AD 2016-24-03

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Bombardier, Inc. Airplanes

AD Number
2016-24-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-4224
FR Citation
81 FR 88623

Applicability

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

Unsafe Condition

Cracked and corroded barrel nuts found at the mid-spar location of the horizontal-stabilizer-to-vertical-stabilizer attachment joint, which could compromise the structural integrity of the vertical-stabilizer attachment joints and lead to loss of control of the airplane.

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

Required Actions

Conduct repetitive detailed inspections of each barrel nut and cradle, check the bolt torque of the preload indicating (PLI) washers, and take corrective action if necessary, including retorquing bolts and replacing barrel nuts. Inspect cracked or broken barrel nuts for damaged bores of the fittings and repair or replace as needed.

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

Compliance Time

Before further flight

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Affected Aircraft

Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes with serial numbers 4001 and subsequent.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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