AD 2004-07-05

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series Airplanes

AD Number
2004-07-05
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 99-NM-255-AD
FR Citation
69 FR 16788

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-9-10 Airworthiness Directives; McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series Airplanes

Unsafe Condition

Fatigue cracking of the engine pylon aft upper spar straps (caps), which could result in major damage to the adjacent structure and reduced structural integrity of the airplane.

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

Required Actions

Conduct new, improved repetitive ultrasonic inspections of the engine pylon aft upper spar straps. Replace the strap with a new one or modify the engine pylon rear spar straps if cracking is detected. Implement a terminating action for the repetitive inspection requirements.

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

Affected Aircraft

McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes, and C-9 (military) 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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