AD 69-08-11

final rule
Data completeness: 70%

Airworthiness Directives; CESSNA Model 210-5 (205), 206, U206 and P206, 210 and T210 Airplanes

AD Number
69-08-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
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

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

AI-generated summary from the source AD text. Verify against the official source before acting.

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.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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