2. Layover Inspection Schedule Issue 09 (A320-232)

7/25/2019 2. Layover Inspection Schedule Issue 09 (A320-232)

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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


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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.


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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


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APPROVAL IGO/E&M/Approval/Insp.Sch/40 dated: 14.06.2016 EFFECTIVITY: IGO ALL


PAGE:4 of 19


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


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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


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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


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SIGNATURE

(CERTIFYING STAFF)AUTH. STAMP


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


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SIGNATURE



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


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SIGNATURE




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


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SIGNATURE




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


AF

15 STABILIZERS AND CONE/REAR FUSELAGE


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


Continued

AF


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SIGNATURE




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


AF

17 LANDING GEAR AND LANDING GEAR DOORS


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


AF

18 DOORS


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


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SIGNATURE




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


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SIGNATURE




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


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SIGNATURE




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


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PAGE:15 of 19

SIGNATURE




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


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SIGNATURE




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


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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


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


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SIGNATURE




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.


EN


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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