Date post: | 22-Dec-2015 |
Category: |
Documents |
Upload: | niojonok82 |
View: | 3 times |
Download: | 0 times |
WHERE?
Sect 1 INTRODUCTION - L2 : Overview
Sect 2 REGULATION - L1 : Regulation 1 – Application of Regulation and Procedural Rules - L2 : Regulation 2 – Type Certificate, Service Release
and Design Acceptance - L3 : Regulation 3 - AEO
- L4 : Regulation 4 - AMO - L5 : Regulation 5 - Aircraft Maintenance and
Management Procedures
Sect 3 GUIDANCE (DESIGN)
Sect 4 GUIDANCE (MAINTENANCE)
WHAT?
S2L3 : Regulation 3 - AEO
3.1 - General (General Application)
3.2 - Engineering Authority Certificates
3.3 - General Requirements of Issue
3.4 - Design Control
3.5 - CI Management
3.6 - Operating Requirements
WHY WE NEED TO AMEND? S2L3 : REGULATION 3 - AEO
Realign With The Current Practice.
Introduce New Sub-Regulation/Clause.
Emphasize The Current Requirement.
Prepare For Future Scope of Design/Engineering
Activities..
Facilitate The Understanding of Regulation.
Uphold/Maintain the Aviation Safety/Aircraft
Airworthiness
Regulation Title Remarks
3 Authorised Engineering Organisation To Be Amended
3.1 General No Change (NC)
3.1.1 Applicability NC
3.2 Engineering Authority Certificates To Be Amended
3.2.1 Applicability NC
3.2.2 Certificate Required NC
3.2.3 Sponsor AEO Requirements To Be Amended
3.2.4 Application To Be Amended
3.2.5 Audit NC
3.2.6 Issue of a Certificate To Be Amended
3.2.7 Duration To Be Amended
3.2.8 Engineering Management Plan To Be Amended
3.3 General Requirements of Issue To Be Amended
3.3.1 Definitions NC
3.3.2 Personnel To Be Amended
3.3.3 Design Support Networks NC
3.3.4 Design Control System NC
3.3.5 CI Management System NC
3.3.6 Data NC
3.3.7 Equipment, Tools and Facilities NC
3.3.8 Records To Be Amended
3.3.9 EMS Internal Evaluation System NC
3.3.10 Documentation Control NC
3.3.11 Prescribe, Revise and Interpret Airworthiness Standards New Regulation
3.4 Design Control To Be Amended
3.4.1 Design Control System To Be Amended
3.4.2 Data Control NC
3.4.3 Issue of Design Approval Certification NC
3.4.4 Design Review To Be Amended
3.4.5 Judgement of Significance NC
3.4.6 Design Acceptance NC
Regulation Title Remarks
3.5 CI Management To Be Amended
3.5.1 Applicability NC
3.5.2 Technical Information Review To Be Amended
3.5.3 Maintenance Engineering Analysis NC
3.5.4 Aircraft Structural Integrity Management To Be Amended
3.5.5 Engine Structural Integrity Management To Be Amended
3.5.6 Modifications NC
3.5.7 Substitutions NC
3.5.8 Deviations NC
3.5.9 Aircraft Stores Clearance and Certification NC
3.5.10 Aerial delivery clearances NC
3.5.11 Special Technical Instructions (STIs) To Be Amended
3.5.12 Incorporation Approval NC
3.5.13 Service Release (Minor Changes to TD) NC
3.5.14 Management of Type Design Data NC
3.5.15 Instructions for Continuing Airworthiness To Be Amended
3.5.16 Flight Manuals and aircraft operating instructions NC
3.5.17 Weight and Balance NC
3.5.18 Non Destructive Testing NC
3.5.19 Production NC
3.5.20 Modification Installation NC
3.5.21 Software Integrity Management New Regulation
3.6 Operating Requirements To Be Amended
3.6.1 Continued Compliance NC
3.6.2 Changes to an AEO’s Organisation NC
3.6.3 Inspections and Audits To Be Amended
REG
NO.
EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.2.3
Sponsor AEO requirements
c. Sponsor AEOs shall develop,
promulgate and adhere to a structured
compliance assurance program when a
commercial organisation is required to
operate as a commercial AEO, to ensure
that the commercial AEO is monitored for
compliance with the TAR’s regulatory
requirements.
Delete the whole paragraph since the compliance
assurance function is undertaken by DGTA
3.2.4
Application
a. The applicant shall submit an
application for an EAC to the TAR:
(1) By the applicant directly when it is
the SAO organisation.
(2) Through the Sponsor AEO when
the applicant is a commercial
organisation.
a. The applicant shall submit an application for
an EAC to the TAR.
(1) By the applicant directly when it is the
SAO organisation.
(2) Through the Sponsor AEO when the
applicant is a commercial organisation.
REG
NO.
EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.2.4 c. For an application from a commercial
organisation, the applicant shall include a
copy of the clauses of the formal
instrument to enforce the regulations in
this regulation.
To cater for an applicant without a contract or
formal instrument)
c. For an application from a commercial
organisation, the applicant shall include a copy of
the clauses of the formal instrument or SAO
sponsor letter to enforce the regulations in this
regulation.
3.2.4 Reg 3.2.4d is not available in the existing
regulation.
To emphasize the requirement.
d. For an application from a commercial
organisation relying substantially upon
subcontractors to perform the engineering
activities listed in the applicant’s EMP, the
application must detail those subcontractors and
the respective scopes of work to be subcontracted.
3.2.6 Issue of a Certificate
a(4) For a commercial AEO, the sponsor
AEO has developed and promulgated a
compliance assurance program as
required by regulation 3.2.3.
Delete the whole paragraph since the compliance
assurance function is undertaken by DGTA
REG
NO.
EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.2.7 Duration
Reg 3.2.7c is not available in the existing
regulation.
To cater for AEO without a contract/formal
instrument.
c. An EAC issued to a commercial AEO with SAO
sponsor letter (without formal instrument) is valid
for a period as stated in the sponsor letter or until
the TAR suspends or revokes it.
3.2.8 Engineering Management Plan
Reg 3.2.8a(3)(d) is not available in the
existing regulation.
To introduce new scope of EA for ASR-AEO.
a(3)(d) The airworthiness standards that the ASR
is authorised to prescribe, revise and interpret in
accordance with Regulation 3.3.11.
3.3.2 Personnel
Reg 3.3.2a(2)(g) is not available in the
existing regulation.
To emphasize ASR’s responsibilities as a SDE.
a(2)(g) For ASR only, prescribing, revising and
interpreting airworthiness standards in
accordance with Regulation 3.3.11.
REG EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.3.2
(3) For a Sponsor AEO, sufficient Auditor
and Lead Auditor qualified personnel,
meeting all the criteria of Annex G to
this regulation, to conduct
compliance assurance activities
required by regulation 3.2.3.
Delete the whole paragraph since the compliance
assurance function is undertaken by DGTA
3.3.2 e(5) For a Sponsor AEO, the SDE
authorises all Auditor and Lead Auditor
personnel.
Delete the whole paragraph since the compliance
assurance function is undertaken by DGTA
3.3.8
Records
a(2) For commercial organisations, agree
to transfer copies of such records to the
Government of Malaysia (delegated SAO)
upon cessation of the commercial AEO
formal instrument in accordance with
terms to be included in the formal
instrument and endorsed by the TAR.
Delete and endorsed by TAR since the TAR will not
be involved in endorsing the formal instrument.
a(2) For commercial organisations, agree to
transfer copies of such records to the Government
of Malaysia (delegated SAO) upon cessation of the
commercial AEO formal instrument in accordance
with terms to be included in the formal instrument.
and endorsed by the TAR.
REG EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.3.11 Reg 3.3.11 is not available in the
existing regulation.
(To introduce new requirement for
ASR-AEO. It is corresponding with the
scope of EA of ASR-AEO (CoE)
Prescribe, Revise and Interpret Airworthiness
Standards
a. Each applicant seeking authority to prescribe, revise
and interpret airworthiness standards, hereinafter
referred to as an Airworthiness Standards
Representative (ASR), must have EMP procedures to
ensure that:
(1) The airworthiness standards that the ASR has
responsibility for are identified in the EMP and are
managed in accordance with Regulation 3.3.10.
(2) There is a pro-active approach to monitoring of
amendments to airworthiness standards.
(3) The competency and on going professional
development requirements for the ASR and those
positions within the AEO deemed to be essential to
an AEO maintaining its COE status, are described in
the EMP and endorsed by the Senior Executive.
REG EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.4.1
Design control system
Reg 3.4.1c(5)(d) is not available in the
existing regulation.
To introduce system safety requirement for AEO.
c(5)(d) The application of System Safety.
3.4.4
Design Review
Reg 3.4.4a(6)(b) is not available in the
existing regulation.
To emphasize the requirement for design review
process.
a(6)(b) The requirements of Regulation 3.4.4
a(1)(a) have been satisfied.
a. The procedure for Design Review required by
Regulation 3.4.1 shall ensure:
(1) Certification of design output as a reviewer
is granted by an authorised person only if
satisfied that:
(a) The design assumptions, design reference
data, design conditions and the method and
tools employed in developing the design
output are assessed as appropriate and valid.
3.5.2
Technical Information Review
a(2)(c) Technical Airworthiness Directives
(TADs) issued by the TAR.
To include additional TI for TIR process.
a(2)(c) Technical Airworthiness Directives (TADs)
or Technical Airworthiness Advisory Circular (TAAC)
issued by the TAR.
REG EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.5.4
Aircraft Structural Integrity Management
c. The ASI management system shall
ensure that:
(1) For a new aircraft type or major
design change, the ASIMP is issued by
the TAR prior to the Design
Acceptance of the aircraft type or
design change in accordance with
Regulation 2.2.3.
To rationalize the function of TAR/DAR.
c. The ASI management system shall ensure that:
(1) For a new aircraft type or major
design change, the ASIMP is issued by
the TAR/DAR prior to the Design
Acceptance of the aircraft type or
design change in accordance with
Regulation 2.2.3 (Issue of a Design Acceptance
Certificate)
3.5.4
c(6) ASI projects are managed by TAR.
To rationalize the function of TAR/DAR.
c(6) ASI projects are managed by TAR/DAR.
3.5.4 d(3) Ensure the authorised structural
inspection program intervals, structural
life limits, and component retirement
times are not exceeded without TAR
approval.
To rationalize the function of TAR/DAR.
d(3) Ensure the authorised structural inspection
program intervals, structural life limits, and
component retirement times are not exceeded
without TAR/DAR approval.
3.5.4
Reg 3.5.4d(6) is not available in the
existing regulation.
To include additional requirement in ASIMP.
d(6) Clearly identified Principal Structural Elements
(PSE) in ASIMP.
REG EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.5.5 Engine Structural Integrity Management
a. Each applicant responsible for the CI
management of an aircraft gas turbine
engine shall establish an Engine
Structural Integrity Management (ESIM)
system to assure the continued
airworthiness of that engine.
b. The ESIM system shall ensure that:
(1) an Engine Structural Integrity
(ESI) Manager is appointed;
(2) critical parts are identified for
each engine;
(3) life limits, inspection and usage
monitoring requirements are
identified for each critical part based
upon the advice of:
(a) the OEM; or (in the absence
of such advice)
(b) a recognised NAA or foreign
military force in accordance with
regulation 2.2.7; or
(c) the TAR;
Engine Structural Integrity Management
a. Each applicant responsible for the CI management
of an aircraft gas turbine engine shall establish and
maintain an Engine Structural Integrity Management
(ESIM) system that ensure:
(1) An Engine Structural Integrity (ESI) Manager is
appointed.
(2) Critical parts are identified for each engine.
(3) Except as otherwise approved by the TAR, life
limits, inspection and Usage Monitoring (UM)
requirements are identified for each critical part
based upon the current advice of:
(a) The OEM.
(b) A recognised NAA or foreign military force as
defined in Regulation 2.2.7.
(c) The ESI Manager are supported by data
provided by an authorized AEO providing ESI
engineering services.
(4) The requirements identified in Regulation
3.5.5.a.(3)are periodically reviewed for applicability
to the SAO configuration, role and environment..
REG EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.5.5 (4) a system for engine usage
monitoring is in place to ensure that
engine operating data is recorded to
enable management against the
limits identified at subparagraph (3);
(5) the requirements identified at
subparagraphs (3) and (4) are
assessed for applicability to the SAO
configuration, role and environment;
and
(6) a system for engine condition
monitoring is in place and includes
adequate review to ensure
effectiveness.
c. The ESIM system shall be
documented by an Engine Structural
Integrity Management Plan (ESIMP).
d. The ESIMP shall be reviewed at an
interval of not more than two years.
e. The ESIM system shall be
implemented by procedures that are
sponsored by the applicant.
(5) An effective system for UM is employed to
prevent exceedance of the limits identified in
Regulation 3.5.5.a.(3).
(6) Systems and processes for Condition
Monitoring, used to maintain airworthiness, are
validated and supported.
(7) The ESI management system is documented
in an Engine Structural Integrity Management
Plan (ESIMP).
(8) The ESIMP is reviewed, and revised if
necessary, at intervals not to exceed two years.
(9) The TAR is notified at the earliest opportunity
following:
(a) Receipt of amendments to critical part
life limits, inspection or UM requirements
issued by the applicable organisation in
Regulation 3.5.5.a.(3).
(b) Receipt of any TAAI applicable to the
engine.
(c) A non-recoverable in-flight shut-down of
an engine.
REG EXISTING REGULATION PROPOSED AMENDMENT/ REMARKS
3.5.5 f. TAR approval is to be sought prior to:
(1) deviation or modification to the
life limits and requirements
established at subparagraph b(3)
above; or
(2) issue of a new or amended
ESIMP.
(10) TAR approval is obtained through DAR
recommendation prior to:
(a) Implementing critical part life limits,
inspection or UM requirements that differ
from those specified by the applicable
organisation in Regulation 3.5.5.a.(3).
(b) Significantly modifying the system for UM
required by Regulation 3.5.5.a.(5).
(c) Releasing the initial and all revised
ESIMPs.
REG EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.5.11
Special Technical Instructions (STIs)
b(14) The status of released STIs is
promulgated at six monthly intervals for
each STI Series status of either ‘active’ or ‘cancelled’.
b(14) STIs are actively monitored for incorporation
status including:
(a) STIs are cancelled at the earliest
possible opportunity.
(b) STIs found not to be fully incorporated
past their incorporation timeframe are
subject to appropriate action as determined
by the SDE.
(c) The status of released STIs is
promulgated at six monthly intervals for
each STI Series status of either ‘active’ or
‘cancelled’.
3.5.15
Instructions for Continuing
Airworthiness (ICA)
Reg 3.5.15a(4)(d) and a(4)(e) are not
available in the existing regulation.
a(4)(d) The instructions identify all Safety Critical
Items and Systems (SCIS).
a(4)(e) The instructions identify Independent
Maintenance Inspection (IMI) requirements for SCIS.
3.5.15 Reg 3.5.15a(7), a(8) and a(9) are not
available in the existing regulation.
a(7) Validate ICA that identify those maintenance
requirements essential to the airworthiness of
aircraft and associated Cis.
a(8) Collect and analyse data used to validate the
ICA that identify maintenance requirements essential
to the airworthiness of aircraft and CIs.
a(9) Ensure that all maintenance requirements
essential to the airworthiness of aircraft and
associated CIs are reviewed as a result of TIR or
other change initiator.
REG NEW STATEMENT
3.5.21
Software Integrity Management
a. Each applicant responsible for the configuration item management of aviation
software or aviation systems containing software must establish and maintain a
Software Integrity Management System, where aviation software is inclusive of:
(1) On-aircraft software, off-aircraft software with aircraft interface, and off-
aircraft software with no interface but which has airworthiness or safety
implications.
(2) Technologies that resemble software development such as Field
Programmable Gate Arrays(FPGAs) and firmware.
b. The Software Integrity Management System must include:
(1) A Software Management Plan (SMP).
(2) Procedures to assure software integrity of new or modified software.
(3) Procedures to provide continuing assurance of the software integrity of
accepted software.
REG NEW STATEMENT
3.5.21
c. The Software Integrity Management System must ensure that:
(1) The SMP is prepared by the SDE, issued by the DAR and approved by the
TAR.
(2) Any amendment to the SMP been approved by the TAR.
(3) All aviation software Configuration Items being managed by the applicant,
including the associated software assurance level, and worst credible failure
condition are identified in the SMP.
(4) All software tools being used by the applicant, including the tool
categorisation and qualification, are identified in the SMP.
(5) The SMP is reviewed at an interval not exceeding two years.
d. The procedures to assure software integrity of new or modified software must:
(1) Ensure software development of safety-related software is conducted to
satisfy the objectives of either a TAR recognised software assurance standard,
or a Software Assurance Matrix approved by the TAR.
(2) Require a software safety program be established for the development of
all software that is safety-related.
REG NEW STATEMENT
3.5.21
(3) Ensure a Plan for Software Aspects of Certification (PSAC), or equivalent
document, is submitted to and approved by the TAR prior to the
commencement of development.
(4) Provide for DGTA oversight of software for safety-related systems to
permit the DGTA to make software compliance findings.
e. The procedures to provide continuing assurance of the software integrity of
accepted software must:
(1) Implement a framework for software problem reporting, problem
assessment, tracking of problem reports and corrective actions to ensure that
errors, faults and failures are identified and resolved within a timely manner as
Regulation 3.5.2.
(2) Ensure the DAR and TAR is notified of any errors, faults or failures of
aviation software which potentially result in a large reduction in safety
margins.
REG EXISTING REGULATION PROPOSED AMENDMENT/REMARKS
3.6.3
Inspections and audits
d. Except as otherwise authorised by the
TAR, each AEO shall be required to
undergo an external audit at an interval
not to exceed two years and as specified
by the applicable compliance assurance
program as required by regulation 3.2.3.c.
e. The audit team shall include a quantity
of qualified Auditors led by a qualified
Lead Auditor, each meeting the criteria in
Annex G (as applicable) to this regulation.
f. The audit team shall be approved by:
(1) for a Service AEO audit, the TAR.
(2) for a commercial AEO audit, the
SDE of the Sponsor AEO.
g. The Sponsor AEO shall provide to the
TAR a copy of the audit report arising from
an external audit of a commercial AEO.
d. Except as otherwise authorised by the TAR, each
AEO shall be required to undergo an external audit
at an interval not to exceed two years. and as
specified by the applicable compliance assurance
program as required by regulation 3.2.3.c.
e. The audit team shall include a quantity of
qualified Auditors led by a qualified Lead Auditor,
each meeting the criteria in Annex G (as applicable)
to this regulation.
f. The audit team shall be approved by TAR.
(1) for a Service AEO audit, the TAR.
(2) for a commercial AEO audit, the
SDE of the Sponsor AEO.
g. The Sponsor AEO shall provide to the TAR a
copy of the audit report arising from an external
audit of a commercial AEO.
CONCLUSION (S2L3 : REGULATION 3 – AEO)
The propsed amendment could benefit all TAMM Reg. 3
Stakeholders i.e. Regulator, Service AEO, Commercial AEO,
DAR, ASR, and Engineering Organisation.
The proposed amendment shall streamline the current
regulation and upgrade it to a level that could accommodate
the current and future design/engineering activities.
The proposed amendment will not significantly impact the
current design/engineering activities of AEO.