# Service difficulty reports: N15941, cancelled Mar 15, 2016 A list on [N15941, cancelled Mar 15, 2016](https://openairdocs.org/deregistered/N15941-2016-03-15.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 3 · 126 reports - [SDR ASOA20140923120](https://openairdocs.org/sdr/ASOA20140923120.md): Battery Pack · discharged · Sep 23, 2014 · N15941 · Emb EMB145EP · Emergency Lighting > DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS WERE REPORTED TO BE INTERMITTENT WHEN TURNED ON BY THE F/A. MAINTENANCE CHARGED THE NR 4 EMERGENCY LIGHT BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140414061](https://openairdocs.org/sdr/ASOA20140414061.md): Battery Pack · discharged · Apr 14, 2014 · N15941 · Emb EMB145EP · Emergency Lighting > DURING MAINTENANCE INSPECTION, AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140208021](https://openairdocs.org/sdr/ASOA20140208021.md): Display · failed · Feb 8, 2014 · N15941 · Emb EMB145EP · Central Display > THE CREW REPORTED THE NR 2 MAIN FLIGHT DISPLAY WAS INOPERATIVE ACCOMPANIED BY AN ODOR OF AN ELECTRICAL FIRE WITH NO SMOKE DETECTED. MAINTENANCE R & R THE NR 2 MFD, OPS TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131215218](https://openairdocs.org/sdr/ASOA20131215218.md): Light · inoperative · Dec 15, 2013 · N15941 · Emb EMB145EP · Emergency Lighting > DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT SEAT 20A INOPERATIVE. R & R LIGHT, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130810198](https://openairdocs.org/sdr/ASOA20130810198.md): Fire Detector · defective · Aug 10, 2013 · N15941 · Emb EMB145EP · Fire Detection > FIRE DETECTION FAIL MESSAGE ON EICAS DURING TAXI. R & R FIRE DETECTOR IAW AMM 26-11-01. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130719125](https://openairdocs.org/sdr/ASOA20130719125.md): Skin · cracked · Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING CYCLE CARD INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRAKED AT A RIVET ON FRAME 75 BELOW STRINGER 02R. MX PERFORMED A FILLER/DOUYBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130719132](https://openairdocs.org/sdr/ASOA20130719132.md): Skin · cracked · Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING INSPECTION, LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 6L. MX PERFORMED A BUSHING REPAIR IAW ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130719131](https://openairdocs.org/sdr/ASOA20130719131.md): Skin · cracked · Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 03L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130719130](https://openairdocs.org/sdr/ASOA20130719130.md): Skin · cracked · Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 4 PLACES AT A SINGLE RIVET ON FRAME 79 BELOW STRINGER 05L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130719129](https://openairdocs.org/sdr/ASOA20130719129.md): Skin · cracked · Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A SINGLE RIVET ON FRAME 77 BELOW STRINGER 8L. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130719128](https://openairdocs.org/sdr/ASOA20130719128.md): Skin · cracked · Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 5R. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/20/2013. - [SDR ASOA20130719126](https://openairdocs.org/sdr/ASOA20130719126.md): Skin · cracked · Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING INSPECTION, RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 75 BELOW STRINGER 02R. MX PERFORMED A FILLER/DOUBLER REPAIR IAW EA EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130719127](https://openairdocs.org/sdr/ASOA20130719127.md): Skin · cracked · Jul 19, 2013 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING CYCLE CARD INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 3R. MX PERFORMED A BUSHING REPAIR IAW DER APPROVED TECHNICAL DISPOSITION ETD2013-145-019577, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/ - [SDR ASOA20130416055H](https://openairdocs.org/sdr/ASOA20130416055H.md): Inverter · inoperative · Apr 16, 2013 · N15941 · Emb EMB145EP · Emergency Lighting > DURING MX INSPECTION, THE EMERGENCY LIGHT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130131257T](https://openairdocs.org/sdr/ASOA20130131257T.md): Skin · cracked · Jan 31, 2013 · N15941 · Emb EMB145ER · Fuselage Main, Plate/Skin > ACFT WAS FOUND WITH A 6MM CRACK FOR RIVET EDGE ON THE LT SKIN AT FRAME 75 BELOW STRINGER 2. MX INSTALL A SMALL PATCH TO THE FUSELAGE SKIN AT FRAME 75, STRINGER 2L IAW EC 5330-02353. PRESSURE CHECKED GOOD AND WAS RELEASED TO SERVICE. - [SDR ASOA20121110137](https://openairdocs.org/sdr/ASOA20121110137.md): Lamp · burned out · Nov 10, 2012 · N15941 · Emb EMB145EP · Emergency Lighting > DURING A CHECK INSPECTION, THE LT AFT OVERWRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LAMP, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120711047V](https://openairdocs.org/sdr/ASOA20120711047V.md): Yoke · cracked · Jul 11, 2012 · N15941 · Emb EMB145EP · Engine Mount Section > DURING C CHECK. RT FWD LOWER ENGINE YOKE IS CRACKED. REPAIRED RT ENGINE FWD LOWER YOKE IAW EC5450-01028. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120711046](https://openairdocs.org/sdr/ASOA20120711046.md): Yoke · cracked · Jul 11, 2012 · N15941 · Emb EMB145EP · Engine Mount Section > DURING C CHECK. LEFT FWD LOWER ENGINE YOKE IS CRACKED. REPAIRED LT FWD LOWER ENGINE YOKE IAW EC5450-01052. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11TY157](https://openairdocs.org/sdr/C2XA11TY157.md): Skin Panel · cracked · Oct 14, 2011 · N15941 · Emb EMB145ER · Fuselage Main, Plate/Skin > TYS - A/C WAS IN MOB WHEN A BELTLOADER HIT THE 191 BELLY PANEL AND CRACKED THE PANEL AFT OF THE PORTABLE WATER DOOR. A/C WAS FERRIED TO TYS WHERE THE COMPOSITE SHOP MADE THE REPAIR IAW ETD 2011-145-106533. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE. - [SDR C2XA11SH111](https://openairdocs.org/sdr/C2XA11SH111.md): Computer · malfunctioned · Aug 1, 2011 · N15941 · Emb EMB145EP · Integrated Flight System > AIRCRAFT 15941 FLIGHT 2734 AHRS 2 FAIL IAH-XNA DIVERTED TO SHV. SHV MAINTENANCE REMOVED AND REPLACED NUMBER 2 AHRS COMPUTER IAW 34-21-01, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11IA165](https://openairdocs.org/sdr/C2XA11IA165.md): Warning System · false activation · Jul 29, 2011 · N15941 · Emb EMB145EP · Landing Gear Position and Warning > IAH - FLIGHT 2734, DURING PREFLIGHT INSPECTION THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL INDICATION. MAINTENANCE RESET THE AIRCRAFT, AND THE INDICATION DID NOT REOCCUR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11IA147](https://openairdocs.org/sdr/C2XA11IA147.md): Proximity Sensor · inoperative · Jul 10, 2011 · N15941 · Emb EMB145EP · Landing Gear Position and Warning > IAH - FLIGHT 2318, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE ON EICAS AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT TRAILING ARM PROXIMITY SENSOR, OPERATIONALLY TESTED WIT - [SDR C2XA11IA134](https://openairdocs.org/sdr/C2XA11IA134.md): Warning System · false activation · Jun 28, 2011 · N15941 · Emb EMB145EP · Landing Gear Position and Warning > MEM - FLIGHT 2998, THE CREW REPORTED A LANDING GEAR AIR/GND FAIL MESSAGE WHEN THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE AIRCRAFT WAS INSPECTED AND FERRIED TO IAH. IAH MAINTENANCE JACKED THE AIRCRAFT AND PERFORMED PROXIMITY - [SDR C2XA11IA118](https://openairdocs.org/sdr/C2XA11IA118.md): Control Lever · faulty · Jun 15, 2011 · N15941 · Emb EMB145EP · Landing Gear Selector > IAH - CREW REPORTED, LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. COULD NOT RAISE LANDING GEAR. AIRCRAFT AIR RETURNED AND LANDED UNEVENTFULLY. IC 1-2 WOW INOP AFTER LANDING. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED LANDING GEAR CONTROL - [SDR C2XA11IA090](https://openairdocs.org/sdr/C2XA11IA090.md): Connector · burned · May 7, 2011 · N15941 · Emb EMB145EP · Light System Wiring > IAH - POST FLIGHT 2812, THE CREW REPORTED ELECTRICAL SMOKE IN THE CABIN AND COCKPIT, AND SEEMED TO BE STRONGEST AROUND ROWS 8 & 9. IAH MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LIGHT CONNECTOR AT ROW 10 TO BE BURNED. MAINTENANCE REMOVED AND REPLACED T - [SDR C2XA10IA261](https://openairdocs.org/sdr/C2XA10IA261.md): Skin Panel · cracked · Sep 24, 2010 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA127](https://openairdocs.org/sdr/C2XA10IA127.md): Ballast · malfunctioned · Apr 23, 2010 · N15941 · Emb EMB145EP · Passenger Compartment Lighting > MEM - DURING POST FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL BY ROWS 16-19. MAINTENANCE INSPECTED THE AIRCRAFT AND IDENTIFIED A BAD BALLAST ABOVE ROW 16. THE CABIN LIGHTS WERE PLACED ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER - [SDR C2XA10IA025](https://openairdocs.org/sdr/C2XA10IA025.md): Fitting · leaking · Jan 17, 2010 · N15941 · Emb EMB145EP · Hydraulic System, Main > IAH - FLIGHT 2895, DURING CLIMB THE CREW REPORTED HYDRAULIC FLUID COMING FROM THE RT WING LOWER WEEP HOLE WHEN THE SPOILERS WERE ACTUATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LEAK IN A - [SDR C2XA09TY273](https://openairdocs.org/sdr/C2XA09TY273.md): Trunnion · damaged · Dec 14, 2009 · N15941 · Emb EMB145EP · Wing, Landing Gear Attach Fittings > RIGHT MLG AFT TRUNNION PITTED. REWORKED TRUNNION WITH BORE MACHINE IAW EC5750-01398. - [SDR C2XA09IA187](https://openairdocs.org/sdr/C2XA09IA187.md): Duct · leaking · Jul 24, 2009 · N15941 · Emb EMB145EP · Pneumatic Distribution System > IAH - FLIGHT 2834, THE CREW REPORTED A BLEED 1 LEAK ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT BEHIND PANEL 271DLW, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WA - [SDR C2XA09TY109](https://openairdocs.org/sdr/C2XA09TY109.md): Module · defective · Jun 12, 2009 · N15941 · Emb EMB145EP · Emergency Lighting > TYS FOR IAH - THERE WAS INTERMITTENT OPERATION OF THE EMERGENCY LIGHTS IN ASSOCIATION WITH THE ECIAS SHOWING NOT ARMED. MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE IAW EMB 145 AMM 33-21-01, OPS CHECK GOOD AND WAS RELEASED. - [SDR C2XA09IA155](https://openairdocs.org/sdr/C2XA09IA155.md): Control Module · inoperative · Jun 11, 2009 · N15941 · Emb EMB145EP · Emergency Lighting > DAL - FLIGHT 2149, DURING PREFLIGHT INSPECTION THE GALLEY, EMERGENCY, AND LAV LIGHTS WERE FOUND TO BE INTERMITTENT, AND NOT OPERATING WITH THEIR RESPECTIVE SWITCHES. MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFEC - [SDR C2XA09IA127A](https://openairdocs.org/sdr/C2XA09IA127A.md): Light · inoperative · May 15, 2009 · N15941 · Emb EMB145EP · Emergency Lighting > IAH - FLIGHT 2046, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS DO NOT ALWAYS ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE AISLE PATH LIGHT BETWEEN SEAT 14 AND 17, OPERATIONALLY TESTED EMERGENCY LIGH - [SDR C2XA09IA070](https://openairdocs.org/sdr/C2XA09IA070.md): Strut · low · Mar 5, 2009 · N15941 · Emb EMB145EP · Nose/Tail Landing Gear Strut/Axle > IAH - FLIGHT 2003 THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH. MAINTENANCE INSPECTED THE AIRCRAFT, SERVICED THE NOSE LANDING GEAR, OPERATIONALLY TESTED THE GEAR RETRACTION AND EXTENSION SYSTEM WITH NO DEFECTS NOTED - [SDR C2XA08TY086](https://openairdocs.org/sdr/C2XA08TY086.md): Battery · discharged · Aug 19, 2008 · N15941 · Emb EMB145EP · Emergency Lighting > NR 1 EMERGENCY LIGHT BATTERY NOT CHARGING. REMOVED AND REPLACED BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE. (S) - [SDR C2XA08IA008](https://openairdocs.org/sdr/C2XA08IA008.md): Light · inoperative · Jan 2, 2008 · N15941 · Emb EMB145EP · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION EMERGENCY FLOOR LIGHT STRIP NR 6 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA07IA189](https://openairdocs.org/sdr/C2XA07IA189.md): Unknown · odor · Sep 3, 2007 · N15941 · Emb EMB145EP · Air Distribution System > LFT - FLIGHT 2734, DURING PREFLIGHT INSPECTION, THE CREW REPORTED A BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND THE ODOR TO BE COMING FROM THE PACKS WITH THE APU RUNNING. MAINTENANCE MEL'D THE APU 49-00-00 (C) CONTRO 128496, A - [SDR C2XA07IA173](https://openairdocs.org/sdr/C2XA07IA173.md): Inverter · inoperative · Jul 24, 2007 · N15941 · Emb EMB145EP · Emergency Lighting > IAH - FLIGHT 2533, DURING POSTFLIGHT INSPECTION THE RIGHT HAND EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. - [SDR C2XA07TY029](https://openairdocs.org/sdr/C2XA07TY029.md): Skin · dented · Jun 12, 2007 · N15941 · Emb EMB145EP · Fuselage Main, Plate/Skin > DENT ON FUSELAGE SKIN AFT OF PAX DOOR. CUT OUT DAMAGE, FABRICATED FILLER & DOUBLER AND INSTALLED IAW EMB 134/145 SRM 51-20-03, 51-40-06, 51-40-02, 53-21-01 & CPM 51-21-04, 05, 06. - [SDR C2XA07TY028](https://openairdocs.org/sdr/C2XA07TY028.md): Rib · dented · Jun 10, 2007 · N15941 · Emb EMB145EP · Nacelle/Pylon, Frame/Spar/Rib > LEFT LWR COWL DENTED. REMOVED AND REPLACED DAMAGED RIB IN CENTER SECTION OF COWL, RECON TOURED DENTS AT OIL SERVICE DOOR, FABRICATED AND INSTALLED EXTERNAL DOUBLER, ALODINED, PRIMED AND PAINTED IAW EC 5430-01059. AIRCRAFT STILL IN C-CHECK. - [SDR C2XA07TY027](https://openairdocs.org/sdr/C2XA07TY027.md): Door Frame · cracked · Jun 8, 2007 · N15941 · Emb EMB145EP · Fuselage Main, Structure > FRAME 68 CRACKED UNDERNEATH CARGO DOOR -HOLD OPEN- HANDLE RETAINING CUP. CUT OUT AFFECTED FRAME, FABRICATED THE FRAME REPAIR SEGMENT FROM A SECTION OF A NEW FRAME AND INSTALLED. WORK ACCOMPLISHED IAW EC 5310-01411, EMB 145 SRM 53-00-04 AND CPM. AIRCRAFT STI - [SDR C2XA05TY031](https://openairdocs.org/sdr/C2XA05TY031.md): Floor Support · corroded · Mar 24, 2005 · N15941 · Emb EMB145ER · Fuselage Miscellaneous Structure > TYS DURING A C-CHECK INSPECTION THE CENTER AISLE SUPPORT STRUCTURE ON THE LEFT SIDE WAS FOUND WITH CORROSION FROM FRAME 20 TO 60. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM ASSEMBLY FROM FR 20 TO 29 AND BLENDED FROM 29 THRU 60 AND WAS FOUND WITHIN - [SDR C2XA05TY030](https://openairdocs.org/sdr/C2XA05TY030.md): Fitting · loose · Mar 23, 2005 · N15941 · Emb EMB145ER · Vertical Stabilizer, Attach Fittings > DURING A SCHEDULED C-CHECK INSPECTION, THE NR 1 RUDDER TO VERTICAL STABILIZER LOWER HINGE FITTING ATTACH POINT BUSHING WAS FOUND TO BE MIGRATED AND LOOSE. THE DEFECTIVE BUSHING WAS REMOVED; THE FITTING HOLE WAS DIMENSIONALLY CHECKED AND FOUND TO BE WORN. MAI - [SDR C2XA05TY029](https://openairdocs.org/sdr/C2XA05TY029.md): Frame · damaged · Mar 20, 2005 · N15941 · Emb EMB145ER · Fuselage Main, Frame > TYS, DURING A SCHEDULED INSPECTION THE LOWER SKIN SUPPORT BRACKET BETWEEN STR 21L AND 21R ON FR21 HAS ELONGATED HOLES. MAINTENANCE PERFORMED REPAIR WITH TWO INTERNAL L ANGLE DOUBLERS ON FR 21 BETWEEN STR 21L AND 21R. ALODINED, PRIMED AND INSTALLED IAW EC5310 - [SDR C2XA05TY028](https://openairdocs.org/sdr/C2XA05TY028.md): Fitting · corroded · Mar 20, 2005 · N15941 · Emb EMB145ER · Vertical Stabilizer, Spar/Rib > TYS, DURING A SCHEDULED INSPECTION FRAME 75, SPAR 1 FITTING SHOWS SIGNS OF FRETTING. MAINTENANCE REMOVED THE FITTING, BLENDED CORROSION ON INNER SKIN SURFACE, DYE PENATRANT TESTED THE AREA, TREATED FOR CORROSION, DRILLED AND INSTALLED A NEW FITTING IAW EC5310 - [SDR C2XA04CL125](https://openairdocs.org/sdr/C2XA04CL125.md): Wire · broken · Dec 8, 2004 · N15941 · Emb EMB145ER · Light System Wiring > CLE FLIGHT 2481 THE CREW REPORTED THE EMERGENCY LIGHTS AT THE CENTER OF THE AIRCRAFT WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED BROKEN WIRES IN THE CEILING AT ROW 12. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA04BT115](https://openairdocs.org/sdr/C2XA04BT115.md): Inverter · faulty · Oct 30, 2004 · N15941 · Emb EMB145ER · Emergency Lighting > CREW REPORTED, EMERGENCY EXIT LIGHT INVERTER INTERMITTENT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SD009](https://openairdocs.org/sdr/C2XA04SD009.md): Bulb · inoperative · Oct 19, 2004 · N15941 · Emb EMB145ER · Emergency Lighting > DURING INSPECTION RIGHT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT WING EMERGENCY LIGHT BULB. OPS CHECK GOOD. - [SDR C2XA04SH459](https://openairdocs.org/sdr/C2XA04SH459.md): Control Valve · inoperative · Jul 9, 2004 · N15941 · Emb EMB145ER · Landing Gear Brake System > SHV - DURING TAXI TO THE GATE BRK OUTBD INOP WAS OBSERVED ON THE EICAS. CREW RESET THE CIRCUIT BREAKERS AND THE MESSAGE WENT AWAY. DURING TAXI TO THE HANGER THE MESSAGE REAPPEARED AND WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE - [SDR C2XA03CL206](https://openairdocs.org/sdr/C2XA03CL206.md): Control Panel · faulty · Dec 20, 2003 · N15941 · Emb EMB145ER · Emergency Lighting > CLE FLIGHT 3253 THE CREW REPORTED THE EMERGENCY LIGHT AISLE PATH LIGHTING STAYED ON. MAINTENANCE REPLACED THE FLIGHT ATTENDANT'S CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD. Next page: https://openairdocs.org/deregistered/N15941-2016-03-15/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 = 'N15941' AND deregistration_id = 'N15941-2016-03-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N15941-2016-03-15/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.