N15948, cancelled Jul 11, 2016

Service difficulty reports · 97

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 = 'N15948' AND deregistration_id = 'N15948-2016-07-11'
  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 ASOA20131026191Duct · crackedCREW REPORTED PACK 1 AND 2 FAILED IN FLIGHT AND A BAD ODOR AFTER SELECTING. RESET PACK 2 CREW CONTINUED TO DESTINATION WITH PACKS DEACTIVATED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE "Y" DUCT BETWEEN THE PACK VALVE AND DUALOct 26, 2013 · N15948 · Emb EMB145EP · Air Distribution SystemSDR ASOA20130915168Light · inoperativeDURING TESTING, NR 3 EMERGENCY LIGHT FAILED TO ILLUMINATE. MX REPLACED THE LIGHT STRIP, OPS TESTED THE SYS AND CLEARED THE DISCREPANCY.Sep 15, 2013 · N15948 · Emb EMB145EP · Emergency LightingSDR ASOA20130421138Skin · corrodedDURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 20R-20L. MX R & R THE SKIN IAW EC5320-01787. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20130421137Stringer · corrodedDURING C-CHECK, STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12-13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Longeron/StringerSDR ASOA20130421136Stringer · corrodedDURING C-CHECK, STRINGER 21L WAS FOUND TO BE CORRODED BETWEEN FRAMES 12 AND 13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Longeron/StringerSDR ASOA20130421135VSill · corrodedDURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20130210012Skin · crackedDURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2R. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.Feb 10, 2013 · N15948 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20130210011Skin · crackedDURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.Feb 10, 2013 · N15948 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR ASOA20120405051Connector · brokenDURING MX INSPECTION, LT WING EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. REPAIRED A BROKEN ELECTRICAL CONNECTOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 6, 2012 · N15948 · Emb EMB145EP · Light System WiringSDR ASOA20120405050Connector · disconnectedDURING MX INSPECTION, THE RT WING EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. RESECURRED THE EXIT SIGN INVERTER ELECTRICAL CONNECTOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 5, 2012 · N15948 · Emb EMB145EP · Light System WiringSDR C2XA11IA138Dimmer · defectiveIAH - FLIGHT 2060, DURING TAXI THE CREW REPORTED A RELAY CLICKING ON THE CAPTAINS SIDE WITH LOTS OF FUMES. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED SWITCH S0019 (DIMMER SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCJul 2, 2011 · N15948 · Emb EMB145EP · Electrical Power SystemSDR C2XA11IA074Blade · brokenFLIGHT 2031, CREW REPORTED NR 2 ENG LP VIBRATIONS EXCEEDED LIMITS. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R & R THE NR 2 ENGINE, OPS AND LEAK CHECK WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETUApr 21, 2011 · N15948 · Emb EMB145EP · Turbine SectionSDR C2XA11IA055Control Handle · inoperativeIAH - FLIGHT 2544, THE CREW REPORTED THAT THE GEAR WAS SLOW TO RETRACT ON DEPARTURE FROM DAL WITH THE ASSOCIATED WARNINGS. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR HANDLE, OPERATIONALLYMar 17, 2011 · N15948 · Emb EMB145EP · Landing Gear SelectorSDR C2XA10IA339Inverter · inoperativeIAH - DURING MAINTENANCE INSPECTION THE LEFT EMERGENCY EXIT LIGHT AT THE WING EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR Dec 17, 2010 · N15948 · Emb EMB145EP · Emergency LightingSDR C2XA10IA284Warning System · malfunctionedIAH - 500 FEET ABOVE THE GROUND THE CREW REPORTED A LANDING GEAR AIR/ GRND FAIL MESSAAGE ON EICAS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE RESET THE LANDING GEAR AIR GROUND CIRCUIT BREAKER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERNov 4, 2010 · N15948 · Emb EMB145EP · Landing Gear Position and WarningSDR C2XA10IA279Proximity Switch · inoperativeIAH - FLIGHT 2876, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON LANDING. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOOct 30, 2010 · N15948 · Emb EMB145EP · Landing Gear Position and WarningSDR C2XA10SH362Skin · crackedSHV - DURING C-CHECK SKIN CRACKS AROUND RIVET HEAD FR 78 RT SIDE. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN FR 78 RT SIDE IAW EC5330-02260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA10SH361Skin · crackedSHV - DURING C-CHECK SKIN CRACKS AROUND RIVET AT RT SIDE FR 77. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN RT SIDE FR 77 IAW EC5330-02260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA10SH360Floor Support · corrodedSHV - DURING C-CHECK (FR 29) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR FOR LT OMEGA BEAM L-FLANGE AT FRAME 29 IAW EMB-145 SRM 53-00-10 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SEOct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH359Floor Support · corrodedSHV - DURING C-CHECK (FR 29) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER BEAM CROSSBEAM SUPPORT AT FR 29 AND RESTORED TO ORIGINAL FINISH IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APOct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH358Floor Support · corrodedSHV - DURING C-CHECK (FR 33) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH357Floor Support · corrodedSHV - DURING C-CHECK (FR 33) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM FR 33 IAW EMB-145 SRM 53-00-10 FIG 202 STEP 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH356Yoke · crackedSHV - DURING C-CHECK NR 1 ENGINE FWD LWR ENGINE YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FWD LWR ENGINE YOKE IAW EC5450-01028 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Engine Mount SectionSDR C2XA10SH355Door Frame · corrodedSHV - DURING C-CHECK CARGO DOOR CUTOUT LWR STRUCTURE CORRODED (LEVEL 2 LOCAL) IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER STRUCTURE IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, StructureSDR C2XA10SH354Bracket · wornSHV - DURING C-CHECK RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) MISSING. MAINTENANCE REMOVED AND REPLACED RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) IAW EMB-145 SRM 51-40-02. Oct 25, 2010 · N15948 · Emb EMB145ER · AileronsSDR C2XA10SH353Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FR 49-50 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH352Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 58 CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 58 CARBON CROSS MEMBER IAW SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICOct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH351Floor Support · corrodedSHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 44 HAS CORROSION (LEVEL 2 LOCAL) TO CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE AT FRM 44 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH350Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 44 TO CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FR 44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH349Beam · corrodedSHV-DURING C-CHECK LT OMEGA BEAM LOWER SUPPORT FLANGE AT FR 54-59 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM LOWER SUPPORT FLANGE AT FRAME 54-59 IAW EMB-145 EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA10SH348Floor Support · corrodedSHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM "L" FLANGE AT 49-50 AT CARBON CROSS MEMBER IAW EMB-145 SRM 51-40-02, 53-00-10 AND RESTORED TO ORIOct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH347Floor Support · corrodedSHV - DURING C-CHECK (FR 38) CTR OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CTR OMEGA BEAM L-FLANGE AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH346Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 20 FLANGE HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 19-20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH345Floor Support · corrodedSHV - DURING C-CHECK (FR 38) LT OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRM 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10IA275Proximity Sensor · dirtyIAH - FLIGHT 2541, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND THE THRUST REVERSERS WOULD NOT DEPLOY ON LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY TESTED THE THRUST REVERSERS WITH NO DEFECTS. CLEANED Oct 24, 2010 · N15948 · Emb EMB145EP · Landing Gear Position and WarningSDR C2XA10IA255Skin · damagedIAH - FLIGHT 2149, DURING POST FLIGHT INSPECTION THE CREW REPORTED A HOLE IN THE RIGHT LOWER SIDE OF RUDDER II. MAINTENANCE REPLACED THE DAMAGED SECTION OF SKIN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 15, 2010 · N15948 · Emb EMB145EP · Rudder, Plate/SkinSDR C2XA10IA207Module · inoperativeIAH - FLIGHT 2547, DURING CLIMB THE CREW REPORTED THAT THE AUTO PRESSURIZATION WAS NOT WORKING AND THAT THE EICAS INDICATIONS WERE INTERMITTENT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CPAM MODULE, Jul 25, 2010 · N15948 · Emb EMB145EP · Cabin Pressure Control SystemSDR C2XA10IA160Indicator · defectiveCRP - FLIGHT 2894, DURING CLIMB THE CREW REPORTED THAT THE NUMBER ONE FUEL QUANTITY INDICATOR DASHED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL QUANTITY REPEATER OPERATIONALLY TESTED THE FUELMay 23, 2010 · N15948 · Emb EMB145EP · Fuel Quantity IndicatorSDR C2XA10IA133Light · out of adjustLRD - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW TWELVE TO BE INOPERATIVE. MAINTENANCE ADJUSTED THE EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 26, 2010 · N15948 · Emb EMB145EP · Emergency LightingSDR C2XA10IA126Light · inoperativeIAH - DURING MAINTENANCE INSPECTION THE CEILING EMERGENCY LIGHT AT ROW 3 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 22, 2010 · N15948 · Emb EMB145EP · Emergency LightingSDR C2XA10IA079Light · shortedIAH - FLIGHT 2720, THE CREW REPORTED, SMELLED ELECTRICAL SMOKE AND CB11 FOR THE COCKPIT READING LIGHTS POPPED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE F/O'S READING LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS. AFeb 22, 2010 · N15948 · Emb EMB145EP · Flight Compartment LightingSDR C2XA10IA045Light · inoperativeIAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT AT ROW 12CB WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 29, 2010 · N15948 · Emb EMB145EP · Emergency LightingSDR C2XA10IA027Unknown · odorIAH - FLIGHT 2372, THE FLIGHT ATTENDANT REPORTED A SMELL OF FUEL IN THE CABIN DURING DESCENT WITH THE SMELL COMING FROM THE WING AREA AND AFT. THE SMELL DISSIPATED AFTER THE RECIRC FAN WAS TURNED OF, AND RETURNED ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOJan 18, 2010 · N15948 · Emb EMB145EP · Air Distribution SystemSDR C2XA09TY119Unknown · fumesTHERE WERE SUFFOCATING FUMES AND ODOR REPORTED BY THE GROUND WORKERS COMING FROM THE CARGO BIN. THE CARGO BIN WAS INSPECTED AND FOUND ODOR TO BE RESIDUAL FROM A PASSENGER TRANSPORTING FISH, THERE WAS NO FLUIDS FOUND IN CARGO AND NO MX OR DISCREPANCIES FOUND.Jun 17, 2009 · N15948 · Emb EMB145ER · Air Distribution SystemSDR C2XA09CL071Turbine 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 DURING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.May 21, 2009 · N15948 · Emb EMB145EP · Turbine SectionSDR C2XA09TY063AConnector · looseSEAT 12BC SIDEWALL AFT EMERGENCY LIGHT INOP. FOUND CONNECTOR LOOSE. TIGHTENED CONNECTOR AND OPS CHECKED GOOD. IAW EMB 145 AMM 33-50-14Apr 20, 2009 · N15948 · Emb EMB145 · Light System WiringSDR C2XA08IA042Skin · crackedIAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THEJan 29, 2008 · N15948 · Emb EMB145EP · Wing, Plate/SkinSDR C2XA06IA082Wire Harness · disconnectedOKC - FLIGHT 2637, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIGN TO BE DISCONNECTED. MAINTENANCE RECONNECTED THE SIGN, OPERATIONALLY CHECKJun 2, 2006 · N15948 · Emb EMB145EP · Light System WiringSDR C2XA06TY006Casting · crackedMAIN DOOR FRAME STRUCTURE UPPER FWD STOP HOLE IS CRACKED (TOP INBOARD HOLE). REMOVED AND REPLACED CASTING FOR UPPER FWD PAX DOOR STOP IAW EMB 145 SRM 51-40-02.Jan 10, 2006 · N15948 · Emb EMB145EP · Fuselage Main, FrameSDR C2XA06TY005Floorbeam · corrodedGALLEY AREA RT OMEGA BEAM CORRODED. BLENDED OUT CORROSION, APPLIED HYSOL, FABRICATED REPAIR DOUBLER, DRILLED COUNTERSANK, ALODINED, PRIMED. INSTALLED PAINT. ALL WORK C/W IAW EMB135/145 SRM 51-10-03, 51-20-03, 51-40-06, 51-40-02 AND 53-21-10 AND CPM 51-21-04Jan 10, 2006 · N15948 · Emb EMB145EP · Fuselage Main, Floor Beam
Back to N15948, cancelled Jul 11, 2016