FAA 8110.53 : 2005
Current
The latest, up-to-date edition.
RECIPROCAL ACCEPTANCE OF REPAIR DESIGN DATA APPROVALS BETWEEN FAA AND TCCA
Hardcopy , PDF
English
01-01-2005
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 PURPOSE
2 DISTRIBUTION
3 WHAT THIS ORDER PERMITS AND APPLIES TO
4 BACKGROUND
5 ACCEPTANCE PROCEDURES
6 REPAIRS TO ENGINES, PROPELLERS AND OTHER COMPONENTS,
APPLIANCES, OR BOTH
7 CANADIAN REPAIR DESIGN APPROVALS - TYPICAL DOCUMENTATION
8 U.S. REPAIR DESIGN APPROVALS - TYPICAL DOCUMENTATION
9 RELATED PUBLICATIONS
10 REQUESTS FOR INFORMATION
11 SUGGESTIONS FOR IMPROVEMENT
12 RECORDS MANAGEMENT
APPENDIX 1 ACRONYMS AND DEFINITIONS
Instructs Federal Aviation Administration (FAA) certification staffs how to implement the October 2003 Memorandum of Understanding (MOU) between us and Transport Canada Civil Aviation (TCCA) for the design approval of aeronautical product repairs. Guides the reciprocal acceptance of repair design data approved by the FAA, the TCCA, and our respective designees/delegates.
| DocumentType |
Standard
|
| Pages |
11
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 43-10 : 2011 | UNITED STATES-CANADIAN BILATERAL AVIATION SAFETY AGREEMENT MAINTENANCE IMPLEMENTATION PROCEDURES |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| FAA 8300.10 : 2004 | AIRWORTHINESS INSPECTOR'S HANDBOOK |
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