# Service difficulty reports: N15983 A list on [N15983](https://openairdocs.org/aircraft/N15983.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 · 87 reports - [SDR ASOA201902167027](https://openairdocs.org/sdr/ASOA201902167027.md): Rib · cracked · Feb 15, 2019 · N15983 · Emb EMB145LR · Wing, Rib/Bulkhead > RT WING RIB 21 CRACKED. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER. AIRCRAFT STILL IN C CHECK. - [SDR ASOA201812067188](https://openairdocs.org/sdr/ASOA201812067188.md): Socket · inoperative · Dec 4, 2018 · N15983 · Emb EMB145LR · Lighting System > MAIN CABIN DOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT SOCKET IAW AMM 33-50-06. - [SDR ASOA201705305081](https://openairdocs.org/sdr/ASOA201705305081.md): Display · shorted · May 30, 2017 · N15983 · Emb EMB145LR · Attitude and Direction Data System > MFD NR 2 WENT BLANK AT THE SAME TIME AS AN ELECTRICAL BURNING ODOR. MX REMOVED AND REPLACED NR 2 MFD WITH OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201704083082](https://openairdocs.org/sdr/ASOA201704083082.md): Light · inoperative · Apr 8, 2017 · N15983 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED FORWARD FLOOR EMERGENCY LIGHT INOPERATIVE. - [SDR ASOA201704083070](https://openairdocs.org/sdr/ASOA201704083070.md): Battery · inoperative · Apr 8, 2017 · N15983 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED FORWARD FLOOR EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. - [SDR ASOA20160427013](https://openairdocs.org/sdr/ASOA20160427013.md): Skin · dented · Apr 25, 2016 · N15983 · Emb EMB145LR · Fuselage Main, Plate/Skin > DENT LOCATED BETWEEN FRAME 19 AND FRAME 20 AT STR 15L AND 16L. CUTOUT DAMAGED SECTION FABRICATED FILLER AND DOUBLER, INSTALLED AND REFINISHED. ACFT RELEASED AND RETURNED TO SERVICE. - [SDR ASOA20151030063](https://openairdocs.org/sdr/ASOA20151030063.md): Skin · dented · Oct 30, 2015 · N15983 · Emb EMB145LR · Fuselage Main, Plate/Skin > GROUND PERSONAL REPORTED DENT DAMAGE AROUND RT REAR AREA OF ACFT FUSELAGE BETWEEN STRINGERS 18R & 19R AND FRAMES 62 & 63A. MAINTENANCE INSPECTED AND PERFORMED REPAIR, FILLER AND DOUBLER OF DENT DAMAGE IAW ETD 2015-145-101284 AND SRM 51-40-02. DAMAGE MEASUREM - [SDR ASOA20141105318](https://openairdocs.org/sdr/ASOA20141105318.md): Profile · corroded · Nov 5, 2014 · N15983 · Emb EMB145LR · Cargo/Baggage Doors > DURING C-CHECK, CARGO DOOR INNER L PROFILE IS CORRODED AROUND NUTPLATES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-40-02 A. - [SDR ASOA20141105317](https://openairdocs.org/sdr/ASOA20141105317.md): Floor Support · corroded · Nov 5, 2014 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C-CHECK, LT OMEGA BEAM FLANGE CORRODED AT FRAME 23. REPAIRED IAW EC5320-01984. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140922107](https://openairdocs.org/sdr/ASOA20140922107.md): Smoke Detector · faulty · Sep 22, 2014 · N15983 · Emb EMB145LR · Smoke Detection > PILOT REPORTED A LAV SMOKE MASTER WARNING ON THE EICAS DURING FLIGHT. OCCURED TWICE FOR APPOXIMATELY 10 SECONDS EACH TIME. MX R & R THE LAVATORY SMOKE SENSOR, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140612069](https://openairdocs.org/sdr/ASOA20140612069.md): Unknown · odor · Jun 12, 2014 · N15983 · Emb EMB145LR · Air Distribution System > CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK AND TOWARDS REAR OF ACFT DURING ARRIVAL. ALSO NOTED THE ACFT WAS VERY WARM WITH THE PACKS TO FULL COLD. MX PERFORMED MULTIPLE OPS CHECKS OF PACKS SUCCESSFULLY. MX ALSO PERFORMED GVI OF CABIN WITH NO - [SDR ASOA20140518042](https://openairdocs.org/sdr/ASOA20140518042.md): Brake Assy · worn · May 18, 2014 · N15983 · Emb EMB145LR · Landing Gear Brake System > THE CREW REPORTED BRAKES COULD NOT BE APPLIED FULL, GRAB HARD AND RELEASE AND PULL LEFT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BRAKE ASSEMBLY. OPS CHECKED GOOD. - [SDR ASOA20140502039](https://openairdocs.org/sdr/ASOA20140502039.md): Light · inoperative · May 2, 2014 · N15983 · Emb EMB145 · Emergency Lighting > DURING ROUTINE MAINTENANCE THE AFT AISLE PATH EMERGENCY LIGHT STRIP WOULD NOT TEST. MAINTENANCE REPLACED THE LIGHT STRIP AND OPS CHECKS WERE GOOD. - [SDR ASOA20130107208](https://openairdocs.org/sdr/ASOA20130107208.md): Light · inoperative · Jan 6, 2013 · N15983 · Emb EMB145LR · Emergency Lighting > MAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE. - [SDR ASOA20120530050](https://openairdocs.org/sdr/ASOA20120530050.md): Sign · inoperative · May 30, 2012 · N15983 · Emb EMB145 · Emergency Lighting > DURING ROUTINE MX, THE LT SIDEWALL EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX REPLACED THE LT SIDEWALL EMERGENCY EXIT SIGN. OPS CHECKED GOOD. - [SDR ASOA20120314023](https://openairdocs.org/sdr/ASOA20120314023.md): Check Valve · torn · Mar 14, 2012 · N15983 · Emb EMB145LR · Aircraft Fuel Distribution System > FLT 4566. DURING TAKEOFF, A SMALL FUEL LEAK WAS REPORTED FROM THE LT WING. CREW PERFORMED AIR RETURN BACK AS PRECAUTION WITHOUT INCIDENT. MX FOUND DEBRIS AND THE LT WING OTBD CHECK VALVE TORN. MX R & R THE CHECK VALVE IAW AMM 28-11-04. FILLED LT WING WITH - [SDR C2XA11IA167](https://openairdocs.org/sdr/C2XA11IA167.md): Battery · discharged · Jul 27, 2011 · N15983 · Emb EMB145LR · Emergency Lighting > MCI - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE - [SDR C2XA11RI027](https://openairdocs.org/sdr/C2XA11RI027.md): Light · inoperative · Feb 20, 2011 · N15983 · Emb EMB145LR · Emergency Lighting > RIC - DURING ROUTINE MAINTENANCE, INSPECTION FOUND EMERGENCY LIGHT FLOOR STRIP AT EMERGENCY EXIT (ROW 12) INOPERATIVE. RIC MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10CL200](https://openairdocs.org/sdr/C2XA10CL200.md): Unknown · smoke · Dec 15, 2010 · N15983 · Emb EMB145LR · Air Distribution System > MCI FLT 3088 THE CREW REPORTED SMOKE IN THE CABIN DURING PACK 2 OPERATION.MAINTENANCE PERFORMED ENGINE 1 AND 2 RUNS WITH BLEED 1 AND 2 OPEN AND BOTH PACKS OPERATING. NO DEFECTS WERE FOUND AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVIC - [SDR C2XA10IA332](https://openairdocs.org/sdr/C2XA10IA332.md): Engine · leaking · Dec 15, 2010 · N15983 · Emb EMB145LR · Engine (Turbine/Turboprop) > IAH - FLIGHT 2496, THE CREW REPORTED AN ACRID BURNING SMELL LIKE TIRES OR GUNPOWDER DESCENDING THROUGH FL270 THAT ONLY LASTED A FEW SECONDS, WITH NOTHING NOTICED BY THE F/A. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED TH - [SDR C2XA10IA331](https://openairdocs.org/sdr/C2XA10IA331.md): Unknown · smoke · Dec 15, 2010 · N15983 · Emb EMB145LR · Air Distribution System > MCI - FLIGHT 3088, DURING TAXI THE CREW REPORTED SMOKE IN THE CABIN DURING PACK 2 OPERATION, THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED E1 & E2 RUNS AND BLEED & PACK SYSTEM CHECKS ALL WITH NO DEFECTS OR SMOKE NOTED, A - [SDR C2XA10SH420](https://openairdocs.org/sdr/C2XA10SH420.md): Rivet · loose · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK RT FUSELAGE HAS WORKING RIVETS BETWEEN FRAMES 75-80 (38 RIVETS). MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN RT SIDE FRAMES 75-80 IAW EMB-145 EC5330-02300. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH419](https://openairdocs.org/sdr/C2XA10SH419.md): Rivet · loose · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK LT FUSELAGE HAS WORKING RIVETS BETWEEN FRAMES 76-80 (23 RIVETS). MAINTENANCE PERFORMED REPAIR ON LT FUSELAGE SKIN FRAMES 76-80 IAW EC5330-02300. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH418](https://openairdocs.org/sdr/C2XA10SH418.md): Floor Support · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK RT OMEGA BEAM IS CORRODED AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 23 IAW EMB-145 EC5320-01443 REV C AND IAW EMB-145 SRM 53-21-10. RESTORED REWORKED REPAIRED AREA IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APP - [SDR C2XA10SH417](https://openairdocs.org/sdr/C2XA10SH417.md): Floor Support · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM IS CORRODED (PNL 231FF) AND RAMP ANGLE AT FRAME 20. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AND REMOVED AND REPLACED LT OMEGA BEAM RAMP ANGLE AT FRAME 20 IAW EMB-145 SRM 51-40-02 AND 51-30-01 AND ALODINED, PREPPED, PRI - [SDR C2XA10SH416](https://openairdocs.org/sdr/C2XA10SH416.md): Fitting · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage, Stabilizer Attach Fittings > SHV - DURING C-CHECK FUSELAGE FITTING-TO-VERTICAL STABILIZER SPAR ATTACHMENT BETWEEN FRAME 75 HAS INDICATION OF CORROSION AT TOP SKIN INTERFACE. MAINTENANCE REMOVED AND RE-INSTALLED FUSELAGE FITTING TO VERTICAL STABILIZER SPAR ATTACHMENT IAW EMB-145 EC5310-0 - [SDR C2XA10SH415](https://openairdocs.org/sdr/C2XA10SH415.md): Sill · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CARGO DOOR SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH414](https://openairdocs.org/sdr/C2XA10SH414.md): Sill · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION REPAIRED SERVICE DOOR CENTER SILL IAW EMB 145 SRM 53-21-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH413](https://openairdocs.org/sdr/C2XA10SH413.md): Attach Fitting · worn · Dec 5, 2010 · N15983 · Emb EMB145LR · Spoilers > SHV - DURING C-CHECK RT GROUND SPOILER O/B ATTACHMENT FITTING HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 SRM 51-20-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH412](https://openairdocs.org/sdr/C2XA10SH412.md): Attach Fitting · worn · Dec 5, 2010 · N15983 · Emb EMB145LR · Spoilers > SHV - DURING C-CHECK RT GROUND SPOILER I/B ATTACHMENT FITTING HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 SRM 51-20-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH411](https://openairdocs.org/sdr/C2XA10SH411.md): Floor Support · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C-CK. LT OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH410](https://openairdocs.org/sdr/C2XA10SH410.md): Floor Support · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C-CK. LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW SRM 53-22-10. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH409](https://openairdocs.org/sdr/C2XA10SH409.md): Floor Support · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C-CK. LT OMEGA BEAM HAS CORROSION AT FR 24. REPAIRED OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH408](https://openairdocs.org/sdr/C2XA10SH408.md): Floor Support · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C-CK, CTR OMEGA BEAM HAS CORROSION AT FR 34. REPAIRED OMEGA BEAM IAW SRM 53-22-10. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH407](https://openairdocs.org/sdr/C2XA10SH407.md): Floor Support · corroded · Dec 5, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C-CK. CTR OMEGA BEAM HAS CORROSION AT FR 20. R & R OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH402](https://openairdocs.org/sdr/C2XA10SH402.md): Floor Support · corroded · Nov 27, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 36-41. REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH399](https://openairdocs.org/sdr/C2XA10SH399.md): Floor Support · corroded · Nov 17, 2010 · N15983 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK RT OMEGA BEAM IS CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR OF RT OMEGA BEAM AT FRAME 23 IAW EMB-145 EC5320-01443 REV C. SRM 53-21-10 RESTORED TO ORIGINAL FINISH TO REWORKED AREA IAW EMB-145 CPM 51-21-06. THE AIR - [SDR C2XA10CL128](https://openairdocs.org/sdr/C2XA10CL128.md): Connector · loose · Aug 6, 2010 · N15983 · Emb EMB145LR · Fire Protection System Wiring > CLE FLT 2537 THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE ON TAKEOFF ROLL. MAINTENANCE INSPECTED THE APU FIRE DETECTOR WIRE HARNESS AND SECURED A LOOSE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10IA209](https://openairdocs.org/sdr/C2XA10IA209.md): Wire · chafed · Jul 25, 2010 · N15983 · Emb EMB145LR · Auto Flight System Wiring > SAV - FLIGHT 2312, THE CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT AND CABIN, AND ON SHORT FINAL AUTO PILOT FAILED, SECONDARY PITCH TRIM FAIL, THEN CA,& F/O MFD'S AND EICAS ALL WENT TO RED X'S FOLLOWED BY THE AUTO PILOT CIRCUIT BREAKER POPPING. THE AIRCRAFT - [SDR C2XA10IA208](https://openairdocs.org/sdr/C2XA10IA208.md): Icu · inoperative · Jul 24, 2010 · N15983 · Emb EMB145LR · Air Conditioning System > SAV - FLIGHT 2312, THE CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT AND CABIN, AND ON SHORT FINAL AUTO PILOT FAILED, SECONDARY PITCH TRIM FAIL, THEN CA, & F/O MFD'S AND EICAS ALL WENT TO RED X'S FOLLOWED BY THE AUTO PILOT CIRCUIT BREAKER POPPING. THE AIRCRAF - [SDR C2XA10RI045](https://openairdocs.org/sdr/C2XA10RI045.md): Connector · loose · Mar 22, 2010 · N15983 · Emb EMB145LR · Fire Protection System Wiring > FLIGHT 2612 - EWR - FLIGHT CREW REPORTED APU FIRE DETECTION SYSTEM FAIL MESSAGE ON EICAS. EWR MX RE-SECURED LOOSE CONNECTOR ON APU FIRE LOOP AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10RI012](https://openairdocs.org/sdr/C2XA10RI012.md): Inverter · inoperative · Jan 12, 2010 · N15983 · Emb EMB145LR · Emergency Lighting > EWR - DURING ROUTINE MAINTENANCE, EWR MX FOUND EMERGENCY LIGHT OVER RIGHT WING EXIT DOOR INOPERATIVE. MX REMOVED AND REPLACED INVERTER AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09RI182](https://openairdocs.org/sdr/C2XA09RI182.md): Hydraulic System · low · Oct 23, 2009 · N15983 · Emb EMB145LR · Hydraulic System, Main > FLIGHT 2138 - RIC - FLIGHT CREW DIVERTED FLIGHT TO RIC DUE TO HYDRAULIC 1 QUANTITY LOW MESSAGE AND FLUID LEVEL DECREASING. CREW LANDED ACFT UNEVENTFULLY. RIC MX SERVICED HYDRAULIC SYSTEM AND PERFORMED LEAK CHECK. NO LEAK WAS FOUND. ACFT WAS APPROVED TO RET - [SDR C2XA09CL126](https://openairdocs.org/sdr/C2XA09CL126.md): Windshield · cracked · Oct 1, 2009 · N15983 · Emb EMB145LR · Flight Compartment Windows > CLE FLT 2995 - THE CREW REPORTED THE CAPTAINS WINDSHIELD WAS CRACKED IN THE LOWER LEFT CORNER ABOUT 3-4 INCHES LONG. MAINTENANCE INSPECTED AND REPLACED THE WINDSHIELD. - [SDR C2XA09CL005](https://openairdocs.org/sdr/C2XA09CL005.md): Ecu · faulty · Jan 11, 2009 · N15983 · Emb EMB145LR · Trailing Edge Flap Control System > CLE FLIGHT NR 2841 THE CREW REPORTED A FLAP FAIL MSG ON THE EICAS ATTEMPTING TO RAISE THE FLAPS TO O AFTER TAKEOFF. INDICATION WAS 9 DEGRESS AND THE FLAP HANDLE IN O DEGREE POSITION. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REP - [SDR C2XA09RI005](https://openairdocs.org/sdr/C2XA09RI005.md): Charger · inoperative · Jan 5, 2009 · N15983 · Emb EMB145LR · Emergency Lighting > EWR MX - DURING ROUTINE MX, EWR MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX R&R NR 1 EMERGENCY LIGHT BATTERY CHARGER AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09RI004](https://openairdocs.org/sdr/C2XA09RI004.md): Charger · inoperative · Jan 5, 2009 · N15983 · Emb EMB145LR · Emergency Lighting > EWR MX - DURING ROUTINE MX, EWR MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX R&R NR 2 EMERGENCY LIGHT BATTERY CHARGER AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09RI003](https://openairdocs.org/sdr/C2XA09RI003.md): Battery Pack · inoperative · Jan 5, 2009 · N15983 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MX, MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX REMOVED AND REPLACED NR2 EMERGENCY LIGHT BATTERY AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07IA225](https://openairdocs.org/sdr/C2XA07IA225.md): Inverter · inoperative · Oct 18, 2007 · N15983 · Emb EMB145LR · Emergency Lighting > IAH - FLIGHT 2455, THE CREW REPORTED THAT THE FORWARD CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE - [SDR C2XA07RI017](https://openairdocs.org/sdr/C2XA07RI017.md): Flex Duct · damaged · Apr 15, 2007 · N15983 · Emb EMB145LR · Air Distribution System > FLT 2987 - EWR - FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN COMING FROM FLOOR VENT BETWEEN ROWS 9-11. EWR MX FOUND NR 1 PACK DUCT TO BE OFF RECIRCULATE FAN AND TO BE DAMAGED. MX REMOVED AND REPLACED DUCT IAW EMB 145 MM 21-20-04. MX PERFORMED OPERATIONAL C Next page: https://openairdocs.org/aircraft/N15983/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 = 'N15983' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N15983/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.