# Service difficulty reports: N15932, cancelled Dec 31, 2022 A list on [N15932, cancelled Dec 31, 2022](https://openairdocs.org/deregistered/N15932-2022-12-31.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 · 116 reports - [SDR ASOA20131218294V](https://openairdocs.org/sdr/ASOA20131218294V.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer Structure > DURING C-CHECK THE HORIZONTAL STAB HINGE PIN FITTING NR 4 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218293](https://openairdocs.org/sdr/ASOA20131218293.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer Structure > DURING C-CHECK THE HORIZONTAL STAB HINGE PIN FITTING, NR 3 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218292](https://openairdocs.org/sdr/ASOA20131218292.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer Structure > DURING C-CHECK, THE HORIZONTAL STAB HINGE PIN FITTING NR 2 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218291V](https://openairdocs.org/sdr/ASOA20131218291V.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer Structure > DURING C-CHECK, HORIZONTAL STAB HINGE PIN FITTING NR 1 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218290](https://openairdocs.org/sdr/ASOA20131218290.md): Skin · cracked · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Plate/Skin > DURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-80 AND STRINGERS 3-7R. MAINTENANCE REMOVED THE CRACKS BY REAMING AND PERFORMED BUSHING REPAIRS IAW EC5330-02840. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218289](https://openairdocs.org/sdr/ASOA20131218289.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Rudder Structure > DURING C-CHECK, THE RUDDER II UPPER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218288](https://openairdocs.org/sdr/ASOA20131218288.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Spoilers > DURING C-CHECK, THE LT SPEED BRAKE CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218287](https://openairdocs.org/sdr/ASOA20131218287.md): Frame · cracked · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Frame > DURING C-CHECK, LEFT FRAME 10 SEGMENT WAS FOUND TO BE CRACKED BETWEEN STRINGERS 9-10L. R & R FRAME SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218286](https://openairdocs.org/sdr/ASOA20131218286.md): Stringer · cracked · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Longeron/Stringer > DURING C-CHECK, STRINGER 6R WAS FOUND TO BE CRACKED AT FRAME 14. R & R STRINGER SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218285](https://openairdocs.org/sdr/ASOA20131218285.md): Floor Support · corroded · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure > DURING C-CHECK, RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. REMOVED CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218284](https://openairdocs.org/sdr/ASOA20131218284.md): Support · corroded · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure > DURING C-CHECK, LAVATORY WASTE DRAIN SUPPORT ASSY WAS FOUND TO BE CORRODED. R & R SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218283](https://openairdocs.org/sdr/ASOA20131218283.md): Sill · corroded · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure > DURING C-CHECK, SERVICE DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130627094](https://openairdocs.org/sdr/ASOA20130627094.md): Skin · cracked · Jun 27, 2013 · N15932 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING 5A INSPECTION, A CRACK INDICATION WAS FOUND AROUND A RIVET AT FR 77 BETWEEN STR 3L & 4L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501 AND THE ACFT WAS APPROVED FOR R - [SDR ASOA20130627093](https://openairdocs.org/sdr/ASOA20130627093.md): Skin · cracked · Jun 27, 2013 · N15932 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING 5A INSPECTION, A CRACK INDICATION WAS FOUND AROUND A RIVET AT FR 78 BETWEEN STR 5L & 6L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501 AND THE ACFT WAS APPROVED FOR RE - [SDR ASOA20130627092](https://openairdocs.org/sdr/ASOA20130627092.md): Skin · cracked · Jun 27, 2013 · N15932 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING 5A INSPECTION, A CRACK INDICATION WAS FOUND AROUND A RIVET AT FR 79 BETWEEN STR 5L & 6L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501 AND THE ACFT WAS APPROVED FOR RE - [SDR ASOA20130627091](https://openairdocs.org/sdr/ASOA20130627091.md): Skin · cracked · Jun 27, 2013 · N15932 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING 5A INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR75 ABOVE STR02L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A TRIPLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, THE ACFT WAS APPROVED F - [SDR ASOA20130606083](https://openairdocs.org/sdr/ASOA20130606083.md): Firewall · cracked · Jun 7, 2013 · N15932 · Emb EMB145EP · APU Cowling/Containment > DURING APU CHANGE THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER LT MOUNTING POINT. MX PERFORMED AN SRM DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH226](https://openairdocs.org/sdr/C2XA10SH226.md): Battery · overtemp · Jul 7, 2010 · N15932 · Emb EMB145EP · Battery/Charger System > DFW - BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA247](https://openairdocs.org/sdr/C2XA09IA247.md): Engine · leaking · Oct 1, 2009 · N15932 · Emb EMB145EP · Engine (Turbine/Turboprop) > IAH - DURING MAINTENANCE INSPECTION AN OIL SMELL WAS REPORTED IN THE CABIN WITH THE NR 2 ENGINE BLEED AND PACS ON FULL HOT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETU - [SDR C2XA09IA246](https://openairdocs.org/sdr/C2XA09IA246.md): Acm · seized · Sep 29, 2009 · N15932 · Emb EMB145EP · Cabin Cooling System > IAH - FLIGHT 2619, THE CREW REPORTED A BURNING RUBBER SMELL FROM THE PACKS IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ACM, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR R - [SDR C2XA09TY218](https://openairdocs.org/sdr/C2XA09TY218.md): Inverter · inoperative · Aug 14, 2009 · N15932 · Emb EMB145EP · Emergency Lighting > TYS - A/C IN FOR AN A-CHECK WHEN INSPECTION FOUND THE MAIN PAX DOOR EXIT SIGN EMERGENCY LIGHT TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 INVERTER AND OPS CHECK GOOD IAW EMB 145 AMM 33-50-11. AIRCRAFT RELEASED TO SERVICE. - [SDR C2XA09IA132](https://openairdocs.org/sdr/C2XA09IA132.md): Light · inoperative · May 20, 2009 · N15932 · Emb EMB145EP · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT STRIP BETWEEN ROWS 8 & 9 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA130](https://openairdocs.org/sdr/C2XA09IA130.md): Landing Gear · low · May 16, 2009 · N15932 · Emb EMB145EP · Nose/Tail Landing Gear > FLIGHT 2468, AFTER TAKEOFF THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, SERVICED THE NLG, OPS TESTED THE AIR/GRND SYS WITH NO DEFECTS NOTED. THE ACFT WAS SUBSEQ - [SDR C2XA09IA128](https://openairdocs.org/sdr/C2XA09IA128.md): Warning System · malfunctioned · May 15, 2009 · N15932 · Emb EMB145EP · Landing Gear Position and Warning > FLIGHT 2934, DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, PERFORMED OPS TEST ON THE GEAR EXTENSION/RETRACTION SYS WITH NO DEFECTS NOTED, AND THE ACF - [SDR C2XA09CL044](https://openairdocs.org/sdr/C2XA09CL044.md): Turbine Wheel · cracked · Apr 20, 2009 · N15932 · Emb EMB145LR · Turbine Section > DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED. - [SDR C2XA09TY038](https://openairdocs.org/sdr/C2XA09TY038.md): Inlet · corroded · Mar 1, 2009 · N15932 · Emb EMB145EP · Turbine Engine Air Inlet Section > AIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND EIGHT BOLT HOLES ON THE NUMBER ONE ENGINE INTAKE INLET THAT WERE CORRODED. MAINTENANCE REPAIRED THE CORRODED BOLT HOLES IAW EC5420-01158 BY USING REAMERS AND NEW BUSHINGS. ALL WORK WAS COMPLIED WITH A - [SDR C2XA09TY034](https://openairdocs.org/sdr/C2XA09TY034.md): Inlet · corroded · Feb 24, 2009 · N15932 · Emb EMB145EP · Engine Air Intake System > DURING A C-CHECK INSPECTION EIGHT BOLT HOLES WERE FOUND SHOWING CORROSION ON THE NR 1 ENGINE INTAKE MOUNT FLANGE. THE HOLES WERE CLEANED AND REAMED TO REMOVE ALL TRACES OF CORROSION IAW EC 5420-01158. A/C IS STILL IN C-CHECK. - [SDR C2XA09TY031](https://openairdocs.org/sdr/C2XA09TY031.md): Frame · damaged · Feb 17, 2009 · N15932 · Emb EMB145 · Fuselage Main, Frame > FRAME 31 HAS MAINTENANCE INDUCED DAMAGE STR 15R AND 16R. CUT OUT DAMAGE AREA ON FRAME 31 & FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-00-04. AIRCRAFT STILL IN C-CHECK. - [SDR C2XA09IA017](https://openairdocs.org/sdr/C2XA09IA017.md): Ballast · burned · Jan 11, 2009 · N15932 · Emb EMB145EP · Passenger Compartment Lighting > DURING POST FLIGHT INSP, CREW REPORTED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT AND F/A JUMPSEAT AREA WITH NO VISIBLE SMOKE. MX INSPECTED THE ACFT, AND R&R THE LIGHTING BALLAST AT SEAT 1A, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETU - [SDR C2X2008F00044](https://openairdocs.org/sdr/C2X2008F00044.md): Electronic Unit · inoperative · Sep 6, 2008 · N15932 · Emb EMB145EP · Landing Gear Retraction/Extension System > THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AC RETURNED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONICS UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AC WAS APPROVED FOR RETURN TO SERVIC - [SDR C2XA07IA248](https://openairdocs.org/sdr/C2XA07IA248.md): Skin · cracked · Dec 16, 2007 · N15932 · Emb EMB145EP · Wing, Plate/Skin > IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A CRACK IN THE UPPER RT WING SKIN. THE CRACK WAS INSPECTED AND PLACED ON A 500 FLIGHT CYCLE DEFERRAL IN ACCORDANCE WITH EMBRAER IC2007-145/08976, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA07SH029](https://openairdocs.org/sdr/C2XA07SH029.md): Smoke Detector · inoperative · May 13, 2007 · N15932 · Emb EMB145EP · Smoke Detection > SHV - DURING ROUTINE MAINTENANCE THE BAGGAGE COMPARTMENT SMOKE DETECTOR FAILED THE OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE DETECTOR IAW EMB 145 AMM 26-11-01. THE ENSUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV - [SDR C2XA06SH135](https://openairdocs.org/sdr/C2XA06SH135.md): Floorbeam · cracked · Dec 9, 2006 · N15932 · Emb EMB145EP · Fuselage Main, Floor Beam > SHV - MAJOR - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CRACKED AT FR 22 AND CORRODED BETWEEN FRAMES 19A-22. MAINTENANCE REMOVED THE DAMAGED AREAS AND INSTALLED DOUBLER REPAIRS IAW EMB 145 SRM 51-40-02 AND EC5320-01081, REV A. THE AIRCRAFT WAS APPRO - [SDR C2XA06SH134](https://openairdocs.org/sdr/C2XA06SH134.md): Firewall · chafed · Dec 8, 2006 · N15932 · Emb EMB145EP · APU Cowling/Containment > SHV - MAJOR - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED AT THE 6 O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A DOUBLER REPAIR IAW EC5310-01359, STEP 1.2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA05BT027](https://openairdocs.org/sdr/C2XA05BT027.md): Odor · detected · May 9, 2005 · N15932 · Emb EMB145ER · Air Distribution System > CREW REPORTED, BURNING ODOR COMING FROM RELAY BOX UNDER GEAR PINS. MAINTENANCE PERFORMED VISUAL INSPECTION OF LEFT HAND POWER DISTRIBUTION PANEL, NO ARCING OR BURNED AREAS NOTED. FOUND FORWARD COOLING AIR DUCT DISCONNECTED, RECONNECTED DUCT AND APPLIED POWER - [SDR C2XA05CL028](https://openairdocs.org/sdr/C2XA05CL028.md): Odor · detected · Apr 25, 2005 · N15932 · Emb EMB145ER · Air Distribution System > PIT FLT 2864, THE CREW REPORTED AN ELECTRICAL BURNING ODOR. CLEVELAND SENT A MAINTENANCE CREW TO INSPECT AND TROUBLESHOOT THE ODOR, THE MAINTENANCE CREW FOUND A MAGAZINE BLOCKING THE HEATING VENT AND COULD NOT DUPLICATE THE REPORTED CONDITIONS. - [SDR C2XA04SH570](https://openairdocs.org/sdr/C2XA04SH570.md): Floor Support · corroded · Dec 6, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure > DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SH569](https://openairdocs.org/sdr/C2XA04SH569.md): Floor Support · corroded · Dec 3, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure > DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED AT FRAME 29. REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SH568](https://openairdocs.org/sdr/C2XA04SH568.md): Floor Support · corroded · Dec 3, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure > DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5320-01177. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SH563](https://openairdocs.org/sdr/C2XA04SH563.md): Floor Support · corroded · Dec 2, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure > DURING C-CHECK THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SH566](https://openairdocs.org/sdr/C2XA04SH566.md): Floor Support · corroded · Nov 20, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure > DURING C CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EC5320-0117. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SH556](https://openairdocs.org/sdr/C2XA04SH556.md): Beam · corroded · Nov 18, 2004 · N15932 · Emb EMB145ER · Fuselage Main, Structure > DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT BEAM WAS FOUND CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE - [SDR C2XA04SH555](https://openairdocs.org/sdr/C2XA04SH555.md): Frame · cracked · Nov 17, 2004 · N15932 · Emb EMB145ER · Passenger/Crew Doors > DURING C-CHECK EDDY CURRENT INSPECTION OF THE PASSENGER DOOR STOP ATTACHMENT AT STRING 14L HAD A CRACK INDICATION. REAMED HOLE TO OVERSIZED CONDITION INSTALLED BUSHING IAW EC5310-01307. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SH554](https://openairdocs.org/sdr/C2XA04SH554.md): Bearing Cap · scratched · Nov 17, 2004 · N15932 · Emb EMB145ER · Main Landing Gear > DURING C-CHECK, THE LEFT MAIN GEAR BEARING CAP WAS FOUND SCRATCHED IN THE BEARING TRACK. REPLACED THE AFFECTED CAP IAW 32-10-01. AIRCRAFT RETURNED TO SERVICE - [SDR C2XA04BT086](https://openairdocs.org/sdr/C2XA04BT086.md): Light · malfunctioned · Aug 8, 2004 · N15932 · Emb EMB145ER · Emergency Lighting > ATL LOG SQUAWK EMERGENCY LIGHTS NOT ARMED EICAS INFLIGHT. PERFORMED ADJUSTMENT TEST ON EMERGENCY LIGHT SYSTEM. OPS CHECK OK IAW EMB AMM 33-50-00. - [SDR C2XA04TY054](https://openairdocs.org/sdr/C2XA04TY054.md): Lens · cracked · Mar 20, 2004 · N15932 · Emb EMB145ER · Emergency Lighting > TYS A/C 932 WAS IN FOR A SERVICE CHECK AND MAINTENANCE FOUND THE LEFT CABIN WALL EXIT LIGHT DAMAGE. MAINTENANCE REMOVED AND REPLACED THE EXIT WALL LENS IAW 145 AMM 33-50-13. OPS CHECK GOOD ALL WORK WAS COMPLIED WITH AND RELEASED. - [SDR C2XA03BT102](https://openairdocs.org/sdr/C2XA03BT102.md): Light · inoperative · Oct 24, 2003 · N15932 · Emb EMB145ER · Emergency Lighting > CREW REPORTED, EMERGENCY AISLE PATH FLOOR LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY AISLE PATH FLOOR LIGHT STRIP IAW EMB145 MM 33-50-00. OPS CHECKED EMERGENCY LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA03CL178](https://openairdocs.org/sdr/C2XA03CL178.md): Inverter · failed · Oct 23, 2003 · N15932 · Emb EMB145ER · Emergency Lighting > DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGNS IN AISLE OVER EXIT DOORS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 INVERTER. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA03CL177](https://openairdocs.org/sdr/C2XA03CL177.md): Light · inoperative · Oct 23, 2003 · N15932 · Emb EMB145ER · Emergency Lighting > CLE FLIGHT 2163 THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. - [SDR C2XA03CL175](https://openairdocs.org/sdr/C2XA03CL175.md): Connector · dirty · Oct 22, 2003 · N15932 · Emb EMB145ER · Emergency Lighting > CLE FLIGHT 2163 THE CREW REPORTED THE EXIT SIGN OVER ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED THE CONNECTOR FOR THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. Next page: https://openairdocs.org/deregistered/N15932-2022-12-31/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 = 'N15932' AND deregistration_id = 'N15932-2022-12-31' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N15932-2022-12-31/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.