AD 84-07-04 R1

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes

AD Number
84-07-04 R1
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 and -30 Series Airplanes
aircraft The Boeing Company DC-9-12 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes
aircraft The Boeing Company DC-9-13 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes
aircraft The Boeing Company DC-9-14 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes
aircraft The Boeing Company DC-9-15 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes
aircraft The Boeing Company DC-9-15F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes
aircraft The Boeing Company DC-9-31 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes
aircraft The Boeing Company DC-9-32 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes
aircraft The Boeing Company DC-9-32 (VC-9C) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes
aircraft The Boeing Company DC-9-32F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10 and -30 Series Airplanes

Unsafe Condition

Fatigue cracks in the non-ventral aft pressure bulkhead webs could result in structural failure.

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

Required Actions

Perform an initial eddy current inspection of the aft pressure bulkhead webs within the specified compliance time. If cracks are found, repair them per Service Bulletin 53-174. Conduct repetitive inspections at intervals not exceeding 14,000 or 17,500 landings depending on aircraft group, with adjustments after preventive modifications.

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

Compliance Time

Prior to the accumulation of 37,500 landings, or within the next 2,500 landings after the effective date of this AD (February 28, 1988), 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 and -30 series airplanes with factory serial numbers listed in Service Bulletin 53-174 (dated August 4, 1983) or later approved revisions.

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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