AD 78-13-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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.
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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.
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Compliance Time
within the next 25 hours' time in service
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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)
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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 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Technology, Inc. Model: M-5-210C | M-5-235C Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 78-13-08 CITATION: This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:
Document Text
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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:
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Retrieved: Apr 8, 2026
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