N420YX
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.
21 reports on file, 2015-10-31 – 2021-07-02.
Part: FITTING — DIRTY (L2 DOOR) · airframe 18,946 hrs · 12,752 cycles
L2 DOOR HARD TO OPEN/CLOSE, LOUD SQUEAK/RUB NOISE. CLEANED DEBRIS ON THE FITTINGS AND TRACKS ON L2 DOOR IAW AMM 52-12-23.
Earlier reports · 2015–2020 · 20 reports
2020
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,450 hrs · 11,797 cycles
FWD PAX CABIN BEFORE COCKPIT EXIT LOCATOR SIGN INOP AFTER DEEP CYCLE ELPU NR 1. R & R ELPU NR 1, IAW AMM 22-50-01.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,450 hrs · 11,797 cycles
AFT PAX CABIN CENTER GALLEY EXIT LOCATOR SIGN L2 DOOR EXIT MARKING SIGN INOPERABLE AFTER DEEP CYCLE ELPU NR 3. R & R ELPU NR 3.
Part: SPAR — CRACKED (LT WING) · airframe 17,090 hrs · 11,557 cycles
CRACKED SPAR 1 ON LT WING TIP. REMOVED AND REPLACED SPAR 1 ON LT WING TIP, REF SRM 51-40-08. SEE EAMS WO NR H7490 SEQ NR 5505 SN 160 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK AT BNA.
2018
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,822 hrs · 8,749 cycles
EMERGENCY LIGHT BATT FAULT MESSAGE ON EICAS. R&R ELPU AFT RT OB IAW AMM 33-50-01. OPS CHECK GOOD, FAULT CLEARED.
Part: BATTERY — FAULTED (CABIN) · airframe 12,211 hrs · 8,342 cycles
EMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE. R&R EMERGENCY LIGHT POWER UNIT BATTERY IAW AMM 33-50-01.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 11,879 hrs · 8,127 cycles
WHILE IN HEAVY CHECK, LT HORIZONTAL STABILIZER RIB 12 CRACKED ALONG TOP FASTENERS BETWEEN FRONT AND MIDDLE SPAR. (MAJOR REPAIR) REMOVED DAMAGED RIB 12, FROM LT HORIZONTAL. LOCATED, DRILLED AND INSTALLED NEW RIB 12, ON LT HORIZONTAL REF SRM 51-40-08.
Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION AT FR 87-88 RT OB GALLEY SUPPORT BRACKET. REMOVED RT OB GALLEY SUPPORT BRACKET AT FR 87-88 PER SRM 51-40-08 LOCATED AND DRILLED RT OB GALLEY SUPPORT BRACKET AT FR 87-88 PER SRM 51-40-02. APPLIED ALODINE TO HOLES PER SRM 51-23-04 INSTALLED FR 87-88 RT OB GALLEY SUPPORT BRACKET PER SRM 51-40-08. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION AT FR 87-88 GALLEY SUPPORT APPROX 18" ROBL. REMOVED, REPLACED SUPPORT WITH NEW AND TOP COATED. P/N 170-86131-001. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION ON FR 87- FR 88 CENTER SHEAR PANEL AS MARKED. REMOVED FR 87- FR 88 CENTER SHEAR PANEL. REF SRM 51-40-08 LOCATED, DRILLED AND ALODINE NEW FR 87- FR 88 CENTER SHEAR PANEL. REF SRM 51-40-02, 51-23-04 INSTALLED NEW FR 87- FR 88 CENTER SHEAR PANEL. REF SRM 51-40-08. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION ON RT GUSSET PLATE AT FR 90 AS MARKED. REMOVED, LOCATED AND DRILLED NEW GUSSET PLATE REF SRM 51-40-08 AND 51-40-02. INSTALLED NEW GUSSET PLATE AT FR 90 REF SRM 51-40-08. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 2,187 cycles
CORROSION AT FR 87 RT BEAM AS MARKED. BLENDED CORROSION AT FR 87 BEAM FOUND TO BE OUT OF LIMITS, LOCATED, DRILLED AND ALODINE NEW RT BEAM AT FR 87. REF SRM 51-40-02, 51-23-04 HFEC INSPECTED BLENDED AREA NO DEFECTS FOUND. REPLACED BEAM AT RT FR 87 REF SRM 51-40-08, RESTORED SURFACE PROTECTION. REF 51-23-06 TOP COAT CPM 51-25-00 CIC. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION FR 90 RT GUSSET AS MARKED. REMOVED, LOCATED AND DRILLED NEW GUSSET PLATE REF SRM 51-40-08 AND 51-40-02. INSTALLED NEW GUSSET PLATE AT FR 90 REF SRM 51-40-08. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION ON FR 87- FR 88 RT SHEAR PANEL AS MARKED. REMOVED FR 87- FR 88 RT SHEAR PANEL. REF SRM 51-40-08 LOCATED, DRILLED AND ALODINE NEW FR 87- FR 88 RT SHEAR PANEL. REF SRM 51-40-02, 51-23-04 INSTALLED SHEAR PANEL ATFR87-FR88 PER SRM 51-40-08. RESTORED SURFACE PROTECTION PER SRM 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION, O/B AFT ATTACH FITTING TO FWD LAV FR 16. REMOVED DAMAGE FROM THE O/B AFT ATTACH FITTING TO FWD LAV FR 16 REF SRM 51-10-03. MATERIAL LOSS IS .020" WHICH IS OUT OF LIMITS REF SRM 51-75-16. REMOVED AND LOCATED NEW O/B AFT ATTACH FITTING TO FWD LAV FR 16. REF SRM 51-40-08 & 51-40-02. INSTALLED NEW O/B AFT ATTACH FITTING TO FWD LAV FR 16 REF SRM 51-40-08 PN 170-13633-001. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION ON FR 89 RT SPLICE PLATE AS MARKED. REMOVED AND REPLACED CORRODED SPLICE PLATE REF SRM 51-40-08, RESTORED SURFACE PROTECTION REF SRM 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,879 hrs · 8,127 cycles
CORROSION, RT 3 HOLE PANEL AS MARKED FR 12-14. REMOVED OLD PANEL, LOCATED, DRILLED, AND ALODINED NEW RT 3 HOLE PANEL AT FR 12-14 REF SRM 51-40-02 SRM 51-23-04, INSTALLED RT 3 HOLE PANEL AT FR 12-14 REF SRM 51-40-08 APPLIED TOPCOAT TO RT 3 HOLE PANEL AT FR 12-14 REF SRM 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: LIGHT — DAMAGED (CABIN) · airframe 11,032 hrs · 7,591 cycles
FWD CABIN NEAR SEAT 1D EMERGENCY LIGHT STRIPS DAMAGED . R & R THE EMERGENCY LIGHT IAW AMM 33-50-21.
2016
Part: ACCESS PANEL — CORRODED (APU INLET) · corrosion level 2 · airframe 6,366 hrs · 4,856 cycles
MAINTENANCE FOUND CORROSION ON APU AIR INLET ACCESS PANEL 315GL ATTACH POINT STRUCTURE. MAINTENANCE REMOVED CORROSION IAW SRM 51-10-03 AND ETD 2016-170-070037.
2015
Part: LIGHT — FADED (CABIN) · airframe 4,909 hrs · 3,524 cycles
MAINTENANCE REPORTED THAT 2 SECTIONS OF EMERGENCY LIGHT STRIPS WERE FADED. MAINTENANCE R & R FADED SECTIONS OF EMEGENCY LIGHT STRIPS IAW AMM AND OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 4,572 hrs · 3,270 cycles
CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R FORWARD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.