N568RP2004 Embraer EMB-145LR
This N-number isn't registered right now. Below is its last known registration, canceled May 15, 2018.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply44 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Tvpx Aircraft Solutions INC Trustee
- Owner type
- Corporation
- City, state
- North Salt Lake, UT
- Certificate issued
- May 10, 2018
- Canceled
- May 15, 2018
- Airworthiness
- Standard · Transport
- Airworthiness date
- May 15, 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
- 145800
- 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
- A74627
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- 2018Tvpx Aircraft Solutions INC TrusteeNorth Salt Lake, UT
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (44)
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 · inoperativeAug 12, 2015
MAINTENANCE WAS CALLED TO SHUTOFF THE EMERGENCY LIGHTS THAT WERE FOUND TO BE ON. MAINTENANCE WAS UNABLE TO ENERGIZE THE COCKPIT TO TURN OFF THE LIGHTS SO THEN REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES AND BOTH MAIN BATTERIES IAW THE AMM AND NO FURTHER DEFECTS HAVE BEEN NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · control lever · inoperativeFeb 22, 2015
THE CREW REPORTED THAT THEY RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE WHILE TRYING TO RETRACT THE LANDING GEAR. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS AND GEAR SWINGS WERE GOOD WITH NO FURTHER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · ballast · defectiveOct 22, 2014
ELECTRICAL BURNING ODOR WAS PRESENT IN THE CABIN IN FLIGHT. THE LIGHTING BALLAST AT SEAT 1A WAS FOUND TO BE CAUSING THE ODOR & WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 10/26/2014 WHEN MX REPLACED THE LIGHTING BALLAST. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · battery · dischargedMay 1, 2014
DURING INSPECTION, THE LIGHTS CONNECTED TO THE NR 1 EMERGENCY LIGHT BATTERY WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery · dischargedJan 6, 2014
DURING INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 2 BATTERY & ALL OPERATIONS CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · attach angle · crackedOct 28, 2013
DURING INSPECTION, THE LT OMEGA BEAM ATTACH FLANGE TO RIB 3 WAS FOUND TO BE CRACKED AT FRAME 47 AND 48. THE ATTACH FLANGE AT FRAME 47 AND 48 WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · attach angle · crackedOct 28, 2013
DURING INSPECTION, THE LT OMEGA BEAM ATTACH FLANGE TO RIB 3 WAS FOUND TO BE CRACKED AT FRAME 47 AND 48. THE ATTACH FLANGE AT FRAME 47 AND 48 WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedOct 28, 2013
DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 20.THE BEAM WAS REPAIRED IAW ETD 2013-145-05335.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedOct 25, 2013
DURING INSPECTION, CORROSION WAS FOUND ON THE SKIN SPLICE AT FRAMES 60 BETWEEN STRINGERS 20 - 21R. THE SPLICE WAS REPAIRED IAW ETD 2013-145-052936.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · structure · corrodedOct 25, 2013
DURING INSPECTION, CORROSION WAS FOUND AROUND THE LAVATORY DUMP CHUTE ON THE EXTERNAL SIDE. THE LAVATORY DUMP CHUTE CUP AND ZEE PROFILE WERE REPLACED IAW SRM 51-20-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 44 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026