AD 66-19-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 210 | Airworthiness Directives; CESSNA Models 210 and 210A Airplanes |
| aircraft | Cessna Aircraft Company | 210A | Airworthiness Directives; CESSNA Models 210 and 210A Airplanes |
Unsafe Condition
Engine power failures caused by the loss of fuel flow resulting from the uncovering of the fuel tank outlet during landing approaches and prolonged slips.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install an operating limitation placard adjacent to the fuel gauges with the specified text: 'Avoid landing approach in red arc and over 30 seconds slips under 1/2 tank (Reference Owner's Manual)'
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 after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
CESSNA Models 210 and 210A Airplanes, Serial Numbers 616, 618, 57001 through 57575, and 21057576 through 21057840
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fuel System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_66-19-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 66-19-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Models 210 and 210A Airplanes Subject: Fuel System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/14/1966 Make: Cessna Aircraft Company Model: 210 | 210A Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 66-19-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-270 AD NUMBER: 66-19-02 SUBJECT HEADING: Airworthiness Directives; CESSNA Models 210 and 210A Airplanes ACTION: SUMMARY: DATES: Effective August 14, 1966. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 66-19-02 CESSNA: Amdt. 39-270 Part 39 Federal Register August 4, 1966. Applies to Models 210 and 210A Airplanes, Serial Numbers 616, 618, 57001 through 57575, and 21057576 through 21057840. Compliance required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished. To prevent engine power failures caused by the loss of fuel flow resulting from the uncovering of the fuel tank outlet during landing approaches and prolonged slips, install an operating limitation placard, reading as follows, adjacent to the fuel gauges: "Avoid landing approach in red arc and over 30 seconds slips under 1/2 tank (Reference Owner's Manual)". (Cessna Service Letter 65-39 pertains to this subject.) This directive effective August 14, 1966. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_66-19-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 66-19-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Models 210 and 210A Airplanes Subject: Fuel System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/14/1966 Make: Cessna Aircraft Company Model: 210 | 210A 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: 66-19-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-270 AD NUMBER: 66-19-02 SUBJECT HEADING: Airworthiness Directives; CESSNA Models 210 and 210A Airplanes ACTION: SUMMARY: DATES: Effective August 14, 1966. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 66-19-02 CESSNA: Amdt. 39-270 Part 39 Federal Register August 4, 1966. Applies to Models 210 and 210A Airplanes, Serial Numbers 616, 618, 57001 through 57575, and 21057576 through 21057840. Compliance required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished. To prevent engine power failures caused by the loss of fuel flow resulting from the uncovering of the fuel tank outlet during landing approaches and prolonged slips, install an operating limitation placard, reading as follows, adjacent to the fuel gauges: "Avoid landing approach in red arc and over 30 seconds slips under 1/2 tank (Reference Owner's Manual)". (Cessna Service Letter 65-39 pertains to this subject.) This directive effective August 14, 1966. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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