AD 2003-14-05

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes

AD Number
2003-14-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NM-156-AD
FR Citation
68 FR 41901

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas 717-200 Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes

Unsafe Condition

Cracking of the support fitting assemblies and stop pads of the main spoiler actuators, which could result in damage of adjacent structure such as the rear spar or upper skin panel, and consequent reduced structural integrity of the airplane.

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

Required Actions

Perform repetitive visual inspections for cracking of the left and right wing, inboard and outboard support fitting assemblies of the spoiler main actuators. If cracking is detected, contact the manufacturer for repair instructions and additional inspections. If no cracking is detected, lubricate the spoiler system.

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

Compliance Time

Within 50 flight hours after the effective date of the AD.

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

Affected Aircraft

All McDonnell Douglas Model 717-200 airplanes, certificated in any category.

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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