N446YX
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.
23 reports on file, 2016-10-14 – 2024-07-13.
Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED 1) · airframe 22,248 hrs · 15,244 cycles
BLEED 1 FAIL EICAS BLEED 1 OVERPRESSURE EICAS MSG CLEARED AFTER RUNNING QRH. EMERGENCY NOT DECLARED. PERFORMED OPERATIONAL TEST OF ENG 1 BLEED SYSTEM IN REF WITH ERJ 175 AMM 36-11-00. NO BLEED 1 FAIL EICAS MESSAGES NOTED. BLEED 1 SYSTEM OPS CHECK GOOD AT THIS TIME.
Earlier reports · 2016–2022 · 22 reports
2022
Part: DOUBLER — DAMAGED · airframe 18,070 hrs · 12,221 cycles
LIGHTING STRIKE DAMAGE BETWEEN FR 02 AND FRA 03 AND STR 26R AND 27R.INSTALLED DOUBLER IAW EMB SRM 53-10-01 REPAIR 12P.
2020
Part: GLOWSTRIP — WORN (CABIN) · airframe 14,163 hrs · 9,561 cycles
PHOTOLUMINESCENT STRIPS WORN IN FWD CABIN. R&R PHOTOLUMINESCENT STRIPS.
2019
Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 12,295 hrs · 8,339 cycles
RT FIRST CLASS SECTION OF PHOTOLUMINESCENT STRIP INOP. R&R PHOTOLUMINESCENT STRIP IAW AMM 33-50-21. OPS CHECK GOOD.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK, CABIN CEILING EMERGENCY LIGHT NOT WORKING (3RD PANEL BACK FROM FRONT OF A/C). REMOVED AND REPLACED NO. 3 EMERGENCY LIGHTING POWER UNIT. REF AMM: 33-50-01. SEE EAMS W/O H6756 SN 535 FOR WORK DETAILS
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY MAINT CHECK VISIT FOUND CORROSION ON AFT WET AREA RH GUSSET PLATE FR90. REMOVED AND REPLACED GUSSET AFT WET AREA FR90 REF. SRM 51-40-08. RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-05. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION
Part: SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK VISIT FOUND CORROSION-FWD WET AREA LH MONUMENT SUPPORT FR16. REMOVED AND REPLACED MONUMENT SUPPORT PN170-13633-001 FR16 REF SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: FLOOR SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK VISIT FOUND CORROSION ON AFT WET AREA FLOOR SPLICE AT FR90 Y= -10.748. REMOVED AND REPLACED AFT WET AREA FLOOR SPLICE AT FR90 Y= -10.748" REF. EMB SRM 51-40-08.RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-05, 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION
Part: HINGE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK VISIT FOUND AFT LAV WASTE DOOR HINGE AND BONDING WIRE AREA IS CORRODED. REMOVED AND REPLACED AFT LAV WASTE DOOR HINGE, RESTORED PROTECTIVE FINISH REF EMB SRM 51-40-08 AND 51-23-00 ALSO REMOVED AND REPLACED BONDING WIRE OHM CHECK GOOD REF E175 AMM 20-10-01 AND 20-13-21. TW 7216 DUE 05-01-19 AND MILLIOHM METER 736 08-15-19. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK VISIT FOUND CORROSION ON AFT WET AREA FLOOR SPLICE AT FR90 Y= +10.748. REMOVED AND REPLACED AFT WET AREA FLOOR SPLICE AT FR90 Y= +10.748. RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-05, 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: FLOOR SUPPORT — CORRODED (FRAMES 90-91) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK VISIT FOUND CORROSION ON AFT WET AREA INTERCOSTAL BETWEEN FR90 AND FR91. REMOVED AND REPLACED INTERCOSTAL AT AFT WET AREA FR90-91 REF. SRM 51-40-08. RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: FLOOR SUPPORT — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK VISIT FOUND CORROSION ON AFT WET AREA INTERCOSTAL BETWEEN FR89 AND FR90. REMOVED AND REPLACED INTERCOSTAL AT AFT WET AREA FR89-90 REF. SRM 51-40-08. RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: FLOOR SPLICE — CORRODED (FRAME 89) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK VISIT FOUND CORROSION ON AFT WET AREA FLOOR SPLICE AT FR89 Y=+10.748. REMOVED AND REPLACED SPLICE AT AFT WET AREA FR89 REF. SRM 51-40-08.RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY CHECK FOUND CORROSION ON AFT WET AREA MIDDLE SHEAR PANEL BETWEEN FR87 AND FR88. REMOVED AND REPLACED MIDDLE SHEAR PANEL FR87-88 REF. EMB SRM 51-40-08.RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-05, 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY MAINT CHECK FOUND CORROSION ON AFT WET AREA RH SHEAR PANEL BETWEEN FR87 AND FR88. REMOVED AND REPLACED RH SHEAR PANEL FR87-88 REF. EMB SRM 51-40-08.RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-05, 51-23-06.ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: SUPPORT — CORRODED (FRAMES 88-91) · corrosion level 2 · airframe 11,162 hrs · 7,546 cycles
DURING HEAVY MAINT CHECK FOUND CORROSION ON AFT WET AREA RH PANEL SUPPORT BETWEEN FR88 AND FR91. REMOVED AND REPLACED PANEL SUPPORT AFT WET AREA FR88-91 REF. SRM 51-40-08. RESTORED SURFACE PROTECTION REF. EMB SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.
Part: FRAME — DAMAGED (LT WINGLET) · airframe 11,162 hrs · 7,546 cycles
REMOVED LH WINGTIP PER REF E175 AMM57-30-00. REMOVED AND REPLACED FRAME 1 ON LH WINGLET PER EAMS W/O: C116051. REINSTALLED WING TIP PER REF E175 AMM 57-30-00. SEE EAMS W/O H6756 SN 124 FOR WORK DETAILS AIRCRAFT REMAINS IN HEAVY CHECK BNA
Part: FRAME — CRACKED (RT WINGLET) · airframe 11,162 hrs · 7,546 cycles
REMOVED RH WINGTIP PER REF E175 AMM 57-30-00. REMOVED AND REPLACED FRAME 1 ON RH WINGLET PER EAMS W/O: C116053. REINSTALLED WINGTIP PER REF E175 AMM 57-30-00. SEE EAMS W/O H6756 SN 125 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
2017
Part: SKIN — DENTED (FRAMES 10-11) · airframe 7,071 hrs · 4,901 cycles
DENT IN THE LT FWD FUSELAGE SKIN AT FRAMES 10L TO 11L, BETWEEN STRINGERS 18L TO 19L. INSTALLED TEMPORARY REPAIR IAW ETD2017-170-094874. MAJOR REPAIR.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,263 hrs · 3,758 cycles
L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R L2 DOOR EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. OPS CHECKED GOOD.
Part: LATCH — DIRTY (L1 DOOR LOCK) · airframe 5,223 hrs · 3,731 cycles
L1 WHEN FULL OPEN AND LOCKED, THE LOCKING MECHANISM LATCH HITS THE HOLDING PIN DIRECTLY, MAKING LOUD CLICK. OPERATES NORMALLY OTHER THAN THAT. INSPECTED AND OPERATED L! DOOR KEEPING MECHANISM. REMOVED DEBRIS AND KEEPING MECH OPERATES NORMALLY. NO LOUD CLICKS NOTED. OK FOR SERVICE PER AMM 52-11-00.
2016
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,302 hrs · 3,086 cycles
CREW REPORTED THAT THE EMERGENCY CEILING LIGHT IN FIRST CLASS WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 4,129 hrs · 2,980 cycles
CREW REPORTED THAT THE OVERHEAD EMERGENCY LIGHT AT ROW 3 WAS INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR IAW AMM AND OPS CHECKED GOOD.