# Service difficulty reports: N233SW A list on [N233SW](https://openairdocs.org/aircraft/N233SW.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 4 · 155 reports - [SDR HKGA20210307001](https://openairdocs.org/sdr/HKGA20210307001.md): Buss · failed · Mar 6, 2021 · N233SW · Emb EMB120ER · DC Power Distribution System > EMPTY LEG REPOSITION FLIGHT FROM KYIP TO KCAK. CLIMBING THROUGH 14,000' AFTER DEPARTING KYIP THE EMERGENCY DC BUS #2 FAILED. EMERGENCY WAS DECLARED WITH ATC AND CREW REQUESTED DIVERSION BACK TO KYIP. LANDING GEAR COLLAPSED UPON LANDING AND AIRCRAFT EXITED THE - [SDR HKGA20190620040](https://openairdocs.org/sdr/HKGA20190620040.md): Cowling · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Plate/Skin > FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER (PER EMB120 SRM 51-40-04 REV 58 AND ETD 2019-120-067917). INSTALLED REPAIR DOUBLER (PER EMB120 SRM 51-40-02 REV 58 AND ETC 2019-120-067917). PN: 120-37974-001 RH INTERMEDIATE COWL SHIM - [SDR HKGA201906260039](https://openairdocs.org/sdr/HKGA201906260039.md): Skin · damaged · Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Plate/Skin > CUT REPLACEMENT INNER PAN REPAIR SECTION (PER ETD 2019-120-050341). MATCH DRILLED AND TRIMMED DOUBLER REPAIR (IAW EMB120 ETD 2019-120-050341 REV A). INSTALLED REPAIR (PER EMB120 ETD 2019-120-050341 REV A). PN: 120-25601-029 DOOR SKIN, 120-25601-005 INNER SKI - [SDR HKGA20190626038](https://openairdocs.org/sdr/HKGA20190626038.md): Panel · chafed · Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Main Frame > PANEL CHAFED. REMOVED DAMAGED SEAL RING, MATCH DRILLED NEW PART, INSTALLED NEW SEAL RING (REF. EMB120 SRM 51-40-02 REV 58, EMB120 SRM 51-25-00 REV 58, EMB120 SRM 51-40-02 REV 58). LOCATED AND DRILLED NEW PNL 429AT (PER EMB120 SRM 51-40-04 REV 58). - [SDR HKGA201906260037](https://openairdocs.org/sdr/HKGA201906260037.md): Support Channel · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Main Frame > SUPPORT CHANNEL CRACKED. MATCH DRILLED NEW HALF FRAME TO COWLING STRUCTURE IAW SRM 51-25-00 REV 58. MATCH DRILLED LATCH PIN GUIDE ASSY'S AND DOOR HOLD OPEN ROD PINS AND INSTALLED ON NEW HALF FRAME IAW AMM 20-10-01-2, REV 43, SRM 51-40-02-PR, AND 51-25-00-PR - [SDR HKGA201906260036](https://openairdocs.org/sdr/HKGA201906260036.md): Skin · damaged · Jun 20, 2019 · N233SW · Emb EMB120ER · Aerodynamic Fairings > TAILCONE SKIN DAMAGED. FABRICATED A DOUBLER AND MATCH DRILLED REPAIR PARTS IAW ETD 209-120-046706, AND SRM 53-31-17, REV 58. INSTALLED THE REPAIRED DOUBLER AND FILLER IAW ETD 2019-120-046706, REV A. - [SDR HKGA201906260035](https://openairdocs.org/sdr/HKGA201906260035.md): Shear Tie · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Internal Mounting Structure > SHEAR TIE CRACKED AT FRAME 16, STRINGER 15R. FABRICATED A NEW SUPPORT IAW DRAWING 120-09850 REV E AND SRM 51-30-01 REV 58. LOCATED AND MATCH DRILLED IAW SRM 51-40-04 REV 58. INSTALLED NEW SUPPORT / SHEAR TIE LESS FASTENERS THRU SKIN IAW SRM 51-40-02 REV 58. - [SDR HKGA201906260034](https://openairdocs.org/sdr/HKGA201906260034.md): Skin · gouged · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Plate/Skin > SKIN GOUGED BETWEEN FRAMES 39-40, STRINGERS 18-19L. FABRICATED A DOUBLER AND FILLER SHIM AND APPLIED ALODINE AND EPOXY PRIMER TO DOUBLER AND SHIM PARTS IAW SRM 50-00-01 REV 58. APPLIED EDGE SEAL AND TOP COAT IAW SRM 51-22-00. - [SDR HKGA201906260033](https://openairdocs.org/sdr/HKGA201906260033.md): Floorbeam · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Floor Beam > FLOORBEAM CORRODED. MATCH DRILLED BEAM CAP AND INSTALLED LT FLOOR BEAM UPPER SURFACE AND BRACKET, RIB IAW SRM 51-40-02 REV 58. APPLIED SURFACE PROTECTION IAW CPM 51-21-00 REV 10. - [SDR HKGA201906260032](https://openairdocs.org/sdr/HKGA201906260032.md): Floorbeam · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Floor Beam > FLOORBEAM CORRODED. MATCH DRILLED NEW BUTT STRAP AND INSTALLED BUTT STRAP IAW SRM 51-40-02 REV 58. - [SDR HKGA201906260031](https://openairdocs.org/sdr/HKGA201906260031.md): Pan · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Miscellaneous Structure > PAN CRACKED. INSTALLED REINFORCING ANGLE IAW SRM 52-10-02 REV 58. - [SDR HKGA20190626030](https://openairdocs.org/sdr/HKGA20190626030.md): Door · damaged · Jun 20, 2019 · N233SW · Emb EMB120ER · Doors > DOOR CHAFED. BLENDED CHAFFING IAW CPM 51-14-00. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED, PRIMED, AND APPLIED TOP COAT IAW COM 51-21-03 REV DATE 6/30/17. - [SDR HKGA201906260029](https://openairdocs.org/sdr/HKGA201906260029.md): Trunnion · damaged · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage, Landing Gear Attach Fittings > TRUNNION DAMAGED. INSTALLED A NEW LT MLG WELDED TRUNNION LUG ASSY IAW CMM 32-12-01 REV 15. - [SDR HKGA201906260028](https://openairdocs.org/sdr/HKGA201906260028.md): Plate · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Structure (General) > PLATE CRACKED. REMOVED DOOR STOP PLATE, MATCH DRILLED NEW PART AND INSTALLED IAW SRM 51-40-02, AND 51-25-00 REV 58. - [SDR HKGA201906260027](https://openairdocs.org/sdr/HKGA201906260027.md): Fitting · chafed · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Attach Fittings > FITTING CHAFED. BLENDED CHAFFING (IAW EMB120 CPM 51-14-00). - [SDR HKGA201906260026](https://openairdocs.org/sdr/HKGA201906260026.md): Shear Tie · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Wing Main, Frame Structure > RT WING SHEAR TIE CRACKED. MATCH DRILL NEW SHEAR CLIP IAW SRM 51-40-02 REV 58. INSTALLED CLIP WITH SEALANT IAW SRM 51-40-02 REV 58. APPLIED TOP COAT IAW CPM 51-21-06 REV 6/30/17. - [SDR HKGA201906260025](https://openairdocs.org/sdr/HKGA201906260025.md): Rib · chafed · Jun 20, 2019 · N233SW · Emb EMB120ER · Empennage Structure > RIB FLANGE CHAFED AND CORRODED. REMOVED CORROSION AND CHAFFING IAW CPM 51-14-00 REV DATE 6/30/17. MATCH DRILLED NEW LEADING EDGE RIB FLANGE IAW SBM 51-5-00 REV 58. INSTALLED THE RIB FLANGE IAW SRM 51-40-02 REV 58. APPLIED PRIMER AND TOP COAT IAW CPM 512106 R - [SDR HKGA201906260024](https://openairdocs.org/sdr/HKGA201906260024.md): Support · burned · Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Main Frame > FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW ETD 2019-120-045306 AND SRM 54-30-02 REV 58. - [SDR HKGA201906260023](https://openairdocs.org/sdr/HKGA201906260023.md): Flap · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Main Frame > FLAP CRACKED. R & R 18 FASTENERS PER EMB120 SRM 51-40-02 REV 58. - [SDR HKGA201906260022](https://openairdocs.org/sdr/HKGA201906260022.md): Doubler · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Passenger/Crew Doors > DOUBLER CRACKED. MATCH DRILLED AND INSTALLED NEW DOUBLER IAW SRM 54-30-01, REV 58. - [SDR HKGA201906260021](https://openairdocs.org/sdr/HKGA201906260021.md): Hinge Fitting · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Rudder Structure > RUDDER HINGE FITTING CORRODED. LOCATED AND DRILLED NEW HINGE FITTING IAW SRM 51-40-04 REV 58. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO HOLES IAW CRM 51-21-07 REV 4. - [SDR HKGA201906260020](https://openairdocs.org/sdr/HKGA201906260020.md): Trim Tab · rusted · Jun 20, 2019 · N233SW · Emb EMB120ER · Elevator, Tab Structure > LEFT ELEVATOR TRIM TAB CORRODED. R & R THE TRIM TAB OUTBOARD 2 HINGE FITTING IAW AMM 20-10-01-2 REV 43. - [SDR HKGA201906260016](https://openairdocs.org/sdr/HKGA201906260016.md): Support · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Miscellaneous Structure > SUPPORT CRACKED. REMOVED AND REPLACED THE SUPPORT AND MATCH DRILLED NEW SUPPORT IAW SRM 51-40-02 REV 58). - [SDR HKGA201906260015](https://openairdocs.org/sdr/HKGA201906260015.md): Shear Tie · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Internal Mounting Structure > REMOVED CRACKED SHEAR TIE AND MATCH DRILLED NEW SHEAR TIE IAW SRM 51-40-02, 51-25-00 REV 58. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 REV 58. TREATED AND APPLIED TOP COAT IAW CPM 51-21-04, REV 10. - [SDR HKGA201906260014](https://openairdocs.org/sdr/HKGA201906260014.md): Shear Tie · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Internal Mounting Structure > REMOVED CRACKED SHEAR TIE AND MATCH DRILLED NEW SHEAR TIE IAW SRM 51-40-02, 51-25-00 REV 58. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 REV 58. TREATED AND APPLIED TOP COAT IAW CPM 51-21-04 REV 10. - [SDR HKGA201906250019](https://openairdocs.org/sdr/HKGA201906250019.md): Doubler · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Empennage Structure > DOUBLER CORROED. MATCH DRILLED REPAIR PARTS IAW SRM 51-70-04, AND 51-40-02, REV 58. INSTALLED DOUBLER AND FILLER IAW STEP 2 OF ETD 2019-120-055992 AND SRM 51-40-02, REV 58. REMOVED REPAIRED DOUBLER IAW SRM 51-40-02, REV 58, CONFIRMED AFFECTED AREA CRACK FR - [SDR HKGA201906250018](https://openairdocs.org/sdr/HKGA201906250018.md): Cover · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Rudder Structure > RUDDER HINGE COVER CORROED. CLEANED, PREPARED A NEW UPPER HINGE PANEL AND APPLIED PRIMER IAW CPM 51-21-04, AND 51-21-05. APPLIED TOP COAT IAW CPM 51-21-06. - [SDR HKGA201906250017](https://openairdocs.org/sdr/HKGA201906250017.md): Bearing · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Rudder Structure > RUDDER HINGE BEARING CORRODED. R & R THE RUDDER LOWER HINGE BEARING IAW MM 20-40-03, REV 43. - [SDR HKGA201906250013](https://openairdocs.org/sdr/HKGA201906250013.md): Shear Tie · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Internal Mounting Structure > SHEAR TIE FOUND DAMAGED. REMOVED AND REPLACED THE DAMAGED SHEAR TIE IAW SRM 51-40-02, REV 58. TREATED, PRIMED AND APPLIED TOP COAT TO FASTENERS IAW CPM 51-21-04 REV 10. - [SDR HKGA201906250012](https://openairdocs.org/sdr/HKGA201906250012.md): Shear Tie · cracked · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Internal Mounting Structure > SHEAR TIE CRACKED AT FRAME 44, BETWEEN STRINGERS 1 & 2. REMOVED AND REPLACED THE DAMAGED SHEAR TIE IAW SPM 51-40-02. TREATED AND APPLIED TOP COAT TO FASTENERS IAW CPM 51-21-04 REV 10. - [SDR HKGA201906250009](https://openairdocs.org/sdr/HKGA201906250009.md): Door · chafed · Jun 20, 2019 · N233SW · Emb EMB120ER · Emergency Exits > OVERWING EXIT WAS CHAFED. REMOVED CHAFE DAMAGE IAW CPM 51-14-00. TREATED, PRIMED AND APPLIED TOP COAT TO AFFECTED AREA IAW CPM 51-21-04. - [SDR HKGA201906250011](https://openairdocs.org/sdr/HKGA201906250011.md): Intercostal · damaged · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Miscellaneous Structure > INTERCOSTAL DAMAGED, REMOVED DAMAGE IAW EPM 51-14-00. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED AND PRIMED AFFECTED AREA IAW CPM 51-21-04. - [SDR HKGA201906240010](https://openairdocs.org/sdr/HKGA201906240010.md): Frame · damaged · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Frame > REMOVED DAMAGED FRAME AND MATCH DRILLED NEW FRAME IAW SRM 51-40-02 REV 58. INSTALLED A NEW FRAME 30 SEGMENT IAW SRM 51-40-02 REV 58. - [SDR HKGA201906250006](https://openairdocs.org/sdr/HKGA201906250006.md): Frame · gouged · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Frame > REMOVED DAMAGED AREA ON FRAME 35 BETWEEN STRINGERS 3 AND 4R IAW SRM 51-40-02, AND 53-00-04, REV 58. INSTALLED A REPAIRED DOUBLER IAW SRM 53-00-04, REV 58. - [SDR HKGA201906250008](https://openairdocs.org/sdr/HKGA201906250008.md): Frame · gouged · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Frame > BLENDED A GOUGE ON THE AFT SIDE OF FRAME 19 IAW CPM 51-14-02 REV 10. CONFIRMED CRACK FREE IN AFFECTED AREA IAW NDIM 51-00-03 REV 3. TREATED AND PRIMED AFFECTED AREA IAW CPM 51-21-04 REV 4. - [SDR HKGA201906250007](https://openairdocs.org/sdr/HKGA201906250007.md): Skin · dented · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Plate/Skin > REWORKED DENT IAW SRM 51-7400 REV 58. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED, PRIMED, AND APPLIED TOPCOAT IAW CPM 51-21-04 REV 10. - [SDR HKGA201906250005](https://openairdocs.org/sdr/HKGA201906250005.md): Shear Tie · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Internal Mounting Structure > SHEAR TIE CORROED. REMOVED FR 19 SEGMENT FROM STR 1R-15R AND 2 DOUBLERS IAW SRM 51-40-02 REV 58. INSTALLED NEW FRAME AND 2 DOUBLERS IAW SRM 51-40-02 REV 08. - [SDR HKGA201906240004](https://openairdocs.org/sdr/HKGA201906240004.md): Cover Plate · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Miscellaneous Structure > REMOVAL AND INSTALLATION OF CARGO DOOR THRESHOLD COVER PLATE COMPLETE (PER ETD 2019-120-062528). PN: 120-16200-001 LOWER CARGO DOOR BEAM - [SDR HKGA201906240003](https://openairdocs.org/sdr/HKGA201906240003.md): Floorbeam · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Floor Panel > FLOOR BEAM SEGMENT CORRODED. INSTALLED A NEW FLOOR BEAM SEGMENT IAW SRM 51-40-02 REV 58. - [SDR HKGA201906240002](https://openairdocs.org/sdr/HKGA201906240002.md): Floor Support · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Miscellaneous Structure > REMOVED FLOOR BEAM UPPER SURFACE (REF. SRM 51-25-00). INSTALLED NEW FLOOR BEAM AT FRAMES 17 - 18 (REF. SRM 51-40-02 REV 58). PN: 120-05805-603 BUTT STRAP REPLACES 120-05805-003 - [SDR HKGA201906240001](https://openairdocs.org/sdr/HKGA201906240001.md): Floor Support · corroded · Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Miscellaneous Structure > UPPER SURFACE OF LH FLOOR BOARD ATTACH ANGLE BETWEEN FRAMES 15A - 16A WAS FOUND TO HAVE CORROSION. REMOVED FLOOR SILL (REF. SRM 51-40-02 REV 58). INSTALLED NEW FLOOR SILL (REF. SRM 51-40-02 REV 58). PN: 120-05802-001 SILL - [SDR HKGA201807274003](https://openairdocs.org/sdr/HKGA201807274003.md): Relay · burned · Jul 24, 2018 · N233SW · Emb EMB120ER · Pitot/Static Anti-Ice System > IN CRUISE, PILOT NOTICED A SMELL LIKE BURNING WIRE AND SMOKE WAS VISIBLE IN THE COCKPIT. DE-ICE LIGHT FAIL INDICATION ILLUMINATED AND THE NR 2 PITOT STATIC CIRCUIT BREAKER POPPED. AIRCRAFT DIVERTED TO THE NEAREST AIRPORT AND LANDED WITHOUT INCIDENT. MX TROUBLE - [SDR SWIA201439884](https://openairdocs.org/sdr/SWIA201439884.md): Ahrs · inoperative · Nov 9, 2014 · N233SW · Emb EMB120ER · Attitude and Direction Data System > DIVERTED TO PSP WITH AN ATTITUDE DISPLAY LIGHT THAT ILLUMINATED FOLLOWED BY F/O ATTITUDE INDICATOR TUMBLING. HEADING FLAG DISPLAYED, AUTOPILOT AND FLIGHT DIRECTOR INOPERATOR. R & R FOS AHRS. - [SDR SWIA201438858](https://openairdocs.org/sdr/SWIA201438858.md): Handle · failed · Jul 24, 2014 · N233SW · Emb EMB120ER · Landing Gear Selector > GEAR WARNING AT 900 DURING LANDING. REPLACED GEAR HANDLE ASSEMBLY AND MLG CONTROL MODULE. - [SDR SWIA201438003](https://openairdocs.org/sdr/SWIA201438003.md): Switch · dirty · Jun 6, 2014 · N233SW · Emb EMB120ER · Landing Gear Position and Warning > WHEN THE GEAR WAS EXTENDED ALL GEAR LIGHTS WERE IN THE GREEN. RECEIVED A GEAR WARNING LIGHT. AFTER LANDING ALL GEAR DOORS WERE FOUND OPEN. CLEANED MICROSWITCHES ON POWER LEVERS AND LUBED THE SELECTOR VALVES, OPS CHECKED GOOD. - [SDR SWIA201437349](https://openairdocs.org/sdr/SWIA201437349.md): Sign · unsecure · May 3, 2014 · N233SW · Emb EMB120ER · Emergency Lighting > EMERGENCY EXIT SIGN AT 9C NOT SECURE. RESECURED EXIT SIGN. - [SDR SWIA201437291](https://openairdocs.org/sdr/SWIA201437291.md): Actuator · failed · Apr 23, 2014 · N233SW · Emb EMB120ER · Landing Gear Retraction/Extension System > DURING GEAR RETRACTION, LEFT MAIN GEAR DISAGREEMENT LIGHT WOULDN'T EXTINGUISH. CYCLED GEAR, LIGHT WENT OUT. PASSED FUNCTIONAL FLIGHT. R & R LT MLG UPLOCK - UNLOCKING ACTUATOR AND ADJUSTED UPLOCK LINK IAW AMM. - [SDR SWIA201437249](https://openairdocs.org/sdr/SWIA201437249.md): Control Module · failed · Apr 22, 2014 · N233SW · Emb EMB120ER · Landing Gear Retraction/Extension System > AFTER TAKEOFF, RETRACTED LANDING GEAR AND HAD A LT MAIN GEAR DISAGREEMENT. RAN QRH AND GEAR RETRACTED NORMALLY. R & R LANDING GEAR RELAY BOX AND REPLACED LANDING GEAR CONTROL MODULE IAW AMM. CHECKED GAPS OF LT MLG DOWNLOCK PROXIMITY SENSORS IAW AMM. CYCLED - [SDR SWIA201436775](https://openairdocs.org/sdr/SWIA201436775.md): Actuator · failed · Mar 15, 2014 · N233SW · Emb EMB120ER · Landing Gear Actuator > LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. RECEIVED LT MAIN GEAR DISAGREE LIGHTS. REPLACED LT MLG ACTUATOR AND REPLACED LT MLG RETRACT ACTUATOR ROD, BRACKET AND ATTACH PIN IAW AMM AND CMM. - [SDR SWIA201436459](https://openairdocs.org/sdr/SWIA201436459.md): Structure · cracked · Feb 9, 2014 · N233SW · Emb EMB120ER · Fuselage Miscellaneous Structure > SHEET METAL CRACKED IN BOTH AFT CORNERS UNDER OBSERVER SEAT AREA. C CHECK INSTALLED DOUBLERS TO LT & RT CORNER CLIPS BELOW OBSERVERS SEAT IAW SRM. Next page: https://openairdocs.org/aircraft/N233SW/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 = 'N233SW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N233SW/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.