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SWI-747-LSHM, Rev 0 Date 02/09/2014

LINE STATION HANDLING MANUAL

SWI-747-LSHM

REVISION

5

DATE

8 Oct 2018

LINE STATION HANDLING MANUAL N°: SWI-747-LSHM Rev: 5 Date: 8 OCT 18


Table of Contents

1. CONTENTS ........................................................................................................................................... 5

1.1. Aircraft data operated by SWI............................................................................................................ 5

1.2. List of abbreviation ............................................................................................................................. 5

1.3. Contact List (CL) ................................................................................................................................ 7

2. LINE MAINTENANCE ACTIVITY .......................................................................................................... 8

2.1. Walk Around Inspection (No CRS is Required) ................................................................................. 8

2.2. CMR 1 & 2 ......................................................................................................................................... 8

2.3. Main Base Check (MBC) ................................................................................................................... 8

2.4. Control of Refueling Quantity/Quality ................................................................................................ 9

2.5. Replenishing of Oils and Fluids ......................................................................................................... 9

2.6. Security and Sealing .......................................................................................................................... 9

2.7. Defect Management .......................................................................................................................... 9

Defect Management where CLX AMO is available ..................................................................... 10

Defect Management where CLX AMO is not available ............................................................... 11

2.8. Minimum Equipment List (MEL)....................................................................................................... 11

Notify Dispatch ............................................................................................................................. 12

MEL Deferred Defect Overrun (Cat B and C only). ..................................................................... 12

Non- Safety Related Equipment (NRE) ....................................................................................... 12

2.9. Mandatory Occurrence Report (MOR) ............................................................................................ 12

2.10. Certificate of Release to Service (CRS) .......................................................................................... 12

Fan Cowl Door Loss Prevention (Ref EASA SIB 2015-15) ..................................................... 12

Duplicate Inspection Policy ...................................................................................................... 13

2.11. Distribution of Maintenance Records ............................................................................................... 13

CLX AMO ................................................................................................................................. 13

Non CLX AMO ......................................................................................................................... 13

3. AIRCRAFT TECHNICAL LOG SYSTEM (ATL) ................................................................................... 14

3.1. Aircraft Technical Log (ATL) Pad .................................................................................................... 14

Aircraft Technical Log filling instructions ..................................................................................... 14

ATL Handling Instructions ............................................................................................................ 14

3.2. Deferred Defects (DMI & DBC) ....................................................................................................... 15

Deferred Maintenance Items (DMI) List ....................................................................................... 15



Deferred Maintenance Item List Handling & Filling instructions .................................................. 16

Dent and Buckle Chart (DBC) ...................................................................................................... 16

3.3. Notice to Crew (NTC) ...................................................................................................................... 16

Notice to Crew Handling & Filling instructions ............................................................................. 17

3.4. Maintenance Support Information (MSI) .......................................................................................... 17

4. PROVISION AND ACCEPTANCE OF COMPONENTS ..................................................................... 17

4.1. Supply of Parts ................................................................................................................................ 17

4.2. Acceptance of Components............................................................................................................. 17

4.3. Swapping policy ............................................................................................................................... 18

5. TECHNICAL DELAY ............................................................................................................................ 18

5.1. CLX AMO ......................................................................................................................................... 18

5.2. Non CLX AMO ................................................................................................................................. 18

6. TECHNICAL LIBRARY ........................................................................................................................ 18

6.1. Documentation On Board ................................................................................................................ 18

6.2. Digital Library ................................................................................................................................... 18

CLX AMO ..................................................................................................................................... 18

Non CLX AMO ............................................................................................................................. 18

7. SUBCONTRACTING ........................................................................................................................... 19

8. COMPLIANCE MONITORING............................................................................................................. 19

9. TRAINING SERVICE ........................................................................................................................... 19

ATTACHMENTS

Attachment 1 B747-400F Walk Around Inspection 20

Attachment 2 Course Register Form (SWI-CAMO-018B) 26



1. CONTENTS

This document provides information and technical procedures for the handling and maintenance services of

SW Italia aircraft by the contracted Approved Maintenance Organizations (AMO) at SWI Outstations.

These procedures are in accordance with the procedures of SWI CAME and must be performed by contracted

AMO qualified by SWI Compliance Monitoring System.

This manual is an integral part of the Standard Ground Handling Agreement and its content must be known to

the technical personnel who provide the line maintenance service. It is SWI responsibility to provide procedure

training to all contracted AMO.

1.1. Aircraft data operated by SWI

All aircraft operated by SWI are B747-400F.

A/C Registration MSN Line

Number

Aircraft

Model Engine Type APU Type

I-SWIA 29729 1189 B747-400F RR211-524H2-T19 P&W 901A

1.2. List of abbreviation

A/C Aircraft

ACARS Aircraft Communications Addressing and Reporting System

AD Airworthiness Directives

AMM Aircraft Maintenance Manual

AMO Approved Maintenance Organization

AOG Aircraft On Ground

APU Auxiliary Power Unit

ATA Air Transport Association

ATL Aircraft Technical Log

CAME Continuing Airworthiness Management Exposition

CAMO Continuing Airworthiness Management Organization

CAS Continuing Airworthiness Surveillance

CDL Configuration Deviation List

CL Contact List

CLX Cargolux

CM Compliance Monitoring

CMM Compliance Monitoring Manager

CMR Certified Maintenance Requirement

CRS Certificate of Release to Service

CS Certifying Staff

DBC Dents and Buckles Chart

DMI Deferred Maintenance Item

EASA European Aviation Safety Agency

EC Engineering Control

EDR Engineering Data Record



EICAS Engine Indicating and Crew Alerting System

EM Engineering Manual

ENAC Ente Nazionale Aviazione Civile (Italian National Aviation Authority)

EP Engineering Procedure

FAK Fly Away Kit

FIM Fault Isolation Manual

GYD Baku (Azerbaijan)

I.A.W. In accordance with

IPC Illustrated Parts Catalog

LCH Line Check Handbook

LLP Life Limited Parts

LRU Line Replaceable Unit

LSHM Line Station Handling Manual

LUX Luxembourg (Luxembourg)

MAREP Maintenance Report

MCC Maintenance Control Center

MBC Main Base Check

MEL Minimum Equipment List

MOR Mandatory Occurrence Report

MPD Maintenance Planning Document

MSI Maintenance Support Information

MXP Malpensa (Italy)

NRE Non-safety Related Equipment

NTC Notice to Crew

OCC Operation Control Center

OEM Original Equipment Manufacturer

PCA SWI CAMO Post Holder

PLR SWI Planning and Records

P/N Part Number

PIREP Pilot Report

QA Quality Assurance

SGHA Standard Ground Handling Agreement

S/N Serial Number

SRM Structural Repair Manual

SW Silk Way

SWI SW Italia

SWPM Standard Wiring Practice Manual

TRAX Airline specific MRO computer software in use with M&E Division to manage the continuing

airworthiness of the fleet and maintenance tasks performed by the AMO.

UTC Universal Time Coordinated



1.3. Contact List (CL)

SW Italia has subcontracted the maintenance services to Cargolux Airlines international S.A.

In case maintenance support is required, please call CLX MCC Maintenance Control Center (24 hours service)

(Ref. to CL No.1).

CL

No. Department & Name Phone Number Fax Mobile E-mail Sita

Cargolux International - LUX

1 CLX Maintenance

Control Center

(CLX MCC)

+352 42113270 +352 42113424 +352 621458225 [email protected]

[email protected]

LUX

MMCV

2 CLX CAMO Technical

Records Department

+352 4211 3672 [email protected]

3 Reserved

SW Italia - MXP

4 SWI Planning &

Record Department

(SWI PLR)

Andrea Mor

+39 0331 1605743 +39 0331 231398 [email protected]

5 SWI CAMO PH

(SWI PCA)

Stefano Bonifacio

+39 0331 1605742 +39 0331 231398 +39 344 0037180 [email protected]

6 Deputy SWI CAMO PH

(SWI ESP)

Luca Cortesi

+39 0331 1605741 +39 0331 231398 +39 345 4327974 [email protected]

7 SWI Compliance

Monitoring Manager

(SWI CMM)

Paolo Rosberti

+39 0331 1605749 +39 0331 231398 [email protected]

8 SWI Safety Manager

(SWI SM)

Paolo Rosberti

+39 0331 1605749 +39 0331 231398 [email protected]

mailto:[email protected]








2. LINE MAINTENANCE ACTIVITY

The contracted AMOs must perform the following maintenance activities according to the scope of work of the

relevant signed SGHA.

2.1. Walk Around Inspection (No CRS is Required)

The Walk Around Inspection is performed to inspect condition of airframe, engines, landing gear, wheels,

brakes, etc. and to debrief the flight crew about the status of the aircraft. This activity is carried out in support

to the Pre-Flight Inspection performed by the flight crew.

For current Walk Around Inspection instructions ref. to "Attachment 1” of this manual.

The Green ATL copy of the inbound flight shall be always removed from the pad by local AMO before aircraft

departure and sent to the addresses defined in the ATL handling instructions (even in case no maintenance

actions have been performed).

2.2. CMR 1 & 2

CMR 1 & 2 are carried out by CLX AMO prior to each departure from Main Base and they are valid for 24

hours elapsed time from accomplishment. If CMR 1 & 2 are expired or are going to expire during subsequent

flight, they must be accomplished by contracted AMO before departure.

CMR 1 & 2 accomplishment must be recorded by signing the dedicated box in the Aircraft Technical Log (ATL)

page.

NOTE. Since CMR 1 & 2 are part of the Main Base Check, signature of the MBC box in the Aircraft

Technical Log (ATL) page also states accomplishment of CMR 1 & 2.

For current CMR 1 & 2 accomplishment instructions, refer to "Line Check Handbook” latest revision, available

on board and in the digital library (ref para 6).

CLX MCC monitors the daily aircraft operation versus the CMR requirements. In case a CMR becomes due at

any outstation, CLX MCC advises the respective outstation accordingly.

In case of Flight Mechanic onboard unable to inform CLX MCC, the Flight Mechanic monitors the MBC

requirements.

2.3. Main Base Check (MBC)

Main Base Check (MBC) is carried out by CLX AMO prior to each departure from Main Base and is valid for

72 hours elapsed time commencing from first “OFF BLOCKS” after accomplishment or 24 hours elapsed time

after accomplishment if the aircraft remains on ground. If MBC is expired or is going to expire during

subsequent flight, it must be accomplished by contracted AMO before departure.

MBC accomplishment must be recorded by signing the dedicated box in the Aircraft Technical Log (ATL) page.

For current MBC accomplishment instructions, refer to "Line Check Handbook” latest revision, available on

board and in the digital library (ref para 6).

CLX MCC monitors the daily airplane operation vs the MBC requirement. In case a MBC becomes due at any

outstation, CLX MCC advises the respective outstation accordingly.



In case of Flight Mechanic onboard unable to inform CLX MCC, the Flight Mechanic monitors the MBC

requirements.

2.4. Control of Refueling Quantity/Quality

The control of refueling quantity/quality is responsibility of the commander. Fuel procedures shall be carried

out by the fuel handler.

Refueling must be performed according to methods provided by the Aircraft Maintenance Manual.

AMO CS shall fill the Fueling Record Form (Form CAMO SWI-CAMO-023), available on board (ref para 6) and

provide it to the commander.

AMO CS shall also ensure that:

the product is free from water and/or other particles;

the product description, which is also specified on the Delivery Certificate, is consistent with company

requirements;

the aircraft is refueled with quantity of product required for the intended flight.

2.5. Replenishing of Oils and Fluids

The oils and fluids servicing shall be carry out i.a.w. the Aircraft Maintenance Manual using oils and fluids listed

in the SWI Engineering Procedure EP-747-12-002, available on board and in the digital library (ref para 6).

2.6. Security and Sealing

For Security and Sealing procedure of unattended aircraft refer to the following:

SWI Engineering Procedure EP-747-12-003 for operations to/from USA locations (USA airports or

non-USA airports serving as last point of departure to USA).

This procedure due to its restricted distribution is only available in the digital library to those stations

who need to know.

SWI Engineering Procedure EP-747-12-001 for all other operations.

This procedure is available on board and in the digital library (ref para 6).

Once sealing procedure is carried out in accordance to one of the above documents, the Form SWI-CAMO-

015 “B747-400F UNATTENDED AIRCRAFT SECURITY CHECKLIST” must be filled, original must be retained

at the station for 30 days and scanned copy must be sent as specified in the procedure to

[email protected] and to [email protected].

2.7. Defect Management

Defects on A/C can result from pilot reports and from the execution of line maintenance tasks.

A defect can be fixed (F) or deferred (D).

When a defect shall be deferred, contracted AMO shall defer the defect according to the applicable approved

maintenance data (MEL/CDL, SRM, other approved document) by filling the Aircraft Technical Log (ATL)

“Action taken” field with a full description of the action performed against the corresponding pilot or

maintenance report and transcribing the relevant approved data reference (MEL item, SRM/AMM paragraph,

etc.).





Deferred Maintenance Item (DMI) list and/or Dents and Buckles Chart (DBC) shall be updated accordingly.

Contracted AMO will inform CLX MCC (Ref. to CL No.1) and SWI PLR (Ref. to CL No.4) about any deferred

defects upon aircraft departure sending maintenance message (CLX AMO) or scanned copy of green ATL

page (Non CLX AMO) according para 2.11.

NOTE: Upon availability of the data, each deferred defect shall be entered into TRAX system by CLX

Maintenance upon return of the aircraft to the Main Base.

Defect Management where CLX AMO is available

If a defect, which does not allow the pursuance of the flight, arises at a destination away from SWI Main Base

where CLX AMO is available, the following procedure shall apply:



Defect Management where CLX AMO is not available

If a defect which does not allow the pursuance of the flight arises at a destination away from SWI main base

where an Approved Part 145 different from CLX AMO is available, the following procedure shall apply:

2.8. Minimum Equipment List (MEL)

The Minimum Equipment List (MEL) is the SW Italia document that lists the equipment that may be temporarily

inoperative, subject to certain conditions, at the commencement of flight.

Copy of latest revision of SWI MEL is available on board and in the digital library (ref para 6).



Notify Dispatch

When an MEL item affects normal operation of the aircraft, it is necessary to notify SW dispatch about such

limitation by sending a message to [email protected] copy to [email protected] with reference to MEL

item involved.

MEL Deferred Defect Overrun (Cat B and C only).

If due to technical or operational reasons, rectification of the defect having interval category B and C is not

possible within the given interval, one time extension can be granted by SWI Postholder for Continuing

Airworthiness (PCA), or Continuing Airworthiness Surveillance responsible (CAS) by means of a Concession.

Copy of the concession is forwarded to contracted AMO to make a dedicated entry into the ATL and to update

the DMI list.

Non- Safety Related Equipment (NRE)

NRE includes those items related to the convenience, comfort, or entertainment of the personnel and

equipment that is used only on ground for maintenance purpose.

Items deferred as NRE are released under MEL Item 25-20-01 Non-Safety Related Equipment (NRE) with

Rectification Interval Category “D”.

For the complete list of NRE, refer to SWI MEL Section 4 – Non-Safety Related Equipment.

2.9. Mandatory Occurrence Report (MOR)

Contracted AMO must notify SWI SM (Ref. to CL No.8) through its own report, about any condition of the

aircraft or component identified by the organization that has resulted, or may result, in an unsafe condition that

hazards seriously the flight safety as per Part 145.A.60 requirements.

2.10. Certificate of Release to Service (CRS)

After any line maintenance activities, performed in accordance with approved data and procedures, the CRS

should be entered by a duly authorized Certifying Staff on the Aircraft Technical Log (ATL).

Without having been trained on the SWI procedures, no Certifying Staff can issue a CRS on the SWI ATL.

The CRS of the work shall be signed off in the ATL by a Certifying Staff, as long as this person has ensured

that:

The defect has been fixed or deferred by clearly and completely quoting the relevant maintenance data,

including MEL and AMM reference when applicable;

Works carried-out are not in conflict with any special procedure relevant to special operations (i.e. CAT

III, etc.);

Critical tasks requiring duplicate inspection (ref para 2.10.2) have been considered and performed;

Task has been performed by the appropriate personnel (within the capability of his Certification

Authorization);

Fan Cowl Door Loss Prevention (Ref EASA SIB 2015-15)

Please make a dedicated ATL entry every time maintenance actions involving the opening/closing, removal

and re-installation, or replacement of a fan cowl door is performed on SW Italia fleet.





Such entries will bring to the attention of the flight crew of the affected airplane that maintenance action has

been performed on engine fan cowls and will improve flight crew awareness to verify proper closure of the

affected door(s) during the pre-flight exterior walk-around.

Duplicate Inspection Policy

SW Italia Duplicate Inspection Policy is detailed in the Engineering Procedure EP-747-00-003 Duplicate

inspection policy, available on board and in the digital library (ref para 6).

In case the duplicated inspection policy of SWI Contracted Maintenance Organization is different from SWI

policy, the most limiting policy applies.

Risk of Multiple Errors

SWI policy regarding the risk of multiple errors and risk of errors repeated in identical maintenance tasks is

included in Engineering Procedure EP-747-00-004 Procedure to minimize risk of multiple errors, available on

board and in the digital library (ref para 6).

In case the policy of SWI Contracted Maintenance Organization is different from SWI policy, the most limiting

policy applies.

2.11. Distribution of Maintenance Records

CLX AMO

After each departure from a CLX station, the following apply:

an aircraft maintenance message as per CLX FSTHM is send to CLX MCC (Ref. to CL No.1) and SWI

PLR (Ref. to CL No.4);

green copy of ATL page of inbound flight, fuel form and components serviceable tags (if any) are always

scanned by the CLX AMO and electronically sent to CLX CAMO Technical Records Department (Ref. to

CL No.2), CLX MCC (Ref. to CL No.1) and SWI PLR (Ref. to CL No.4);

in exceptional cases when a work order is performed, the completed work order is scanned by the CLX

AMO and electronically sent, together with the green copy of ATL page, to CLX CAMO Technical Records

Department (Ref. to CL No.2), CLX MCC (Ref. to CL No.1) and SWI PLR (Ref. to CL No.4).

Non CLX AMO

After each departure from a Non CLX station, the following apply:

green copy of ATL page of inbound flight, fuel form and components serviceable tags (if any) are always

scanned by the contracted AMO and electronically sent to CLX CAMO Technical Records Department

(Ref. to CL No.2), CLX MCC (Ref. to CL No.1) and SWI PLR (Ref. to CL No.4);

in exceptional cases when a work order is performed, the completed work order is scanned by the

contracted AMO and electronically sent, together with the green copy of ATL page, to CLX CAMO

Technical Records Department (Ref. to CL No.2), CLX MCC (Ref. to CL No.1) and SWI PLR (Ref. to CL

No.4).



3. AIRCRAFT TECHNICAL LOG SYSTEM (ATL)

The SWI Aircraft Technical Log (ATL) is a system for recording flight activity, defects and malfunctions during

the aircraft operation and for recording details of all maintenance carried out on an aircraft. In addition, it is

used for recording flight safety and maintenance information the operating crew need to know.

The Aircraft Technical Log (ATL) System of the SWI, as described in the following chart, is a combination of

computer system and paper.

NOTE: The four paper parts are contained in a single folder on board of the aircraft.

3.1. Aircraft Technical Log (ATL) Pad

The ATL Pad constitutes the core of the ATL System. It is the mean to report all flight data necessary for the

technical management of the aircraft, to record the accomplishment of maintenance actions and relevant CRS

both for scheduled and unscheduled maintenance and to record the commander’s acceptance of the aircraft

for the intended flight.

Aircraft Technical Log filling instructions

See inside cover of ATL Pad available on board (ref para 6).

ATL Handling Instructions

1) The ATL is composed by the cover page (SWI-CAMO-001A Form), the handling/filling instructions (SWI-

CAMO-001B Form) and 50 pages (SWI-CAMO-001C Form) sequentially identified (see item 2).

2) Each page of any ATL is pre-printed with a six digits sequential and univocal page number. ATL pads will

not be numbered and can be used regardless of the sequence of the page numbers between two pads.

3) Each page is reproduced in four (4) coloured copies:

a. White copy: is the original one and must remain always in the pad. Removal of the original white

copy from the pad is not allowed for whatever reason.

b. Pink copy: is managed by CLX AMO at main base and it is used to update the aircraft maintenance

record system. At main base, at every Main Base Check, CLX AMO removes all the

pink pages since previous Main Base Check performed at Main Base, scans and sends

them to CLX CAMO Technical Records Department (Ref. to CL No.2) and SWI PLR

(Ref. to CL No.4). Original pink pages are sent to CLX CAMO Technical Records (Ref.

to CL No.2) for review and filing.

AIRCRAFT TECHNICAL LOG (ATL) SYSTEM

TRAX

(Computer)

AIRCRAFT TECHNICAL

LOG PAD

(Paper)

DEFERRED DEFECTS

(DMI & DBC) (Paper)

MAINTENANCE SUPPORT

INFORMATION

(Paper)

NOTICE TO CREW

(Paper)



c. Green copy: is for the local contracted AMOs which are responsible to remove it before aircraft

departure and to archive it in accordance with their own procedures. Local AMOs, as

soon after aircraft departure, scans and sends removed page to Cargolux CAMO

Technical Records (Ref. to CL No.2), Cargolux MCC (Ref. to CL No.1) and SW Italia

Planning & Records (Ref. to CL No.4).

d. Yellow copy: is for the handling company. It is removed before aircraft departure and given by the

Flight Crew to the Handling Company which is responsible to archive it in accordance

with its own procedures.

4) Three pads should be always present on board, the previous completed, the actual in use and one blank

as spare. A new pad shall be put on board as soon as the spare one is used.

5) Each new ATL pad is initiated by SWI PLR by stamping on the cover page the aircraft registration marks.

6) Before distribution to AMO Main Base, each ATL pad must be registered by SWI PLR in the ATL Pad

electronic register.

7) ATL pad cover page to be filled by the person (maintenance staff or commander) beginning the new ATL

pad. Fill with the date from which the pad is in use (field “FROM DATE”), the date till the pad was in use

(field “TO DATE”), the number of the last page of the previous ATL pad (field “LAST PAGE No. OF

PREVIOUS ATL PAD”) and the number of the first page of the subsequent ATL pad (field “FIRST PAGE

No. OF SUBSEQUENT ATL PAD”).

8) A completed pad must remain on board until the subsequent pad is in use, then shall be removed and

sent to SWI PLR to be archived.

9) If, for whatever reason, a pad has to be definitely removed before its full completion, all blank pages must

be crossed by the person involved (Maintenance Staff or Flight Crew).

3.2. Deferred Defects (DMI & DBC)

All defects or malfunctions deferred during aircraft operation must be reported in the ATL.

SWI policy is to rectify defects as soon as possible before A/C dispatch and within the available ground time.

However, aircraft allowable defects, which cannot be fixed for whatever reason before A/C departure, may be

temporarily deferred according maintenance data such as MEL, CDL, AMM or SRM.

Deferred Defects must be reported in the Deferred Maintenance Items (DMI) List or in the Dents and Buckles

Chart (DBC).

As a general rule, defects that could affect the conduct and/or the operation of the flight shall be reported in

the DMI List while structural damages shall be reported in the DBC.

Before entering a new defect in the ATL, it is mandatory to check first the content of DMI and DBC in order to

verify if such defect has already been recorded and it is under control.

Deferred Maintenance Items (DMI) List

The primary intent of the DMI list is to provide the commander in accepting the aircraft, with a concise and

complete summary of all deferred defect that could affect the conduct and/or the operation of the flight. In no

way an aircraft can be accepted for flight with defects expired.



The DMI List is used for whichever type of deferred defect that has been opened in the ATL; in no way the

DMI List may be used to report different information from those already recorded in the ATL. Each Deferred

Maintenance Item (DMI) is univocally identified by an univocal DMI number.

The DMI List must be always present in the ATL System folder. Each DMI List document contains a maximum

of eight items. At aircraft main maintenance base, when convenient or when available empty lines are not

sufficient for new entries, the DMI List shall be closed and a new one shall be initiated. When opening a new

List, all items still open must be transferred to the new document keeping their original numbers.

The deferment, the extension or the closure of each item must be first entered in the ATL then reported in the

DMI List. In no way the DMI List can be used as record of the CRS.

When a DMI List is closed, it shall be removed from the ATL system folder at Main Base and delivered to CLX

CAMO Technical Records Department (Ref. to CL No.2).

Deferred Maintenance Item List Handling & Filling instructions

For handling and filling instructions, see back side of DMI form.

Dent and Buckle Chart (DBC)

The Dent and Buckle Chart (DBC) provides the commander in accepting the A/C or the line maintenance staff

in performing line inspections to the aircraft, with a view of all structural damages on the whole aircraft,

including engine cowls and engine blades. The DBC is supplementary to the entries made into the ATL for the

same damages and provides additional detailed information of the structural damage.

The primary intent of the DBC is to avoid duplication of ATL entries for the same damage, probably leading to

unnecessary maintenance actions and/or departure delays due to damage assessment. The DBC must be

always present in the ATL System folder.

Prominently visible dents, chafe marks, damaged engine acoustic liners etc, on airplane / powerplant that have

been previously assessed, either as within limits or carried over for later repair, are identified by a EDR sticker

applied in the vicinity of the damage. This is to easily identify that the Engineering Data Record (EDR) for this

damage can be found in the flight deck library.

The mere presence of a sticker in the vicinity of a visible damage is not a sufficient damage disposition. EDR

for the damage needs to be filed in the flight deck library to be accessible to any Inspector.

When the damage is repaired, and is no longer prominently visible as un-repaired damage, the EDR from the

flight deck library and the sticker on the airframe / powerplant is removed by CLX AMO.

New defects must be first entered in the ATL then reported in the DBC. In no way the DBC can be used as

record of the CRS.

3.3. Notice to Crew (NTC)

The primary intent of the NTC List is to inform the commander, in accepting the aircraft, with notices concerning

technical aspects. It may be also used to require the commander to perform some specific actions to be

reported in the Aircraft Technical Log (ATL).



The NTC List must be always present in the ATL System folder. Each NTC List document contains a maximum

of ten items. On aircraft main maintenance base, when convenient or when available empty lines are not

sufficient for new entries, the NTC List shall be closed and a new one shall be initiated. When opening a new

List, all notices still open must be transferred to the new document.

When a NTC List is closed it must be removed from the ATL system folder and delivered to CLX CAMO

Technical Records Department (Ref. to CL No.2).

Notice to Crew Handling & Filling instructions

For handling and filling instructions, see back side of NTC form.

3.4. Maintenance Support Information (MSI)

The Maintenance Support Information list contains any necessary maintenance support information that the

aircraft commander needs to know. Such information would include data on how to contact Approved

Maintenance Organization if problems arise at main maintenance base or at the outstations.

4. PROVISION AND ACCEPTANCE OF COMPONENTS

4.1. Supply of Parts

SWI has the Pool Parts Arrangement with Cargolux Airlines international S.A.

CLX MCC must be contacted for the supply of any component (Ref. to CL No.1).

NOTE: Two spare wheels, an axle jack and a Flight Away Kit (FAK) are available in the bulk cargo.

For the FAK management instruction and content list refer to “Fly-Away-Kit List B747-400F”

available in the ATL folder.

Each contracted AMO is responsible to supply standard consumables and expendables (C&E) material for

requested maintenance and/or defect rectification.

4.2. Acceptance of Components

A component, which has to be fitted on SWI aircraft, must be in compliance with the applicable EASA PART

145 requirements. This requires that all parts are in satisfactory condition and provided with appropriate

documentation.

Prior to installation of a component the organization shall ensure that the particular component is eligible

(checking the EASA form 1 or equivalent) to be fitted when different modification and/or airworthiness directive

standard may be applicable.

The EASA form 1 or equivalent identifies the status of the component.

Particular attention must be done to the block 12 (remarks) for vital airworthiness information.

When a component has not an appropriate release certificate, it is permissible to temporarily fit a component

without the appropriate release certificate for a maximum of 30 (thirty) flight hours or until the aircraft first

returns to the main base, whichever is the sooner, subject to the component having a suitable release

certificate but otherwise in compliance with all applicable maintenance and operational requirements.



4.3. Swapping policy

SWI policy concerning swapping of components is included in Engineering Procedure EP-747-00-002

Swapping policy, available on board and in the digital library (ref para 6).

5. TECHNICAL DELAY

To monitor technical performance of SWI fleet it is necessary to report each technical delay or cancellation.

5.1. CLX AMO

CLX AMO communicates with CLX reliability through the CLX internal system and to SWI with aircraft

maintenance message as per para 2.11.

5.2. Non CLX AMO

Non CLX AMO fills and sends by mail or fax to SWI PLR (Ref. to CL No.4) the SWI Technical Delay Report

Form (SWI-CAMO-017) available on board and in the digital library (ref para 6).

6. TECHNICAL LIBRARY

6.1. Documentation On Board

Latest revision of maintenance data and continuing airworthiness documentation required for management of

SWI fleet is available on board. Part of the documentation is located in the flight deck and part is located in the

personnel accommodation compartment stowage.

For the list and location of the documentation on board please refer to Engineering Procedure EP-747-00-001

filed in the documentation folder in the personnel accommodation compartment stowage.

6.2. Digital Library

CLX AMO


SWI fleet is provided by SWI Library to CLX Technical Library who is therefore responsible for distribution.

Non CLX AMO


SWI fleet is available through the SWI Library accessible via internet connection (http://extranet.switalia.eu).

SWI provides each outstation with the necessary information to get access to the library through FORM SWI-

CAMO-019.

Once connection is successfully established, signed copy of FORM SWI-CAMO-019 is returned to SW Italia

to confirm successful access.

No notification of new revision is provided by SW Italia, each outstation is responsible to use only the revision

available online.

http://extranet.switalia.eu/



7. SUBCONTRACTING

The contracted AMO cannot subcontract tasks to a third party (whether this third party is Part-145 approved

or not). In exceptional cases, the contracted AMO shall apply to SWI PCA (Ref. to CL No.5) to obtain the ad

hoc approval before subcontracting to a third party.

8. COMPLIANCE MONITORING

SWI will carry out Quality Audits to the contracted AMO for the purpose of performing quality surveillance upon

the Part-145 Approved Organization at the concerned location.

The intended audits will be notified in writing (e-mail or fax) by SWI CMM (Ref. to CL No.7) at least one month

in advance of the date the intended audit will take place.

The audit will be limited to a maximum of two (2) days.

Any recommendations and/or non conformities resulting from the audits, will be laid down in a written audit

report which will be submitted by SWI CMM (Ref. to CL No.7) to the AMO Quality Assurance. Once closed

and within due times, the AMO/QA will give written feedback to SWI CMM (Ref. to CL No.7).

9. TRAINING SERVICE

SWI will provide the “Training service” on this manual by a qualified SWI Instructor to the contracted AMO

staff.

Once the first training has been carried out, the SWI Instructor and SWI Compliance Monitoring Manager may

qualify one contracted AMO trained Staff, as Instructor.

In this case, all the subsequent trainings carried out by the contracted AMO qualified instructor, shall be notified

to the SWI CMM (Ref. to CL No.7) filling the SWI training form SWI-CAMO-018B, ref to “Attachment 2” of this

manual.

LINE STATION HANDLING MANUAL N°: SWI-747-LSHM Rev: 3 Date: 12 Apr 2016


ATTACHMENT 1

B747-400F

WALK AROUND INSPECTION



B747-400F

THE WALK-AROUND INSPECTION (NO CRS REQUIRED)

The walk-around inspection must verify the aircraft condition including, in particular, any obvious signs of wear,

damage or leakage.

The inspection must ensure that fuel, consumable fluids, gases etc. uplifted prior the flight are of the correct

specification, free from contamination and correctly recorded.

Use the below detailed inspection route to check that:

• The surfaces and structural are clear, not damaged, not missing parts and there are no fluid leaks;

• The tires are not too worn, not damaged, there is no tread separation and are properly inflated;

• The gear struts are not fully compressed;

• The engine inlets and tailpipes are clear, the access panel are secured, the exterior is not damaged, and

the reversers are stowed;

• The doors and access panels that are not in use are latched;

• The probes, vents, and static ports are clear and not damaged & marked for identification for identification

of this critical area (RVSM ITEMS);

• The skin area adjacent to the pitot probes and static ports is not wrinkled (RVSM ITEMS);

• The antennas are not damaged (RVSM ITEMS);

• The light lenses are clean and not damaged;

• A control that all doors are securely fastened;

• A control that surface and landing gear locks, pitot/static covers, restraint devices and engine/ aperture

blanks have been removed;

• A control that all aircraft’s external surfaces and engines are free from ice, snow, sand, dust etc. and an

assessment to confirm that, as the result of meteorological conditions and de-icing/anti-icing fluids have

been previously applied on it, there are no fluid residues that could endanger flight safety.



Left Forward Fuselage Probes, sensor, ports, vents, and drains (as applicable)……….. .............................................................Check Nose Nose Cargo Door (Not in use) ................................................................................................................Latched Radome ....................................................................................................................................................Check Diverter strips……………………………………………………………………………………………………..Secure Windshield wipers ............................................................................................. …………………..Against stops TAT probes ...............................................................................................................................................Check Nose Wheel Well Tires and wheels .......................................................................................................................................Check Gear strut and doors .................................................................................................................................Check Exterior lights ............................................................................................................................................Check Nose wheel steering assembly .............................................................................................................Checked Nose wheel steering lockout pin ........................................................................................................As needed Gear pins ...........................................................................................................................................As needed Main electrical and electronic (E/E) compartment door ...........................................................................Secure Right Forward Fuselage Probes, sensors, ports, vents, and drains (as applicable) .........................................................................Check Doors and access panels (not in use) ....................................................................................................Latched Negative pressure relief doors .................................................................................................................Closed Oxygen pressure relief green disc .............................................................................. …………………..In place



Right Wing Root, Pack, and Lower Fuselage Probes, sensors, ports, vents, and drains (as applicable) ....................................................................... Check Exterior lights ........................................................................................................................................... Check Pack inlet and pneumatic access doors ................................................................................................. Secure Fuel measuring sticks ...............................................................................................................Flush and secure Leading edge flaps ................................................................................................................................... Check Number 3 and 4 Engines Access panels ........................................................................................................................................Latched Probes, sensors, ports, vents, and drains (as applicable) ....................................................................... Check Fan blades, probes, and spinner ............................................................................................................... Check Strut midspar fuse pins alignment stripes ................................................................................................ Check A minimum of ½ of each stripe must align. A stripe is on the inboard and outboard side of each strut. Thrust reversers ..................................................................................................................................... Stowed Popout pin…………………………………………………………………………………………………………..Check Exhaust area and tailcone ........................................................................................................................ Check Fuel measuring sticks (as applicable) ..................................................................................... Flush and secure Right Wing and Leading Edge Access panels ........................................................................................................................................Latched Leading edge flaps ......................................................................................................... ………………….Check Fuel measuring sticks (as applicable) ........................................................... ………………….Flush and secure Wing Surfaces ................................................................................................................ ………………….Check Fuel tank vent ........................................................................................................................................... Check Right Wing Tip and Trailing edge Navigation and strobe lights ..................................................................................................................... Check Wing Tip Rear Facing Marker Light (as applicable) ........................................................ …………………Check Static discharge wicks .................................................................................................... ………………….Check Fuel jettison nozzle ................................................................................................................................... Check Ailerons and trailing edge flaps ..................................................................................... …………………..Check Right Wing and body Gear Tires, brakes and wheels ......................................................................................................................... Check Verify that the wheel chocks are in place as needed. If the parking brake is set, the brake wear indicator pins must extend out of the guides. Gear strut, actuators, and doors .............................................................................................................. Check Hydraulic lines ........................................................................................................................................ Secure Gear pins .......................................................................................................................................... As needed Wheel wells .............................................................................................................................................. Check APU FIRE CONTROL handle .......................................................................................................................... In Right Aft Fuselage Doors and access panels (not in use) ....................................................................................................Latched Negative pressure relief door ...................................................................................................................Closed Probes, sensors, ports, vents, and drains (as applicable) ........................................................................ Check Outflow valve ............................................................................................................................................ Check Tail Navigation and strobe lights ...................................................................................................................... Check Vertical stabilizer and rudder .................................................................................................................... Check Static ports ......................................................................................................................………………….Check Horizontal stabilizer and elevator ...................................................................................…………………..Check APU exhaust outlet ................................................................................................................................... Check Static discharge wicks .....................................................................................................………………….Check Left Aft Fuselage Side Cargo door and access panels (not in use) ...................................................................................Latched Doors and access panels (not in use) ....................................................................................................Latched



Probes, sensors, ports, vents, and drains (as applicable) ...............................................………………….Check Outflow valve .................................................................................................................…………………..Check Left Body and Wing Gear Tires, brakes and wheels .......................................................................................................................... Check Verify that the wheel chocks are in place as needed. If parking brake is set, the brake wear indicator pins must extend out of the guides. Gear strut, actuators, and doors ......................................................................................…………………Check Hydraulic lines ................................................................................................………………….Secure, no leaks Gear pins .................................................................................................................................... Verify removed Wheel wells .....................................................................................................................………………….Check Left Wing Tip and Trailing Edge Ailerons and trailing edge flaps ................................................................................................................. Check Fuel jettison nozzle ....................................................................................................................................Check Static discharge wicks .............................................................................................................................. Check Navigation and strobe lights ...........................................................................................…………………..Check Wing Tip Rear Facing Marker Light (as applicable) ..................................................................................Check Left Wing and Leading Edge Wing Surfaces .......................................................................................................................................... Check Fuel tank vent ........................................................................................................................................... Check Fuel measuring sticks .............................................................................................................. Flush and secure Leading edge flaps (as applicable) ........................................................................................................... Check Access panels ........................................................................................................................................Latched Number 1 and 2 Engines Access panels ........................................................................................................................................Latched Probes, sensors, ports, vents, and drains (as applicable) .............................................. …………………Check Fan blades, probes, and spinner ............................................................................................................. Check Strut midspar fuse pins alignment stripes ................................................................................................ Check A minimum of ½ of each stripe must align. A stripe is on the inboard and outboard side of each strut. Thrust reversers ...............................................................................................................………………..Stowed Popout pin ………………………………………………………………………………………………………….Check Exhaust area and tailcone .........................................................................................................................Check Fuel measuring sticks (as applicable) ...............................................................……………….Flush and secure Left Wing Root, Pack, and Lower Fuselage Fuel measuring sticks .....................................................................................………………….Flush and secure Probes, sensors, ports, vents, and drains (as applicable) ........................................................................ Check Exterior lights .........................................................................................................................…………….Check Pack inlet and pneumatic access doors ........................................................................…………………..Secure Leading edge flaps ..........................................................................................................………………….Check Positive pressure relief doors ...................................................................................................................Closed Main Deck The walk-around type inspection of the aircraft must check the emergency equipment for condition. In addition, must be checked the presence of all required emergency equipment. Main Deck Cargo Compartment .....................................................................................………………….Check Check compartment after cargo doors are closed: • Check sidewall and ceiling panels for damage.

• Check all pallets are locked down correctly (pallet locks in place).

• Check all pallet loads are secure and fastened to the pallets securely.

• Check tie down on oversize cargo as required.

• Check no leaks from cargo.

• Check no water / snow accumulation on top of pallets or on deck. Nose Cargo door Indicating Lights ...................................................................................………………...Check • Check all annunciator LATCHED lights illuminated (Green).



• Threshold and nose spot light OFF. Side Cargo Door Handle and Indicating Lights ............................................................... ………………...Check • Check door closed, latch handle retainer in the closed position, DOOR OPEN and LATCHES CLOSED lights extinguished. Emergency Equipment ............................................................................................................................Check • Fire extinguishers – Checked and stowed • Crash axe – Stowed

• Other needed equipment – Checked and stowed Smoke Barrier Door ...................................................................................................................................Close • Close smoke barrier door after main entry door has been closed. Upper / Flight Deck The inspection of the Aircraft Technical Log system (ATL, DMI, DBC) must ensure that the intended flight is not adversely affected by any outstanding deferred defects and that no scheduled maintenance actions are overdue or will become overdue during the flight. The walk-around type inspection of the aircraft must check the emergency equipment for condition. In addition, must be checked the presence of all required emergency equipment. Upper Deck Light Panel ............................................................................................................................Check • Upper Deck lights as required. Main Deck Sidewall Lights and Ceiling Lights OFF. Emergency Equipment .............................................................................................................................Check • Fire extinguisher – Checked and Stowed

• Crash axe – stowed

• Emergency escape devices – Stowed

• Other needed equipment – Checked and stowed Upper Deck Door Escape Slide ................................................................................................................Check Check slide pack intact and locked in deployment position.



ATTACHMENT 2

COURSE REGISTER

FORM SWI-CAMO-018B

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