OTAR Part 39 Storage / Transition MAINTENANCE PROGRAMME

for

[Aircraft Registration]

Bermuda OTAR 39 Approval Reference: BDA/CAMO/XXX

Maintenance Programme Approval Number BDA/MP/XXX

Table of Contents

1	Record of Revisions	4

2	List of Effective Pages	4

3	Approval	5

4	Distribution	5

5	Acronyms and Abbreviations	6

5.1	MSG-3 Task Categories	8

6	General Information	9

6.1	Aircraft Information	9

6.2	Operator / Owner and CAMO information	9

7	Certification Statement	10

8	Limits and Utilization	11

8.1	Anticipated Utilization	11

8.2	Maintenance Programme Limit of Validity / Design Service Goal	11

9	Source Data	11

9.1	Airframe and systems	11

9.2	Engines and APU	11

9.3	National and Additional Requirements	12

9.4	Airworthiness Directives	12

9.5	STC & Modifications	12

9.6	Repairs	13

9.7	Service Bulletins	13

10	Maintenance Schedule	13

11	Specific Inspection Requirements	14

12	Status of Sampling Programme	14

13	Program Review and Revision Procedure	14

13.1	General	14

13.2	Revision Procedure	15

13.3	Maintenance Programme Approval	15

14	Escalation and De-escalation of Maintenance Tasks	15

15	Variations to Maintenance Intervals	15

16	Maintenance Standards	16

16.1	Inspection Standards	16

16.2	Requirements for Certificate of Release to Service	17

17	Human Factors and Human Performance Limitations	17

17.1	Maintenance Planning	18

17.2	Mandatory Inspection Tasks	18

17.3	Required Reporting	18

17.4	Maintenance Resource Planning	18

17.5	Critical Systems	18

17.6	Critical Task Controls	19

18	Parking, Storage and Return To Service	19

18.1	Special requirements for Parked or Stored Aircraft	19

18.2	Return to Service	20

19	Bridging Check	20

20	Reporting Requirements	21

21	Operational Requirements	21

22	Pre-flight Inspection	21

23	Reliability Monitoring	21

Record of Revisions

Rev. No.	Revision Date	Details

List of Effective Pages

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Approval

Signature:
Prepared by:
Reviewed by Technical Coordinator:
BCAA Approval:

Distribution

This organisation shall distribute the Maintenance Programme to:

Contracted Part-145 Maintenance Organizations,

CAMO Sub-Contractor (in case of valid contract in place),

The BCAA,

Acronyms and Abbreviations

A/C	Aircraft
AD	Airworthiness Directive
AFL	Aircraft Flights/Cycles
AFM	Aircraft Flight Manual
AH	APU Hours
ALI	Airworthiness Limitation Item
AMC	Acceptable Mean of Compliance
AMM	Aircraft Maintenance Manual
AMP	Approved Maintenance Programme
APU	Auxiliary Power Unit
AWL	Airworthiness Limitation
AWOPS	All Weather Operations
BCAA	Bermuda Civil Aviation Authority
CAME	Continuing Airworthiness Management Exposition
CAMO	Continuing Airworthiness Management Organization
CAMP	Computerized Aircraft Maintenance Program
CAT	Category
CDCCL	Critical Design Configuration Control Limitations
CH	Chapter
CMM	Component Maintenance Manual
CMR	Certification Maintenance Requirement
CPCP	Corrosion Prevention and Control Programme
DY	Days
DAH	Design Approval Holder
DIS	Discard
EASA	European Union Aviation Safety Agency
EHM	Engine Health Monitoring
EIS	Entry Into Service
EMM	Engine Maintenance Manual
ENG CNG	Engine Change
ETLM	Engine Time Limits Manual
FAA	Federal Aviation Authority
FC	Flight Cycle
FH	Flight Hours
FNC	Functional Check
GVFD	Global Vision Flight Deck
GVI	General Visual Inspection
HPC	High Pressure Compressor
HR	Elapsed Clock Hours
ICA	Instructions for Continuing Airworthiness
ICAO	International Civil Aviation Organization
IDG CNG	Integrated Drive Generator Change
LIF LIM	Life Limited
LLP	Life Limited Parts
LDG CNG	Landing Gear Change
LOV	Limit Of Validity
LUB	Lubrication
MAREP	Maintenance Report
MO	Months/Calendar Months
MOE	Maintenance Organization Exposition
MP	Maintenance Programme
MPD	Maintenance Planning Document
MRB	Maintenance Review Board
MRBR	Maintenance Review Board Report
N/A	Not Applicable
NAA	National Aviation Authority
NAT HLA	North Atlantic High Level Airspace
NAT REQ	National Requirement
OEM	Original Equipment Manufacturer
OM	Operation Manual
OPC	Operational Test
P/N	Part Number
PIREP	Pilot Report
PPL	Power Plant Limitations
RST	Restoration
RVSM	Reduced Vertical Separation Minimum
S/N	Serial Number
SB	Service Bulletin
SDI	Special Detailed Inspection
SHP VST	Shop Visit
SMM	Supplemental Maintenance Manual
SSIP	Supplemental Structure Inspection Programme
STC	Supplemental Type Certificate
STCH	Supplemental Type Certificate Holder
STLMC	Supplemental Time Limits Maintenance Check
SVC	Servicing
T/O	Take-off
TAH	Total Aircraft Hours
TCDS	Type Certificate Data Sheet
TCH	Type Certificate Holder
TLM	Time Limits Manual
TLMC	Time Limits Maintenance Check
VCK	Visual Check
VEN REC	Vendor Recommendation
WO	Work Order
YRS	Year
ZIP	Zonal Inspection Programme

MSG-3 Task Categories

Task	Category
LUB = Lubrication	Consumable replenishment by lubricating.
SVC = Servicing	Consumable replenishment by servicing.
OPC = Operational Check	A failure finding task to determine if an item is fulfilling its intended purposes. Does not require quantitative tolerances.
VCK = Visual Check	A visual failure finding task through observation to determine if an item is fulfilling its intended purpose. Does not require quantitative tolerances.
GVI = Inspection - General Visual	A visual examination that will detect obvious unsatisfactory conditions.
FNC = Functional Check	A quantitative check to determine if one or more functions of an item performs within specified limits. This is a potential failure finding task.
DET/DVI = Inspection - Detailed	An intensive visual examination of a specified detail, assembly, or installation. A potential failure finding task.
RST = Restoration	Reworking, replacement of parts or cleaning necessary to return an item to a specific standard.
DIS = Discard	The removal from service of an item at a specified life limit.

General Information

Aircraft Information

Aircraft Information
Registration(s)
Manufacturer
Type/Model
S/N airframe(s)
Engine Manufacturer and P/N
Propeller Manufacturer and P/N
APU Manufacturer and P/N
TCDS airframe
TCDS engine
TCDS Propeller
First Certificate of Airworthiness
Entry Into Service (EIS) Date

Operator / Owner and CAMO information

Operator / Owner
Street
ZIP City
Country
E-mail

CAMO
Approval No.	BDA/CAMO/XXXX
Address
Country
E-mail
Technical Coordinator

Certification Statement

In the preparation of this Maintenance Programme to meet the requirements of OTAR Part 39, the recommendations made by the TCH/STCH and OEM have been evaluated and incorporated. The A/C will be maintained in accordance with this Maintenance Programme.

This Maintenance Programme lists the Tasks and identifies the practices and procedures, which form the basis for the scheduled maintenance of the airplane(s). This organisation undertakes to ensure the safe operation of the A/C the maintenance program is applicable.

The data contained in this Maintenance Programme will be reviewed for continued validity at least annually in the light of operating experience or when a revision to the TCH/STCH recommendations is issued.

The standards applied to the individual task inspections meet the requirements of the Type Certificate holder’s recommended standards and practices.

It is accepted that this Maintenance Programme does not prevent the necessity for complying with any new or amended OTAR where these new or amended regulations may override elements of this Maintenance Programme.

It is understood that compliance with this Maintenance Programme alone does not discharge the operator from ensuring that the Maintenance Programme reflects the maintenance needs of the A/C, such that continuing safe operation can be assured. It is further understood that the BCAA reserves the right to suspend, vary or cancel approval of the Maintenance Programme if it has evidence that the requirements of the Maintenance Programme are not being followed or that the required standards of airworthiness are not being maintained.

Name:

Technical Coordinator

For and on behalf of this organisation

Date:

Limits and Utilization

Anticipated Utilization

The aircraft is not expected to fly more than 10 flight cycles / 20 hours on this Maintenance Programme.

This Maintenance Programme satisfies the requirements of OTAR Part 39.61 while the aircraft is in storage or transition between operators. The aircraft may operate for the purposes of testing after maintenance, demonstration flights or relocation to a place of maintenance under a special flight permit.

This Maintenance Programme may be used for the issuance of a C of A or Export C of A as required for the purposes of transitioning to another operator.

Maintenance Programme Limit of Validity / Design Service Goal

The Limit of Validity (LOV) / Design Service Goal (DSG) reflects the Limit of Validity of the engineering data that supports the structural maintenance program that corresponds to the period of time during which it is demonstrated that Widespread Fatigue Damage (WFD) will not occur in the aircraft. The LOV is defined per aircraft series as follow:

Aircraft Series	Limit of Validity (LOV)
Flight Hours (FH)	Flight Cycles (FC)

Source Data

Airframe and systems

Document	Reference	Revision
MRBR	D626A001-MRBR	06 Nov 2023
MPD	D626A001	15 Oct 2024
Airworthiness Limitations	D626A001-9-01	01 Jan 2024
Airworthiness Limitations Line Number Specific	D626A001-9-02	01 Jul 2020
CMR	D626A001-9-03	01 Jul 2021
Special Compliance Items / Airworthiness Limitations	D626A001-9-04	01 May 2022

Engines and APU

Document	Reference	Revision
CFM 56-7B Shop Manual	SM.10	Jun 2023
APU 131-9B Shop Manual	49-26-95	09 Aug 2022

National and Additional Requirements

Reference	Requirement	Interval
OTAR 39.81	Aircraft weighing	60 Mos
OTAR 39.61(h)(10) OTAC 39-13	Flight Data Recorder readout and serviceability	12 Mos
OTAR 39.61(h)(10) OTAC 39-13	Cockpit Voice Recorder readout and serviceability	12 Mos
OTAR 39.61(h)(10) OTAC 39-13	Inspection of DLR recording system	24 Mos
OTAR 91 Section III SPA.001RVSM (c)(1)	Monitoring of height-keeping performance	24 Mos / 1000 hrs, whichever longer

Airworthiness Directives

The following Airworthiness Directives (AD’s) are applicable to aircraft maintained in accordance with this Program;

FAA/EASA* Airworthiness Directives

EASA/FAA* Airworthiness Directives

It is the responsibility of this organisation to evaluate and monitor implementation of all applicable AD’s and to ensure that they are complied with in accordance with the requirements of the AD.

In case of contradicting requirement, FAA/EASA* ADs will take precedence over EASA/FAA* AD, as the Aircraft is under the FAA/EASA TCDS.

*Prioritise the state of ADs based on state of the TCDS against which the aircraft is operated.

AD’s which require repetitive actions (e.g. regular inspections) must trigger a revision of the Maintenance Programme accordingly.

AD Reference	Requirement	Interval

STC & Modifications

The list below constitutes the instructions for continued airworthiness for all modifications installed on the aircraft and equipment detailed in Section 6.1 of this Maintenance Programme prescribed by the STCH or DAH. For further information concerning modifications installed on the aircraft, refer to [modification status report reference].

Modification Reference	Requirement	Interval

Repairs

The list below constitutes the instructions for continued airworthiness for all repairs installed on the aircraft and equipment detailed in Section 6.1 of this Maintenance Programme. For further information concerning repairs installed on the aircraft, refer to [repair status report reference].

Repair Reference and Location	Requirement	Interval

Service Bulletins

It is the responsibility of this organisation to evaluate and monitor implementation of all applicable Service Bulletins and to ensure that all AD related SB and/or ACB are complied with in accordance with the requirements of the SB.

SB’s which require repetitive actions (e.g. regular inspections) must trigger a revision of the Maintenance Programme accordingly.

Service Bulletin Reference	Requirement	Interval

Maintenance Schedule

The maintenance schedule is based on the source data referenced in Section 9 of this Maintenance Programme, without deviation. However, as the source data is generic to the type, the documents contain tasks that due to modification standard, configuration or operating environment are not applicable to the aircraft detailed in Section 6.1 of this Maintenance Programme.

[reference of maintenance task database] contains the list of maintenance tasks required by the documents referenced in Section 9 of this Maintenance Programme, customized for the model, serial number, modification standard, configuration and operating environment of the aircraft detailed in Section 6.1 of this Maintenance Programme.

Check frequency as defined in OEM source data.

Specific Inspection Requirements

This Maintenance Programme is developed from the documents detailed in Section 9 of this Maintenance Programme and in respect of guidance and rules associated with specific programme requirements, refer to the TCH references below.

Requirement	Reference
Fuel System Maintenance	MPD D626A001 Section 1.B.8.
EWIS	MPD D626A001 Section 1.B.9
Pressure Cylinder Qualification	MPD D626A001 Section 1.E.
Ageing and Supplement Structural Inspection Programme	MPD D626A001 Section 2.D.
CPCP	MPD D626A001 Section 2.E.
Zonal Inspection Programme	MPD D626A001 Section 3

Status of Sampling Programme

Where previous operators have implemented sampling programmes as part of their maintenance schedule, this organisation shall determine the status of sampling performed on the aircraft and implement in the bridging check any such inspections or tests to restore the requirements of the maintenance schedule.

Program Review and Revision Procedure

General

In order to meet the requirements of the Air Navigation (Overseas Territories) Order (AN(OT)O), it is the responsibility of the nominated person/organisation identified in Section 6.2 to ensure that instructions for continued airworthiness, with regard to mandatory and non-mandatory requirements, incorporated design changes (modifications and repairs) and any requirements deemed necessary by the BCAA are evaluated for applicability. Once evaluated, suitable amendments to the Maintenance Programme must be developed and approved.

This organisation is responsible for performing a full review of the Maintenance Programme at least once per year to ensure it reflects the latest amendment standards of the documents listed in Section 9 of this Maintenance Programme.

Revision Procedure

This organisation shall review the Maintenance Program periodically at least once a year to reflect:

Applicable Mandatory Directives

Applicable evaluations of reliability analysis

Operational issues

Maintenance findings

Type Certificate holder's recommendations

Revisions to the MRB report

Revisions the MPD

Revisions to Chapter 5 Maintenance Manual

Applicable Supplemental Type Certificate Holders’ revisions to instructions for continued airworthiness

Aircraft utilisation (hours/cycles etc)

Changes to aircraft operational utilisation (Type of operation and climatic conditions)

Review of aircraft and equipment life limits.

If applicable, a review of the Corrosion Prevention Control Programme (CPCP) tasks and findings

Following a review of the listed information, this organisation shall maintain records of technical justification supporting the amendment decisions for both inclusion and non-inclusion in the Maintenance Programme.

For new or revised task requirements that are already overdue or will become overdue within the quoted threshold / interval, this organisation shall ensure the task is performed during the return to service maintenance work pack.

Maintenance Programme Approval

Pursuant to OTAR 39.61(b), the BCAA shall approve the Maintenance Programme and all amendments. The Technical Coordinator is responsible for submitting the Maintenance Programme and amendments to the BCAA for approval in accordance with the BCAA supplement / MCM.

Escalation and De-escalation of Maintenance Tasks

This organisation shall not escalate any tasks beyond the intervals specified in the documents contained in Section 9 of this Maintenance Programme.

Variations to Maintenance Intervals

A variation should not be understood to be a maintenance planning tool, but as an exceptional means to allow the operator to fly for a limited period of time until the required maintenance is performed. The use of this provision should be limited to occasions when compliance with the approved maintenance program cannot be achieved due to circumstances which could not reasonably have been foreseen by the operator.

It is the responsibility of the Technical Coordinator (TC) or contracted approved Continued Airworthiness Management Organisation to ensure that arrangements are effectively established to maintain the aircraft in accordance with the approved Maintenance Program.

The policy related to permitted variations does not apply to:

Life limitations identified in the Airworthiness Limitations Sections.

Tasks required to satisfy Airworthiness Directives related to a specific unsafe condition.

Damage - Tolerant Airworthiness Limitation Items as stated in Airworthiness Limitations Section.

Certification Maintenance Requirements, unless specified otherwise in the Boeing CMR document.

Fuel system Airworthiness Limitation Items, unless specified otherwise in the Airworthiness Limitations Sections.

Engine Life Limited Parts and APU Life Limited Parts.

The maximum pre-approved variation permitted by this Maintenance Programme are prescribed below.

Period	Maximum Variation
Items controlled by flying hours
5000 flying hours or less	10%
More than 5000 flying hours	500 flying hours
Items controlled by calendar time
One year or less	The lessor of 10% or one month
More than 1 year but less than 3 years	Two months
Items controlled by cycles or landings
500 cycles / landings or less	The lesser of 10% or 25 cycles / landings
More than 500 cycles / landings	The lesser of 10% or 500 cycles / landings

For items controlled by more than one limit, e.g. items controlled by flying hours and calendar time or flying hours and landings/cycles, the more restrictive limit should be applied.

The variation periods mentioned above should be supported by appropriate technical justification. This should be established from a detailed review of the aircraft records, maintenance and operational history. It should also establish inspection requirements that cannot be subject to variation as per mention above.

The period to the next required inspection shall be deemed to begin at the point prior to when the task/interval was extended. No variation may be taken towards the next required inspection.

Maintenance Standards

Inspection Standards

Practices and procedures to satisfy the Maintenance Program shall follow the standards specified in the TC or STC holder’s Maintenance Instructions.

Task	Definition
GVI – General Visual Inspection	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 enhance visual access to all exposed surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, 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.
DET/DVI – Detailed Visual Inspection	An intensive visual examination of a specific structural area, system, 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 by the inspector. Inspection aids such as mirrors, magnifying lenses, etc. may be used. Surface cleaning and elaborate access procedures may be required.
SDI – Special Detailed Inspection	An intensive examination of a specific item(s), installation or assembly to detect damage, failure or irregularity. The examination is likely to make extensive use of specialized inspection techniques and/or equipment. Intricate cleaning and substantial access or disassembly procedures may be required.
Zonal Inspection	A collective term comprising selected general visual inspections and visual checks that is applied to each zone, defined by access and area, to check system and power plant installations and structure for security and general condition.

Requirements for Certificate of Release to Service

The Release to Service shall be documented as required by OTAR Part 43.105, and shall refer to the ‘work recorded’. This may reference the Work Order and/or Work Pack accordingly together with reference to the applicable Maintenance Data.

Human Factors and Human Performance Limitations

This maintenance program includes human factor principles permitting the reader to identify requirements, maintenance tasks breakdown and combined maintenance tasking, particularly safety critical tasks in order to mitigate human factors and human performance limitations.

In order to eliminate maintenance personnel errors, caused by human factors, Maintenance Programme tasks comply with the following:

Layout of the operator tasks is easily understandable for maintenance staff;

Simple English language is used;

Instructions are clear, brief and understandable;

Operator tasks have standardized forms;

All notes, warnings, and cautions are apparent by the suggested use of boxing, bolding and underlining text;

Clear instructions are given for the mechanic/inspector as to where to sign, certify and date the task;

The important graphic details are included in operator tasks if necessary;

Full Maintenance Programme identification is used for some tasks instead of referencing to a separate document that may distract the mechanic.

Maintenance Planning

With regards to the complexity of the maintenance work scope, this organisation shall produce maintenance work pack including the arrangement of inspections in a manner that avoids conflict of inspection/maintenance activities.

Mandatory Inspection Tasks

This organisation shall ensure that maintenance planning personnel have clear visibility of mandatory tasks, preventing any unauthorized escalation. Section 13 of this Maintenance Programme provides further information concerning the limits permitted for varying maintenance intervals.

Required Reporting

This organisation shall highlight tasks associated with reporting such as the Aging Aircraft Programme Supplemental Structural Inspection Document (SSID) and CPCP to ensure they are readily identified.

Maintenance Resource Planning

This organisation shall ensure that contracted maintenance providers are notified of tasks requiring specialised tooling and or techniques and that required resources are readily identified.

Critical Systems

The practice of performing maintenance on any critical multiple system may present opportunities for error. Maintenance of all multiple critical aircraft systems at the same time or by the same individual or team presents the potential for similar errors being introduced onto multiple systems. This risk of error can be offset through staggered maintenance, varying maintenance personnel, developing specific processes for critical system maintenance and educating maintenance personnel about critical systems.

System maintenance requirements should be purposely designed to avoid working on critical redundant systems during a single maintenance visit. Additional processes or instructions such as checklists, cross checking work performed, using tooling provided by the airframe manufacturers and engine companies or additional functional tests should be developed for those occasions when such maintenance cannot be avoided during maintenance visits.

The following critical systems have scheduled maintenance requirements and are included in this list for consideration in the separation of tasks to address multiple system error potential.

Air conditioning

Electrical power

Fire protection

Fuel

Hydraulics

Ice and Rain

Navigation

Pneumatics

Auxiliary Power

Engines

MPD [add reference] defines all scheduled maintenance tasks that are applicable to critical systems.

Critical Task Controls

This organisation shall ensure tasks that are critical in nature are planned and allocated in a segregated manner that prevents the possibility of multiple error across the same system. Where this cannot be achieved, this organisation shall ensure that the maintenance provider performs independent inspections to ensure correct task accomplishment.

Parking, Storage and Return To Service

When an aircraft is parked or stored, the procedures and accompanying maintenance practices for short term parking, extended/prolonged parking or storage, whichever apply, need to be performed in accordance with the AMM Chapter 10, applicable engine type EMM, APU type CMM and Bermuda Advisory Circular BAC-AW-02.

Special requirements for Parked or Stored Aircraft

An aircraft which has been taken out of operation and is parked or stored for more than 24 hours has to be maintained according to the following rules:

All scheduled maintenance requirements and checks defined in this Maintenance Programme, which become due during the parking/storage period, may be postponed until the end of the parking period (unless required by AMM 10-00-00).

All deferred defects and open items, which are scheduled for rectification during the parking period, may be postponed until the end of the parking period (unless required by AMM 10-00-00).

All changes of components, which become due during the parking period, may be postponed until the end of the parking period (unless required by AMM 10-00-00).

All EOs, SBs, AOTs, SILs, ADs, CNs and National Airworthiness Requirements, which become due during the parking/prolonged parking period, may be postponed until the end of the parking period, provided there is no specific requirement for the parking/storage period.

Provisioning related component, APU or engine removals during the parking/storage period are possible in general. The reinstallation of a component, APU or engine can be postponed until the end of the parking/storage period but has to be performed in accordance with all relevant procedures. All outstanding work and component replacements must be completed before the return of the aircraft back into service. For appropriate handling of a removed component, APU or engine before installation in another aircraft, refer to the relevant procedures.

For maintenance requirements and maintenance checks which are limited in the Maintenance Programme with calendar time, an interval credit may be used in principle. The amount of the interval credit depends on the duration and the condition of the parking/storage and is subject to BCAA approval.

Return to Service

Before the aircraft is returned to service, all postponed maintenance requirements and checks defined in the Maintenance Programme, all component changes as required by the CMS, EOs, SBs, AOTs, SILs, ADs, CNs, and rectification of deferred defects/open items have to be reviewed and implemented as required.

For details concerning the maintenance tasks required, refer to the following:

Maintenance Requirement	Reference
Parking	AMM 10-11-00
Storage	AMM 10-12-00
Mooring	AMM 10-20-00
Return to Service	AMM 10-30-00

Bridging Check

This organisation shall perform a bridging check for all aircraft listed in this Maintenance Programme. This review shall consist following steps:

Create a status report against the latest amendment of the TCH MPD and relevant ALS Parts.

Compare the previous operator´s maintenance program and previous operator´s MPD status against the current MPD requirements, including the status of any items affected by a sampling programme and incorporate these into the maintenance work order.

Review the previous operator´s self-generated tasks for applicability and incorporate those applicable into the maintenance work order.

Review any repetitive inspections resulting from repairs or modifications and incorporate these into the maintenance work order.

Review all mandatory requirements and incorporate these into the maintenance work order.

Review component maintenance and life limited parts as required by MPD or vendor recommendations and incorporate these into the maintenance work order.

Review all BCAA requirements and incorporate these into the maintenance work order.

Provide a work order to the contracted maintenance provider to ensure all maintenance items identified during steps 1 – 7 are satisfactorily implemented.

Reporting Requirements

This organisation shall report to the TCH and BCAA and findings of corrosion which exceed Level 1 (i.e., Levels 2, 3) and Aging Aircraft Programme Supplemental Structural Inspection Document (SSID) in accordance with CAME [add reference]. For CPCP level classification refer to the TCH data referenced in Section 10 of this Maintenance Programme.

Operational Requirements

Special operations including, AWOPS, MNPS, RVSM, EDTO, offshore, Emergency Medical Service and dangerous goods are not applicable to aircraft under this Maintenance Programme.

Pre-flight Inspection

The pre-flight inspection is meant to ensure airworthiness and must be performed before each flight. It is the responsibility of the flight crew to perform the pre-flight inspection in accordance with the AFM. All other maintenance on the aircraft must be performed by approved maintenance organization.

Reliability Monitoring

As the aircraft is in storage and/or transition, this organisation is unable to collate sufficient information to support a reliability programme. As such, the BCAA accepts that in the current circumstances, a reliability programme is not required.

This organisation shall revise this document to establish a reliability programme if the aircraft returns to service.