AD 79-10-13

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes

AD Number
79-10-13
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 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-12 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-13 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-14 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-15 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-15F Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-21 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-31 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-32 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes
aircraft The Boeing Company DC-9-32 (VC-9C) Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Series and Military C-9 Series Airplanes

Unsafe Condition

Fatigue cracks in the forward passenger entry door lock mechanism crank assembly parts, P/N 4918613-3 (crank) and P/N 4918613-5 (clevis), could result from riding on unserrated surfaces of mating parts, leading to door lock failure.

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

Required Actions

Inspect crank assembly P/N 4918613-1 for proper serration engagement before disassembly. Perform dye penetrant inspections on P/N 4918613-3 and -5 parts per Service Bulletin 52-111. Replace cracked parts or those with serration misalignment with unmodified, modified, or new parts as specified in paragraphs (c)(1)(i)-(iii).

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

Compliance Time

Within the next 3,500 landings after the effective date of this AD, or before accumulating 22,500 total landings whichever occurs later

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

Affected Aircraft

MCDONNELL DOUGLAS DC-9 Series (models DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, etc.) and Military C-9 Series airplanes, certificated in all categories.

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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