EPF107 Preflight_Transit Check_ Rev 09

A320/A321 MAINTEN MAINTENANCE ANCE SCHED SCHEDULE ULE Applicabilit Applicability y

FORM EPF107 REV. 09 DATE: 08 Oct 2015 A320/A321 A320/A321

PRE-FLIGHT/TRANSIT CHECK SHEET A/C Reg. Reg. Number Number

1.

THEPRE-FLIGHT/ TRANSIT CHECK SHALL BE CARRIED OUT BEFORE EACH FLIGHT BUT NOT EARLIER THAN TWO (2) HOURS BEFORE THE FLIGHT. 2. THIS CHECK SHEET MUST BE REFERRED TO WHEN PERFORMING A PRE-FLIGHT / TRANS IT CHECK. PERFORMED BY AN AUTHORISED AUTHORISED PIC OR OR CRS CRS ENGINEER. 3. ALL MAINTENANCE ACTIVITIES MUST BE PERFORMED 4. CERTIFICATION OF THIS TRANSIT CHECK SHALL BE IN TECHNICAL LOG BY THE APPROPRIATE AUTHORISAT ION UPLIFTED MUST BE RECORDED ON THE CURRENT AIRCRAFT AIRCRAFT TECHNICAL TECHNICAL LOGBOOK. 5. ALL FLUIDS UPLIFTED SAFETY PRECAUTION AT AIRCRAFT ARRIVAL ENSURE PARKING AREA IS CLEAR OF FOREIGN OBJECTS OR ANY OTHER OBSTRUCTIONS, CHECKOPERATION OF AIRCRAFT EXTERIOR LIGHTS DURING TAXIING IN IF OPPORUNITY ALLOWS

ITEM 1.0

1.1

TASK DESCRIPTION PREPARATION Install wheel chocks after beacon light is off (for transit check only). Chocks must be positioned at forward and aft of nose wheels AND at the forward and aft of EITHER side of outboard main wheels. NOTE: Consideration should be given to allow sufficient clearance between the chock and the wheel for aircraft settling during fuelling and passenger embarkation.

1.2

If aircraft towing is required, install landing gear ground lock safety and steering bypass pins.

2.0

PRELIMINARY ITEMS

2.1

Check matching of flight control positions between controls in flight compartment and external movable surfaces.

NOTE: If the A/C electrical network is not energized, perform item 2.2 otherwise continue with item 2.3 onwards. Energize the aircraft electrical network (Reference: AMM 24-41-00). 2.2

CAUTION:

PERFORM SAFETY CHECK OF THE FLIGHT COMPARTMENT FOR CONDITION OF THE CONTROLS PRIOR TO ENERGIZING THE ELECTRICAL NETWORK.

Check BATTERY 1 and 2 volts immediately BEFORE selection of GU/APU or IF power has been off more than six hours.

2.3

BATT 1 AND 2 BATT 1 AND 2 VOLTAGE

CHECK OFF CHECK ABOVE 25V

If Batteries voltage above 25V, No further action is required. If batteries voltage below 25V, perform charging of about 20 minutes by pushing-in BAT1/BAT2 push button on OVH panel (35VU). 2.4

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Inspect the flight compartment windshields and side windows for damage and cleanliness. Clean if required.




ITEM

TASK DESCRIPTION Ensure Essential documents folder and contents are on board, properly stowed and in good condition: 1. Essential folder: a. Certificates (COA, COR, Radio License, Noise certificate, AOC, insurance cert etc.) b. Report forms: MOR, OSSR c. EEL d. LOPA e. CMR

2.5

f. Etc. 2. Tech log folder: a. ADD logs b. Concession c. Tech log book d.Etc. 3. Cabin Log Note: follow Note: follow Table of Content in each folder to check its completeness

2.6

2.7

3.0

Review Aircraft Technical Log, Airworthiness Deferred Defect Log, Non Airworthiness Deferred Defect Log. Check for open ADDs that require maintenance actions and start corrective actions as necessary before flight or alert to flight crew. Review cabin condition log for airworthiness items, if found, transfer to Aircraft Technical Log for corrective actions. NOTE: If ground time is more than one hour, APU must be shutdown with GPU connected. If no GPU is available, actions are left to the flight crew decision. FLUIDS MONITORING On ECAM display, check oxygen, oil, fuel, and hydraulic fluids for normal operation indications. If the ECAM ENG OIL QTY LOW LEVEL advisory is reported, visually check engine oil quantity on the oil tank sight gauge. Uplift if necessary (Reference: AMM 12-13-79). WARNING: IF NECESSARY TO REMOVE THE OIL TANK CAP, YOU MUST WAIT A MINIMUM OF 5 MINUTES AND NO GREATER THAN 60 MINUTES AFTER ENGINE SHUT-DOWN TO LET OIL SYSTEM AIR PRESSURE BLEED OFF. Record engine oil Uplift in Aircraft Technical Log or annotate nil/zero if no uplift is required. EXTERNAL CHECKS Perform aircraft walk-around and check the engines, fuselage, wings (including winglets or sharklets) and empennage inclusive of probes and ports to make sure there is no: Impact/Damage Lightning Strike Foreign Objects Fluid leakage Missing or loose parts Missing overpressure discharge discs, Damage of the fuselage tail skin by ground contact during takeoff, takeoff, Obstruction of inlets/outlets, inlets/outl ets, and probes/ports which may have occurred during the last flight. If necessary, where snow or ice condition exists, ensure aircraft exterior especially control surfaces and engine intakes are free from ice and snow, deicing may be required. Techlog entry for deicing is required.    

3.1

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A320/A321 MAINTEN MAINTENANCE ANCE SCHED SCHEDULE ULE

FORM EPF107 REV. 09 DATE: 08 Oct 2015

Applicabilit Applicability y

A320/A321 A320/A321


ITEM

TASK DESCRIPTION RVSM REQUIREMENTS Perform visual inspection of the Pitot Probes, Static Ports and AOA Sensors for obvious damage. Check aircraft skin in the vicinity of Pitot Probes and Static Ports for any sign of damage before first departure of the day (Reference: AMM 34-13-00).

3.2 Review open ADDs for MEL items that affect RVSM operations, inform to VJC MCC as required. NOTE: If damage or irregularities are found (which are within limits for normal flight), the aircraft must not be dispatched into RVSM airspace until evaluation is performed refer SRM ATA 53. Techlog entry and Notice to Crew shall be clearly stated in the Aircraft Technical Logbook. Check the engine and make sure: There is no damage damage on the air intake and the the fan blades or acoustic acoustic liners liners There are no foreign objects in the engine air intake, There is no fluid leakage on the drain mast, The cowl doors are correctly closed and latched. There is no damage or metal metal deposit at the turbine exhaust, inclusive of LPT blades, nozzle and plug.  

3.3

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Check the landing gear doors, wheels, brakes, tires and make sure: The NLG and MLG shock absorber shows normal extension, Tires: there’s no abnormal wear, no obvious damage and or signs of under inflation. There is no hydraulic fluid leakage on the brake units. Make sure that the wear indicators are in the limits (protruding) when the brakes are cold (brake temperature less than 60 oC) and with the parking brake ON.   

3.4

NOTE:

Check tire pressure before first departure of the day (Reference: AMM 32-41-00) and record in Aircraft Technical Log, including including P/N P/N and S/N of the gauge used for the tire pressure check.

CAUTION: CAUTION:

TYRE PRESSURES MUST BE CHECKED AND CORRECTED WHEN THE TYRES ARE COLD. SERVICE TYRES WITH DRY NITROGEN NITROGEN ONLY (AD 87-08-09). REFER TO AMM TASK 3241-00-10-003-A FOR MAINTENANCE PRACTICE. PRACTICE.

4.0

4.1

PASSENGER COMPARTMENT Generally check control and passenger cabin including lavatories and galleys for obvious discrepancy and are in clean and presentable condition. For first departure of the day, check trash cans are installed in all lavatories and galleys.

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ITEM

TASK DESCRIPTION For first departure of the day, day , perform a check of the emergency equipment for presence and proper stowage IAW EEL. 

Check Emergency Emergency first aid kit for proper seal and date of validity. validity. NOTE:

If seal is broken, check content and replace as required and reseal immediately if expiry date due is less than 1 week, replace kit or apply MEL (if necessary and applicable).

4.2 

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Check that the portable oxygen bottle masks and infant masks are compatible with the portable oxygen bottles. Check indicator light and seals on DME Flashlights (or the operation of other types of flashlight). Check seal intact on Cabin Fire Extinguisher for presence. Check passenger life vests on each seat position for presence. Check crew on each crew position for presence. Check quantity of spares: 10% adult life vests and 10% infant life vests

5.0

REFUELING

5.1

Refuel aircraft up to the required dispatch quantity and record uplift/content in the Aircraft Technical Log (Reference: AMM 12-11-28).

5.2

Ensure that the refuel coupling caps are in place and secured.

5.3

Ensure that the Magnetic Level Indicators (MLIs) (If Used) are correctly retracted and secured.

6.0

WATER/WASTE SERVICING

6.1

Service the potable water system and toilet waste tank as required. After servicing ensure the area is dry and no leak. Rectify defects before flight if any.

7.0

FINAL ITEMS

7.1

Remove the protective covers from the aircraft if installed. Record removal in Aircraft Technical Log.

7.2

Check and record corrective actions in Aircraft Technical Log.

7.3

Remove the nose and the main landing gear ground safety lock and protective covers if installed. Record the removal in Aircraft Technical Log.

7.4

Certify the Preflight/Transit Check and fuel record in the Aircraft Technical Log. Note: Only an Authorized PIC or CRS engineer can certify and release the aircraft into service.

8.0

FINAL CLOSURE ACTIONS ACTIONS PERFORM A FINAL AIRCRAFT WALK AROUND: NOTE: Can be performed by either authorized CRS person or Authorized Headset/Pushback person Carry out a walk-around check ensuring all filler caps, fuel dipstick, servicing and inspection panels, cargo, service and passenger doors are CLOSED AND SECURED. Ensure no foreign objects at air intakes and all blanks are removed.

8.1

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If necessary, where snow or ice condition exists, ensure aircraft exterior especially control surfaces and engine intakes are free from ice and snow.




ITEM 8.1

TASK DESCRIPTION Make sure that all passenger/crew doors, cargo compartment doors and service panel doors are correctly closed and secured. Make sure that no damage has been caused by ground equipment, during baggage loading and/or servicing Prepare aircraft for departure, with necessary personnel and equipment available, observing all the safety precautions. Depart the aircraft. NOTE: APPLI NOTE: APPLICABL CABLE E WHEN WHEN AEROBR AEROBRIDGE IDGE IS USED. USED.

8.2 After the the aircraft aircraft doors doors have been closed closed and aerobridge aerobridge retracted, retracted, ensure aircraft aircraft pilot heads heads and stall stall warning probes are free from damage. Contact the flight crew to inform them the aircraft is ready for dispatch.

8.4

If external power has been used, request the flight crew instructions for GPU de-energize and disconnection. Make sure that the aircraft surrounding area is clear for dispatch.

8.5

Remove wheel chocks (Upon flight crew instruction).

8.3

After After aircraft aircraft towing towing or push back, ensure the the towing towing pin is removed removed and the towing lever lever is in the the normal normal (Spring loaded) position. 8.6 CAUTION: DISCONNECT THE TOW BAR BEFORE YOU REMOVE THE TOWING LEVER SAFETY PIN. THIS PREVENTS POSSIBLE DAMAGE TO THE SYSTEM.

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EPF107 Preflight_Transit Check_ Rev 09

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