AD 63-19-04

final rule
Data completeness: 70%

SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers

AD Number
63-19-04
Status
final_rule
Effective Date
Product Category
propeller
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Sensenich Propeller Manufacturing Company, Inc. C-2FM3 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. C-2FM4 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. C-2FM5 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. C-2FM6-1 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. C3FR4 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. CS-2FM4 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. CS-2FM5 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. CS-2FM6 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. CS-3FM4 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers
aircraft Sensenich Propeller Manufacturing Company, Inc. CS-3FR5 SENSENICH Models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 Propellers

Unsafe Condition

Cracks in the wood blade shank and split retaining groove in the blade ferrule, loose or broken lag screws, and cracks in the hub lock ring groove could lead to propeller failure.

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

Required Actions

Inspect the wood blade shank and split retaining groove in the blade ferrule for cracks, check and tighten lag screws to 160 inch-pounds torque, magnetically inspect the ferrule and hub's ferrous parts, replace blades with broken lag screws, cracked wood shanks, or cracked ferrule before further flight.

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

Compliance Time

Within specified intervals based on engine type and propeller time in service: inspections required within 10 hours propeller time after effective date or prior to specific hour limits, followed by recurring inspections every 100 or 300 hours propeller time from last inspection.

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

Affected Aircraft

Sensenich Propeller Manufacturing Company, Inc. models C-2FM, CS-2FM, C-3FR4, CS-3FR5, and CS-3FM4 propellers installed on various aircraft including Piper PA-12, -14, -16, -20, -22, Monocoupe 90AL-115, Stinson 108-2 and -3, Bellanca 14-13, and Goodyear GA-2B.

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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