N261412003 Embraer EMB-145XR
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply26 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- United Airlines INC
- Owner type
- Corporation
- City, state
- Chicago, IL
- Certificate issued
- Dec 10, 2019
- Expires
- Dec 31, 2029
- Airworthiness
- Standard · Transport
- Airworthiness date
- Feb 25, 2005
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Embraer
- Model
- EMB-145XR
- Year
- 2003
- Serial number
- 145733
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 55
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A285B2
Engine
- Make and model
- Rolls-Royc Ae3007 Ser
- Type
- Turbo-fan
- Power
- 6,442 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2019 – nowUnited Airlines INCChicago, IL · current
- 1959 – 1975Curtis Sky RanchFort Worth, TX · different airframe: 1943 Piper J3c-65 S/N 4099
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (6)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-08-07 | Flight Controls | Jun 26, 2025 | Airframe (EMB-145XR) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145XR) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145XR) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-145XR)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002 |
| 2002-14-23 | Empresa Brasileira de Aeronautica S.A. | Aug 2, 2002 | Airframe (EMB-145XR)Serial numbers per EMBRAER Service Bulletin 145-27-0088, dated February 1, 2002. Only with: Equipped with horizontal stabilizer actuator (HSA) assemblies having part numbers and serial numbers listed in EMBRAER Service Bulletin 145-27-0088. |
Show all 6 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2000-09-09 | EMBRAER Model EMB-145 Series Airplanes | Jun 16, 2000 | Airframe (EMB-145XR)Certain serial numbers: EMB-145 145004–145047; EMB-145 145049–145051. Only with: Equipped with IC-600 #1 P/N 7017000-82402; excluding airplanes modified per EMBRAER SB 145-22-0001, SB 145-22-0004 Rev 01, or SB 145-31-0007 Rev 02. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (26)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Lights · battery pack · dischargedAug 18, 2013
DURING MX INSPECTION, THE 2 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · shuttle valve · leakingJun 14, 2012
THE CREW REPORTED HYD SYS NR 1 DROPPED INTO AMBER RANGE IN FLIGHT AND RECEIVED A WARNING MESSAGE ON THE EICAS. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 AND NR 4 BRAKE SHUTTLE VALVES. SERVICED HYD SYS AND OPS CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · beam · corrodedDec 10, 2011
DURING C-CHECK, REMOVED CARGO DOOR LOWER BEAM BETWEEN FRAMES 65-68 TO FOM. MX R & R CARGO DOOR LOWER BEAM BETWEEN FRAMES 65-68 IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · skin · dentedDec 10, 2011
DURING C-CHECK (FRAME 22/STRINGER 18L) DENT/PROTRUSION IN FUSELAGE. MX PERFORMED REPAIR WITH INSTALLED FABRICATED DOUBLER BETWEEN FRAME 22 AND 23 STRINGER 17L AND 18L IAW SRM 53-21-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · sill · corrodedDec 10, 2011
DURING C-CHECK CENTER SERVICE DOOR SILL CORRODED. MX R & R CENTER SERVICE DOOR SILL IAW SRM 51-90-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedNov 26, 2011
DURING C-CHECK SKIN SPLICE BETWEEN (FRAME 13 AND 14 STRINGER 21L-20R) HAS CORROSION. MX PERFORMED REPAIR ON SKIN SPLICE AT FRAME 13-14, STRINGER 20L-20R IAW SRM 53-00-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ice and rain protection · sensor · faultyJul 11, 2011
ORD FLT 5814 THE CREW REPORTED A PITOT HEAT 3 FAIL MESSAGE ALONG WITH A ELECTRIC SMELL. MAINTENANCE REPLACED THE NR 3 PITOT CURRENT SENSOR. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Pneumatic · o-ring · leakingMay 20, 2011
IAH - FLIGHT 3136, DURING CLIMB THE CREW REPORTED A BLEED TWO LEAK INDICATION. THE AIRCRAFT RETURNED TO IAH WHERE OT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE O-RINGS AT JOINT 24, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Pneumatic · o-ring · failedMay 18, 2011
FLIGHT 2049, THE CREW REPORTED A BLEED LEAK INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO GDL WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BLEED O-RINGS AT JOINTS 10,18, & 20 OF THE NUMBER TWO SYSTEM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedMar 27, 2010
SHV - DURING C-CHECK SEVERAL EXTERNAL SKIN CRACKED AROUND RIVET HEADS AT FRAME 78 BETWEEN STR'S 1R-7R. MAINTENANCE PERFORMED REPAIR OF SEVERAL EXTERNAL SKIN CRACKS AROUND RIVET HEADS AT FRAME 78 BETWEEN STR'S 1R-7R IAW EC5330-02091. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 26 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026