AD 69-08-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 206 | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 206H | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210 | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210-5 (205) | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210A | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210B | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210C | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210D | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210E | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210F | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210G | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210H | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210J | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210K | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210L | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210M | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210N | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | 210R | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | P206 | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | P206A | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | P206B | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | P206C | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | P206D | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | P206E | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210F | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210G | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210H | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210J | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210K | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210L | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210M | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210N | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | T210R | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | U206 | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | U206A | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | U206B | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | U206C | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | U206D | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | U206E | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | U206F | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
| aircraft | Cessna Aircraft Company | U206G | Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes |
Unsafe Condition
Complete loss of engine power when using the fuel boost pump due to an inadequate fuel boost pump electrical circuit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install a resistor in the fuel boost pump electrical circuit in accordance with Cessna Service Letter No. SE 69-9 or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Central Region.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours' time-in-service after the effective date of this airworthiness directive
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Affected Aircraft
Cessna Models 210-5 (205), Serial Numbers 205-0001 through 205-0577; Models 206, U206 and P206, Serial Numbers 206-0001 through U206-1284 and P206-0001 through P206-0566; Models 210 and T210, Serial Numbers 21058221 through 21059111 and T210-0001 through T210-0424.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fuel Boost Pump
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_69-08-11.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-08-11 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes Subject: Fuel Boost Pump Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/22/1969 Make: Cessna Aircraft Company Model: 206 | 206H | 210 | 210-5 (205) | 210A | 210B | 210C | 210D | 210E | 210F | 210G | 210H | 210J | 210K...Show more 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: 69-08-11 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-755 AD NUMBER: 69-08-11 SUBJECT HEADING: Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes ACTION: SUMMARY: DATES: Effective April 22, 1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-08-11 CESSNA: Amdt. 39-755. Applies to Models 210-5 (205), Serial Numbers 205-0001 through 205-0577; Models 206, U206 and P206, Serial Numbers 206-0001 through U206-1284 and P206-0001 through P206-0566; Models 210 and T210, Serial Numbers 21058221 through 21059111 and T210-0001 through T210-0424 series airplanes. Compliances: Within 50 hours' time-in-service after the effective date of this airworthiness directive, unless already accomplished: To prevent complete loss of engine power when using the fuel boost pump, accomplish the following: Modify the fuel boost pump electrical circuit by installing a resistor in accordance with Cessna Service Letter No. SE 69-9, dated April 11, 1969, or any equivalent method approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Central Region. This amendment becomes effective April 22, 1969. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_69-08-11.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-08-11 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes Subject: Fuel Boost Pump Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/22/1969 Make: Cessna Aircraft Company Model: 206 | 206H | 210 | 210-5 (205) | 210A | 210B | 210C | 210D | 210E | 210F | 210G | 210H | 210J | 210K...Show more 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: 69-08-11 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-755 AD NUMBER: 69-08-11 SUBJECT HEADING: Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes ACTION: SUMMARY: DATES: Effective April 22, 1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-08-11 CESSNA: Amdt. 39-755. Applies to Models 210-5 (205), Serial Numbers 205-0001 through 205-0577; Models 206, U206 and P206, Serial Numbers 206-0001 through U206-1284 and P206-0001 through P206-0566; Models 210 and T210, Serial Numbers 21058221 through 21059111 and T210-0001 through T210-0424 series airplanes. Compliances: Within 50 hours' time-in-service after the effective date of this airworthiness directive, unless already accomplished: To prevent complete loss of engine power when using the fuel boost pump, accomplish the following: Modify the fuel boost pump electrical circuit by installing a resistor in accordance with Cessna Service Letter No. SE 69-9, dated April 11, 1969, or any equivalent method approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Central Region. This amendment becomes effective April 22, 1969. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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