AD 67-15-02

final rule
Data completeness: 70%

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

AD Number
67-15-02
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 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27A Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27B Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27F Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27G Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27J Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27M Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes
aircraft Maryland Air Industries, Inc. FH-227 Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes
aircraft Maryland Air Industries, Inc. FH-227B Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes
aircraft Maryland Air Industries, Inc. FH-227C Airworthiness Directives; Fairchild-Hiller Model F-27 and FH-227 Series Airplanes

Unsafe Condition

Loss of electrical power to flight instruments due to a single ground fault in the d.c. power system, violating former CAR 4b.603(e), (f), (g) (effective December 31, 1953).

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

Required Actions

Modify the emergency electrical power system to the attitude indicator, turn and bank indicator, and gyroscopic direction indicator to ensure power is not derived solely from the d.c. power system. Use Allegheny Airlines Engineering Order 67-81F or later FAA-approved revision, or an FAA-approved equivalent.

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

Compliance Time

within the next 200 hours' time in service after the effective date of this AD unless already accomplished

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

Affected Aircraft

Fairchild-Hiller Model F-27 (F-27, F-27A, F-27B, F-27F, F-27G, F-27J, F-27M) and FH-227 Series (FH-227, FH-227B, FH-227C, FH-227D, FH-227E) airplanes.

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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