Embraer EMB-145LR
Service difficulty reports · 36,797
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'EMB145LR' 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 aircraft_model_key = 'EMB145LR' 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 HNAA2023030600059None · nonePACK 2 OVRTEMP FOLLOW PACK SHUTDOWN MULTIPLE TIMES INFLIGHT. FOLLOWED FIM TASK 21-51-00. PERFORMED OPS CHECK IAW EMB 145 AMM 21-5-00. OPS CHECK GOOD. NO DEFECTS OR FAULT MESSAGES NOTED. THIS CLEARS MEL 21-15-1. OK FOR SERVICE.SDR SIMA20230304001None · noneRH OVERWING EMERGENCY LIGHT INOP.-C/A-RAR RH OVERWING LIGHT LAMP IAW 145 AMM 33-50-07. OPC GOOD. MEL ITEM RESTORED.SDR SIMA20230304002None · noneELECTRICAL BURNING SMELL IN PLANE. APU NOT RUNNING. GPU ATTACHED. PCA HEAT CART ATTACHED. ENGINES WERE NOT RUNNING-C/A-T/S IAW EMB 145 FIM 21-20-00-810-801-A. DUPLICATED CONDITIONS FOR OVER 1 HOUR THAT EXISTED AT TIME OF DISCREPANCY WITH PCA AIR BEING SUPPLIEDSDR HNAA202303060057None · noneDURING TAKE OFF ROLL STRONG SMOKE ODOR NOTED IN FLIGHT DECK AND CABIN. ODOR DISSIPATED WHEN RETURNING TO GATE.
HISTORY: SECOND OCCURENCE, NO HISTORY 30 DAYS
FACT 04MAR23 02:19 FLO
REMOVED BOTH PACK PANELS AND PERFORMED GVI - NO DEFECTS SDR HNAA2023030600056None · noneBURNING SMELL NOTED IN FLIGHT DECK AND CABIN UPON LANDING
HISTORY: NONE
FACT 04MAR23 20:46 FLO TROUBLE SHOT IAW FIM 21-20-00-810-801-A WITH NO DEFECTS NOTED. RAN APU AND PACKS INDEPENDENTANTLY WITH CREW WITH NO DEFECTS NOTEDSDR HNAA2023030600058None · noneMAIN PITCH TRIM INOP EICAS MESSAGE DURING CLIMBOUT, AUTO PILOT NOT SELECTED, FO FLYING
FACT 03MAR23 10:36 PHL
INSP CMC FOUND HSCU FAILURE. R&R'D HSCU IAW EMB 145 MM 27-40-01 OPS CHECK GOOD OK FOR SERVICESDR V0XR202304250001Beam · corrodedBAGGAGE DOOR LOWER DOOR FRAME BEAM CORRODED. REMOVED AND REPLACED BEAM ASSY IAW EMB 145 SRM 51-40-02SDR HNAA2023032400108Unknown · unknownPAX DOOR CUTOUT, THE FWD PAX DOOR FLOOR TRIM BRACKET IS CORRODED (LEVEL 2). REPAIRED IAW EMB145 SRM 51-10-03 AND 53-21-02AD.SDR HNAA2023032400102Unknown · unknownAREA AROUND LOWER FASTENER ON LH BANANA PANEL BETWEEN LAV/CARGO IS CORRODED (LEVEL 2). REPAIRED IAW SRM51-40-02SDR HNAA2023032400101Unknown · unknownRH BANANA PANEL BETWEEN LAV/CARGO IS CORRODED (LEVEL 2) AROUND LOWER FASTENER. REPAIRED IAW SRM 51-40-02.SDR HNAA2023031100081Unknown · unknownACCOMPLISH PERMANENT REPAIR OF RUDDER PROTRACTOR MISSING NUTPLATE. REAIRED IAW PIEDMONT EO 1-05-23-0053SDR SIMA20230302001Lamp · inoperativeLAMP INOP LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. OPS CHECK GOOD.SDR HNAA2023032400107Unknown · unknownPAX DOOR CUTOUT, THE AFT PAX DOOR FLOOR TRIM BRACKET IS CORRODED (LEVEL 2). REPAIRED IAW SRM 51-40-02.SDR SIMA20230301002Lamp · inoperativePHOTOLUMINESCNET LIGHT INOP MAIN CABIN DOOR LINER, EMERGENCY LIGHT ASSY, DAMAGED-C/A-RAR MAIN CABIN DOOR LINER, EMERGENCY LIGHT ASSY OPC GOOD IAW AMM 25-23-04SDR HNAA2023032400103Unknown · unknownFR 59 STRAP CHAFFED AT STR 8L. REPAIRED IAW SRM51-40-02 AND 51-20-01SDR V0XD20230320002Beam · corrodedCORROSION ON UPPER SURFACE OF HAT BEAM AT Y + 479 BETWEEN FR 59- FR 61. CORRECTIVE ACTION: CUT OUT DAMAGE ON HAT BEAM AROUND NUTPLATE ON R/H SIDE BTWN. FR 59-61 ( 2 LOCATIONS ) . FABRICATED 2 REPAIR DOUBLERS P/N: 2024-T3 .040. LOCATED DRILLED AND INSTALLED 2 NSDR V0XR202304210001Floorbeam · corrodedCABIN CENTER FLOOR BEAM AT FRAME 57 TO 61.5 IS CORRODED AROUND NUTPLATE HOLES. REMOVED AND REPLACED CENTER FLOOR BEAM IAW EMB 145 SRM 53-24-10, SRM 51-40-02, SRM 51-20-03SDR V0XD20230413001Seat Track · corrodedL/H SIDE SEAT TRACK BETWEEN FR 36-47 IS CORRODED BEYOND LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED L/H SIDE SEAT TRACK BETWEEN FR 36-47 IAW EMB 135/145 AMM 53-01-06. SEE AVMAX WORK ORDER 81033 WORK CARD 1115.SDR HNAA2023032400098Unknown · unknownRH CARGO FLOOR SILL #3 CORRODED (LEVEL 2). REPAIRED IAW SRM51-40-02SDR HNAA2023032400097Unknown · unknownLH CARGO FLOOR SILL #2 CORRODED(LEVEL 2). REPAIRED IAW SRM51-20-03 AND 51-40-02SDR HNAA2023032400096Unknown · unknownRH CARGO FLOOR SILL CORRODED (LEVEL 2). REPAIRED IAW SRM51-20-03 AND 51-40-02SDR HNAA2023032400095Unknown · unknownCARGO DOOR LOWER SILL CORRODED. REPAIRED IAW SRM 51-40-02SDR HNAA2023032400094Unknown · unknownFR 65 SHEAR CLIP IS CORRODED (LEVEL 2). REPAIRED IAW SRM51-10-03, 53-31-04, 51-20-03, AND 51-40-02SDR HNAA2023032400092Unknown · unknownFR 65 CORRODED (LEVEL2) AT STR18L. REPAIRED IAW SRM 51-40-02SDR V0XR2023031700002Beam · corrodedFLOOR BEAM AT RBL 479 BETWEEN FRAME 58 AND 61 IS CORRODED AROUND NUT PLATE HOLES. PART REPLACEDSDR V0XR20230317AV1Beam · corrodedCABIN FLOOR BEAM AT -479 BETWEEN FRAMES 58 AND 61 IS CORRODED AROUND NUT PLATE HOLES. PART REPLACEDSDR HNAA2023031000074Unknown · unknownCOCKPIT LH LATERAL BRACKET, LH OF OVERHEAD PANEL, BETWEEN FR 12 AND 13 CRACKED. REPAIRED IAW 145 SRM51-40-02SDR 4DPA2023022700001Hydraulic Line · leakingISSUE- CREW REPORTED AT APPROX 13,000FT DURING CLIMB OUT IN MIA HYD 1 LO QTY EICAS MESSAGE APPEARED. VERIFIED WITH MFD AND SHORTLY AFTER RECEIVED E1 HYD PUMP FAIL. RAN QRH AND RETURNED TO MIA. ON LANDING RECEIVED SPOILER FAIL AND HOT BRAKES INDICATION DUE TO HSDR HNAA2023022800055None · noneBLEED 2 LEAK EICAS MSG APPEARED IN FLIGHT. INSPECTED #2 BLEED LEAK AND FOUND #2 PYLON Y-DUCT LEAKING AT IDLE. TIGHTENED ALL DUCT CLAMPS AND GROUND RAN A/C AT POWER FOR OPS CHECK REF AMM 36-00-00-700-803-A. OPS CHECK GOOD AT THIS TIME.SDR HNAA2023022700054None · noneAFTER TAKE-OFF A BURNING SMELL WAS NOTED IN CABIN AND CIRCUIT BREAKER H-10 FOUND POPPED. (PASS SIGNS).
FACT 27FEB23 10:39 PHL T/S AND FOUND STERILE LIGHT TO BE THE CAUSE OF CB H-10 TO POP. DID NOT DETECT ANY UNUSUAL ODORS WHEN RUNNING PACKS AND WITHOUT. RSDR V0XD20230227001Seat Track · corrodedLH FLOOR SEAT TRACK HAS MULTIPLE SIGNS OF CORROSION AT FR 18 TO FR 24. CORRECTIVE ACTION: REMOVED AND REPLACED LH FLOOR SEAT TRACK AT FR 18 TO FR 24 IAW EMB 135/145AMM 53-01-06.SDR HNAA2023031000075None · nonePILOT'S BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED. REPAIRED IAW EO1-53-23-0046SDR HNAA2023032400106Unknown · unknownR/H EXTERNAL FUSELAGE SKIN CRACKED AROUND 2 RIVETS AT FR77 BETWEEN STR3R AND STR4R. REPAIED IAW PIEDMONT EO1-53-23-0061.SDR HNAA2023032400105Unknown · unknownL/H EXTERNAL FUSELAGE SKIN CRACKED AROUND 1 RIVET FR79 BETWEEN STR5L AND STR6L. REPAIRED IAW EO1-53-23-0060.SDR HNAA2023032400104Unknown · unknownEXTERNAL FUSELAGE SKIN HAS BURN MARK BETWEEN FR 14 AND FR 15 BETWEEN STR3R AND STR4R. REPAIRED IAW EO1-53-23-0069SDR HNAA2023022700053None · noneUPON TAKEOFF, CAB ALT AND RATE INDICATIONS SHOWED 0 FROM 2000 TO 8000 FT IN AUTO MODE.
FACT 24FEB23 21:52 CLT CYCLED CPAM C/B, PERFORMED PRESSURIZATION CONTROL SYSTEM FUNCTIONAL TEST IN AUTO MODE IAW AMM 21-31-00-700-802-A. SYSTEM OPS NORMAL, OK FOR SERVISDR V0XD20230406003Frame · chafedCHAFFING AND ARCING DAMAGE TO FRM 3 BETWEEN STGR 15R-17R, FWD ELECTRONICS BAY. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR DOUBLER AT FRM 3 BETWEEN STGR 15R-17R IAW ETD2023-145-007395 REV 1. SEE AVMAX WO: 81033 WC: 1109.SDR 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 4DPA2023022300001Pump · leakingISSUE- CREW REPORTED THEY RECEIVED A HYD2 LO QTY ADVISORY FOLLOWED BY ENG2 HYD PUMP FAIL. AND RETURNED TO DAL. CORR ACTION- MX R&R'D ENGINE DRIVEN PUMP ALL OPS AND LEAK CHECKS GOOD.SDR V0XD20230418001Seat Track · corrodedSEAT TRACK SUPPORT AT FR 35 Y=479.0 CORRODED BEYOUND LIMITS. CORRECTIVE ACTION : REMOVED AND REPLACED SEAT TRACK SUPPORT I\A/W SRM 51-40-02 SEE AVMAX WORK ORDER 81033 WORK CARD 1101SDR V0XD20230406002Floor Support · corrodedCABIN FLOOR SILL AT FRM 23-24 STGR 15L CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SILL AT FRM 23-24 STGR 15L IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-40-09. SEE AVMAX WO: 81033 WC: 1099.SDR V0XD20230317002Floor Support · corrodedCORROSION FOUND ON CABIN FLOOR SILL FR 48 - FR 52 STR 15 LEFT. CORRECTIVE ACTION IS TO REMOVE AND REPLACE WITH NEW L/H FLOOR SILL FR 48-52 STR 15L. IAW EMB 145 SRM 51-40-02. AVMAX WO 81033 WC 1098.SDR HNAA2023031100078Unknown · unknownLEVEL 2 CORROSION ON INTERNAL FUSELAGE REINFORCEMENT SKIN PLATE BETWEEN FRAMES 62-63 STRINGERS 20L-21L. REPAIRED IAW EMB 145 SRM51-40-02 AND 145-53-0068SDR V0XD20230313001Beam · corrodedFLOOR LATERAL BEAM AT Y 0.0 TO Y -479 AT FR 20 HAS SIGNS OF CORROSION. REMOVED AND INSTALLED FLOOR LATERAL BEAM P/N:145-20600-603 AND Y 0.0 TO Y - 479 AT FR 20 IAW EMB 145 SRM 51-20-03 AND 51-40-02.SDR HNAA2023030800064Unknown · unknownLEVEL 2 CORROSION ON CARGO DOOR SILL. REPAIRED IAW SRM 51-40-02, 51-20-03, AND 51-40-06SDR HNAA2023022200051None · noneSMOKE AND SMELL IN FLIGHT DECK IN ICING. WINDSCREENS SEEM DISCOLORED AT BOTTOM OF CENTER POST NO RELEVANT EICAS MESSAGES APPEARED DURING EVENT.
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