Aircraft model

Cessna 350/400 Corvalis

Cessna Aircraft Company

Airworthiness Directives
10
Manufacturer bulletins
00 Service Bulletins
Last live check
2026-10-0110 of 10 re-checked, oldest 2026-09-30
This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

Also known as: Cessna 400, Columbia 350, Columbia 400, Corvalis TT, LC40, LC41, TTx

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What Airworthiness Directives apply to the Cessna 350/400 Corvalis

The FAA has published 10 Airworthiness Directives that name the Cessna 350/400 Corvalis (Cessna Aircraft Company), the earliest in 2004 and the newest on 2013-06-21. The index also holds 1 correction notice for an earlier directive.

Newest

  1. AD 2013-11-10 Airworthiness Directives; Cessna Aircraft Company Airplanes 2013-06-21
  2. AD 2011-03-04 Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Col... 2011-02-07
  3. AD 2010-26-54 Airworthiness Directives; Cessna Aircraft Company (Cessna) (Type Certificate A00003SE Prev... 2011-01-10

See all 10 directives

The ones owners meet again

  1. AD 2011-03-04 Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Col... 2011-02-07 Repetitive inspection or action
  2. AD 2009-09-09 Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Col... 2009-04-30 Repetitive inspection or action
  3. AD 2007-07-06 R1 Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Col... 2008-10-31 Repetitive inspection or action
  4. AD 2007-07-06 Airworthiness Directives; Columbia Aircraft Manufacturing (Previously the Lancair Company)... 2007-04-03 Repetitive inspection or action
  5. AD 2005-12-20 Airworthiness Directives; The Lancair Company Model LC41-550FG Airplanes 2005-06-20 Repetitive inspection or action

We index directives by model, not by serial number or N-number; the record page and the official document say which serials apply.

How to use this page: check the newest directives at every annual, keep the repetitive items on your inspection calendar, and open the official Federal Register text before any work - our summaries are a reading aid, not a determination of compliance.

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Independent owner associations, listed as a courtesy; not affiliated with AircraftDirectives.

Airworthiness Directives

10 records · 1 correction attached
ADAD 2013-11-10Cessna Aircraft Company Airplanes2013-07-26Active
AD

2013-11-10

FR doc 2013-14689 · 78 FR 37448

AD 2013-11-10Published 2013-06-21Effective 2013-07-26

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.

Cessna Aircraft Company Airplanes

Requires insertions into the pilot's operating handbook (POH) and the airplane maintenance manuals (AMM) regarding proper use of the brakes and inspection of the aft fuselage.

Full official abstract

Airworthiness Directives; Cessna Aircraft Company Airplanes

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) (previously COLUMBIA or LANCAIR) Models LC40-550FG, LC41-550FG, and LC42-550FG airplanes. This AD was prompted by reports that during maximum braking, if the brakes lock up and a skid occurs, a severe oscillatory yawing motion or "wheel walk" may develop, which could result in further significant structural damage to the airplane. This AD requires insertions into the pilot's operating handbook (POH) and the airplane maintenance manuals (AMM) regarding proper use of the brakes and inspection of the aft fuselage. We are issuing this AD to correct the unsafe condition on these products.

Source: Federal Register document 2013-14689, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2011-03-04Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously the Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes2011-03-14Active
AD

2011-03-04

FR doc 2011-2008 · 76 FR 6525

AD 2011-03-04Published 2011-02-07Effective 2011-03-14

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.

Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously the Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

Requires repetitive inspections of the rudder hinges and the rudder hinge brackets for damage, i.

Full official abstract

Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously the Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

We are superseding an existing airworthiness directive (AD) for the products listed above. AD 2009-09-09 currently requires repetitive inspections of the rudder hinges and the rudder hinge brackets for damage, i.e., cracking, deformation, and discoloration. If damage is found during any inspection, AD 2009-09-09 also requires replacing the damaged rudder hinge and/or rudder hinge bracket. This new AD retains the inspection requirements of AD 2009-09-09, adds airplanes to the Applicability section, and adds a terminating action for the repetitive inspection requirements. This AD resulted from the manufacturer developing a modification that terminates the repetitive inspections and from the manufacture adding airplane serial numbers into the Applicability section. We are issuing this AD to detect and correct damage in the rudder hinges and the rudder hinge brackets, which could result in failure of the rudder. This failure could lead to loss of control.

Source: Federal Register document 2011-2008, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 2010-26-54Cessna Aircraft Company (Cessna) (Type Certificate A00003SE Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC41-550FG and LC42-550FG Airplanes2011-01-10Active
AD

2010-26-54

FR doc 2010-33336 · 76 FR 1349

AD 2010-26-54Published 2011-01-10Effective 2011-01-10

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.

Cessna Aircraft Company (Cessna) (Type Certificate A00003SE Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC41-550FG and LC42-550FG Airplanes

Requires obtaining written approval from the Manager, Wichita Aircraft Certification Office (ACO), to operate the airplane.

Full official abstract

Airworthiness Directives; Cessna Aircraft Company (Cessna) (Type Certificate A00003SE Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC41-550FG and LC42-550FG Airplanes

We are adopting a new airworthiness directive (AD) for the products listed above. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD requires obtaining written approval from the Manager, Wichita Aircraft Certification Office (ACO), to operate the airplane. This written approval must clearly state that operation is approved per Emergency AD 2010-26-54. This AD was prompted by a Cessna Model LC41-550FG airplane that suffered a significant structural failure in the wing during a production acceptance flight test. We are issuing this AD to prevent catastrophic failure of the wing due to disbonding of the wing skin from the wing spar.

Source: Federal Register document 2010-33336, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2009-09-09Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes2009-05-11Active
AD

2009-09-09

FR doc E9-9793 · 74 FR 19873

AD 2009-09-09Published 2009-04-30Effective 2009-05-11

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.

Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

Requires you to repetitively inspect the rudder hinges and the rudder hinge brackets for damage, i.

Full official abstract

Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing (Previously The Lancair Company)) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Type Certificate previously held by Columbia Aircraft Manufacturing (previously The Lancair Company)) Models LC40- 550FG, LC41-550FG, and LC42-550FG airplanes. This AD requires you to repetitively inspect the rudder hinges and the rudder hinge brackets for damage, i.e., cracking, deformation, and discoloration. If damage is found during any inspection, this AD also requires you to replace the damaged rudder hinge and/or rudder hinge bracket. This AD results from reports that cracked lower rudder hinge brackets were found on two of the affected airplanes. We are issuing this AD to detect and correct damage in the rudder hinges and the rudder hinge brackets, which could result in failure of the rudder. This failure could lead to loss of control.

Source: Federal Register document E9-9793, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 2007-07-06 R1Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes2008-12-05Active
AD

2007-07-06 R1

FR doc E8-25500 · 73 FR 64876

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

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.

Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

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…

Full official abstract

Airworthiness Directives; Cessna Aircraft Company (Type Certificate Previously Held by Columbia Aircraft Manufacturing) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

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.

Source: Federal Register document E8-25500, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 2007-07-06Columbia Aircraft Manufacturing (Previously the Lancair Company) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes2007-04-09Active
AD

2007-07-06

FR doc E7-6011 · 72 FR 15822

AD 2007-07-06Published 2007-04-03Effective 2007-04-09

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.

Columbia Aircraft Manufacturing (Previously the Lancair Company) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

Requires you to add information to the Limitations section of the Airplane Flight Manual (AFM).

Full official abstract

Airworthiness Directives; Columbia Aircraft Manufacturing (Previously the Lancair Company) Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes

The FAA is adopting a new airworthiness directive (AD) for Columbia Aircraft Manufacturing (previously The Lancair Company) Models LC40-550FG, LC41-550FG, and LC42-550FG airplanes. This AD requires you to add information to the Limitations section of the Airplane Flight Manual (AFM). This AD also requires you to repetitively inspect the aileron and the elevator linear bearings and control rods for foreign object debris, scarring, or damage and take all necessary corrective actions. This AD results from reports of possible foreign object contamination of the linear bearings. 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.

Source: Federal Register document E7-6011, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2006-25-08Columbia Aircraft Manufacturing Models LC41-550FG and LC42-550FG Airplanes2006-12-21Active
AD

2006-25-08

FR doc E6-20860 · 71 FR 71478

AD 2006-25-08Published 2006-12-11Effective 2006-12-21

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.

Columbia Aircraft Manufacturing Models LC41-550FG and LC42-550FG Airplanes

Requires you to deactivate the deice system and install a placard in clear view of the pilot.

Full official abstract

Airworthiness Directives; Columbia Aircraft Manufacturing Models LC41-550FG and LC42-550FG Airplanes

The FAA is adopting a new Airworthiness Directive (AD) for all Columbia Aircraft Manufacturing (previously The Lancair Company) Models LC41-550FG and LC42-550FG airplanes equipped with Kelly Aerospace Thermal Systems Supplemental Type Certificate (STC) SA02260CH, Thermawing Deice System (also known as E-Vade). This AD requires you to deactivate the deice system and install a placard in clear view of the pilot. This AD results from problems with the installation of the Kelly Aerospace Thermal Systems Thermawing Deice System following STC SA02260CH. We are issuing this AD to prevent a short circuit condition at the deice heater connector, which could result in damage to the wings and horizontal stabilizer. This damage could lead to reduced structural integrity of the airplane.

Source: Federal Register document E6-20860, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2005-12-20The Lancair Company Model LC41-550FG Airplanes2005-06-21Active
AD

2005-12-20

FR doc 05-11880 · 70 FR 35370

AD 2005-12-20Published 2005-06-20Effective 2005-06-21

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.

The Lancair Company Model LC41-550FG Airplanes

Requires both visual and dye penetrant inspections of the elevator torque tube assembly for cracks.

1 correction to this AD FAA · 2005-06-28

Correction published 2005-06-28

Issued by
Federal Aviation Administration
Published
2005-06-28
Document
Federal Register 05-12676 · Final rule; correction
Corrects
the version published June 20, 2005 at 70 FR 35370

This document makes a correction to Airworthiness Directive (AD) 2005-12-20, which was published in the Federal Register on June 20, 2005 (70 FR 35370), and applies to certain The Lancair Company (Lancair) Model LC41-550FG airplanes. We incorrectly referenced the affected airplane model as LC41-550F in the applicability section. The correct airplane model is LC41-550FG. This action corrects the regulatory text.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 05-12676, retrieved 2026-08-17

Full official abstract

Airworthiness Directives; The Lancair Company Model LC41-550FG Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain The Lancair Company (Lancair) Model LC41-550FG airplanes. This AD requires both visual and dye penetrant inspections of the elevator torque tube assembly for cracks. If a crack is found, this AD requires replacement with a modified assembly that incorporates a steel doubler. This AD also requires replacement of the modified elevator torque tube assembly every 300 hours time-in-service or 18 months (whichever occurs first). This AD results from cracks found in the weld area of the elevator torque tube assembly. We are issuing this AD to detect and correct cracks in the elevator torque tube assembly, which could result in failure of the elevator torque tube assembly and subsequent loss of control of the airplane.

Source: Federal Register document 05-11880, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2005-02-01The Lancair Company Models LC40-550FG and LC42-550FG Airplanes2005-01-21Active
AD

2005-02-01

FR doc 05-831 · 70 FR 2944

AD 2005-02-01Published 2005-01-19Effective 2005-01-21

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.

The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

Requires you to incorporate additional takeoff chart distance values information into the Performance Section of the FAA- approved Airplane Flight Manual (AFM).

Full official abstract

Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain The Lancair Company (Lancair) Models LC40-550FG and LC42-550FG airplanes. This AD requires you to incorporate additional takeoff chart distance values information into the Performance Section of the FAA- approved Airplane Flight Manual (AFM). This AD results from flight testing that revealed that the takeoff distance values for the affected airplanes could not be duplicated. We are issuing this AD to prevent potential impact with terrain or obstruction during takeoff due to incorrect takeoff distance values.

Source: Federal Register document 05-831, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2004-06-09The Lancair Company Models LC40-550FG and LC42-550FG Airplanes2004-05-03Active
AD

2004-06-09

FR doc 04-6498 · 69 FR 15657

AD 2004-06-09Published 2004-03-26Effective 2004-05-03

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.

The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

Requires you to repetitively inspect the fuel pressure transducer for evidence of chafing and measure the cross section diameter (as necessary).

Full official abstract

Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain The Lancair Company (Lancair) Models LC40-550FG and LC42-550FG airplanes. This AD requires you to repetitively inspect the fuel pressure transducer for evidence of chafing and measure the cross section diameter (as necessary). The AD also requires you to install a compliance kit at a time dependent on the outcomes of the inspections and measurement. Installation of the kit is terminating action for the repetitive inspection requirements. This AD is the result of several reports of the fuel pressure transducer wearing through at the threads where it attached to the fuel line. We are issuing this AD to detect and correct chafing and wear of the fuel pressure transducer, which could result in failure of the transducer threaded fitting with a resulting fuel leak. These fuel leaks could lead to engine power loss or fire.

Source: Federal Register document 04-6498, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

Service Bulletins

0 records

No Service Bulletins in our index yet for this airframe. We only list SBs we have individually sourced from the manufacturer — we never invent one.

This page indexes 10 ADs and 0 SBs from primary sources. The FAA may have issued additional directives for this airframe that are not yet included.

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