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Airworthiness Directive

AD 2007-07-06 R1 73 FR 64876 Active

Federal Aviation Administration · 14 CFR part 39

Requires the following: Adding information to the limitations section of the airplane flight manual (AFM); repetitively inspecting the aileron and the elevator linear bearings and control rods for foreign object debris, scarring…

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FR document
E8-25500
Amendment
39-15713
Published
2008-10-31
Effective
2008-12-05
Models covered
1

Last live check: 2026-08-19

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AD

2007-07-06 R1

FR doc E8-25500 · 73 FR 64876

AD 2007-07-06 R1Published 2008-10-31Effective 2008-12-05

Revises 2007-07-06

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires the following: Adding information to the limitations section of the airplane flight manual (AFM); repetitively inspecting the aileron and the elevator linear bearings and control rods for foreign object debris, scarring, or damage; and taking all necessary corrective actions.

Full official abstract

We are adopting a new airworthiness directive (AD) to revise AD 2007-07-06, which applies to certain Cessna Aircraft Company (type certificate previously held by Columbia Aircraft Manufacturing) (Cessna) Models LC40-550FG, LC41-550FG, and LC42-550FG airplanes. AD 2007-07-06 currently requires the following: Adding information to the limitations section of the airplane flight manual (AFM); repetitively inspecting the aileron and the elevator linear bearings and control rods for foreign object debris, scarring, or damage; and taking all necessary corrective actions. Since we issued AD 2007-07-06, Cessna has issued a new service bulletin that contains procedures for installing an access panel to facilitate the required inspections. Consequently, this AD retains the actions currently required in AD 2007-07-06; allows installing access panels; and changes the serial number applicability. We are issuing this AD to prevent jamming in the aileron and elevator control systems, which could result in failure. This failure could lead to loss of control.

More directives for Cessna 350/400 Corvalis

  1. AD 2013-11-10 Airworthiness Directives; Cessna Aircraft Company Airplanes Effective 2013-07-26
  2. AD 2011-03-04 Airworthiness Directives; Cessna Aircraft Company (Type Certificate Prev... Effective 2011-03-14
  3. AD 2010-26-54 Airworthiness Directives; Cessna Aircraft Company (Cessna) (Type Certifi... Effective 2011-01-10
  4. AD 2009-09-09 Airworthiness Directives; Cessna Aircraft Company (Type Certificate Prev... Effective 2009-05-11
  5. AD 2007-07-06 Airworthiness Directives; Columbia Aircraft Manufacturing (Previously th... Effective 2007-04-09

All Cessna 350/400 Corvalis directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index