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AD 74-18-12 ACTIVE

Fuel Control Orifice Assembly
Key Information
AD Number 74-18-12 Status Active
Effective Date September 03, 1974 Issue Date Not specified
Docket Number Unknown Amendment 39-1941
Product Type ["Engine"] Product Subtype Not specified
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Honeywell International Inc.
Model(s) TFE731-2
Regulatory Text

74-18-12 AIRESEARCH MANUFACTURING COMPANY of ARIZONA: Amendment 39-1941. Applies to AiResearch Model TFE 731-2-2B engines installed in, but not limited to Lear-Gates Learjet model 35/36 Aircraft, certificated in all categories.

(A) Before further flight, unless previously accomplished, and prior to the installation of replacement fuel control assemblies, replace the hydromechanical fuel control orifice assembly in accordance with AiResearch Alert Service Bulletin TFE 731-A73-3006, dated August 12, 1974, or later FAA approved revisions.

(B) Equivalent procedures may be approved by the Chief, Aircraft Engineering Division, FAA Western Region, upon submission of adequate substantiation data.

(C) Aircraft may be flown to a base for performance of maintenance required by this AD per FAR's 21.197 and 21.199.

This amendment is effective September 3, 1974, for all persons except those to whom it was made effective immediately by telegram dated August 5, 1974.