# AD 90-24-03: Rudder Trim Link Assemblies - Type: Airworthiness directive - Status: Current - Products: M7 Aerospace SA226-AT, SA226-T, SA226-TC, SA226-T(B), SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), SA227-PC, SA227-TT, SA26-AT and 1 more - Effective: January 25, 1991 - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Small/large airplane - Amendment: 39-6837 - Docket: 90-CE-69-AD - Registered aircraft: 180 may be affected, by airframe or engine model (OpenAirDocs) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B9B16E081292036C862569880073ADF0.0001 - DRS record last changed: May 30, 2024 - Page: https://openairdocs.org/ad/90-24-03 ## The airworthiness directive 90-24-03 FAIRCHILD AIRCRAFT (SWEARINGEN AIRCRAFT): Amendment 39-6837. Final copy of Priority Letter 90-24-03. Docket No. 90-CE-69-AD. Applicability: SA26, SA226, and SA227 series airplanes (all serial numbers), certificated in any category. Compliance: Required within the next 15 hours time-in-service or 10 calendar days after receipt of this AD, whichever occurs first, unless already accomplished. To prevent aerodynamic vibration, structural deformation, and possible loss of control of the airplane, accomplish the following: (a) Visually inspect the rudder trim tab link assemblies (Part Numbers 27-42025-001 through 27-42025-009 as installed) as follows: (1) Remove the fairing strip between the vertical fin and rudder. (2) Check each connecting rod end for freedom of movement and corrosion around the bearing as follows: (i) Move the rudder trim system from full left to full right deflection and check for any indications of corrosion or binding in the rod end fittings. (ii) If necessary, remove the bolt connecting the actuator and each rod end and check the bearings for freedom of movement. (iii) Check the bolts connecting the rudder actuator to each rod end to insure each bolt is oriented vertically. (3) If either rod end is corroded, prior to further flight replace the affected rod end with a serviceable part. (4) If the rudder trim mechanism is incorrectly installed, or if either rod end bearing is binding, prior to further flight replace the affected connecting rod and rod end assembly with serviceable parts. (5) If corrosion or binding is not found, reinstall the fairing strip and return the airplane to service. NOTE 1: Fairchild Aircraft Service Notes 26-SN-061, 226-SN-162, and 227-SN-074 pertain to the subject of this AD. NOTE 2: Although not required by this AD, the inspections specified in this AD should be included in the regular aircraft maintenance program. (b)Airplanes may be flown in accordance to FAR 21.197 and 21.199 to a location where this AD may be accomplished. (c) An alternate method of compliance or adjustment of the compliance times that provides an equivalent level of safety may be approved by the Manager, Airplane Certification Office, Southwest Region, FAA, Fort Worth, Texas 76193-0150; Telephone (817) 624-5150. NOTE 3: The request should be forwarded through an FAA Maintenance Inspector, who may add comments and then send it to the Manager, Airplane Certification Office, Fort Worth, Texas 76193-0150. This amendment (39-6837, AD 90-24-03) becomes effective on January 25, 1991, as to all persons except those persons to whom it was made immediately effective by priority letter AD 90-24-03, issued November 20, 1990, which contained this amendment. ## Affected data sheets (3) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A5SW](https://openairdocs.org/tcds/A5SW): Ontic Engineering and Manufacturing Inc.; names 6 of 7 models: SA227-AT, SA227-TT, SA26-AT, SA226-AT, SA26-T, SA226-T(B) - [TCDS A8SW](https://openairdocs.org/tcds/A8SW): Ontic Engineering and Manufacturing Inc.; names 4 of 4 models: SA226-TC, SA227-PC, SA227-AC (C-26A), SA227-BC (C-26A) - [TCDS A18SW](https://openairdocs.org/tcds/A18SW): Ontic Engineering and Manufacturing Inc.; names 2 of 2 models: SA227-CC, SA227-DC (C-26B) ## Registered aircraft it may apply to (OpenAirDocs) Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment. - Aircraft: 180 (180 by airframe model, 0 by engine model) - Makers: Fairchild 92, Swearingen 88 Models with the most aircraft: - [Fairchild SA227-AC](https://openairdocs.org/model/fairchild-sa227-ac): 54 aircraft (airframe model) - [Swearingen SA-226T](https://openairdocs.org/model/swearingen-sa-226t): 21 aircraft (airframe model) - [Swearingen SA226-T(B)](https://openairdocs.org/model/swearingen-sa226-t-b): 16 aircraft (airframe model) - [Fairchild SA227-DC](https://openairdocs.org/model/fairchild-sa227-dc): 12 aircraft (airframe model) - [Swearingen SA227-AT](https://openairdocs.org/model/swearingen-sa227-at): 12 aircraft (airframe model) - [Swearingen SA227-TT](https://openairdocs.org/model/swearingen-sa227-tt): 11 aircraft (airframe model) - [Fairchild SA227-AT](https://openairdocs.org/model/fairchild-sa227-at): 9 aircraft (airframe model) - [Swearingen SA-26AT](https://openairdocs.org/model/swearingen-sa-26at): 9 aircraft (airframe model) - [Fairchild SA227-DC (C26B)](https://openairdocs.org/model/fairchild-sa227-dc-c26b): 8 aircraft (airframe model) - [Swearingen SA226TC](https://openairdocs.org/model/swearingen-sa226tc): 8 aircraft (airframe model) - [Swearingen SA227-AC](https://openairdocs.org/model/swearingen-sa227-ac): 8 aircraft (airframe model) - [Fairchild SA226-T(B)](https://openairdocs.org/model/fairchild-sa226-t-b): 3 aircraft (airframe model) - [Fairchild SA227BC](https://openairdocs.org/model/fairchild-sa227bc): 3 aircraft (airframe model) - [Swearingen SA-226AT](https://openairdocs.org/model/swearingen-sa-226at): 3 aircraft (airframe model) - [Fairchild SA226-TC](https://openairdocs.org/model/fairchild-sa226-tc): 1 aircraft (airframe model) - [Fairchild SA226-T](https://openairdocs.org/model/fairchild-sa226-t): 1 aircraft (airframe model) - [Fairchild SA226-AT](https://openairdocs.org/model/fairchild-sa226-at): 1 aircraft (airframe model) All 17 models: https://openairdocs.org/ad/90-24-03/models.md Every aircraft: https://openairdocs.org/ad/90-24-03/aircraft.md Its text cites no advisory circulars or STCs. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.