AD 68-17-04

final rule
Data completeness: 70%

Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes

AD Number
68-17-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 150 Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150A Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150B Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150C Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150D Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150E Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150F Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150G Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150H Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes
aircraft Cessna Aircraft Company 150J Airworthiness Directives; CESSNA Model 150, 172, 177, 180, 185, F150, and F172H Airplanes

Unsafe Condition

Failure of the pneumatic stall warning system to provide a clearly audible warning during stall conditions due to improper operation or blockage of the reed assembly and horn bell.

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

Required Actions

Test the pneumatic stall warning system preflight by covering the wing opening with a cloth and applying suction. Install a placard on the instrument panel within 10 hours time in service after the effective date. Repair non-functioning systems by replacing the reed assembly with Part Number 0413483-2, installing mesh screens over the horn bell and wing opening, or using approved modifications. Recalibrate if necessary.

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

Compliance Time

within 10 hours time in service after the effective date of this Airworthiness Directive

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

Affected Aircraft

Cessna Models 150 (Serial Numbers 15061533 through 15069308), 172 (17254893 through 17257161), 177 (17700001 through 17701164), 180 (18051824 through 18051977), 185 (185-1198 through 185-1429), F150 (F150-0001 and up), F172H (F172-0320 and up), and Reims Rocket (FR172-0001 and up) with pneumatic stall warning system Part Number 0413029-200, or where this system was installed as a replacement.

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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