AD 69-06-01

final rule
Data completeness: 70%

FAIRCHILD-HILLER Model F-27 Airplanes

AD Number
69-06-01
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 FAIRCHILD-HILLER Model F-27 Airplanes
aircraft Maryland Air Industries, Inc. F-27A FAIRCHILD-HILLER Model F-27 Airplanes
aircraft Maryland Air Industries, Inc. F-27B FAIRCHILD-HILLER Model F-27 Airplanes
aircraft Maryland Air Industries, Inc. F-27F FAIRCHILD-HILLER Model F-27 Airplanes
aircraft Maryland Air Industries, Inc. F-27G FAIRCHILD-HILLER Model F-27 Airplanes
aircraft Maryland Air Industries, Inc. F-27J FAIRCHILD-HILLER Model F-27 Airplanes
aircraft Maryland Air Industries, Inc. F-27M FAIRCHILD-HILLER Model F-27 Airplanes

Unsafe Condition

Flap drive system failure whereby the flaps are driven off the drive screw jacks due to contact pitting or discoloration of contacts in the Cutler Hammer P/N 6046 H46 Relay.

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

Required Actions

Inspect contacts of the flap control system relay every 200 hours time in service; replace relay if contacts are pitted or discolored. Rewire the flap drive circuit per Service Bulletin F-27-27-67 or equivalent modification within 500 hours time in service after the effective date.

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, and thereafter at 200 hour intervals from the date of the last inspection for inspections. Rewiring must be done within the next 500 hours time in service after the effective date.

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) airplanes, serial numbers 1 through 124 inclusive, with Cutler Hammer P/N 6046 H46 Relay in the flap control system.

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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