# Service difficulty reports: N17138

A list on [N17138](https://openairdocs.org/aircraft/N17138.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 148 reports

- [SDR JJBA20260728018](https://openairdocs.org/sdr/JJBA20260728018.md): Lamp · burned out · Jul 28, 2026 · N17138 · Emb EMB145XR · Emergency Lighting
  > AFT AISLE EMERGENCY LIGHT BURNED OUT. REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT LAMP. OPS CHECK GOOD
- [SDR JJBA20250822045](https://openairdocs.org/sdr/JJBA20250822045.md): Elec Connector · faulted · Aug 18, 2025 · N17138 · Emb EMB145XR · Flight Control System Wiring
  > FLAP FAIL, SPS ADVANCED EICAS MESSAGE DISPLAYED AFTER MOVING FLAP HANDLE DURING APPROACH. REMOVED AND REPLACED ELECTRICAL CONNECTOR PLUG P1104. FLAPS OPS CHECK GOOD. PERFORMED FLAP SCREWJACK ACTUATOR LUBRICATION ON ALL FLAP ACTUATORS. PERFORMED FLAP SCREWJACK
- [SDR JJBA20250805132](https://openairdocs.org/sdr/JJBA20250805132.md): Inverter · inoperative · Jul 31, 2025 · N17138 · Emb EMB145XR · Emergency Lighting
  > RIGHT EMERGENCY EXIT HATCH UPPER LIGHT PLACARD INOPERATIVE. REMOVED AND REPLACED INVERTER ASSEMBLY AT POSITION 5. OPS CHECK SAT.
- [SDR JJBA20250716045](https://openairdocs.org/sdr/JJBA20250716045.md): Flap System · failed · Jul 13, 2025 · N17138 · Emb EMB145XR · Trailing Edge Flap Control System
  > FLAP FAIL WHILE MOVING FROM 9 TO 22. FLAP SURFACES AND FSL ARE SET TO 9 DEGREES. ALSO, CONNECTORS P3683 AND P3682 ARE DISCONNECTED AND SECURED FOR FLAPS 9 FERRY FLIGHT. STARTED ZERO RIGGING OF LH IB FLAP. COMPLETED ZERO RIGGING. OPS CHECK SAT. CONNECTORS P3683
- [SDR JJBA20250609008](https://openairdocs.org/sdr/JJBA20250609008.md): Panel · out of position · Jun 8, 2025 · N17138 · Emb EMB145XR · Passenger/Crew Doors
  > MCD WONT CLOSE, TOP PANEL HAS GAP AND EXTERNAL HANDLE NOT FLUSH. PERFORMED MCD ADJUSTMENT/TEST AND PERFORMED CHECK WITH THE FORCE GAUGE. LOAD IS WITHIN LIMITS, FOUND RH UPPER ROLLER CAM TO BE LOOSE. RESECURED CAM. SERVICED/LUBRICATED MCD. MCD CYCLE OPEN/CLOSE.
- [SDR JJBA20250602004](https://openairdocs.org/sdr/JJBA20250602004.md): Lamp · inoperative · Jun 1, 2025 · N17138 · Emb EMB145XR · Emergency Lighting
  > MCD EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20250602003](https://openairdocs.org/sdr/JJBA20250602003.md): Lamp · inoperative · Jun 1, 2025 · N17138 · Emb EMB145XR · Emergency Lighting
  > CENTER AISLE CEILING EMERGENCY LIGHT AT ROW 18 INOPERATIVE. REMOVED AND REPLACED ROW 18 CENTER AISLE CEILING EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20250512050](https://openairdocs.org/sdr/JJBA20250512050.md): Bolt · loose · May 11, 2025 · N17138 · Emb EMB145XR · Passenger/Crew Doors
  > MAIN CABIN DOOR DIFFICULT TO CLOSE. FOUND INNER HANDLE BOX ATTACHMENT BOLTS TO BE LOOSE - TORQUED HANDLE BOX AND LUBRICATED DOOR. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.
- [SDR JJBA20250509045](https://openairdocs.org/sdr/JJBA20250509045.md): Handle · faulted · May 7, 2025 · N17138 · Emb EMB145XR · Passenger/Crew Doors
  > MCD EXTERIOR DOOR HANDLE NOT FULLY FLUSH. FA REPORTED LOUDER THAN NORMAL WHISTLING SOUNDS. RE-SEALED LOOSED FRAME SEAL. PERFORMED PRESSURIZATION CHECK. OPS CHECK, LEAK CHECK SAT. NO NOISES PRESENT. DOOR HANDLE SEATS FLUSH.
- [SDR JJBA20250221030](https://openairdocs.org/sdr/JJBA20250221030.md): Drive Unit · failed · Feb 18, 2025 · N17138 · Emb EMB145XR · Trailing Edge Flap Actuator
  > FLAP FAIL MESSAGE ON EICAS. NO FLAP CHANGE WHEN MOVING FLAP LEVER. REMOVED AND REPLACED FPDU. OPS CHECK GOOD.
- [SDR JJBA20230605001](https://openairdocs.org/sdr/JJBA20230605001.md): Unknown · unknown · Jun 1, 2023 · N17138 · Emb EMB145XR · Doors
  > MAIN CABIN DOOR UNLOCKING HANDLE LOWER ROLL PIN PULLED OUT RESECURED MAIN CABIN DOOR UNLOCKING HANDLE LOWER ROLL PIN.
- [SDR JJBA20230303019](https://openairdocs.org/sdr/JJBA20230303019.md): None · none · Feb 27, 2023 · N17138 · Emb EMB145XR · Emergency Lighting
  > PHOTO LUMINESCENT LIGHT STRIP LOOSE AT 3A. RESECURED EMERGENCY LIGHT STRIP AT 3A
- [SDR JJBA20221227026](https://openairdocs.org/sdr/JJBA20221227026.md): Charger · inoperative · Dec 26, 2022 · N17138 · Emb EMB145XR · Emergency Lighting
  > LH FWD WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK SAT.
- [SDR JJBA20220912007](https://openairdocs.org/sdr/JJBA20220912007.md): Lamp · inoperative · Sep 9, 2022 · N17138 · Emb EMB145XR · Emergency Lighting
  > MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT
- [SDR JJBA20220721023](https://openairdocs.org/sdr/JJBA20220721023.md): Light · inoperative · Jul 18, 2022 · N17138 · Emb EMB145XR · Emergency Lighting
  > RH EXTERNAL LOWER EMERGENCY LIGHT RETAINER ASSY NOT FLUSH WITH FUSELAGE AND IS MISSING SEALANT. R&R EXTERNAL LOWER EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.
- [SDR JJBA20220613010](https://openairdocs.org/sdr/JJBA20220613010.md): None · inoperative · Jun 13, 2022 · N17138 · Emb EMB145XR · Cabin Pressure Control System
  > AC CABIN ALT RAPIDLY CLIMBED TO 8400 THEN 9000 FEET, CAB RATE CONTINUED TO -150. CAB ALT CONTINUED TO RISE. DID A RAPID DECENT AND EMERGENCY DECLARED. OPENED BOTH COCKPIT DV WINDOWS, INSPECTED SEALS, FOUND NO DEFECTS. THEN FULLY CLOSED BOTH WINDOWS. REMOVED AN
- [SDR JJBA20220519036](https://openairdocs.org/sdr/JJBA20220519036.md): None · leaking · May 19, 2022 · N17138 · Emb EMB145XR · Brake Anti-Skid Section
  > BRAKE DEGRADED CAUTION MESSAGE ON FINAL APPROACH. ALL WHEEL SPEED SENSORS CHECKED AND FOUND SATISFACTORY. AIRCRAFT TAXIED OUT AND FOUND #2 BRAKES ON MFD HOTTER THAN ALL OTHER WHEELS. AIRCRAFT JACKED AND FOUND #2 BRAKES BINDING. REMOVED AND REPLACED #2 BRAKE AS
- [SDR JJBA20220515027](https://openairdocs.org/sdr/JJBA20220515027.md): Lamp · inoperative · May 15, 2022 · N17138 · Emb EMB145XR · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20220515026](https://openairdocs.org/sdr/JJBA20220515026.md): Battery Pack · inoperative · May 15, 2022 · N17138 · Emb EMB145XR · Emergency Lighting
  > LH FWD WTF FAIRING EMERGENCY LIGHT INOPERATIVE. FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE ON THE SAME CIRCUIT. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT
- [SDR JJBA20211001004](https://openairdocs.org/sdr/JJBA20211001004.md): None · none · Oct 1, 2021 · N17138 · Emb EMB145XR · Fuselage Structure (General)
  > COCKPIT ENTRY FLOOR BEAM HAS SIGNS OF CORROSION, TOOLING MARKS AND INCORRECT NUT PLATE INSTALLED. REMOVED AND REPLACED DAMAGE PROFILE REINFORCEMENT AT COCKPIT ENTRY FLOOR BEAM. CORROSION LEVEL 2
- [SDR JJBA20211001003](https://openairdocs.org/sdr/JJBA20211001003.md): None · none · Oct 1, 2021 · N17138 · Emb EMB145XR · Fuselage Structure (General)
  > COPILOT SIDE SEAT TRACKS (INBD/OUTBD) FLOOR BEAMS SHOW SIGNS OF CORROSION. REMOVED CORROSION AND EVALUATED AREA FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER IND/OUT ISDE AT COPILOT SIDE SEAT TRACKS FLOOR BEAMS. INSTALL REPAIR DOUBLER. CORROSION LEVEL 2
- [SDR JJBA20210930007](https://openairdocs.org/sdr/JJBA20210930007.md): None · none · Sep 30, 2021 · N17138 · Emb EMB145XR · Fuselage Structure (General)
  > PILOT SIDE INBD AND OUTBD SEAT TRACK FLOOR BEAMS SHOW SIGNS OF CORROSION (FS9-FS10 4WD LBL12 AND LBL24). BLENDED AREA FOUND TO BE OUT OF LIMITS IN RIGHT SIDE INBD AND OUTBD SIDE TRACK PLACE BEAM. FABRICATED 2 REPAIR DOUBLER IN INBD AND OTBD SIDE. APPLIED ALODI
- [SDR JJBA20210926002](https://openairdocs.org/sdr/JJBA20210926002.md): None · none · Sep 26, 2021 · N17138 · Emb EMB145XR · Fuselage Structure (General)
  > AFT FUSELAGE, UNDER TOILET AREA, RH GUSSET BEAMS, FROM FR 61 TO 59, BOTH HAT BEAMS HAS SIGNS OF CORROSION AT BOLT HOLES 4 EACH. BLENDED OUT CORROSION AND EVALUATED AT RH GUSSET FROM FR 59 - FR 60 FOUND TO BE OUT OF LIMITS. REMOVE DAMAGE GUSSET, LOCATE AND DRIL
- [SDR JJBA20210924010](https://openairdocs.org/sdr/JJBA20210924010.md): None · none · Sep 24, 2021 · N17138 · Emb EMB145XR · Fuselage Structure (General)
  > M/D CABIN RH SIDE, AT FRAME 53 - 34 FR SIGNS OF CORROSION ALONG FLOOR SILL. REMOVED AND REPLACED FLOOR SILL ON MID CABIN RH SIDE FR 56-41 AND FR 48-52. PERFORMED UTT BY NDT OF BLENDED AREA ON FR 41-48 MID RH CABIN FOUND TO BE WITHIN LIMITS
- [SDR JJBA20210923006](https://openairdocs.org/sdr/JJBA20210923006.md): None · none · Sep 23, 2021 · N17138 · Emb EMB145XR · Fuselage Structure (General)
  > HAT BEAM RH AFT OF FR 59 FOUND TO HAVE CORRODED AREA AT NUT PLATE AREA. CUTOUT DAMAGE AREA. FABRICATED REPAIR DOUBLER. APPLIED ALODINE, PRIMER, TOP COAT AND INSTALLED REPAIR DOUBLER. CORROSION LEVEL 2
- [SDR JJBA20210921033](https://openairdocs.org/sdr/JJBA20210921033.md): None · none · Sep 21, 2021 · N17138 · Emb EMB145XR · Fuselage Structure (General)
  > LH FUSELAGE AT FR60 SILL AREA, SMALL PLATE FOR WATER SUPPLY HAS A CRACK AT NUT PLATE. INSTALLED EWIS PROTECTION ON LH FUSELAGE AT FR60 TO FR 59. REMOVED CABLE AND DUCT FAIRING FOR ACCESS. REMOVED DAMAGED SMALL PLATE, LOCATED AND DRILLED NEW PLATE. RE-INSTALLED
- [SDR JJBA20210919027](https://openairdocs.org/sdr/JJBA20210919027.md): None · none · Sep 19, 2021 · N17138 · Emb EMB145XR · Fuselage Structure (General)
  > RH FR19, Y=479 SUSPECT CORROSION ON HAT-BEAM. REMOVED AND REPLACED HAT BEAM AT Y=479 RH FR19 CORROSION LEVEL 2
- [SDR JJBA20210821003](https://openairdocs.org/sdr/JJBA20210821003.md): Rib · corroded · Aug 21, 2021 · N17138 · Emb EMB145XR · Ailerons
  > LH AILERON INBD RIB SHOWS SIGNS OF CORROSION. FABRICATED AND REPLACED LH AILERON INBD RIB.
- [SDR JJBA20210818048](https://openairdocs.org/sdr/JJBA20210818048.md): Panel · corroded · Aug 18, 2021 · N17138 · Emb EMB145XR · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB INSIDE PANEL 325CL THE UPPER RUDDER ACTUATOR CONNECTING HARDWARE IS CORRODED. REMOVED & REPLACED UPPER RUDDER ACTUATOR BOLT & HARDWARE
- [SDR JJBA20210719021](https://openairdocs.org/sdr/JJBA20210719021.md): Target · out of adjust · Jul 19, 2021 · N17138 · Emb EMB145XR · Landing Gear Position and Warning
  > LG AIR/GROUND FAIL CAUTION MESSAGE RIGHT AFTER ROTATION FOLLOWED BY ENG 1-2 REV DISAGREE. ADJUSTED NLG DOWNLOCK PROX SWITCH TARGET. OPS CHECK SAT. PERFORMED OPERATIONAL CHECK OF #1 AND #2 T/R. OPS CHECK SAT. NO FAULTS FOUND AT THIS TIME. OPS CHECK SAT ON GEAR
- [SDR JJBA20210523025](https://openairdocs.org/sdr/JJBA20210523025.md): None · none · May 23, 2021 · N17138 · Emb EMB145XR · Aircraft Fuel System
  > FUEL LEAK COMING FROM PANEL 651CB. REMOVED PANEL 651 CB. FOUND FUEL IN THE DRY BAY OUTSIDE OF RIB 20. AILERON PCA`S HAD FUEL ON THEM, THE HYDRAULIC LINE CLOTH COVERS WERE SOAKED IN FUEL WITH FUEL ON THE PANEL AND IN THE DRY BAY AREA. UNABLE TO CLASSIFY THE LEA
- [SDR JJBA20210402007](https://openairdocs.org/sdr/JJBA20210402007.md): Seat Frame · cracked · Apr 2, 2021 · N17138 · Emb EMB145XR · Passenger Compartment Equipment
  > CRACKED AISLE SIDE FRAMES ON SEATS 4A, 10A, 19A, AND 22A. R&R SEATS 4A, 10A, 19A, AND 22A.
- [SDR JJBA20201213026](https://openairdocs.org/sdr/JJBA20201213026.md): Battery Pack · no test · Dec 13, 2020 · N17138 · Emb EMB145XR · Emergency Lighting
  > DURING OPERATIONS CHECKS OF EMERGENCY LIGHT FOUND SERVICE DOOR. EXIT IDENTIFIER, EXIT MARKER, EXIT LOCATOR ALL LOCATED IN GALLEY AREA INOPERATIVE. REMOVED AND INSTALLED NEW NR 2 BATTERY PACK AND CHARGER. EMERGENCY LIGHT OPERATION TEST GOOD.
- [SDR JJBA20201209023](https://openairdocs.org/sdr/JJBA20201209023.md): Seat Track · corroded · Dec 9, 2020 · N17138 · Emb EMB145XR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT AISLE UNDER SEAT TRACK NR 29 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 29 FLOOR BEAM.
- [SDR JJBA20201207017](https://openairdocs.org/sdr/JJBA20201207017.md): Stringer · damaged · Dec 7, 2020 · N17138 · Emb EMB145XR · Fuselage Main, Longeron/Stringer
  > STRINGER HAS GROOVE CUT IN THE BOTTOM SIDE, AT FR 17X+10.562 AND STGR 15R. REMOVED DAMAGED SECTION OF STRINGER 15R BETWEEN FRAMES 15 AND 16 ENDING AT FRAME 20 AND SPLICED IN NEW SECTION OF STRINGER.
- [SDR JJBA20201204025](https://openairdocs.org/sdr/JJBA20201204025.md): Seat Track · corroded · Dec 4, 2020 · N17138 · Emb EMB145XR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT AISLE, UNDER SEAT TRACK NR 31 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 31 FLOOR BEAM.
- [SDR JJBA20201204024](https://openairdocs.org/sdr/JJBA20201204024.md): Seat Track · corroded · Dec 4, 2020 · N17138 · Emb EMB145XR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT AISLE, UNDER SEAT TRACK NR 30 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 30 FLOOR BEAM.
- [SDR JJBA20201204022](https://openairdocs.org/sdr/JJBA20201204022.md): Buttstrap · corroded · Dec 4, 2020 · N17138 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT FLOOR STRUCTURE UNDER SEAT 1A CORROSION ON BUTT STRAP IN 2 LOCATIONS. REMOVED AND REPLACED BUTT STRAP FLOOR STRUCTURE UNDER SEAT 1A.
- [SDR JJBA20201125021](https://openairdocs.org/sdr/JJBA20201125021.md): Frame · corroded · Nov 25, 2020 · N17138 · Emb EMB145XR · Nacelle/Pylon, Main Frame
  > RIGHT ENGINE, FORWARD FRAME AFT FLANGE TO COMPOSITE OUTER BYPASS DUCT HAS MULTIPLE LOCATIONS OF CORROSION AROUND CIRCUMFERENCE APPROXIMATELY 60 PERCENT OF THE CIRCUMFERENCE. UPON FURTHER EVALUATION THE LOCATIONS OF CORROSION FOUND ON RIGHT ENGINE, FORWARD FRA
- [SDR RAIA2019121080001](https://openairdocs.org/sdr/RAIA2019121080001.md): Flap System · unknown · Dec 8, 2019 · N17138 · Emb EMB145XR · Trailing Edge Flap Control System
  > FLAP FAIL ON APPROACH AT 0 DEGREE---PERFORMED GVI OF FLAP SYSTEM AND RAN OPS CHECKS OF FLAPS,OPS CHECK GOOD ACFT OK FOR SERVICE
- [SDR RAIA201909230002](https://openairdocs.org/sdr/RAIA201909230002.md): Control Unit · inoperative · Sep 23, 2019 · N17138 · Emb EMB145XR · Stabilizer Actuator
  > PITCH TRIM MAIN INOP FOLLOWED BY PITCH TRIM BACKUP INOP. RETURNED FROM FLIGHT AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. R&R HSCU AND MAIN PITCH TRIM CUTOUT SWITCH. OPS CHECK GOOD.
- [SDR RAIA2019083029001](https://openairdocs.org/sdr/RAIA2019083029001.md): Frame · corroded · Aug 29, 2019 · N17138 · Emb EMB145XR · Cargo/Baggage Doors
  > LOWER FRAME ON CARGO DOOR HAS CORROSION AROUND NUTPLATE HOLES. R&R LOWER FR ON CARGO DOOR.
- [SDR RAIA2019083027003](https://openairdocs.org/sdr/RAIA2019083027003.md): Gusset · corroded · Aug 27, 2019 · N17138 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LH OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AT FRAME 59. REMOVED & REPLACED LH OMEGA BEAM GUSSET, NUT PLATES STILL NEED TO BE INSTALLED. INSTALLED NUT PLATES.
- [SDR RAIA2019082970002](https://openairdocs.org/sdr/RAIA2019082970002.md): Frame · cracked · Aug 27, 2019 · N17138 · Emb EMB145XR · Fuselage Main, Frame
  > COCKPIT FRAME 10 RH SIDE IS CRACKED AT UPPER END- R & R FR 10 RH.
- [SDR RAIA2019082970001](https://openairdocs.org/sdr/RAIA2019082970001.md): Frame · cracked · Aug 27, 2019 · N17138 · Emb EMB145XR · Fuselage Main, Frame
  > COCKPIT FRAME 10 LH SIDE IS CRACKED AT UPPER END. R & R FRAME 10 LH.
- [SDR RAIA201908260001](https://openairdocs.org/sdr/RAIA201908260001.md): Web · cracked · Aug 26, 2019 · N17138 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT WW REAR WEB IS CRACKED AT LOWER O/B CORNER. R&R LT WW REAR WEB.
- [SDR RAIA201908200008](https://openairdocs.org/sdr/RAIA201908200008.md): Shear Tie · cracked · Aug 20, 2019 · N17138 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > RT SHEAR CLIP AT FR 80 BETWEEN STR 5&6 IS CRACKED. REMOVED CRACKED SHEAR CLIP AT FRAME 80 BETWEEN STRINGERS 5&6 AND INSTALLED NEW SHEAR CLIP.
- [SDR RAIA201908200007](https://openairdocs.org/sdr/RAIA201908200007.md): Shear Tie · cracked · Aug 20, 2019 · N17138 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > LT SHEAR CLIP AT FR 80 BETWEEN STR 5&6 IS CRACKED. REMOVED LT SHEAR CLIP AT FRAME 80 RT BETWEEN STRINGERS 5 & 6 AND INSTALLED HI-LOKS INTO NEW PART, AIRCRAFT RIVETS NEED TO BE INSTALLED. FINISHED SHEAR CLIP INSTALLATION BY INSTALLING ALL RIVETS AND ANY OTHER R
- [SDR RAIA2019083020006](https://openairdocs.org/sdr/RAIA2019083020006.md): Floor Support · corroded · Aug 20, 2019 · N17138 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LH FLOOR SILL HAS LIGHT CORROSION ON UPPER SURFACE BETWEEN FRAME 54 & 55 LH. REMOVED AND STARTED INSTALLING LH FLOOR SILL AT FR 54-55. FINISHED INSTALLING LH FLOOR SILL AT FR 54-55.
- [SDR RAIA2019083020005](https://openairdocs.org/sdr/RAIA2019083020005.md): Gusset · corroded · Aug 20, 2019 · N17138 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > AFT LAV CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAVE CORROSION AROUND NUTPLATE HOLE AT FRAME 59. REMOVED & REPLACED AFT LAV CENTER OMEGA BEAM GUSSET, NUTPLATES STILL REQUIRED TO BE INSTALLED. INSTALLED NUTPLATES.

Next page: https://openairdocs.org/aircraft/N17138/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 n_number = 'N17138' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N17138/reports

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