AD 2001-24-27

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes; Model DC-9-81, -82, -83, and -87 Series Airplanes; Model MD-88 Airplanes; and C-9 Airplanes

AD Number
2001-24-27
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-206-AD
FR Citation
66 FR 64109

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-9-10 Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes; Model DC-9-81, -82, -83, and -87 Series Airplanes; Model MD-88 Airplanes; and C-9 Airplanes

Unsafe Condition

Cracking of the rudder pedal adjuster hub assembly, which could lead to loss of rudder pedal control and reduction of braking capability.

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

Required Actions

Accomplish a new terminating action for repetitive inspections of the rudder pedal adjuster hub assembly. Replace the assembly if necessary.

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

Compliance Time

Within 18 months of the effective date of this AD.

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; Model DC-9-81, -82, -83, and -87 series airplanes; Model MD-88 airplanes; and C-9 series airplanes, as listed in McDonnell Douglas Service Bulletin DC9-27-325R02, Revision 02, dated December 12, 1995.

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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