# Service difficulty reports: N48901

A list on [N48901](https://openairdocs.org/aircraft/N48901.md).

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

Page 1 of 2 · 72 reports

- [SDR ASOA2020040984014](https://openairdocs.org/sdr/ASOA2020040984014.md): Light · intermittent · Apr 8, 2020 · N48901 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 4229, DURING MX INSPECTION THE MAIN PAX DOOR EMERGENCY LIGHT WAS FOUND TO BE INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201907195087](https://openairdocs.org/sdr/ASOA201907195087.md): Light · inoperative · Jul 19, 2019 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING MX THE EMERGENCY LIGHT FLOOR PROXIMITY STRIP ROW 22A TO 24A WAS DISCOVERED INOP. MX PLACED ON MEL. ON 7/24/19 MX REMOVED AND REPLACED THE LIGHT STRIP WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2019062433035](https://openairdocs.org/sdr/ASOA2019062433035.md): Acm · seized · Jun 23, 2019 · N48901 · Emb EMB145LR · Cabin Cooling System
  > THE CREW REPORTED FUMES AND VAPOR/MINOR SMOKE IN CABIN IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE #2 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA201904017035](https://openairdocs.org/sdr/ASOA201904017035.md): Frame · cracked · Mar 29, 2019 · N48901 · Emb EMB145LR · Fuselage Main, Frame
  > CRACKED FRAME RT SIDE ABOVE RT WINDSHIELD LATERAL POST. REMOVED CRACKED SECTION OF LATERAL BRACKET, INSTALLED NEW SECTION OF LATERAL BRACKET AND DOUBLER. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA201903247034](https://openairdocs.org/sdr/ASOA201903247034.md): Skin · corroded · Mar 24, 2019 · N48901 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND FUSELAGE CORRODED UNDER THE RA ANTENNA BETWEEN FRAMES 69 AND 70 AND STR 21L AND 21R. MAINTENANCE PERFORMED A DOUBLER ON THE FUSELAGE BELOW THE RA ANTENNA AT FRAMES 69 AND 70 IAW SRM 53-00-23. ALL WORK ACCOMPLISHED A
- [SDR ASOA2018042655110](https://openairdocs.org/sdr/ASOA2018042655110.md): Connector · unsecure · Apr 25, 2018 · N48901 · Emb EMB145LR · Light System Wiring
  > DURING MX INSPECTION THE RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT WAS DISCOVERED INOPERATIVE. MX RE-SEATED CANON PLUG AND PERFORMED OPERATIONAL CHECK WITH GOOD RESULT. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201706105086](https://openairdocs.org/sdr/ASOA201706105086.md): Inverter · inoperative · Jun 10, 2017 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, THE EMERGENCY LIGHTS FROM ROWS 3 TO 7 WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE INVERTER NR 3. OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201706105085](https://openairdocs.org/sdr/ASOA201706105085.md): Battery Pack · inoperative · Jun 10, 2017 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, THE MAIN CABIN DOOR, EXIT, OVERHEAD ROW 3, AND FWD LEFT WING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201612121596](https://openairdocs.org/sdr/ASOA201612121596.md): Skin · cracked · Dec 12, 2016 · N48901 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CK FR 75 FUSELAGE SKIN IS CRACKED BTW STR 1R-2R. REPAIRED FR 75 SKIN AT STR 1-2R BY CUTTING DAMAGE AND INSTALLING A FILLER AND DOUBLER IAW SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201612121586](https://openairdocs.org/sdr/ASOA201612121586.md): Stringer · cracked · Dec 12, 2016 · N48901 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CK STRINGER 2L IS CRACKED AT FR 75. REPAIRED STRINGER 2L IAW SRM 53-00-03 TABLE 202. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160323013V](https://openairdocs.org/sdr/ASOA20160323013V.md): Power Supply · inoperative · Mar 21, 2016 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE FORWARD CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY ASSY IAW AMM 33-50-04. THE LIGHTS OPERATIONALLY CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20160317018](https://openairdocs.org/sdr/ASOA20160317018.md): Battery · inoperative · Mar 17, 2016 · N48901 · Emb EMB145XR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE LT WING EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS WERE GOOD.
- [SDR ASOA20150326015](https://openairdocs.org/sdr/ASOA20150326015.md): Solenoid Valve · faulty · Mar 26, 2015 · N48901 · Emb EMB145LR · Landing Gear Door Retract Section
  > ON APPROACH AT 5000 FT PILOTED REPORTED THE NOSE GEAR DOORS OPENED AND REMAINED OPEN WITH THE GEAR LEVER IN THE UP POSITION. MAINTENANCE R & R THE NOSE GEAR DOOR SOLENOID VALVE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150104002](https://openairdocs.org/sdr/ASOA20150104002.md): Inverter · inoperative · Jan 4, 2015 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FLOOR EMERGENCY LIGHT STRIPS WERE NOT ILLUMINATING DURING A TEST. MAINTENANCE R & R THE NR 6 EMERGENCY LIGHT DC/AC INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20141017085](https://openairdocs.org/sdr/ASOA20141017085.md): Bleed Valve · faulty · Oct 17, 2014 · N48901 · Emb EMB145LR · Compressor Bleed Valve
  > THE CREW REPORTED AFTER STARTING APU, RECEIVED A STRONG FUEL ODOR IN COCKPIT, WHICH DISSIPATED. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPS CHECKED GOOD.
- [SDR ASOA20140607064](https://openairdocs.org/sdr/ASOA20140607064.md): Battery Pack · inoperative · Jun 7, 2014 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE NR 3 EMERGENCY LIGHT BATTERY WOULD NOT ILLUMINATE THE EMERGENCY LIGHTS. MX R & R THE NR 3 EMERGENCY LIGHT SYS BATTERY PACK, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140506053](https://openairdocs.org/sdr/ASOA20140506053.md): Flapper Valve · broken · May 6, 2014 · N48901 · Emb EMB145LR · Aircraft Fuel Distribution System
  > PILOT REPORTED A SUSPECTED FUEL LEAK, ENGINE NR 2, FUEL PPH AT CRUISE SET SIMILAR, YET TANK NR 2 INDICATOR SHOWED TANK NR 2 FUEL USAGE WAS MUCH GREATER. AFTER INSPECTION MX FOUND A BROKEN FLAP VALVE IN NR 2 FUEL TANK AND R & R WITH LEAK CHECK GOOD. ACFT WAS A
- [SDR ASOA20130802088](https://openairdocs.org/sdr/ASOA20130802088.md): Flapper Valve · leaking · Aug 2, 2013 · N48901 · Emb EMB145LR · Fuel Storage
  > CREW REPORTED FUEL LEAKING FROM THE RT WING AFTER TAKEOFF ALONG WITH FUEL IMBALANCE. CREW PERFORMED UNEVENFUL AIR RETURN. MX R & R THE RT WING FLAPPER VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130607085](https://openairdocs.org/sdr/ASOA20130607085.md): Unknown · smoke · Jun 7, 2013 · N48901 · Emb EMB145LR · Air Distribution System
  > THE CREW REPORTED SMOKE IN THE CABIN, APPROX 2 MINUTES AFTER SELECTING ENGINE BLEEDS, WITH A SMELL BEING IMMEDIATELY NOTICEABLE. THE ACFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, PERFORMED GROUND RUNS OF THE ENGINES, ALL WITH NO
- [SDR ASOA20130315027R](https://openairdocs.org/sdr/ASOA20130315027R.md): Bulb · inoperative · Mar 15, 2013 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE CEILING GALLEY EMERGENCY LIGHT WAS FOUND TO BE DIM DURING OPERATION. MX R & R THE CEILING GALLEY EMERGENCY LIGHT BULB, OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121126136V](https://openairdocs.org/sdr/ASOA20121126136V.md): Sill · corroded · Nov 26, 2012 · N48901 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CARGO DOOR SILL CORRODED. MX R & R CARGO DOOR SILL IAW CPM 51-21-06 AND SRM 53-31-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121126135V](https://openairdocs.org/sdr/ASOA20121126135V.md): Skin · corroded · Nov 26, 2012 · N48901 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK CARGO DOOR CUTOUT FWD AND AFT LOWER CORNERS CORRODED (LOCAL LEVEL 2). MX R & R CARGO DOOR CUTOUT FWD AND AFT LOWER CORNERS IAW EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121125134](https://openairdocs.org/sdr/ASOA20121125134.md): Floor Support · corroded · Nov 25, 2012 · N48901 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK RT OMEGA BEAM HAS CORROSION, LOCAL LEVEL 2, AT NUTPLATE FRAME 19A. MX PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 18-19A IAW EC5320-01718 (ORIG). THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121125133V](https://openairdocs.org/sdr/ASOA20121125133V.md): Sill · corroded · Nov 25, 2012 · N48901 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, SERVICE DOOR CENTER SILL CORRODED, LOCAL LEVEL 2. MX R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02 AND CPM 51-21-00. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11RI123](https://openairdocs.org/sdr/C2XA11RI123.md): Anti-Ice Valve · defective · Jul 6, 2011 · N48901 · Emb EMB145LR · Air Intake Anti/De-Ice System
  > FLIGHT 2829 - EWR - FLIGHT CREW REPORTED ENG NR 2 ANTI ICE FAIL IN FLIGHT. EWR MX REMOVED AND REPLACED NR 2 ENG ANTI-ICE VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA11CL151](https://openairdocs.org/sdr/C2XA11CL151.md): Proximity Switch · dirty · Jun 20, 2011 · N48901 · Emb EMB145LR · Landing Gear Position and Warning
  > ORD FLT 6131 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND CLEANED AND RE-SECURED LANDING GEAR PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11RI001](https://openairdocs.org/sdr/C2XA11RI001.md): Warning System · false activation · Jan 6, 2011 · N48901 · Emb EMB145LR · Landing Gear Position and Warning
  > FLIGHT 2228 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10CL139](https://openairdocs.org/sdr/C2XA10CL139.md): Manifold · faulty · Aug 28, 2010 · N48901 · Emb EMB145LR · Hydraulic System, Main
  > THE CREW REPORTED AN AILERON SYSTEM 2 INOPERATIVE MESSAGE ON THE ECIAS DURING CRUISE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AILERON HYDRAULIC MANIFOLD. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09RI007](https://openairdocs.org/sdr/C2XA09RI007.md): Sign · inoperative · Jan 8, 2009 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX, MX FOUND LOWER EMERGENCY LIGHT IDENTIFIER SIGN AT SEAT 12A INOPERATIVE. MX R&R SIGN AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09IA012](https://openairdocs.org/sdr/C2XA09IA012.md): Engine · malfunctioned · Jan 6, 2009 · N48901 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > THE CREW REPORTED A LAV FIRE DETECTION INDICATION IN FLIGHT. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND PLACED THE LAV SMOKE DETECTOR ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT LANDED WHERE MX
- [SDR C2XA09IA010A](https://openairdocs.org/sdr/C2XA09IA010A.md): Engine · malfunctioned · Jan 6, 2009 · N48901 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > SAT - FLIGHT 2630, THE CREW REPORTED A LAV FIRE DETECTION INDICATION IN FLIGHT. THE ACFT RETURNED TO SAT WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND PLACED THE LAV SMOKE DETECTOR ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE AC
- [SDR C2XA08IA273](https://openairdocs.org/sdr/C2XA08IA273.md): Smoke Detector · malfunctioned · Dec 23, 2008 · N48901 · Emb EMB145LR · Smoke Detection
  > IAH - FLIGHT 2406, THE CREW REPORTED A LAV SMOKE INDICATION ON T/O FROM DAL. THE SYSTEM WAS RESET SUCCESSFULLY PER THE QRH, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO
- [SDR C2XA08IA260](https://openairdocs.org/sdr/C2XA08IA260.md): Smoke Warning · malfunctioned · Dec 20, 2008 · N48901 · Emb EMB145LR · Smoke Detection
  > FLIGHT 2220 SHV-IAH - THE CREW REPORTED A MOMENTARY LAVATORY SMOKE WARNING DURING CRUISE. NO SMOKE CONDITIONS WERE NOTED AT THAT POINT AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE GROUND RUNS AND COULD NOT DUPLICATE THE CONDI
- [SDR C2XA08SH164](https://openairdocs.org/sdr/C2XA08SH164.md): Inlet · corroded · Dec 19, 2008 · N48901 · Emb EMB145LR · Engine Air Intake System
  > VARIOUS BOLTHOLES ON THE LT ENG AIR INLET CORRODED. REPAIRED BOLT HOLE ON LT ENG AIR INLET IAW EC 5420-01179. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08SH163](https://openairdocs.org/sdr/C2XA08SH163.md): Floor Support · corroded · Dec 19, 2008 · N48901 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER OMEGA BEAM HAS CORROSION IN RADIUS AT FR 20. CENTER OMEGA BEAM WAS REPAIRED IAW SRM 53-21-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08SH162](https://openairdocs.org/sdr/C2XA08SH162.md): Shroud · corroded · Dec 18, 2008 · N48901 · Emb EMB145LR · Ailerons
  > SHV DURING C-CHECK LT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED LT LOWER AILERON SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08SH161](https://openairdocs.org/sdr/C2XA08SH161.md): Nut Plate · corroded · Dec 18, 2008 · N48901 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV DURING C-CHECK SERVICE DOOR LOWER NUTPLATE HOLES HAD CORROSION. MX REPAIRED SERVICE DOOR LOWER NUTPLATE HOLES BY REMOVING CORROSION AND FINDING SERVICE DOOR LOWER NUT PLATE HOLES TO BE WITHIN LIMITS IAW EMB SRM 51-10-03 AND EC 5210-01154. MX THEN TREATED
- [SDR C2XA08SH160](https://openairdocs.org/sdr/C2XA08SH160.md): Shroud · corroded · Dec 18, 2008 · N48901 · Emb EMB145LR · Ailerons
  > SHV DURING C-CHECK RT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT AILERON LWR SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08SH159](https://openairdocs.org/sdr/C2XA08SH159.md): Plate · corroded · Dec 18, 2008 · N48901 · Emb EMB145LR · Wing Miscellaneous Structure
  > SHV DURING C-CHECK RT AILERON UPPER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT UPPER AILERON SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08SH158](https://openairdocs.org/sdr/C2XA08SH158.md): Panel · corroded · Dec 18, 2008 · N48901 · Emb EMB145LR · Aerodynamic Fairings
  > SHV DURING C-CHECK PANEL 191EL WAS FOUND TO HAVE CORRODED BONDING PLATES. MX R&R BONDING PLATES ON PANEL 191EL IAW EC 5750-01315 REV "E". THE ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08CL111](https://openairdocs.org/sdr/C2XA08CL111.md): Control Unit · faulty · Oct 9, 2008 · N48901 · Emb EMB145LR · Landing Gear Brake System
  > CLE FLIGHT NR 2626 THE CREW REPORTED A NR 1 T/R DISAGREE AND A SPOILER FAIL MSG IN FLIGHT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE BRAKE CONTROL UNIT AND RELAYS KO479 AND K1202. OPS CHECKS WERE GOOD.
- [SDR C2X2008F00012](https://openairdocs.org/sdr/C2X2008F00012.md): Bracket · broken · Jul 18, 2008 · N48901 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > ACFT WAS IN FOR A SERVICE CHECK AND THE RT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY HOLDER ASSEMBLY IAW AMM 33-50-04. OPS CHECK GOOD AND WAS RELEASED. (S)
- [SDR C2XA08RI047](https://openairdocs.org/sdr/C2XA08RI047.md): Proximity Switch · defective · Mar 13, 2008 · N48901 · Emb EMB145LR · Landing Gear Position and Warning
  > FLIGHT 3156 - EWR - CREW REPORTED BANGING NOISE COMING FROM NOSE LANDING GEAR AREA DURING TAXIING. CREW RETURNED TO GATE. EWR MX REMOVED AND REPLACED UPLOCK BOX PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN T
- [SDR C2XA07CL107](https://openairdocs.org/sdr/C2XA07CL107.md): Inverter · inoperative · Dec 25, 2007 · N48901 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, THE OVERWING EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07IA213](https://openairdocs.org/sdr/C2XA07IA213.md): Inverter · inoperative · Sep 23, 2007 · N48901 · Emb EMB145LR · Emergency Lighting
  > LCH - FLIGHT 3015, THE CREW REPORTED THE LEFT HAND WALL EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY EXIT LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA07RI073](https://openairdocs.org/sdr/C2XA07RI073.md): Connector · loose · Aug 31, 2007 · N48901 · Emb EMB145LR · Light System Wiring
  > RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT ON SEAT 12A INOP. MX REMOVED THE EMERGENCY LIGHT ASSEMBLY AND FOUND CONNECTOR LOOSE. MX RESECURED CONNECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07IA155](https://openairdocs.org/sdr/C2XA07IA155.md): Sensor · shorted · Jun 27, 2007 · N48901 · Emb EMB145LR · Trailing Edge Flap Control System
  > IAH - FLIGHT 2852, THE CREW REPORTED A W/S 1 FAIL MESSAGE ON EICAS FOLLOWED BY LOUD CLICKING OF RELAYS AND A STRONG BURNED ELECTRICAL ODOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE WINDSHIELD HEAT ON
- [SDR C2XA07BT022](https://openairdocs.org/sdr/C2XA07BT022.md): Charger · inoperative · Feb 28, 2007 · N48901 · Emb EMB145LR · Emergency Lighting
  > EWR MX LOG SQUAWK FLT NR 3005 FOUND EMERGENCY LIGHTS (RT WING FUSELAGE FRONT FAIRING AND ISLE LIGHT NR 2) INOP. REMOVED AND REPLACED CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. CLOSED
- [SDR C2XA06IA046](https://openairdocs.org/sdr/C2XA06IA046.md): Inverter · inoperative · Mar 22, 2006 · N48901 · Emb EMB145LR · Emergency Lighting
  > STL - DURING MAINTENANCE INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETU
- [SDR C2XA05SH034](https://openairdocs.org/sdr/C2XA05SH034.md): Floor Support · corroded · May 13, 2005 · N48901 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRM 29-36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRM 29 IAW EC5320-01237 AND EC5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/aircraft/N48901/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N48901' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N48901/reports

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