# N18102: 2002 Embraer EMB-145XR, registration cancelled 2025-03-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 13, 2025
- Exported to: Bahamas
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-145XR](https://openairdocs.org/model/embraer-emb-145xr) (registry code 3260214)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145643
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2005
- Certificate issued: June 1, 2023
- Last registry action: June 30, 2023
- Mode S code: A146D6
- Owner when cancelled: [Enterprise Aircraft Finance LLC](https://openairdocs.org/faa-owner/ENTERPRISE%20AIRCRAFT%20FINANCE%20LLC)
- Location: [Clayton, MO](https://openairdocs.org/faa-place/MO/Clayton)
- Owner type: LLC
- Owner's area on the map: 38.6443° N, 90.3281° W: Placed by OpenAirDocs at the center of ZIP code 63105, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N18102
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=18102
- Page: https://openairdocs.org/deregistered/N18102-2025-03-13

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer EMB-145XR: https://openairdocs.org/model/embraer-emb-145xr.md

## Service difficulty reports (69, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR RAIA2019080631001](https://openairdocs.org/sdr/RAIA2019080631001), Jul 31, 2019: ANGLE. CORRODED. AFT CARGO DOOR CUTOUT FWD LATERAL "L" SHAPE ANGLE HAVE CORROSION AT FRAME 65 LOWER CORNER IN 3 PLACES. REMOVED AND REPLACED L ANGLE
- [SDR RAIA201905190001](https://openairdocs.org/sdr/RAIA201905190001), May 19, 2019: CONTROL SYSTEM. INOPERATIVE. E1 OPERATING 9% BELOW N1 RATING DURING CLIMBOUT. A/C IS STILL IN WORK. SUPPLIMENTAL INFORMATION FROM ORIGINAL ENTRY. R&R CONTROL STAND ASSEMBLY. OPS CHECK GOOD.
- [SDR RAIA2018082960001](https://openairdocs.org/sdr/RAIA2018082960001), Aug 26, 2018: FUEL CELL. LEAKING. LEFT WING HAD FLUID COMING FROM IT DURING FLT. FOUND FUEL TO BE LEAKING FROM BOTTOM OF LT WING 18 INCHES FWD OF THE JACK POINT FROM SKIN JOINT. CLASSIFIED AS RU
- [SDR RAIA201806050001](https://openairdocs.org/sdr/RAIA201806050001), Jun 5, 2018: FAN. MALFUNCTIONED. COCKPIT RECIR FAN INOP IN FLIGHT. R&R RECIRC FAN OPS TEST GOOD.
- [SDR RAIA201803160001](https://openairdocs.org/sdr/RAIA201803160001), Mar 16, 2018: HYDRAULIC SYSTEM. MALFUNCTIONED. IN FLIGHT, THE NR 1 HYDRALIC PUMP FAILED, CAUSING THE NR 1 HYDRAULIC SYSTEM TO FAIL. INSPECTED THE NR 1 HYDRALIC SYSTEM FLUID LEVEL, FOUND GOOD. GV INSPECTED BO
- [SDR RAIA201705120001](https://openairdocs.org/sdr/RAIA201705120001), May 12, 2017: BOLT. BROKEN. LG LEVER DISAGREE EICAS WARNING AFTER DEPARTURE WITH A RED HATCHED BOX OVER LEFT MAIN LANDING GEAR INDICATOR. REMOVED AND REPLACED BROKEN TOP BOLT OF LT SHOCK A
- [SDR RAIA201612210001](https://openairdocs.org/sdr/RAIA201612210001), Dec 21, 2016: BULB. INOPERATIVE. CEILING EMERGENCY LIGHT AT ROW 18 INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR RAIA201605170001](https://openairdocs.org/sdr/RAIA201605170001), May 17, 2016: RADAR. INOPERATIVE. RADAR WILL PAINT AN IMAGE ON THE RT SWEEP BUT ERASES EITHER SOME OR ALL OF THE IMAGE ON THE LT SWEEP. THIS OCCURED ON ALL RANGES AND ON BOTH MFD'S. R & R WEATHE
- [SDR RAIA201605070001](https://openairdocs.org/sdr/RAIA201605070001), May 7, 2016: CONTROL PANEL. INOPERATIVE. ALL EMERGENCY LIGHTS WILL NOT COME ON WITH SWITCH ON F/A'S CONTROL PANEL. R & R F/A CONTROL PANEL. OPS CHECK GOOD.
- [SDR RAIA201603220001](https://openairdocs.org/sdr/RAIA201603220001), Mar 22, 2016: ENGINE. LEAKING. ON TAKEOFF AT 100 KNOTS, STRONG SMOKE/BURNING ODOR WITH A LIGHT BLUE HAZE IN THE COCKPIT, ALSO NOTICED IN THE CABIN, EMERGENCY LANDING. MAINTENANCE REPLACED NR 
- [SDR RAIA201603170001](https://openairdocs.org/sdr/RAIA201603170001), Mar 17, 2016: LIGHT. INOPERATIVE. LARGE EMERGENCY EXIT LIGHT ON SIDEWALL PANEL AT ROW 18A IS INOPERATIVE. MAINTENANCE DISCONNECTED CONNECTORS, INSPECTED, RECONNECTED CONNECTORS, NO DEFECTS NOTED
- [SDR RAIA201602280001](https://openairdocs.org/sdr/RAIA201602280001), Feb 28, 2016: HYDRAULIC SYSTEM. UNKNOWN. STEADY LOSS OF HYDRAULIC FLUID IN FLIGHT. DID A FULL HYDRAULIC TEST AND LEAK CHECK OF NR 1 SYSTEM HYDRAULICS. NO DEFECTS FOUND AT THIS TIME. SERVICE HYDRAULIC F
- [SDR RAIA201507280002](https://openairdocs.org/sdr/RAIA201507280002), Jul 28, 2015: LIGHT. UNKNOWN. PAX DOOR SWING ARM EMERGENCY LIGHT IS INOPERATIVE. OPS CHECKED EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR ASOA20121117132](https://openairdocs.org/sdr/ASOA20121117132), Nov 18, 2012: FRAME. CRACKED. DURING C-CHECK, FRAME 10 CRACKED UNDER RT DV WINDOW CUTOUT. VERIFIED WITH EDDY CURRENT. MX R & R FRAME 10 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO 
- [SDR ASOA20121117131](https://openairdocs.org/sdr/ASOA20121117131), Nov 17, 2012: FRAME. CRACKED. DURING C-CHECK, FRAME 10 CRACKED UNDER LT DV WINDOW CUTOUT. VERIFIED WITH EDDY CURRENT. MX R & R FRAME 10 UNDER LT DV WINDOW IAW SRM 51-40-02. THE ACFT WAS APPR
- [SDR ASOA20121117130](https://openairdocs.org/sdr/ASOA20121117130), Nov 17, 2012: FRAME. BENT. DURING C-CHECK, FRAME 72 BENT AT STRINGER 15L-16L. MX R & R FRAME 72, BETWEEN 16L AND 13R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117129](https://openairdocs.org/sdr/ASOA20121117129), Nov 17, 2012: FRAME SPLICE. CRACKED. DURING C-CHECK, FRAME 72 SPLICE CRACKED AT STRINGER 15L-16L. MX R & R FRAME 72 SPLICE AT FRAME 72, STRINGER 15L AND 16L IAW SRM 51-40-02. THE ACFT WAS APPROVED 
- [SDR ASOA20121117128](https://openairdocs.org/sdr/ASOA20121117128), Nov 17, 2012: FRAME. CRACKED. DURING C-CHECK,K FRAME 72 CRACKED AT RIVET ON STRINGER 16L. MX R & R FRAME 72 BETWEEN STRINGER 16L AND 13R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20121117127](https://openairdocs.org/sdr/ASOA20121117127), Nov 17, 2012: FLOORBEAM. CORRODED. DURING C-CHECK CENTER FLOORBEAM AT FRAME 49 AREA HAS CORROSION . MX COMPLETED AND INSTALLED THE FABRICATED REPAIR DOUBLER AT CENTER FLOORBEAM AT FRAME 49 AREA I
- [SDR ASOA20121117126](https://openairdocs.org/sdr/ASOA20121117126), Nov 17, 2012: FLOORBEAM. CORRODED. DURING C-CHECK, LT FLOORBEAM AT FRAME 38 CROSSBEAM AREA HAS CORROSION. MX COMPLETED REPAIR ON LT FLOORBEAM AT FRAME 38 IAW SRM 53-00-10. DETERMINED TO BE A MINO
- [SDR ASOA20121117125](https://openairdocs.org/sdr/ASOA20121117125), Nov 17, 2012: FLOOR SUPPORT. CORRODED. DURING C-CHECK, LT OMEGA BEAM AT FRAME 59 CROSSBEAM AREA HAS CORROSION. MX COMPLETED INSTALL OF LT OMEGA BEAM REPAIR AT FRAME 59 CROSSBEAM AREA IAW EC5310-01466
- [SDR ASOA20121117124V](https://openairdocs.org/sdr/ASOA20121117124V), Nov 17, 2012: FLOOR SUPPORT. CORRODED. DURING C-CHECK , RT OMEGA BEAM AT FRAME 23 IS CORRODED AT NUTPLATE. MX FABRICATED AND INSTALLED REPAIR DOUBLER AT RT OMEGA BEAM AT FRAME 23 AT NUTPLATE IAW EC53
- [SDR ASOA201112140008](https://openairdocs.org/sdr/ASOA201112140008), Dec 14, 2011: CONTROL UNIT. FAILED. ADC 1 WENT OUT IN FLIGHT. R & R NR 1 COMMS UNIT IAW AMM 23-00-01. OPS CHECKED GOOD, ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11IA220](https://openairdocs.org/sdr/C2XA11IA220), Sep 17, 2011: APU. MALFUNCTIONED. IAH - FLIGHT 2373 THE CREW REPORTED THAT THE APU FAILED ON ROTATION OUT OF JAX WITH AN APU OIL LO PRESS MESSAGE AND A BURNING OIL ODOR. THE AIRCRAFT CONTINUED T
- [SDR C2XA11TY125](https://openairdocs.org/sdr/C2XA11TY125), Jul 25, 2011: CASE. FOD. TYS - A/C WAS FERRIED FRON BNA TO TYS FOR FOD DAMAGE WHERE MAINTENANCE REMOVED AND REPLACED THE FAN CASE (PN-145-75001-409-SN-NC1476); MULTIBLE BYPASS VANES (PN
- [SDR C2XA11RI085](https://openairdocs.org/sdr/C2XA11RI085), May 23, 2011: CONTROLLER. DEFECTIVE. FLIGHT 2398 - EWR - FLIGHT CREW REPORTED PRESSURIZATION DIFFERENTIAL READS ABOUT 1-2 PSI LOWER THAN IT SHOULD AT ALL ALTITUDES - FL350- 5.9 PSI. EWR MX REMOVED 
- [SDR C2XA11RI084](https://openairdocs.org/sdr/C2XA11RI084), May 23, 2011: CONTROLLER. DEFECTIVE. FLIGHT 2398 - EWR - FLIGHT CREW REPORTED PRESSURIZATION DIFFERENTIAL READS ABOUT 1-2 PSI LOWER THAN IT SHOULD AT ALL ALTITUDES - FL350- 5.9 PSI. EWR MX REMOVED 
- [SDR C2XA11SH046](https://openairdocs.org/sdr/C2XA11SH046), Feb 21, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 20. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH045](https://openairdocs.org/sdr/C2XA11SH045), Feb 21, 2011: SKIN. CRACKED. SHV - DURING C-CHECK FUSELAGE SKIN IS CRACKED AROUND RIVETS AT FR 80. REPAIRED SKIN IAW EC5330-02364. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10RI153](https://openairdocs.org/sdr/C2XA10RI153), Dec 2, 2010: CONTROLLER. INOPERATIVE. FLIGHT 2451 - STL - FLIGHT CREW REPORTED AUTO PRESS INOP IN FLIGHT AND DECLARED EMERGENCY DESCENT INTO STL. IAH MX REMOVED AND REPLACED AUTO PRESS CONTROLLER AN
- [SDR C2XA09TY200](https://openairdocs.org/sdr/C2XA09TY200), Jul 30, 2009: SILL. CORRODED. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND CORROSION ON THE RIGHT FLOOR SILLS FROM FRAME 29 THRU FRAME 48 OUT OF MFG LIMITS. MAINTENANCE REMOVED AND R
- [SDR C2XA09TY198](https://openairdocs.org/sdr/C2XA09TY198), Jul 30, 2009: SILL. CORRODED. TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LEFT FLOOR SILLS FROM FRAME 19A TO FRAME 36 CORRODED BEYOND MFG'S LIMITS. MAINTENANCE REMOVED 
- [SDR C2XA09TY205](https://openairdocs.org/sdr/C2XA09TY205), Jul 29, 2009: FLOOR SUPPORT. CORRODED. LT OMEGA BEAM TOP CAP IN LAV BETWEEN FRM 59-62 IS CORRODED AROUND RIVETS AND NUT PLATES. BLENDED OUT CORROSION AND IS WITHIN LIMITS, ALODINED, PRIMED AND PAINTE
- [SDR C2XA09TY204](https://openairdocs.org/sdr/C2XA09TY204), Jul 29, 2009: MOUNT. CORRODED. LT FRM MOUNT FOR LT CARBON FIBER BEAM BULKHEAD SUPPORT AT FRM 61 HAS CORROSION AT LOWER EDGE. BLENDED CORRODED AREA, FABRICATED EXTERNAL DOUBLERS, ALODINED, PRI
- [SDR C2XA09TY202](https://openairdocs.org/sdr/C2XA09TY202), Jul 29, 2009: FLANGE. CORRODED. NR 1 ENG INLET ATTACH FLANGE HAS CORROSION AROUND BOLT HOLES. REAMED AND INSTALLED BUSHING IAW EC5420-01158.
- [SDR C2XA09TY196](https://openairdocs.org/sdr/C2XA09TY196), Jul 29, 2009: SILL. CORRODED. RT FLOORBOARD SILL BETWEEN FRM 53-60 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.
- [SDR C2XA09TY195](https://openairdocs.org/sdr/C2XA09TY195), Jul 29, 2009: SILL. CORRODED. LT FLOORBOARD SILL BETWEEN FRMS 53-60 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.
- [SDR C2XA09TY194](https://openairdocs.org/sdr/C2XA09TY194), Jul 29, 2009: FLOOR SUPPORT. CORRODED. RT OMEGA BEAM TOP CAP IN LAV HAS CORROSION UNDER CARBON BEAM AT FRM 61. REMOVED AND REPLACED TOP CAP.
- [SDR C2XA09TY191](https://openairdocs.org/sdr/C2XA09TY191), Jul 28, 2009: FLOOR SUPPORT. CORRODED. LT OMEGA BEAM TOPCAP IN LAV BETWEEN FRMS 59-62 IS CORRODED AROUND RIVETS AND NUT PLATES. BLENDED OUT CORROSION, IS WITHIN LIMITS. ALODINED, PRIMED AND PAINTED.
- [SDR C2XA09TY190](https://openairdocs.org/sdr/C2XA09TY190), Jul 28, 2009: SILL. CORRODED. LT SIDE FLOORBOARD SILL BETWEEN FRM 41-48 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.
- [SDR C2XA09TY189](https://openairdocs.org/sdr/C2XA09TY189), Jul 28, 2009: SILL. CORRODED. RT FLOORBOARD SILL BETWEEN FRM 48-53 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.
- [SDR C2XA09TY188](https://openairdocs.org/sdr/C2XA09TY188), Jul 28, 2009: SILL. CORRODED. LT SIDE OF FLOOBOARD SILL BETWEEN FRM 29-35 HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.
- [SDR C2XA09TY183](https://openairdocs.org/sdr/C2XA09TY183), Jul 24, 2009: SILL. CORRODED. TYS - THE RIGHT FLOOR SILL BETWEEN FR 59 THRU 61 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL IAW 145XR SRM 51-40-02 AND CPM 51-21-
- [SDR C2XA09TY182](https://openairdocs.org/sdr/C2XA09TY182), Jul 24, 2009: BRACKET. CORRODED. TYS - THE LAV FLOOR TOPCAP HAS SURFACE CORROSION UNDER THE POTABLE WATER OVERFILL B-NUT. MAINTENANCE REMOVED AND REPLACED THE WATER POTABLE SUPPORT BRACKET IAW 
- [SDR C2XA09TY181](https://openairdocs.org/sdr/C2XA09TY181), Jul 24, 2009: SILL. CORRODED. TYS - CORROSION WAS FOUND ON THE LEFT SILL BETWEEN FR 59 TO FR 60. MAINTENANCE REMOVED AND REPLACED THE SILL IAW EMB A45XR SRM 51-40-02 AND CPM 51-21-04-05-06. 
- [SDR C2XA09TY172](https://openairdocs.org/sdr/C2XA09TY172), Jul 22, 2009: ATTACH FITTING. CORRODED. NR 2 ENG INLET ATTACH FLANGE HAS CORROSION AROUND 9 NUT PLATE HOLES. REAMED TO REMOVE CORROSION AND INSTALLED BUSHINGS IAW EC5420-01158.
- [SDR C2XA09TY168](https://openairdocs.org/sdr/C2XA09TY168), Jul 22, 2009: SKIN. CHAFED. TYS - A/C IN A C-CHECK STATUS WHEN THE VENTRAL TANK WAS FOUND CHAFING THE LOWER FORWARD EDGE OF BELLY SKIN. MAINTENANCE BLENDED AREA AND FOUND TO BE WITHIN LIMI
- [SDR C2XA09SH192](https://openairdocs.org/sdr/C2XA09SH192), Jul 6, 2009: INVERTER. INOPERATIVE. RIGHT OVERWING EXIT SHROUD EXIT IDENTIFIER SIGN INOPERATIVE. REMOVED AND REPLACED NR 3 DC/AC INVERTER P/N 7824-1, S/N ILLEGIBLE WITH P/N 7824-1 S/N PT4563 IAW E
- [SDR C2XA09RI122](https://openairdocs.org/sdr/C2XA09RI122), Jun 19, 2009: LIGHT. BROKEN. FLIGHT CREW REPORTED EMERGENCY LIGHT STRIP BROKEN. MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERV
- [SDR C2XA09TY082](https://openairdocs.org/sdr/C2XA09TY082), May 4, 2009: FUSE. BLOWN. TYS - DURING ROUTINE MX BOTH OVERWING EMERGENCY LIGHTS WERE FOUND INOP. THE NR 4 BATTERY FUSES WERE REMOVED AND REPLACED AND OPS CHECKED GOOD IAW RADIANT POWER 

All 69: https://openairdocs.org/deregistered/N18102-2025-03-13/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20151223021369I](https://openairdocs.org/incident/20151223021369I), Dec 23, 2015: Embraer EMB-145XR (N18102), Montrose, CO, No damage. This incident is being reported in conjunction with the submittal of an aviation safety action program report (asap) therefore any certificate and or pilot…
- [Incident 20040619023599I](https://openairdocs.org/incident/20040619023599I), Jun 19, 2004: Emb EMB145XR (N18102), Lafayette, LA. (-23) Flight encountered severe turbulence at FL 350 15 miles south of lft. 1 minor passenger injury reported. Flight landed uneventfully at iah. Passenger…

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