AD 78-13-08

final rule

Airworthiness Directives; Maule Models M-5-210C and M-5-235C

AD Number
78-13-08
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 Maule Aerospace Technology, Inc. M-5-210C Airworthiness Directives; Maule Models M-5-210C and M-5-235C
aircraft Maule Aerospace Technology, Inc. M-5-235C Airworthiness Directives; Maule Models M-5-210C and M-5-235C

Unsafe Condition

Deformed fuel line tubes and hexagonal head clamps could reduce fuel feed or supply to the engine.

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

Required Actions

Inspect fuel line tube clamps. If clamps have hexagonal heads, drain tanks, loosen clamps, inspect tubes for deformation. Replace deformed tubes with specified part numbers and use round head Aeroseal hose clamps torqued to 15-20 inch pounds. Leak check fuel system before return to service.

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

Compliance Time

within the next 25 hours' time in service

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

Affected Aircraft

Maule Models M-5-210C (S/N 6190C through 6204C), M-5-235C (S/N 7061C through 7160C, 7163C through 7167C, 7194C and 7197C)

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

Federal Register Abstract

Engine Fuel Supply

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_78-13-08.html
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Details
AD Number:
78-13-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Maule Models M-5-210C and M-5-235C
Subject:
Engine Fuel Supply
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/05/1978
Make:
Maule Aerospace Technology, Inc.
Model:
M-5-210C | M-5-235C
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Superseded AD: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Superseded By: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: 78-13-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3251

AD NUMBER:   78-13-08

SUBJECT HEADING:   Airworthiness Directives; Maule Models M-5-210C and M-5-235C

ACTION:  

SUMMARY:  

DATES:   Effective July 5, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   78-13-08 MAULE AIRCRAFT CORPORATION: Amendment 39-3251. Models M-5- 210C, S/N 6190C through 6204C, M-5-235C, S/N 7061C through 7160C, 7163C through 7167C, 7169C through 7192C, 7194C and 7197C.
To prevent reduction of fuel feed or supply to the engine, accomplish the following within the next 25 hours' time in service:
Remove the wing root fairings on both sides to gain access to both main tank outlets (two outlets per tank).
(1) If the fuel line tube clamps do not have hexagonal heads, no further inspection is necessary. Replace fairing and return aircraft to service.
(2) If the fuel line tube clamps have hexagonal heads, drain fuel tanks, and loosen the tube clamp(s), pull the fuel hose off of the fuel line(s) and tank outlets and inspect tube(s) for deformed tube sections. If fuel line tube(s) are deformed, replace tube(s), front tubes Maule P/N 5092X-7 left, 5092X-8 right; rear tube(s) P/N 5092X-1 left and 5092X-9 right. Use round head Aeroseal hose clamps P/N QS-100-M8S, or existing hose clamps, during reassembly. Torque clamps to 15-20 inch pounds. Leak check fuel system prior to returning aircraft to service.
An alternate method of compliance with this A. D. may be used if approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region, Atlanta, Georgia.
Maule Service Letter 39 dated May 10, 1978, or later FAA approved revision, pertains to the same subject.
This amendment becomes effective July 5, 1978.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_78-13-08.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
78-13-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Maule Models M-5-210C and M-5-235C
Subject:
Engine Fuel Supply
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/05/1978
Make:
Maule Aerospace Technology, Inc.
Model:
M-5-210C | M-5-235C
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: 78-13-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3251

AD NUMBER:   78-13-08

SUBJECT HEADING:   Airworthiness Directives; Maule Models M-5-210C and M-5-235C

ACTION:  

SUMMARY:  

DATES:   Effective July 5, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   78-13-08 MAULE AIRCRAFT CORPORATION: Amendment 39-3251. Models M-5- 210C, S/N 6190C through 6204C, M-5-235C, S/N 7061C through 7160C, 7163C through 7167C, 7169C through 7192C, 7194C and 7197C.
To prevent reduction of fuel feed or supply to the engine, accomplish the following within the next 25 hours' time in service:
Remove the wing root fairings on both sides to gain access to both main tank outlets (two outlets per tank).
(1) If the fuel line tube clamps do not have hexagonal heads, no further inspection is necessary. Replace fairing and return aircraft to service.
(2) If the fuel line tube clamps have hexagonal heads, drain fuel tanks, and loosen the tube clamp(s), pull the fuel hose off of the fuel line(s) and tank outlets and inspect tube(s) for deformed tube sections. If fuel line tube(s) are deformed, replace tube(s), front tubes Maule P/N 5092X-7 left, 5092X-8 right; rear tube(s) P/N 5092X-1 left and 5092X-9 right. Use round head Aeroseal hose clamps P/N QS-100-M8S, or existing hose clamps, during reassembly. Torque clamps to 15-20 inch pounds. Leak check fuel system prior to returning aircraft to service.
An alternate method of compliance with this A. D. may be used if approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region, Atlanta, Georgia.
Maule Service Letter 39 dated May 10, 1978, or later FAA approved revision, pertains to the same subject.
This amendment becomes effective July 5, 1978.

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.