AD 93-13-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | T210K | Airworthiness Directives; Cessna Models T210K, T210L, T210M and T210N Airplanes |
| aircraft | Cessna Aircraft Company | T210L | Airworthiness Directives; Cessna Models T210K, T210L, T210M and T210N Airplanes |
| aircraft | Cessna Aircraft Company | T210M | Airworthiness Directives; Cessna Models T210K, T210L, T210M and T210N Airplanes |
| aircraft | Cessna Aircraft Company | T210N | Airworthiness Directives; Cessna Models T210K, T210L, T210M and T210N Airplanes |
Unsafe Condition
Air induction hose failure, which could result in loss of engine power.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect between the turbocharger and intercooler to determine if a Gates air induction hose (P/N 20987 or 21370) is installed. If installed, remove the Gates hose and install The Aircraftsman hose (P/N MW1118), then tighten the two AN737-TW clamps. Special flight permits may be issued to operate the airplane to a location where the AD requirements can be accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 50 hours time-in-service after the effective date of this AD, unless already accomplished
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Models T210K, T210L, T210M, and T210N equipped with a Continental TSIO-520R engine and intercooler installation per STC SA2231CE (T210K/L) or SA3203NM (T210M/N)
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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