AD 79-19-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 210L | Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes |
| aircraft | Cessna Aircraft Company | 210M | Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes |
| aircraft | Cessna Aircraft Company | P210N | Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes |
| aircraft | Cessna Aircraft Company | T210L | Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes |
| aircraft | Cessna Aircraft Company | T210M | Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes |
Unsafe Condition
Possible fuel leak caused by the installation of Symbolic Displays, Inc. fuel flow indicating system per STC SA3835WE.
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Required Actions
Inspect the fuel flow transducer installation. If an NAS 424-4 coupling is installed, replace it with hose assembly Aeroquip P/N AE7010001E0040 or Stratoflex P/N 111D417-4S-0040. Alternative actions approved by the FAA may be used.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 25 hours' time-in-service or thirty (30) days from the effective date of this AD, whichever occurs first
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Affected Aircraft
Cessna Model 210L, T210L (serial numbers 21061040 and subsequent), 210M, T210M, and P210N series airplanes modified with STC SA3835WE fuel flow system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fuel Flow System Per STC SA3835WE
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_79-19-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 79-19-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes Subject: Fuel Flow System Per STC SA3835WE Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/17/1979 Make: Cessna Aircraft Company Model: 210L | 210M | P210N | T210L | T210M Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 79-19-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-3558 AD NUMBER: 79-19-06 SUBJECT HEADING: Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes ACTION: SUMMARY: DATES: Effective September 17, 1979. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 79-19-06 CESSNA AIRCRAFT COMPANY: Amendment 39-3558. Applies to Cessna Model 210L, Model T210L, Serial Numbers 21061040 and subsequent, Model 210M, Model T210M and Model P210N series airplanes modified to incorporate Symbolic Displays, Inc. fuel flow indicating system per STC SA3835WE. Compliance required within 25 hours' time-in-service or thirty (30) days from the effective date of this AD, whichever occurs first, unless already accomplished. To prevent a possible fuel leak caused by the installation of Symbolic Displays, Inc. fuel flow indicating system per STC SA3835WE accomplish the following: (a) Inspect the fuel flow transducer installation on the upper left side of the engine near the fuel distributor manifold. (b) If a 4 inch long flexible hose (Aeroquip P/N AE7010001E0040 or Stratoflex P/N 111D417-4S-0040) is installed between the transducer and the fuel distributor, no further action is required per this AD. (c) If an NAS 424-4 coupling is installed between the fuel flow transducer and the fuel distributor, remove and replace the coupling with hose assembly Aeroquip Part Number AE7010001E0040 or hose assembly Part Number 111D417-4S-0040 (Stratoflex). NOTE: Symbolic Displays, Inc. Service Information Bulletin No. 72 dated June 15, 1979 and Installation Diagram Drawing No. 204724, Revision "B," pertain to this matter. (d) Alternative inspections, modifications or other actions which provide an equivalent level of safety may be used when approved by the Chief, Aircraft Engineering Division, FAA Western Region. This amendment becomes effective September 17, 1979. FOOTER:
Document Text
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AD Final Rules - DRS_79-19-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 79-19-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes Subject: Fuel Flow System Per STC SA3835WE Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/17/1979 Make: Cessna Aircraft Company Model: 210L | 210M | P210N | T210L | T210M 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: 79-19-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-3558 AD NUMBER: 79-19-06 SUBJECT HEADING: Airworthiness Directives; CESSNA Model 210L, T210L, 210M, T210M and P210N Series Airplanes ACTION: SUMMARY: DATES: Effective September 17, 1979. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 79-19-06 CESSNA AIRCRAFT COMPANY: Amendment 39-3558. Applies to Cessna Model 210L, Model T210L, Serial Numbers 21061040 and subsequent, Model 210M, Model T210M and Model P210N series airplanes modified to incorporate Symbolic Displays, Inc. fuel flow indicating system per STC SA3835WE. Compliance required within 25 hours' time-in-service or thirty (30) days from the effective date of this AD, whichever occurs first, unless already accomplished. To prevent a possible fuel leak caused by the installation of Symbolic Displays, Inc. fuel flow indicating system per STC SA3835WE accomplish the following: (a) Inspect the fuel flow transducer installation on the upper left side of the engine near the fuel distributor manifold. (b) If a 4 inch long flexible hose (Aeroquip P/N AE7010001E0040 or Stratoflex P/N 111D417-4S-0040) is installed between the transducer and the fuel distributor, no further action is required per this AD. (c) If an NAS 424-4 coupling is installed between the fuel flow transducer and the fuel distributor, remove and replace the coupling with hose assembly Aeroquip Part Number AE7010001E0040 or hose assembly Part Number 111D417-4S-0040 (Stratoflex). NOTE: Symbolic Displays, Inc. Service Information Bulletin No. 72 dated June 15, 1979 and Installation Diagram Drawing No. 204724, Revision "B," pertain to this matter. (d) Alternative inspections, modifications or other actions which provide an equivalent level of safety may be used when approved by the Chief, Aircraft Engineering Division, FAA Western Region. This amendment becomes effective September 17, 1979. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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