AD 2017-19-09

final rule
Data completeness: 70%

Airworthiness Directives; Bombardier, Inc., Airplanes

AD Number
2017-19-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0334
FR Citation
82 FR 43829

Applicability

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

Unsafe Condition

Corrosion of a certain bolt at the pivot pin link, resulting in potential failure of the pivot pin retention bolt, which could lead to loss of directional control or loss of an NLG tire during takeoff or landing.

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

Required Actions

Modify the nose landing gear (NLG) shock strut assembly by installing a new, improved pivot pin retention mechanism and a new retention bolt.

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

Compliance Time

Before further flight

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

Affected Aircraft

Bombardier, Inc., Model DHC-8-400 series airplanes equipped with nose landing gear shock strut assembly part number 47100-19 or any assembly with Bombardier Service Bulletin (SB) 84-32-110 incorporated, or part numbers 47100-9, 47100-11, 47100-13, 47100-15, or 47100-17 without SB 84-32-110 incorporated.

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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