N186SW, cancelled Feb 21, 2006

Service difficulty reports · 71

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 = 'N186SW' AND deregistration_id = 'N186SW-2006-02-21'
  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 SWIA200515683Light · brokenRT OVERWING EMERGENCY LIGHT BROKEN. REPLACED RIGHT WING EMERGENCY EXIT LIGHT ASSY, OPERATIONAL CHECK GOOD.Oct 13, 2005 · N186SW · Emb EMB120ER · Emergency LightingSDR SWIA200515564Lamp · burned outROW 9A FLOOR EMERGENCY LIGHTING, ONE RED LIGHT INOP. RELAMPED BULB TO LIGHT SOCKET, OPERATIONAL CHECK GOOD.Sep 15, 2005 · N186SW · Emb EMB120ER · Emergency LightingSDR SWIA200514491Line · leakingAFTER GEAR EXTENSION, GREEN HYDRAULIC LOW LEVEL LIGHT, THE GUAGE CONFIRMED ZERO QUANTITY. REPLACED GEAR DOWN HYDRAULIC FLEXIBLE LINE ON RIGHT MAIN GEAR. SERVICED HYDRAULICS TO PROPER LEVEL. OPERATIONAL CHECK GOOD.Jan 15, 2005 · N186SW · Emb EMB120ER · Hydraulic System, MainSDR SWIA200414044Door · bindingMAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED DOOR, CLEANED AND REPLACED HARDWARE IAW 52-10-00.Nov 1, 2004 · N186SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200413896Rib · crackedLEFT WING AT RIB 8 WING TO WEB CLIP IS CRACKED. ITEM FOUND AT C-CHECK. REPLACED SUPPORT BRACKET IAW SRM 51-25-00, 51-40-00.Jul 16, 2004 · N186SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200413313Power Supply · malfunctionedREAR HALF OF EMERGENCY FLOOR LIGHTING STRIPS ARE NOT WORKING. REMOVED AND REPLACED NR 4 POWER SUPPLY IAW 33-50-00. OPS CHECK GOOD. P/N: D366-04-001, S/N ON: 1204, S/N OFF: 1209.May 10, 2004 · N186SW · Emb EMB120ER · Emergency LightingSDR SWIA200413009Control Unit · malfunctionedDURING TAKEOFF RUN JUST AFTER POWER UP, A SINGLE CHIME WITH FLAP, CONTROL FAULT, ADVANCED SWS. PERFORMED THE ABORT AND RETURNED TO THE GATE. RERACKED FLAP CONTROL UNIT PER MAINT MM 22-50-06. CYCLED POWER, PERFORMED HIGH SPEED TAXI WITH CREW. OPS CHECK GOODMar 8, 2004 · N186SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200412948Annunciator · malfunctionedFLAP FAULTS INTERMITTENTLY IN AIR AND ON GROUND. REPLACED FLAP ANNUNCIATOR. OPS CHECKED GOOD.Feb 20, 2004 · N186SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200412837Panel · crackedSTRINGER ON LT WING FORWARD OF NR 2 FUEL PANEL CRACKED. DISCOVERED DURING LINE INSPECTION. REPAIRED LEFT WING FORWARD STRINGER AT NR 2 FUEL PANEL IAW SRM 120 57-20-03 PG 205 TO 211, FIG 202 & IAW RII CARD 28-301.Jan 26, 2004 · N186SW · Emb EMB120ER · Wing, Plate/SkinSDR SWIA200312108Roller · bindingOUTBOARD FLAP DISAGREEMENT DURING FLAP RETRACTION. RESET BY SLOWING TO APPROX 140 AND RESETTING LEVER. FOUND RIGHT OUTBOARD FLAP LOWER MOVEABLE CHANNEL MISSING ROLLER AND FLAP WAS BINDING. INSTALLED NEW ROLLER AND SUPPORT BRACKET IAW MM 57-52-00. OPS CHECJun 18, 2003 · N186SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200311938Switch · out of positionHYDRAULIC LOCK ON MAIN CABIN DOOR WITH OCCASIONAL FORWARD ACTUATOR LIGHT ON OVERHEAD PANEL. PERFORMED QRH PROCEDURE AND THE DOOR OPENED. REPOSITIONED SWITCH IN HOUSING. TESTED AND DOOR WORKS OK. WORK PERFORMED IAW EMB MM 52-12-00.Apr 29, 2003 · N186SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200311765Indicator · malfunctionedON DEPARTURE FROM SLC, WHEN CLIMB POWER WAS SET 84 PERCENT TORQUE THE RIGHT TORQUE GUAGE FLUCTUATED, BOTH ANALOG AND DIGITAL. ALL OTHER ENGINE PARAMETER STAYED STABILIZED. FLUCTUATIONS WERE FROM 84 PERCENT TO APPROXIMATELY 50 PERCENT. REMOVED AND REPLACED RJan 28, 2003 · N186SW · Emb EMB120ER · Engine BMEP/Torque IndicatingSDR SWIA200211499Battery · dischargedEMERGENCY LIGHTS INOPERATIVE, INSTALLED SERVICEABLE EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD.Nov 18, 2002 · N186SW · Emb EMB120ER · Emergency LightingSDR SWIA200211184Hydraulic Line · crackedDURING APPROACH, EXPERIENCED LOSS OF HYDRAULIC FLUID IN BLUE SYSTEM. FOLLOWED QRH, LANDED UNEVENTFULLY. FOUND CRACKED LINE IN RIGHT NACELLE. REMOVED AND REPLACED LINE. RAN ENGINES. LEAK CHECK GOOD.Aug 29, 2002 · N186SW · Emb EMB120ER · Hydraulic System, MainSDR SWIA200211171Frame · crackedFOUND DURING C-CHECK, RIGHT NACELLE FRAME -0- HAS SEVERAL CRACKS IN IT. REMOVED AND REPLACED FRAME -0- IAW SRM 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211170Intercostal · crackedFOUND DURING C-CHECK, INTERCOSTAL AFT OF PILOT'S SIDE WINDOW CRACKED. FABRICATED AND INSTALLED DOUBLER TO PART IAW EMB SRM 51-00-00 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200211169Frame · crackedFOUND DURING C-CHECK, RIGHT NACELLE FRAME NR 1 CRACKED. ACCOMPLISHED EMB S/B 120-54-0036 REV 2. C/W PART 1-2.2.1, 2.2.2.1 THROUGH 2.2.3.8 & PART 2-2.3.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211168Frame · crackedFOUND DURING C-CHECK, LEFT NACELLE FRAME ONE IS CRACKED AT THE I/B TORSION MOUNT. COMPLIED WITH S/B 120-54-0036 REV 2 NACELLES - INSPECTION/REPLACEMENT OF NACELLE FRAME ONE.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211167Bracket · crackedFOUND DURING C-CHECK, AT FRAME 13, THE BRACKET THAT HOLDS THE POWER POSITION PULLEY QUADRANT, RT NACELLE, I/B SIDE IS CRACKED. REMOVED AND REPLACED THE CRACKED BRACKET AT FRAME 13, RT NACELLE IAW EMB SRM 51-00-00 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon Miscellaneous StructureSDR SWIA200211166Frame · crackedFOUND DURING C-CHECK, RIGHT SIDE NACELLE O/B SIDE FRAME 15 CRACKED. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EMB SRM 51-00-00 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211165Frame · crackedFOUND DURING C-CHECK, RIGHT NACELLE I/B SIDE FRAME 16 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211164Frame · crackedFOUND DURING C-CHECK, LEFT NACELLE I/B SIDE FRAME 15 CRACKED. STOP-DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 51-70-05.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211163Frame · crackedFOUND DURING C-CHECK, LEFT NACELLE O/B SIDE FRAME 17 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211162Frame · crackedC-CHECK, LT NACELLE O/B SIDE FRAME 15 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05 AND 51-40-02.Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR SWIA200211161Bushing · corrodedDURING C-CHECK, RIGHT AILERON TRIM TAB BUSHINGS AND HARDWARE ARE CORRODED. REMOVED AND REPLACED RIGHT AILERON TRIM TAB BUSHINGS AND HARDWARE IAW 57-60-00.Jul 19, 2002 · N186SW · Emb EMB120ER · Aileron TabsSDR SWIA200211160Bushing · corrodedDISCOVERED DURING C-CHECK, LEFT AILERON TRIM TAB BUSHINGS AND HARDWARE ARE CORRODED. REMOVED AND REPLACED LEFT AILERON TRIM TAB BUSHINGS AND HARDWARE IAW 57-60-00.Jul 19, 2002 · N186SW · Emb EMB120ER · Aileron TabsSDR SWIA200211159Seat Track · corrodedDISCOVERED DURING C-CHECK, LEFT AND RIGHT FWD FLOOR SEAT TRACKS ARE CORRODED. REMOVED AND REPLACED LEFT AND RIGHT FWD FLOOR SEAT TRACKS IAW 53-01-05.Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200211158Seat Track · corrodedDISCOVERED DURING C-CHECK, LEFT AND RIGHT FWD AND AFT WALL SEAT TRACKS ARE CORRODED. REMOVED AND REPLACED LEFT AND RIGHT FWD AND AFT WALL SEAT TRACKS IAW 53-01-05.Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200211157Cable · corrodedDURING C-CHECK, FOUND CABLES AND PULLEYS ON CARGO DOOR CORRODED. REMOVED AND REPLACED CABLES AND PULLEYS IAW 52-31-00.Jul 19, 2002 · N186SW · Emb EMB120ER · Cargo/Baggage DoorsSDR SWIA200211156Antenna · corrodedDURING C-CHECK FOUND SEVERAL LOWER FUSELAGE ANTENNAS WITH CORROSION: MKR 1/TDR 1/ DME 2/ RADAR ALT/ TDR 2. REPLACED DME AND MARKER BEACON ANTENNAS. FUNCTION CHECKED FOLLOWING SYSTEM: DME 1 & 2 IAW 34-51-00, ATC 1 & 2 IAW 34-52-00, MARKER BEACON 1 & 2 IAW 3Jul 19, 2002 · N186SW · Emb EMB120ER · DME/TACAN SystemSDR SWIA200211033Connector · faultyAFTER TAKEOFF AT 100 AGL, RECEIVED AN AURAL OIL WITH TRIPLE CHIME. NO ASSOCIATED MAP WARNINGS AND NO ENGINE PARAMETERS TO SUPPORT THE WARNING. ALARM WAS CONTINUOUS AND COULD NOT BE CANCELLED. RETURNED TO SLC. REMOVED AND REPLACED OIL PRESSURE TRANSDUCER CAJul 4, 2002 · N186SW · Emb EMB120ER · Engine Oil PressureSDR SWIA200211012Actuator · failedFLAP CONTROL FAULT INDICATION WITHOUT SELECTING ANY FLAP SETTINGS. LEFT OUTBOARD FLAP ACTUATOR FAILED THE OHM TEST. REMOVED AND REPLACED ACTUATOR ON LEFT OUTBOARD FLAP IAW 27-50-00.Jul 3, 2002 · N186SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200210995Cover · out of positionABORTED TAKEOFF WHEN LEFT ENGINE FEATHERED ON TAKEOFF ROLL. INSPECTED AND FOUND SWITCH COVER FOR LEFT ENGINE ELECT FEATHER INTERFERING WITH THE SWITCH. REPOSITIONED SWITCH COVER AND ENSURED CLEARANCE ON SWITCH. PERFORMED EXTENSIVE GROUND RUNS WITH NO FURTHEJun 27, 2002 · N186SW · Emb EMB120ER · Propeller Feathering/ReversingSDR SWIA200210981Headset · shortedELECTRICAL BURNING SMELL IN CABIN ASSOCIATED WITH TWO FLASHING CABIN PASSENGER LIGHTS ON CAPTAIN'S SIDE. REMOVED AND REPLACED FLIGHT ATTENDANT'S HANDSET IAW MM 23-41-01. OPS CHECKS GOOD.Jun 24, 2002 · N186SW · Emb EMB120ER · Interphone/Passenger Announcement (PA) SystemSDR SWIA200210625Switch · looseFORWARD CABIN DOOR LIGHT ON TAKEOFF. ABORTED TAKEOFF. INSPECTED/RECYCLED DOOR. LIGHT DID NOT ILLUMINATE AGAIN. FOUND UPPER MICRO SWITCH LOOSE. ADJUSTED SWITCH AND SECURED. OPS CHECKS GOOD.Jan 24, 2002 · N186SW · Emb EMB120ER · Door Warning SystemSDR SWIA200210596Switch · looseFORWARD DOOR WARNING LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. CYCLED DOOR AS PER MX CONTROL. DOOR LIGHT EXTINGUISHED. FORWARD DOOR WARNING LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF. INSPECTED FORWARD DOOR INDICATION SYSTEM. WORKING NORMALLY, NO Jan 22, 2002 · N186SW · Emb EMB120ER · Door Warning SystemSDR SWIA200110401Boot · damagedLEFT AND RIGHT MIDDLE WING DEICE BOOTS LIGHTS CAME ON IN CLIMB.PATCHED HOLE IN LEFT MIDDLE WING DEICE BOOT IAW CMM.Nov 29, 2001 · N186SW · Emb EMB120ER · Airfoil Anti/De-ice SystemSDR SWIA200110343Battery Pack · dischargedTHREE CONSECUTIVE WHITE EMERGENCY LIGHTS (ROW 3-6), 1 RED FLOOR EMERGENCY LIGHT OUT AT ROW 6, 4 EXIT SIGNS AT ROW 6 OUT, 2 OVERHEAD WHITE EXIT LIGHTS OUT AT ROW 6. INSTALLED SERVICEABLE ELBP IN MID EMERGENCY LIGHT SECTION IAW MM 33-50-00. CHECKS GOOD.Nov 2, 2001 · N186SW · Emb EMB120ER · Emergency LightingSDR SWIA972456Actuator · failedFLAP CONTROL FAULT ON TAXI OUT. COULD NOT RESET. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW 27-50-09. OPS AND LEAK CHECK GOOD. P/N ON 320300-1007, S/N ON 1093, S/N OFF 1146.Mar 26, 2001 · N186SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA972455Actuator · faultyINTERMITTENT CONTROL FAULT FOR ALMOST THE ENTIRE FLIGHT, OUTBOARD FLAP INDICATING FLASHING. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR PER MM 27-50-09 AND RII 27-307. OPS CHECKS GOOD, NO LEAKS. P/N ON 320300-1007, S/N ON 0864, S/N OFF 0552.Mar 25, 2001 · N186SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA971939Flap · malfunctionedFLAP CONTROL DID NOT RESET. DIVERTED TO SFO. FLAP 0 DEG LANDING. CHECKED THE RESISTANCE BETWEEN PIN G AND D AND E AS PER FAULT ISOLATION MANUAL 27-50-00 ON BOTH OUTBOARD FLAP ACTUATORS. FOUND THE RESISTANCE WITHIN LIMITS. PERFORMED FUNCTIONAL CHECK SEVERAAug 19, 2000 · N186SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA971885Warning System · false activationON TAKEOFF ROLL, RECEIVED TAKEOFF AUTO FEATHER AURAL WARNING. ABORTED, VERIFIED SWITCH POSITION ON, NO CBS POPPED. REMOVED AND REPLACED AUTO FEATHER ON/OFF SWITCH MM 615320, RAN BOTH ENGINES, PERFORMED POWER RUNS AND AUTO FEATHER TEST CHECKS GOOD. P/N 8856KJul 18, 2000 · N186SW · Emb EMB120ER · Propeller Feathering/ReversingSDR SWIA971748Switch · dirtyAFTER DEPARTURE FROM SLC, RECEIVED LANDING GEAR AURAL WARNING AND RED LIGHT ON MAP ALARM, WOULD NOT CANCEL. RETURNED TO SLC. CLEANED POWER LEVER MICRO SWITCHES AS REQUIRED, OPS CHECKS GOOD.Mar 31, 2000 · N186SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA971713Harness · malfunctionedRIGHT A SYSTEM GEAR LIGHT WOULD NOT EXTINGUISH, ON RETRACTION THE GEAR WOULD NOT COME DOWN, HAD TO USE ELECTRIC OVERRIDE SWITCH. REMOVED AND REPLACED RIGHT MLG A SYSTEM WIRING HARNESS PER MM 326101, CYCLED GEAR.Feb 26, 2000 · N186SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA971159Prox Sensor · malfunctionedLEFT MAIN LANDING GEAR DOES NOT INDICATE GREEN WHEN SELECTED DOWN. REPAIRED LEFT A SYSTEM DOWN LOCK PROX SENSOR IAW MM 32-61-01. OPS CHECKS GOOD.Apr 4, 1998 · N186SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA971085Sensor · failedRIGHT MAIN GEAR IGNITION A GREEN LIGHT ON IN FLIGHT. GEAR WOULD NOT EXTEND NORMALLY SO USED EMERGENCY OVERRIDE TO EXTEND. REPLACED RIGHT MAIN A SYSTEM DOWN LOCK SENSOR PER MM 32-60-00. LANDING GEAR FUNCTIONAL CHECKS GOOD.Feb 23, 1998 · N186SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA971093Doors · iced upRIGHT MAIN LANDING FAILED TO EXTEND UPON DOWN SELECTIONS. RIGHT MAIN WOULD ALSO NOT EXTEND DURING EMERGENCY EXTENSION PROCEDURE. INDICATIONS IN BOTH CASES, 2 RED TRANSIT LIGHTS ONLY ON RIGHT MAIN. RIGHT EVENTUALLY EXTENDED DURING A NORMAL SELECTION CYCLE. Feb 4, 1998 · N186SW · Emb EMB120ER · Landing Gear Door Retract SectionSDR SWIA971075Oil Syst · reqd serviceMOMENTARY LOW OIL PRESSURE INDICATION ON LEFT ENGINE ON CLIMB-OUT. RETURNED TO TWF. SERVICED OIL TO THE ADD 1 QUART MARK ON SIGHT GLASS. CHECKED ENGINE FOR OIL LEAKS BUT NONE WERE NOTED. GROUND RUN CHECKS GOOD WITH NO LEAKS.Jan 8, 1998 · N186SW · Emb EMB120ER · Turbine Engine Oil SystemSDR SWIA971069Oil Syst · reqd serviceAFTER DEPARTURE FROM EKO, HAD A INTERMITTENT LOW OIL PRESSURE INDICATION ON LEFT ENGINE. RETURNED TO EKO. ADDED TWO QUARTS OF EXXON 2380 OIL TO LEFT ENGINE PER INSTRUCTIONS FROM MAINTENANCE CONTROL. AIRCRAFT WAS RUN UP TO 100 PERCENT ENGINE INSTRUMENTS SHOWJan 8, 1998 · N186SW · Emb EMB120ER · Turbine Engine Oil SystemSDR SWIA971061Stringer · corrodedCORROSION FOUND AT PASSENGER ENTRY AREA BELOW FORWARD AND AFT DOOR ACTUATORS, STRINGER 17. REMOVED AND REPLACED STRINGER 17 BELOW CABIN DOOR OPENING, IAW SRM 51-40-02.Dec 5, 1997 · N186SW · Emb EMB120ER · Fuselage Main, Longeron/Stringer
Back to N186SW, cancelled Feb 21, 2006