AD 73-26-09

final rule
Data completeness: 70%

Airworthiness Directives; CESSNA Model 500 Airplanes

AD Number
73-26-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 500 Airworthiness Directives; CESSNA Model 500 Airplanes

Unsafe Condition

Cracks in the left and right flight compartment side windows (P/Ns 5511265-3 and -4) at attachment locations could lead to failure of the window panes, compromising pressurization integrity.

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

Required Actions

Inspect windows using x-ray or visual inspection per Cessna SL56-2 or approved method. Replace unairworthy windows if cracks progress past retainer edges, interconnect three screw holes, exceed three inches in length, or total cracks exceed six inches. Inspect every 100 hours if cracks exist but do not meet replacement criteria. Discontinue requirements after installing P/N 5511285-3/-4 per SB56-4.

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

Compliance Time

within the next 25 hours' time in service after October 9, 1974, and thereafter every 200 hours' time in service (or 100 hours if cracks are found but not requiring replacement)

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

Affected Aircraft

Cessna Model 500 airplanes (Serial Numbers 500-0001 through 500-0183) with 400 or more hours' time in service.

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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