Canadair Limited Airworthiness Directives

99 ADs indexed for Canadair Limited aircraft.

Models

Recent ADs

2023-07-10 Recurring

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Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

Unsafe Condition: uncommanded opening of the water doors, which, at high speed during the take-off run, water pick-up run, or landing run, could cause serious damage to the airplane.

Effective: Jun 20, 2023 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

2019-25-11 Recurring

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Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

Unsafe Condition: cracks on the wing lower skin under the drag angle at a certain wing station (WS)

Effective: Feb 10, 2020 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

2019-08-12 Recurring

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Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

Unsafe Condition: parts manufactured with a higher percentage of fiberglass may cause wear and rupture of control cables due to greater friction if contacted, which could lead to reduced controllability of the airpl...

Effective: Jun 13, 2019 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

2019-02-05 Recurring

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Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

Unsafe Condition: Cracked wing structure, which could result in failure of the wing.

Effective: Mar 22, 2019 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

2017-17-17 Recurring

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Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

Unsafe Condition: Failure of the screw cap or end cap of certain accumulators, which could result in impact damage to various components, potentially leading to fuel spillage, uncommanded flap movement, or loss of a...

Effective: Oct 11, 2017 Category: aircraft Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.; Canadair Limited) Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2017-15-14

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Airworthiness Directives; Bombardier, Inc. (Type Certificate Previously Held by Canadair Limited) Airplanes

Unsafe Condition: An oxygen bottle was found loose while the clamp strap was in the locked position, caused by the quick release latch assembly not achieving the proper clamping pressure.

Effective: Sep 5, 2017 Category: aircraft Compliance: Within 12 months after the effective date of this AD.

Why matched: Airworthiness Directives; Bombardier, Inc. (Type Certificate Previously Held by Canadair Limited) Airplanes

2001-02-05

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Airworthiness Directives; CL-604 Variant of Bombardier Model Canadair CL-600-2B16 Series Airplanes Modified in Accordance With Supplemental Type Certificate SA8060NM-D, SA8072NM-D, or SA8086NM-D

Unsafe Condition: Electrical sparks from a grounded object contacting the fuel port flood light housing of the fuel service panel, which could result in a fuel fire due to the close proximity of the fuel service pan...

Effective: Mar 5, 2001 Category: aircraft Compliance: Within 90 days after the effective date of March 5, 2001.

Why matched: Airworthiness Directives; BOMBARDIER, INC. (Formerly Canadair) CL-604 Variant of Bombardier Model Canadair CL-600-2B16 series airplanes

2000-01-51

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Airworthiness Directives; CL-604 Variant of Bombardier Model Canadair CL-600-2B16 Series Airplanes Modified in Accordance With Supplemental Type Certificate SA8060NM-D, SA8072NM-D, or SA8086NM-D

Unsafe Condition: An electrical spark was noted when the fuel cap chain contacted the maintenance light housing of the fuel service panel, which could result in a fuel fire due to the close proximity of the fuel ser...

Effective: Jan 7, 2000 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; CL-604 Variant of Bombardier Model Canadair CL-600-2B16 Series Airplanes Modified in Accordance With Supplemental Type Certificate SA8060NM-D, SA8072NM-D, or SA8086NM-D

96-23-13

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Airworthiness Directives; Canadair Model CL-215-1A10 Series Airplanes

Unsafe Condition: Extra unconnected bare copper wire inside DC generators (part number 2CM70D-( )) could cause a short circuit and present a fire hazard if a combustible fuel-air mixture is present.

Effective: Dec 5, 1996 Category: aircraft Compliance: Within 50 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Canadair Model CL-215-1A10 Series Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

96-05-06

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Airworthiness Directives; Canadair Model CL-215-1A10 Series Airplanes

Unsafe Condition: Loose or missing hardware on a terminal from an inverter power relay shorted out a voltage regulator in the main distribution center, causing total loss of electrical power during flight.

Effective: Mar 22, 1996 Category: aircraft Compliance: Within 10 flight hours after the effective date of this AD. Discrepancies must be corrected prior...

Why matched: Airworthiness Directives; Canadair Model CL-215-1A10 Series Airplanes

Amdt-39-9532

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Airworthiness Directives; Canadair Model CL-215-1A10 Series Airplanes

Unsafe Condition: Total loss of electrical power during flight caused by shorting out of the voltage regulator in the main distribution center.

Effective: Mar 22, 1996 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Canadair Model CL-215-1A10 Series Airplanes

93-16-06 R2

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Airworthiness Directives: Canadair Models CL-215-1A10 and CL-215-6B11 Series Airplanes

Unsafe Condition: Potential flutter of the rudder-aileron interconnect tab, which could result in reduced controllability of the airplane.

Effective: Oct 15, 1995 Category: aircraft Compliance: Within 12 months after the effective date of this AD

Why matched: Airworthiness Directives: Canadair Models CL-215-1A10 and CL-215-6B11 Series Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Amdt-39-9157

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Airworthiness Directives; Bombardier (Formerly Canadair) Model CL-600-2B19 (Regional Jet Series 100) Series Airplanes

Unsafe Condition: Passenger doors froze shut during flight and could not be opened after landing.

Effective: Apr 7, 1995 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bombardier (Formerly Canadair) Model CL-600-2B19 (Regional Jet Series 100) Series Airplanes

95-04-05

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Airworthiness Directives; Bombardier (Formerly Canadair) Model CL-600-2B19 (Regional Jet Series 100) Series Airplanes

Unsafe Condition: Passenger doors freezing shut during flight, preventing passengers from exiting in an emergency.

Effective: Apr 7, 1995 Category: aircraft Compliance: Within 14 days after the effective date (April 7, 1995), and subsequent intervals not exceeding 3...

Why matched: Airworthiness Directives; Bombardier (Formerly Canadair) Model CL-600-2B19 (Regional Jet Series 100) Series Airplanes

95-03-06

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Airworthiness Directives; Canadair Model CL-600-1A11, -2A12, and -2B16 Series Airplanes

Unsafe Condition: Unintentional engine shutdown due to throttle levers bypassing the idle stop into the shut-off position during taxiing or flight.

Effective: Mar 31, 1995 Category: aircraft Compliance: Within 50 hours time-in-service after the effective date (for the initial test) and within 150 ho...

Why matched: Airworthiness Directives; Canadair Model CL-600-1A11, -2A12, and -2B16 Series Airplanes

Amdt-39-9143

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Airworthiness Directives; Canadair Model CL-600-1A11, -2A12, and -2B16 Series Airplanes

Unsafe Condition: Unintentional engine shutdown due to problems associated with operation of the engine throttle quadrant.

Effective: Mar 31, 1995 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Canadair Model CL-600-1A11, -2A12, and -2B16 Series Airplanes

94-22-06

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Airworthiness Directives; Bombardier (formerly Canadair) Model CL-600-2B19 (Regional Jet Series 100) Series Airplanes

Unsafe Condition: The attitude and heading reference system (AHRS) could send conflicting input to the stall protection computer (SPC), leading to loss of stall warning protection on the airplane.

Effective: Dec 12, 1994 Category: aircraft Compliance: Within 30 days after the effective date (for SPS input wiring) and within 9 months after the effe...

Why matched: Airworthiness Directives; Bombardier (formerly Canadair) Model CL-600-2B19 (Regional Jet Series 100) Series Airplanes

94-14-08

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Airworthiness Directives; Canadair Model CL-600-2B16 (CL-601-3A) Series Airplanes

Unsafe Condition: Chafing of the wiring harness of the air driven generator (ADG) could result in electrical shorting, leading to loss of ADG power to the essential bus during emergency deployment.

Effective: Aug 10, 1994 Category: aircraft Compliance: Within 25 hours time-in-service after the effective date (for inspection) and within 60 days afte...

Why matched: Airworthiness Directives; Canadair Model CL-600-2B16 (CL-601-3A) Series Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

94-08-15

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Airworthiness Directives; Canadair Model CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A) Series Airplanes

Unsafe Condition: Failure of the flap actuator on the left wing inboard flap could cause asymmetric deployment or retraction (blow back) of the flaps, which could reduce controllability of the airplane.

Effective: May 20, 1994 Category: aircraft Compliance: Within 30 days after the effective date of this AD, or prior to further flight if discrepancies a...

Why matched: Airworthiness Directives; Canadair Model CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A) Series Airplanes

94-01-14

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Airworthiness Directives; CANADAIR LIMITED Model CL-600-2B19 (Regional Jet) Series Airplanes

Unsafe Condition: The retaining ring can become unseated from its positional groove on the input shaft of the integrated drive generator (IDG) constant speed drive (CSD), resulting in loss of IDG oil and subsequent ...

Effective: Jan 28, 1994 Category: aircraft Compliance: Within 14 days after the effective date of this AD, or prior to further flight as specified.

Why matched: Airworthiness Directives; CANADAIR LIMITED Model CL-600-2B19 (Regional Jet) Series Airplanes

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