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AIRWORTHINESS REQUIREMENTS TEMPORARY REVISION 2B−2280 C Airworthiness Requirements Part 2 of Maintenance Requirements Manual Appendix B − Airworthiness Limitations Page 1 of 3 FILING INSTRUCTIONS: This Temporary Revision (TR) 2B−2280 supersedes TR 2B−2276. Remove and discard TR 2B−2276 and insert this TR 2B−2280 facing page 2B−40, in Part 2 of the Maintenance Requirements Manual (MRM).
Record the incorporation of this Temporary Revision on the RECORD OF TEMPORARY REVISIONS sheet at the front of the MRM Part 2.
Keep this Temporary Revison until normal revision service incorporates this information into the Maintenance Requirements Manual.
DESCRIPTION: This Temporary Revision is issued to revise AWL 53−41−206 and AWL 53−41−207.
Superseded TR 2B−2276 was issued to add AWL NUMBER 53−41−206 and AWL 53−41−207.
CL 600 2B19 Jun 12/2020 TR# 2B−2280 The contents of this Temporary Revision have been approved by the Chief, Engineering (or designate), National Aircraft Certification Branch, Transport Canada Civil Aviation Date 12 June 2020 . Signed P. Ngassam.
AIRWORTHINESS REQUIREMENTS TEMPORARY REVISION 2B−2280 C Airworthiness Requirements Part 2 of Maintenance Requirements Manual Appendix B − Airworthiness Limitations Page 2 of 3
STRUCTURAL AIRWORTHINESS LIMITATIONS NDT
INSPECTION INTERVAL AWL NUMBER
MRB TASK
REFERENCE NDT MANUAL DESCRIPTION INSPECTTYPE 51000 lb MTOW 53000 lb MTOWNUMBER REFERENCE REF . TYPE THRESHOLD (LANDINGS) REPEAT (LANDINGS)
THRESHOLD (LANDINGS) REPEAT (LANDINGS) 53−41−206 Superseded by 53−41−207 CL 600 2B19 Jun 12/2020 TR# 2B−2280
AIRWORTHINESS REQUIREMENTS TEMPORARY REVISION 2B−2280 C Airworthiness Requirements Part 2 of Maintenance Requirements Manual Appendix B − Airworthiness Limitations Page 3 of 3 AWL NUMBER
INSPECTION INTERVAL
INSPECT
TYPEDESCRIPTION NDT MANUAL REF .
MRB TASK
REFERENCE AWL NUMBER 53000 lb MTOW51000 lb MTOWINSPECT
TYPEDESCRIPTION NDT MANUAL REF .
MRB TASK
REFERENCE AWL
NUMBER REPEAT (LANDINGS)
THRESHOLD (LANDINGS) REPEAT (LANDINGS)
THRESHOLD (LANDINGS)
INSPECT
TYPEDESCRIPTION NDT MANUAL REF .
MRB TASK
REFERENCE 53−41−207 53−41−206 Part 6 53−41−207 Part 6 Longitudinal skin splice at STR 6 and 20 EC Inspection procedure (NDTM Part 6, Chap.
53−41−206) PHASE−IN:
Within 2,000 FC from the last inspection IAW AWL 53−41−109 or AWL 53−41−206 or Alternate MOI inspection procedure (NDTM Part 6, Chap. 53−41−207) PHASE−IN:
For AC that were previously inspected IAW AWL 53−41−109 or AWL 53−41−206*, within 2,000 FC from the last inspection For AC that were previously inspected IAW AWL 53−41−205:
AC that had accumulated less than 42,000 FC at the time of their last inspection: within 6,000 FC from the last inspection AC that had accumulated 42,000 FC or more at the time of their last inspection: before 48,000 FC *Note: Switching from EC to MOI inspection is permitted only once in the lifetime of the aircraft, i.e.
inspection procedure must continue to be MOI after switching.
Special Detailed Special Detailed 40000 40000 2000 6000 40000 40000 2000 6000 CL 600 2B19 Jun 12/2020 TR# 2B−2280