AD 73-05-02

final rule
Data completeness: 70%

Airworthiness Directives; Bellanca Model 17-30A, Model 17-31A, and Model 17-31ATC Airplanes

AD Number
73-05-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Alexandria Aircraft, LLC 17-30A Airworthiness Directives; Bellanca Model 17-30A, Model 17-31A, and Model 17-31ATC Airplanes
aircraft Alexandria Aircraft, LLC 17-31A Airworthiness Directives; Bellanca Model 17-30A, Model 17-31A, and Model 17-31ATC Airplanes
aircraft Alexandria Aircraft, LLC 17-31ATC Airworthiness Directives; Bellanca Model 17-30A, Model 17-31A, and Model 17-31ATC Airplanes

Unsafe Condition

Failure of the rudder control system due to cracks or other failures in the rudder pedal shaft assemblies with .049" thick horizontal tube walls.

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

Required Actions

Inspect rudder pedal shaft assemblies (Part Numbers 195266, 195268, 195270, 195272) for cracks or failures every 25 hours time in service. Replace cracked assemblies before further flight with new parts having .058" wall thickness. Replace all shaft assemblies with .049" horizontal tube walls within 100 hours time in service with those having .058" thickness unless exempt.

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

Compliance Time

Within the next 10 hours time in service after the effective date for initial inspection, and thereafter every 25 hours time in service. Replace within 100 hours time in service unless already accomplished.

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

Affected Aircraft

Bellanca Model 17-30A (Serial Numbers 30346 through 73-30496), Model 17-31A (Serial Numbers 32-37 through 73-32-97), and Model 17-31ATC (Serial Numbers 31015 through 73-31045). Excluded are serial numbers 73-30497 through 73-30509, 73-32-98 through 73-32-100 with reinforcement gussets.

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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