# Service difficulty reports: N830AE A list on [N830AE](https://openairdocs.org/aircraft/N830AE.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 2 · 94 reports - [SDR SIMA202001132006](https://openairdocs.org/sdr/SIMA202001132006.md): Light · inoperative · Jan 12, 2020 · N830AE · Emb EMB135KL · Emergency Lighting > MAIN DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED DOOR EMERGENCY LIGHT I.A.W EMB 140 AMM 33-50-10 OPS CHECK GOOD - [SDR SIMA201911297002](https://openairdocs.org/sdr/SIMA201911297002.md): Control Panel · failed · Nov 27, 2019 · N830AE · Emb EMB135KL · Elevator Tab Control System > PTCH TRIM BACK UP INOP DURING CRUSING. PITCH TRIM FAIL MSG. DECLARED EMERG. LANDED SAFELY-C/A-RAR PITCH TRIM CONTROL PANEL IAW EMB 140 AMM 20-13-10. OPC GOOD IAW EMB 140 AMM 27-40-00. NO DEFECTS NOTED. - [SDR SIMA201910286002](https://openairdocs.org/sdr/SIMA201910286002.md): Brake · unknown · Oct 26, 2019 · N830AE · Emb EMB135KL · Landing Gear Brake System > PARKING BRAKE IS NOT WORKING PROPERLY. DIFFICULTY SETTING IT-C/A-PERFORMED OPC OF PARKING EMERGENCY BRAKE IAW EMB 140 AMM 32-44-00. OPC GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. - [SDR SIMA201910232002](https://openairdocs.org/sdr/SIMA201910232002.md): None · none · Oct 22, 2019 · N830AE · Emb EMB135KL · Standard Practices/Structures > BIRD STRIKE ON T/O ROLL ON NOSE CONE AN 2 RH WING LEADING EDGE HIGH SPEED ABORT LESS THAN 110 KT-C/A-C/W BIRD STRIKE INSPECTION WORK CARD 05-200-07 NO DAMAGE NOTED OK FOR SERVICE - [SDR SIMA20190906001](https://openairdocs.org/sdr/SIMA20190906001.md): Battery · discharged · Sep 6, 2019 · N830AE · Emb EMB135KL · Emergency Equipment > AFT FLASHLIGHT INOP. C/A-REMOVED AND REPLACED AFT FLASHLIGHT BATTERY IAW CMM 25-60-11 OPC GOOD. - [SDR SIMA20190904002](https://openairdocs.org/sdr/SIMA20190904002.md): O-Ring · damaged · Sep 4, 2019 · N830AE · Emb EMB135KL · Pneumatic Distribution System > AT 19000 FT DURING ICE PROT PNEUMATIC TEST, BLD 2 LEAK / FA REPORTS LOUD BANG. QRH CLEARED MSG. C/A-REMOVED AND REPLACED RT BLEED JOINT NR 2 O-RING AND REASSEMBLED IAW AMM 36-11-10. - [SDR SIMA201908221003](https://openairdocs.org/sdr/SIMA201908221003.md): Control Unit · failed · Aug 21, 2019 · N830AE · Emb EMB135KL · Trailing Edge Flap Control System > FLAP FAIL ON EICAS CAUTION MESSAGE AFTER SELECTING FLAPS 9 FLAPS STAYED UP. RESET FLAPS SYSTEM IAW FIM TASK 27-51-00-810-801-A, RECEIVED FLAPS AT 9 DEGREES FOR FERRY FLIGHT PERFORMED GVI OF FLAPS NO DEFECTS NOTED. PERFORMED CMC DOWNLOAD IAW AMM 45-45-00, C - [SDR SIMA201908221004](https://openairdocs.org/sdr/SIMA201908221004.md): Warning Message · false activation · Aug 21, 2019 · N830AE · Emb EMB135KL · Trailing Edge Flap Control System > FLAP FAIL MSF WHEN SELECTING FLAPS 22. RESET SYSTEM C/W OPERATIONAL CHECK IAW E140 AMM 27-51-00-700-801-A. NO FAULTS FOUND. A/C OK FOR SERVICE - [SDR SIMA20190528001](https://openairdocs.org/sdr/SIMA20190528001.md): Flashlight · broken · May 28, 2019 · N830AE · Emb EMB135KL · Emergency Equipment > AFT CABIN CREW FLASHLIGHT BASE BROKEN. C/A-REMOVED AND REPLACED CABIN CREW FLASHLIGHT BASE IAW AMM 33-50-16. OPC GOOD. - [SDR SIMA201809054001](https://openairdocs.org/sdr/SIMA201809054001.md): Bleed Valve · malfunctioned · Sep 4, 2018 · N830AE · Emb EMB135KL · Compressor Bleed Valve > ADVISORY MESSAGE BLD 2 VLV CLOSED. REMOVED AND REPLACED ENGINE BLEED 2 VALVE IAW AMM 36-11-05. REMOVED AND REPLACED BLEED AIR NR 2 PUSHBUTTON IAW AMM 20-13-04. PERFORMED OPERATIONAL CHECK OF ENGINE NR 2 BLEED VALVE IAW AMM 36-11-05. ALL OPS NML AT THIS TIME. - [SDR SIMA20180628002](https://openairdocs.org/sdr/SIMA20180628002.md): Hydraulic Line · failed · Jun 28, 2018 · N830AE · Emb EMB135KL · Hydraulic System, Main > HYDRAULIC SYSTEM 1 LOW QUANTITY FOLLOWED BY A RAPID LOSS OF HYDRAULIC FLUID. TRANSFERRED HYDRAULIC FLUID FROM SYS 2 TO SYS 1 IAW ETN-EM-29-023R2. FOUND LT AND RT MLG RETRACT ACTUATOR RETRACT HOSES LEAKING. APPLIED TORQUE TO BOTH HOSES IAW AMM 32-33-08-400-801A - [SDR SIMA2018061108008](https://openairdocs.org/sdr/SIMA2018061108008.md): Selector · failed · Jun 8, 2018 · N830AE · Emb EMB135KL · Trailing Edge Flap Control System > FLAP INDICATION WHEN SET IN ANY POSITION. COMPLETED A FLAP FAIL CHECKLIST AND PERFORMED NO FLAP LANING. AFTER LANDING FLAPS INDICATED 0 IN FLAPS 22 POSITION. FLAPS UP OUTSIDE AIRCRAFT. REMOVED AND REPLACED THE FLAPS SELECTOR LEVER IAW AMM 27-53-03. COMPLI - [SDR SIMA20180130007](https://openairdocs.org/sdr/SIMA20180130007.md): Wire · broken · Jan 30, 2018 · N830AE · Emb EMB135KL · Light System Wiring > EMERGENCY LIGHT CONNECTOR HAS A BROKEN WIRE. REPAIRED THE WIRE IAW SWPM 20-00-03, AND 20-21-00. - [SDR SIMA20180130004](https://openairdocs.org/sdr/SIMA20180130004.md): Skin · cracked · Jan 30, 2018 · N830AE · Emb EMB135KL · Fuselage Main, Plate/Skin > FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 6 FASTENERS ON FR 78 RT SIDE BELOW VERTICAL STAB. REPAIRED FUSELAGE SKIN CRACKS ON 6 FASTENERS ON FR78 IAW ERS-EM-53MR-3087. - [SDR SIMA20180130002](https://openairdocs.org/sdr/SIMA20180130002.md): Frame · dented · Jan 30, 2018 · N830AE · Emb EMB135KL · Fuselage Main, Frame > DENT ON RT FWD FUSELAGE STRINGER 14R AFT OF RADOME. REPAIRED DENT ON RT FWD FUSELAGE STRINGER 14R AFT OF RADOME IAW ERS-EM-53MR-3107. - [SDR SIMA20180123011](https://openairdocs.org/sdr/SIMA20180123011.md): Support · cracked · Jan 23, 2018 · N830AE · Emb EMB135KL · Fuselage Miscellaneous Structure > LT OMEGA BEAM OUTBOARD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. REPAIRED LEFT OMEGA BEAM OUTBOARD SUPPORT BETWEEN FRAMES 47-48 IAW SRM 53-23-10. - [SDR SIMA20180122001](https://openairdocs.org/sdr/SIMA20180122001.md): Floor Support · corroded · Jan 22, 2018 · N830AE · Emb EMB135KL · Fuselage Miscellaneous Structure > LEFT OMEGA BEAM IS CORRODED AT FRAME 59. REPAIRED THE OMEGA BEAM IAW EO-EM-53MR-1518, REV 3. - [SDR SIMA20180122003](https://openairdocs.org/sdr/SIMA20180122003.md): Floor Support · corroded · Jan 22, 2018 · N830AE · Emb EMB135KL · Fuselage Miscellaneous Structure > CENTER OMEGA BEAM IS CORRODED AT FRAME 59. REPAIRED THE OMEGA BEAM IAW EO-EM-53MR-1518, REV 3. - [SDR SIMA20180122002](https://openairdocs.org/sdr/SIMA20180122002.md): Stop Fitting · cracked · Jan 22, 2018 · N830AE · Emb EMB135KL · Service Doors > SERVICE DOOR FORWARD LOWER STOP BRACKET IS CRACKED. REMOVED AND REPLACED THE SERVICE DOOR FORWARD LOWER STOP BRACKET IAW SRM 51-40-02. - [SDR SIMA20180122004](https://openairdocs.org/sdr/SIMA20180122004.md): Skin · cracked · Jan 22, 2018 · N830AE · Emb EMB135KL · Fuselage Main, Plate/Skin > FUSELAGE SKIN CRACKED, FRAME 77 AND 78. REPAIRED THE SKIN IAW ERS-EM-53MR-3709. - [SDR SIMA20180117005](https://openairdocs.org/sdr/SIMA20180117005.md): Stringer · damaged · Jan 17, 2018 · N830AE · Emb EMB135KL · Fuselage Main, Longeron/Stringer > STRINGER 13L DAMAGED BETWEEN FRAMES 48 AND 50. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02, AND 51-20-01 - [SDR SIMA20180117004](https://openairdocs.org/sdr/SIMA20180117004.md): Door Sill · corroded · Jan 17, 2018 · N830AE · Emb EMB135KL · Fuselage Miscellaneous Structure > CARGO DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02 - [SDR SIMA20180117002](https://openairdocs.org/sdr/SIMA20180117002.md): Skin · cracked · Jan 17, 2018 · N830AE · Emb EMB135KL · Fuselage Main, Plate/Skin > FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R. REPAIRED THE SKIN IAW SRM 53-31-01 - [SDR SIMA20180117001](https://openairdocs.org/sdr/SIMA20180117001.md): Rib · cracked · Jan 17, 2018 · N830AE · Emb EMB135KL · Elevator, Spar/Rib > LEFT ELEVATOR NOSE RIB ON INBOARD HINGE CUTOUT INBOARD SIDE CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-40-02 - [SDR SIMA20171212008](https://openairdocs.org/sdr/SIMA20171212008.md): Support · cracked · Dec 12, 2017 · N830AE · Emb EMB135KL · Fuselage Main, Structure > RIGHT OMEGA BEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47 - 48. REMOVED AND REPLACED THE SUPPORT IAW SRM 53-23-02. - [SDR SIMA20171212009](https://openairdocs.org/sdr/SIMA20171212009.md): Crossmember · corroded · Dec 12, 2017 · N830AE · Emb EMB135KL · Fuselage Main, Structure > CENTER AISLE CROSSMEMBER CORRODED BETWEEN FRAMES 33-34. REMOVED AND REPLACED THE CROSSMEMBER IAW SRM 51-40-02, SRM 51-20-01, AND ETN-EM-53-241. - [SDR SIMA20171212010](https://openairdocs.org/sdr/SIMA20171212010.md): Crossmember · corroded · Dec 12, 2017 · N830AE · Emb EMB135KL · Fuselage Main, Structure > CENTER AISLE CROSSMEMBER CORRODED BETWEEN FRAMES 24-25. REMOVED AND REPLACED THE CENTER AISLE CROSSMEMBER IAW SRM 51-40-02, SRM 51-20-01, AND ETN-EM-53-241. - [SDR SIMA20160629006](https://openairdocs.org/sdr/SIMA20160629006.md): Holder · broken · Jun 29, 2016 · N830AE · Emb EMB135KL · Emergency Equipment > F/O'S FLASHLIGHT HOLDER BROKEN. REMOVED AND INSTALLED F/O'S FLASHLIGHT CRADLE IAW AMM 33-50-16. - [SDR SIMA20160620003](https://openairdocs.org/sdr/SIMA20160620003.md): Lever · defective · Jun 20, 2016 · N830AE · Emb EMB135KL · Door Warning System > BAGGAGE DOOR WARNING SYS MFD/EICAS, BAGGAGE DOOR WARNING ILLUMINATED AFTER TAKEOFF AND EXTINGUISHED AFTER LANDING. RESTORATION OF MEL ITEMS REVIEW THE MEL AND ENSURE APPROPRIATE MAINTENANCE ACTIONS ARE TAKEN TO RESTORE THE ITEM, SYSTEM CONDITIONS AND LIMITATI - [SDR SIMA20160402001](https://openairdocs.org/sdr/SIMA20160402001.md): Lever · defective · Apr 2, 2016 · N830AE · Emb EMB135KL · Door Warning System > ON ROLL OUT AT 80KTS, RECEIVED ADVISORY CARGO DOOR OPEN. TAKEOFF ABORTED. RETURNED TO GATE. GND PERSONNEL REVISED DOOR. DOOR INDICATION ON MFD FLICKERING GREEN TO RED & EICAS MSG KEPT DISPLAYING. VERIFIED BAG DOOR CLOSES & LATCHES FLUSH AS REQUIRED IAW ME - [SDR SIMA20160211003](https://openairdocs.org/sdr/SIMA20160211003.md): Smoke Detector · failed · Feb 11, 2016 · N830AE · Emb EMB135KL · Smoke Detection > BAGGAGE COMPARTMENT SMOKE DETECTOR FAILS FIRE TEST. R & R BAGGAGE COMPARTMENT FWD SMOKE DETECTOR IAW AMM 26-15-01. OPERATIONAL CHECKED GOOD. - [SDR SIMA20160118003](https://openairdocs.org/sdr/SIMA20160118003.md): Light · inoperative · Jan 18, 2016 · N830AE · Emb EMB135KL · Emergency Lighting > LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT LAMP IAW AMM 33-50-07. OPERATIONS CHECKED GOOD. - [SDR SIMA20150726001](https://openairdocs.org/sdr/SIMA20150726001.md): Proximity Sensor · failed · Jul 26, 2015 · N830AE · Emb EMB135KL · Drag Control System > SPOILER FAIL MSG PRESENTED. SPOILERS SHOWED OPEN INTERMITTENTLY. RAN INADVERTENT SPOILER OPEN IN FLIGHT CHECKLIST. FLIGHT ATTENDANT DID NOT OBSERVE OPEN SPOILERS. NO CHANGES IN FLIGHT CHARACTERISTICS NOTED. R & R LT INBD SPOILER PROX SWITCH IAW AMM 27-63- - [SDR SIMA20150623004](https://openairdocs.org/sdr/SIMA20150623004.md): Warning System · activated · Jun 23, 2015 · N830AE · Emb EMB135KL · Hydraulic Quantity Indicator > HYDRAULIC SYS 1 LO LEVEL IN FLIGHT. LEVEL 3/4 FULL ON GND & AT CRUSE. DECREASED INTO AMBER. HYD LO LEVEL ON EICAS, SUSPECT LEAK. TRANSFERRED HYD FLUID IAW ETN EM-29-023. PERFORMED WALK AROUND INSPECTION NO LEAKS NOTED. - [SDR SIMA20150426001](https://openairdocs.org/sdr/SIMA20150426001.md): Light · inoperative · Apr 26, 2015 · N830AE · Emb EMB135KL · Emergency Lighting > IAW PS1 CHECK, RT EXTERNAL EMER LIGHT IS INOPERATIVE. REMOVED & INSTALLED RT EXTERNAL EMER LIGHT IAW AMM 33-50-10. - [SDR SIMA20150408005](https://openairdocs.org/sdr/SIMA20150408005.md): Wire · pulled · Apr 8, 2015 · N830AE · Emb EMB135KL · Light System Wiring > LAST EMER LIGHT PROXIMITY STRIP AFT WIRES PULLED FROM SPLICES. R & R SPLICES SP 9502 & SP 9503 IAW SWPM 20-21-00. EMER LIGHT STRIP OPERATIONS CHECKED GOOD IAW AMM 33-50-00. - [SDR SIMA20140815001](https://openairdocs.org/sdr/SIMA20140815001.md): Door · lack of lube · Aug 15, 2014 · N830AE · Emb EMB135KL · Passenger/Crew Doors > FLIGHT ATTENDANT REPORTS CABIN ENTRY DOOR IS HARDER TO OPERATE WHEN OPENING. CLEAN & LUBED MAIN CABIN DOOR. OPERATIONS CHECKED GOOD IAW SP. - [SDR SIMA20140724004](https://openairdocs.org/sdr/SIMA20140724004.md): Control Module · faulty · Jul 24, 2014 · N830AE · Emb EMB135KL · Fire Detection > ON TAXI GOT APU FIRE EICAS WHILE APU WAS OFF. PRESSED APU EXT BUTTON IAW CHECK LIST. MSG EXTINGUISHED THEN REAPPEARED & EXTINGUISHED AGAIN. R & R APU FIRE DETECT CONTROL MODULE & TROUBLE SHOT SYS IAW AMM 26-12-02 & FIM 26-12-00. - [SDR SIMA20140718001](https://openairdocs.org/sdr/SIMA20140718001.md): Skin · cracked · Jul 18, 2014 · N830AE · Emb EMB135KL · Fuselage Main, Plate/Skin > DURING IMBV INSPECTION, QA FOUND LT AFT FUSELAGE FASTENER HOLE CRACKED AT FRAME 75 STRINGER 2 AREA. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR ON LT AFT FUSELAGE FASTENER - [SDR SIMA20140714005](https://openairdocs.org/sdr/SIMA20140714005.md): Frame · cracked · Jul 14, 2014 · N830AE · Emb EMB135KL · Fuselage Main, Frame > DURING IMBV INSPECTION, QA FOUND FRAME 23 CRACKED BETWEEN STRINGER 15R - 16R. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR ON FRAME 23 BETWEEN STRINGER 15R - 16R IAW EO-EM-5 - [SDR SIMA20140628017](https://openairdocs.org/sdr/SIMA20140628017.md): Wire · broken · Jun 28, 2014 · N830AE · Emb EMB135KL · Light System Wiring > ONE PROX LIGHT WITH ARROWS & ONE PROX LIGHT WITHOUT ARROWS HAVE BROKEN WIRES AT PROX LIGHT. R & R IAW AMM 33-50-12. SEE NRTC BOW 159263 FOR FINAL INSTALL & OPERATIONS CHECK. - [SDR SIMA20140628011](https://openairdocs.org/sdr/SIMA20140628011.md): Skin · cracked · Jun 28, 2014 · N830AE · Emb EMB135KL · Fuselage Main, Plate/Skin > AFT UPPER LT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 77. REPAIRED DAMAGE BY INSTALL BUSHING & FILET SEALED IAW ERS-EM-5300-562. SEE TURNOVER FOR DETAILS. - [SDR SIMA20140628008](https://openairdocs.org/sdr/SIMA20140628008.md): Light · inoperative · Jun 28, 2014 · N830AE · Emb EMB135KL · Emergency Lighting > NUMBER 1 AISLE EMER LIGHT STRIP NOT WORKING. R & R NR 1 AISLE EMER FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE BOW 159263 TASK NR 1 FOR OPERATIONAL CHECK. - [SDR SIMA20140628009](https://openairdocs.org/sdr/SIMA20140628009.md): Wire · broken · Jun 28, 2014 · N830AE · Emb EMB135KL · Light System Wiring > FORWARD PROXIMITY LIGHT STRIP WIRE BROKEN AT SPLICE CONNECTOR. REPAIRED FWD PROXIMITY LIGHT STRIP WIRE AT SPLICE CONNECTOR IAW SWPM 20-21-00 STEP 6. - [SDR SIMA20140628015](https://openairdocs.org/sdr/SIMA20140628015.md): Flange · corroded · Jun 28, 2014 · N830AE · Emb EMB135KL · Wing Miscellaneous Structure > RIGHT LE NR 2 OTBD MACHINED FLANGE IS CORRODED. REPAIRED IAW ERS-EM-5700-182. SEE TURNOVER FOR DETAILS. - [SDR SIMA20140628014](https://openairdocs.org/sdr/SIMA20140628014.md): Support · cracked · Jun 28, 2014 · N830AE · Emb EMB135KL · Fuselage Miscellaneous Structure > CABIN RT FLOORBEAM OTBD SUPPORT CRACKED AT WING BOX BETWEEN FRAME 47 & 48. REMOVED RT CABIN OMEGA BEAM TO WING BOX OTBD SUPPORT ANGLE & DRILLED FASTENER HOLES IN NEW TWO PIECE REPAIR ANGLE IAW SRM 53-23-02 & 51-20-03. - [SDR SIMA20140628013](https://openairdocs.org/sdr/SIMA20140628013.md): Skin · cracked · Jun 28, 2014 · N830AE · Emb EMB135KL · Fuselage Main, Plate/Skin > AFT UPPER RT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 78. REPAIRED DAMAGE BY INSTALLING BUSHING IAW ERS-EM-5300-563. SEE TURNOVER FOR DETAILS. - [SDR SIMA20140628012](https://openairdocs.org/sdr/SIMA20140628012.md): Splice Plate · cracked · Jun 28, 2014 · N830AE · Emb EMB135KL · Fuselage Miscellaneous Structure > GALLEY UNDERFLOOR FWD TO AFT DIGITAL SPLICE REINFORCEMENT CRACKED AT LT FLOORBEAM. R & R SPLICE PLATE IAW SRM 51-30-01, 51-40-02 & GPM 17-13. SEE WIPS & TASKS FOR ADDITIONAL INFORMATION. - [SDR SIMA20140628016](https://openairdocs.org/sdr/SIMA20140628016.md): Frame · cracked · Jun 28, 2014 · N830AE · Emb EMB135KL · Fuselage Main, Frame > RIGHT AFT FUSELAGE FRAME 75 FASTENER HOLE CRACKED STRINGER 3 AREA MARKED. REPAIRED DAMAGE AT RT AFT FUSELAGE BY INSTALLING BUSHING IAW ERS-EM-5300-575. SEE TURNOVER FOR DETAILS. - [SDR SIMA20140628010](https://openairdocs.org/sdr/SIMA20140628010.md): Skin · cracked · Jun 28, 2014 · N830AE · Emb EMB135KL · Fuselage Main, Plate/Skin > AFT UPPER RT EXTERNAL FUSELAGE SKIN CRACKED AT RIVET FRAME 79 MARKED. REAMED FASTENER HOLE ON AFT UPPER RT EXTERNAL FUSELAGE SKIN AT FRAME 79 BETWEEN STRINGER 3R - 4R AS REQUIRED TO REMOVE DAMAGE. FABRICATED & INSTALLED BUSHING IAW ERS-EM-5300-588. SEE TASK Next page: https://openairdocs.org/aircraft/N830AE/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 = 'N830AE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N830AE/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.