# NJS145 LLC: FAA repair station DXTR401D

- Type: FAA-certificated repair station (14 CFR Part 145)
- Certificate number: DXTR401D
- Designator: DXTR
- Address: 4111 BRIDGEWAY AVENUE, COLUMBUS, OH 43219
- Accountable manager: DUGGER, BRADLEY, (614) 849-7011, bdugger@netjets.com
- Liaison: DUGGAR, BRAD, (614) 849-7011, bduggar@netjets.com
- On the FAA list: On the list of October 26, 2026; listed since October 26, 2026 or earlier (OpenAirDocs’ first copy)
- Service difficulty reports filed: 269
- Source: FAA Find a Facility dashboard, https://www.faa.gov/av-info/facility-dashboard
- Page: https://openairdocs.org/faa-repair-station/DXTR401D/njs145-llc

The FAA writes names in capitals; the mixed case here is OpenAirDocs'. The dashboard has no certificate dates, and nothing on it shows whether a certificate is in good standing.

## Ratings

- Airframe: Limited
- Powerplant: Limited
- Radio: Limited
- Instrument: Limited
- Accessory: Limited
- Limited: Emergency equipment

A Limited class covers only the makes and models in the station's operations specifications (14 CFR 145.61), which the FAA doesn't publish.

## Service difficulty reports (269, newest 50)

Filed under designator DXTR by a repair station (submitter type B).

- [SDR DXTR2026111102](https://openairdocs.org/sdr/DXTR2026111102), Nov 11, 2026: Cessna 680A. COMPRESSOR BLADE. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSPECTION. DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW  (N915QS)
- [SDR DXTR2026111101](https://openairdocs.org/sdr/DXTR2026111101), Nov 11, 2026: Cessna 680A. COMPRESSOR BLADE. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. R & R ENGINE IAW AMM 72- (N591)
- [SDR DXTR2026103102](https://openairdocs.org/sdr/DXTR2026103102), Oct 31, 2026: Cessna 680A. TURBINE BLADES. CRACKED. 2ND STAGE HIGH PRESSURE TURBINE BLADES FAILED SCHEDULED BORESCOPE INSPECTION DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-0 (N914QS)
- [SDR DXTR20261031](https://openairdocs.org/sdr/DXTR20261031), Oct 31, 2026: Cessna 680A. TURBINE BLADES. CRACKED. 2ND STAGE HIGH PRESSURE TURBINE BLADES FAILED BORESCOPE INSPECTION DUE TO CRACKS OUT OF LIMITS IAW SI 33-2026R3 DATED OC (N581QS)
- [SDR DXTR2026101701](https://openairdocs.org/sdr/DXTR2026101701), Oct 17, 2026: Cessna 680A. TURBINE BLADES. CRACKED. 2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00- (N597QS)
- [SDR DXTR2026092701](https://openairdocs.org/sdr/DXTR2026092701), Sep 27, 2026: Cessna 680A. COMPRESSOR BLADE. CRACKED. RIGHT ENGINE, SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP, DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R THE (N585QS)
- [SDR DXTR2026091102](https://openairdocs.org/sdr/DXTR2026091102), Sep 11, 2026: Cessna 680A. TURBINE BLADES. CRACKED. 2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. R&R ENGINE PER CE-680A AMM  (N912QS)
- [SDR DXTR2026091101](https://openairdocs.org/sdr/DXTR2026091101), Sep 11, 2026: Cessna 680A. TURBINE BLADES. CRACKED. 2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. CORRECTIVE ACTION: R&R ENGI (N912QS)
- [SDR DXTR2026090311](https://openairdocs.org/sdr/DXTR2026090311), Sep 3, 2026: Cessna 680A. TURBINE BLADES. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72- (N916QS)
- [SDR DXTR2026090310](https://openairdocs.org/sdr/DXTR2026090310), Sep 3, 2026: Cessna 680A. TURBINE BLADES. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72- (N916QS)
- [SDR DXTR2026090308](https://openairdocs.org/sdr/DXTR2026090308), Sep 3, 2026: Cessna 680A. TURBINE BLADES. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72- (N905QS)
- [SDR DXTR2026090307](https://openairdocs.org/sdr/DXTR2026090307), Sep 3, 2026: Cessna 680A. TURBINE BLADES. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. R&R ENGINE IAW AMM 72-00 (N902QS)
- [SDR DXTR2026090306](https://openairdocs.org/sdr/DXTR2026090306), Sep 3, 2026: Cessna 680A. TURBINE BLADES. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72- (N677QS)
- [SDR DXTR2026090305](https://openairdocs.org/sdr/DXTR2026090305), Sep 3, 2026: Cessna 680A. TURBINE BLADES. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-
- [SDR DXTR2026090304](https://openairdocs.org/sdr/DXTR2026090304), Sep 3, 2026: Cessna 680A. TURBINE BLADES. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R&R ENGINE IAW AMM 72-00 (N528QS)
- [SDR DXTR2026090303](https://openairdocs.org/sdr/DXTR2026090303), Sep 3, 2026: Cessna 680A. TURBINE BLADES. CRACKED. SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. (N528QS)
- [SDR DXTR2026090302](https://openairdocs.org/sdr/DXTR2026090302), Sep 3, 2026: Cessna 680A. BLADES. CRACKED. BLADE S/N PMOXM75 SUCTION SIDE CRACK .155 INCH. PRESSURE SIDE CRACK .407 INCH (OPEN) THROUGH COOLING HOLE WITH CRACK PRE (N572QS)
- [SDR DXTR2026090301](https://openairdocs.org/sdr/DXTR2026090301), Sep 3, 2026: Cessna 680A. RIB. CRACKED. FOUND CRACK ON THE PYLON RIB RT AFT FIREWALL REMOVED THE CRACKED RIB IAW SRM 51-40-05. MATCH DRILLED HOLES IN NEW RIB IA (N572QS)
- [SDR DXTR2026090300192](https://openairdocs.org/sdr/DXTR2026090300192), Sep 3, 2026: Cessna 680A. RIB. CRACKED. FOUND CRACK IN PYLON RIB RIGHT AFT FIREWALL. REMOVED CRACKED RIB IAW SRM 51-40-05. MATCH DRILLED HOLES IN NEW RIB IAW SR (N572QS)
- [SDR DXTR2026090201](https://openairdocs.org/sdr/DXTR2026090201), Sep 2, 2026: Cessna 680A. COMPRESSOR BLADE. CRACKED. FAULT: DURING 100 HR 2ND STAGE HPT BORESCOPE RE-INSPECT OF ENGINE, FOUND PREVIOUS CRACK ON SUCTION SIDE OF BLADE HAS MIG (N572QS)
- [SDR DXTR2026071701](https://openairdocs.org/sdr/DXTR2026071701), Jul 14, 2026: Cessna 680A. FUEL LINE. CRACKED. FOUND L/H ENG FUEL LEAK AT FUEL PRESSURE SWITCH ON FUEL SUPPLY LINE WITH FUEL RUNNING AFT OF SWITCH AND DRIPPING FROM AD (N508QS)
- [SDR DXTR2026050100314](https://openairdocs.org/sdr/DXTR2026050100314), May 1, 2026: Cessna 680A. SKIN. CORRODED. POSSIBLE CORROSION ON LOWER LT WING SKIN AT TIP CAP. REMOVED CORROSION FROM SKIN REF SRM 51-10-01. NDT SERVICES PROVIDED (N506QS)
- [SDR 2026FA0000298](https://openairdocs.org/sdr/2026FA0000298), Apr 25, 2026: Cessna 680A. SKIN. CORRODED. LH HORIZONTAL STAB UPPER SKIN 3 SPOTS OF CORROSION FWD OF PANEL 351AC. FIX... COMPLIED WITH RFTS 117040 DATED 24APR26 AN (N653QS)
- [SDR DXTR2025102901](https://openairdocs.org/sdr/DXTR2025102901), Oct 29, 2025: Emb EMB505. WIRE HARNESS. FAULTED. DURING APPROACH WHILE HANDFLYING, THERE HAD TO BE SIGNIFICANT INPUT IN AILERON TO MAINTAIN LEVEL FLIGHT. FUEL INDICATION (N327QS)
- [SDR DXTR2025101801](https://openairdocs.org/sdr/DXTR2025101801), Oct 18, 2025: Cessna 680A. SUPPORT. CRACKED. LH FWD WHEEL WELL FAIRING SUPPORT FRAME P/N 6910269-49 CRACKED AT RIVET.... EDDY CURRENT NDT INSPECTION PERFORMED BY TOL (N562QS)
- [SDR DXTR2025072901](https://openairdocs.org/sdr/DXTR2025072901), Jul 28, 2025: Textrn TEXTRON700. CAP SEAL. FRACTURED. WHILE ACCOMPLISHING LT MLG LUBRICATION TASK CARD AMM 12-20-10-612, AND WHILE LUBRICATING INBOARD END OF LT MLG ACTUATOR, (N830QS)
- [SDR DXTR202502270055](https://openairdocs.org/sdr/DXTR202502270055), Feb 27, 2025: Cessna 680A. SKIN. GOUGED. GOUGE, TAILCONE, AFT UPPER MIDDLE SKIN. ACCOMPLISHED FR-680A-0063-14787 REV - DATED 2-20-25 AND FAA FORM 8110-3 DATED 02 (N525QS)
- [SDR DXTD2025021200097](https://openairdocs.org/sdr/DXTD2025021200097), Feb 12, 2025: Cessna 680A. DECK PLATE. CORRODED. FOUND POTTY DECK CORRODED ON UNDER SIDE. COMPLIED WITH NETJETS RFTS-112907 N608QS (680A-0255) TOILET DECK SKIN CORROSION (N608QS)
- [SDR DXTR2024111101](https://openairdocs.org/sdr/DXTR2024111101), Nov 11, 2024: Cessna 680A. VORTEX GEN. CORRODED. CORROSION UNDER LH LOWER VORTEX GENERATOR TAIL CONE STINGER. RESOLUTION: ACCOMPLISHED MINOR REPAIR IAW RFTS-112233 (N681QS)
- [SDR DXTR2024101901](https://openairdocs.org/sdr/DXTR2024101901), Oct 19, 2024: Textrn TEXTRON700. PANEL. CORRODED. APU PANEL 331CR CONTAINS LEVEL 2 CORROSION. ACCOMPLISHED MINOR PERMANENT REPAIR IAW AQRD RFTS-11996 DATED OCT 19/2024. (N804QS)
- [SDR DXTR2024092201](https://openairdocs.org/sdr/DXTR2024092201), Sep 22, 2024: Cessna 680A. ACCESS PANEL. CORRODED. CORROSION ON LH HORIZONTAL STAB ACCESS PANEL NUT PLATES FOR PANEL 351AB,351BB,341AR, 341CR, 341DR, 341ER,341AL AND 341CL (N515QS)
- [SDR DXTR2024082501](https://openairdocs.org/sdr/DXTR2024082501), Aug 16, 2024: Cessna 680A. FITTING. CORRODED. NLG ACTUATOR AFT ATTACHMENT CASTING IS CORRODED, STARTED REMOVAL OF CORROSION ON NLG ACTUATOR AFT ATTACHMENT FITTING IAW (N591QS)
- [SDR DXTR2024072101](https://openairdocs.org/sdr/DXTR2024072101), Jul 21, 2024: Textrn TEXTRON700. THRUST REVERSER. CORRODED. LH & RH ENGINE UPPER AND LOWER THRUST REVERSER DOORS HAVE EVIDENCE OF CORROSION.....LH & RH ENGINE UPPER AND LOWER THRUS (N805QS)
- [SDR DXTR2024071501](https://openairdocs.org/sdr/DXTR2024071501), Jul 15, 2024: Textrn TEXTRON700. THRUST REVERSER. CORRODED. LEFT THRUST REVERSER UPPER AND LOWER PIVOT DOOR ASSEMBLIES HAVE SEVERAL AREAS OF CORROSION. DETERMINED CORROSION AROUND  (N828QS)
- [SDR DXTR2024070401](https://openairdocs.org/sdr/DXTR2024070401), Jul 4, 2024: Textrn TEXTRON700. THRUST REVERSER. CORRODED. RH TR INNER SURFACE LEVEL 1 CORROSION. ACCOMPLISHED MINOR REPAIR IAW AQRD RFTS-111168 (N838QS)
- [SDR DXTR2024070400001](https://openairdocs.org/sdr/DXTR2024070400001), Jul 4, 2024: Textrn TEXTRON700. SKIN. CORRODED. RH & LH THRUST REVERSER BUCKET SKIN CONTAINS LEVEL 1 CORROSION. ACCOMPLISHED MINOR REPAIR IAW AQRD RFTS 111171. (N838QS)
- [SDR DXTR2024062502](https://openairdocs.org/sdr/DXTR2024062502), Jun 25, 2024: Textrn TEXTRON700. STRUCTURE. CORRODED. LEFT THRUST REVERSER UPPER BUCKET, LOCATED ON O/B SIDE NEEDS PAINT TOUCH-UP. REPAIR OF PAINT & CORROSION PER AQRD EWO-59 (N830QS)
- [SDR DXTR20224062501](https://openairdocs.org/sdr/DXTR20224062501), Jun 25, 2024: Textrn TEXTRON700. FRAME. CORRODED. R/H T/R I/B FRAME BETWEEN BUCKETS NEEDS PAINT TOUCH-UP. REPAIR OF PAINT & CORROSSION PER AQRD EWO-5999 REV. IR. & AQRD 9 (N830QS)
- [SDR DXTR2024061601](https://openairdocs.org/sdr/DXTR2024061601), Jun 16, 2024: Textrn TEXTRON700. STRUCTURE. CORRODED. R/H T/R BUCKET HAS SIGNS OF CORROSION BEGINNING TO FORM... ACCOMPLISHED MINOR PERMANENT REPAIR IAW RFTS-111031 DATED 06/ (N829QS)
- [SDR DXTR2024061201](https://openairdocs.org/sdr/DXTR2024061201), Jun 5, 2024: Textrn TEXTRON700. THRUST REVERSER. CORRODED. LH T/R BUCKET HAS CORROSION ON OUTBD SIDE, L/H T/R TO BE REMOVED AND SENT OUT TO BE REPAIRED PER CUSTOMER REQUEST. REMOV (N829QS)
- [SDR DXTR2023092601](https://openairdocs.org/sdr/DXTR2023092601), Sep 26, 2023: Textrn TEXTRON700. FIRE BOTTLE. FALSE ACTIVATION. LEFT ENGINE FIRE BOTTLE SQUIB ASSEMBLIES FOUND IN OPPOSITE POSTIONS. OUR INVESTIGATATION REVEALLED THAT THE DISCHARGE OU (N809QS)
- [SDR DXTR2023082401](https://openairdocs.org/sdr/DXTR2023082401), Aug 24, 2023: Cessna 680A. CHECK VALVE. DETACHED. 2-EACH RIGHT WING FUEL TANK FUEL CHECK VALVE DETACHED FROM MOUNT. (N681QS)
- [SDR DXTR2022082602](https://openairdocs.org/sdr/DXTR2022082602), Aug 26, 2022: Cessna 120. GALLEY. SCRATCHED. DESCRIPTION: 1. 5" SCRATCHES AFT SIDE OF GALLEY DOORS - 2. TABLE BETWEEN SEAT 7 AND 9 LAMINATE GOUGED - 3. GALLEY COFFEE (N812QS)
- [SDR DXTR20220826](https://openairdocs.org/sdr/DXTR20220826), Aug 26, 2022: Cessna 120. PANEL. ELONGATED. VERTICAL STABILIZER HAS AN ELONGATED FASTENER HOLE AT THE 341CL PANEL (LH SIDE). RESOUTION: ACCOMPLISHED MAJOR REPAIR IA (N516QS)
- [SDR DXTR202204131](https://openairdocs.org/sdr/DXTR202204131), Apr 13, 2022: Cessna 560XL. LIGHT. BURNED OUT. RIGHT MLG INDICATOR LIGHT: ON FINAL APPROACH WE SELECTED THE GEAR DOWN AND HAD NO RIGHT MAIN GEAR INDICATOR LIGHT TO ILL (N661QS)
- [SDR DXTR20220329](https://openairdocs.org/sdr/DXTR20220329), Mar 29, 2022: Bombdr BD7001A11. HYDRAULIC LINE. DISCONNECTED. - PROBLEM DESCRIPTION: DURING OIL SERVICE TECH FOUND THE #2 ENGINE HYD PRESSURE LINE HAS LOOSE JAM NUT AND THREADS ARE M (N101QS)
- [SDR DXTR2022022801](https://openairdocs.org/sdr/DXTR2022022801), Feb 28, 2022: Cessna 560XL. AUTOPILOT SYS. BROKEN. YAW DAMPER: YAW DAMPER DOESN'T SEEM TO WORK IN TURBULENT AIR. PLANE FISH TAILS AND DUTCH ROLLS IN UNSTABLE AIR, BUT IS F (N588QS)
- [SDR DXTR2021062801](https://openairdocs.org/sdr/DXTR2021062801), Jun 28, 2021: Cessna 680A. SKIN. CORRODED. CORROSION FOUND ON THE TRAILING EDGE OF LEFT HORIZONTAL STABLIZER UPPER & LOWER SURFACES. REPAIRED IAW AQRD ERO-105005 D (N542QS)
- [SDR DXTR2021040601](https://openairdocs.org/sdr/DXTR2021040601), Apr 6, 2021: Cessna 680A. WIRE HARNESS. OPEN. LEFT HAND TAXI LIGHT INOPERATIVE.FOUND NLG WIRE HARNESS HAS OPEN IN WIRE. REMOVED AND REPLACED WIRE HARNESS PN - 8469800 (N521QS)
- [SDR DXTR2021031101](https://openairdocs.org/sdr/DXTR2021031101), Mar 10, 2021: Cessna 680A. CANISTER. CRACKED. DURING DESCENT, A FAINT SMELL OF FUEL WAS NOTICED IN CABIN FOR APPROXIMATELY 30 SECONDS. FOUND FUEL POOLING IN FLAP JACK (N513QS)

All 269: https://openairdocs.org/faa-repair-station/DXTR401D/njs145-llc/reports.md

---
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, except the copies of manufacturers’ service documents, which belong to their rights holders.