRF 5606H AS REQUIRED
18
FUEL TANK DRAINING KIT
a) ADAPTING PIPE WATER DRAINING FROM
FUEL TANK.
b)
PURGERWATER DRAIN FOR WING TANKS.
c)
WATER DRAIN PURGER FOR CENTRE TANK.
98A28101000000/ 98D28104000000
98A28104000000
98A28104000002
97A28002117002
1
1
1
1
19 ONE LITER GLASS JAR FOR FUEL SAMPLE NOT SPECIFIC 1
20 FUEL SAMPLING KIT AQUADIS DETECTOR (HYDROKIT) AS REQUIRED
21 COVER-TOTAL TEMPERATURE SENSOR 98A10001013000 222 COVER-PITOT PROBE 98A10001005000 3
23 COVER-SLIP ON ANGLE OF ATTACK SENSOR
98A10001500000/
98D10003003000/
98F10001000000
3
24 COVER-STATIC PROBE 98D10103500001 6
25 COVER - ICE DETECTION PROBE 98D10103501000 2
26 PUMP - SUCTION NOT SPECIFIC 1
27 CART - SERVICING, WATER, POTABLE NOT SPECIFIC 1
28 WATER SOURCE - GROUND NOT SPECIFIC 1
29 CART - SERVICING, TOILET NOT SPECIFIC 1
30 DEODORANT-AIRCRAFT TOILETS MATERIAL NO. 11GCA1 AS REQUIRED
31 FILM - POLYETHYLENE NOT SPECIFIC AS REQUIRED
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
6/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:6 of 19
FORM NO.IGO/E&M/A320/LO/41A
SN NOMENCLATURE PART NUMBER / SPECIFICATION QTY
32 TAPE - ADHESIVE NOT SPECIFIC AS REQUIRED
33 VACUUM CLEANER NOT SPECIFIC 1
34 GENERAL NON AQUEOUS CLEANER MATERIAL NO. 08BAA9 AS REQUIRED
35 PETROLEUM BASED NON AQUEOUS CLEANER MATERIAL NO. 08BBB1 AS REQUIRED
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
7/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:7 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
THIS SCHEDULE CONSISTS 35 TASKS
SN DESCRIPTIONSKILL
CODETECH
CERTIFYING
STAFF
ARRIVAL
1 Install the wheel chocks.
REF: AMM TASK 10-11-00-555-015AF
2 Install the nose landing gear and the main landing gear ground lock safety
devices (as necessary). REF: AMM TASK 32-00-00-481-001AF
3 If aircraft towing is required, place the towing lever in the "towing position"
and install pin.REF: AMM TASK 09-10-00-860-092
AF
4 Install protection devices on the fuselage if aircraft ground time is over 4
hours.
REF: AMM TASK 10-11-00-555-069
AF
5 Review the aircraft technical log and start corrective actions as necessary. AF
NOTE: If the aircraft electrical network is not energized, perform items 6 and
7 otherwise continue with item 8AF
6 Do a safety check of the flight compartment for proper position of the
controls. AF
7 Energize the aircraft electrical network.
REF: AMM TASK 24-41-00-861-002AF
8 If STS has appeared on the upper ECAM DU, check for messages in the
maintenance section of the STATUS page on the lower ECAM DU. Start
corrective actions as required.
AF
9 ENGINE OIL
(MPD 791000-I1-1-IGO) REF: AMM TASK 12-13-79-610-011
Check oil level and replenish.
WARNING: IF NECESSARY TO REMOVE THE OIL TANK CAP, YOU MUST
WAIT A MINIMUM OF 5 MINUTES AFTER ENGINE SHUT-DOWN TO ALLOW PRESSURE IN OIL TANK TO DECREASE.
WARNING: OIL IS DANGEROUS IF IT IS ALLOWED TO BE ABSORBED
THROUGH THE SKIN AND INTO THE BODY. IMMEDIATELY
FLUSH THE OIL WITH WATER.
CAUTION: DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE ENGINE
BACK TO THE OIL TANK.
CAUTION: IF THE ENGINE WAS STOPPED FOR MORE THAN ONE HOUR,
DO SPECIFIC MAINTENANCE ACTION (REFER SUBTASK 12-13-
79-869-051) TO MAKE SURE THAT OIL LEVEL IS CORRECT. THIS
WILL PREVENT OVERSERVICING IF OIL IS ADDED.
Continued
EN
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
8/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:8 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
i. For NON-EDTO A/C:
Do a check of engine oil level as per AMM 12-13-79-610-011
and replenish, if required. Record the uplift in the aircraft
technical log.
ii.
For EDTO certified A/C:
a)
Do a check of the engine oil level on the tank sight gauge
within a period of 5 to 60 minutes after engine shutdown.
If the oil tank sight glass shows less than FULL, replenish
the oil tank to FULLlevel. Compute oil consumption since
last uplift and record in the aircraft technical log.
b)
Check no oil filter CLOG indication on ECAM ENG Page.
Record Oil uplift:
Engine No. 1 ........... Qts Engine No. 2 ...Qts
Also record the oil uplift in Tech Log and on page no.4 of this schedule.
EN
10APU OIL LEVEL CHECK
Check oil level and replenish.
CAUTION: IF POSSIBLE, WAIT AT LEAST 1 HOUR AFTER THE APU SHUT
DOWN TO ALLOW THE OIL TO BECOME COOL BEFORE YOUSERVICE THE SYSTEM. THIS WILL MAKE SURE THE SIGHT
GLASS READING IS ACCURATE.
i. For NON-EDTO A/C:
If ECAM APU page shows LOW OIL LEVEL message,
replenish APU oil tank to FULL level as per AMM TASK 12-
13-49-612-001 and record uplift in the aircraft technical
log.
ii. For EDTO certified A/C:
a)
If ECAM APU page shows LOW OIL LEVEL message,
replenish APU oil tank to FULL level as per AMM TASK 12-
13-49-612-001. Compute oil consumption since last uplift
and record in the aircraft technical log.b)
Check no Oil filter clog (APU Maintenance status on
ECAM.) Follow the TSM procedure if Class 2 message
indicates discrepancy with APU system including oil filter
clog.
Record Oil uplift.Qts.
Record following: APU S/N .. APU HRS ... APU CYC .
Also record the oil uplift in Tech Log and on page no.4 of this schedule.
EN
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
9/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:9 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
11
HYDRAULIC RESERVOIR QUANTITY CHECK
WARNING: DO NOT GET HYDRAULIC FLUID ON THE SKIN OR EYES. FLUSH
WITH CLEAN WATER AND GET MEDICAL AID.
Do a fluid level check of the Green, Blue and Yellow hydraulic reservoirs
(On ECAM LOWER DISPLAY, HYD page).
Add hydraulic fluid to the reservoirs as necessary. Record uplift(s)
Green ..Qts. Blue Qts Yellow .. Qts
Also record the hydraulic uplift in Tech Log
AF
EXTERNAL WALK AROUND (AIRFRAME)
12 INTEGRATED DRIVE GENERATOR
(MPD 242100-07-1) Ref. AMM 24-21-51-200-010
(NOTE: TO BE PERFORMED ON EDTO CERTIFIED AIRCRAFT ONLY).
CHECK IDG OIL LEVEL AND DIFFERENTIAL PRESSURE INDICATOR
Record Oil uplift:
IDG No. 1 ..... Qts IDG No. 2 ....Qts
Also record the oil uplift in Tech log.
EN
13 LOWER HALF OF FUSELAGE
(MPD ZL-100-01-1-IGO) REF: AMM TASK: 05-21-00-200-001
Do a general visual inspection of the lower half of the fuselage from ground
as far as visible, including:
Pitot probes, static ports and AOA sensors: No obstruction
(Inspection with protective covers removed)
Avionics equipment ventilation: Air inlet and air outlet valves
Batteries ventilation outlet (Venturi): No obstruction
Waste water drain mast
Antennas: No damage Wing and engine scan lights: Cleanliness
Wing-to-fuselage fairings and belly fairing
Anti-collision beacon light: Cleanliness
Radome: No damage, latches engaged and locked
Crew oxygen cylinder overpressure indicator: Green disc in place
(Near access door 812).
LP/HP GRD connection panelsCLOSED
Ram air inlet flap
Ram air intakes and outlets: No obstruction
Inspect the belly fairing access panels for missing fasteners.
Ensure that there are no signs of corrosion, cracks or damage.
AF
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
10/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:10 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
14 UPPER HALF OF THE FUSELAGE
(MPD ZL-200-01-1-IGO) REF: AMM TASK:05-22-00-200-001
Do a general visual inspection of upper half of fuselage from ground as far as
possible for signs of corrosion, cracks or damage, including:
Cockpit & cabin windows: adjoining structure
Emergency exits
Anti-collision beacon light: Cleanliness
Antennas: No damage
Ensure that there are no signs of corrosion, cracks or damage.
AF
15 STABILIZERS AND CONE/REAR FUSELAGE
(MPD ZL-300-01-1-IGO) REF: AMM TASK: 05-23-00-200-001
Do a general visual inspection of the rear fuselage with cone and stabilizers
from ground as far as visible, including:
THS and elevators: Damage, evidence of fluid leakage
Fin and rudder: Damage, evidence of fluid leakage
Static dischargers
Tail cone strobe light
Waste water drain mast
Outflow valve
Fuselage tail damage due to ground contact
Ensure that there is no sign of corrosion, cracks or damage.
AF
16 WING
(MPD ZL-500-01-1-IGO) REF: AMM TASK:05-25-00-200-001
WARNING: DO NOT EXTEND THE SLATS AND FLAPS WHEN THE THRUST
REVERSER COWLS ARE DEPLOYED IN THE 45 UNIT POSITION
Do a general inspection of LH and RH wings from ground as far as visible.
(A)RIGHT/LEFT WING LEADING EDGE
Do a general visual inspection of the wing leading edge from ground as far as
visible, including:
Slats
Leading edge access panels(pressure relief panels in place)
Surge tank NACA air intake: No obstruction
Surge tank overpressure protector: White cross visible
Ensure that there are no signs of corrosion, cracks or damage.
Continued
AF
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
11/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:11 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
(B) RIGHT/LEFT WING TIP AND TRAILING EDGE
Do a general visual inspection of the wing tip and trailing edge from ground
as far as visible, including:
Navigation and strobe lights for condition
Static dischargers missing or damaged
Control surfaces, flaps and flap track fairings: Damage, evidence of
fluid leakage
Lower wing surface: Damage, evidence of fuel leakage
Wing tank overpressure protector: Burst disk in place (White cross
visible Landing light: No damage, cleanliness
Ensure that there are no signs of corrosion, cracks or damage.
AF
17 LANDING GEAR AND LANDING GEAR DOORS
(MPD ZL-700-01-1-IGO) REF: AMM TASK: 05-27-00-200-001
Do a general visual inspection of the main and nose landing gears and
landing gear doors from ground as far as visible, including:
Doors and wheel well
Gear assembly structure: Damage, evidence of leakage
Shock absorber: Signs of leakage and normal extension
Shock absorber sliding tube: Scoring/damage, cleanliness,
(if necessary, make a clean cloth moist with mineral hydraulic fluid
(Mat. No. 02-001), clean tube and dry with a clean cloth)
Proximity detectors: Security, cleanliness
Brake units: Evidence of leakage or overheating
Ensure that there are no signs of corrosion, cracks or damage.
AF
18 DOORS
(MPD ZL-800-01-1-IGO) REF: AMM TASK: 05-28-00-200-001
Do a general visual inspection of all pax, service and cargo doors from
ground for signs of corrosion, cracks or damage.
4 Passenger/Crew doors
3 cargo compartment doors
4 overwing emergency exits
Service panel doors, avionic compartment access doors,
AF
19 TANKS
(MPD 281100-01-2) REF: AMM TASK: 12-32-28-281-001
Drain water from wing tanks and center tank at water drain valves
Take fuel samples from all tanks. Check for any contamination. Check water
contents in the samples with Aquadis detector (HYDROKIT).
After drainage, make sure that the drain valves are correctly closed and not
leaking.
AF
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
12/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:12 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
20 WHEELS
(MPD 324100-01-1) REF: AMM TASK: 32-41-00-210-003
Inspect Nose, RH / LH Main Landing Gear Wheels and Tyres for satisfactory
condition (Wear & Damage) including:
Wheels: Rim damage, sheared/missing tie bolts
Tyres: Wear, damage and signs of under inflation/over inflation.
NOTE: For tyre damage, cuts, chord breakage etc refer to AMM Task
32-41-00-210-002.
CAUTION:
1. TYRE PRESSURE MUST BE CHECKED WHEN THE TYRES ARE NOT
HOT.
2. SERVICE TYRES WITH NITROGEN ONLY.
3. ON ANY DAY IF LOW TYRE PRESSURE IS SUSPECTED ON ANY WHEEL
DURING INSPECTION THEN CHECK THE TYRE PRESSURE OF THE
SUSPECTED WHEEL/S AND INFLATE TO MAXIMUM TYRE PRESSURE.
4. AT LINE STATION IF DRY NITROGEN GAS IS NOT AVAILABLE THEN
AIR MAY BE USED. BUT BEFORE USE IT MUST BE ENSURED THATTHE AIR BEING USED HAS OXYGEN NOT MORE THAN 5% BY
VOLUME.
HOWEVER IF AIR WITH UNKNOWN OXYGEN CONTENT IS USED
THEN THIS AIR SHOULD BE REMOVED FROM TYRES WITHIN 15
HOURS AND THE TYRES CHARGED WITH DRY NITROGEN.
ACCORDINGLY A NOTING SHOULD BE REFLECTED IN DEFERRED
MAINTENANCE AND WORKORDER.
5. THE CHEMICAL REACTION BETWEEN THE OXYGEN IN THE TYRES
AND GASES FROM THE INNER LINER OF THE TYRE MAY CAUSE A
TYRE EXPLOSION.
Check and record tyre pressure and inflate to maximum specified tyre
pressure, if necessary
(TO BE DONE DURING NIGHT HALT ON SUNDAY, TUESDAY & THURSDAY)
NOTE: MLG Tyre Pressure - Min : 210 psi Max: 220 psi
NLG Tyre Pressure - Min : 178 psi Max: 187 psi
CAUTION: IN CASE TYRE PRESSURE IS FOUND BELOW 170 PSI FOR NLG OR
BELOW 190 PSI FOR MLG REFER AMM TASK 32-41-00-210-059 FOR FURTHER
ACTION.
Continued
AF
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
13/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:13 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
INITIAL TYRE PRESSURE:
Main Wheels Nose Wheels
#1 #2 #3 #4 #1 #2
Tyre Pr.
(PSI)
FINAL TYRE PRESSURE:
Main Wheels Nose Wheels#1 #2 #3 #4 #1 #2
Tyre Pr.
(PSI)
Record the following Data:
TP Gauge Serial No. ..
Gauge Calibration date: . Next due on
AF
21 MAIN LANDING GEAR BRAKES
(MPD 324227-01-1) REF: AMM TASK:32-42-27-210-003
WARNING: PUT SAFETY DEVICES AND WARNING NOTICES IN POSITION
BEFORE STARTING INSPECTION NEAR MLG AND THE RELATED
DOORS.
Functional check of brake heat pack for wear by use of the wear indicator
(parking brake applied)
Ensure that there are no leaks from brake assemblies and hydraulic lines.
AF
WASTE/WATER SERVICING
NOTE: In freezing conditions, drain the potable water system and the toilet
waste tank. Service before aircraft departure.
NOTE: Obey the cold weather maintenance procedure (Ref. TASK 12-31-38-
660-001).
NOTE: If the temperature in the aircraft is below 4 DEG.C (39.20 DEG.F) do
the pre-conditioning procedure (Ref. TASK 12-33-21-618-001).
AF
22 Ensure that the potable water system is serviced as required.
To fill the potable water system with electrical power (Ref. AMM TASK 12-
15-38-613-001).
To fill the potable water system without electrical power (Ref. AMM TASK
12-15-38-613-002).
AF
23 Ensure that the toilet waste tank is serviced as required (Ref. AMM TASK 12-
16-38-613-001). AF
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
14/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:14 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
FLIGHT COMPARTMENT
24CREW OXYGEN SYSTEM
On the DOOR/OXY page (lower ECAM DU), ensure that the oxygen pressure
is indicated in Green
AF
25AIRCRAFT DOCUMENTS
Check for the presence and validity (where applicable) of the following
documents. Torn/mutilated/missing/invalid documents must be replaced.
1.
Certificate of Registration
2.
Certificate of Airworthiness
3. Airworthiness Review Certificate (ARC)
4.
Aircraft Station License
5.
Noise Certificate
6.
Permit to Operate
7. Certificate of Insurance
8.
Weight Schedule
9.
Emergency Equipment Location Chart
10.
LOPA11. MEL Vol 1 and Vol 2
12.
Flight Report Book (FRB)
13.
Dent & Buckle Chart
14.
Cabin Defect Log Book (CDLB)in passenger compartment.
AF
26 EMERGENCY EQUIPMENT:
Check the emergency equipment for presence, correct stowage & validity
(where applicable).
Refer Emergency Equipment Location Chart in Documents on -board file
for location and quantity of the equipment.
1.
Crash Axe
2.
Fire proof gloves
3.
Life vest for crew
4.
Portable fire extinguisher
5. Portable Breathing Equipment
6. Flash light
7.
Escape Rope
AF
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
15/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:15 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
27Check for the presence of Fan Cowl Doors (FCD) Latch Keys (Qty. 2) in the L/G
pins stowage compartment in cockpit.
Ensure that a flag "remove before flight" is attached to the keys.
NOTE:
1. TO BE PERFORMED ON AIRCRAFT WITH MODIFIED FAN COWL DOOR
LATCH (POST MOD SB A320-71-1069 & Goodrich VSB NAC-71-0331).
2. THE MODIFIED FAN COWL DOOR LATCH CAN BE IDENTIFIED BY THE
FOLLOWING:
a.
ON THE FAN COWL, USE KEY SHALL BE PAINTED ADJACENT
TO THE LATCH.
b. IN THE COCKPIT, THE LANDING GEAR PINS STOWAGE
COMPARTMENT SHALL HAVE AN ADDITIONAL PLACARD
STATING FCD KEYS At the backof STWG.
EN
PASSENGER COMPARTMENT
28 EMERGENCY EQUIPMENT
Check the emergency equipment for presence, correct stowage & validity(where applicable).
Refer Emergency Equipment Location Chart in Documents on-board file
for location and quantity of the equipment.
1.
First Aid Kit (FAK)
2.
Medical Kit (MK)
3. Universal Precaution Kit (UPK)
NOTE: REPLACE THE FAK, MK OR UPK IF THE VALIDITY IS LESS
THAN 3 DAYS.
4. Megaphone
5.
Life vest for cabin crew
6.
Life vest for infants7.
Portable fire extinguisher
8. Portable oxygen bottle & masks
9.
Portable Breathing Equipment
10.
Manual Release Tools
11.
Portable ELT
12.
Flash lights
13. PAX Life Vests
14. Automated External Defibrillators (AED)
Ensure that the Green Ready light is blinking.
- If the Ready light is steady: The AED is in use or running
a self-test.
Continued
AF
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
16/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:16 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
NOTE:
-
If the Ready light is off, the AED is chirping, and the i-
button is flashing: The following may be the probable
causes:
a)
A self-test error has occurred,
b)
there is a problem with the pads,
c) the Infant/Child Key has been left installed,
d)
the battery power is low.
Press the i-button for instructions.
-
If the Ready light is off but the AED is not chirping and
the i-button is not flashing: The following may be the
probable causes:
a)
there is no battery inserted,
b) the battery is depleted,
c)
the defibrillator needs repair.
15.
Additional Emergency Equipment on EDTO certified A/C:
a) Survival Kit
b)
Over-wing Escape Life Lines
c)
Supplemental Life Raft
d) Portable ELT
AF
29 DEMO KIT CONTENTS:
Check the FWD and AFT Demo Kits contentsas mentioned below:
SN Description FWD Demo Kit AFT Demo Kit
1 DEMO MASK 1 2
2 DEMO BELT 1 2
3 EXTENSION BELT 2 24 PAX INFO CARD 1 2
5 DEMO LIFE VEST 1 2
AF
30 General visual check of the left and right wing upper surface and control
surfaces, through cabin windows.
AF
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
17/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:17 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
AIRCRAFT CLEANING
31 COCKPIT AREA
Check and clean the cockpit area including windshield & windows, crew and
observer seats, floor area and cockpit door.AF
32 CABIN
Check passenger compartment for general cleanliness including PSU,
Stowage compartments in galleys, toilets, doors, ceiling and side wall panels.
Passenger seat upholstery, carpets and passenger windows.
AF
33
EXTERIOR CLEANING
REF: AMM TASK 12-21-11-615-002
External surface of fuselage, wing control surfaces, landing gear doors.
Check that fuselage exterior is free from streaks and deposits.
AF
EXTERNAL WALK AROUND (APU)
AUXILLARY POWER UNIT
34Visual check of the APU area from ground for general condition:
Air intake
Doors: Closed and secured
Drain mast, drains and vents
Exhaust
Fire extinguisher overpressure discharge indicator: Red disc in
place
Ensure that there are no signs of corrosion, cracks or damage.
EN
EXTERNAL WALK AROUND (ENGINES)
35 POWER PLANT, NACELLES AND PYLON
(MPD ZL-400-01-1-IGO) Ref: AMM Task: 05-24-00-200-001
Visual inspection of power plant, nacelles and pylon from ground as far as
visible(cowl doors closed) including:
Pylon fairing and fillets: No damage, pressure relief doors closed
Engine air inlet: lip and outer and inner skin, riveting, acoustic
panels, and visible probes and sensors (P2/T2)
Fan blades, annulus fillers and spinner: No damage
Fan rotor path, splitter fairing, inlet guide vanes, fan outlet guide
vanes and fan duct. Check Fan free rotation by hand.
External surface of the fan cowl doors and thrust reverser doors,
Doors closed and correctly latched. Access doors and pressure
relief doors in place, closed and secured.
Continued
EN
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
18/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:18 of 19
SIGNATURE
(CERTIFYING STAFF)AUTH. STAMP
FORM NO.IGO/E&M/A320/LO/41A
SN DESCRIPTIONSKILLCODE
TECHCERTIFYING
STAFF
Air inlets/outlets: No obstruction.
Translating sleeves correctly stowed.
CNA (Common Nozzle Assembly) and exhaust: Last stage LPT
blades, struts, nozzle and plug (for damage and metal deposit)
Drain mast and pylon drains: No obstruction, evidence of leakage.
Fan Exhaust: Acoustic lining, exit vanes, struts and thrust reverser
blocker doors.
Ensure that there are no signs of corrosion, cracks or damage.
EN
7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)
19/19
LAYOVER INSPECTION SCHEDULE
(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)
APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY:IGO ALL
INTERVAL To be performed once every 36 calendar hoursISSUE: 09 Rev 00 DATED: 14.06.2016
PAGE:19 of 19
FORM NO.IGO/E&M/A320/LO/41A
CERTIFICATE OF RELEASE TO SERVICE
ORGANIZATION NAME INTERGLOBE AVIATION LIMITED (INDIGO)
ORGANIZATION APPROVAL
REFERENCE
DAW, DELHI REGION LETTER NO. INDIGO/FAPP/1034 DATED
31/07/2006
CERTIFICATE OF RELEASE TO SERVICE IN ACCORDANCE WITH CAR 145
AIRCRAFT AIRBUS A320-232 MSN REGISTRATION TAH TAC
HAS BEEN MAINTAINED AS SPECIFIED IN THE WORK ORDERWORK ORDER
NO.
RECORD WORKORDER & TASKCARD NUMBERS (AS APPLICABLE), INCLUDING A BRIEF DESCRIPTION OF WORK
PERFORMED*
CERTIFIES THAT THE WORK SPECIFIED EXCEPT AS OTHERWISE SPECIFIED WAS CARRIED OUT IN ACCORDANCE WITH
CAR-145 AND IN RESPECT TO THAT WORK THE AIRCRAFT/AIRCRAFT COMPONENT IS CONSIDERED READY FOR
RELEASE TO SERVICE.
CERTIFYING
STAFF (NAME)SIGNATURE
LIC/APP./AUTH.
STAMP
LOCATION** DATE TIME
* REFERENCE TO APPROVED DATA USED TO PERFORM THE WORK
** LOCATION WHERE THE WORK WAS PERFORMED
FORM NO. IGO/E&M/CRS/No. 7 Issue 1
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