N725YX
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.
25 reports on file, 2020-01-12 – 2023-06-06.
Part: LEVER — INOPERATIVE (ZONE 700) · airframe 18,566 hrs · 12,584 cycles
LANDING GEAR DID NOT RETRACT AFTER TAKE OFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R LANDING GEAR CONTROL LEVER.
Part: HINGE — CORRODED (ZONE 900) · corrosion level 2 · airframe 18,227 hrs · 12,291 cycles
CF III WATER ACCESS DOOR HINGE CORRODED. R&R IAW SRM 51-41-02.
Part: SUPPORT BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,227 hrs · 12,291 cycles
AFT CARGO DOOR SURROUND SUPP CLIP CORRODED AT FR 80 STGR 26R. R&R IAW SRM 51-41-02 AND 51-43-03.
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,227 hrs · 12,291 cycles
FLOOR STRUCTURE GUSSET PLATE CORRODED AT FR 90 RBL 24. R&R IAW SRM 51-41-02.
Earlier reports · 2020–2021 · 21 reports
2021
Part: RIB — CRACKED (ZONE 300) · airframe 13,838 hrs · 9,160 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CRACK FOUND ON VERT STAB AFT RIB SPAR 9/10. REPLACED AFT SPAR RIB 9/10 IAW SRM 51-41-01.
Part: RIB — CRACKED (ZONE 300) · airframe 13,838 hrs · 9,160 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CRACK FOUND ON VERT STAB AFT SPAR RIB 11. AFT SPAR RIB 11 WAS REPLACED IAW SRM 51-41-01.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
DURING HEAVY CHECK MAINTENANCE FOUND LEVEL 2 CORROSION ON CENTER FUSELAGE 3 FLOOR STRUCTURE LH INBD SEAT TRACK BEAM AT FR 86. SEAT TRACK BEAM WAS REPLACED IAW SRM 51-43-03.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
CORROSION FOUND ON CENTER FUSELAGE III FLOOR STRUCTURE R/H INBOARD SEAT TRACK BEAM AT FR 86. CENTER FUSELAGE III FLOOR STRUCTURE R/H INBOARD SEAT TRACK AT FRAME 86 REPLACED WITH NEW P/N: 170-86082-005 IAW E175 SRM 51-43-03 & 51-41-01.
Part: RIB — CRACKED (ZONE 300) · airframe 13,838 hrs · 9,160 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CRACK ON RH HORZ. STAB RIB 12. RIB WAS REPLACED IAW EMB170EO-55-10-0004.
Part: SHEAR PANEL — CORRODED (FRAME 88) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
CORROSION FOUND ON CENTER FUSELAGE III FLOOR SUPPORT SHEAR PANEL AT FR 88 AND RBL9. FLOOR SUPPORT SHEAR PANEL @ FR 88 & RBL 9 FOUND CORRODED HAS BEEN REMOVED & REPLACED IAW ERJ 175 SRM 51-43-01 & 51-42-01.
Part: FLOOR SUPPORT — CORRODED (FRMS 88-90) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
LEVEL 2 CORROSION WAS FOUND ON RH PANEL SUPPORT BTWN FR88-90. SUPPORT WAS REPLACED IAW SRM 51-42-01
Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
CORROSION FOUND ON FWD FUSELAGE FLOOR STRUCTURE L/H INBOARD SEAT TRACK UPPER SURFACE AT FR 16. FWD FUSELAGE FLOOR STRUCTURE, L/H INBD SEAT TRACK AT FR 16, REMOVED AND REPLACED IAW EMB 170/175 SRM 51-41-01 AND 51-43-01
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
CORROSION FOUND ON CENTER FUSELAGE III FLOOR SUPPORT STRUCTURE IB GUSSET PLATE AT FR 90, RHS. FLOOR SUPPORT STRUCTURE I/B GUSSET PLATE @ FR 90 R/H FOUND CORRODED HAS BEEN REMOVED AND REPLACED IAW ERJ 175 SRM 51-41-02
Part: SEAT TRACK — CORRODED (FRM 16) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
CORROSION FOUND ON FWD FUSELAGE FLOOR STRUCTURE L/H INBOARD SEAT TRACK UPPER SURFACE AT FR 16. FWD FUSELAGE FLOOR STRUCTURE CORRODED L/H INBD SEAT TRACK AT FR16, REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-41-01 AND 51-43-01.
Part: DOUBLER — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
CFIII, CORROSION FOUND ON DOUBLER RH SIDE BTWN FR 85-86. DOUBLER FOUND CORRODED RH SIDE BTWN FR 85-86 HAS BEEN REMOVED & REPLACED IAW ERJ 175 SRM 51-41-01 & 51-43-01
Part: GUSSET — CORRODED (FRM 90) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
LEVEL 2 CORROSION WAS FOUND ON CENTER FUSELAGE 3 SUPPORT GUSSET PLATE FR90 IAW SRM 51-41-02
Part: SHEAR PANEL — CORRODED (FRAME 88) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
CORROSION FOUND ON CENTER FUSELAGE III FLOOR SUPPORT SHEAR PANEL AT FR 88 ND LBL9. FLOOR SUPPORT SHEAR PANEL @ FR 88 & LBL 9 FOUND CORRODED HAS BEEN REMOVED AND REPLACED IAW ERJ 175 SRM 51-43-01 & 51-42-01.
Part: DOUBLER — CORRODED (FRMS 85-86) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
LEVEL 2 CORROSION FOUND ON DOUBLER BTWN FR85-86. DOUBLER WAS REPLACED IAW SRM 51-41-01
Part: SHEAR PANEL — CORRODED (FRAME 88) · corrosion level 2 · airframe 13,838 hrs · 9,160 cycles
CORROSION FOUND ON CENTER FUSELAGE III FLOOR SUPPORT MID SHEAR PANEL AT FR 88. FLOOR SUPPORT MID SHEAR PANEL @ FR 88 FOUND CORRODED HAS BEEN REMOVED & REPLACED IAW ERJ 175 SRM 51-42-01 & 51-43-01
Part: SPAR — CRACKED (ZONE 500) · airframe 13,838 hrs · 9,160 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CRACK WAS FOUND AT LH WING OB SPAR 1 AT WING TIP ATTACHMENT. SPAR WAS REPLACED IAW SRM 51-43-02
Part: RIB — CRACKED (ZONE 300) · airframe 13,838 hrs · 9,160 cycles
RH H-STAB RIB 10A RH CRACKED. R/H H-STAB RIB 10A REPLACED REFERENCE 170 EO 55-10-0004_1 TASK 4500882-3000-0053 FOR CORRECTIVE ACTION
Part: SPAR — CRACKED (ZONE 600) · airframe 13,838 hrs · 9,160 cycles
SUSPECT CRACK AT RH WING O/B SPAR AT WINGTIP ATTACHMENT. R/H WING O/B SPAR 1 AT WINGTIP ATTACHMENT REPLACED WITH NEW IAW E175 51-43-01 / -02 AND 51-41-02.
2020
Part: SKIN — OUT OF LIMITS (FRAMES 3-4) · airframe 11,712 hrs · 7,732 cycles
***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** EXTERNAL FUSELAGE SKIN, UNRECORDED BLENDOUT FOUND AT SKIN FR3+12" & 2" BELOW STGR12R RVSM AREA. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW ETD2020-170-001206. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: SKIN — CRACKED (LT WINGLET) · airframe 11,712 hrs · 7,732 cycles
***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** LH WINGTIP FOUND CRACKED. REPLACED LH WINGTIP IAW AMM 57-30-00-400-801-A. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: STRUCTURE — CRACKED (RT WING TIP) · airframe 11,712 hrs · 7,732 cycles
***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** RH WINGTIP FOUND CRACKED. REPLACED RH WINGTIP IAW AMM 57-30-00-400-801-A. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.