AD 2011-05-13

final rule
Data completeness: 70%

Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 2000 Airplanes

AD Number
2011-05-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-1198
FR Citation
76 FR 13072

Applicability

TypeManufacturerModelDetails
aircraft Saab AB Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 2000 Airplanes
aircraft Aviat Various Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 2000 Airplanes

Unsafe Condition

Corrosion has been found on the rear spar upper cap of the horizontal stabilizer of SAAB 2000 aeroplanes, adjacent to the inboard elevator hinge where electrical wiring harnesses are located. Corrosion damage in these areas can result in crack propagation, impairing the structural integrity of the horizontal stabilizer upper spar cap.

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

Required Actions

Within 12 months after the effective date, perform a detailed visual inspection for corrosion on the left-hand and right-hand horizontal stabilizers, inspect for chafing or damage on the harness in the adjacent area, and install convoluted tubing on the harness. If corrosion is found, repair it before next flight using an approved method.

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

Compliance Time

Within 12 months after the effective date of this AD

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

Affected Aircraft

All Saab AB, Saab Aerosystems Model SAAB 2000 airplanes, certificated in any category.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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