AD 2016-08-15

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Bombardier, Inc. Airplanes

AD Number
2016-08-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2015-3988
FR Citation
81 FR 26121

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Various Airworthiness Directives; Bombardier, Inc. Airplanes

Unsafe Condition

Incorrectly oriented or fractured fasteners attaching the inboard flap hinge-box forward fitting at Wing Station (WS) 76.50 and WS 127.25 could result in premature failure of the fasteners, leading to detachment of the flap hinge box and the flap surface, and consequent loss of control of the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the inboard flap fasteners of the hinge-box forward fitting at WS 76.50 and WS 127.25 to determine the orientation and condition of the fasteners. Replace the incorrectly oriented or fractured fasteners. If necessary, perform repetitive inspections until the terminating action is accomplished.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 12 months of the effective date of this AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Bombardier, Inc. Model CL-600-2B16 airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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