# Service difficulty reports: Embraer EMB-145ER

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

Newest first. General aviation reporting is voluntary.

Page 1 of 26 · 1,266 reports

- [SDR OEJA202504070001](https://openairdocs.org/sdr/OEJA202504070001.md): Unknown · odor · Apr 4, 2025 · N905FL · Emb EMB145ER · Air Distribution System
  > ON 04/04/2025 AT 12:15PM, LEGACY600 TAKING OFF FORM KVRB 12R, CREW EXPERINCED SMOKE IN THE COCKPIT COMING FROM THE AIR VENTS. CREW IMMEDITATELY ABORTED TAKE OFF AND RETURNED TO THE FBO, CREW THEN NOTIFIED MAINTENANCE CHIEF. TROUBLESHOT THE ISSUE, AND RESOLVED
- [SDR ASOA2018051605126](https://openairdocs.org/sdr/ASOA2018051605126.md): Transducer · faulty · May 12, 2018 · N13988 · Emb EMB145ER · Landing Gear Brake System
  > CREW REPORTED BRAKES WERE SLOW TO REPOND ON LANDING ROLLOUT FOR LANDING. BRAKING WAS NORMAL ON BOTH SIDES ON TAXI TO GATE. REMOVED AND REPLACED THE NR 3 WHEEL SPEED TRANDSDUCER IAW MM 32-41-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR HNAA2017092000321](https://openairdocs.org/sdr/HNAA2017092000321.md): Light · inoperative · Sep 18, 2017 · N609 · Emb EMB145ER · Emergency Lighting
  > LEFT SIDE EMERGENCY EXIT DOOR UPPER LIGHT NOT ILLUMINATING. R&R EMERGENCY LIGHT AT LT EXIT DOOR IAW AMM TASK 33 50-14-000/400-801-A. P/N OFF 7444-9.
- [SDR HNAA2017092000320](https://openairdocs.org/sdr/HNAA2017092000320.md): Inverter · inoperative · Sep 18, 2017 · N609 · Emb EMB145ER · Emergency Lighting
  > ROW 3B EMERGENCY EXIT LIGHT NOT ILLUMINATING. R&R EMERGENCY LIGHT DC/AC INVERTER IAW AMM TASK 33-50-11-000/400-801-A. P/N OFF INVERTER 7824-1
- [SDR HNAA2017092000323](https://openairdocs.org/sdr/HNAA2017092000323.md): Connector · broken · Sep 16, 2017 · N604 · Emb EMB145ER · Light System Wiring
  > SERVICE DOOR EMERGENCY LIGHT INOP. FOUND CONNECTOR ON EMERGENCY SERVICE DOOR LIGHT BROKEN. R&R CONTACT + MALE CONNECTOR IAW SWPM 20-21-00. OPS CHECK GOOD OK FOR SERVICE.
- [SDR HNAA2017092000322](https://openairdocs.org/sdr/HNAA2017092000322.md): Knob · missing · Sep 15, 2017 · N632 · Emb EMB145ER · Lavatories
  > LAV DOOR EMERGENCY KNOB MISSING. INSTALLED NEW EXTERNAL LAV KNOB IN REF TO AMM 25-40-02-000/400-801-A. OK FOR SERVICE.
- [SDR V0XR2015091000002](https://openairdocs.org/sdr/V0XR2015091000002.md): Skin · corroded · Sep 10, 2015 · N809HK · Emb EMB145ER · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON THE INTERIOR SURFACE OF THE FUSELAGE SKIN BETWEEN FRAMES 12-13 AND STRINGERS 2021R. REPAIRED IAW ETD-2015-145-070110, REV C, REPAIR B AND EO-EMB145-53-013-R2.
- [SDR V0XR2015091000001](https://openairdocs.org/sdr/V0XR2015091000001.md): Skin · corroded · Sep 10, 2015 · N809HK · Emb EMB145ER · Fuselage Main, Plate/Skin
  > CORROSION AND PIN HOLES IN SKIN AT FR 13-14, STR 16-17R. REPAIRED CORROSION DAMAGE BY CUTTING THE SKIN BETWEEN FRAME 13-14, STR 16-17R AND INSTALLING A NEW SKIN SECTION AND DOUBLER, TRIPLE IAW ETD2015-145-07011 AND EO EMB145-53-013 R2. THIS REPAIR IS CONSIDE
- [SDR ASOA20140625144](https://openairdocs.org/sdr/ASOA20140625144.md): Frame · cracked · Jun 25, 2014 · N14933 · Emb EMB145ER · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 66 WAS FOUND TO BE CRACKED AT STRINGER 16R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140624135V](https://openairdocs.org/sdr/ASOA20140624135V.md): Hinge Fitting · worn · Jun 24, 2014 · N13936 · Emb EMB145ER · Rudder Structure
  > DURING C-CHECK THE TOP MOUNTING HINGE ON THE VERTICAL STABILIZER FOR RUDDER, FOUND TO BE WORN. MAINTENANCE R & R THE HINGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140622134V](https://openairdocs.org/sdr/ASOA20140622134V.md): Floor Support · corroded · Jun 23, 2014 · N14933 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, FIGURE 202, SHEET 2. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413043](https://openairdocs.org/sdr/ASOA20140413043.md): Door Frame · cracked · Apr 13, 2014 · N14930 · Emb EMB145ER · Cargo/Baggage Doors
  > CARGO DOOR AFT FRAME LOWER INSIDE CORNER HAS A CRACKED NUTPLATE. REPAIRED IAW EC5230-01326. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413042](https://openairdocs.org/sdr/ASOA20140413042.md): Firewall · cracked · Apr 13, 2014 · N14930 · Emb EMB145ER · APU Cowling/Containment
  > DURING C-CHECK, APU FIREWALL CRACKED AT UPPER LT MOUNT. REPAIRED IAW EC5330-02578, REV B. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413041](https://openairdocs.org/sdr/ASOA20140413041.md): Housing · worn · Apr 13, 2014 · N14930 · Emb EMB145ER · Horizontal Stabilizer Structure
  > DURING C-CHECK, HORIZONTAL STAB HINGE FITTING HOUSINGS IS OUT OF LIMITS. REPAIRED IAW SRM 55-30-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413040V](https://openairdocs.org/sdr/ASOA20140413040V.md): Floor Support · corroded · Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CENTER OMEGA BEAM CORRODED ON LOWER SIDE AT FRAME 59. MAINTENANCE PERFORMED REPAIR IAW EC5310-01473. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413039](https://openairdocs.org/sdr/ASOA20140413039.md): Shear Tie · corroded · Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED, AT FRAME 65, STRINGER 17L. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413038](https://openairdocs.org/sdr/ASOA20140413038.md): Beam · corroded · Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Main, Structure
  > DURING C-CHECK, CARGO LOWER BEAM FROM FRAMES 65-68 HAS CORROSION. MAINTENANCE R & R LOWER BEAM IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140318054](https://openairdocs.org/sdr/ASOA20140318054.md): Channel · corroded · Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > C-CHECK, THE CENTER OMEGA BEAM GUSSET WAS CORRODED AT NUTPLATES AT FRAME 16. MAINTENANCE REMOVED THE CORROSION AND FABRICATED A NEW REPAIR IAW EC 5320-01215, REV ORIGINAL.
- [SDR ASOA20140318053T](https://openairdocs.org/sdr/ASOA20140318053T.md): Channel · corroded · Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE RT SIDE OMEGA BEAM TOPCAP WAS FOUND CORRODED AT FRAME 59. MAINTENANCE R & R THE RT SIDE OMEGA BEAM GUSSET AT FRAME 59 IAW SRM 51-40-02
- [SDR ASOA20140318052T](https://openairdocs.org/sdr/ASOA20140318052T.md): Shear Tie · cracked · Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Internal Mounting Structure
  > DURING C-CHECK, LT CENTER FUSELAGE FRAME 46 HAS A SHEAR TIE CRACKED. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-40-02.
- [SDR ASOA20140318051](https://openairdocs.org/sdr/ASOA20140318051.md): Floor Support · cracked · Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > C-CHECK, THE LT FLOOR SUPPORT SPLICE WAS FOUND CRACKED AT FRAMES 23 AND 24. MAINTENANCE R & R IAW SRM 51-40-02.
- [SDR ASOA20140311025](https://openairdocs.org/sdr/ASOA20140311025.md): Seal · debonded · Mar 11, 2014 · N14938 · Emb EMB145ER · Cargo/Baggage Doors
  > EXPERIENCED CABIN DEPRESSURIZATION AT ALTITUDE AND THEN DIVERTED. MAINTENANCE FOUND CARGO DOOR RUBBER TRIM SEAL DEBONDED AND HANGING OUT IN THE AIRSTREAM. REINSTALLED CARGO DOOR RUBBER TRIM SEAL IAW AMM 52-30-02. PERFORMED LEAK CHECK ON PRESSURIZATION AND O
- [SDR ASOA20140101003](https://openairdocs.org/sdr/ASOA20140101003.md): Mount · cracked · Jan 1, 2014 · N22971 · Emb EMB145ER · Engine Mount Section
  > DURING C-CHECK NR 1 ENGINE FWD LOWER ENGINE MOUNT YOKE CRACKED.
- [SDR ASOA20140101002](https://openairdocs.org/sdr/ASOA20140101002.md): Frame · dented · Jan 1, 2014 · N22971 · Emb EMB145ER · Fuselage Main, Frame
  > DURING C-CHECK FRM 74 IS DENTED AT STR 14L-15L. MAINTENANCE PERFORMED REPAIR OF FRAME 74 AT STR 14L-15L IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218294V](https://openairdocs.org/sdr/ASOA20131218294V.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer Structure
  > DURING C-CHECK THE HORIZONTAL STAB HINGE PIN FITTING NR 4 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218293](https://openairdocs.org/sdr/ASOA20131218293.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer Structure
  > DURING C-CHECK THE HORIZONTAL STAB HINGE PIN FITTING, NR 3 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218292](https://openairdocs.org/sdr/ASOA20131218292.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer Structure
  > DURING C-CHECK, THE HORIZONTAL STAB HINGE PIN FITTING NR 2 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218291V](https://openairdocs.org/sdr/ASOA20131218291V.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer Structure
  > DURING C-CHECK, HORIZONTAL STAB HINGE PIN FITTING NR 1 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218290](https://openairdocs.org/sdr/ASOA20131218290.md): Skin · cracked · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-80 AND STRINGERS 3-7R. MAINTENANCE REMOVED THE CRACKS BY REAMING AND PERFORMED BUSHING REPAIRS IAW EC5330-02840. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218289](https://openairdocs.org/sdr/ASOA20131218289.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Rudder Structure
  > DURING C-CHECK, THE RUDDER II UPPER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218288](https://openairdocs.org/sdr/ASOA20131218288.md): Hinge Fitting · worn · Dec 18, 2013 · N15932 · Emb EMB145ER · Spoilers
  > DURING C-CHECK, THE LT SPEED BRAKE CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218287](https://openairdocs.org/sdr/ASOA20131218287.md): Frame · cracked · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Frame
  > DURING C-CHECK, LEFT FRAME 10 SEGMENT WAS FOUND TO BE CRACKED BETWEEN STRINGERS 9-10L. R & R FRAME SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218286](https://openairdocs.org/sdr/ASOA20131218286.md): Stringer · cracked · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 6R WAS FOUND TO BE CRACKED AT FRAME 14. R & R STRINGER SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218285](https://openairdocs.org/sdr/ASOA20131218285.md): Floor Support · corroded · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK, RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. REMOVED CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218284](https://openairdocs.org/sdr/ASOA20131218284.md): Support · corroded · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LAVATORY WASTE DRAIN SUPPORT ASSY WAS FOUND TO BE CORRODED. R & R SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131218283](https://openairdocs.org/sdr/ASOA20131218283.md): Sill · corroded · Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK, SERVICE DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131125447](https://openairdocs.org/sdr/ASOA20131125447.md): Bracket · worn · Nov 25, 2013 · N17928 · Emb EMB145ER · Spoilers
  > AIRCRAFT IS IN C-CHECK WHEN INSPECTION FOUND THE RT GROUND SPOILER INBD HINGE FITTING AT THE WING SPAR AREA INBD/OTBD BUSHIONS MIGRATED AND OBLONG THE FITTING. MAINTENANCE R & R THE THE RT GROUND SPOILER FITTING IAW AMM 20-10-01. ALL WORK ACCOMPLISHED AND WI
- [SDR ASOA20130610173](https://openairdocs.org/sdr/ASOA20130610173.md): Tire · failed · Jun 10, 2013 · N14937 · Emb EMB145ER · Tire
  > FLIGHT 4358. RT MLG NR 3 TIRE BLEW OUT AT V1 DAMAGING OTHER ITEMS. R & R NR 3 TIRE.
- [SDR ASOA20130423156](https://openairdocs.org/sdr/ASOA20130423156.md): Skin · corroded · May 12, 2013 · N16944 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE CENTER FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 14-15 AND STRINGERS 19R-20L. MX R & R THE SKIN IAW EC5330-02761. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130423153](https://openairdocs.org/sdr/ASOA20130423153.md): Frame · cracked · May 11, 2013 · N16944 · Emb EMB145ER · Fuselage Main, Frame
  > DURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED DIRECTLY BELOW THE PILOTS DV WINDOW AT STRINGER 9L. MX R & R THE CRACKED FRAME SECTION IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421138](https://openairdocs.org/sdr/ASOA20130421138.md): Skin · corroded · Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 20R-20L. MX R & R THE SKIN IAW EC5320-01787. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421137](https://openairdocs.org/sdr/ASOA20130421137.md): Stringer · corroded · Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12-13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421136](https://openairdocs.org/sdr/ASOA20130421136.md): Stringer · corroded · Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 21L WAS FOUND TO BE CORRODED BETWEEN FRAMES 12 AND 13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421135V](https://openairdocs.org/sdr/ASOA20130421135V.md): Sill · corroded · Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226089](https://openairdocs.org/sdr/ASOA20130226089.md): Skin · corroded · Mar 7, 2013 · N14943 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > DURING C-CHECK THE COCKPIT BELLY SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 18R-19L. MX R & R THE SKIN IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226088](https://openairdocs.org/sdr/ASOA20130226088.md): Beam · corroded · Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Main, Structure
  > DURING C-CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED FROM FRAMES 65-68 BETWEEN STRINGERS 15L-16L. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226087](https://openairdocs.org/sdr/ASOA20130226087.md): Shear Tie · corroded · Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Internal Mounting Structure
  > DURING C-CHECK THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226086](https://openairdocs.org/sdr/ASOA20130226086.md): Shear Angle · corroded · Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226085](https://openairdocs.org/sdr/ASOA20130226085.md): Shear Angle · cracked · Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE RIB 1 SHEAR CLIP FROM FRAMES 40-45 WAS FOUND TO BE CRACKED. MX R & R THE SHEAR CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130131257T](https://openairdocs.org/sdr/ASOA20130131257T.md): Skin · cracked · Jan 31, 2013 · N15941 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > ACFT WAS FOUND WITH A 6MM CRACK FOR RIVET EDGE ON THE LT SKIN AT FRAME 75 BELOW STRINGER 2. MX INSTALL A SMALL PATCH TO THE FUSELAGE SKIN AT FRAME 75, STRINGER 2L IAW EC 5330-02353. PRESSURE CHECKED GOOD AND WAS RELEASED TO SERVICE.

Next page: https://openairdocs.org/model/embraer-emb-145er/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 = 'EMB145ER'
ORDER BY difficulty_date DESC
```

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

---
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