N203NN
Service difficulty reports · 49
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 = 'N203NN' 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.
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 = 'N203NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SIMA20260818001Door · no discrepancyCATERING TRIED TO OPEN L2 DOOR AND THEY COULDN'T OPEN IT FROM OUTSIDE. OPERATED L2 DOOR IAW AMM 52-12-00 AND FOUND NO DEFECTSSDR SIMA20260531001Engine · vibrationE2 LP VIBRATION IN AMBER AT 4,0 APPROX AT FL180, COULD NOT MAINTAIN CLIMB WITHOUT ENG 2 IN THE CAUTION ABOVE 4.0. WE RAN THE QRH PROCEDURE AND VIBRATIONS IMMEDIATELY CAME BACK EMERGENCY DFECLARED. PERFORMED HIGH POWER RUN ON E2 IAW LMM72-00-00-760-041 HIGHEST SDR SIMA20260505001Landing Gear · faultedGEAR WOULD NOT COME UP ON TAKEOFF. GEAR LEVER LOCKED DOWN. NO EICAS MESSAGE DISPLAYED. CREW DID USE THE DN LOCK REL RED BUTTON TO BRING THE GEAR UP PER THE QRH. CREW DID NOT USE THE DN LOCK REL RED BUTTON TO BRING THE GEAR UP PER THE QRH. NO EMERGENCY DECLAREDSDR SIMA20260122002Skin · dentedRH WING SLAT TRACK #4 CUTOUT SKIN DAMAGED ON LINKAGE ASSY DURING MANUAL RAISING OF TRACKS (MAJOR REPAIR). RAR THE RH WING LEADING EDGE SKIN AT THE RH WING SLAT TRACK #4 CUTOUT IAW ERJ 175 SRM 51-40-08SDR SIMA20251204001Regulator · failedBLEED 2 FAIL AT ALTITUDE. ENG BLEED SYS - XBLD OPERATIVE - M1 BLEED 1 PRESSURE UNSTABLE IN CRUISE 6-47 PSI AND RATE CHANGES OF -250/200 MSG EVENTUALLY CLEARED VIA QRH PROCEDURE INFO TO MTX. INFO NOTED TO MTX MOC 230070. RAR LH ENGINE NAPRSOV HIGH STAGE BLEED VSDR SIMA202512054001Bleed Air Sys · faultedBLEED 2 FAIL AT ALTITUDE. MSG EVENTUALLY CLEARED VIA QRH PROCEDURE INFO TO MTX. INFO NOTED TO MTX MOC 230070. PENDING CORRECTIVE ACTIONSDR SIMA20250430001Seat Track · corrodedSSI 53-23-005 AFT GALLEY AREA RH SEAT TRACK BEAM CORRODED BTW FR 84-85. (MAJOR REPAIR) (LEVEL 2 CORROSION). REPAIRED AFT GALLEY AREA RH SEAT TRACK BEAM BTW FR 84-85 IAW ERS-EJ-53MR-5187.SDR SIMA20250428002Floor Support · corrodedSSI 53-23-005 AFT GALLEY AREA LH CENTER FLOOR BEAM BETWEEN FR 86-87 CORRODED. (LEVEL 2 CORROSION) (MAJOR REPAIR) COMPLETED INSTALLATION OF SERVICEABLE AFT GALLEY LH CTR FLOOR BEAM BTW FR 86-89 IAW EMB 175 SRM 51-40-08SDR SIMA20250427005Shear Panel · corrodedSSI 53-23-005 AFT GALLEY AREA RH SHEAR PANEL IS CORRODED (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT GALLEY AREA RH SHEAR PANEL IAW EMB 175 SRM 51-40-08SDR SIMA20250427009Crossbeam · corrodedSSI 53-23-005 AFT GALLEY AREA FR 84 CROSSBEAM IS CORRODED BETWEEN THE RH AND LH CTR SEAT TRACK SUPPORTS. (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED AFT GALLEY AREA FR 84 CROSSBEAM IAW EMB 175 SRM 51-40-08.SDR SIMA20250427006Seat Track · corrodedSSI 53-10-027 RH CTR FLOOR BEAM HAS CORROSION LOCATED AT INTERSECTION WITH FR17 CROSSBEAM (ON TOP AND LOWER SIDE). (MAJOR REPAIR) (LEVEL 2 CORROSION). PERFORMED PERMANENT REPAIR TO RH CTR FLOOR BEAM AT INTERSECTION WITH FR 17 CROSSBEAM IAW ERS-EJ-53MR-5186.SDR SIMA20250427007Floorbeam · corrodedSSI 53-10-027 LH CTR FLOOR BEAM HAS CORROSION LOCATED AROUND SEAT TRACK FWD END. (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED LH CTR FLOOR BEAM BETWEEN FR 12-21 IAW EMB 175 SRM 51-40-08.SDR SIMA20250427008Shear Panel · corrodedSSI 53-23-005 AFT GALLEY AREA RH SHEAR PANEL IS CORRODED. (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT GALLEY AREA RH SHEAR PANEL IAW EMB 175 SRM 51-40-08.SDR SIMA20250427003Floor Support · corrodedAFT GALLEY AREA LH CTR FLOOR BEAM UPPER SHEET BETWEEN FR 85-86 IS CORRODED. (LEVEL 2 CORROSION) (MAJOR REPAIR) REMOVED AND REPLACED AFT GALLEY AREA LH CENTER FLOOR BEAM SHEET BETWEEN FRAMES 85-86 IAW EMB 175 SRM 51-40-08SDR SIMA20250427004Floor Support · corrodedAFT GALLEY AREA RH CTR FLOOR BEAM BETWEEN FR88-89 IS CORRODED. (LEVEL 2 CORROSION) (MAJOR REPAIR) INSTALLED R/H FLOOR BEAM LOCATED BETWEEN FR86-89 IAW EMB 175 SRM 51-- 40-08SDR SIMA20250427001Gusset · corrodedAFT GALLEY AREA RH OUTBD SPLICE AT FR 90 IS CORRODED. (LEVEL 2 CORROSION). REMOVED AND REPLACED AFT GALLEY AREA RH OUTBD SPLICE AT FR90 IAW EMB 175 SRM 51-40-08SDR SIMA20250427002Floor Support · corrodedSSI 53-23-005 AFT GALLEY AREA RH CTR FLOOR BEAM UPPER SHEET BETWEEN FR 85-86 IS CORRODED. (LEVEL 2 CORROSION). REMOVED AND REPLACED AFT GALLEY AREA RH CTR FLOOR BEAM UPPER SHEET BETWEEN FR 85-86 IAW EMB 175 SRM 51-40-08SDR SIMA20250425002Seal Rest · corrodedFWD CARGO DOOR CUTOUT LOWER FWD CTR AND AFT SEAL RESTS HAVE CORROSION AROUND THE NUTPLATES (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED FWD CARGO DOOR CUTOUT LOWER FWD, CENTER, AND AFT SEAL RESTS IAW EMB 175 SRM 51-40-08.SDR SIMA20250220001Battery · inoperativeFWD SERVICE DOOR LOWER EMERGENCY EXIT IDENTIFIER LIGHT INOP. RAR FWD RH EXIT IDENTIFIER LIGHT IAW AMM 33-50-15 AND RAR EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-01. OPC GOOD. NO FURTHER DEFECTS NOTED.SDR SIMA202411085003Skin · gougedONETIME PERMANENT REPAIR - ERS-EJ-57MR-1246 OPS PTC DUE - WING LEADING EDGE - RH SKIN RIB 32 TO RIB 37- UNDER RIB 32 - GOUGE - PERMANENT REPAIR. (MAJOR REPAIR). REMOVED AND REPLACED RH WING LEADING EDGE SKIN BETWEEN RIB 32 AND RIB 37 IAW EO EJ-57MR-1246 AND EMSDR SIMA202401298001None · noneFLAPS OVERSPEED 250KTS FOR 10 SECS. FLAP OVERSPEED INSPECTION COMPLETED IAW ENVOY MTX TASK CARD 05-50-07-200-801. NO DEFECTS NOTED OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICESDR SIMA20230226001None · noneEMERGENCING DECLARED AFTER TAKEOFF SELECTED LG UP RECEIVED LG LEVER DISAG MESSAGE ON EICAS .PERFORMED CHECKLIST BUT NS GEAR REMAINED DOWN.ON THE GROUND RECEIVED LG NO DISPATCH-C/A-REF IT# 2 THIS LOG PG. AFTER REMOVAL OF NLG SAFTY PIN, LANDING GEAR OPS CHECKS GSDR SIMA2023013017001Spar · crackedAFTER REMOVAL OF RH WINGTIP, FOUND RH WING OUTBD SPAR 1 TO BE CRACKED (MAJOR REPAIR)-C/A-REMOVED AND REPLACED SERVICEABLE R/ H WING OUTBD SPAR 1 IAW EMB 175 SRM 51-40-- 08, 51-42-02SDR SIMA2023013016006Gusset · corrodedAFT GALLEY FLOOR STRUCTURE OUTBD SPLICE IS CORRODED AT FR 90 (LEVEL 2 CORROSION)-C/A-REMOVED AND INSTALLED AFT GALLEY FLOOR STRUCTURE OUTBD SPLICE AT FR 90 IAW EMB-175 SRM 51-40?08SDR SIMA20230116004Shear Panel · corrodedAFT GALLEY FLOOR STRUCTURE RIGHT SHEAR PANEL BETWEEN FR 87 AND FR 88 IS CORRODED (LEVEL 2 CORROSION). R & R AFT GALLEY FLOOR STRUCTURE RH SHEAR PANEL BETWEEN FR 87-88 IAW EMB-175 SRM 51-40-08.SDR SIMA2023012716005Shear Panel · corrodedAFT GALLEY FLOOR STRUCTURE CENTER SHEAR PANEL IS CORRODED (LEVEL 2 CORROSION). R & R AFT GALLEY STRUCTURE CENTER SHEAR PANEL IAW EMB-175 SRM 51-40-08.SDR SIMA2023012716003Shear Panel · corrodedSSI 53-23-005 AFT GALLEY FLOOR STRUCTURE LEFT SHEAR PANEL IS CORRODED (LEVEL 2 CORROSION)-C/A-RAR AFT GALLEY LH SHEAR PANEL IAW EMB-175 SRM 51-40-08.SDR SIMA2023012716002Floorbeam · corrodedAFT GALLEY FLOOR STRUCTURE RIGHT OUTBD PANEL SUPPORT IS CORRODED AT FR 89 (LEVEL 2 CORROSION)-C/A- INSTALLED SERVICEABLE AFT GALLEY RH OUTBD FLOOR PANEL SUPPORT IAW SRM 51-40-08SDR SIMA20230115003Rib · crackedLH WING FIXED LEADING EDGE HAS A CRACKED RIB #36, LOCATED BETWEEN SLAT #4 TRACKS. (MAJOR REPAIR)-C/A-ACCOMPLISHED REPAIR OF LH WING FIXED LEADING EDGE RIB 36 IAW ETD# ETD2023-170-001856 REV. B AND ERS-EJ-57MR-1489SDR SIMA20230115002Seat Track · gougedRH FLOOR SEAT TRACK GOUGED JUST FWD OF FR 82 (MAJOR REPAIR)-C/A-REPAIRED RH FLOOR SEAT TRACK GOUGED AREA JUST FWD OF FR 82 (WITH REPAIR AREA BETWEEN FR 80-81) IAW EMB 175 SRM 53-00-10 RE01P, 51-40-08, ETN-EJ-51-010.SDR SIMA2023013015001Seat Track · gougedLH FLOOR SEAT TRACK GOUGED AT FR 81 (MAJOR REPAIR) REMOVED DAMAGED SECTION OF LT LOWER FLOOR BEAM AT FR 81 AREA AND FABRICATED AND INSTALLED SPLICE PARTS AND REPLACEMENT BEAM SECTION IAW SRM 53-00-10 REPAIR 01P SECTION 6 AND FIGURE 205 AND ETN-EJ-53-010 R1.SDR SIMA20230110003None · inoperativePHOLUMINESCENT LIGHT INOP PHOTOLUMINESENT INDICATOR STRIPE LH1, RH1, RH2, RH3 DISCOLORATION-C/A-COMPLETE:RAR PHOTOLUMINESENT INDICATOR STRIPE LH1, RH1, RH2, RH3 IAW EMB 175 AMM 33-50-21SDR SIMA20230110002None · inoperativePHOTOLUMINESCENT LIGHT INOP #2LH,#3LH AND #5 RH PHOTO LLUMINECENT FLOOR LIGHTS CRACKED-C/A-COMPLETE:RAR #2LH,#3LH AND #5 RH PHOTO LLUMINECENT FLOOR LIGHTS IAW EMB 175 AMM 33-50-21SDR SIMA20230110001Strip · inoperativePHOTOILUMINESENT LIGHT INOP INDICATOR STRIPS LH4 LH8 , RH10, AND RH12 CRACKED-C/A-COMPLETE:RAR PHOTOILUMINESENT INDICATOR STRIPS LH4 LH8 , RH10, AND RH12 IAW EMB 175 AMM 33-50-21SDR SIMA20220423002Engine · warning messageDIVR SAT ENGINE 2 LP VIBE 4.0 UNABLE TO CLEAR VIA QRH. .EMRGENCY DECLARED. FLT CONT -C/A-PERFORMED INSPECTION FOR FOD ALSO PERFORMED INSPECTION FOR STUCK BLADES NO DEFECTS NOTED. DEFERRAL DATA ANAYLSIS TO BE PERFORMED WITHIN 25 FLIGHT CYCLES ALL WORK DONE IAW SDR SIMA202006110001Power Unit · inoperativeFWD SERVICE DOOR LOWER EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT POWER UNIT FOR THE FWD SERVICE DOOR LOWER EMERGENCY LIGHT IAW AMM 33-50-01. OPS CHK GOOD.SDR SIMA2020061109004Skin · gougedRT WING FIXED L/E UPPER SKIN GOUGED, UNDER INBD END OF SLAT NR 4. ACCOMPLISHED TEMPORARY REPAIR TO RT WING FIXED L/E UPPER SKIN GOUGE UNDER INBD END OF SLAT NR 4 IAW ERS-EJ-57MR-1246 PT A.SDR SIMA20200605002Glowstrip · rupturedRT NR 1,2 AND 3 PHOTOLUMINESCENT STRIPS APPEAR TO BE RUPTURED AND NO LONGER LIGHT UP (FOUND DURING CONFORMITY). REMOVED AND REPLCED RT NR 1, 2 AND 3 PHOTOLUMINESCENT STRIP IAW AMM 33-50-21. OP CK GOOD. STRIP LIGHT PHOTOLUMINESCENINDICA P/N SG 0004-2128D RT NR SDR SIMA20200605001Glowstrip · rupturedLT NR 1 PHOTOLUMINESCENT STRIP APPEARS TO BE RUPTURED AND NO LONGER LIGHTS UP (FOUND DURING CONFORMITY). REMOVED AND REPLACED LT NR 1 PHOTOLUMINESCENT STRIP IAW AMM 33-50-21. OP CK GOOD.SDR C77A2019111400004Stringer · mislocatedDURING ACCOMPLISHMENT OF THE ISP MODIFICATION AT EAMS, DAMAGE WAS INCURRED ON THE CENTER FUSELAGE II
STRINGERS 15L, 16L, AND 17L (P/N 170-12505-405, P/N 170-12505-405, P/N 170-12506-405) WHEN THE WRONG LOCATIONS WERE DRILLED. REFERENCE FIGURES 1-3 FOR DETAILSDR C77A2019111400003Stringer · mislocatedDURING ACCOMPLISHMENT OF THE ISP MODIFICATION AT EAMS, DAMAGE WAS INCURRED ON THE CENTER FUSELAGE II
STRINGERS 15L, 16L, AND 17L (P/N 170-12505-405, P/N 170-12505-405, P/N 170-12506-405) WHEN THE WRONG LOCATIONS WERE DRILLED. REFERENCE FIGURES 1-3 FOR DETAILSDR C77A2019111400002Stringer · mislocatedDURING ACCOMPLISHMENT OF THE ISP MODIFICATION AT EAMS, DAMAGE WAS INCURRED ON THE CENTER FUSELAGE II
STRINGERS 15L, 16L, AND 17L (P/N 170-12505-405, P/N 170-12505-405, P/N 170-12506-405) WHEN THE WRONG LOCATIONS WERE DRILLED. REFERENCE FIGURES 1-3 FOR DETAILSDR C77A2019111400001Floorbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON-CONDITION REPAIR OF CORROSION OR OTHER DAMAGE TO THE CENTER FUSELAGE III AFT CABIN RH FLOOR BEAM P/N 170-65669-004. THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THE AFFESDR C77A2020011540014Finger Doubler · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE CENTER FUSELAGE III
CARGO DOOR SURROUND LOWER FINGER PLATE. REFERENCE ETD2019-170-152677 FIGURE 1 FOR
DETAILS, FOR THE DAMAGE LOCATIONS AND DIMENSION. THE DAMAGE IS IN A NO DAMAGE ALLOWED
AREA OFSDR C77A2019072200001Shutoff Valve · failedBLEED 2 OVERPRESS FOLLOWED BY BLEED 2 FAIL. DEACTIVATED RT NAPRSOV IAW AMM 36-11-03. PARTS ON ORDER. THIS WO REMAINS OPEN FOR FURTHER T/S. REMOVED NACELLE PRESSURE REGULATING SHUTOFF VALVE IAW AMM 36-11-03-000-801-A . THIS WO REMAINS OPEN A/C OK FOR SVC. REMOVSDR C77A20170918001Doubler · gougedGOUGE DAMAGE ON THE CO-PILOT’S SIDE CUTOUT IN THE FORWARD UPPER SKIN WINDSHIELD WIPER DOUBLER, BLENDED IAW ETD2016-170-069750-A, FIGURE 4. TSDR C77A20160824002Warning System · false activationFLIGHT DIVERTED DUE TO A FWD LAV SMOKE EICAS MESSAGE. THE CABIN CREW CHECKED THE LAV AND CABIN AND NO INDICATION OF SMOKE/FIRE WAS FOUND. THE MESSAGE WENT OUT WHILE STILL IN FLIGHT. THE FLIGHT LANDED. MAINTENANCE PERFORMED FWD LAV SMOKE DETECTOR OPS TEST IASDR C77A20160706001Module · malfunctionedAT 1000 FT, CREW WAS ALERTED VIA EICAS OF A, AVNX MAU 3B FAIL, SPOILER FAULT, FDR AFT FAIL, AND DATALINK 1 FAIL. CREW RAN THE QRH PROCEDURES FOR BOTH THE AVNX MAU 3B FAIL AND THE SPOILER FAULT MESSAGES BUT WERE UNABLE TO CLEAR THE MESSAGES. ATC WAS ALERTED. SDR C77A20150814001Power Unit · inoperativeCOCKPIT EMER CEILING LIGHT & FWD CABIN EMER CEILING LIGHT INOPERATIVE. R & R EMER LIGHT POWER PACK IAW AMM 33-50-01. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.
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