# AD 2011-01-52: Rotorcraft Tailboom - Type: Emergency airworthiness directive - Status: Historical - Products: Schweizer 269A, 269A-1, 269B, 269C and 269C-1 - Issued: December 20, 2010 - Issued as: Emergency AD - Superseded by: [AD 2011-12-16](https://openairdocs.org/ad/2011-12-16) - Product type: Aircraft, Rotorcraft - Registered aircraft: 416 may be affected, by airframe or engine model (OpenAirDocs) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3B72D4B5E515A376862577FF0079E131.0001 - DRS record last changed: August 7, 2025 - Page: https://openairdocs.org/ad/2011-01-52 ## The airworthiness directive FAA Aviation Safety EMERGENCY AIRWORTHINESS DIRECTIVE www.faa.gov/aircraft/safety/alerts/ DATE: December 20, 2010 AD #: 2011-01-52 Background This emergency AD is prompted by a locknut working loose on the tailboom aft cluster fitting strut. Further investigation revealed that the locknut installed on the expandable bolt did not have the proper threads. This condition, if not corrected, could result in the strut and driveshaft separating from the helicopter and subsequent loss of control of the helicopter. FAA’s Determination We are issuing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other helicopters of these same type designs. AD Requirements This AD requires, before further flight, unless accomplished previously, removing the locknut, part number MS21043-3. Reinstalling the locknut while determining the locknut drag torque is then required. If the drag torque is a minimum of 2 in-lbs, retorquing the locknut to 23 in-lbs is required. If the drag torque is not at least 2 in-lbs, replacing the locknut with an airworthy locknut is required. Authority for this Rulemaking Title 49 of the United States Code specifies the FAA’s authority to issue rules on aviation safety. Subtitle I, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency’s authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, “General requirements.” Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Pursuant to this Authority delegated to me by the Administrator, we are hereby issuing this Emergency Airworthiness Directive (AD). 2011-01-52 SCHWEIZER AIRCRAFT CORPORATION: Directorate Identifier 2010-SW-111- AD. Effective Date (a) This Emergency AD is effective upon receipt. 1 Affected A Ds (b) None. Applicability (c) This AD applies to Model 269A, A-1, B, C, C-1, and Th-55 series helicopters, that have an Aft Cluster Fitting Modification Kit, part number SA-269K-106, installed; Model 269C helicopters, serial numbers 1846 and larger; and Model 269C-1 helicopters, serial numbers 0156 and larger, certificated in any category. Unsafe Condition (d) This AD is prompted by a locknut working loose on the tailboom aft cluster fitting strut. Further investigation revealed that the locknut installed on the expandable bolt did not have the proper threads. This condition, if not corrected, could result in the strut and driveshaft separating from the helicopter and subsequent loss of control of the helicopter. Compliance (e) Required before further flight, unless accomplished previously, remove the locknut, part number MS21043-3. Reinstall the locknut while determining the locknut drag torque. If the drag torque is a minimum of 2 in-lbs, retorque the locknut to 23 in-lbs. If the drag torque is not at least 2 in-lbs, replace the locknut with an airworthy locknut. Special Flight Permit (f) Special flight permits will not be issued. Alternative Methods of Compliance (AMOCs) (g) The Manager, New York Aircraft Certification Office (NYACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the NYACO, send it to the attention of the Continued Operational Safety program manager. Note: Before using any approved AMOC, we request that you notify your appropriate principal inspector, or lacking a principal inspector, your local Flight Standards District Office. Other Information (h) For further information about this AD, contact: Stephen Kowalski, Aerospace Engineer, Airframe and Propulsion Branch, ANE-171, 1600 Stewart Ave., suite 410, Westbury, New York 11590, telephone (516) 228-7327, fax (516) 794-5531. Subject (i) The Joint Aircraft System Component (JASC) Code is 5302: Rotorcraft Tailboom. 2 Issued in Fo rt Worth, Texas, on December 20, 2010. M. Monica Merritt, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service. 3 ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS 4H12](https://openairdocs.org/tcds/4H12): Schweizer RSG LLC; names 5 of 6 models: 269B, 269A-1, 269A, 269C, 269C-1 ## 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: 416 (416 by airframe model, 0 by engine model) - Makers: Hughes 207, Schweizer 204, Schweizer RSG 5 Models with the most aircraft: - [Schweizer 269C](https://openairdocs.org/model/schweizer-269c): 115 aircraft (airframe model) - [Hughes 269A](https://openairdocs.org/model/hughes-269a): 97 aircraft (airframe model) - [Schweizer 269C-1](https://openairdocs.org/model/schweizer-269c-1): 84 aircraft (airframe model) - [Hughes 269C](https://openairdocs.org/model/hughes-269c): 74 aircraft (airframe model) - [Hughes 269B](https://openairdocs.org/model/hughes-269b): 31 aircraft (airframe model) - [Hughes 269A-1](https://openairdocs.org/model/hughes-269a-1): 5 aircraft (airframe model) - [Schweizer HUGHES 269C](https://openairdocs.org/model/schweizer-hughes-269c): 4 aircraft (airframe model) - [Schweizer RSG 269C](https://openairdocs.org/model/schweizer-rsg-269c): 3 aircraft (airframe model) - [Schweizer RSG 269C-1](https://openairdocs.org/model/schweizer-rsg-269c-1): 2 aircraft (airframe model) - [Schweizer 269A](https://openairdocs.org/model/schweizer-269a): 1 aircraft (airframe model) All 10 models: https://openairdocs.org/ad/2011-01-52/models.md Every aircraft: https://openairdocs.org/ad/2011-01-52/aircraft.md ## Related documents - [AD 2011-12-16](https://openairdocs.org/ad/2011-12-16): Rotorcraft Tailboom · Schweizer 269A, 269A-1, 269B and 2 more. Effective Jul 21, 2011. Supersedes this AD Its text cites no advisory circulars or STCs. ## NTSB investigations that cite this AD (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN10LA560](https://openairdocs.org/ntsb/CEN10LA560), Sep 20, 2010: Schweizer 269C (N34LB), Schaumburg, IL, substantial damage. Probable cause: The in-flight separation of the left aft cluster fitting assembly following the loss of torque on the lock nut due to a manufacturing defect. --- 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.