Embraer EMB-145LR
Service difficulty reports · 36,795
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 HNAA2024052200448Floor Support · cracked53-2056 CTR FUSE 3 UNDERFLOOR, RH OMEGA BEAM AFT IB ANGLE CRACKED AT FR45-50. RAR BEAM IAW SRM51-40-02SDR HNAA2024052200447Floor Support · cracked53-2051 CTR FUSE 3 UNDERFLOOR, RH SILL BTW FR35-36 IS CRACKED. RAR SILL IAW SRM 51-40-02SDR HNAA2024052200446Doubler · corroded53-2041 DOUBLER CORRODED ON RH BEAM AT FR22. RAR IAW SRM 51-40-02SDR HNAA2024052200445Doubler · corroded53-2040 DOUBLER CORRODED ON RH BEAM AT FR20. RAR DOUBLER IAW SRM 51-40-02SDR HNAA2024052200444Beam · corroded53-2039 SERVICE DOOR CUTOUT LWR BEAM CORRODED BTW FR20-22. RAR BEAM IAW SRM 51-40-02SDR HNAA2024052200443Gusset · corroded53-2037 CTR GUSSET CORRODED AT BTW FR20-23. RAR GUSSET IAW SRM 51-40-02SDR HNAA2024052200442Shear Tie · cracked53-2034 SHEAR CLIP CRACKED AT FR15 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02SDR HNAA2024052200441Support · corroded53-2032 RH SILL #1 CORRODED. RAR SILL IAW SRM51-40-02SDR HNAA2024052200440Shear Tie · cracked53-2031 SHEAR CLIP CRACKED AT FR28 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02SDR HNAA20240500439Shear Tie · cracked53-2030 SHEAR CLIP CRACKED AT FR26 BTW 16R-17R.. RAR SHEAR CLIP IAW SRM 51-40-02SDR HNAA2024052200438Shear Tie · cracked53-2029 SHEAR CLIP CRACKED AT FR26 BTW 15-16R. RAR SHEAR CLIP IAW SRM 51-40-02SDR HNAA2024052200437Shear Tie · cracked53-2028 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02SDR HNAA2024052200436Shear Tie · cracked53-2027 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM51-40-02SDR HNAA2024052200435Floor Support · cracked53-2026 CTR OMEGA BEAM #1 CRACKED AND CORRODED AT FR29. REPAIRED IAW EO1-53-24-0245SDR HNAA2024052200434Floor Support · cracked53-2025 LH OMEGA BEAM #2 HAS 4 CRACKS AND CORROSION. RAR OMEGA BEAM IAW SRM 51-40-02SDR HNAA2024052200433Support · corroded53-2023 LH SILL #2 CORRODED. RAR SILL IAW SRM 51-40-02SDR HNAA2024051600420Shear Tie · crackedE031804 SHEAR CLIP IS CRACKED AT FRAME 56 BETWEEN STRINGERS 15L-16L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 56 BETWEEN STRINGERS 15L-16L IAW EMB145 SRM 51-40-02.SDR HNAA2024051600418Shear Tie · crackedE031786 SHEAR CLIP IS CRACKED AT FRAME 26 BETWEEN STRINGERS 15R AND 16R. : REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 15R AND 16R IAW EMB145 SRM 51-40-02.SDR HNAA2024051600416Shear Tie · crackedE031784 SHEAR CLIP IS CRACKED AT FRAME 24 BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15R AND 16R IAW EMB145 SRM 51-40-02.SDR HNAA2024051400391Skin · crackedE031667 LH AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 79. FABRICATED AND INSTALLED BUSHING AT LH AFT UPPER FUSELAGE SKIN ON FRAME 79 STR 3L-4L ,IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0303SDR HNAA2024051400390Skin · crackedE031665 LH AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUNDRIVETS ON FRAME 77. FABRICATED AND INSTALLED BUSHING AT LH AFT UPPER FUSELAGE SKIN ON FRAME 77 STR 4L-5L ,IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0303SDR HNAA2024051400389Skin · crackedE031613 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 80. FABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 80 STR 6R-7R IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0302SDR HNAA2023051400388Skin · crackedE031612 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 78. ABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 78 STR 4R-5R AND 6R-7R IAW EMB 145 SRM 53-32-01, ITEM 9, FIGURE 213 AND EO1-53-24-0302SDR HNAA2024051400387Skin · crackedE031611 RH SIDE AFT UPPER FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND RIVETS ON FRAME 77. FABRICATED AND INSTALLED BUSHING AT RH SIDE AFT UPPER FUSELAGE SKIN ON FRAME 77 STR 5R-6R IAW EMB 145 SRM 53-32-01. ITEM 9, FIGURE 213 AND EO1-53-24-0302SDR HNAA2024051400373Yoke · corrodedE031858 R/H ENG. FWD. ENGINE YOKE, FWD. FITTING HAS POSSIBLE CRACK. : REMOVED AND INSTALLED NEW R/H ENG. YOKE UPPER AND LOWER FWD. AND AFT LINKAGE IAW FCD1-54-21-0017DSDR HNAA2024050900336Rivet · corroded00119 CORROSION FOUND ON FWD RIB AND RIVET LINE IN RH WHEEL WELL. REMOVED AND REPLACED FWD RIB P/N 145-72022-002 AT RH WHEEL WELL IAW EMB 145 SRM 51-40-02SDR HNAA2024052200432Skin · cracked53-2021 2 CRACKS BTW STR6R-8R AND FR77-78. REPAIRED IAW EO1-53-24-0247SDR HNAA2024052200431Skin · dented53-2020 DENT ON FUSELAGE 3" FWD OF FR23 AND 2" ABOVE STR13L. REPAIRED IAW EO1-53-24-0253SDR HNAA2024052200430Skin · gouged53-2017 MULTIPLE GOUGES FOUND ON FUSELAGE EXTERNAL SKIN AT FR7-8 STR20R-21R. REPAIRD IAW EO1-53-24-0260SDR HNAA2024052200429Skin · dented53-2014 DENT FOUND ON FUSELAGE SKIN ON FR9 AND 6" ABOVE STR20L. REPAIRED IAW EO1-53-24-0264SDR HNAA2024051600415Door Frame · damagedE031373 SERVICE DOOR AFT FRAME IS CORRODED AT BOTTOM SCREW HOLE PREVIOUSLY BLENDED PAINTED BLUE. PERFORMED FRAME SPLICE REPAIR ON SERVICE DOOR AFT FRAME CUTOUT AND INSTALLED SERVICEABLE LOWER FRAME SECTION (FR22) IAW PIEDMONT EO1-53-24-0285, ETD2024-145-01121SDR HNAA2024051600414Access Panel · crackedE031218 POSSIBLE CRACK ON RH WING RIB 21 UNDER ACCESS PANEL 651CB. PERFORMED PERMANENT REPAIR TO CRACK ON R/H WING RIB 21 UNDER ACCESS PANEL 651CB IAW PIEDMONT EO1-57-24-0314, EMB 145 SRM 57-20-07, ITEM#4, FIGURE 203.SDR HNAA2024051600413Rib · gougedE031190 LH OTBD WING TIP RIB 25 LOWER AND UPPER SURFACE IS SCRATCHED AND GOUGED. REMOVED AND REPLACED LH OTBD WING TIP RIB 25 IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03.SDR HNAA2024042900326Acm · inoperativeIN CRUISE FLT AT FL 240 BURNING SMELL NOTED ON FLT DECK. SMELL DISAPPATED AFTER ABOUT 2 MIN. SMELL ALSO REPORTED IN CABIN FACT 10APR24 20:52 MDT FOUND #100 AIR CYCLE MACHINE INOP.R&R'D ACM POS #100 IRW 21-51-03. OPS CHECKS SYSTEM IRW 21-51-00 OPS CHECKS OKSDR HNAA2024051400386Angle · corrodedE031084 LH VERTICAL STAB TO FUSELAGE ANGLE HAS POSSIBLE CRACK TOWARDS THE FWD END. RAR CRACKED LH VERTICAL STAB TO FUSELAGE ANGLE AND REPAIR ANGLE DOUBLER INCORPORATED WITH ANGLE IAW EMB 145 SRM 51-40-02SDR HNAA2024041000285Control Unit · faultedSPOILER WARNING MSG DURING T/O ROLL. REJECTED TO AT 90 KTS FACT 08APR24 13:22 PHL R/R SCU IAW AMM 27-63-02 OPS CHECK GOOD FDR COMFIRMED ISSUE OK FOR SERVICESDR HNA2024050900001Bonding Strap · corrodedCORROSION FOUND ON UPPER AND LOWER ATTACHMENT BRACKETS ON RH WING TIP. FABRICATED AND INSTALLED UPPER AND LOWER BONDING STRAPS ON R/H WINGTIP IAW EMB-145LR SRM 51-40-02SDR HNA202405090002Attach Bracket · corrodedCORROSION FOUND ON UPPER AND LOWER ATTACHMENT BRACKETS ON RH WING TIP. FABRICATED AND INSTALLED UPPER AND LOWER BONDING STRAPS ON R/H WINGTIP IAW EMB-145LR SRM 51-40-02SDR HNAA2024041000284Warning Message · illuminatedPACK 1 O/H ON T/O ROLL. RESET PACK NO FURTHER ISSUES. NO 30 DAY HISTORY. FACT 06APR24 06:38 SCE IRREGULARITY CLEARED USEING NORMAL CREW PROCEDURESSDR HNAA2024040400283Relay · faultedICE COND AND A/ICE INOP EICAS MESSAGES DISPLAYED ON T/O ROLL. REMOVED AN REPLACED RELAYS K0532 AND K0531 IAW AMM 20-13-02, PERFORMED OPS CEHCK IAW AMM 30-00-00 NO DEFECTS NOTED AT THIS TIME. OKAY FOR SERVICESDR 4DPA2024040200001Access Door · missingCREW REPORTED- AFTER GEAR RETRACTION WE HEARD LOUD WIND BLOWING NOISE AROUND THE FRONT OF THE AIRCRAFT. AS WE TRIED TO FIGURE OUT THE PROBLEM UPON REACTION 7-8 THOUSAND FEET THE FWD ACCESS DOOR OPEN EICAS MSG APPEARED. RETURNED TO BURBANK AND HAD IT INSPECTESDR HNAA2024040400282Relay · faultedTAT 1 INOP. CLEARED ON ITS OWN. FOUND TAT 1 C/B POPPED OUT. PUSHED IT BACK IN. A/C OK FOR SERVICE AT THIS TIME. R/R RELAY K0064 IAW AMM 20-13-02. TAT SENSORS OPS CHECK GOOD IAW AMM 30-33-00. OK FOR SERVICE AT THIS TIMESDR HNAA2024040400281Valve · faultedBLD 2 OVER TEMP DURING CLIMB BETWEEN 16K AND 18K IN ICING CONDITIONS. REMOVED AN REPLACED #200 FAN AIR VALVE IAW AMM 36-11-03. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.SDR HNAA2024050100329Warning Message · false activationBRAKE DEGRADED EICAS MESSAGE, LH IB BRAKE NO TEMP RISE AND LACK OF BRAKING FACT 30APR24 16:25 LYH CYCLED CBS A7, A27, E16, AND E19. VERIFIED BRAKING OPERATIONS. PERFORMED TAXI CHECK WITH CREW. NO DEFECTS NOTED. A/C OK FOR SERVICE.SDR 4DPA2024040100001Landing Gear · lack of lubeCREW REPORTED; ON CLIMB OUT, VERY LOUD BANGING NOISE WHEN LANDING GEAR RETRACTED. CORR ACTION; MX PERFOMRED DETAIL INSPECTION OF LANDING GEAR AND LANDING GEAR SYSTEMS. LUBRICATED ALL GEAR. PERFORMED OPERATIONAL GEAR SWINGS ON AIRCRAFT. OP CHECK GOOD.SDR HNAA2024040200246Control Unit · faultedPITCH TRIM MAIN INOP IN FLIGHT. FACT 02APR24 03:58 FWA TROUBLE SHOT PER FIM TASK 27-43-00-810-803-A NO EICAS MESSEGE UPON ARRIVAL R/R HORIZONTAL STAB CONTROL UNIT IAW AMM 27-40-01. OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK FOR SERVICE.SDR HNAA2024040100237Sensor · false indicationBLEED 2 OVERTEMP MSG IN ICING CONDITIONS FACT 30MAR24 20:00 PHL R+R BLEED 2 TEMP SENSOR AT PRECOOLER IAW AMM 36-20-01. OPS CHECK GOOD IAW 36-00-00-700-806A AND 30-00-00-700-801A, 802BSDR HNAA2024040100236Display · inoperativeEICAS SCREEN WENT BLANK. FACT 29MAR24 20:52 CLT R/R EICAS DISPLAY IAW AMM 34-22-01 OPS CHK DONE IAW AMM 31-41-00 OPS CHECK GOOD A/C OK FOR SERVICESDR 4DPA2024032800001Warning Message · false activationCREW REPORTED- RAM AIR VALVE FAIL EICAS MESSAGE APPEARED AFTER DEPARTING KBJC AND NEVER FULLY PRESSURIZED DURING CLIMB OUT. CABIN ALT REACHED 10,000. RETURNED TO DEPARTURE AIRPORT. CORR ACTION- MX CND NO RAM AIR VALVE FAIL MESSAGE PRESENT. INSPECTED RAM AIR VASDR HNAA2024032800235Wire Harness · damaged#2 ENG HUNG START WITH HEAVY FUEL SMELL (ONLY 0N FADEC 2A). MEL 28MAR24 06:10 RIC B08803 74-1 IGNITION SYSTEM CHANNELS. FOUND DAMAGED/BENT PIN ON PMA A PLUG PIN A. R+R PIN A IAW RR MM 74-11-15. R+R W11 BLUE EXTERNAL HARNESS IAW RR MM 76-11-20. LEAK CK.
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