AD 2000-03-51

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
2000-03-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-58-AD
FR Citation
65 FR 10379

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

Excessive wear of the jackscrew assembly of the horizontal stabilizer could result in loss of pitch trim capability, leading to loss of vertical control of the airplane.

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

Required Actions

Inspect the general condition of the jackscrew assembly and the area around the jackscrew assembly to detect the presence of metal shavings and flakes.

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

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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