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 4DPA2023080400001Controller · failedISSUE CREW REPORTED YAW DAMPER WILL FAIL IN FLIGHT EVEN WITH THE AUTOPILOT OFF. RETURNED TO DALLAS. CORR ACTION MX R/R AUTOPILOT CONTROLLER OPS TEST GOOD.SDR HNAA2023080200259Unknown · unknownIN FLIGHT PTRIM BACK UP INOP DISPLAYED ON EICAS
FACT 29JUL23 18:31 PHL
PDPU THE AC/ PERFORMED OPS IAW AMM 27-40-00-700-802-A. OPS CHECK GOOD, OK FOR SERVICESDR HNAA2023080100258Unknown · unknownREJECTED T/O FOR WARNING MESSAGE T/O CONFIG AND CAUTION MSG BRAKE TEMP NO DISPLAY ON R/H BRAKE TEMP IND. C/W DEACTIVATION OF NO.4 BRAKE TEMP SENSOR IAW MEL APPENDIX 1, R & R BRAKE TEMP SENSOR #400 IAW AMM 32-47-01. OPS CHECK GOOD. OK FOR SERVICE. CLEAR MELSDR HNAA2023080100257Unknown · unknownON TAKE OFF POSSIBLE MULTIPLE BIRDSTRIKES. FACT 01AUG23 20:39 RIC SDR HNAA2023091800326Unknown · unknownE988431 ACCOMPLISH PERMANENT REPAIR PER FCD1-54-21-0017 RH PYLON - REPLACEMENT OF FWD PYLON LINKAGE FITTINGS AND BUSHINGS. ACCOMPLISHED PERMANENT REPAIR PER FCD1-54-21-0017 RH PYLON - REPLACEMENT OF FWD PYLON LINKAGE FITTINGS AND BUSHINGSSDR HNAA2023073000256Unknown · unknownIN CRUISE FLT, STRONG BURNING ODOR DETECTED IN CABIN & FLIGHT DECK. INSPECTED ACFT FOUND PACK 1 TO HAVE OVERTEMPED & MELTED ALL OF SLEEVES ASSOCIATED WITH PACK. RAN PACK 2 WITH APU & BOTH ENG BLEEDS WITH NO SMELLS NOTED. RAN ENGINES 2 TIMES AT MAX POWER ONSDR HNAA2023072800257Unknown · unknownON T/O ROLL #1 ENG OIL PSI PASSED THROUGH 120PSI. REF RR FIM 79-37-00-810-805 GRND RAN ENG 1 REF 71-00-00-810-804 RESULTS ACCEPTABLE PER FIG 201 A/C OK FOR SERVICESDR HNAA2023072700255Unknown · unknownCREW CALLED WITH REJECTED T/O. AT 80 KTS THEY GOT A STEER INOP MSG WITH A "NO CONFIG" MSG. IRREGULARITY CLEARED USING NORMAL CREW PROCEDURESSDR HNAA2023072500314Unknown · unknownHN00103339 CORROSION FOUND ON RH FLOOR SILL BETWEEN FRM 52-48. REMOVED RH FLOOR SILL BETWEEN FRM 52-48 IAW EMB145 SRM 51-40-02-PR. LOCATED AND DRILLED NEW SERVICEABLE R/H FLOOR SILL (P/N: 145-25800-016) BETWEEN FR 48 & 52 FRM 22-29 IAW EMB 145 51-20-03-PR. ISDR HNAA2023080700294Unknown · unknownE987694 RUDDER 2 RIB ZV 1171.0 DAMAGED AT AFT FASTENER HOLE ON LH AND RH SIDES AND HAS TOOLING MARKS ON LH SIDE AT AFT END. FABRICATED SERVICEABLE RUDDER 2 RIB ZV-1171.0 AND INSTALLED SERVICEABLE RUDDER 2 RIB ZV-1171.0 IAW ETD# ETD2023-145-018625 AND EMB 145 SDR HNAA2023072500253Unknown · unknownSPOILER FAIL MSG ON EICAS AFTER TAKEOFF, SPOILERS WERE OPENED AND STAYED OPEN. T/S PER FIM TASK 27-63-00-800-806-A, BLOCKS 1 TO 5,15, 21 GROUND SPOILER VALVE FOUND TO BE DEFECTIVE PER FIM R&R GROUND SPOILER VALVE IRT AMM 27-62-03. OPS CHECK / LEAK CHECK GOOD SDR HNAA2023072500254Unknown · unknownLAV SMOKE INDICATION IN FLIGHT WITH VAPE LIKE FUMES VISUALLY INSPECTED LAV AND LAV INDICATOR FOR DEFECTS. NO DEFECTS NOTED AT THIS TIME PERFORMED LAV SMOKE DETECTION OPS CHECK IAW AMM 26-14-00 OPS CHECK OK. A/C OK FOR SERVICE.SDR HNAA2023072400318Unknown · unknownHN00103354 CORROSION FOUND ON CROSSBEAM BETWEEN -479 AND + 479 AT FRM 25. BLENDED CORROSION ON LH CROSSBEAM AT FRM28 BETWEEN Y-479 AND LH FLOOR SILL AS PER STEPS 1 - 5.A.(6) IAW EMB-145 SRM 51-10-03-PR. FOUND TO BE WITHIN LIMITS IAW EMB-145 SRM 53-22-10-AD.SDR 4DPA2023072400002Unknown · unknownISSUE; CREW REPORTED SHORTLY AFTER TAKEOFF GOT IECAS MESSAGE BAGGAGE DOOR OPEN, WE ALSO WENT MFD PAGE T/O IT SHOWS BAGGAGE DOOR OPEN, ASK THE FLIGHT ATTENDANT TO LOOK BACK AND VERIFY IF THERE’S ANY LIGHT COMING THROUGH SHE VERIFIED IT WAS SUNLIGHT COMING THROUSDR 4DPA2023072400001Duct · leakingISSUE; CREW REPORTED BLEED 1 OVER TEMP WARNING MESSAGE. BLEED 1 TEMP IN RED. RAN QRH AND RETURNED TO KLAS. CORR ACTION; MX FOUND PRE COOLER DUCT UNSERVICEABLE ON THE AIRCRAFT. REMOVED AND REPLACED THE PRE COOLER DUCT. OPS AND LK GOOD.SDR HNAA2023080700295Unknown · unknownE987413 LH AND RH RUDDER EXTERNAL SKIN DENTED/CRACKED AT FASTENER HOLE JUST FWD OF TRAILING EDGE ON RIB ZV 1171.0. ACCOMPLISHED REPAIR OF THE LH AND RH RUDDER 2 SKIN AT RIB ZV-1171.0 IAW ETD2023-145-018320 AND PIEDMONT EO1-55-23-0212SDR HNAA2023072300252Unknown · unknownAT ALTITUDE LEFT FUEL QUNTY DROPED AT FASTER RATE OF FUEL BURN THEN CACULATED, DIVERTED TO MDT AS PRECAUTION. MEASURE STICKS CONFIRMED LEFT INDICATION FAULTY
MEL 23JUL23 12:39 MDT B20412 28-9
WING TANK FUEL QTY INDC EICAS MFE
FACT SDR HNAA2023071900251Unknown · unknownON CLIMBOUT #2 ENGINE OIL TEMP REACHED 140C. R&R ENGINE #2 OIL TEMP/PRESSURE SENSOR IAW ROLLS-ROYCE MM 79-31-10. OPS CHECK GOOD. OK FOR SERVICE. DOWNLOADED CMC WITH NO EXCEEDANCE MESSAGES FOUND.SDR HNAA2023071900250Unknown · unknownT/O CONFIG SPOILER REJECTED TAKEOFF. MX PERFORMED SPOILER OPERATIONAL TEST. OPS CHECK GOOD NO DEFECTS NOTED, AIRCRAFT RETURN TO SERVICE.SDR HNAA2023071800249Unknown · unknownDURING TAKEOFF SPOILER FAIL DISPLAYED ON EICAS. WITH SPOILER I/B FAIL DISPLAYED ON CMC. FOUND "SPOILER IB FAIL" ON CMC. INSPECTED I/B SPOILERS PROX SENSORS WITH NO DEFECTS NOTED. REMOVED AND REPLACED RELAYS K0059 AND K0362 IN REF TO AMM 20-13-000/400-801-ASDR HNAA2023071700248Unknown · unknownPITOT 2 INOP EICAS MESSAGE DISPLAYED. T/S W/U FOR PITOT 2 MSG ON EICAS. R/R RELAY K0054 IAW AMM 30-31-01 NO FIX. SLAVED IN PITOT 2 SENSOR. HEAT CAME ON. TEMPORARILY REINSTALLED OLD PITOT SENSOR. REQUIRES FURTHER T/S.SDR 4DPA2023071600001Unknown · unknownISSUE-BLEED 1 OVER TEMP WARNING MESSAGE. BLEED 1 TEMP IN RED. RAN QRH AND RETURNED TO KLAS. CORR ACTION NOT YET COMPLETED CURRENTLY STILL MEL'D EXPIRES 7/26.SDR HNAA2023080700285Floorbeam · corrodedLAV CENTER FLOORBEAM GUSSSET HAS LEVEL 1 CORROSION. BLENDED CORROSION ON LAV FLOORBEAM GUSSET IAW EMB145 SRM 511003. UPON INVESTIGATION LAV CENTER FLOORBEAM GUSSET ORIGINAL THICKNESS SHOWN IN SRM 53-24-10AD SHOWS TO HAVE NOMINAL THICKNESS=.040". REMAINING TSDR HNAA2023071750247Unknown · unknownEICAS BLANKED OUT WITH BURNING SMELL SWAPPED EICAS AND FO MFD IAW AMM 34-22-01 PER MEL 34-1. OPS CHECK GOOD. INSPECTED ELECTRICAL CONNECTORS WITH NO DEFECTS NOTED. SEE THIS LP SEQ 2 FOR MEL. SWAPPED EICAS AND FO MFD DUE TO EICAS BLANKING OUT WITH BURNING SSDR HNAA2023080700284Unknown · unknownE986248 REAR FUSELAGE SKIN BUSHING REPAIRS AT FR 77 STGR 4R-5R (LOWER BUSHING), AND STGR 8R-9R. REQUIRE DT INSPECTION IAW EMB 145 SRM 53-32-01, ITEM 10. ACCOMPLISHED DVI ON REAR FUSELAGE SKIN BUSHING REPAIRS AT FR 77 STGR 4R-5R (LOWER BUSHING), AND STGR 8R-9SDR HNAA2023071400246Unknown · unknownBURNT RUBBER SMELL IN FLIGHT DECK AND CABIN. INSP COCKPIT NO-DEFECTS NOTED RAN BOTH PACKS ON APU BLD NO BURNING SMELL NOTED GROUND RAN BOTH ENGINES OPS 1&2 SYS AND BOTH PACKS. NO BURNT RUBBER SMELL NOTED A/C OK FOR SERVICE AT THIS TIMESDR HNAA2023080700289Unknown · unknownE986166 EXTERNAL FUSELAGE REPAIR FRAME 7-8 STR 13L-15L HAS NO DTI INFO. : RECEIVED PIEDMONT EO1-05-23-0186 FOR EXISTING EXTERNAL FUSELAGE REPAIR AT FR 7-8 AND BTW STR 13L-15L. EO ACCEPTS REPAIRED AREA AS IS AND HAS INSTRUCTIONS FOR DTISDR HNAA2023080700283Unknown · unknownUNDER AFT BELLY PANEL EXTERNAL FUSELAGE STGR 19R REPAIR BTW FR 52--53 NO REPAIR INFO. REMOVED PREVIOUS REPAIR UNDER AFT BELLY PANEL EXTERNAL FUSELAGE STR 19R BTW FR 52-53 WITH NO REPAIR INFORMATION AND REPAIRED STR 19R IAW PIEDMONT EO EO1-53-23-0211 AND EMB 1SDR HNAA2023080700282Unknown · unknownUNDER AFT BELLY PANEL EXTERNAL FUSELAGE STGR 19L PREVIOUS REPAIR IS CHAFED BTW FR 52-53. REMOVED CHAFED PREVIOUS REPAIR UNDER AFT BELLY PANEL EXTERNAL FUSELAGE STR 19L BTW FR 52-53 AND REPAIRED STR 19L IAW PIEDMONT EO1-53-23-0210 AND EMB 145 SRM 53-24-02RE ITSDR HNAA2023080700279Unknown · unknownCARGO DOOR WEBBING PREVIOUS REPAIR AT FWD LOWER ENDIS GOUGED. : REMOVED GOUGED DOUBLER, FABRICATED AND INSTALLED SERVICABLE NEW DOUBLER TO CARGO DOOR WEBBING AT HB4 AND FWD EDGE IAW EMB 145 SRM 52-30-01 RE SECTION 12 FIGURE 213 AND PIEDMONT EO1-52-23-0185.SDR 4DPA2023071300001Bleed Valve · failedCREW REPORTED APU BLEED AND BLEED 1 FAIL MESSAGE IN CLIMB. RAN QRH AND RETURNED TO LAS. MX OPS TESTED BLEED 1 NO FAULT FOUND. MX TROUBLESHOT APU BLEED AND FOUND BAD APU BLEED VALVE. R&R'D APU BLEED VALVE OPS AND LK CHECK GOODSDR HNAA2023080700293Pressure Deck · crackedCOCKPIT UNDERFLOOR MAINTENANCE HATCH CUTOUT LH BRACKED HAS LEVEL 1 CORROSION BETWEEN BRACKET AND SKIN. BLENDED AREA ON COCKPIT UNDERFLOOR BETWEEN BRACKET AND SKIN IA ACCEPTED PERMANENT REPAIR IAW ETD2023-145-017636SDR HNAA2023080700288Unknown · unknownE985348 STRINGER 6R CRACKED BEHIND FRAME 13 R/H SIDE OF COCKPIT. EMOVED AND REPLACED STRINGER 6R BEHIND FRAME 13 R/H SIDE OF COCKPIT IAW EMB145 SRM 51-40-02.SDR HNAA2023080700287Unknown · unknownE985328 L/H WINDSHIELD LATERAL POST UPPER ATTACH POINT SKIN CRACKED JUST FWD OF SPEAKER. RAR L/H WINDSHIELD LATERAL POST IAW EMB 145 SRM 51-40-02.SDR HNAA2023080700292Unknown · unknownE985210 R/H #2 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED WITH SERVICABLE R/H #2 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.SDR HNAA2023080700291Unknown · unknownE985209 R/H #1 FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED WITH SERVICEABLE R/H #1 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02SDR HNAA2023080700290Unknown · unknownE985174 PAX DOOR ENTRENCE AFT FLOORBOARD SUPPORT HAS CORROSION. REMOVED AND REPLACED PAX DOOR ENTRANCE AFT FLOORBOARD SUPPORT IAW EMB145 SRM 51-40-02SDR HNAA2023080700296Unknown · unknownE985046 LH WING RIB 21 IS CRACKED. FABRICATED FILER, DOUBLER AND SHIM, AND INSTALLED DOUBLER, SHIM, AND FILLER ON LH WING RIB 21 IAW EMB-145 SRM 57-20-07 RE 4. TABLE 202, DET. C, FIGURE 203 AND EO1-57-23-0199SDR 4DPA2023070700002Control Unit · failedISSUE- CREW REPORTED TANK 1 FLUCTUATES FUEL AMOUNT FOR INCORRECT READINGS LEADING TO FUEL IMBALANCE MESSAGES. BETWEEN FLUCTUATIONS, THE TANK 1 INDICATOR DASHES OUT INTERMITTENTLY. CORR ACTION- MX REMOVED AND REPLACED FCU OPS CHECK GOOD.SDR 4DPA2023070700001Unknown · unknownCREW REPORTED RUDDER OSCILLATIONS AFTER AUTOPILOT ENGAGED TO 14000 FEET THEN STOPPED, ALMOST AS THOUGH THE AIRCRAFT WAS OVER CORRECTING RUDDER INPUT. OSCILLATED TO THE EXTENT OF CAUSING THE AIRCRAFT TO NOT ROLL INTO TURN SMOOTHLY BUT RATHER ROLLED SO FAR AND SSDR HNAA2023060600245Unknown · unknownLEFT MAIN GEAR DISPLAYS INTERMITTENT WHITE AND AMBER ON EICAS, DURING RETRACTION AND THUMPING NOISE HEARD ON FIRST OFFICERS SIDE HYDRAULIC COMPARTMENT. R & R #100 UPLOCK BOX IAW AMM 32-33-10 UP TO STEP K6. AIRCRAFT REQUIRES FUNCTIONAL CHECK OF LDG EMERGENCYSDR V0XD20230705002Gusset · corrodedCENTER LAV FLOOR GUSSET LOCATED AT FRM 59-61 SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGED FLOOR GUSSET (P/N:145-22226-003) IAW EMB 145 SRM 51-40-02SDR HNAA2023060400244Unknown · unknownBLEED 1 LEAK DISPLAYED ON EICAS AFTER TAKE OFF. THIS LP BLEED 1 LEAK FACT 04JUL23 16:47 REMOVED BOTH PACK PANELS AND INSPECTED PACK AREA, NO DEFECTS NOTED. REINSTALLED PANELS AS REQ. INSPECTED AFT AVIONICS AREA, NO DEFECTS NOTED. REQUIRES FURTHER TROUBLESDR HNAAQ202307030024Unknown · unknownBLD 1 VLV CLOSED MSG IN FLIGHT. R&R ENG 1 BLEED VLV IAW AMM 36-11-05. NO FIX. R&R AIR COND. PNUMATIC PANEL IAW AMM 20-13-10. PERFORMED OPS CHECK IAW AMM 36-11-05 ON BOTH ENGINES. OPS AND LEAK CHECK GOOD. OK FOR SERVICE AT THIS TIMESDR HNAA2023070300242Unknown · unknownPACK 1 AND 2 VLV CLSD DURING CLIMB. FACT 02JUL23 14:08 CLT
R&R'D 2 SLEEVES ON DSCV ON #1 SIDE ASSDR HNAA2023080700300Unknown · unknownE983801 SSI 53-30-03 CORROSION ON SHEAR CLIP AT BAGGAGE DOOR CUT-OUT AT FRAME 65 PREVIOUS REPAIR. REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP AT BAGGAGE DOOR CUTOUT AT FRAME 65 IAW EMB 145 SRM 53-31-04 AND PIEDMONT EO1-53-23-0194.SDR HNAA2023080700299Unknown · unknownE983799 SSI 53-30-03 CORROSION ON SHEAR CLIP AT BAGGAGE DOOR CUT-OUT AT FRAME 68 PREVIOUS REPAIR. REMOVED AND INSTALLED SERVICEABLE FRAME 68 SHEAR CLIP LOWER SECTION IAW EMB 145 SRM 53-31-04 AND PIEDMONT EO1-53-23-0193.SDR HNAA2023080700286Unknown · unknownE983976 RH WING RIB 21 AND UPPER SUPPORT "L" SHAPED PROFILE CRACKED. INSTALLED DOUBLER, FILLER, SHIM & "L" SHAPED BRACKET ON RH WING RIB 21 IAW EMB-145 SRM 57-20-07 RE 4. STEPS I & K, DET. B & C, FIGURE 203 AND PIEDMONT EO1-57-23-0190,SDR HNAA2023070100241Unknown · unknownHYD 1 LOW QUANTITY DISPLAYED CRZ
FACT 01JUL23 13:10 PHL
FOUND NO. 1 ENGINE HYD PUMP LEAKING. R/R NO. 1 HYD PUMP IAW EMB 145 MM 29-10-03. OPS CHECK AND LEAK CHECK GOOD.SDR HNAA2023080700298Unknown · unknownE983490 FRAME 22 CORRODED AT SERVICE DOOR CUT-OUT LOWER AFT CORNER. CUT, FABRICATED, DRILLED AND INSTALLED FR 22 REPLACEMENT SECTION BTW STGR 11R-18R AND L-ANGLE SPLICES IAW EMB 145 SRM 53-00-04 ITEM 17 FIGURE 209, ETD# ETD2023-145-017207, EO1-53-23-0196, AND
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