AD 93-07-14

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-9-33F, -34, -34F, -41, and -51 Series Airplanes, and C-9 (Military) Airplanes

AD Number
93-07-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
92-NM-171-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-9-32F (C-9A) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-33F, -34, -34F, -41, and -51 Series Airplanes, and C-9 (Military) Airplanes
aircraft The Boeing Company DC-9-32F (C-9B) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-33F, -34, -34F, -41, and -51 Series Airplanes, and C-9 (Military) Airplanes
aircraft The Boeing Company DC-9-33F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-33F, -34, -34F, -41, and -51 Series Airplanes, and C-9 (Military) Airplanes
aircraft The Boeing Company DC-9-34 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-33F, -34, -34F, -41, and -51 Series Airplanes, and C-9 (Military) Airplanes
aircraft The Boeing Company DC-9-34F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-33F, -34, -34F, -41, and -51 Series Airplanes, and C-9 (Military) Airplanes
aircraft The Boeing Company DC-9-41 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-33F, -34, -34F, -41, and -51 Series Airplanes, and C-9 (Military) Airplanes
aircraft The Boeing Company DC-9-51 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-33F, -34, -34F, -41, and -51 Series Airplanes, and C-9 (Military) Airplanes

Unsafe Condition

Main landing gear wheel assembly separation during wheel rotation due to incorrect hardness of the wheel spacer retainer assemblies or improper installation of the anti-rotation pin.

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

Required Actions

Conduct a one-time inspection of the main landing gear wheel spacer retainer assemblies for correct hardness and proper installation of the anti-rotation pin. If within limits, mark the assembly with 'S/B 32-228'. If not, replace the assembly and mark it. Only install assemblies marked 'SB 32-228'.

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

Compliance Time

Within 2,000 landings or 18 months after the effective date of this AD, whichever occurs first.

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

Affected Aircraft

McDonnell Douglas DC-9-33F, -34, -34F, -41, and -51 series airplanes, and C-9 (military) airplanes as listed in Service Bulletin 32-228, Revision 1.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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