AD 97-06-11

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes

AD Number
97-06-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
96-CE-44-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. 35R Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. A35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. B35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. C35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. D35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. E35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. F35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. G35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes
aircraft Textron Aviation Inc. H35 Airworthiness Directives; Raytheon Aircraft Company (formerly Beech Aircraft Corporation) 35 Series Airplanes

Unsafe Condition

Failure of the ruddervator differential tail control rod assembly due to corrosion or cracks in the ruddervator control push rod, which could result in loss of control of the airplane.

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

Required Actions

Inspect the ruddervator differential tail control rod assembly for cracks and corrosion in accordance with Raytheon MSB No. 2668. Repair or replace any corroded or cracked parts as specified. Apply anti-corrosion sealant to the ruddervator control pushrods per the same service bulletin.

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

Compliance Time

within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished

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

Affected Aircraft

Raytheon Aircraft Company (formerly Beech Aircraft Corporation) Models 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35TC, V35A, V35A-TC, V35B, and V35B-TC airplanes, serial numbers D-1 through D-10403, D-15001, and D-15002.

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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