- Registered owner
- United Airlines Inc
- Location
- Chicago, IL
- Owner type
- Corporation
- Serial number
- 17000798
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 24, 2019
- Certificate issued
- May 23, 2019
- Expires
- May 31, 2029
- Mode S code
- A7D7F3
Embraer S A ERJ 170-200 LLTCDS A56NMAirframe · Embraer S A ERJ 170-200 LLTCDS E00063ENEngine · GE CF34-8E5
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 30
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2004 | 1 |
|---|---|
| 2005 | 1 |
| 2008 | 2 |
| 2009 | 1 |
| 2013 | 1 |
| 2017 | 2 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 4 |
| 2021 | 3 |
| 2022 | 6 |
| 2023 | 5 |
| 2024 | 2 |
| 2025 | 3 |
| 2026 | 2 |
Airframe · Embraer S A ERJ 170-200 LL
AD 2026-13-02NavigationAD 2025-14-05Nacelles/PylonsAD 2025-01-05Time Limits/Maintenance ChecksInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Embraer S A ERJ 170-200 LL
SAIB NM-20-12Powerplant System - Operating in Icing ConditionsNTSB investigations
No NTSB investigations matched to N604UXMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Embraer S A ERJ 170-200 LL aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SWIA2026052776651Skin · dentedDURING JACKING PROCEDURES, TAIL JACK STAND SLIPPED OFF JACK PAD AND CAUSED A DENT RIGHT OF THE TAIL JACK PORT. REPAIRED DAMAGE ON REAR FUSELAGE CLOSE TO JACKING POINT IN BETWEEN STRINGERS 28R AND 29L, IAW ETD 2026-170-009310, REV.: A DISPOSTION 001- REAR FUSELSDR SWIA2025072301Bracket · bentAFTER TAKEOFF GROUND SPOILER FAIL EICAS MESSAGE RECEIVED. RAN QRH, VIEWED STATUS PAGE, & DETERMINED THAT A SPOILER ON LT WING POSSIBLY STUCK UP, AS INDICATED BY STATUS PAGE. NOTED MORE RT AILERON REQUIRED ON TAKEOFF THAN NORMAL FOR RT CROSSWIND. (FLIGHT 58SDR SWIA2025072200001Warning Message · illuminatedAFTER TAKEOFF GROUND SPOILER FAIL EICAS MESSAGE RECEIVED. WE RAN THE QRH, VIEWED THE STATUS PAGE, AND DETERMINED THAT A SPOILER ON THE LEFT WING WAS POSSIBLY STUCK UP, AS INDICATED BY THE STATUS PAGE. WE ALSO NOTED THAT MORE RIGHT AILERON WAS REQUIRED ON TAKEOSDR SWIA2025071400011Valve · brokenLG WOW SYS FAIL EICAS MESSAGE (FLIGHT 5408 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30470009 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT WITH FAULT CODE 32611306PSS FIM 32-61-00, DURING INITIAL EVALUATION FOUND IF 32611306PSS NLG WOSDR SWIA2025043013Doubler · damagedAFT FUSELAGE ACCESS DOOR OPENING DOUBLER DAMAGED BY AFT LOWER STRIKER PLATE (C-CHECK RO 04/29/2025)PERFORMED CUTOUT DOUBLER REPAIR OF AFT FUSELAGE ACCESS DOOR OPENING CUTOUT AT AFT LOWER STRIKER PLATE, REF ETD2025-170-906061. REPAIR PARTS WEIGHED LESS THAN 2SDR SWI2025F00611Seat Track · corrodedRH FLOOR BEAM SEAT TRACK CORRODED AS MARKED FR79-81. (C-CHECK RO 04/29/2025)REMOVED AND REPLACED RH FLOOR BEAM SEAT TRACK AS MARKED FR73-84. REF: EMB SRM 51-40-08, SEE CONTINUATION CARD FOR WORK ACOMPLISHED. NO CHANGE TO WEIGHT AND BALANCE - OEM PARTS CHANGE.SDR SWIA2025043011Seat Track · corrodedLH FLOOR BEAM SEAT TRACK CORRODED AS MARKED FR79-83. (C-CHECK RO 04/29/2025)REMOVED AND REPLACED L/H FLOOR BEAM FR73-84. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. NO CHANGE TO WEIGHT AND BALANCE - OEM PARTS CHANGE.NO CHANGES TO AIRCRFSDR SWI2025F00610Floorbeam · corrodedRH FLOOR BEAM HAS CORROSION AROUND FASTENER AT FR87. (C-CHECK RO 04/29/2025)REMOVED AND REPLACED RH FLOOR BEAM AT FR87. REF: EMB SRM 51-40-08. (SEE CONTINUATION CARD FOR WORK ACCOMPLISHED)SDR SWIA202508060410Spring · brokenFORWARD-SERVICE-DOOR EVACUATION SLIDE AFT FITTING SPRING BROKE. (C-CHECK RO 04/29/2025)REMOVED AND REPLACED SPRING IN FWD SERVICE DOOR EVACUATION SLIDE AFT FLOOR FITTING. REF EMB 175 AMM 53-10-25.SDR SWIA2025043009Skin · damagedLIGHTNING STRIKE DAMAGE UPPER FUSELAGE ON SKIN BETWEEN FRAMES 49-50 AND STRINGERS 1R-2R. (C-CHECK RO 04/29/2025)REPAIRED LIGHTNING STRIKE BY INSTALLIING FABRICATED DOUBLER TO CFII, EXTERNAL SKIN BETWEEN FRAMES 49-50 AND STRINGERS 1R-2R AS MARKED. SEE CONTINUASDR SWIA202266346None · damagedR/H I/B FLAP TRACK 1A HAS THICKNESS REDUCTION OF .029". THIS IS OUT OF THE LIMITS OF SRM 57-52-03/AD01. ASSET TC2-7153 DUE 11-18-22. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED RH INBOARD FLAP AFT TRACK 1A. REF AMM 57-54-25. TQ 7402 CAL 5-10-23. FLAP OP
STCs that may be installed · 20
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 20 STCs