AD 2001-23-16

final rule
Data completeness: 70%

Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Itda. Models AMT-100 and AMT-200 Powered Sailplanes

AD Number
2001-23-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-CE-40-AD
FR Citation
66 FR 58915

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Itda. Models AMT-100 and AMT-200 Powered Sailplanes

Unsafe Condition

Bending or warping in the main landing gear lever could interfere with the elevator control rod, potentially jamming the elevator control and leading to loss of control.

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

Required Actions

Inspect the main landing gear lever and elevator control rod for interference, warping, or incorrect gaps. Reconfigure or replace discrepant parts. Report any instances of interference, warping, or incorrect gaps to the FAA.

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

Compliance Time

Before further flight

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

Affected Aircraft

Aeromot-Industria Mecanico Metalurgica Itda. Models AMT-100 (serial numbers 100.001 through 100.003, 100.005 through 100.015, 100.017, 100.019, 100.022 through 100.039, and 100.041 through 100.044), AMT-100 remotorized to AMT-200 (serial numbers 100.004, 100.016, 100.018, 100.020, and 100.021), and AMT-200 (serial numbers 200.040, 200.045 through 200.105, 200.108 through 200.111, 200.113 through 200.118, and 200.121).

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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