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.

SDR ASOA201704243109Seat Track · corrodedCABIN RT OUTBOARD SEAT TRACK NR 4 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-06-400-801-A.Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201704243108Seat Track · corrodedCABIN RT OUTBOARD SEAT TRACK 3 CORRODED. SEAT TRACKED 3 REPLACED IAW AMM 53-01-06-400-801-AApr 24, 2017 · N13988 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201704243107Seat Track · corrodedRT CABIN SEAT TRACK NR 1 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-06-400-801AApr 24, 2017 · N13988 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201704243106Shear Tie · crackedFRAME 80 RT SHEAR TIE CRACKED. THE SHEAR TIE WAS REPLACED IAW 51-40-02Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Internal Mounting StructureSDR ASOA201704243105Shear Tie · crackedFRAME 80 LT SHEAR TIE CRACKED. THE SHEAR TIE WAS REPLACED IAW 51-40-02.Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Internal Mounting StructureSDR ASOA201704243103Bushing · corrodedHORIZONTAL STAB RT PIN BUSHING CORRODED. PIN BUSHING REPLACED.Apr 24, 2017 · N13988 · Emb EMB145LR · Horizontal Stabilizer StructureSDR ASOA201704243104Pin · corrodedHORIZONTAL STAB RT PIN CORRODED. PIN REPLACED IAW MM 55-10-01Apr 24, 2017 · N13988 · Emb EMB145LR · Horizontal Stabilizer StructureSDR ASOA201704243102Bushing · corrodedHORIZONTAL STAB LT PIN BUSHING CORRODED. BUSHING REPLACED IAW MM 55-10-01.Apr 24, 2017 · N13988 · Emb EMB145LR · Horizontal Stabilizer StructureSDR ASOA201704243101Channel · corrodedSERVICE DOOR LOWER CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.Apr 24, 2017 · N13988 · Emb EMB145LR · Service DoorsSDR ASOA201704243100Angle · crackedCOCKPIT LT FRAME 10, UPPER ANGLE CRACKED. THE FRAME ANGLE WAS REPLACED IAW SRM 51-40-02.Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201704243099Frame · crackedCOCKPIT RT FRAME 10 CRACKED. THE FRAME WAS REPLACED IAW SRM 51-40-02.Apr 24, 2017 · N13988 · Emb EMB145LR · Fuselage Main, FrameSDR SIMA20170423001Light · inoperativeEMERGENCY LIGHT AFT OF THE EMERGENCY ROW SEATING INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-50-12.Apr 23, 2017 · N933JN · Emb EMB145LR · Emergency LightingSDR SIMA20170423002Charger · inoperativeAFT FACING EXIT LOCATOR SIGN AT ROW 12 WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER NR 3 IAW AMM 33-50-04 AND INVERTER NR 4 IAW AMM 33-50-11 OPS CHECKED GOOD AT THIS TIME.Apr 23, 2017 · N698CB · Emb EMB145LR · Emergency LightingSDR HNAA2017052600188Relay · burnedDURING INSPECTION OF PIVOT, NR 3 RELAYS AND SOCKET CIRCURITY, FOUND WIRE W102027016 BURNED ALONG WITH SOCKET IN RECEPTICLE WIRE W102-0288-16 WAS BURNED ALONG WITH SOCKET 2 IN RECEPTICLE, RELAY SHOWED EVIDENCE OF BURNING, MELTING, AND DISCOLORATION, ALL WIRES Apr 22, 2017 · N635AE · Emb EMB145LR · Pitot/Static Anti-Ice SystemSDR SIMA20170421001Flashlight · inoperativeF/A TRIED TO USE THE FWD FLASHLIGHT ON ARRIVAL AND WOULD NOT COME ON. REMOVED AND REPLACED FLASHLIGHT, OPS CHECK IAW STANDARD MAINT PRACTICES, OPS CHECKED GOODApr 21, 2017 · N689EC · Emb EMB145LR · Emergency EquipmentSDR SIMA20170420001Battery Pack · inoperativeDURING PS-2 INSPECTION FOUND LT EXTERIOR AFT OVERWING LIGHT INOPERATIVE. REMOVED AND REPLACED NR3 BATTERY AND CHARGER IAW AMM 33-50-04. REMOVED AND REPLACED LT EXTERIOR AFT OVERWING LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD.Apr 20, 2017 · N905JH · Emb EMB145LR · Emergency LightingSDR ASOA201704203098Crossbeam · crackedNLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.Apr 20, 2017 · N13988 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201704203097Crossbeam · crackedNLG UPLOCK FORWARD CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.Apr 20, 2017 · N13988 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201704203096Crossbeam · crackedNLG UPLOCK AFT CROSSBEAM CRACKED. THE UPLOCK CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.Apr 20, 2017 · N16987 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201704203095Crossbeam · crackedNLG UPLOCK FORWARD CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.Apr 20, 2017 · N16987 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201704203094Crossbeam · crackedNLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.Apr 20, 2017 · N17984 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201704203093Crossbeam · crackedNLG UPLOCK FORWARD CROSSBEAM CRACKED. FORWARD CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.Apr 20, 2017 · N17984 · Emb EMB145LR · Fuselage Main, StructureSDR SIMA20170419001Warning Message · illuminatedHIGH SPEED ABORT FOR MASTER WARNING SPS 1-2 INOPERATIVE, AT 120 KTS. NORMAL BRAKING AND NO OVERHEATING ON BRAKES. -TIGHTENED SPC MOUNTING TRAY KNOBS AS NEEDED. PERFORMED OPS CHECKS IAW AMM 27-36-00. OPS CHECKS GOOD.Apr 19, 2017 · N617AE · Emb EMB145LR · Elevator Control SystemSDR ASOA201704193092Skin · corrodedON CARGO LOWER SKIN, AFT LOWER SKIN, AFT RADIO ALTIMETER 2 RETAINER CORRODED AND FWD RADIO ALTIMETER 2 R/H FWD DOME NUT BROKEN. FR 65 ANTENNA BASE CLEANED UP AND ANTENNA INSTALLED WITH NEW RETAINER. HFEC PERFORMED ON FR 65 AND 68 AFTER BLENDING, AS PER ETD ANDApr 19, 2017 · N14543 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA201704193091Post · crackedCRACK FOUND ON THE RT FWD LATERAL WINDSHIELD POST STARTING FROM THE FIRST TOP INBOARD RIVET. THE WINDSHIELD POST WAS REPAIRED IAW ETD2017-145-029522.Apr 19, 2017 · N14543 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201704193090Skin · crackedFUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 21. SKIN REPAIRED WITH DOUBLER AS PER SRM 53-31-01. PARA II, FIG 219 SHEET 1.Apr 19, 2017 · N14543 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA201704193089Skin · crackedRIGHT FUSELAGE SKIN CRACKED AT FRAME 75, NEAR STRINGER 2R. THE SKIN WAS REPAIRED IAW SRM 53-31-01, PARA II, FIG 219, SHEET 1.Apr 19, 2017 · N14543 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA201704193088Stringer · crackedREAR FUSELAGE TOP STRINGER 2L AND 2R CRACKED AT FRAME 75. STRINGER REPAIRED IAW SRM 53-00-03, ITEM 3, FIG 202.Apr 19, 2017 · N14543 · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR SIMA20170418005Light · dimFORWARD FLOOR EMERG LIGHT STRIP DIM. REMOVED AND REPLACED FORWARD FLOOR EMERG LIGHT STRIP IAW AMM 32-50-12; OPS CK GOOD.Apr 18, 2017 · N676AE · Emb EMB145LR · Emergency LightingSDR SIMA20170418006Door · corrodedCARGO DOOR IS CORRODED AROUND 1 SCREW HOLE FWD LOWER END. ACCOMPLISHED DOUBLER AND FILLER REPAIR AROUND SCREW HOLE FWD LOWER END IAW ERS-EM-52MR-741.Apr 18, 2017 · N673AE · Emb EMB145LR · Cargo/Baggage DoorsSDR SIMA20170418001Handle · looseMAIN CABIN DOOR IS DIFFICULT TO OPEN. DURING DETAILED VISUAL INSPECTION, FOUND THE BOLTS FOR THE INTERNAL HANDLE BOX LOOSE. TIGHENED BOLTS AND PERFORMED SIDE HINGED MAIN DOOR ADJUSTMENT TEST. OPS CHECKED GOOD. OK FOR SERVICE. ALL WORK DONE IAW AMM 52-18-00.Apr 18, 2017 · N647AE · Emb EMB145LR · Passenger/Crew DoorsSDR ASOA201704183087Floor Support · corrodedCABIN LEFT FLOOR SUPPORT NR 6 CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02Apr 18, 2017 · N14543 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201704183086Post · crackedFRAME CRACKED ABOVE COCKPIT RT WINDOW LATERAL POST. RT LATERAL POST REPLACED AS PER SRM 51-40-02..Apr 18, 2017 · N14543 · Emb EMB145LR · Fuselage Main, StructureSDR SIMA20170417006Skin · crackedEXTERNAL FUSELAGE SKIN POSSIBLE CRACK AROUND FASTENER FR 78 STR 3L-4L. PREPPED, FABRICATED, DRILLED FILLERS (3 TOTAL) AND INSTALLED EXTERNAL FUSELAGE SKIN REPAIR AT FR 78 STRINGER 4L AREA IAW ERS-EM-53MR-2723.Apr 17, 2017 · N626AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA20170417007Frame · crackedFR 66 AT STR 16R HAS POSSIBLE CRACK ABOVE UPPER END OF SHEAR CLIP. REPAIRED FR 66 AT STR 16R ABOVE UPPER END OF SHEAR CLIP IAW ERS-EM-53MR-2706.Apr 17, 2017 · N626AE · Emb EMB145LR · Fuselage Main, FrameSDR SIMA20170417008Skin · crackedRT AFT FUSELAGE SKIN HAS CRACK AT CUT OUT FR 77 BELOW STR 7. PERFORMED PERMANENT REPAIR OF SKIN CRACK AT FR77 BELOW STR 7R IAW ERS-EM-53MR-2724.Apr 17, 2017 · N626AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA20170417005Spar · crackedRT WING SPAR 1 LOWER FLANGE IS CRACKED AT FIRST SCREW HOLE OUTBOARD OF RIB 9, FROM AFT SIDE OF HOLE REARWARD ALMOST TO RADIUS OF SPAR WEB. REPAIRED CRACK ON RT WING SPAR 1 IAW ERS-EM-57MR-811.Apr 17, 2017 · N626AE · Emb EMB145LR · Wing SparSDR SIMA20170417004Wire · damagedEMERGENCY LIGHT EXIT SIGN ON THE CEILING PANEL 233BLC INOP. REPAIRED WIRE ON EMERGENCY LIGHT EXIT SIGN ON THE CEILING PANEL 233BLC IAW SWPM 20-21-00. OPS CHECK IS GOOD.Apr 17, 2017 · N626AE · Emb EMB145LR · Light System WiringSDR SIMA20170417003Skin · crackedCRACK AROUND RIVET ON FRAME 75 AT STRINGER 2L. PERFORMED PERMANENT REPAIR OF CRACK AROUND RIVET ON FRAME 75 AT STRINGER 2L IAW SRM 53-31-01 RE FIG 219, SHEET 2.Apr 17, 2017 · N681AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA20170417002Light · inoperativeRT OVER WING EMERGENCY LAMP INOP. RELAMPED IAW AMM 33-50-10 OPS CHECK GOOD.Apr 17, 2017 · N699AE · Emb EMB145LR · Emergency LightingSDR SIMA20170416003Structure · corrodedEXTERNAL SIDE OF LAV BUCKET CORRODED AT DRAIN VALVE AFT UPPER CORNER. REMOVED AND INSTALLED NEW SERVICEABLE LAV BUCKET IAW SRM 51-40-02.Apr 16, 2017 · N685AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2017041700126Unknown · odorSTRONG BURNING ODOR THROUGHOUT ACFT DURING FLT, AT ABOUT 25K. ACFT IN HIGH ELECTRICFIED STATIC FIELD, NO VISABLE SMOKE, ANTI-ICE WAS OFF, APU WAS OFF. NO CIRCUIT BREAKERS FOUND TRIPPED. ODOR DISSIPATED DURING DESCENT. INSPECTED THE RIGHT RELAY SUPPORT PANEL Apr 16, 2017 · N636 · Emb EMB145LR · Air Distribution SystemSDR HNAA2017041700125Warning Message · illuminatedAFTER TAKEOFF, AND EICAS SHOWED A NR 1 BLEED LEAK MESSAGE.Apr 16, 2017 · N635 · Emb EMB145LR · Pneumatic Distribution SystemSDR HNAA2017041700124Clamp · looseNR 1 BLEED LEAK ECAS WARNING MESSAGE ALONG WITH LEAK ILLUMINATED ON THE NR 1 BLEED SWITCH. COMPLIED WITH THE QRH AND BOTH MESSAGES EXTINGUISHED. APU WAS OFF. INSPECTED THE DUCTS AND SENSE LINES AT THE NR 1 PRECOOLER AREA AND FOUND SEVERAL CLAMPS LOOSE. SECUApr 16, 2017 · N608 · Emb EMB145LR · Pneumatic Distribution SystemSDR SIMA20170415004Fitting · corrodedCARGO DOOR CUTOUT LATERAL L-SHAPE IS CORRODED AT LWR GUIDE PLATE ON FRAME 65. REPAIRED CARGO DOOR CUTOUT LATERAL L-SHAPE CORROSION AT LWR GUIDE PLATE ON FRAME 65 IAW SRM 53-31-04.Apr 15, 2017 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20170415005Skin · burned3 BURNS IN SKIN BETWEEN FRAMES 26-27 STRINGERS 21L-21R. REPAIRED FUSELAGE SKIN BURNS BETWEEN FRAMES 26-27 STRINGERS 21L-21R IAW SRM 53-22-01.Apr 15, 2017 · N681AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA20170415006Frame · corrodedFRAME 65 IS CORRODED AT LOWER GUIDE PLATE. FABRICATED AND INSTALLED REPAIR DOUBLER ON FRAME 65 AT LWR GUIDE PLATE IAW SRM 53-31-04, FIG 212, SHEET 2Apr 15, 2017 · N681AE · Emb EMB145LR · Fuselage Main, FrameSDR SIMA20170415002Rmu · failedAFTER POWER UP, THE NR 2 RMU FAILED, ACCOMPANIED WITH ELECTRICAL BURNING ODOR. R & R THE NR 2 RMU. CONFIRMED THE BURNING ELECTRICAL ODOR COMING FROM RMU IAW AMM 23-81-01-000-801/23-81-01-400-801. OPS CHECKED GOOD.Apr 15, 2017 · N689EC · Emb EMB145LR · Communications SystemSDR SIMA20170414008Floor Support · crackedCOCKPIT FLOOR SUPPORT CRACKED UNDER 221GF. PERFORMED PERMANENT REPAIR OF COCKPIT FLOOR SUPPORT CRACKED UNDER 221GF IAW ERS-EM-53MR-2680.Apr 14, 2017 · N630AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20170414006Spar · crackedLT WING SPAR I LEADING EDGE LOWER ATTACHMENT FLANGE IS CRACKED AT RIB 9. REPAIRED LT WING SPAR I LEADING EDGE LOWER ATTACHMENT FLANGE AT RIB 9 IAW ERS-EM-57MR-799.Apr 14, 2017 · N630AE · Emb EMB145LR · Wing Spar
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