| AD Number | 69-08-11 | Status | Active |
| Effective Date | April 22, 1969 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-755 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Cessna Aircraft Company |
| Model(s) | 206 206H 210 210-5 (205) 210A 210B 210C 210D 210E 210F 210G 210H 210J 210K 210L 210M 210N 210R P206 P206A P206B P206C P206D P206E T210F T210G T210H T210J T210K T210L T210M T210N T210R U206 U206A U206B U206C U206D U206E U206F U206G |
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.