N683AE
Service difficulty reports · 166
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 = 'N683AE' 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 = 'N683AE' 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 HNAA2026041200283Switch · failedMAIN PITCH TRIM INOP MESSAGE DURING CLIMB USING CAPT YOKE SWITCH. R&R PITCH TRIM SWITCH IAW EMBR AMM 27-40-03. PERFORMED HORIZONTAL STAB ADJUSTMENT TEST EMBR 145 AMM 27-40-00 TROUBLESHOOTED USING EMBR 145 FIM 27-43-00-810-801-A. NO DEFECTS NOTED, A/C GOOD FOSDR HNAA2026032700249Switch · intermittentDURING CLIMB PITCH TRIM MAIN AND BACKUP FAILED ON BOTH SIDES WITH NO EICAS MESSAGES, NO CMC MESSAGES. WAS STUCK UP 2 DEGREES. NO CMC MESSAGES. FACT 26MAR26 08:00 PIT FOLLOWED FIM 27-43-00-810-820-A BLOCKS 1, 2, 3, 8. PERFORMED OPS CHECK IAW AMM 27-40-0SDR HNAA2025100300661Floor Support · corrodedF068535 CORROSION ON LH OTBD #2 FLOOR SILL. REMOVED AND REPLACED FLOOR SILL ON LH OTBD #2 FLOOR SILL IAW EMB145 SRM 51-40-02.SDR HNAA2025100300670Skin · buckledF069494 RH WHEEL WELL INTERNAL SKIN IS BUCKLED AT FR3. REPAIRED BUCKLED RH WHEEL WELL INTERNAL SKIN AT FR 3 IAW PIEDMONT EO1-53-25-0329 AND ETD2025-145-928107.SDR HNAA2025100300669Crossbeam · damagedCROSSMEMBER AT FRAME 5 HAS ELONGATED FASTENER HOLES NEAR STGR 15R. REPAIRED CROSSMEMBER AT FR 5 ELONGATED FASTENER HOLES NEAR STR 15R IAW EO1-53-25-0326 AND ETD2025-145-927858.SDR HNAA2025100300668Frame · damagedFRAME 5 HAS ELONGATED FASTENER HOLES NEAR STGR 15R. REPAIRED FR 5 ELONGATED FASTENER HOLES NEAR STR 15R IAW EO1-53-25-0330 AND ETD2025-145-927849.SDR HNAA2025100300675Shear Tie · damagedFRAME 3 BETWEEN STR 14R AND 17R IS DENTED AND BENT AT SKIN ATTACHMENT FLANGE. RAR FR3 BETWEEN STGR 11R-19R IAW EMB 145 SRM 51-40-02SDR HNAA2025100300667Frame · damagedFRAME 4 IS DAMAGED AT STGR 15R. REPAIRED FR 4 DAMAGE AT STR 15R IAW PIEDMONT EO1-53-25-0327 AND ETD2025-145-927854.SDR HNAA202510030075Frame · damagedFRAME 3 BETWEEN STR 14R AND 17R IS DENTED AND BENT AT SKIN ATTACHMENT FLANGE. RAR FR3 BETWEEN STGR 11R-19R IAW EMB 145 SRM 51-40-02SDR HNAA2025100300674Stringer · damagedSTRINGER 14R HAS AN OVERSIZED HOLE AT FR2. RAR STRINGER 14R BTW FR 1A-6 IAW EMB 145 SRM 51-40-02. DURING REPLACEMENT FOUND 13 HOLES BETWEEN FR 2-3 TO ONLY HAVE 1.5D EDGE DISTANCE. 13 HOLES ARE ACCEPTED AS A PERMANENT REPAIR IAW ETD2025-145-928801 AND EO1-53-2SDR HNAA2025100300676Frame · damagedFRAME 4 IS DAMAGED AT STGR 15R. REPAIRED FR 4 DAMAGE AT STR 15R IAW EO1-53-25-0327 AND ETD2025-145--927854.SDR HNAA2025100300664Floor Support · corrodedF068625 GALLEY FLOOR SUPPORT BRACKET AT FR-23 AND STGR-16 HAS CORROSION. RAR GALLEY FLOOR SUPPORT BRACKET AT FR-23 AND R/H STGR 16 IAW EMB 145 SRM 51-40-02.SDR HNAA2025100300673Shear Tie · crackedF068552 SHEAR CLIP IS CRACKED AT FRAME 26 BETWEEN STRINGERS 16R-17R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 16R-17R IAW EMB 145 SRM 51-40-02.SDR HNAA2025100300672Skin · damagedF068464 FWD FUSELAGE I SKIN PANEL FROM FR 1A-3 STR 14R TO THE NLG CUTOUT REQUIRES REPLACEMENT DUE TO MULTIPLE TOOL MARKS. REMOVED MULTIPLE TOOLING MARKED FWD FUSELAGE I SKIN PANEL FROM FR 1A-3 STR 14R TO THE NLG CUTOUT, PREPPED AND INSTALLED SERVICEABLE SKIN SDR HNAA2025100300666Floor Support · corrodedF068510 CABIN L/H OMEGA BEAM GUSSET BETWEEN FR-35/38 HAVE CORROSION. REMOVED AND REPLACED CABIN L/H OMEGA BEAM GUSSET #4 IAW EMB 145 SRM 51-40-02SDR HNAA2025100300665Floorbeam · corrodedF068508 CORROSION ON LH #3 FLOOR BEAM GUSSET. REMOVED AND REPLACED LH #3 FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02SDR HNAA2025100300663Floorbeam · corrodedF068549 CORROSION ON RH CROSS FLOORBOARD SUPPORT AT FRAME 28. R & R RH CROSS FLOORBOARD SUPPORT AT FRAME 28 IAW EMB 145 SRM 51-40-02.SDR HNAA2025100300662Floor Support · corrodedF068545 CABIN L/H OMEGA BEAM GUSSET BETWEEN FR-51/53 HAVE CORROSION. REMOVED AND REPLACED L/H OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02.SDR HNAA2025100300660Floor Support · crackedF068523 CABIN CENTER OMEGA BEAM GUSSET BETWEEN FR-39/42 HAVE CORROSION. REMOVED AND REPLACED CABIN CENTER OMEGA BEAM GUSSET BTW FR 39-42 (NO.4) IAW EMB 145 SRM 51-40-02SDR HNAA2025100300671Skin · crackedF066756 REAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT FR 77 BETWEEN STGR 6R / 7R. ACCOMPLISHED BUSHING REPAIR ON REAR FUSELAGE EXTERNAL SKIN AT FR 77 BETWEEN STGR 6R /7R IAW EO1-53-25-0351 AND EMB-145 SRM 53-32-01 RE, ITEM 9, FIGURE 213, SHEETS 1-3.SDR HNAA2023120400454Unknown · unknownAUTO FAIL WITH AUTO TRIM FAIL. OPS CHECK AUTOPILOT AND AUTO PILOT TRIM IAW 22-11-00. OPS CHECK GOOD CLEAR MEL 22-1-1.SDR HNAA2023051600160Unknown · unknownPACK 2 OVERHEAT DISPLAYED ON EICAS DURING TAKE OFF, AIR COND PACK N650 AND ABOVE AMENDED. R & R PACK 2 OVERTEMP SWITCH, TEMP SENSOR, AND CONDENSOR MIXER. RAN ENGINES AT POWER WITH BLEEDS AND PACKS ON. NO PACK 2 OVHT MESSAGE DISPLAYED AT THIS TIME. R/R #2 PASDR HNAA2023031100079Unknown · unknownVERTICAL STABILIZER LH AND RH SPHERICAL BEARING HOUSINGS ARE OUT OF DIMENSIONAL TOLERANCE. REPAIRED IAW EO1-55-23-0044SDR HNAA2023031000074Unknown · unknownCOCKPIT LH LATERAL BRACKET, LH OF OVERHEAD PANEL, BETWEEN FR 12 AND 13 CRACKED. REPAIRED IAW 145 SRM51-40-02SDR HNAA2023031000075None · nonePILOT'S BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED. REPAIRED IAW EO1-53-23-0046SDR HNAA2023031100082Unknown · unknownLH WING TIP UPPER ATTACHMENT FLANGE IS SCRATCHED. REPAIRED IAW EMB145 SRM 51-10-03 AND 57-20-07ADSDR HNAA2023031100080Unknown · unknownFRAME 65 IS CHAFED BETWEEN STRINGERS 2L-3L. REPAIRED IAW ETD 2023-145-004197SDR HNAA2023031000076Unknown · unknownRH FWD VERTICAL STAB TO FUSELAGE ANGLE HAS POSSIBLE CRACK AT MARKED LOCATIONS. REPAIRED IAW EMB145 SRM 51-40-02SDR HNAA2023031000073Unknown · unknownAFT UPPER L/H SIDE OF FUSELAGE FR78 HAS ONE (1) FASTNER WITH POSSIBLE CRACKED SKIN. REPAIRED IAW EO1-53-23-0042SDR HNAA2023031000072Unknown · unknownAFT UPPER L/H SIDE OF FUSELAGE FR78 HAS ONE (1) FASTNER WITH POSSIBLE CRACKED SKIN. REPAIRED IAW EO1-53-23-0042SDR HNAA2023030800064Unknown · unknownLEVEL 2 CORROSION ON CARGO DOOR SILL. REPAIRED IAW SRM 51-40-02, 51-20-03, AND 51-40-06SDR HNAA2023030800086Unknown · unknownLEVEL 2 CORROSION IN LAV FLOOR GUSSET BETWEEN FRAMES 59-61. REPAIRED IAW EMB145 SRM 51-10-03, 51-40-02, 51-20-03, AND 53-24-10ADSDR HNAA2023031100077Unknown · unknownLEVEL 2 CORROSION IN GALLEY FLOOR LH CROSSBEAM AT FRAME 18. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-01, AND 51-21-06.SDR HNAA2023030800068Unknown · unknownLEVEL 2 CORROSION ON CROSS BEAM BRACKET BETWEEN LH FLOOR GUSSET AND LH FLOOR SIL IN LAV AREA BETWEEN FRAMES 60-61. REPAIRED IAW EMB145 SRM 51-20-03 AND 51-40-02.SDR HNAA2023030800067Unknown · unknownLEVEL 2 CORROSION ON SPLICE BRACKET ON LH FLOOR SILL IN LAV BETWEEN FRAMES 60-61. REPAIRED IAW EMB145 SRM 51-20-03, AND 51-40-02.SDR HNAA2023030800066None · noneLEVEL 2 CORROSOIN IN LAV FLOOR GUSSET BETWEEN FRAMES59-61. REPAIRED IAW EMB145 SRM 51-10-03, 53-24-10AD, 51-40-02, AND 51-20-03.SDR HNAA2023030800065Unknown · unknownLEVEL 2 CORROSION ON LH #3 FLOOR SILL. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-03, AND 51-40-09SDR HNAA2023030800062Unknown · unknownLEVEL 2 CORROSOIN ON INTERNAL FUSELAGE REINFORCEMENT SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 20L-21L. REPAIRED IAW EMB145 SRM 51-40-02 AND SB145-53-0068 FIG 7 DETAIL A2SDR HNAA2023030800063Unknown · unknownLEVEL 2 CORROSION ON INTERNAL FUSELAGE SKIN PLATE BETWEEN FRAMES 62-63 STRINGERS 20L-21L. REPAIRED IAW EMB145 SRM 51-40-02 AND SB145-53-0068SDR HNAA2023010500018Clamp · looseON DESENT, ACFT THROUGH RAIN & TURBULENCE. A SUDDEN ELECTRICAL ODOR IN FLT DECK & GALLEY FOR APPROX 5 MINS. ODOR DISSIPATED ON ITS OWN WITHOUT CREW INPUT. AT GATE UNDER APU POWER NO ODOR NOTED. PERFORMED GVI UNDER INSTRUMENT PANEL IN COCKPIT, INSP CIRCUISDR HNAA2022111400302Localizer · faultedBOTH LOCALIZER SIGNALS UNRELIABLE ON APPROACH TO FWA. DIVERTED TO DAY. PERFORMED VOR/ILS SYSTEM OPERATIONAL TEST IAW AMM 34-32-00-700-801-A. VOR/ILS SYSTEMS #1 AND #2 OPERATIONAL TESTS PASSED. AIRCRAFT OK FOR SERVICESDR HNAA2022062300226None · nonePDIS 683 28-41 2646932 22JUN22 CLT CLOSE
AFTER TAKE OFF #1 FUEL QTY READ 0 AND TOTAL FUEL QTY READ 0
FACT 22JUN22 18:39 CLT
UPON ARRIVAL TO A/C FOUND FUEL QTY TO BE OPERATING NORMALLY. AS POSITIVE MX R&R FUEL CONDITIONING UNIT SDR HNAA2021102600523Control Unit · faultedFLAP FAILURE ON APPROACH, FLAP FAIL STUCK ON 14 DEGREES. R+R FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02-000/400-801-A. OPS CHECK GOOD OK FOR SERVICE.SDR HNAA2021052500224Indicator · faultedPDIS 683 28-41 2407312 21MAY21 GSP CLOSE
ON DECENT FUEL 1 QTY DISPLAYED 0LBS. 10 MINUTES LATER FUEL QTY 2 DISPLAYED 0LBS. BOTH INDICATIONS CAME BACK AFTER 1 MINUTE.
FACT 21MAY21 23:09 GSP
PERF ELEC FUEL QTY IND OPS CHECK IN REFSDR HNAA2021030800094Unknown · odorPDIS 683 21-01 2532571 08MAR21 FLO ASSGN
PACK 2 OVERHEAT WITH BURNING SMELL IN COCKPIT AND TR
OUBLE COOLING A/C. BURNING SMELL ALSO NOTICED WITH O
NLY PACK 1 RUNNING (NOTE: CREW STATED IT TAKES RUN
NING 3 MINS BEFORE SMESDR HNAA2021021100048Unknown · odorPDIS 683 21-01 2343301 10FEB21 SDF CLOSE
ON TAKEOFF AT APPROX 115KTS BURNING SMELL NOTICED IN FLIGHT DECK, FOLLOWED BY ICE COND A/ICE INOP MSG ON EICAS.
FACT 10FEB21 20:17 SDF
RAN AIRCRAFT WITH CREW, NO DEFECTS OR BURNING SMELLSDR HNAA2021010500004Switch · malfunctionedAFTER T/O SMOKE SMELL IN COCKPIT. SHORTLY AFTER PACK 1 OVERHEAT MESSAGE ON EICAS. PACK 1 SHUTDOWN AUTOMATICALLY AND SMELL DISAPPATED W/I 3-4 SECONDS. CW FIM TASK 21 51 00 810 803 A BLOCKS 1 AND 2. RAN WITH APU AND ENGINE NO EICAS MESSAGE/TRANSITORY COND. SDR HNAA2020120700336Pressure Switch · malfunctionedPDIS 683 27-21 2302681 05DEC20 ALB CLOSE. ON CLIMB OUT RUD 1-2 FAIL EICAS MESSAGE PRESENTED. PERFORMED QRH RUD SYSTEM 1 CAME BACK ONLINE. FACT 05DEC20 12:34 ALB. FOLLOWED EMB 145 FIM 27-22-00-810-804 A TO BLOCK 19 FOUND TO BE TRANSITORY CONDITION OF THE RUSDR HNAA2020051800149Sensor · failedFLAP FAIL EICAS MESSAGE ON ARRIVAL TO HTS WHEN FLAPS SELECTED TO 9 DEGREES WITH NO FLAP MOVEMENT. R&R'D L/H FLAP VELOCITY SENSOR IAW AMM 27-51-12. RAN FLAPS UP AND DOWN A COUPLE TIMES OPS CHECK GOOD AT THIS TIME.SDR HNAA2020050500148Warning System · false activationFLAP FAIL ON EICAS WHEN FLAPS SELECTED DOWN. TROUBLESHOT IAW FIM TASK 27-51-00-810-816-A, STEPS 1,2,3, OPS CHECK IAW 27-51-00-700-801-A. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.
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