AD 68-07-07

Airworthiness directive · Rudder Pedal Assembly · Cessna 188, 188A, 188B and 3 more

Effective
April 11, 1968
Models
188, 188A, 188B, A188, A188A, A188B
Data sheet
TCDSA9CE
Registered aircraft
284 matched by model
Product
Aircraft · Small airplane
Amendment
39-575

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

On this page

The airworthiness directive

68-07-07 CESSNA: Amdt. 39-575. Applies to Models 188 and A188 aircraft up to and including Serial Number 188-0317, except Serial Numbers 188-0052, 188-0055, 188-0212, 188- 0215, 188-0217, 188-0219, 188-0220, 188-0225, 188-0246, 188-0263, 188-0279, 188-0287, 188- 0288, 188-0290, 188-0298, 188-0304, 188-0306, 188-0307, 188-0308, 188-0310, 188-0311, 188- 0312, and 188-0314.

Compliance: Required as indicated, unless already accomplished.

To prevent the separation of the rudder pedal assembly from the pedal shaft at the stub tube weld, accomplish the following:

Within the next 25 hours' time in service after the effective date of this airworthiness directive, modify the rudder pedal assembly in accordance with either of the 2 methods contained in Cessna Service Letter 67-47, dated August 22, 1967, or any other method approved as an equivalent by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Central Region.

This amendment becomeseffective April 11, 1968.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 284

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Cessna284 aircraft
By year built
19661983
Registered aircraft by year built: 255 aircraft
196620
19679
19689
19694
19709
197113
197212
197326
197441
197548
197630
197713
197810
19792
19803
19815
19831

29 with no year recorded

By model

Aircraft

See all 284 aircraft