Airworthiness directives › 2019-26-10
AD 2019-26-10 Airworthiness Directives; Bombardier, Inc. Airplanes
Applicability*9
This AD applies to the airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, all serial numbers. (1) Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series 700, 701 & 702) airplanes. (2) Bombardier, Inc., Model CL-600-2D15 (Regional Jet Series 705) airplanes. (3) Bombardier, Inc., Model CL-600-2D24 (Regional Jet Series 900) airplanes. (4) Bombardier, Inc., Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 30 days after the effective date of this AD, revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Task 251700-202, “Functional Check of the Flight Compartment Door Decompression Latches,” of Section 1, “Systems and Power Plant Program,” Subject 1-25, “Equipment and Furnishings,” of the Bombardier Model CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 Series 700/705/900/1000 Maintenance Review Board Report, Maintenance Requirements Manual—Part 1, Volume 1, CSP B-053, Revision 18, dated July 25, 2018. The initial compliance time for doing the task is within 8,000 flight hours after this task is incorporated into the existing maintenance or inspection program, or within 30 days after the effective date of this AD, whichever occurs later. Repeat the task thereafter at intervals not to exceed 8,000 flight hours.
Unsafe condition
This AD was prompted by a report of incorrectly installed flight compartment door edge protection plates on both sides of the upper decompression panel. The FAA is issuing this AD to address incorrect installation of the flight compartment door edge protection plates on both sides of the flight compartment door upper decompression panel. This condition, if not corrected, could result in the inability of the flight compartment door upper decompression panel to open during a rapid decompression event. This inability to relieve the pressure in the flight compartment may compromise the structural integrity of the bulkhead between the flight compartment and the passenger cabin.
Affected ADs
None.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1