# Service difficulty reports: Embraer EMB-145

A list on [Embraer EMB-145](https://openairdocs.org/model/embraer-emb-145.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 61 · 3,003 reports

- [SDR OEJA2025082900001](https://openairdocs.org/sdr/OEJA2025082900001.md): Warning Message · illuminated · Aug 27, 2025 · N904FL · Emb EMB145 · Cabin Cooling System
  > ON CLIMB OUT HEADING TOWARDS 25,000 FT A PACK 2 VAILVE FAIL CAS MESSAGE APPEARED, WHE THE AIRCRAFT REACHED 25,000 THE CABIN BEGAN TO RAPIDLY RISE. CREW PERFORMED A EMEGANCY DESENT TO 10,000 FEET AND CHOSE TO DEVERT TP KRAP. LANDED THE AIRCRAFT SAFTLEY
- [SDR KY72024F00006](https://openairdocs.org/sdr/KY72024F00006.md): Sensor · defective · Jun 9, 2024 · N971DC · Emb EMB145 · Engine Indicating System
  > BLEED1 OVERTEMP IN FLIGHT ATB. REMOVED & REPLACED #1 HIGH TEMP THERMOSTAT 36-11-06, OPS CHECK GOOD.
- [SDR OEJA2023100900915](https://openairdocs.org/sdr/OEJA2023100900915.md): Unknown · unknown · Oct 5, 2023 · N307LL · Emb EMB145 · Service Doors
  > DEPARTING OMAHA, NEBRASKA KOMA FOR MCALLEN TEXAS KMFE THURSDAY AFTERNOON AT 2200Z, IMMEDIATELY AFTER TAKEOFF DURING CLIMB-OUT A SERVICE DOOR OPN FUEL DOOR INDICATION WAS PRESENTED VIA A WARNING LIGHT AND EIACAS MESSAGE.
- [SDR OEJA202301100026](https://openairdocs.org/sdr/OEJA202301100026.md): Control Box · failed · Jan 8, 2023 · N905FL · Emb EMB145 · Trailing Edge Flap Control System
  > UPON APPROACH IN TO KDRO WE STARTED TO CONFIGURE THE AIRCRAFT FOR LANDING. WHEN WE PUT THE FLAPS TO 9 WE RECEIVED A FLAPS FAIL CAUTION. WE THEN VECTORED AROUN A FEW MINUTES TO RUN THE QRH THEN DECIDED TO DIVER TO DKEN WHICH HAD A LONGER RUNWAY AND MORE OPT
- [SDR SIMA20221031004](https://openairdocs.org/sdr/SIMA20221031004.md): Light · unserviceable · Oct 31, 2022 · N613AE · Emb EMB145 · Emergency Lighting
  > DURING PS-1 CHECK FOUND EXTERNAL EMERGENCY LIGHT RH OVERWING INOP-C/A-RAR EXTERNAL EMERGENCY LIGHT ASSEMBLY RH OVERWING IAW EMB 145 AMM 33-50-10, OPS CHECK GOOD IAW EMB 145 AMM 33-50-00 NO FURTHER DEFECTS NOTED AT THIS TIME
- [SDR 9JLA2022031430862](https://openairdocs.org/sdr/9JLA2022031430862.md): Pcb · defective · Feb 21, 2022 · N10HC · Emb EMB145 · Central Display
  > THE FLIGHT CREW REPORTED THAT PRIOR TO TAXI THE 3 LEFT DISPLAY SCREENS ALL DISPLAYED RED X. THE MAINTENANCE TEAM DETERMINE THE IC-600 CARD WAS DEFECTIVE. THE CARD WAS REMOVED AND REPLACED WITH A REPAIRED CARD. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS
- [SDR 9JLA2021110324848](https://openairdocs.org/sdr/9JLA2021110324848.md): Power Unit · defective · Oct 23, 2021 · N10HC · Emb EMB145 · Alternator-Generator Drive
  > THE FLIGHT CREW REPORTED OF A "GEN 1 BEARING FAIL" ADVISORY MESSAGE DISPLAYED ON THE EICAS SYSTEM. OPERATIONS WERE CONTINUED PER MEL. THE MAINTENANCE VENDOR DETERMINED THE LEFT OUTBOARD POWER UNIT WAS DEFECTIVE AND WAS REPLACED WITH AN OVERHAULED UNIT. GROUND
- [SDR SIMA20210701001](https://openairdocs.org/sdr/SIMA20210701001.md): Battery Pack · inoperative · Jul 1, 2021 · N613AE · Emb EMB145 · Emergency Lighting
  > ROWS 8-12 EMERGENCY LIGHTS INOP-C/A-T/S IAW EMB FIM 33-50-00-810-804-A. FOUND #3 BATTERY BAD. RAR #3 BATTERY AND CHARGER IAW ENVOY W/C 33-700-19. OPS CHECK GOOD. NO DEFECTS NOTED. END.
- [SDR SIMA20210517004](https://openairdocs.org/sdr/SIMA20210517004.md): Control Module · faulted · May 17, 2021 · N610AE · Emb EMB145 · Emergency Lighting
  > EMERGENCY LIGHT NOT ARMED CAUTION ON EICAS W/ EMERG LT SWITCH ARMED TRIED CYCLING MULTIPLE TIMES"TRANSFERRED TO NRWC 610-ORD-03512" GR 417418-C/A-RAR CONTROL MODULE IAW EMB 145 MM 33-21-01. OPS CK GOOD. REF NRWC 610-ORD-03512 FOR SUPPORTING ACTION
- [SDR KY7A20210503002](https://openairdocs.org/sdr/KY7A20210503002.md): A/C Pack · malfunctioned · May 3, 2021 · N972DC · Emb EMB145 · Cabin Cooling System
  > CREW REPORTED ON CLIMB OUT OF MSP THEY RECEIVED A PACK 1 FAIL CAS MESSAGE. WHEN TRYING TO RESET PACK 1, PACK 2 FAILED. WHILE TRYING TO RESET BOTH PACKS THEY NOTICED CABIN ALTITUDE BEGINNING TO RISE. CREW ASKED ATC TO LEVEL AT FL190, UPON LEVELING THE CABIN
- [SDR SIMA20210417003](https://openairdocs.org/sdr/SIMA20210417003.md): Bulb · inoperative · Apr 17, 2021 · N613AE · Emb EMB145 · Emergency Lighting
  > LEFT HAND OVER WING EMERGANCY LIGHT INOP-C/A-REMOVED AND REPLACED LEFT HAND OVER WING EMERGANCY LIGHT BULB IAW AMM 33-50-10. OPERATIONAL CHECK GOOD.
- [SDR SIMA20210330001](https://openairdocs.org/sdr/SIMA20210330001.md): Lamp · inoperative · Mar 30, 2021 · N607AE · Emb EMB145 · Emergency Lighting
  > AFT EMERGENCY LIGHT CEILING LIGHT INOP-C/A-RAR AFT EMERGENCY LIGHT CEILING LIGHT LAMP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR 9JLA2021022524810](https://openairdocs.org/sdr/9JLA2021022524810.md): Generator · defective · Feb 14, 2021 · N10HC · Emb EMB145 · DC Generator-Alternator
  > THE FLIGHT CREW REPORTED THAT DURING FLIGHT THE GEN 2 BEARING FAIL EICAS MESSAGE ILLUMINATED. THE MAINTENANCE VENDOR DETERMINED THAT NO2 DC GEN WAS DEFECTIVE. THE DEFECTIVE DC GEN WAS REMOVED AND AN OVERHAULED GEN WAS INSTALLED. GROUND RUNS AND OPS CHECKS WE
- [SDR 9JLA2021022529157](https://openairdocs.org/sdr/9JLA2021022529157.md): Pressure Switch · defective · Feb 14, 2021 · N809TD · Emb EMB145 · Hydraulic System, Main
  > THE FLIGHT CREW REPORTED THAT DURING FLIGHT WITH HYDRAULIC SYSTEM ON NO1 RUDDER SYSTEM CAUTION ILLUMINATED ON EICAS. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE NO1 RUDDER PRESSURE SWITCH TO BE DEFECTIVE. THE SWITCH WAS REMOVED AND A NEW PRESSUR
- [SDR SIMA20210125002](https://openairdocs.org/sdr/SIMA20210125002.md): Structure · cracked · Jan 25, 2021 · N613AE · Emb EMB145 · Fuselage Main, Structure
  > THE COCKPIT RT DIAGONAL CEILING MEMBER IS CRACKED JUST FORWARD OF THE SPEAKER, AS MARKED. C/A: R & R COCKPIT RT DIAGONAL CEILING MEMBER, IAW EMB 145 SRM 51-40-02. REPLACEMENT PN: 123-07751-006.
- [SDR SIMA20210125003](https://openairdocs.org/sdr/SIMA20210125003.md): Fan · odor · Jan 25, 2021 · N611AE · Emb EMB145 · Air Distribution Fan
  > BRIEFLEY ON TAKEOFF AND INTERMITTENTLY IN FLIGHT AN ODD SMELL WOULD COME UP IN THE COCKPIT/CABIN SMELL WAS SIMILAR TO ELECTRICAL BURNING. TRANSFERRED TO NRWC 611-DFW-03584. C/A: R & R NR 1 RECIRCULATION FAN, PER AMM 21-22-05. OPERATIONAL CHECK GOOD SWEE NRW
- [SDR SIMA20210111001](https://openairdocs.org/sdr/SIMA20210111001.md): Bulb · inoperative · Jan 11, 2021 · N611AE · Emb EMB145 · Emergency Lighting
  > RT OVERWING EXIT AFT EMERGENCY LIGHT INOPERABLE. C/A: REMOVED AND INSTALLED LIGHT BULB, IAW EMB AMM 33-50-10. OPERATIONS CHECK GOOD.
- [SDR SIMA20210105003](https://openairdocs.org/sdr/SIMA20210105003.md): Yoke · cracked · Jan 5, 2021 · N613AE · Emb EMB145 · Nacelle/Pylon, Attach Fittings
  > DURING IMBV INSPECTION, QC FOUND RT PYLON FWD LOWER YOKE FITTING CRACKED. C/A: REMOVED AND REPLACED RT FWD LOWER YOKE FITTING, IAW ERS-EM-54MR-698.
- [SDR SIMA20210101002](https://openairdocs.org/sdr/SIMA20210101002.md): Lamp · inoperative · Jan 1, 2021 · N611AE · Emb EMB145 · Emergency Lighting
  > CABIN AFT AISLE EMERGENCY LIGHT INOPERABLE. C/A: REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT LAMP, IAW EMB 145 AMM 33-50-08. OPERATIONAL CHECK GOOD.
- [SDR SIMA20201223003](https://openairdocs.org/sdr/SIMA20201223003.md): Floor Support · corroded · Dec 23, 2020 · N613AE · Emb EMB145 · Fuselage Miscellaneous Structure
  > LT OMEGA BEAM AT FRAME 20 PREVIOUS REPAIR IS CORRODED. C/A: REACCOMPLISHED REPAIR ON LT OMEGA BEAM AT FRAME 20, IAW EMB 145 SRM 53-00-10RE.
- [SDR SIMA20201221002](https://openairdocs.org/sdr/SIMA20201221002.md): Support · corroded · Dec 21, 2020 · N613AE · Emb EMB145 · Fuselage Miscellaneous Structure
  > TOILET WASTE VALVE SUPPORT EXTERIOR HAS CORROSION. C/A: REMOVED AND REPLACED THE TOILET WASTE VALVE SUPPORT, IAW EMB 145 SRM 51-40-02.
- [SDR SIMA20201220007](https://openairdocs.org/sdr/SIMA20201220007.md): Spar · cracked · Dec 20, 2020 · N613AE · Emb EMB145 · Wing Spar
  > LT WING SPAR I CRACKED AT RIB 9. CRACK LENGHT 0.3 NUMBER OF CRACKS 1. C/A: ACCOMPLISHED PERMANENT REPAIR ON LT WING SPAR I AT RIB 9, IAW EMB 145 SRM 57-20-05 ITEM 3.
- [SDR SIMA20201220001](https://openairdocs.org/sdr/SIMA20201220001.md): Skin · chafed · Dec 20, 2020 · N613AE · Emb EMB145 · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL LOWER SKIN CHAFED AT VB5 BETWEEN HB4 AND HB3. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER, IAW EMB 145 SRM 51-40-02, 52-30-01 AND ETN-EM-52-043.
- [SDR SIMA20201220003](https://openairdocs.org/sdr/SIMA20201220003.md): Skin · chafed · Dec 20, 2020 · N613AE · Emb EMB145 · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL LOWER SKIN CHAFFED AT HB4 APPROXIMATELY 2' FROM FWD EDGE. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER ON CARGO DOOR LOWER INNER SKIN AT HB4 APPROXIMATELY 2 FROM FWD EDGE, IAW EMB 145 SRM 52-30-01 AND ETN
- [SDR SIMA20201220002](https://openairdocs.org/sdr/SIMA20201220002.md): Skin · chafed · Dec 20, 2020 · N613AE · Emb EMB145 · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL LOWER SKIN CHAFED BETWEEN HB3 AND HB2. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER ON CARGO DOOR LOWER INNER SKIN BETWEEN HB3 AND HB2, IAW EMB 145 SRM 51-40-02, 52-30-01 AND ETN-EM-52-043.
- [SDR HNAA2020121200360](https://openairdocs.org/sdr/HNAA2020121200360.md): Starter Gen · malfunctioned · Dec 10, 2020 · N638AE · Emb EMB145 · Starter-Generator
  > APU GEN OFF BUS MESSAGE APPEARED ON EICAS WITH CLICKING NOISE AND ELECTRICAL BURNING SMELL IN COCKPIT. RESTARTED APU WITH GEN OFF NO SMELL NOTED OR CB S POPPED. R & R APU START GEN, IAW W/C 24-80-01. OPERATIONS CHECK GOOD.
- [SDR SIMA20201105002](https://openairdocs.org/sdr/SIMA20201105002.md): Lamp · inoperative · Nov 5, 2020 · N611AE · Emb EMB145 · Emergency Lighting
  > DURING PS-2 CHECK FOUND RIGHT HAND CENTER FAIRING EMERGENCY LIGHT OUT. C/A: R & R RT CENTER FAIRING EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-10. OPERATIONS CHECK GOOD.
- [SDR SIMA20200921001](https://openairdocs.org/sdr/SIMA20200921001.md): Lamp · inoperative · Sep 21, 2020 · N610AE · Emb EMB145 · Emergency Lighting
  > RT AFT OVERWING EMERGENCY LIGHT INOP. C/A: R & R RT AFT OVERWING EMERGENCY LAMP, IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD, IAW EMB 145 AMM 33-50-00.
- [SDR SIMA2020060130002](https://openairdocs.org/sdr/SIMA2020060130002.md): Support · corroded · May 30, 2020 · N612AE · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING MBV INSPECTION, QC FOUND THE TOILET WASTE VALVE SUPPORT CORRODED. REMOVED AND REPLACED THE TOILET WASTE VALVE SUPPORT IAW SRM 51-40-02.
- [SDR SIMA2020060130001](https://openairdocs.org/sdr/SIMA2020060130001.md): Spar · cracked · May 30, 2020 · N612AE · Emb EMB145 · Wing Spar
  > DURING MBV INSPECTION, QC FOUND THE RT WING SPAR 1 CRACKED AT A PREVIOUS REPAIR AT RIB 9. REPAIRED RT WING SPAR 1 AT RIB 9 IAW SRM 57-20-05-RE ITEM 3.
- [SDR SIMA2020060219002](https://openairdocs.org/sdr/SIMA2020060219002.md): Bracket · cracked · May 19, 2020 · N611AE · Emb EMB145 · Fuselage Miscellaneous Structure
  > FORWARD CARGO DOOR TORSION BAR BRACKET AT FRAME 61 HAS A 1/8" CRACK. INSTALLED NEW BRACKET IAW SRM 51-40-02.
- [SDR SIMA2020042018001](https://openairdocs.org/sdr/SIMA2020042018001.md): Structure · cracked · Apr 18, 2020 · N607AE · Emb EMB145 · Fuselage Miscellaneous Structure
  > SMALL CRACK IN SHEET METAL WHERE LH NLG FORWARD HINGE ASSEMBLY PASSES THROUGH TO ATTACHMENT POINT.-C/A-REPAIRED LH NLG DOOR FORWARD HINGE ASSY PASS THROUGH POINT IAW ERS-EM-53MR-4100.
- [SDR SIMA20200416002](https://openairdocs.org/sdr/SIMA20200416002.md): Frame · chafed · Apr 16, 2020 · N607AE · Emb EMB145 · Fuselage Main, Frame
  > FR 59 LH IS CHAFFED AT THE OVER HEAD BIN ATTACHMENT ARM NEAR STR. 5 LH.-C/A-REPAIRED SRM 53-00-04. CHAFE DAMAGE ASSIGNED DT-EM-53-1299.
- [SDR ASOA202004147036](https://openairdocs.org/sdr/ASOA202004147036.md): Flap · delaminated · Apr 13, 2020 · Emb EMB145 · Trailing Edge Flaps
  > L/H I/B FLAP HAS AREAS OF DELAMINATION ON TRAILING EDGE. REPAIRED DELAMINATION IAW EA12-2020-055. FLAP WAS RETURNED TO STOCK.
- [SDR ASOA202004027033](https://openairdocs.org/sdr/ASOA202004027033.md): Door Sill · corroded · Apr 2, 2020 · N11535 · Emb EMB145 · Fuselage Miscellaneous Structure
  > CARGO DOOR CUT-OUT SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR CUT-OUT SILL. AIRCRAFT STILL IN C CHECK.
- [SDR SIMA2020042030004](https://openairdocs.org/sdr/SIMA2020042030004.md): Skin · cracked · Mar 30, 2020 · N607AE · Emb EMB145 · Cargo/Baggage Doors
  > BAGGAGE DOOR SKIN HAS A CRACK JUST UNDER THE OPEN/CLOSE HANDLE. (CRACK APPROX 1 " LONG)-C/A-C/W ERS-EM-52MR-1073 BAGGAGE DOOR CARGO DOOR HANGLE CUTOUT CRACK PERMANENT REPAIR.
- [SDR SIMA2020041625008](https://openairdocs.org/sdr/SIMA2020041625008.md): Support Angle · cracked · Mar 25, 2020 · N607AE · Emb EMB145 · Wing Miscellaneous Structure
  > RH WING-TO-FUSELAGE LOWER SUPPORT ANGLE #2 IS CRACKED ON THE FWD END. UP TO THE 1ST RIVET, AND IS APPROX 3/8" LONG. -C/A-C/W REPLACEMENT OF #2 RH WING TO FUSELAGE LOWER SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR SIMA2020041625007](https://openairdocs.org/sdr/SIMA2020041625007.md): Frame · cracked · Mar 25, 2020 · N607AE · Emb EMB145 · Fuselage Main, Frame
  > CARGO BAY UNDER FLOOR FRAME IS CRACKED AT FR 72 LH AND STR.16 LH. -C/A-REPAIRED FRAME 72 IAW ERS-EM-53MR-4094.
- [SDR SIMA2020041618005](https://openairdocs.org/sdr/SIMA2020041618005.md): Structure · corroded · Mar 18, 2020 · N607AE · Emb EMB145 · Fuselage Miscellaneous Structure
  > TDMI 607T5323 ORIGNAL LG PG 4475656/3 TRANSFERRED FROM NRTC E710113, COCKPIT UNDERFLOOR BETWEEN FRAMES 13 AND 14 AND STRINGERS 20R AND 18L HAS SURFACE CORROSION ERS-EM-53MR-3758 PTB TRANSFERRED TO NRTC E782419 C BRODA 460360. UPGRADED TO A MAJOR REPAIR REFEREN
- [SDR ASOA202001287014](https://openairdocs.org/sdr/ASOA202001287014.md): Nut Plate · corroded · Jan 27, 2020 · Emb EMB145 · Passenger/Crew Doors
  > MAIN DOOR BOTTOM NUTPLATE CUTOUT HOLES HAVE CORROSION. BLENDED AND TREATED NUTPLATE HOLES ON BOTTOM OF MAIN DOOR, REPAIRED AFT MOST NUTPLATE HOLE BY CUTTING OUT DAMAGE, FABRICATING AND INSTALLING DOUBLER.
- [SDR SIMA201911298002](https://openairdocs.org/sdr/SIMA201911298002.md): Lamp · inoperative · Nov 28, 2019 · N611AE · Emb EMB145 · Emergency Lighting
  > ROW 12 B/C OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR ROW 12 B/C OVERHEAD EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD. END
- [SDR RAIA201909100001](https://openairdocs.org/sdr/RAIA201909100001.md): Skin · cracked · Sep 10, 2019 · N21128 · Emb EMB145 · Fuselage Main, Plate/Skin
  > FUSLAGE SKIN UNDER AFT DRAIN MAST CRACKED AND HAS HOLE. REPAIR INFORMATION ATTACHED TO SUPPLIMENTAL E-MAIL SENT TO 9-AMC-AFS-SDR@FAA.GOV.
- [SDR ASOA20190415052](https://openairdocs.org/sdr/ASOA20190415052.md): Bulb · inoperative · Apr 10, 2019 · N24103 · Emb EMB145 · Emergency Lighting
  > DURING MX INSPECTION THE EMERGENCY LIGHT OVER SEAT 18A WAS INOP. MX REMOVED AND REPLACED THE BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201902197029](https://openairdocs.org/sdr/ASOA201902197029.md): Hinge Fitting · worn · Feb 16, 2019 · Emb EMB145 · Vertical Stabilizer
  > R/H AND L/H VERTICAL STAB HINGE FITTING BORES WORN TO LIMITS. REAMED R/H AND L/H BORES AND INSTALLED BEARINGS. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA201901307023](https://openairdocs.org/sdr/ASOA201901307023.md): Yoke · cracked · Jan 30, 2019 · N16546 · Emb EMB145 · Engine Mount Section
  > NR 1 ENGINE FORWARD YOKE, LOWER FORWARD FITTING CRACKED ON RADIUS EDGE. REMOVED AND REPLACED YOKE FITTING. AIRCRAFT STILL IN C CHECK.
- [SDR HNAA2019012300026](https://openairdocs.org/sdr/HNAA2019012300026.md): Valve · malfunctioned · Jan 22, 2019 · N632AE · Emb EMB145 · Pneumatic Distribution System
  > PDIS 632 36-10 1856433 22JAN19 PHL CLOSE HS VLV 2 FAIL EICAS MSG DURING TAKE OFF ROLL HISTORY: FACT 22JAN19 20:17 PHL TROUBLESHOT WITH FIM 36-11-00-810-810-A UP TO BLOCK 7. R&R'D NR 2 HIGH STAGE VALVE IAW AMM 36-11-02. OPS CHECK GOOD. OKAY FOR SERVICE
- [SDR ASOA2018111217184](https://openairdocs.org/sdr/ASOA2018111217184.md): Skin · gouged · Nov 21, 2018 · Emb EMB145 · Passenger/Crew Doors
  > GOUGES ON MAIN DOOR EXTERNAL SKIN AT PREVIOUS REPAIR. CUT-OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER & DOUBLER. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA2018101515246](https://openairdocs.org/sdr/ASOA2018101515246.md): Light · arced · Oct 11, 2018 · N11544 · Emb EMB145 · Passenger Compartment Lighting
  > FLT 4096 MKE-EWR PILOT REPORTED "STRONG ELECTRICAL SMELL DURING CRUISE FLIGHT. SMELL INIDENTIFIED 1 MIN DURATION THEN DISSIPATED". MX RELAMPED 4 EACH CEILING AND SIDEWALL LAMPS. INSPECTED RELAY PANELS, CONTACTOR POWER BOXES, OPERATED BOTH PACKS AND NO SMELL NO
- [SDR HNAA2018100300241](https://openairdocs.org/sdr/HNAA2018100300241.md): Unknown · odor · Oct 2, 2018 · N665BC · Emb EMB145 · Air Distribution System
  > PDIS 665 05-52 1743622 02OCT18 PHL CLOSE POSSIBLE LIGHTNING STRIKE IN CRUISE FLIGHT. CREW RETURNED TO PHL AIRPORT. STRONG ELECTRICAL SMELL IN COCKPIT. 22107 00 JJC HISTORY: NO ISTORY:.FACT 02OCT18 23:42 PHL INSP A/C IAW W/C 05-20-00 FOUND ON EVIDENCE OF
- [SDR ASOA201809027159](https://openairdocs.org/sdr/ASOA201809027159.md): Stringer · chafed · Aug 29, 2018 · N16976 · Emb EMB145 · Fuselage Main, Longeron/Stringer
  > CHAFE DAMAGE ON PREVIOUS REPAIR AT STRINGER 19L AT FRAME 52. REMOVED AND REPLACED DAMAGED SECTION OF PREVIOUS REPAIR ON STRINGER. AIRCRAFT STILL IN C CHECK.

Next page: https://openairdocs.org/model/embraer-emb-145/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'EMB145'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/embraer-emb-145/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.