AD 81-14-01

final rule
Data completeness: 70%

Airworthiness Directives; EMBRAER Models EMB-110P1 and EMB-110P2 Airplanes

AD Number
81-14-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Embraer S.A. EMB-110P1 Airworthiness Directives; EMBRAER Models EMB-110P1 and EMB-110P2 Airplanes
aircraft Embraer S.A. EMB-110P2 Airworthiness Directives; EMBRAER Models EMB-110P1 and EMB-110P2 Airplanes

Unsafe Condition

Failure of the rudder upper hinge support and associated structure of the vertical stabilizer.

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

Required Actions

Remove the two existing rudder leading edge fairings adjacent to the rudder upper hinge and conduct a dye-penetrant inspection of the entire rudder upper hinge support (fin side). Reinforce the support as per EMBRAER Service Bulletin 110-55-017 if no cracks or only small cracks in Area 'A' are found. Replace the support with P/N 110-3348 if cracks are found in other areas, following 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 the AD

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

Affected Aircraft

Embraer S.A. Models EMB-110P1 and EMB-110P2, Serial Numbers 110001 through 110226, certificated in all categories.

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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