AD 83-19-03

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-24-180/250/260, PA-24-400, PA-30 and PA-39 Airplanes

AD Number
83-19-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-24 Airworthiness Directives; Piper Model PA-24-180/250/260, PA-24-400, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-24-250 Airworthiness Directives; Piper Model PA-24-180/250/260, PA-24-400, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-24-260 Airworthiness Directives; Piper Model PA-24-180/250/260, PA-24-400, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-24-400 Airworthiness Directives; Piper Model PA-24-180/250/260, PA-24-400, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-30 Airworthiness Directives; Piper Model PA-24-180/250/260, PA-24-400, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-39 Airworthiness Directives; Piper Model PA-24-180/250/260, PA-24-400, PA-30 and PA-39 Airplanes

Unsafe Condition

Wing lower main spar cap damage and possible cracks where it enters the fuselage at the lower wing root fairing.

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

Required Actions

Within 100 hours time-in-service after the effective date, inspect the lower spar cap for chafing damage and cracks per Piper SB 751. Polish out chafing damage or replace cracked parts before further flight. Trim the lower portion of seal plates per SB 751 before reinstallation. Use equivalent methods if approved.

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

Compliance Time

Within the next 100 hours time-in-service after the effective date of this AD, and prior to further flight.

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

Affected Aircraft

Piper Models PA-24-180/250/260 (S/N 24-1 and up); PA-24-400 (S/N 26-2 and up); PA-30 (S/N 30-2 thru 30-2000); PA-39 (S/N 39-1 thru 39-155).

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.