N15932, cancelled Dec 31, 2022

Service difficulty reports · 116

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASOA20131218294VHinge Fitting · wornDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20131218293Hinge Fitting · wornDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20131218292Hinge Fitting · wornDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20131218291VHinge Fitting · wornDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20131218290Skin · crackedDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20131218289Hinge Fitting · wornDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Rudder StructureSDR ASOA20131218288Hinge Fitting · wornDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · SpoilersSDR ASOA20131218287Frame · crackedDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, FrameSDR ASOA20131218286Stringer · crackedDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Longeron/StringerSDR ASOA20131218285Floor Support · corrodedDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20131218284Support · corrodedDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20131218283Sill · corrodedDURING 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.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20130627094Skin · crackedDURING 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 RJun 27, 2013 · N15932 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130627093Skin · crackedDURING 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 REJun 27, 2013 · N15932 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130627092Skin · crackedDURING 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 REJun 27, 2013 · N15932 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130627091Skin · crackedDURING 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 FJun 27, 2013 · N15932 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130606083Firewall · crackedDURING 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.Jun 7, 2013 · N15932 · Emb EMB145EP · APU Cowling/ContainmentSDR C2XA10SH226Battery · overtempDFW - 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.Jul 7, 2010 · N15932 · Emb EMB145EP · Battery/Charger SystemSDR C2XA09IA247Engine · leakingIAH - 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 RETUOct 1, 2009 · N15932 · Emb EMB145EP · Engine (Turbine/Turboprop)SDR C2XA09IA246Acm · seizedIAH - 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 RSep 29, 2009 · N15932 · Emb EMB145EP · Cabin Cooling SystemSDR C2XA09TY218Inverter · inoperativeTYS - 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.Aug 14, 2009 · N15932 · Emb EMB145EP · Emergency LightingSDR C2XA09IA132Light · inoperativeIAH - 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.May 20, 2009 · N15932 · Emb EMB145EP · Emergency LightingSDR C2XA09IA130Landing Gear · lowFLIGHT 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 SUBSEQMay 16, 2009 · N15932 · Emb EMB145EP · Nose/Tail Landing GearSDR C2XA09IA128Warning System · malfunctionedFLIGHT 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 ACFMay 15, 2009 · N15932 · Emb EMB145EP · Landing Gear Position and WarningSDR C2XA09CL044Turbine Wheel · crackedDURING 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.Apr 20, 2009 · N15932 · Emb EMB145LR · Turbine SectionSDR C2XA09TY038Inlet · corrodedAIRCRAFT 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 AMar 1, 2009 · N15932 · Emb EMB145EP · Turbine Engine Air Inlet SectionSDR C2XA09TY034Inlet · corrodedDURING 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.Feb 24, 2009 · N15932 · Emb EMB145EP · Engine Air Intake SystemSDR C2XA09TY031Frame · damagedFRAME 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.Feb 17, 2009 · N15932 · Emb EMB145 · Fuselage Main, FrameSDR C2XA09IA017Ballast · burnedDURING 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 RETUJan 11, 2009 · N15932 · Emb EMB145EP · Passenger Compartment LightingSDR C2X2008F00044Electronic Unit · inoperativeTHE 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 SERVICSep 6, 2008 · N15932 · Emb EMB145EP · Landing Gear Retraction/Extension SystemSDR C2XA07IA248Skin · crackedIAH - 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.Dec 16, 2007 · N15932 · Emb EMB145EP · Wing, Plate/SkinSDR C2XA07SH029Smoke Detector · inoperativeSHV - 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 SERVMay 13, 2007 · N15932 · Emb EMB145EP · Smoke DetectionSDR C2XA06SH135Floorbeam · crackedSHV - 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 APPRODec 9, 2006 · N15932 · Emb EMB145EP · Fuselage Main, Floor BeamSDR C2XA06SH134Firewall · chafedSHV - 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.Dec 8, 2006 · N15932 · Emb EMB145EP · APU Cowling/ContainmentSDR C2XA05BT027Odor · detectedCREW 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 POWERMay 9, 2005 · N15932 · Emb EMB145ER · Air Distribution SystemSDR C2XA05CL028Odor · detectedPIT 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.Apr 25, 2005 · N15932 · Emb EMB145ER · Air Distribution SystemSDR C2XA04SH570Floor Support · corrodedDURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE.Dec 6, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH569Floor Support · corrodedDURING 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.Dec 3, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH568Floor Support · corrodedDURING 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.Dec 3, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH563Floor Support · corrodedDURING 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.Dec 2, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH566Floor Support · corrodedDURING 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.Nov 20, 2004 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH556Beam · corrodedDURING C-CHECK, THE LOWER CARGO DOOR CUTOUT BEAM WAS FOUND CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICENov 18, 2004 · N15932 · Emb EMB145ER · Fuselage Main, StructureSDR C2XA04SH555Frame · crackedDURING 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.Nov 17, 2004 · N15932 · Emb EMB145ER · Passenger/Crew DoorsSDR C2XA04SH554Bearing Cap · scratchedDURING 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 SERVICENov 17, 2004 · N15932 · Emb EMB145ER · Main Landing GearSDR C2XA04BT086Light · malfunctionedATL LOG SQUAWK EMERGENCY LIGHTS NOT ARMED EICAS INFLIGHT. PERFORMED ADJUSTMENT TEST ON EMERGENCY LIGHT SYSTEM. OPS CHECK OK IAW EMB AMM 33-50-00.Aug 8, 2004 · N15932 · Emb EMB145ER · Emergency LightingSDR C2XA04TY054Lens · crackedTYS 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.Mar 20, 2004 · N15932 · Emb EMB145ER · Emergency LightingSDR C2XA03BT102Light · inoperativeCREW 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.Oct 24, 2003 · N15932 · Emb EMB145ER · Emergency LightingSDR C2XA03CL178Inverter · failedDURING 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.Oct 23, 2003 · N15932 · Emb EMB145ER · Emergency LightingSDR C2XA03CL177Light · inoperativeCLE FLIGHT 2163 THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED.Oct 23, 2003 · N15932 · Emb EMB145ER · Emergency LightingSDR C2XA03CL175Connector · dirtyCLE 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.Oct 22, 2003 · N15932 · Emb EMB145ER · Emergency Lighting
Back to N15932, cancelled Dec 31, 2022