N429YX
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.
22 reports on file, 2014-09-23 – 2023-06-29.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,746 hrs · 15,437 cycles
CORRODED SHEAR CLIP AT FRAME 75, STRINGER 29R-28R. CORRECTION: DISCREPANCY SHOULD STATE "CORRODED SHEAR CLIP AT FRAME 74, STRINGER 29R-28R- ". ALL WORK PERFORMED ON THIS TASK CARD WAS DONE AT FR 74, STGR 29R-28R. SHEAR CLIP AT FR 75 WAS NOT REPLACED. REMOVED AND REPLACED SHEAR CLIP AT FRAME 74, STRINGER 29R-28R REF EMB SRM 51-40-08. SEE WIPS AND TASKS FOR WORK ACCOMPLISHED.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,746 hrs · 15,437 cycles
AFT PASSENGER DOOR CUTOUT STRUCTURE, HAVE AREAS OF CORROSION AROUND FWD AND AFT EVACUATION SLIDE FITTING AT FR 85-87 STGR 17L AS MARKED. REMOVED AND REPLACED AFT PASSENGER DOOR CUTOUT LOWER BEAM AT FR 85-87 STGR 17L REF EMB SRM 51-40-08 . SEE WIP'S AND TASK FOR WORK ACCOMPLISHED
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,746 hrs · 15,437 cycles
FWD CARGO DOOR LOWER BEAM IS CORRODED AS MARKED BELOW THE CENTER SEAL REST. REMOVED AND REPLACED FWD CARGO LOWER BEAM. REF EMB SRM 51-40-08. SEE WIPS AND TASKS FOR WORK ACCOMPLISHED
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 22,746 hrs · 15,437 cycles
CENTER FUSELAGE III PAX CABIN FLOOR STRUCTURES LOCATED AT AFT WET AREA, HAVE CORROSION ON RH BEAM AT FR 86-89 STGR 17R AS MARKED. REMOVED AND REPLACED RH BEAM BETWEEN FR 86-89. REF EMB SRM 51-40-08.
Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,746 hrs · 15,437 cycles
CROSSBEAM FR 17, CENTER, HAS TWO AREAS OF CORROSION ON UPPER SURFACE. PERFORMED PERMANENT REPAIR BY CUTOUT AND L-ANGLE REPAIR ON CROSSBEAM FR 17 IN TWO EACH LOCATIONS IN ACCORDANCE WITH. REF SRM 53-00-10 REPAIR 03. SEE WIP'S AND TASKS FOR WORK PERFORMED.
Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,746 hrs · 15,437 cycles
CROSSBEAM FR 14, RIGHT SIDE, HAS TWO AREAS OF CORROSION ON UPPER SURFACE. PERFORMED PERMANENT DOUBLER REPAIR ON CROSSBEAM 14. REF EMB SRM 53-00-10 /REPAIR 03P. SEE WIPS AND TASKS FOR WORK ACCOMPLISHED
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,746 hrs · 15,437 cycles
CORROSION ON SHEER CLIP AT FR88 BETWEEN STR. 27-28R.REMOVED AND REPLACED SHEAR CLIP AT FR88 BETWEEN STR. 27-28R. REF EMB SRM 51-40-08. SEE WIP'S AND TASKS FOR WORK PERFORMED.
Earlier reports · 2014–2020 · 15 reports
2020
Part: GLOWSTRIP — WORN (CABIN) · airframe 16,562 hrs · 11,131 cycles
PHOTOLUMINESCENT STRIPS WORN ON LT SIDE OF FIRST CLASS SEAT 1A 2A. R & R PHOTOLUMINESCENT STRIPS.
Part: GLOWSTRIP — NOT REPORTED (CABIN) · airframe 15,968 hrs · 10,724 cycles
PHOTOLUMINESCENT LIGHT STRIP NEAR FWD GALLEY WARDROBE REQUIRES REPLACEMENT. R&R FWD GALLEY PHOTOLUMINESCENT LIGHT STRIP IAW AMM 33-50-21.
2019
Part: GLOWSTRIP — WORN (CABIN) · airframe 14,762 hrs · 9,959 cycles
PHOTOLUMINESCENT STRIP IN FRONT OF WARDROBE WORN. R&R PHOTOLUMINESCENT STRIP IAW AMM 33-50-21.
2018
Part: SERVICE DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,643 hrs · 7,855 cycles
WHILE IN HEAVY MAINT CHECK FOUND CORROSION INTERNAL SIDE OF WASTE SERVICE DOOR AT LATCHES AND BONDING JUMPER CONNECTION. REMOVED AND REPLACED WASTE SERVICE DOOR REF. AMM 20-10-07 .
Part: INTERCOSTAL — CORRODED (CABIN) · corrosion level 2 · airframe 11,643 hrs · 7,855 cycles
UPON REMOVAL OF RH SHEAR PANEL FR87-88, CORROSION FOUND ON OTBD INTERCOSTAL FOR GALLEY SUPPORT AT ATTACH HOLE. REMOVED AND REPLACED OTBD INTERCOSTAL FOR GALLEY SUPPORT REF. EMB SRM 51-40-08. SEE EAMS W/O H6442 SN 367 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,643 hrs · 7,855 cycles
CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 CENTER SHEAR PANEL. REMOVED AND REPLACED SHEAR PLATE REF SRM 51-40-08, APPLIED SURFACE PROTECTION TO SHEAR PANEL REF SRM 51-23-05,51-23-06-51-23-07. SEE EAMS W/O H6442 SN 186 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: STRUCTURE — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 11,643 hrs · 7,855 cycles
CORROSION STRUCTURAL FWD FUSELAGE WET AREA 53-10 RH FWD SILL. REMOVED AND REPLACED FWD RH SILL AT FR 12-14 APPLIED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05,51-23-06. SEE EAMS W/O H6442 SN 207 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 11,643 hrs · 7,855 cycles
CORROSION-RH SEAT TRACK AT FR84. COMPLIED WITH PERMANENT REPAIR OF RH IB SEAT TRACK IAW ETD2018-170-099194. SEE EAMS W/O H6442 SN 198 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 11,643 hrs · 7,855 cycles
CORROSION STRUCTURAL FWD FUSELAGE WET AREA 53-10 LH MONUMENT SUPPORT FR16. REMOVED AND REPLACED MONUMENT SUPPORT SRM 51-45-00, 51-23-04 APPLIED SURFACE PROTECTION TO NEW MONUMENT SUPPORT REF SRM 51-23-05,51-23-06,51-23-07. SEE EAMS W/O H6442 SN 209 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,643 hrs · 7,855 cycles
CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH CENTER GUSSET FRAME 90. REMOVED AND REPLACED REF. SRM 51-40-02,51-23-04,51-40-08,APPLIED SURFACE PROTECTION REF SRM 51-23-06. SEE EAMS W/O H6442 SN 191 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: FLOOR SUPPORT — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 11,643 hrs · 7,855 cycles
CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH AFT PANEL SUPPORT. REMOVED AND REPLACED RH AFT PANEL SUPPORT REF SRM 51-40-08, APPLIED SURFACE PROTECTION TO SHEAR PANEL REF SRM 51-23-05,51-23-06-51-23-07. SEE EAMS W/O H6442 SN 187 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
2016
Part: FLASHLIGHT — DISCHARGED (AFT CABIN) · airframe 6,374 hrs · 4,476 cycles
CREW REPORTED THAT THE AFT TWO FLIGHT ATTENDANT FLASHLIGHTS WERE INOPERATIVE. MAINTENANCE CHARGED THE FLASHLIGHTS IAW AMM AND OPS CHECKED GOOD.
Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 4,769 hrs · 3,377 cycles
MAINTENANCE REPORTED THAT THE AFT LT F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R FLASHLIGHT BULB IAW AMM AND OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 4,647 hrs · 3,294 cycles
THE CREW REPORTED THE THE F/O'S FLASHLIGHT WAS NOT OPERATIVE. R & R FLASHLIGHT BATTERIES IAW AMM AND OPS CHECKED GOOD.
2014
Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 763 hrs · 528 cycles
CREW REPORTED THAT THE AUTOTHROTTLES FAILED AND THEY COULD NOT GET THE GUIDANCE TO LOCK. CREW DECLARED AN EMERGENCY, RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET ACFT POWER IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.