Airworthiness directives › 2018-17-02
AD 2018-17-02 Airworthiness Directives; Bombardier, Inc., Airplanes
Applicability*9
This AD applies to the Bombardier, Inc., airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category. (1) Model CL-600-1A11 (600) airplanes, serial numbers 1002 and 1004 through 1085 inclusive. (2) Model CL-600-2A12 (601) airplanes, serial numbers 3001 through 3066 inclusive. (3) Model CL-600-2B16 (601-3A and 601-3R Variants) airplanes, serial numbers 5001 through 5194 inclusive. (4) Model CL-600-2B16 (604 Variant) airplanes, serial numbers 5301 through 5665 inclusive, 5701 through 5990 inclusive, and 6050 and subsequent.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
For airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD: Within 60 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the life limit AWL tasks identified in table 1 to paragraph (g) of this AD, as specified in the applicable service information identified in paragraph (g)(1), (g)(2), or (g)(3) of this AD. The initial compliance time is within 500 flight cycles of the effective date of this AD, or at the applicable time (in terms of landings) specified in the applicable AWL task identified in table 1 to paragraph (g) of this AD, whichever occurs later. (1) For Model CL-600-1A11 (600) airplanes, Section 5-10-10, “Time Limits (Structural),” of Section 5-10-00, “Airworthiness Limitations,” of Bombardier Challenger 600 Time Limits/Maintenance Checks, Publication No. PSP 605, Revision 39, dated January 8, 2018. (2) For Model CL-600-2A12 (601) airplanes, the applicable task specified in paragraph (g)(2)(i), (g)(2)(ii), or (g)(2)(iii) of this AD, as identified in Section 5-10-00, “Airworthiness Limitations,” of Bombardier Challenger 601 Time Limits/Maintenance Checks, Publication No. PSP 601-5, Revision 46, dated January 8, 2018. (i) Section 5-10-10, “Time Limits (Structural)—Pre SB 601−0280.” (ii) Section 5-10-11, “Time Limits (Structural)—Post SB 601−0280.” (iii) Section 5-10-12, “Time Limits (Structural)—Post SB 601−0360.” (3) For Model CL-600-2B16 (601-3A and 601-3R Variants) airplanes, the applicable task specified in paragraph (g)(3)(i), (g)(3)(ii), or (g)(3)(iii) of this AD, as identified in Section 5-10-00, “Airworthiness Limitations,” of Bombardier Challenger 601 Time Limits/Maintenance Checks, Publication No. PSP 601A-5, Revision 42, dated January 8, 2018. (i) Section 5-10-10, “Time Limits (Structural).” (ii) Section 5-10-11, “Time Limits (Structural).” (iii) Section 5-10-12, “Time Limits (Structural).” ER15AU18.002
Unsafe condition
This AD was prompted by a determination that the safe life limits of the horizontal stabilizer trim actuator (HSTA) attachment pins and trunnions were not listed in certain airworthiness limitations (AWLs) and that the HSTA attachment pins and trunnions were not serialized. We are issuing this AD to prevent failure of the HSTA attachment pins and trunnions, which could lead to a disconnect of the horizontal stabilizer and subsequent loss of the airplane.
Affected ADs
None.
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