N229SW

Service difficulty reports · 119

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 = 'N229SW' AND registry_match = 'registration'
  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 SWIA200210677Web · crackedNACELLE WEB ON INBOARD RIGHT NACELLE CRACKED. INSTALLED NEW INBOARD FITTING AFT OF FRAME 13 AT NACELLE STATION 2425, SRM 51-10-02 AND 51-40-02.Jan 12, 2002 · N229SW · Emb EMB120ER · Nacelle/Pylon, Main FrameSDR SWIA200210676Clip · crackedFRAME 9 SKIN CLIP CRACKED ON COPILOT'S SIDE.Jan 12, 2002 · N229SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200210547Comparator · faultyDURING FLIGHT, ATT DISPLAY ON MAP CAME ON. A/P DISCONNECTED, GYRO AND COMPUTER FLAGS ON COPILOT'S ADI, HDG FLAG ON COPILOT'S HSI. AFTER A/P DISCONNECT FLAGS WENT AWAY, BUT DURING TURNS F/O'S ATT IND STAYED STRAIGHT AND LVL. F/O COMMAND BARS SHOW BELOW AIRPLJan 5, 2002 · N229SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA200210540Comparator · failedF/O ADI WON'T DISPLAY A/C ATT TURNING GAUGES GYRO, COMP AND HDG FLAGS. REPLACED NR 2 AHC85 WITH SERVICEABLE UNIT. OPS CHECK GOOD ON TAXI. S/N OFF: 2731.Jan 5, 2002 · N229SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA200110440Warning System · false activationABORTED TAKEOFF DUE TO TAKEOFF AURAL WARNING. AURAL WARNING CB FOUND POPPED. COMPLIED WITH TEST OF AURAL WARNING UNIT PER EMB MM 31-53-00. OPS CHECK GOOD AT THIS TIME.Dec 12, 2001 · N229SW · Emb EMB120ER · Central WarningSDR SWIA972616Actuator · failedWHEN FLAPS WERE SELECTED TO 15 DEGREES ON APPROACH, FLAP DISAGREEMENT WAS NOTED FOLLOWED BY LOSS OF BLUE HYDRAULIC SYSTEM. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-00. OPS AND LEAK CHECK GOOD. SERVICED BLUE HYDRAULIC RESERVOIR AND CHECKED HJun 4, 2001 · N229SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA972524Boot · failedOVER VTU IN ICING CONDITIONS, BOTH ENGINE DEICE BOOTS FAILED. RECYCLED SWITCHES, LEFT ENGINE DEICE BOOT FAILED AND RIGHT ONE WORKED NORMALLY. RETURNED TO LAX. REPLACED LEFT ENGINE INLET DUCT WITH SERVICEABLE UNIT. S/N OFF 080 ON 213. RAN ENGINE, OPS CHECKApr 20, 2001 · N229SW · Emb EMB120ER · Air Intake Anti/De-Ice SystemSDR SWIA972429Computer · faultyAFTER TAKEOFF STALL WARNING LIGHT WITH ASSOCIATED TRIPLE CHIME WENT ON THEN OFF. REPEATED EVERY FEW MINUTES, BUT NO STALL WARNING PANEL LIGHT. REPLACED NUMBER TWO STALL WARNING COMPUTER WITH SERVICEABLE UNIT. ALSO, REPLACED STALL WARNING CONTROL PANEL WITH Mar 10, 2001 · N229SW · Emb EMB120ER · Stall Warning SystemSDR SWIA972368Actuator · failedDURING DESCENT, RUDDER REQUIRED FULL NOSE LEFT RUDDER TRIM TRAVEL TO STOP. RUDDER TRIM INEFFECTIVE. PERFORMED RUDDER ACT HEALTH CHECK, AND PCU CHECK IAW EMB 120 MM 27-22-00. FOUND GREEN RUDDER ACTUATOR TO FAIL. REMOVED AND REPLACED GREEN RUDDER ACTUATOR WIFeb 17, 2001 · N229SW · Emb EMB120ER · Rudder ActuatorSDR SWIA972366Control Box · malfunctionedUPON RETRACTION AFTER TAKEOFF ALL OF THE LANDING GEAR RED AND GREEN LIGHTS ILLUMINATE WITHOUT COMPLETING GEAR RETRACTION. WHEN RECYCLED, LANDING GEAR ONLY RETRACTS AFTER ABOUT A 5 SECOND DELAY AND EXTENDS NORMALLY. PERFORMED MULTIPLE GEAR SWINGS, COULD NOT DFeb 12, 2001 · N229SW · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR SWIA972279Latch · looseAT 90 KNOTS TAKEOFF ROLL, GOT DOOR WARNING ON MAP AND FLASHING MASTER WARNING. NO TRIPLE CHIME LIGHT WENT OFF ON DECELERATION. FOUND INBOARD FUEL SERVICE DOOR AFT CAMLOC TO BE LOOSE AND PUSHED THROUGH. REPLACED CAMLOC AND ADJUSTED SWITCH ON OUTBOARD FUEL SEJan 11, 2001 · N229SW · Emb EMB120ER · Fluid Service DoorsSDR SWIA972132Computer · failedINTERMITTENT HDG AND ATT FLAGS AND COMPUTER FLAG ATT INDICATOR WANDERING ON CAPTAINS SIDE. ABORTED TAKEOFF. REPLACED NUMBER ONE AHRS COMPUTER. OPS CHECK GOOD. P/N 622-6190-204, S/N 2746.Nov 19, 2000 · N229SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA971997Indicator · fluctuatesRIGHT ENGINE TORQUE GAUGE INDICATION FLUCTUATES WHILE VIBRATION FELT DURING CLIMBOUT. RETURNED TO SBA. INSTALLED SCU AND TORQUE PROBE IAW 61-23-00 AND 71-00-00. PERFORMED RUN TEST AND GROUND POWER TEST. OPS CHECKS GOOD. NO ABNORMAL VIBRATIONS FELT. (S/N Sep 25, 2000 · N229SW · Emb EMB120ER · Engine BMEP/Torque IndicatingSDR SWIA971833Light · inoperativeC-CHECK, CABIN EMERGENCY LIGHT ON RIGHT FORWARD EXIT BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT HAND OVERWING EMERGENCY EXIT WITH SERVICEABLE UNIT. OPS CHECK GOOD. (P/N 10130115) MR #24634.Jun 25, 2000 · N229SW · Emb EMB120ER · Emergency LightingSDR SWIA971672Engine · malfunctionedPULLING POWER BACK AT 6,000 FEET, TORQUE DROPPED AND AIRCRAFT YAWED. RETURNED TO SFO. PERFORMED POWER RUN ON LEFT ENGINE, ON GROUND AND COULD NOT DUPLICATE DISCREPANCY. DEFERRED LEFT EEC FOR TROUBLESHOOTING AS PER MEL 73211.Jan 27, 2000 · N229SW · Emb EMB120ER · Engine (Turbine/Turboprop)SDR SWIA971557Actuator · failedAFTER TAKEOFF IN CLIMB, RIGHT RUDDER LOCKED AND RESTRICTED IN FORWARD TRAVEL. RETURNED TO SAN. REPLACED BLUE HYDRAULIC SYSTEM RUDDER ACTUATOR PER MM 27-22-02. NO LEAKS NOTED.Sep 9, 1999 · N229SW · Emb EMB120ER · Rudder ActuatorSDR SWIA971565Tq Probe · failedDURING FLIGHT, RIGHT TORQUE FLUCTUATES FROM 64 PERCENTS DOWN TO 0 PERCENTS (ANALOG AND DIGITAL). RETURNED TO SFO. REPLACED RIGHT ENGINE TORQUE PROBE. OPS CHECKED GOOD ON ENGINE RUN.Sep 5, 1999 · N229SW · Emb EMB120ER · Engine BMEP/Torque IndicatingSDR SWIA971351Transducer · failedLEFT OIL PRESSURE DROPPED TO APPROXIMATELY 50 PSI AND STAYED IN YELLOW ARC. DIVERTED FROM MRY TO SBA. REPLACED LEFT OIL PRESSURE TRANSDUCER. PERFORMED RUNS AT ALL POWER SETTINGS, OPS AND LEAK CHECKS GOOD.Dec 25, 1998 · N229SW · Emb EMB120ER · Engine Oil PressureSDR SWIA95785Door Seal · looseCABIN WOULD NOT PRESSURIZE AND CABIN ALT REMAINED AT 10,000 THROUGH OUT CLIMB. RESECURED ELECTRO PNEUMATIC VALVE CLOSED AS PER MEL 21-30-01, GROUND RUN SHOWS MANUAL CHECKS GOOD. FOUND LOOSE SECTION OF CARGO DOOR SEAL. PRESSURIZED ACFT TO 5.0 PSID IN AUTO ANDec 1, 1996 · N229SW · Emb EMB120ER · Cargo/Baggage Doors
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