AD 83-15-51

final rule
Data completeness: 70%

Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes

AD Number
83-15-51
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, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-12 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-13 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-14 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-15 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-15F Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-31 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-32 Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-32 (VC-9C) Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes
aircraft The Boeing Company DC-9-32F Airworthiness Directives; McDONNELL DOUGLAS DC-9-10, -30, -40, and C-9 Series Airplanes

Unsafe Condition

Cracks in the ventral aft pressure bulkhead web along AD4 rivet rows and firex support stiffeners due to insulation material contact.

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

Required Actions

Roll back or remove and retain insulation material, clean and perform close detail visual checks for cracks in specified areas, rework cracked bulkhead panels using specified service sketches, and obtain special flight permits if needed. Alternate compliance may be approved.

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

Compliance Time

within the next 100 additional cycles after 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, -30, -40, and Military C-9 series airplanes, fuselage numbers 20 through 264, with ventral aft pressure bulkhead not in compliance with Service Bulletin A53-144.

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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