AD 47-27-04

final rule
Data completeness: 60%

DOUGLAS Model C-54 and DC-4 Series Airplanes

AD Number
47-27-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company C54-DC DOUGLAS Model C-54 and DC-4 Series Airplanes
aircraft The Boeing Company C54A-DC DOUGLAS Model C-54 and DC-4 Series Airplanes
aircraft The Boeing Company C54B-DC DOUGLAS Model C-54 and DC-4 Series Airplanes
aircraft The Boeing Company C54D-DC DOUGLAS Model C-54 and DC-4 Series Airplanes
aircraft The Boeing Company C54E-DC DOUGLAS Model C-54 and DC-4 Series Airplanes
aircraft The Boeing Company C54G-DC DOUGLAS Model C-54 and DC-4 Series Airplanes
aircraft The Boeing Company DC-4 DOUGLAS Model C-54 and DC-4 Series Airplanes

Unsafe Condition

Cracking failure of the collector ring 'Y' outlet assembly due to breathing of the exhaust stack, which induces failure creating a fire hazard.

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

Required Actions

Weld a scalloped stiffener flange on the exhaust collector aft of the 'Y' outlet assembly. Inspect for cracks immediately and at intervals not exceeding 50 hours of operation until the repair is completed.

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

Compliance Time

Not later than the first engine change subsequent to July 15, 1947, but in any event not later than October 15, 1947.

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

Affected Aircraft

All C-54 and DC-4 Series Airplanes having exhaust collector rings made up of top segments P/N 5174842-56 L.H. and 5174529-56 R.H.

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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