- Registered owner
- United Airlines Inc
- Location
- Chicago, IL
- Owner type
- Corporation
- Serial number
- 17000830
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 5, 2019
- Certificate issued
- December 5, 2019
- Expires
- December 31, 2029
- Mode S code
- A8233A
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 N623UXMatched 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
No FAA accident or incident reports matched to N623UXMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Embraer S A ERJ 170-200 LL aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SWI2025F01716Flap Track · wornRIGHT WING FLAP TRACK 2A OTBD HAS WIDTH REDUCTION WEAR OF 1.16MM MAX ALONG ENTIRE LENGTH. REMOVED AND REPLACED RT WING FLAP TRACK 2A OTBD IAW AMM 57-54-25.SDR SWI2025F01715Flap Track · wornLEFT WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF .98MM MAX ALONG FWD SIDE. REMOVED AND REPLACED THE LT WING FLAP TRACK 1A IAW AMM 57-54-25.SDR SWI2025F01714Seat Track · corrodedAFT WET AREA CORROSION AT AFT END OF LT INBD SEAT TRACK FRS 84 - 85. REPAIRED THE LT INBD SEAT TRACK BETWEEN FR 83-85 IAW SRM 53-00-10, REPAIR 01, AND ETD2022-170-022163, REV C.SDR SWI2025F01713Floor Support · corrodedAFT WET AREA CORROSION ON LT FLOOR SUPPORT ON RIVETS AROUND FR 87. REMOVED AND REPLACED BETWEEN FR 86-89 IAW SRM 51-40-08. REPLACED WITH FACTORY PART.SDR SWI2025F01712Seat Track · corrodedAFT WET AREA CORROSION AT AFT END OF RT INBD SEAT TRACK, FRAME 84 - 85. PERFORMED REPAIR ON THE RT INBD SEAT TRACK IAW ETD2022-170-022163, REV C, & SRM 53-23-10AD01.SDR SWIA2025120300115Floor Support · corrodedAFT WET AREA CORROSION ON RT FLOOR SUPPORT AT FR 87. REMOVED AND REPLACED THE FLOOR SUPPORT FR 86-89 WITH NEW IAW SRM 51-40-08. REPLACED WITH OEM PART,SDR SWIA2025120300114Seat Track · corrodedFORWARD CABIN FLOOR STRUCTURE TRACK, LT UPPER SURFACE HAS CORROSION BETWEEN FR 19 AND 20. REPAIRED FORWARD CABIN FLOOR STRUCTURE TRACK, LT UPPER SURFACE IAW ETD2025-170-932399.SDR SWIA2025120300113Doubler · corrodedWASTE SERVICE PANEL CUTOUT FLANGE HAS CORROSION ON FWD SIDE. REMOVED AND REPLACED WASTE SERVICE BOX DOUBLER IAW SRM 51-40-08. REPLACED WITH FACTORY PART.SDR SWIA2025061200010Hydraulic System · warning messageDIVERTED TO KPDX FOR A TOTAL LOSS OF SYSTEM 1 HYDRAULIC QUANTITY. €ŒHYD 1 LO QTY€? EICAS APPEARED. SYSTEM 1 PSI REMAINED AROUND 3,000 PSI WITH THE ASSSUMED HELP OF THE HYD SYSTEM 2. (FLIGHT 5217 - FILED CLOSED) PLEASE REFERENCE AML 1625121. PERFORMED GVI OFSDR SWIA202310200001Unknown · dentedCOMPLY WITH ETD 2023-170-026423 FOR THE PERMANENT REPAIR (PARA. B. 1.) OF THE DENT FOUND ON THE AFT EDGE (FR 27) OF THE FWD CARGO DOOR BETWEEN APROX STRG 21R AND 23R WITHIN 10 FC. DUE BY TAC: 4755. DENT MEASURES DEPTH = 0.40 IN, L= 1.5 IN, W=0.25 IN. PER EMSDR SWIA202309100029Unknown · separatedFWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FLEX- BALL CABLE SLEEVE SEPERATED FROM UPPER FITTING AND INNER CABLE IS EXPOSED. (C-CHECK RO 10/6/2023) REPAIRED FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FLEX- BALL CABLE SLEEVE AT UPPER FITTING REF EMB
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