AD 86-05-09

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes

AD Number
86-05-09
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 Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27A Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27B Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27F Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27G Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27J Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27M Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. FH-227 Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. FH-227B Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes
aircraft Maryland Air Industries, Inc. FH-227C Airworthiness Directives; Fairchild Model F27 and FH227 Series Airplanes

Unsafe Condition

Cracks in the FH227 and F27 main landing gear drag strut assemblies due to surface break-up in the bores of some tubes generated during the drawing process.

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

Required Actions

Inspect left and right upper main undercarriage drag stay for flaws using eddy current or ultrasonic inspection equipment following Dowty Rotol Service Bulletins 32-45N (FH227) or 32-81C (F27). Replace damaged parts before next flight if flaws are found.

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

Compliance Time

Within 400 hours time-in-service after April 13, 1986 for airplanes with ≥20,000 landings prior; within 800 hours time-in-service for those with 10,000-20,000 landings; and within 2,000 hours time-in-service for others. Adjustments possible upon FAA approval.

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

Affected Aircraft

Maryland Air Industries, Inc. Models F27 (all variants) and FH227 series 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 8, 2026

Rights: U.S. Government Public Domain

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