AD 2000-17-11

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Aircraft, Inc., SA226 Series and SA227 Series Airplanes

AD Number
2000-17-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-CE-41-AD
FR Citation
65 FR 53158

Applicability

TypeManufacturerModelDetails
aircraft Fairchild Various Airworthiness Directives; Fairchild Aircraft, Inc., SA226 Series and SA227 Series Airplanes

Unsafe Condition

Cracks in the main landing gear (MLG) drag brace assembly, which could lead to MLG failure and result in loss of control of the airplane during takeoff or landing operations.

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

Required Actions

Repetitively inspect the MLG drag brace assembly (consisting of both brace and links) for cracks. Replace or rework any cracked MLG drag brace assembly, with rework limited to cracks of 0.080 inches or less in length.

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

Compliance Time

Within 50 flight hours after the effective date of the AD.

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

Affected Aircraft

Fairchild Aircraft, Inc., SA226 Series (models SA226-T, SA226-AT, SA226-T(B), SA226-TC) and SA227 Series (models SA227-AT, SA227-TT, SA227-AC (C-26A)) airplanes, all serial numbers, certificated in any category, equipped with Ozone Industries, Inc., MLG assemblies as specified.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.