Hybrid Technique for Inferior Turbinate Surgery
Background and Objectives Inferior turbinate hypertrophy causes nasal obstruction. When conservative treatments fail, surgical intervention is needed to preserve function and allow for repeatability. This paper details a hybrid surgical technique combining submucosal microdebrider-assisted turbinoplasty (MAT) and coblation-channeling turbinoplasty (CCT) for mucosa-sparing inferior turbinate reduction.Subjects and Method This technique uses MAT for precise volume reduction of the thick medial mucosal layer (MML) and CCT (via an ArthroCare ReFlex Ultra 45 wand [ArthroCare Corporation]) to contract the venous sinusoid-rich inferior mucosal layer (IML) while carefully preserving the lateral mucosal layer (LML), which is crucial for humidification and mucociliary clearance. Procedures are typically office-based and carried out under local anesthesia.Results This hybrid turbinoplasty significantly improves nasal airway patency. For a 45-yearold male with chronic bilateral nasal obstruction, his Nasal Obstruction Symptom Evaluation (NOSE) score improved from 75 to 20 and Visual Analog Scale (VAS) from 8/10 to 2/10 6 months post-op, with preserved mucosa. For a 32-year-old female with persistent allergic rhinitis-induced obstruction, her NOSE score decreased from 65 to 15 and VAS from 7/10 to 1/10 at 6 months, showing excellent healing. No significant complications were observed.Conclusion This hybrid technique is an effective, physiologically conscious method for inferior turbinate reduction. Strategically targeting specific mucosal layers optimizes volume reduction while maximizing functional preservation, representing a patient-centered advancement in turbinate surgery.
Authors
- Dong Hyun Kim
- Jin Lee
- Jae Hoon Lee
Publication Details
- Journal
- Korean Journal of Otorhinolaryngology - Head and Neck Surgery
- Published
- 2025-09-03
- DOI
- https://doi.org/10.3342/kjorl-hns.2025.00325
- Primary Topic
- Nasal Surgery and Airway Studies
- Type
- article
- Field-Weighted Citation Impact
- 0.00