- Registered owner
- Delux Public Charter LLC
- Location
- Dallas, TX
- Owner type
- LLC
- Serial number
- 145763
- Year built
- 2003
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 14, 2003
- Certificate issued
- August 1, 2019
- Expires
- August 31, 2029
- Mode S code
- A24ADE
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 104
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1998 | 5 |
|---|---|
| 1999 | 5 |
| 2000 | 10 |
| 2001 | 7 |
| 2002 | 3 |
| 2003 | 6 |
| 2004 | 12 |
| 2005 | 16 |
| 2006 | 10 |
| 2007 | 4 |
| 2008 | 8 |
| 2009 | 3 |
| 2010 | 8 |
| 2011 | 3 |
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 2 |
| 2017 | 3 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 1 |
| 2021 | 2 |
| 2023 | 1 |
| 2025 | 2 |
| 2026 | 1 |
Airframe · Embraer EMB-145LR
AD 2026-13-02NavigationAD 2025-08-07Flight ControlsAD 2024-26-07FuselageInformation bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Embraer EMB-145LR
SAIB AIR-21-15R1Navigation SystemSAIB AIR-20-17Air Conditioning - Cabin Pressure Control SystemSAIB NM-19-17Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT RelaysSAIB NM-10-13Navigation: Flight Management SystemSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsSAIB NM-08-15Instruments: Contamination of the Attitude Heading Reference System (AHRS) ComputersSAIB NM-07-40Embraer EMB-135/145 Landing Gear IncidentSAIB NM-07-20Flight Data RecordersHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N247JXMatched 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 EMB-145LR aircraft
FAA incident reports
No FAA accident or incident reports matched to N247JXMatched 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 EMB-145LR aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 4DPA2024102700001Strut · underservicedCREW REPORTED- AFTER ROTATION WE RECEIVED LDG AIR/GND FAIL EICAS. FO TRIED TO RAISE THE LANDING GEAR LEVER AND IT WOULD NOT BUDGE. THE GEAR REMAINED DOWN FOR THE DURATION OF THE RETURN. WE EXECUTED THE QRH FOR THE ASSOCIATED MESSAGE. CORR ACTION- MX TROUBLESHOSDR 4DPA2024071900001Pin · installedCREW REPORTED ON CLIMB OUT OUR LANDING GEAR INDICATED NORMALLY BUT THERE WAS A LOUD SOUND IN THE COCKPIT WHICH I SUSPECTED WAS THE NOSE GEAR DOOR BEING OPEN. UPON LANDING IN HOUSTON I CALLED MISSION CONTROL AND MAINTENANCE CONTROL AND HAD 2 MECHANICS IN HOUSTOSDR 4DPA2023072400001Duct · leakingISSUE; CREW REPORTED BLEED 1 OVER TEMP WARNING MESSAGE. BLEED 1 TEMP IN RED. RAN QRH AND RETURNED TO KLAS. CORR ACTION; MX FOUND PRE COOLER DUCT UNSERVICEABLE ON THE AIRCRAFT. REMOVED AND REPLACED THE PRE COOLER DUCT. OPS AND LK GOOD.SDR 4DPA2023071600001Unknown · unknownISSUE-BLEED 1 OVER TEMP WARNING MESSAGE. BLEED 1 TEMP IN RED. RAN QRH AND RETURNED TO KLAS. CORR ACTION NOT YET COMPLETED CURRENTLY STILL MEL'D EXPIRES 7/26.SDR 4DPA2023020600001Clamp · failedISSUE-CREW REPORTED ON CLIMB OUT AT FL180, PERFORMED ICE DETECTION TEST WITH NORMAL PARAMETERS. TESTED OK, WENT BACK TO ICE DETECTION AUTO. ENG 1 A/ICE FAIL EICAS DISPLAYED. ENG 1 ICE VALVE STAYED OPEN. RAN QRH AND MESSAGE PERSISTED. A/ICE FAIL MESSAGE ANSDR V0XD20220318003Antenna · corrodedRADIO ALTIMITER MOUNTING BASE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED RADIO ALTIMITER MOUTING BASE IAW EMB145 SRM 51-40-02. ALL WORK PERFORMED ON AVMAX W/O: 80992 W/C: 1035.SDR V0XD20220318002Skin · corrodedFUSELAGE SKIN AT AFT RADIO ALTIMITER FAYING SURFACE IS CORRODED. CORRECTIVE ACTION: REMOVED CORROSION ON FUSELAGE SKIN AT AFT RADIO ALTIMITER FAYING SURFACE BY BLENDING. NOMINAL SKIN THICKNESS IS .063. SKIN THICKNESS AFTER REPAIR IS .058, FOUND TO BE WITHIN LISDR V0XD20220318001Linkage · crackedR/H PYLON, LOWER FWD YOKE PIVOT FITTING(LINKAGE PN: 145-29426-001) IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED THE R/H PYLON, LOWER FWD PIVOT FITTING(LINKAGE) IAW EMB 145 AMM 54-51-01-000-801-A ,EMB14554-51-01-400-801-A AND EMBRAER ETD2022-145-008534 SDR V0XD20220310001Bracket · corrodedSIGNS OF CORRSION ON BRACKETS UNDER THE PASSENGER DOOR ON FUSELAGE. CORRECTIVE ACTION: FABRICATED NEW BRACKET UNDER THE PASSENGER DOOR AND INSTALLED REPAIR PART IAW EMB145 SRM 51-30-01. REFER TO AVMAX W/O 80992 W/C 1030 FOR ALL WORK PERFORMED.SDR 4DPA2021101100001None · noneISSUE-LG DISAGREE AFTER TAKEOFF; CREW TRIED CYCLING GEAR SEVERAL TIMES, FOLLOWED QRH WITH NO FIX. AFTER TAKEOFF RH MLG INDICATION DASHED OUT AND LG DISAGREE ILLUMINATED. FIX-R&R'D RH MLG UPLOCK BOX ASSY. COMPLETED JACK AND RETRACT PROCEDURE OPS TESTED GOOD. NSDR 4DPA2021073000001Unknown · abnormalAT 4000 FEET OF THE AIRCRAFT BEGAN YAWING TO THE RIGHT REQUIRING LEFT RUDDER. ATTEMPTED YAW TRIM AND FOUND YAW TRIM INOP. APPLIED FULL LEFT RUDDER. FOLLOWED QRH OAKS BROUGHT PLANE BACK. WHEN BACK ON GROUND TRIED YAW TRIM AGAIN AND SEEMED TO WORK FINE. PERFORSDR 4DPA2021051700001O-Ring · deterioratedBLEED 2 FAIL ON CLIMBOUT PASSING 7000FT. R&R'D O-RINGS @ GAMMA CLAMPS #9, #15, #16 & #17 LEAK AND OPS TEST GOODSDR 4DPA2021040700001Seal · deteriorated"BLD 2 LEAK" WARNING MESSAGE ON EICAS, RED "LEAK" LIGHT ON BLEED 2 AIR CONDITIONING/PNEUMATIC PANEL IN FLIGHT AT 16000FT. "BLEED 1 LEAK" ON GROUND AFTER ENG SHUTDOWN WHILE ON APU BLEED.
STCs that may be installed · 75
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Embraer EMB-145LR
STC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST02176AT-DInstallation of a Teledyne Mini Flight Data Acquistion UnitSTC ST02216AT-DInstallation of Teledyne Mini Flight Data Acquisition Unit in a Provisioned EMB-135/145.