AD 52-28-02

final rule

Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft

AD Number
52-28-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

Applicability

TypeManufacturerModelDetails
aircraft Bellanca Aircraft Corporation 14-13 Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft
aircraft Bellanca Aircraft Corporation 14-13-2 Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft
aircraft Bellanca Aircraft Corporation 14-13-3 Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft

Unsafe Condition

Excessive pressure from the engine-driven fuel pump may create a possible hazard.

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

Required Actions

Install a high-pressure relief valve between the fuel pump outlet and the inlet side of the hand wobble pump.

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

Compliance Time

As soon as practicable, but not later than next engine overhaul after January 1, 1953.

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

Affected Aircraft

Bellanca Aircraft Corporation Models 14-13, 14-13-2, 14-13-3, Serial Numbers up to Number 1584.

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

Federal Register Abstract

Fuel Pump Relief Valve

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_52-28-02.html
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Details
AD Number:
52-28-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft
Subject:
Fuel Pump Relief Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Bellanca Aircraft Corporation
Model:
14-13 | 14-13-2 | 14-13-3
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 52-28-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   52-28-02

SUBJECT HEADING:   Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
52-28-02 BELLANCA: Applies to Models 14-13, 14-13-2, 14-13-3 Aircraft, Serial Numbers Up to Number 1584.

Compliance required as soon as practicable, but not later than next engine overhaul after January 1, 1953.

In order to eliminate possible hazard due to excessive pressure from the engine-driven fuel pump, install a high-pressure relief valve between the fuel pump outlet and the inlet side of the hand wobble pump.

(Bellanca Service Bulletin No. 23 covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_52-28-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
52-28-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft
Subject:
Fuel Pump Relief Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Bellanca Aircraft Corporation
Model:
14-13 | 14-13-2 | 14-13-3
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 52-28-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   52-28-02

SUBJECT HEADING:   Airworthiness Directives; Bellanca Model 14-13, 14-13-2 and 14-13-3 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
52-28-02 BELLANCA: Applies to Models 14-13, 14-13-2, 14-13-3 Aircraft, Serial Numbers Up to Number 1584.

Compliance required as soon as practicable, but not later than next engine overhaul after January 1, 1953.

In order to eliminate possible hazard due to excessive pressure from the engine-driven fuel pump, install a high-pressure relief valve between the fuel pump outlet and the inlet side of the hand wobble pump.

(Bellanca Service Bulletin No. 23 covers this same subject.)

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.