AD 98-16-04

final rule
Data completeness: 70%

Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes

AD Number
98-16-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-CE-14-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 180 Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180A Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180B Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180C Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180D Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180E Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180F Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180G Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180H Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes
aircraft Cessna Aircraft Company 180J Airworthiness Directives; Cessna Models 180, 182, and 185 Series Airplanes

Unsafe Condition

Failure of the wing due to the absence of an angle stiffener along the lower spar splice between Wing Station 90 and 110, which could cause loss of control of the airplane during flight.

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

Required Actions

Inspect inside the left and right wings between Wing Station 90 and 110 for an angle stiffener. If not installed, install a stainless steel reinforcement strap along the lower spar at Wing Station 100.50. Comply with Air Research Technology SB-1-96, Issue 1.

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

Compliance Time

within the next 50 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished

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

Affected Aircraft

Cessna Models 180, 182, and 185 series airplanes with wing extension STC SA00276NY or STA SA93-136, all serial numbers.

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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