AD 2000-15-15

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-9, Model MD-90-30, Model 717-200, and Model MD-88 Airplanes

AD Number
2000-15-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-89-AD
FR Citation
65 FR 48355

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-9 Airworthiness Directives; McDonnell Douglas Model DC-9, Model MD-90-30, Model 717-200, and Model MD-88 Airplanes
aircraft Lake Various Airworthiness Directives; McDonnell Douglas Model DC-9, Model MD-90-30, Model 717-200, and Model MD-88 Airplanes

Unsafe Condition

Presence of metallic particles (including slivers, dust, shavings, and flakes) in the jackscrew assembly and surrounding area of the horizontal stabilizer, which could lead to excessive wear and loss of pitch trim capability.

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

Required Actions

Inspect the jackscrew assembly and surrounding area for metallic particles; perform follow-on actions including repetitive inspections, testing of horizontal shutoff controls, and lubrication; take corrective actions such as removing dirt/grease, performing wear checks, adjusting systems, and replacing the jackscrew assembly if necessary.

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

Compliance Time

Within 650 flight hours for initial inspection, with subsequent inspections every 2,000 flight hours.

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

Affected Aircraft

McDonnell Douglas Model DC-9, Model MD-90-30, Model 717-200, and Model MD-88 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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