AD 68-07-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 188 | Airworthiness Directives; CESSNA: Models 188 and A188 Airplanes |
| aircraft | Cessna Aircraft Company | 188A | Airworthiness Directives; CESSNA: Models 188 and A188 Airplanes |
| aircraft | Cessna Aircraft Company | 188B | Airworthiness Directives; CESSNA: Models 188 and A188 Airplanes |
| aircraft | Cessna Aircraft Company | A188 | Airworthiness Directives; CESSNA: Models 188 and A188 Airplanes |
| aircraft | Cessna Aircraft Company | A188A | Airworthiness Directives; CESSNA: Models 188 and A188 Airplanes |
| aircraft | Cessna Aircraft Company | A188B | Airworthiness Directives; CESSNA: Models 188 and A188 Airplanes |
Unsafe Condition
Separation of the rudder pedal assembly from the pedal shaft at the stub tube weld.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the rudder pedal assembly according to Cessna Service Letter 67-47 or an approved equivalent method.
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 airworthiness directive
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Models 188 and A188 airplanes up to and including Serial Number 188-0317, excluding specified serial numbers listed in the AD.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.