AD 76-15-07

final rule

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

AD Number
76-15-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

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

Unsafe Condition

Loose elevator balance weights could cause possible hazards in flight.

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

Required Actions

Alter the elevator balance weight attachment using Piper Modification Kits No. 761 040 (PA-31-325) or No. 761 041 (PA-31-350) or approved equivalent alterations. Equivalent alterations require approval by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

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

Compliance Time

within the next fifty hours in service from the effective date of this AD unless previously accomplished

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

Affected Aircraft

Piper Models PA-31-325 (Serial Nos. 31-7400990, 31-7512006 through 31-7512058) and PA-31-350 (Serial Nos. 31-5001 through 31-7552108)

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

Federal Register Abstract

Elevator Balance Weights

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_76-15-07.html
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Details
AD Number:
76-15-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-31-325 and PA-31-350 Airplanes
Subject:
Elevator Balance Weights
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
07/29/1976
Effective Date:
08/03/1976
Make:
Piper Aircraft Inc.
Model:
PA-31-325 | PA-31-350
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 76-15-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2680

AD NUMBER:   76-15-07

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-31-325 and PA-31-350 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 3, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-15-07 PIPER: Amendment 39-2680. Applies to Models PA-31-325, Serial Nos. 31-7400990, 31-7512006 through 31-7512058; PA-31-350, Serial Nos. 31-5001 through 31-7552108 certificated in all categories.

To prevent possible hazards in flight associated with loose elevator balance weights, accomplish the following within the next fifty hours in service from the effective date of this AD unless previously accomplished:

a. Alter the elevator balance weight attachment in accordance with Piper Elevator Balance Weight Modification Kits No. 761 040 applicable to Model PA-31-325 or No. 761 041 applicable to Model PA-31-350 or approved equivalent alterations.

b. Equivalent alterations must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

(Piper Service Bulletin Number 500 refers to this subject).

This amendment is effective August 3, 1976.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_76-15-07.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-15-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-31-325 and PA-31-350 Airplanes
Subject:
Elevator Balance Weights
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
07/29/1976
Effective Date:
08/03/1976
Make:
Piper Aircraft Inc.
Model:
PA-31-325 | PA-31-350
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 76-15-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2680

AD NUMBER:   76-15-07

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-31-325 and PA-31-350 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 3, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-15-07 PIPER: Amendment 39-2680. Applies to Models PA-31-325, Serial Nos. 31-7400990, 31-7512006 through 31-7512058; PA-31-350, Serial Nos. 31-5001 through 31-7552108 certificated in all categories.

To prevent possible hazards in flight associated with loose elevator balance weights, accomplish the following within the next fifty hours in service from the effective date of this AD unless previously accomplished:

a. Alter the elevator balance weight attachment in accordance with Piper Elevator Balance Weight Modification Kits No. 761 040 applicable to Model PA-31-325 or No. 761 041 applicable to Model PA-31-350 or approved equivalent alterations.

b. Equivalent alterations must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

(Piper Service Bulletin Number 500 refers to this subject).

This amendment is effective August 3, 1976.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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