Chapter 1: CARs and Regulations - Standard 566, 571, 573, Approved Data, Maintenance Release
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CARs and Regulations - Standard 566, 571, 573, Approved Data, Maintenance Release
Overview
This chapter covers the regulatory framework governing aircraft maintenance in Canada under the Canadian Aviation Regulations (CARs). It focuses on the standards that define how maintenance must be performed, recorded, and certified, as well as the classification of repairs and modifications. The key standards addressed are Standard 571 (Maintenance), Standard 573 (Approved Maintenance Organizations), and Standard 566 (Maintenance Control Systems). Understanding these regulations is essential for ensuring airworthiness and compliance during all maintenance activities.
Key Concepts
Maintenance Standards and Data Requirements (Standard 571.02)
Manufacturer's Recommendations as Primary Standard
Standard 571.02 establishes that all maintenance must be performed in accordance with the aircraft manufacturer's recommended practices. When the aircraft manufacturer's recommendations conflict with those of an engine, propeller, or appliance manufacturer, the aircraft manufacturer's recommendations take precedence. This hierarchy ensures that airframe integrity and overall aircraft compatibility are prioritized over component-specific guidance.
Use of Alternative Standards
When the manufacturer has not published specific recommendations for a task, the AME must use standard industry practices. These include:
- Methods published by Transport Canada
- Methods published by a foreign civil aviation authority with which Canada has an agreement
- Methods published by the manufacturer of a similar product
- Other generally accepted industry practices
Advisory Circular AC 43.13 (issued by the FAA) is recognized as a standard industry practice and may be used when manufacturer data is unavailable.
Personnel Qualification Requirements
Standard 571.02(3) requires that persons performing specified tasks meet the applicable personnel qualification or training standards. This ensures that complex or safety-critical tasks are performed only by individuals with appropriate training and certification.
Maintenance Recording Requirements (Standard 571.03)
Required Elements of a Maintenance Record Entry
Standard 571.03 specifies the information that must be recorded for each maintenance task:
- Product identification (aircraft registration, component part number, serial number)
- Description of work performed
- Reference to standards used (if other than manufacturer's recommended practice)
- Date of maintenance
- Employee identification (AME license number or personal identifier)
- Details of defects found during disassembly
Documentation of Defects Found During Disassembly
Standard 571.03(f) specifically requires that when disassembly is required during maintenance, a general description of any defect found prior to re-assembly must be recorded. This ensures that hidden damage is documented and traceable.
Recording of Alternative Standards Used
Standard 571.03(c) requires that when a standard other than the manufacturer's recommended practice is used, the reference to that standard must be recorded. This provides traceability and accountability for the maintenance performed.
Documentation of Partially Completed Work
Standard 571.03(g) requires that when a task is partially completed, a general description of any outstanding work must be recorded, including the specific location of any parts or systems that have been disturbed. This prevents incomplete work from being forgotten and ensures proper completion.
Information NOT Required in Maintenance Records
The cost of the repair is not a required element in the technical maintenance record. The focus is on technical accuracy and traceability, not financial information.
Classification of Repairs and Modifications (Standard 571.06)
Major Repair Definition
A major repair is defined as a repair that has other than a negligible effect on:
- Weight
- Balance
- Structural strength
- Performance
- Powerplant operation
- Flight characteristics
- Environmental characteristics
The classification is based on the effect on airworthiness, not on cost, specific processes (such as welding), or the type of structure involved.
Major Modification Definition
A major modification is an alteration that has other than a negligible effect on the same characteristics listed above for major repairs. A change in color or other cosmetic alterations with negligible effect does not qualify as a major modification.
Approved Data vs. Acceptable Data
Standard 571.06 distinguishes between two categories of technical data:
Approved Data includes documents that have undergone a formal type design approval process:
- Type Certificates (TC)
- Supplemental Type Certificates (STC)
- Repair Design Approvals (RDA)
- Type Certificate Data Sheets (TCDS)
Acceptable Data includes documents that provide an acceptable means of compliance but have not undergone formal approval for a specific installation:
- Advisory Circulars (e.g., FAA AC 43.13-1B, AC 43.13-2A)
- Transport Canada advisory documents
- Foreign airworthiness authority advisory documents (with which Canada has an agreement)
Application of Data Types
- Major repairs and modifications require approved data (STC or RDA)
- Minor repairs may use acceptable data (such as AC 43.13)
- The AME can install a modification but cannot approve the design; design approval requires an STC or RDA
Maintenance Release Requirements (Standard 571.10)
Definition and Purpose
A maintenance release is the certification statement that maintenance has been performed correctly and the aeronautical product is fit for return to service. It is required for all maintenance performed, not just major repairs or modifications.
Required Elements of a Maintenance Release
The maintenance release must certify that:
- The maintenance has been performed in accordance with applicable standards
- The aeronautical product is ready for return to service
Authorization to Sign a Maintenance Release
For a major repair on a large aircraft operated under Part VII (commercial operations), the person signing the maintenance release must:
- Hold the appropriate AME license category (e.g., M or S)
- Have the applicable certification authority
The regulation focuses on the license and certification authority, not solely on whether the person performed the work.
Maintenance Release for Components Overhauled Outside an AMO
When maintenance is performed outside an AMO under a maintenance arrangement per CARs 573.11, the maintenance release must be issued by the AMO that has the arrangement. The AMO is responsible for the work performed under their control.
Specialized Maintenance Requirements (Standard 571.04)
Approved Maintenance Organization (AMO) Requirements
Specialized maintenance such as welding on primary structures and non-destructive testing (NDT) must be performed by an AMO with the appropriate category for that process. A generic AME license or non-aviation certification is not sufficient for these specialized tasks.
Maintenance Control for Commercial Operations (Standard 571.05)
AMO Control Requirement
Maintenance on aircraft operated under Part IV (flight training) or Part VII (commercial operations) must be performed under the control of an AMO approved pursuant to section 573.02. This ensures a higher level of oversight for commercial and training aircraft.
Elementary Work (Standard 625)
Definition and Examples
Elementary work is defined in Standard 625 and includes simple tasks that do not require complex technical judgment:
- Changing tires
- Servicing (fluids, lubricants)
- Minor adjustments
- Simple inspections
Maintenance Release for Elementary Work
Even elementary work requires a maintenance release if it constitutes a maintenance action. For example, blending out a corrosion pit (even within allowable limits) is a maintenance task and requires a maintenance release.
Used Parts (Standard 571.08)
Requirements for Installation
When installing a used part on an aircraft, Standard 571.08 requires confirmation that:
- The part is in a serviceable condition
- The part conforms to its type design
These requirements ensure the part is airworthy. Cost, paint condition, or origin from a similar model are not primary regulatory requirements.
Important Regulations and Procedures
Hierarchy of Maintenance Data
- Aircraft manufacturer's recommendations (primary)
- Engine/propeller/appliance manufacturer's recommendations (when compatible with aircraft manufacturer)
- Standard industry practices (when manufacturer data is unavailable)
- Acceptable data (advisory circulars, foreign authority documents)
- Approved data (STC, RDA) for major repairs/modifications
Documentation Flow for Maintenance Tasks
- Identify the task and required data
- Determine if manufacturer data exists
- If not, select appropriate acceptable data
- Record the standard used (if not manufacturer's)
- Document defects found during disassembly
- Record partially completed work details
- Complete maintenance release upon task completion
Classification Decision Tree
- Does the alteration have more than negligible effect on airworthiness characteristics?
- Yes → Major repair or major modification (requires approved data)
- No → Minor repair or minor modification (may use acceptable data)
Common Relationships Between Concepts
Relationship Between Data Type and Repair Classification
- Minor repairs typically use acceptable data (AC 43.13)
- Major repairs require approved data (STC or RDA)
- The AME can perform the installation but cannot approve the design for major modifications
Relationship Between Maintenance Type and Release Requirements
- All maintenance requires a maintenance release
- Elementary work requires a release if it is a maintenance action
- The release certifies proper performance and return to service
Relationship Between AMO Control and Specialized Tasks
- Welding on primary structures requires an AMO with appropriate category
- NDT requires an AMO with appropriate category
- Commercial operations require AMO control for all maintenance
Relationship Between Documentation and Traceability
- Recording alternative standards ensures traceability
- Documenting defects found during disassembly ensures hidden damage is tracked
- Recording partially completed work prevents oversight
- The maintenance release provides the final certification of airworthiness
Diagram
Practice this chapter
Reinforce CARs and Regulations - Standard 566, 571, 573, Approved Data, Maintenance Release with 25 Transport Canada–style practice questions, matched to your weak areas.