AD 71-09-07 R1

final rule
Data completeness: 70%

Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes

AD Number
71-09-07 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company T207 Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T207A Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T210F Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T210G Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T210H Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T210J Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T210K Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T210L Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T210M Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes
aircraft Cessna Aircraft Company T210N Airworthiness Directives; CESSNA Model TU206 series, TP206 series , T207 series, T210 thru T210N Airplanes

Unsafe Condition

Exhaust gases entering the cabin due to cracks or leakage in the exhaust manifold heat exchanger area.

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

Required Actions

Inspect the exhaust manifold heat exchanger within 25 hours time-in-service after the effective date, and every 50 hours thereafter. Replace defective parts with airworthy ones if cracks, breaks, or leakage are found during the pressure test.

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, unless already accomplished within the last 25 hours TIS, and thereafter at intervals not to exceed 50 hours TIS since the last inspection per this AD prior to its revision.

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

Affected Aircraft

Cessna Models TU206 Series, TP206 Series, T207 Series (all serial numbers), and Models T210 thru T210N (Serial Numbers T210-0001 through T210-0454 and 21059200 through 21064897).

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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