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Airworthiness Directives – A TCCA Perspective
EASA AD Workshop
Cologne, Germany • 2-3 December 2014
Outline
• Issuing ADs – Why, When, What?
• Differences from EASA
• AMOCs
• Continuing Airworthiness Information
System (CAWIS)
• When questions arise
• How can TCCA ADs be improved?
EASAAD Workshop, 2-3 December 2014 2
What
Canadian Aviation Regulation (CAR) 101.01:
“an instruction issued by the Minister or by a civil
aviation authority responsible for an aeronautical
product type design that mandates a maintenance or
operation action to ensure that an aeronautical
product conforms to its type design and is in a
condition for safe operation”
EASAAD Workshop, 2-3 December 2014 3
What
Mandatory Continuing Airworthiness
Instruction (MCAI) in accordance with ICAO
Annex 8
Issued in English and French, except for
Emergency AD which can be issued in
English only
EASAAD Workshop, 2-3 December 2014 4
What
Number of ADs issued:
EASAAD Workshop, 2-3 December 2014 5
Year No. of ADs
2012 33
2013 41
2014 42
Why
An unsafe condition has been identified on
an aeronautical product
“aeronautical product” means any aircraft, aircraft
engine, aircraft propeller or aircraft appliance or part or
the component parts of any of those things, including
any computer system and software
Aeronautics Act
EASAAD Workshop, 2-3 December 2014 6
Why
CAR compels the Minister of Transport to
issue AD when there is unsafe condition
521.427 (1) The Minister shall issue an airworthiness
directive in respect of an aeronautical product if
(a) an unsafe condition exists in the aeronautical
product and the condition is likely to exist or develop in
other aeronautical products
EASAAD Workshop, 2-3 December 2014 7
Why
However, TC can accept a campaign from
the DADH instead of issuing an AD
“Note:
TCCA does not necessarily automatically issue an
airworthiness directive. It may allow the manufacturer to
campaign the replacement of defective parts. Where
that campaign is not successful, then TCCA will issue
an airworthiness directive.”
TCCA/EASA Technical Implementation Procedures for
Airworthiness and Environmental Certification
EASAAD Workshop, 2-3 December 2014 8
Why
An unsafe condition has not been verified,
but there is reason to believe that it exists or
is likely to come into existence in an
aeronautical product
EASAAD Workshop, 2-3 December 2014 9
Why
EASAAD Workshop, 2-3 December 2014 10
Why
An existing AD (foreign or Canadian) needs to be
cancelled or amended
CAR 521.427 (1) The Minister shall issue an airworthiness directive in
respect of an aeronautical product if
(b) it is necessary to modify or cancel the requirements of an airworthiness
directive issued by the foreign airworthiness authority having jurisdiction
over the type design of the aeronautical product because the Minister
considers the airworthiness directive inappropriate for reasons related to
the environment, safety, the delayed receipt of an instruction issued by the
foreign airworthiness authority or reliance on foreign legislation; or
(c) it is necessary to modify or cancel a Canadian airworthiness directive
that is in force, because a condition for issuance referred to in paragraph
(a) or (b) has changed or ceased to exist.
EASAAD Workshop, 2-3 December 2014 11
Why
EASAAD Workshop, 2-3 December 2014 12
Why
EASAAD Workshop, 2-3 December 2014 13
Why
Need to override a global Alternative Means
of Compliance (AMOC) granted by the state
of design
EASAAD Workshop, 2-3 December 2014 14
Why
Emergency equipment intended to minimize
the effects of survivable accidents is not
performing its intended function
EASAAD Workshop, 2-3 December 2014 15
Why
EASAAD Workshop, 2-3 December 2014 16
Why
Hazard of collateral damage/injuries on
ground/personnel caused by components
that have detached from the aircraft
EASAAD Workshop, 2-3 December 2014 17
MLG door landed in Maryland park Engine part damaged car in Toronto
Why
EASAAD Workshop, 2-3 December 2014 18
Why
Deficiency in components which are
involved in fire protection or are intended to
minimize/retard the effects of fire/smoke in a
survivable crash (e.g. non-compliance with
the applicable flammability requirements)
EASAAD Workshop, 2-3 December 2014 19
Why
EASAAD Workshop, 2-3 December 2014 20
Why
Design features used to assist in the enquiry
following an accident (e.g. CVR, FDR, ELT
are not performing their intended function
EASAAD Workshop, 2-3 December 2014 21
Why
EASAAD Workshop, 2-3 December 2014 22
When – Types of AD
•Normal AD
•Emergency AD
EASAAD Workshop, 2-3 December 2014 23
When – Compliance Time
Establishing compliance time based on:
•Urgency of the Unsafe Condition
•Parts Availability
•Practicality of Performing the Required Tasks
•Impact of Required Actions on Existing Maintenance
and Overhaul Schedules
•Need for a “Phase-In Period”
EASAAD Workshop, 2-3 December 2014 24
What – Equipment AD
•For items with approval certificate such as
TSO, STC, Part Design Approval (PDA)
•AD applicability section identifies affected
components/installed modifications using
words “Installed on, but not limited to, [list
known affected aeronautical products].”
EASAAD Workshop, 2-3 December 2014 25
What – Equipment AD
EASAAD Workshop, 2-3 December 2014 26
What – AD on Airworthiness
Limitations
AD is required when:
•New or more restrictive Airworthiness Limitations
(AWL), Fuel System Limitations, Flight Manual
Limitations, Certification Maintenance Requirements
(CMR) are introduced post-certification.
Except if:
•Non-compliance with new or more restrictive
limitations/requirements will not result in unsafe
condition
EASAAD Workshop, 2-3 December 2014 27
What – AD on Airworthiness
Limitations
Example of “more restrictive”:
•Reduction of inspection interval
•Reduction in Safe Life Limit/mandatory replacement
time
•Reduction in operational limitations (e.g. Never Exceed
Speed)
•Change of inspection method from visual to NDI
EASAAD Workshop, 2-3 December 2014 28
What – AD on Airworthiness
Limitations
EASAAD Workshop, 2-3 December 2014 29
What – AD on Airworthiness
Limitations
Typical wording:
EASAAD Workshop, 2-3 December 2014 30
What – Unilateral AD
State of design authority may disagree with
TCCA on the unsafe condition and decide
not to issue AD
This type of AD issued by TCCA is generally
not of concern to EU operators
EASAAD Workshop, 2-3 December 2014 31
What – Unilateral AD
EASAAD Workshop, 2-3 December 2014 32
What – Supersede vs. Cancel
Supersedure
•ADs are superseded if a different Canadian AD is
issued
EASAAD Workshop, 2-3 December 2014 33
What – Supersede vs. Cancel
Cancellation
•ADs are cancelled if the requirements are completely
cancelled, with no other requirements, or if a foreign AD
is applicable
EASAAD Workshop, 2-3 December 2014 34
What – Supersede vs. Cancel
EASAAD Workshop, 2-3 December 2014 35
Differences from EASA
Wording used
“air time” is defined in CAR 101.01 and operators
are required to track that
EASAAD Workshop, 2-3 December 2014 36
EASA TCCA
Flight hours Hours Air Time
Does not approve
SBs
Approves SB
Differences from EASA
Approval of SB
CAR 521.356 If the Minister determines that a
corrective action is required to rectify an unsafe
condition in an aeronautical product, the holder of the
design approval document in respect of the
aeronautical product shall
(a) submit to the Minister for approval the corrective
action required to rectify the unsafe condition
EASAAD Workshop, 2-3 December 2014 37
Differences from EASA
Types of AD
EASAAD Workshop, 2-3 December 2014 38
EASA TCCA
AD Correction without AD
revision
Correction to AD requires
AD revision
Differences from EASA
EASAAD Workshop, 2-3 December 2014 39
Differences from EASA
EASAAD Workshop, 2-3 December 2014 40
EASAAD Workshop, 2-3 December 2014 41
What to do when caught in a difficult
situation?
AMOC
AMOC
3.5(2) “The State of Design shall, upon
request, assist in determining the
acceptability of a specific AMOC request
submitted to the Importing Party on an
airworthiness directive that has been issued
by the State of Design for its own civil
aeronautical products.”
TCCA/EASA Technical Implementation Procedures for
Airworthiness and Environmental Certification
EASAAD Workshop, 2-3 December 2014 42
AMOC
EASAAD Workshop, 2-3 December 2014 43
“…submitted to the Importing Party...”
AMOC
EASAAD Workshop, 2-3 December 2014 44
“The State of Design shall, upon request,
assist in determining the acceptability...”
AMOC
3.5(1) “An AMOC of general applicability that
is issued by either Competent Authority for
its own State of Design civil aeronautical
products is considered automatically
accepted by the other Competent
Authority.”
TCCA/EASA Technical Implementation Procedures for
Airworthiness and Environmental Certification
EASAAD Workshop, 2-3 December 2014 45
AMOC
“general applicability” would mean “Global
AMOCs” issued by TCCA
“Global AMOC” applies to multiple
owners/operators of affected Canadian state
of design aeronautical products
Issued to a DADH
EASAAD Workshop, 2-3 December 2014 46
Global AMOC
A letter issued by Chief of Continuing
Airworthiness with AMOC number (e.g
AARDG 2014/A23)
DADH distribute and communicate to
owner/operators (e.g. AOM)
Not published in TCCA website
EASAAD Workshop, 2-3 December 2014 47
Continuing Airworthiness Information
System
CAWIS
EASAAD Workshop, 2-3 December 2014 48
CAWIS
http://wwwapps3.tc.gc.ca/Saf-Sec-
Sur/2/CAWIS-SWIMN/logon-
cs0101.asp?lang=E
Repository of ADs
Includes Canadian and foreign ADs
applicable in Canada
EASAAD Workshop, 2-3 December 2014 49
CAWIS
EASAAD Workshop, 2-3 December 2014 50
When questions arise
Specific AD interpretation/questions
Contact person in the AD
EASAAD Workshop, 2-3 December 2014 51
When questions arise
AMOC
CAA of State of Registry/EASA
EASAAD Workshop, 2-3 December 2014 52
When questions arise
General questions on AD/CAWIS
cawwebfeedback@tc.gc.ca
EASAAD Workshop, 2-3 December 2014 53
How can TCCA improve our ADs?
Comments?
Suggestions?
Questions?
EASAAD Workshop, 2-3 December 2014 54
Thank you for your attention
EASAAD Workshop, 2-3 December 2014 55
Presented by: Philip Tang (philip.tang@tc.gc.ca)

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EASA AD Workshop 2014 - 06_TCCA AD presentation.pdf

  • 1. Airworthiness Directives – A TCCA Perspective EASA AD Workshop Cologne, Germany • 2-3 December 2014
  • 2. Outline • Issuing ADs – Why, When, What? • Differences from EASA • AMOCs • Continuing Airworthiness Information System (CAWIS) • When questions arise • How can TCCA ADs be improved? EASAAD Workshop, 2-3 December 2014 2
  • 3. What Canadian Aviation Regulation (CAR) 101.01: “an instruction issued by the Minister or by a civil aviation authority responsible for an aeronautical product type design that mandates a maintenance or operation action to ensure that an aeronautical product conforms to its type design and is in a condition for safe operation” EASAAD Workshop, 2-3 December 2014 3
  • 4. What Mandatory Continuing Airworthiness Instruction (MCAI) in accordance with ICAO Annex 8 Issued in English and French, except for Emergency AD which can be issued in English only EASAAD Workshop, 2-3 December 2014 4
  • 5. What Number of ADs issued: EASAAD Workshop, 2-3 December 2014 5 Year No. of ADs 2012 33 2013 41 2014 42
  • 6. Why An unsafe condition has been identified on an aeronautical product “aeronautical product” means any aircraft, aircraft engine, aircraft propeller or aircraft appliance or part or the component parts of any of those things, including any computer system and software Aeronautics Act EASAAD Workshop, 2-3 December 2014 6
  • 7. Why CAR compels the Minister of Transport to issue AD when there is unsafe condition 521.427 (1) The Minister shall issue an airworthiness directive in respect of an aeronautical product if (a) an unsafe condition exists in the aeronautical product and the condition is likely to exist or develop in other aeronautical products EASAAD Workshop, 2-3 December 2014 7
  • 8. Why However, TC can accept a campaign from the DADH instead of issuing an AD “Note: TCCA does not necessarily automatically issue an airworthiness directive. It may allow the manufacturer to campaign the replacement of defective parts. Where that campaign is not successful, then TCCA will issue an airworthiness directive.” TCCA/EASA Technical Implementation Procedures for Airworthiness and Environmental Certification EASAAD Workshop, 2-3 December 2014 8
  • 9. Why An unsafe condition has not been verified, but there is reason to believe that it exists or is likely to come into existence in an aeronautical product EASAAD Workshop, 2-3 December 2014 9
  • 10. Why EASAAD Workshop, 2-3 December 2014 10
  • 11. Why An existing AD (foreign or Canadian) needs to be cancelled or amended CAR 521.427 (1) The Minister shall issue an airworthiness directive in respect of an aeronautical product if (b) it is necessary to modify or cancel the requirements of an airworthiness directive issued by the foreign airworthiness authority having jurisdiction over the type design of the aeronautical product because the Minister considers the airworthiness directive inappropriate for reasons related to the environment, safety, the delayed receipt of an instruction issued by the foreign airworthiness authority or reliance on foreign legislation; or (c) it is necessary to modify or cancel a Canadian airworthiness directive that is in force, because a condition for issuance referred to in paragraph (a) or (b) has changed or ceased to exist. EASAAD Workshop, 2-3 December 2014 11
  • 12. Why EASAAD Workshop, 2-3 December 2014 12
  • 13. Why EASAAD Workshop, 2-3 December 2014 13
  • 14. Why Need to override a global Alternative Means of Compliance (AMOC) granted by the state of design EASAAD Workshop, 2-3 December 2014 14
  • 15. Why Emergency equipment intended to minimize the effects of survivable accidents is not performing its intended function EASAAD Workshop, 2-3 December 2014 15
  • 16. Why EASAAD Workshop, 2-3 December 2014 16
  • 17. Why Hazard of collateral damage/injuries on ground/personnel caused by components that have detached from the aircraft EASAAD Workshop, 2-3 December 2014 17 MLG door landed in Maryland park Engine part damaged car in Toronto
  • 18. Why EASAAD Workshop, 2-3 December 2014 18
  • 19. Why Deficiency in components which are involved in fire protection or are intended to minimize/retard the effects of fire/smoke in a survivable crash (e.g. non-compliance with the applicable flammability requirements) EASAAD Workshop, 2-3 December 2014 19
  • 20. Why EASAAD Workshop, 2-3 December 2014 20
  • 21. Why Design features used to assist in the enquiry following an accident (e.g. CVR, FDR, ELT are not performing their intended function EASAAD Workshop, 2-3 December 2014 21
  • 22. Why EASAAD Workshop, 2-3 December 2014 22
  • 23. When – Types of AD •Normal AD •Emergency AD EASAAD Workshop, 2-3 December 2014 23
  • 24. When – Compliance Time Establishing compliance time based on: •Urgency of the Unsafe Condition •Parts Availability •Practicality of Performing the Required Tasks •Impact of Required Actions on Existing Maintenance and Overhaul Schedules •Need for a “Phase-In Period” EASAAD Workshop, 2-3 December 2014 24
  • 25. What – Equipment AD •For items with approval certificate such as TSO, STC, Part Design Approval (PDA) •AD applicability section identifies affected components/installed modifications using words “Installed on, but not limited to, [list known affected aeronautical products].” EASAAD Workshop, 2-3 December 2014 25
  • 26. What – Equipment AD EASAAD Workshop, 2-3 December 2014 26
  • 27. What – AD on Airworthiness Limitations AD is required when: •New or more restrictive Airworthiness Limitations (AWL), Fuel System Limitations, Flight Manual Limitations, Certification Maintenance Requirements (CMR) are introduced post-certification. Except if: •Non-compliance with new or more restrictive limitations/requirements will not result in unsafe condition EASAAD Workshop, 2-3 December 2014 27
  • 28. What – AD on Airworthiness Limitations Example of “more restrictive”: •Reduction of inspection interval •Reduction in Safe Life Limit/mandatory replacement time •Reduction in operational limitations (e.g. Never Exceed Speed) •Change of inspection method from visual to NDI EASAAD Workshop, 2-3 December 2014 28
  • 29. What – AD on Airworthiness Limitations EASAAD Workshop, 2-3 December 2014 29
  • 30. What – AD on Airworthiness Limitations Typical wording: EASAAD Workshop, 2-3 December 2014 30
  • 31. What – Unilateral AD State of design authority may disagree with TCCA on the unsafe condition and decide not to issue AD This type of AD issued by TCCA is generally not of concern to EU operators EASAAD Workshop, 2-3 December 2014 31
  • 32. What – Unilateral AD EASAAD Workshop, 2-3 December 2014 32
  • 33. What – Supersede vs. Cancel Supersedure •ADs are superseded if a different Canadian AD is issued EASAAD Workshop, 2-3 December 2014 33
  • 34. What – Supersede vs. Cancel Cancellation •ADs are cancelled if the requirements are completely cancelled, with no other requirements, or if a foreign AD is applicable EASAAD Workshop, 2-3 December 2014 34
  • 35. What – Supersede vs. Cancel EASAAD Workshop, 2-3 December 2014 35
  • 36. Differences from EASA Wording used “air time” is defined in CAR 101.01 and operators are required to track that EASAAD Workshop, 2-3 December 2014 36 EASA TCCA Flight hours Hours Air Time Does not approve SBs Approves SB
  • 37. Differences from EASA Approval of SB CAR 521.356 If the Minister determines that a corrective action is required to rectify an unsafe condition in an aeronautical product, the holder of the design approval document in respect of the aeronautical product shall (a) submit to the Minister for approval the corrective action required to rectify the unsafe condition EASAAD Workshop, 2-3 December 2014 37
  • 38. Differences from EASA Types of AD EASAAD Workshop, 2-3 December 2014 38 EASA TCCA AD Correction without AD revision Correction to AD requires AD revision
  • 39. Differences from EASA EASAAD Workshop, 2-3 December 2014 39
  • 40. Differences from EASA EASAAD Workshop, 2-3 December 2014 40
  • 41. EASAAD Workshop, 2-3 December 2014 41 What to do when caught in a difficult situation? AMOC
  • 42. AMOC 3.5(2) “The State of Design shall, upon request, assist in determining the acceptability of a specific AMOC request submitted to the Importing Party on an airworthiness directive that has been issued by the State of Design for its own civil aeronautical products.” TCCA/EASA Technical Implementation Procedures for Airworthiness and Environmental Certification EASAAD Workshop, 2-3 December 2014 42
  • 43. AMOC EASAAD Workshop, 2-3 December 2014 43 “…submitted to the Importing Party...”
  • 44. AMOC EASAAD Workshop, 2-3 December 2014 44 “The State of Design shall, upon request, assist in determining the acceptability...”
  • 45. AMOC 3.5(1) “An AMOC of general applicability that is issued by either Competent Authority for its own State of Design civil aeronautical products is considered automatically accepted by the other Competent Authority.” TCCA/EASA Technical Implementation Procedures for Airworthiness and Environmental Certification EASAAD Workshop, 2-3 December 2014 45
  • 46. AMOC “general applicability” would mean “Global AMOCs” issued by TCCA “Global AMOC” applies to multiple owners/operators of affected Canadian state of design aeronautical products Issued to a DADH EASAAD Workshop, 2-3 December 2014 46
  • 47. Global AMOC A letter issued by Chief of Continuing Airworthiness with AMOC number (e.g AARDG 2014/A23) DADH distribute and communicate to owner/operators (e.g. AOM) Not published in TCCA website EASAAD Workshop, 2-3 December 2014 47
  • 49. CAWIS http://wwwapps3.tc.gc.ca/Saf-Sec- Sur/2/CAWIS-SWIMN/logon- cs0101.asp?lang=E Repository of ADs Includes Canadian and foreign ADs applicable in Canada EASAAD Workshop, 2-3 December 2014 49
  • 50. CAWIS EASAAD Workshop, 2-3 December 2014 50
  • 51. When questions arise Specific AD interpretation/questions Contact person in the AD EASAAD Workshop, 2-3 December 2014 51
  • 52. When questions arise AMOC CAA of State of Registry/EASA EASAAD Workshop, 2-3 December 2014 52
  • 53. When questions arise General questions on AD/CAWIS cawwebfeedback@tc.gc.ca EASAAD Workshop, 2-3 December 2014 53
  • 54. How can TCCA improve our ADs? Comments? Suggestions? Questions? EASAAD Workshop, 2-3 December 2014 54
  • 55. Thank you for your attention EASAAD Workshop, 2-3 December 2014 55 Presented by: Philip Tang (philip.tang@tc.gc.ca)