AD 78-01-02

final rule
Data completeness: 70%

Airworthiness Directives; Piper Models PA-31, PA-31-325, and PA-31-350 Airplanes

AD Number
78-01-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-31 Airworthiness Directives; Piper Models PA-31, PA-31-325, and PA-31-350 Airplanes
aircraft Piper Aircraft Inc. PA-31-325 Airworthiness Directives; Piper Models PA-31, PA-31-325, and PA-31-350 Airplanes
aircraft Piper Aircraft Inc. PA-31-350 Airworthiness Directives; Piper Models PA-31, PA-31-325, and PA-31-350 Airplanes

Unsafe Condition

Adverse stability or handling qualities due to incorrect tension in the elevator bungee spring.

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

Required Actions

Inspect the elevator bungee spring for correct tension (30 lb. ±1 lb. for PA-31, 37 lb. ±1 lb. for PA-31-325 and PA-31-350). If tension is incorrect, alter the link per Piper Service Bulletin No. 549 or equivalent approved by the FAA. Submit substantiating data through an FAA Maintenance Inspector for compliance time adjustment.

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

Compliance Time

within the next 25 hours in service after the effective date of this Airworthiness Directive unless already accomplished

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

Affected Aircraft

Piper Models PA-31 (serial nos. 31-7612001-080, 31-7612082-091, 31-7612096, 31-7612099, 31-7612101-102, 31-7612104-105, 31-7612107-108), PA-31-325 (same serial ranges as PA-31), and PA-31-350 (serial nos. 31-7652001-015, 31-7652017-162, 31-7652164-170)

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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