N126BZ
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (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, 2021-08-17 – 2026-04-24.
Part: BATTERY PACK — FAILED (ZONE 200) · airframe 42,054 hrs · 21,503 cycles
EMERGENCY LIGHTS FLICKERING ON AND OFF IN ARMED PPOSITION. EMERGENCY LIGHTS ALSO TURNED ON AFRTER AIRCRAFT WAS POWERED DOWN WITH SWITCH IN OFF POSITION. ERMER LT BATT FAULT EICAS INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT NR 4.
Part: BATTERY — FAILED (ZONE 200) · airframe 42,041 hrs · 21,498 cycles
EMERGENCY LIGHT BATTERY FAULT. R & R LT FWD EMERGENCY LIGHT BATTERY.
Part: BATTERY PACK — FAILED (ZONE 200) · airframe 42,054 hrs · 21,503 cycles
EMERGENCY BATT FAULT ON EICAS, FWD RH ELPU FAILED. R/R FWD RH ELPU PER AMM. OPS CHECK GOOD. - LATE SUBMISSION
Part: LIGHT SYS — MALFUNCTIONED (ZONE 200) · airframe 41,983 hrs · 21,462 cycles
FWD EMERGENCY LIGHTS FLICKERING. PERFORMED AIRCRAFT POWER RESET. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS PER AMM. OP CHECKED PASSED.
Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 41,975 hrs · 21,457 cycles
FWD EMERGENCY LIGHT BATTERY FAULT. EMERGENCY LIGHTS CAME ON UNCOMMANDED IN THE FWD GALLEY. CYCLED POWER. ITEM CLEARED.
Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 41,928 hrs · 21,425 cycles
EMER LT BATT FAULT. EMERGENCY LIGHTS CAME ON AND STAYED ON IN THE ARMED POSITION. CHARGED EMERGENCY LIGHTS. PERFORMED OPS CHECK WITH ENGINES RUNNING. OPS CHECKED GOOD.
Part: ELEC CONNECTOR — UNSECURE (ZONE 200) · airframe 41,898 hrs · 21,405 cycles
FA REPORTS EMERGENCY LIGHTS FLICKERING AT OVERWING EXIT. RESECURED ELECTRICAL CONNECTOR, OPS CHECK GOOD.
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles
RH FWD ELPU FUALTY. ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED FWD RH ELPU
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles
RH AFT ELPU FAULTY. ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED THE RH AFT ELPU
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles
ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED THE RH CENTER ELPU.
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles
ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. LH MIDDLE ELPU REPLACED
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles
ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED FWD LH ELPU.
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles
LH AFT ELPU FAULTY. ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED LH AFT ELPU.
Earlier reports · 2021–2025 · 20 reports
2025
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,345 hrs · 21,061 cycles
LH OVERWING EMERGENCY DOOR INTERIOR EXIT SIGN AND LH OVERWING FWD EXTERIOR EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTING ELPU #4.
2024
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 40,563 hrs · 20,546 cycles
EMERGENCY LIGHTS POWER UNITS INOP, THREE INTERIOR EMERGENCY LIGHTS INOP, R/R #2, #3, #6 EMERGENCY LIGHT POWER UNITS.
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 40,563 hrs · 20,546 cycles
EMERGENCY LIGHTS POWER UNITS INOP. THREE INTERIOR EMERGENCY LIGHTS INOP. R/R #2, #3, AND #5 EMERGENCY LIGHT POWER UNITS. PN 3400-22-10 AND SN'S 001821, 007464, 002963.
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 40,563 hrs · 20,546 cycles
EMERGENCY LIGHT POWER UNITS INOP. THREE INTERIOR EMERGENCY LIGHTS INOP. R/R #2, #3, AND #5
Part: ENGINE — VIBRATION (NR 2) · airframe 40,510 hrs · 20,511 cycles
ENGINE 2 VIBRATION ON HIGH PASS DURRING TAXI, AND THERE WAS A SLIGHT HAZE AND UNUSUAL SMELL. NO FIRE INDICATIONS NOR SMOKE IN THE COCKPIT OCCURED. AIRCRAFT RETURNED TO THE GATE. ENGINE R/R IN PROCESS FOR CORRECTIVE ACTION.
2023
Part: BATTERY — DISCHARGED (UNKNOWN)
THIS SDR SUBMITTED LATE DUE TO AUDIT FINDING. AFT EMERGENCY LIGHTS IN AFT GALLEY AREA WOULD NOT TURN OFF WHEN POWER WAS REMOVED. REPLACED BATTERY.
Part: SPLICE PLATE — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
AFT WET AREA CORROSION AT LH SHEAR PANEL FR 87 - FR 88. REMOVED AND REPLACED LH SPLICE PANEL AT FR 87 - FR 88 IAW EMB 190 SRM 51-40-08.
Part: UPPER SHEET — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
AFT WET AREA - CORROSION AT BEAM UPPER SHEET - FR85 - FR86 "Y" +10", BLENDED CORROSION ON BEAM UPPER SHEET FR85 - FR86 Y +10" IAW E-190 SRM 51-10-03. REMOVED AND REPLACED UPPER SHEET ON FR85 - FR86 Y+10" IAW E-190 SRM 51-40-08
Part: ATTACH FITTING — CORRODED (ZONE 900) · airframe 39,222 hrs · 19,640 cycles
FWD LAV FLOOR MOUNT ATTACH POINT CORRODED ON THE FLOOR DOUBLER 170-012118-001 TOP SURFACE AT FRM-16, STR-16L OUTBD - REMOVED AND REPLACED FWD LAV FLOOR MOUNT FITTING AT FRM-16, STR-16L (Y-273.0) IAW E-190 SRM 51-40-08
Part: SHEAR PANEL — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
AFT WET AREA - CORROSION AT RH CROSSBEAM DOUBLER - AT FR84. REMOVED AND REPLACED DOUBLER (SHEAR PANEL) AT FR 84 IAW E190 SRM 51-40-08.
Part: DOUBLER — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
CORROSION ON FLOOR DOUBLER ON CENTER MAIN BEAM AT FR 16. REMOVED AND REPLACED DOUBLER IAW E190 SRM 51-10-10
Part: ATTACH FITTING — CORRODED (ZONE 100) · airframe 39,222 hrs · 19,640 cycles
FWD LAV FLOOR MOUNT ATTACH POINT CORRODED ON FLOOR DOUBLER 170-012118-001 TOP SURFACE AT FRM-16, STR-16L INBD (Y-273.0) CORROSION DETERMINED OUT OF LIMITS. REMOVED AND REPLACED DOUBLER AT FWD LAV ATTACH MOUNT IAW EMB 190 SRM 51-40-02.
Part: SHEAR PANEL — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
AFT WET AREA - CORROSION AT CNTR "Y" SHEAR PANEL BETWEEN FR 87 AND FR 88 MULTIPLE LOCATIONS. REMOVED AND REPLACED SHEAR PANEL BETWEEN FR 87 AND FR 88 AT CNTR "Y" IAW EMB 190 SRM 51-40-08.
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
SEAT TRACK FR26 - FR27 STR-15L OUTBD CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EAM 190 SRM 51-40-08
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
FR-27 STR-15R OUTBD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EAM 190 SRM 51-40-02
Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
LH #1 DOOR CUT-OUT LOWER BEAM HAS CORROSION - MULTIPLE LOCATIONS. REMOVED AND REPLACED L1 DOOR LOWER BEAM IAW EMB 190 SRM 51-40-08
Part: FLOOR SPLICE — CORRODED (ZONE 100) · airframe 39,222 hrs · 19,640 cycles
AFT WET AREA - CORROSION AT SPLICE - FR 90 "Y". REMOVED AND REPLACED AFT WET AREA SPLICE AT FR 90 "Y" IAW E190 SRM 51-40-08.
Part: CROSSBEAM — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
AFT WET AREA - CORROSION AT CLIP RH CROSSBEAM TO INTERCOSTAL - FR90 "Y" -10. INSTALLED NEW AFT WET AREA GUSSET PLATE RH CROSSBEAM TO INTERCOSTAL - FR90 "Y" -10 IAW E190 SRM 51-40-08
Part: BEAM — CORRODED · corrosion level 2 · airframe 39,222 hrs · 19,640 cycles
AFT WET AREA - CORROSION AT SPLICE - FR87-FR88 "Y" +10". BLENDED CORROSION ON R/H BEAM FR87 - FR88 Y +10" IAW E-190 SRM 51-10-03. REMOVED AND REPLACED RH BEAM FR 87 THRU FR88 +10" IAW E190 SRM 51-40-08.
2021
Part: BLEED AIR SYS — FAILED (NR 2) · airframe 37,812 hrs · 18,648 cycles
BLEED 2 FAIL MESSAGE APPROACHING FL290. BLEED 1 DEFERRED. EMERGENCY DESCENT ACCOMPLISHED. CABIN ALT REMAINED BELOW 10,000FT. - PERFORMED ENGINE RUN ON #2 ENGINE DUE TO BLEED ISSUE OPERATED BLEED AND CYCLED WTH NO DEFECT - OPS CHECK PERFORMED PER AMM 36-11-06. SYSTEM OPS CHECK GOOD