AD 76-21-03

final rule
Data completeness: 70%

Airworthiness Directives; Grumman Model G-164 Airplanes

AD Number
76-21-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Allied Ag Cat Productions, Inc. G-164 Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164A Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164B Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164B-15T Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164B-20T Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164B-34T Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164B (with 73 inch wing gap) Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164C Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164D Airworthiness Directives; Grumman Model G-164 Airplanes
aircraft Allied Ag Cat Productions, Inc. G-164D (with 73 inch wing gap) Airworthiness Directives; Grumman Model G-164 Airplanes

Unsafe Condition

Main landing gear strut failures associated with Frenco Co. P/N 1428 struts installed under STC SA647WE.

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

Required Actions

Inspect main gear struts P/N 1428 for cracks via dye penetrant or magnetic particle inspection within 100 landings after AD effective date (if not done in last 1900 landings), then every 2000 landings. Replace cracked struts with unused same P/N before flight.

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

Compliance Time

Within the next 100 landings after the effective date of this airworthiness directive, unless accomplished within the last 1900 landings, and thereafter at intervals not to exceed 2000 landings from the last inspection

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

Affected Aircraft

Grumman Model G-164 airplanes with Frenco Co. main landing gear struts P/N 1428 installed under STC SA647WE

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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