AD 89-06-04

final rule
Data completeness: 70%

Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes

AD Number
89-06-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-9-11 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-12 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-13 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-14 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-15 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-15F Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-21 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-31 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-32 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-32 (VC-9C) Airworthiness Directives; McDONNELL DOUGLAS DC-9-10 through -30 Series and C-9 (Military) Series Airplanes

Unsafe Condition

Cracks in the non-ventral aft pressure bulkhead attach tee sections could result in structural failure.

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

Required Actions

Inspect the aft pressure bulkhead attach tee sections using optically aided visual and high frequency eddy current inspections. Repeat inspections at intervals not exceeding 1,500 or 500 landings respectively. Replace or repair cracked tees with approved parts and drawings.

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

Compliance Time

Prior to the accumulation of 25,000 landings or within 500 landings after the effective date of this AD, whichever occurs later.

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

Affected Aircraft

McDonnell Douglas DC-9-10 through -30 Series and C-9 (Military) Series airplanes equipped with a non-ventral aft pressure bulkhead.

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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