AD 66-30-04

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes

AD Number
66-30-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Maryland Air Industries, Inc. F-27 Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. F-27A Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. F-27B Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. F-27F Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. F-27G Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. F-27J Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. F-27M Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. FH-227 Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. FH-227B Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes
aircraft Maryland Air Industries, Inc. FH-227C Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Type Airplanes

Unsafe Condition

Cracks in the engine mount support tube assembly (post support) and engine mount support tube bracket (support assembly) could result in engine separation.

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

Required Actions

Inspect tube assemblies and brackets for cracks using a 10-power glass or equivalent. Repair or replace cracked parts with FAA-approved repairs or equivalent parts. Inspections must be conducted at intervals not exceeding specified service hours.

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

Compliance Time

Within the next 50 hours in service after the effective date for those with 10,000+ hours, or before 10,050 hours in service for those with less than 10,000 hours. Subsequent inspections at intervals not exceeding 300 hours in service.

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

Affected Aircraft

Fairchild-Hiller Model F-27 (all variants) and FH-227 Type airplanes with specific part numbers listed in the AD.

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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