N575RP2004 Embraer EMB-145LR
This N-number isn't registered right now. Below is its last known registration, canceled Nov 7, 2018.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply21 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Wells Fargo Trust Co NA Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Jan 12, 2017
- Canceled
- Nov 7, 2018
- Airworthiness
- Standard · Transport
- Airworthiness date
- Sep 17, 2004
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-145LR
- Year
- 2004
- Serial number
- 14500847
- 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
- A76281
Engine
- Make and model
- Rolls-Royc Ae 3007a1p
- Type
- Turbo-fan
- Power
- 8,338 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- 2017 – 2018Wells Fargo Trust Co NA TrusteeSalt Lake City, UT
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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-145LR) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145LR) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145LR) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-145LR)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-145LR)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-145LR)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 (21)
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 · light · inoperativeApr 15, 2015
DURING INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS REPLACED. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · controller · failedApr 3, 2015
THE CREW REPORTED THAT WHILE THE AUTO PRESSURIZATION SYSTEM WAS DEFERRED, THE MANUAL PRESSURIZATION SYSTEM WOULD NOT PRESSURIZE THE CABIN. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE LOCKED OPEN BOTH OUTFLOW VALVES AND THE DEFERRAL WAS RECLASSIFIED. THE DEFERRAL WAS CLEARED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine air · bleed valve · failedJan 24, 2015
THE CREW REPORTED THAT THEY RECEIVED A NR 1 BLEED VALVE FAIL MESSAGE AND A STAB ANIT-ICE VALVE FAIL MESSAGE DURING CLIMB OUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE BLEED VALVE. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · floor support · corrodedJul 1, 2014
DURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 & FRAME 59. THE BEAM WAS REPAIRED IAW ETD 2014-145-055505.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedJul 1, 2014
DURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 BETWEEN FRAME 19 & 23. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · repair · dentedJun 29, 2014
DURING INSPECTION, A PREVIOUS REPAIR ON THE CARGO DOOR WAS FOUND TO BE DENTED AT THE LOWER AFT EDGE. THE DENT WAS REPAIRED IAW ETD 2014-145-055666.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · fitting · crackedJun 29, 2014
DURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR CLIP ON THE APU FIREWALL AT STRINGER 10L & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL CLIP AT FRAME 80 & STRINGER 10L WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · crackedJun 29, 2014
DURING INSPECTION, AFT FUSELAGE INSIDE ACCESS PANEL 312AR ANGLE ON THE APU FIREWALL AT STRINGER 10R & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL ANGLE WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · fitting · crackedJun 29, 2014
DURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR FRAME 80 SHEAR CLIP WAS FOUND CRACKED AT STRINGER 1L. THE SHEAR CLIP WAS REPLACED IAW WITH SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · fitting · crackedJun 28, 2014
DURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & STRINGER 15R WAS FOUND CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 21 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026