N406YX
Registered owner: REPUBLIC AIRWAYS INC, IN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
33 reports on file, 2013-11-07 – 2024-10-16.
Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,640 hrs · 18,933 cycles
CENTER FUSELAGE III STRINGER 20R CORRODED BETWEEN FRAMES 85-86. PERFORMED A SPLICE REPAIR IAW ETD2024-170-028307 AND SRM 53-22-03.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,640 hrs · 18,933 cycles
WHILE IN HEAVY CHECK - CENTER FUSELAGE III STRINGER 20R CORRODED BETWEEN FRAMES 85-86. PERFORMED STRINGER SPLICE REPAIR ON CENTER FUSELAGE III STGR 20R BETWEEN FRAMES 83-84 REFER ETD2024-170-028307 AND SRM 53-22-03/REPAIR 02P.
Earlier reports · 2013–2021 · 31 reports
2021
Part: BELLCRANK — OUT OF LIMITS (NR 1 ENGINE VG) · airframe 19,911 hrs · 13,323 cycles
ENGINE 1 CONTROL FAULT DURING DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R E1 VG ACTUATOR BELL CRANK IAW ESM 72-00-00 SP016.
2020
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,585 hrs · 11,792 cycles
FWD 3 EMERGENCY LIGHTS FLICKER. TROUBLESHOT SYSTEM AND R&R FWD CEILING EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-50-01.
Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 17,422 hrs · 11,681 cycles
WHILE IN HEAVY CHECK FOUND CORROSION ON RH CENTER SEAT TRACK FRAME 84. CUT OUT CORRODED SEAT TRACK AT FRAME 84 AND PERFORMED REPAIR SPLICE REF EMB ETD2020-170-000476.
2019
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,713 hrs · 11,403 cycles
EXIT SIGN ABOVE COCKPIT DOOR DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS TESTED. R&R EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. OPS CHECK OK.
2018
Part: WEB — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 11,913 hrs · 8,050 cycles
MAINTENANCE DISCOVERED MULTIPLE AREAS OF CORROSION AT FWD WET AREA RT FLOOR WEB. FRAMES 12 - 14. REMOVED AND REPLACED THE FWD SILL PLATE IAW SRM 51-43-03, AND 51-41-01.
Part: SKIN — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
CORROSION BETWEEN FRAMES 24 AND 25. AT EDGE OF FORWARD CARGO DOOR CUTOUT. BLENDED AND RESTORED FINISH IAW ETD2018-170-009072.
Part: SEAL REST — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
FORWARD CARGO DOOR CUTOUT AFT CORNER SEAL REST IS CORRODED AROUND THE NUTPLATE. REMOVED AND REPLACED THE FORWARD CARGO DOOR CUTOUT AFT CORNER SEAL REST IAW SRM 51-40-08.
Part: SUPPORT — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA BETWEEN FRAMES 89 AND 90, RBL 12 RT SUPPORT IS CORRODED. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-08, 51-23-04, 51-23-05, AND 51-23-06.
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
GUSSET AT FRAME 90, LBL 12 IS CORRODED. REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-08.
Part: FINGER DOUBLER — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
FWD CARGO DOOR CUTOUT BETWEEN FRAMES 24 AND 25 FWD FINGER DOUBLER IS CORRODED. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-40-08, AND 51-40-02.
Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA BETWEEN FRAMES 87 AND 88, LBL 10 TO RBL 10 CENTER SHEAR PANEL IS CORRODED. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-42-01, SRM 51-23-04.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
SURFACE CORROSION ON BOTH LOWER ANGLES ON PANEL 1431DL. REMOVED AND REPLACED LOWER ANGLES ON 1431DL REF. SRM 51-40-02,51-40-08 AMM 20-10-07. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA
Part: SPLICE — CORRODED (FRAME 89) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA AT FRAME 89, RBL 12 RT SPLICE CORRODED. REMOVED AND REPLACED THE SPLICE IAW SRM 51-40-08.
Part: SUPPORT — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA BETWEEN FRAMES 88 AND 89, LBL 45 SUPPORT PANEL IS CORRODED. REMOVED AND REPLACED SUPPORT PANEL IAW SRM 51-40-08.
Part: FINGER DOUBLER — CORRODED (FRAMES 77-78) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT CARGO DOOR CUTOUT FORWARD FINGER DOUBLER HAS BUBBLED PAINT WITH CORROSION BETWEEN FRAMES 77 AND 78. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-43-01, 51-43-02, AND 51-40-02.
Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA AT FRAME 84 RBL12, SEAT TRACK IS CORRODED. PERFORMED A DOUBLER AND FILLER REPAIR IAW SRM 53-23-10, REPAIR 4.
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA AT FRAME 90, RBL 12 RT GUSSET IS CORRODED, REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-08.
Part: FINGER DOUBLER — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
FWD CARGO DOOR CUTOUT BETWEEN FRAMES 26 AND 27 AFT FINGER DOUBLER IS CORRODED. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-40-08, AND 51-40-02.
Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA AT FRAME 89, RBL 45 RT FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-01, AND 51-43-03.
Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,744 hrs · 5,014 cycles
AFT WET AREA BETWEEN FRAMES 87 AND 88, RBL 13 TO 45. RT SHEAR PANEL IS CORRODED. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-42-01, 51-41-02, 51-43-04, AND 51-40-08.
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA AT FRAME 90, LBL 12 LT MIDDLE GUSSET IS CORRODED. REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-08.
Part: ANGLE — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA BETWEEN FRAMES 89 AND 90, RBL 12, THE INTERCOSTAL ATTACHED TO THE RT BEAM IS CORRODED. REMOVED AND REPLACED THE L ANGLE IAW SRM 51-23-04, 51-23-05, 51-23-06, AND 51-40-08.
Part: SEAL REST — CORRODED (FRAMES 25-26) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
FORWARD CARGO DOOR CUTOUT CENTER SEAL REST CORRODED. REMOVED AND REPLACED FORWARD CARGO CUTOUT CENTER SEAL REST IAW SRM 51-40-08.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
SURFACE CORROSION ON BOTH LOWER ANGLES ON PANEL 1441FR. REMOVED AND REPLACED LOWER ANGLES ON 1441FR REF SRM 51-40-02, 51-40-08 AMM 20-10-07. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA BETWEEN FRAMES 85 AND 86, RBL 12 RT UPPER SHEET IS CORRODED. REMOVED AND REPLACED THE UPPER SHEET IAW SRM 51-41-01, 51-40-02, 51-43-04, AND 51-23-06.
Part: SUPPORT — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
FWD WET AREA RT SUPPORT AT FRAMES 13 AND 14 CORRODED. REMOVED AND REPLACED THE SUPPORT SRM 51-23-04, 51-23-05, 51-23-06, AND 51-40-08.
Part: STAND OFF — CORRODED (FRAME 85) · corrosion level 2 · airframe 11,744 hrs · 8,014 cycles
AFT WET AREA AT FRAME 87, RBL 35 RT NUTPLATE STANDOFF IS CORRODED. REPLACED NUTPLATE STANDOFF IAW SRM 51-23-05.
2017
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,663 hrs · 7,332 cycles
FOUND L2 DOOR EXIT LIGHT INOPERATIVE DURING RTWO DAY CHECK. R & R THE EMERGENCY LIGHT BATTERY NR 3 IAW AMM 33-55-01. OPS CHECKED GOOD.
2015
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,293 hrs · 2,903 cycles
MAINTENANCE REPORTED THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE R & R EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
2014
Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 970 hrs · 620 cycles
CREW REPORTED THAT DURING EMERGENCY EVACATION OF ACFT AT GATE, THE R1 DOOR DID NOT FULLY OPEN AND THE SLIDE DID NOT DEPLOY. F/O KICKED DOOR AND THE SLIDE FULLY DEPLOYED. ACFT IS CURRENTLY OUT OF SERVICE.
2013
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 324 hrs · 226 cycles
CREW REPORTED THAT THE F/O FLASHLIGHT WAS INOPERATIVE. MAINTEANCE R & R F/O FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.