AD 2005-07-03

Recurring final rule
Data completeness: 80%

Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes; and Model DC-9-81 (MD-81) and DC-9-82 (MD-82) Airplanes

AD Number
2005-07-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2004-18774
FR Citation
70 FR 16098

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-9-10 Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes; and Model DC-9-81 (MD-81) and DC-9-82 (MD-82) Airplanes

Unsafe Condition

Fatigue cracks in the upper and lower caps of the wing spar, which could result in structural failure of the wings.

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

Required Actions

Repetitive detailed inspections of the upper and lower caps of the rear spar of the left and right wings are required. Corrective action is necessary if cracks are found. If only one spar cap is cracked, the cracked spar cap must be repaired (permanently or temporarily), and inspections continue on the uncracked spar cap on that spar.

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

Compliance Time

Within the compliance times specified in the AD, unless the actions have already been done.

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

Affected Aircraft

McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 series airplanes; and Model DC-9-81 (MD-81) and DC-9-82 (MD-82) airplanes, as listed in McDonnell Douglas DC-9 Service Bulletin 57-179, Revision 1, dated December 21, 1994.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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