AD 92-13-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-600-1A11 (CL-600) | Airworthiness Directives; CANADAIR, LTD. Models CL-600-1A11, CL-600-2B16 and CL-600-2A12 Series Airplanes |
| aircraft | Bombardier Inc. | CL-600-2A12 (CL-601) | Airworthiness Directives; CANADAIR, LTD. Models CL-600-1A11, CL-600-2B16 and CL-600-2A12 Series Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B16 (CL-601-3A) | Airworthiness Directives; CANADAIR, LTD. Models CL-600-1A11, CL-600-2B16 and CL-600-2A12 Series Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B16 (CL-601-3R) | Airworthiness Directives; CANADAIR, LTD. Models CL-600-1A11, CL-600-2B16 and CL-600-2A12 Series Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B16 (CL-604) | Airworthiness Directives; CANADAIR, LTD. Models CL-600-1A11, CL-600-2B16 and CL-600-2A12 Series Airplanes |
Unsafe Condition
Potential crossed wiring in the engine fire extinguishing and detection systems and unlocked or inoperative pins in electrical connectors could lead to severe damage to the airplane in the event of an engine fire.
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Required Actions
Within 30 days after February 11, 1992, inspect for crossed wiring and unlocked/inoperative pins in engine fire systems per applicable service bulletins. If discrepancies found, correct them and replace connectors before further flight. Within 120 days after July 23, 1992, or when fire bottles are removed, modify warning harnesses and perform functional tests per service bulletins.
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Compliance Time
Within 30 days after February 11, 1992 (for initial inspections) and within 120 days after July 23, 1992 (for modifications), or when fire bottles are removed, whichever occurs first.
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Affected Aircraft
CANADAIR, LTD. Models CL-600-1A11 (serials 1004-1085 except 1037), CL-600-2A12 (serials 3001-3066), and CL-600-2B16 (serials 5001-5049).
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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