AD 51-10-04

final rule
Data completeness: 60%

Airworthiness Directives; CESSNA Model 190 Airplanes

AD Number
51-10-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 190 Airworthiness Directives; CESSNA Model 190 Airplanes

Unsafe Condition

Cracking and failures of the cowl mounting ring channels may result in the cowl moving forward into the propeller.

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

Required Actions

Inspect cowl mounting channels for cracks every 25 hours of operation. Replace with specified 4130 steel channels (Cessna P/N 0352161, 0352163, 0352163-1) and aluminum alloy reinforcing angles (Cessna P/N 0352146, 0352147-1, 0352147-2, 0352152-5, 0352152-6) until installed. Immediate installation required if cracks are found.

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

Compliance Time

Not later than May 1, 1951, and every 25 hours of operation thereafter until new components are installed.

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

Affected Aircraft

Cessna Model 190 Aircraft, Serial Numbers 7004 Through 7594.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.