AD 74-09-04

final rule

Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes

AD Number
74-09-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-28-140 Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes
aircraft Piper Aircraft Inc. PA-28-180 Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes
aircraft Piper Aircraft Inc. PA-28-235 Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes
aircraft Piper Aircraft Inc. PA-28R-200 Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes

Unsafe Condition

The rear seat safety belt outboard attachments may not be properly located, increasing the risk of inadequate restraint during turbulence or sudden maneuvers.

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

Required Actions

Relocate the rear seat safety belt outboard attachments in accordance with Piper Service Bulletin Number 393 or an equivalent approved by the FAA.

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 from the effective date of this AD

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

Affected Aircraft

Piper Models PA-28-140 (Serial Numbers 28-7225001 through 28-7325674), PA-28-180 (Serial Numbers 28-7205001 through 28-7305601), PA-28-235 (Serial Numbers 28-7210001 through 28-7310176), and PA-28R-200 (Serial Numbers 28R-7235001 through 28R-7335446)

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

Federal Register Abstract

Rear Seat Belt Installation

Applicability Source Text

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AD Number:
74-09-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes
Subject:
Rear Seat Belt Installation
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
04/19/1974
Effective Date:
04/24/1974
Make:
Piper Aircraft Inc.
Model:
PA-28-140 | PA-28-180 | PA-28-235 | PA-28R-200
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: 74-09-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1821

AD NUMBER:   74-09-04

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 24, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-09-04 PIPER: Amendment 39-1821. Applies to Model PA-28-140 Serial Numbers 28-7225001 through 28-7325674; Model PA-28-180 Serial Numbers 28-7205001 through 28- 7305601; Model PA-28-235 Serial Numbers 28-7210001 through 28-7310176; and Model PA- 28R-200 Serial Numbers 28R-7235001 through 28R-7335446, certificated in all categories.

Compliance required within the next 100 hours time in service from the effective date of this AD, unless already accomplished.

To provide a safer rear seat belt installation, accomplish the following:

Relocate the rear seat safety belt outboard attachments in accordance with Piper Service Bulletin Number 393 or equivalent approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region, Atlanta, Georgia.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made apart hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Piper Aircraft Corporation, Vero Beach Division, Vero Beach, Florida 32960. These documents may also be examined at the Federal Aviation Administration, Southern Region, 3400 Whipple Street, East Point, Georgia 30344 and at Federal Aviation Administration Headquarters, 800 Independence Avenue, S.W., Washington, D.C. A historical file on this AD which includes the incorporated material in full is maintained by the FAA at its Headquarters in Washington, D.C., and at the Federal Aviation Administration, Southern Region.

This amendment becomes effective April 24, 1974.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-09-04.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-09-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes
Subject:
Rear Seat Belt Installation
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
04/19/1974
Effective Date:
04/24/1974
Make:
Piper Aircraft Inc.
Model:
PA-28-140 | PA-28-180 | PA-28-235 | PA-28R-200
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: 74-09-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1821

AD NUMBER:   74-09-04

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-28-140, PA-28-180, PA-28-235, and PA-28R-200 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 24, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-09-04 PIPER: Amendment 39-1821. Applies to Model PA-28-140 Serial Numbers 28-7225001 through 28-7325674; Model PA-28-180 Serial Numbers 28-7205001 through 28- 7305601; Model PA-28-235 Serial Numbers 28-7210001 through 28-7310176; and Model PA- 28R-200 Serial Numbers 28R-7235001 through 28R-7335446, certificated in all categories.

Compliance required within the next 100 hours time in service from the effective date of this AD, unless already accomplished.

To provide a safer rear seat belt installation, accomplish the following:

Relocate the rear seat safety belt outboard attachments in accordance with Piper Service Bulletin Number 393 or equivalent approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region, Atlanta, Georgia.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made apart hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Piper Aircraft Corporation, Vero Beach Division, Vero Beach, Florida 32960. These documents may also be examined at the Federal Aviation Administration, Southern Region, 3400 Whipple Street, East Point, Georgia 30344 and at Federal Aviation Administration Headquarters, 800 Independence Avenue, S.W., Washington, D.C. A historical file on this AD which includes the incorporated material in full is maintained by the FAA at its Headquarters in Washington, D.C., and at the Federal Aviation Administration, Southern Region.

This amendment becomes effective April 24, 1974.

FOOTER:

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.