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Airworthiness directives › 2023-07-04

AD 2023-07-04 Airworthiness Directives; Bombardier, Inc., Airplanes

2023-05-30
2023-04-24
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Airframe
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Applicability*9

This AD applies to Bombardier, Inc., Model CL-600-2B16 (604 Variant) airplanes, certificated in any category, serial numbers (S/N) 5301 through 5665 inclusive, 5701 through 5988 inclusive, and 6050 through 6160 inclusive.

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: Do the applicable actions specified in paragraph (g)(1) through (3) of this AD. (1) For Model CL-600-2B16 (604 variant), S/N 5301 through 5665 inclusive: Revise the existing AFM to incorporate the information specified in paragraphs (g)(1)(i) and (ii) of this AD of Bombardier Challenger 604 Airplane Flight Manual—Publication No. PSP 604-1, Revision 120, dated December 8, 2020. (i) Sub-section 2. “Automatic Flight Control System,” of section 02-08, Systems Limitations, of Chapter 2—LIMITATIONS. (ii) Sub-sub-section B., “Engine Failure in Climb During (V) ALTS CAP or (V) ALTV CAP,” of sub-section 1. “Single Engine Procedures” of section 05-03, “Single Engine Procedures,” of Chapter 5—ABNORMAL PROCEDURES. Note 1 to paragraph (g)(1): For obtaining Bombardier Challenger 604 Airplane Flight Manual—Publication No. PSP 604-1, use Document Identification No. CH 604 AFM. (2) For Model CL-600-2B16 (604 variant), S/N 5701 through 5988 inclusive: Revise the existing AFM to incorporate the information specified in paragraphs (g)(2)(i) and (ii) of this AD of Bombardier Challenger 605 Airplane Flight Manual—Publication No. PSP 605-1, Revision 58, dated December 8, 2020. (i) Sub-section 2. “Automatic Flight Control System,” of section 02-08, Systems Limitations, of Chapter 2—LIMITATIONS. (ii) Sub-sub-section B., “Engine Failure in Climb During (V) ALTS CAP or (V) ALTV CAP,” of sub-section 1. “Single Engine Procedures” of section 05-03, “Single Engine Procedures,” of Chapter 5—ABNORMAL PROCEDURES. Note 2 to paragraph (g)(2): For obtaining Bombardier Challenger 605 Airplane Flight Manual—Publication No. PSP 605-1, use Document Identification No. CH 605 AFM. (3) For Model CL-600-2B16 (604 variant), S/N 6050 through 6160 inclusive: Revise the existing AFM to incorporate the information specified in paragraphs (g)(3)(i) and (ii) of this AD of Bombardier Challenger 650 Airplane Flight Manual—Publication No. PSP 650-1, Revision 23, dated December 8, 2020. (i) Sub-section 2. “Automatic Flight Control System,” of section 02-08, Systems Limitations, of Chapter 2—LIMITATIONS. (ii) Sub-sub-section B., “Engine Failure in Climb During (V) ALTS CAP or (V) ALTV CAP,” of sub-section 1. “Single Engine Procedures” of section 05-03, “Single Engine Procedures,” of Chapter 5—ABNORMAL PROCEDURES. Note 3 to paragraph (g)(3): For obtaining Bombardier Challenger 650 Airplane Flight Manual—Publication No. PSP 650-1, use Document Identification No. CH 650 AFM.

Unsafe condition

This AD was prompted by a determination that during (V) ALTS CAP or (V) ALTV CAP modes, the flight guidance/autopilot does not account for engine failure while capturing an altitude. The FAA is issuing this AD to address the possible occurrence of an engine failure during or before a climb while in (V) ALTS CAP or (V) ALTV CAP modes, which could cause the airspeed to decrease rapidly. The unsafe condition, if not addressed, could result in the airplane failing to maintain a safe operating speed.

Affected ADs

None.

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