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A/C TYPE:A320 / A321/A319CHECK TYPE: TRANSIT CHECK

FORM: MP 320-A A/C Reg.: Flt. No. : Page 1 of 11ISSUE: 06/18-08-2012 A/C HRS: Station: DATE:

ITEM WORK DESCRIPTION MECHSUPV/

INSP

For any inquiries, please contact Mr. Iyad AWARTANI, IP 3340, Email; [email protected]

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A. PRE. SERVICE ITEMS

1. Review A/C log book and cabin log bookNote: Correct continued items consistent with available ground time, spare parts,and manpower.

2. Read the post flight report on CFDS.3. Review Yellow Sheet for proper entry and corrective action4. Check Aircraft library content for the following doc.

1- Original C OF A & Original C OF R2- Original Airworthiness Review Certificate - ARC3- Original or true copy of Noise Certificate4- Original or true copy of Air Operator Certificate and OPS SPECS5- INSURANCE CERTIFICATE6- RADIO LICENCE

7- RVSM8- Dent & Buckle Chart9- Technical Log +Cabin Log book and additional copies10- Minimum Equipment list (MEL) and Master Minimum Equipment list

(MMEL)

General Items

The exterior inspection ensures that the overall condition of the aircraft and its visiblecomponents and equipment are safe or the flight. Do a visual inspection of thefuselage, empennage, wings, nacelles and associated elements to

Check structure for impact damage Check that there is no evident fuel, oil or hydraulic leak Check that all ground access door are closed

NOTE: Due to RVSM condition, special attention shall be paid during the visualinspection to check for dents, deformation and any other structural damage atmarked areas of skin around the following elements:

Sensor Angle of Attack (3 positions) Probe Pitot (3 positions) Probe Static (6 positions) Sensor TAT (2 positions)

WALK AROUND CHECK

The parking brake must be ON during the exterior inspection, to allow checking ofthe break wear indicators.

1. Carry out a walk around check of the fuselage, wings, nacelles andempennage for general condition, cleaning and security.

2. Check screws/rivets availability and looseness3. Ensure intakes are clear of foreign objects4. Check external placards for condition & availability

LH FUSELAGE- Wing and engine scan lights...CONDITION- AOA probe.....CONDITION- Static ports.... CONDITION /CLEAR- Avionics Skin Inlet valve.....CONDITION- LH Avionics compartment door .CLOSED

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NOSE SECTION- Pitot probes...CONDITION- TAT probes....CONDITION- Crew oxygen discharge indicator...GREEN- Radome and latches....CONDITION/LATCHED- FWD Avionics compartment door .CLOSED- Ice detection probes.CONDITION- Ground electrical power door (if not required)...CLOSED- Static ports.... CONDITION /CLEAR

NOSE L/G- Taxi and turn off light.......CONDITION- Nose wheel chocks...IN PLACES

- Wheels and tires...CONDITION- Nose gear structure..CONDITION- Hydraulic lines and electrical wires....CONDITION- Wheel well......CHECK- Shock absorber.....CONDITION- Safety pin............REMOVEDRH FORWARD FUSELAGE- AOA probes .....CONDITION- TAT probes.....CONDITION- Pitot probes.....CONDITION- Static ports.... CONDITION /CLEAR- Cargo loading operation access door....... CLOSED- Cargo door operation access door.CLOSED

- Cargo door.....CLOSED- Wing and engine scan lights.....CONDITION- RH FWD Avionics compartment door .CLOSED- RH AFT Avionics compartment door .CLOSED- Avionic vent outlet valve ..........CONDITION

LOWER CENTER FUSELAGE- LP ground connection door.............CLOSED- Antennas..........CONDITION- Drain mast CONDITION- Anticollision light...CHECK- Pack air intakes and outlets...............CLEAR- HP ground connection door..CLOSED- Ground hydraulic connection blue..... CLOSED- Left L/G ground opening access door.....CLOSED- Right L/G ground opening access door..CLOSED- Ground hydraulic connection yellow...CLOSED

RH CENTER WING- Inner tank magnetic fuel levels ......................................................FLUSH- Fuel water drain valves (inner tank)...NO LEAK- Refuel panel ....CLOSED- Landing light....CONDITION- Slats ..CONDITION

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ENG 2 LH SIDE- Engine Oil fill access door........CLOSED- Master Magnetic chip detector access door..CLOSED- Thrust reversers cowl door...CLOSED- Pressure relief doors.CLOSED- Fan cowl door..CLOSED/LATCHED- Drain masts....CONDITION/NO LEAK- Access door to reversers latches....CLOSED- Engine inlet and fan bladesCHECK

ENG 2 RH SIDE- Fan Cowl door....CLOSED/LATCHED- Thrust reverser cowl door.CLOSED

- Access to starter valve manual override....CLOSED- Pressure relief doorCLOSED- Turbine exhaust....CLEAR

-Check engine oil quantity on ECAM lower display Engine page within 5 minutesafter engine shut-down as per AMM ref. 12-13-79.

If indication is below minimum, check engine oil level at sight glass, and serviceengine oil as required with ESSO 2380 (Accomplish step 2 prior to servicing).

Recorded quantity added in Log Book and below make sure that filler caps areproperly installed after servicing).ENG. NO. 1 -----------------------------------------

ENG. NO. 2 -----------------------------------------

-Prior to servicing, perform SNIFF / SMELL check for evidence of fuel contamination.Check IDG low oil level (within green range) and carry out complete servicing if low.

-Check cowlings and Pylons for damage and evidence of fuel, oil and hydraulicleakage.-Inspect visually stage 4 blades for unlatching and shingling.(FOR CFM EnginesONLY)-Fan thrust reverser door latches for proper closing (red indicator and protruding)Access doors and over pressure doors in place, closed and secured.-Check fan blades and spinner (free rotation by hand).-Check nose cowl, fan reverser and turbine nozzle for damage loose or missingrivets.-Check last stage LPT blades as visible with a flashlight for obvious damage andmetal deposit.-Ensure hydraulic hand pump, used to open and close the thrust reverser cowls, isstowed on board of A/C.-Inspect the Intakes for fan blade damage and oil leaks-Inspect the air intake for security and proper fit-Inspect the cowling doors for security and proper fit-Inspect the lower cowling security and evidence of fluid leaks-Inspect the exhaust for turbine and tailpipe damage and evidence of fluids-Inspect the reverser doors for stowage and security, evidence of fluids

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RH LEADING EDGE- Refuel coupling door..CLOSED- Magnetic fuel levels ..FLUSH- Fuel water drain valve (outer tank).NO LEAK- Slats ..CONDITION

RH WING TIP- Fuel ventilation overpressure disc...........................INTACT- Wing fence.....CONDITION- Magnetic fuel levels FLUSH- Fuel water drain valve (Surge tank)....NO LEAK- Surge tank air inlet.....CLEAR

- Slats ..CONDITION- Navigation light .CONDITION- Antennas on top of fuselage...CONDITION

RH WING TRAILING EDGE- Control surfaces...CONDITION- Flaps and fairings.CONDITION- Static dischargers.....CHECKMissing static discharge eliminators (number missing in accordance with MEL/CDL

RH LANDING GEAR- Chocks.REMOVED- Wheels and tires......CONDITION

- Brakes and brake wear indicators.CONDITION- Hydraulic lines...CHECK- Landing gear structure.CHECK- Downlock springs.....CHECK- Safety pin....REMOVED

- Check if there is any indication of wear, chaffing lines, chaffing wires, cracks, dents,or other damage- Check structural of gear doors for condition (cracks, dents or other damage)- Hydraulic leaks (gear struts, actuators, steering valves etc)- Check Wheel cab and fan cover for condition and secure- War, line security, leaks and installation of brakes- Corrosion- Check shock struts for correct extension. Clean and apply fluid 41 if required.- Check proximity detectors and taxi lights for security and cleanliness.- Check brakes for wear and overheating. (Ref. AMM 324227/6).

At Hangar ONLY: (If the heat pack wear indicator PIN is less than 2mm,Remove the Brake and send for O/H)

Note: check each heat pack wear indicator (with barking pressure applied) andcircle Yes or NO in the below table.

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Brake Pins

No. 1 No. 2 No. 3 No. 4

within limit within limit within limit within limit

Yes No Yes No Yes No Yes No

- Check wheels for rim damage, sheared / missing tie-bolt and tire for wear cuts,bulges and flat spots.- Check tire pressure values in relation to the aircraft weight (MRW) and tire sizes asper the tables available in the AMM Ref. 32-41-00/601

Tire checked: Hot [ ] Cold [ ]

NLG MLG

LH RH 1 2 3 4

CENTER FUSELAGE- Refuel electric control panel..CLOSED- APU FUEL drain....CONDITION/NO LEAK- Ground hydraulic connection green and reservoir filing.CLOSED- Antennas...CONDITION

RH AFT FUSELAGE- Drain mast.CONDITION- Cargo loading operation access door.....CLOSED- Cargo door operation access door..CLOSED- Cargo door..CLOSED- Bulk door.CLOSED- Waste service panel..CLOSED- Outflow valve .. CONDITION

TAIL- Stabilizer, elevator, fin and rudder........CONDITION- Static dischargers (elevator rudder)..CHECK- Lower fuselage structure (tail impact on run away).CONDITION

- Flight records access doorCLOSED- Check tail section including empennage from ground for obvious damage, fluidleakage, static discharges for presence, outflow valve for conditions and evidence ofscraping runway

APU- Access door....CLOSED- Air intake...CONDITION- Exhaust...CLEAR- Navigation light.CONDITION

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- Fire extinguishing overpressure indication (red disc)..................IN PLACE- Check APU area for obvious damage and evidence of fluid leakage, doors closed,fire extinguisher overpressure discharge indicator (red disc) in place and Air intakeflap closed- Check Elevators & rudders (cracks, corrosion, dents, delamination)- Check Evidence of elevator and rudder servo actuator for hydraulic leaks

LH AFT FUSELAGE- Stabilizer, elevator, fin and rudder.CONDITION- Portable water service panel...CLOSED

LH L/G AND FUSELAGE

- Chocks.....REMOVED- Wheels and tires..CONDITION- Brakes and brake wear indicator...CONDITION- Hydraulic lines...CHECK- L/G structure..CHECK- Downlock springCHECK- Safety pin.REMOVED

- Check if there is any indication of wear, chaffing lines, chaffing wires, cracks, dents,or other damage- Check structural of gear doors for condition (cracks, dents or other damage)- Hydraulic leaks (gear struts, actuators, steering valves etc)- Check Wheel cab and fan cover for condition and secure

- War, line security, leaks and installation of brakes- Corrosion- Check shock struts for correct extension. Clean and apply fluid 41 if required.- Check proximity detectors and taxi lights for security and cleanliness.- Check brakes for wear and overheating. (Ref. AMM 324227/6).

At Hangar ONLY: (If the heat pack wear indicator PIN is less than 2mm,Remove the Brake and send for O/H)

Note: check each heat pack wear indicator (with barking pressure applied) andcircle Yes or NO in the below table.

Brake Pins

No. 1 No. 2 No. 3 No. 4within limit within limit within limit within limit

Yes No Yes No Yes No Yes No

- Check wheels for rim damage, sheared / missing tie-bolt and tire for wear cuts,bulges and flat spots.- Check tire pressure values in relation to the aircraft weight (MRW) and tire sizes asper the tables available in the AMM Ref. 32-41-00/601

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Tire checked: Hot [ ] Cold [ ]

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LH RH 1 2 3 4

LH WING TRAILING EDGE- Flaps and fairing...CONDITION- Control surfaces...CONDITION- Static dischargers.CHECKMissing static discharge eliminators (number missing in accordance with MEL/CDL

LH WING TIP- Navigation light.CONDITION- Slats ..CONDITION- Surge tank air inlet....CLEAR- Fuel water drain valve (surge tank)...NO LEAK- Magnetic fuel levels ....FLUSH- Wing fence....CONDITION- Fuel ventilation overpressure disc.INTACT

LH WING LEADING EDGE- Magnetic fuel levels ....FLUSH- Fuel water drain valve (outer tank)...NO LEAK- Slats .....CONDITION

- Refuel coupling door.CLOSED

ENG 1 LH SIDE- Engine Oil fill access door...................CLOSED- Master Magnetic chip detector access door...CLOSED- Thrust reversers cowl door......CLOSED- Pressure relief doors.CLOSED- Fan cowl door..CLOSED/LATCHED- Drain masts....CONDITION/NO LEAK- Access door to reversers latches....CLOSED- Engine inlet and fan blades.CHECK

ENG 1 RH SIDE

- Fan Cowl door.CLOSED/LATCHED- Thrust reverser cowl door.CLOSED- Access to starter valve manual override....CLOSED- Pressure relief doorCLOSED- Turbine exhaust....CLEAR

-Check engine oil quantity on ECAM lower display Engine page within 5 minutesafter engine shut-down as per AMM ref. 12-13-79.

If indication is below minimum, check engine oil level at sight glass, and serviceengine oil as required with ESSO 2380 (Accomplish step 2 prior to servicing).Recorded quantity added in Log Book and below make sure that filler caps are

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properly installed after servicing).ENG. NO. 1 -----------------------------------------

ENG. NO. 2 -----------------------------------------

-Prior to servicing, perform SNIFF / SMELL check for evidence of fuel contamination.Check IDG low oil level (within green range) and carry out complete servicing if low.-Check cowlings and Pylons for damage and evidence of fuel, oil and hydraulicleakage.-Inspect visually stage 4 blades for unlatching and shingling.(FOR CFM EnginesONLY)-Fan thrust reverser door latches for proper closing (red indicator and protruding)Access doors and over pressure doors in place, closed and secured.

-Check fan blades and spinner (free rotation by hand).-Check nose cowl, fan reverser and turbine nozzle for damage loose or missingrivets.-Check last stage LPT blades as visible with a flashlight for obvious damage andmetal deposit.-Ensure hydraulic hand pump, used to open and close the thrust reverser cowls, isstowed on board of A/C.-Inspect the Intakes for fan blade damage and oil leaks-Inspect the air intake for security and proper fit-Inspect the cowling doors for security and proper fit-Inspect the lower cowling security and evidence of fluid leaks-Inspect the exhaust for turbine and tailpipe damage and evidence of fluids-Inspect the reverser doors for stowage and security, evidence of fluids

LH CENTER WING- Inner tank magnetic fuel levels ......................................................FLUSH- Fuel water drain valves (inner tank)...NO LEAK- Water drain valve panel...,,,..CLOSED- Landing light..CONDITION- Slat ...,,,..CONDITION- RAT air inlet flap......CONDITION- RAT door.....CLOSED

D. FUSELAGE EXTERIOR CHECK ITEMSInspect the following1. Check fuselage, skin, service panels, doors, windows, antennas and fairings for

obvious and evidence of fluid leakage and exterior light for cleanliness.2. Clean exterior of A/C if required.3. Structure for cracks, corrosion, dents, or other damage4. Fasteners (loose, improper, missing)5. Lavatory servicing areas (evidence of blue water streaks)6. Cargo compartments for condition7. Emergency exit identification / marking (two inch contrasting borders out lining

exits)8. Registration marking (match airworthiness and registration certificates)9. All lights (general condition, broken lenses etc)

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E. WING AND PYLONS CHECK ITEMS

CHECK THE FOLLOWING

1. Check L.E ventilation and surge tank air intake for condition.2. Check lower wings surface and upper wings surface (through cabin windows) for

general condition and evidence of fuel leaking.3. Structure for cracks, corrosion, dents, or other damage4. Leading edge (dents and/or damage in line with engine inlets)5. Leading edge devices (when open for actuator leaks, general condition of line,

wires, and plumbing)6. Evidence of fuel leaks (if found, maintenance must prove leak is within limits)7. all lights (general condition, broken lenses, etc)8. flaps (cracks, corrosion, dents and delamination)9. Flap fairings (general condition of lines, wires, and plumbing)

10. static eliminators (number missing in accordance with MEL/CDL)11. Ailerons (cracks, corrosion, dents, delamination)12. Missing, loose, or improperly secured access door/inspection panels and blow

out panels

F. COCKPIT / CREW CHECK ITEMS

1. Clean cockpit and passenger cabin, toilets, galleys and empty ashtrays andcheck carefully waste bins for condition and closing flaps for proper operation.

2. Check pressure of portable oxygen cylinders fully charged in green band.3. Check cockpit emergency equipment including crash axe for presence and

proper stowage.4. Check all onboard PBE s for conditions & serviceability

5. Visual check of windshield outer seal6. Check cockpit windshield and windows for damage.a. Detailed Visual Inspection of All Cockpit Windows from Outside as

per AMM. 56-10-00-200-005.b. Inspection of the Windshields as per AMM. 56-11-11-200-001 ,

Delamination: (Ref. to Fig. 604/TASK 56-11-11-991-008 SHEET 604.1)Bubbles : (Ref. to Fig. 606/TASK 56-11-11-991-010 SHEET 606.1)

G. Fuelling (if applicable)

Fuelling of Aircraft to check the following

1. Refueling pressure2. Condition of refueling units (leaks, filter change dates, exhaust system . Etc)3. Ground connections and procedure4. Fire Protection5. General fuelling procedure

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H. POST SERVICE ITEMS

1. Drain A/C potable water system, when required fill prior to departure (winteroperation, or when A/C is on ground for more than 48 hours).

2. Ensure toilets are serviced as required.3. Drain water from all fuel tanks at water drain valves, check for contamination of

fuel from water and foreign matters as judged by color (Ref. to applicableAMM12-32-28/3). After drainage ensure drain valves are properly seated andnot leaking. (Ref. AMM 12-32-28/3).

4. Ensure refuel coupling caps are in place and secure.5. Ensure dipsticks are retracted and secured.6. Ensure serviceable spare tires are on board the A/C7. Ensure all cabin doors, cargo compartment doors and service panels are

properly closed and secured.

I. Make sure that all service panels bonding wires are available and in good condition

J. Make sure that all oil service panels are closed and secured (Tap the panel by hand to

make sue it is closed)

Make sure that the AVIONICS TRANSIT MP Form # A320-B (latest issue) isSigned and attach the signed copy with this Transit check.

Make sure that the CABIN GENERAL AVIONICS TRANSIT MP Form #A320-C (latest issue) is Signed and attach the signed copy with this Transit

check

Make sure that the FLEET CABIN MECH. MP Form # 061-ALL (latest issue )

is Signed and attach the signed copy with this Transit check Make sure that the SECURITY CHECK LIST MP form SCL100 is Signed

before A/C Departure (at LM only) and attach the signed copy with this Transit

check

ICING CONDITIONIn Cold weather condition: Check that the A/C is free from ice deposits, frost,

snow, slush (wing, control surfaces, vertical & horizontal stabilizer and rudders)

Plan an eventual de-icing. Remove deposits from engine Air Intakes.

CARRY OUT ITEM 1 & 2 IF REQUIRED I.A.W RJ FORM NO. MP/144 latest issue

WORK ACCOMPLISHMENT

Raise a DISCREPANCY SHEET or a LOG BOOK Maintenance entry for alldiscrepancies found during TRANSIT AVIONICS and CABIN TRANSIT ITEMSreviewed.

B DEFECTS reviewed

B DEFECTS cleared

B DEFECTS entered

Above WORK ITEMS A TO J satisfactory accomplished.

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