# Service difficulty reports: N11181

A list on [N11181](https://openairdocs.org/aircraft/N11181.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 2 · 67 reports

- [SDR JJBA20220305006](https://openairdocs.org/sdr/JJBA20220305006.md): Lamp · inoperative · Mar 5, 2022 · N11181 · Emb EMB145XR · Emergency Lighting
  > RH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK SAT
- [SDR JJBA20210407014](https://openairdocs.org/sdr/JJBA20210407014.md): Line · chafed · Apr 7, 2021 · N11181 · Emb EMB145XR · Engine Oil Pressure
  > E2 OIL LOW PRESSURE EICAS MASTER WARNING IN FLIGHT. OIL ON COWLINGS AFTER LANDING. FOUND CHAFED OIL LINE CONNECTED TO AGB TO OIL TANK PRESSURE LINE. R&R THE OIL LINE AND PERFORMED ENGINE RUNS. OPS CHECK AND LEAK CHECK SAT AT THIS TIME.
- [SDR JJBA2021360004](https://openairdocs.org/sdr/JJBA2021360004.md): Seat Frame · cracked · Mar 6, 2021 · N11181 · Emb EMB145XR · Passenger Compartment Equipment
  > CRACK AT SEATS 3A, 2A & 18A STRUCTURE BELOW ARMREST. R&R SEATS 18A, 3A & 2A.
- [SDR JJBA20201223027](https://openairdocs.org/sdr/JJBA20201223027.md): Control Unit · inoperative · Dec 23, 2020 · N11181 · Emb EMB145XR · Landing Gear Brake System
  > BRAKE INBOARD INOPERATIVE MESSAGE ON EICAS. INSPECTED FOR HYDRAULIC LEAKS ON INBOARD BRAKES. CHECKED HYDRAULIC LEVEL AND PRESSURE. NO DEFECTS FOUND. R & R BRAKE CONTROL UNIT. NO MESSAGES ON EICAS. OPERATIONS CHECK GOOD.
- [SDR JJBA202007297004](https://openairdocs.org/sdr/JJBA202007297004.md): Inverter · inoperative · Jul 27, 2020 · N11181 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE ABOVE SERVICE DOOR. R&R INVERTER #2. OPS CHECK SAT.
- [SDR JJBA202003265020](https://openairdocs.org/sdr/JJBA202003265020.md): Doubler · corroded · Mar 25, 2020 · N11181 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION - COCKPIT FLOOR DOUBLER Y=+293.0 FR10/11. REMOVED AND REPLACED COCKPIT FLOOR DOUBLER AT Y= +293.0 AND 3EA. REPAIR DOUBLER
- [SDR JJBA202003265019](https://openairdocs.org/sdr/JJBA202003265019.md): Gusset · corroded · Mar 25, 2020 · N11181 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION - COCKPIT FLOOR DOUBLER Y=-607 FR8/11. REMOVED AND REPLACED LH OB COCKPIT GUSSET FR8-11.
- [SDR JJBA202003265014](https://openairdocs.org/sdr/JJBA202003265014.md): Support · corroded · Mar 25, 2020 · N11181 · Emb EMB145XR · Wing Miscellaneous Structure
  > RH WING - O/B LWR SHROUD, O/B BOTH CENTERS AND I/B SPRING SUPPORTS HAVE CORROSION. REMOVED AND REPLACED RH WING - OB LWR SHROUD, OB BOTH CENTERS AND I/B SPRING SUPPORTS.
- [SDR JJBA202003264015](https://openairdocs.org/sdr/JJBA202003264015.md): Support · corroded · Mar 24, 2020 · N11181 · Emb EMB145XR · Wing Miscellaneous Structure
  > L/H WING - I/B LWR SHROUD, I/B SPRING SUPPORT HAVE CORROSION AS MARKED. REMOVED AND REPLACED L/H WING - I/B LWR SHROUD, I/B SPRING SUPPORT
- [SDR JJBA202003264013](https://openairdocs.org/sdr/JJBA202003264013.md): Support · corroded · Mar 24, 2020 · N11181 · Emb EMB145XR · Wing Miscellaneous Structure
  > L/H WING - O/B LWR SHROUD, O/B AND BOTH CENTER SPRING SUPPORTS HAVE CORROSION AS MARKED. REMOVED AND REPLACED 3EA L/H WING O/B LWR SHROUD, O/B AND BOTH CENTER SPRING SUPPORTS
- [SDR JJBA202003261016](https://openairdocs.org/sdr/JJBA202003261016.md): Support · corroded · Mar 21, 2020 · N11181 · Emb EMB145XR · Wing Miscellaneous Structure
  > R/H WING - I/B LWR SHROUD, I/B AND O/B SPRING SUPPORT HAVE CORROSION AS MARKED. INSTALLED NU PLATES, REMOVED AND REPLACED R/H WING - I/B LWR SHROUD, I/B AND O/B SPRING SUPPORT
- [SDR JJBA2020032616018](https://openairdocs.org/sdr/JJBA2020032616018.md): Skin · not reported · Mar 16, 2020 · N11181 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > LOCATE THE CIRCULAR DOUBLER REPAIR AT FRAME 28, STRINGER 16R. REMOVE THE DOUBLER, REPORT THE SKIN CONDITION TO RTS FOR PERMANENT REPAIR INSTRUCTIONS AND DAMAGE TOLERANCE-BASED SUPPLEMENTAL INSPECTION REQUIREMENTS, AS NEEDED. ACCOMPLISH THE PERMANENT REPAIR. RE
- [SDR JJBA2020032615021](https://openairdocs.org/sdr/JJBA2020032615021.md): Skin · damaged · Mar 15, 2020 · N11181 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FOUND SEVERAL TOOLING MARKS BELOW ADF ANTENNA. INSTALLED REPAIR DOUBLER TO INTERNAL FUSELAGE BETWEEN FR42-FR44 STR1R
- [SDR JJBA2020032015011](https://openairdocs.org/sdr/JJBA2020032015011.md): Doubler · corroded · Mar 15, 2020 · N11181 · Emb EMB145XR · Wing Miscellaneous Structure
  > RH WING PANEL 198 DOUBLER FOR NUT PLATES HAS CORROSION ALONG DOUBLER AS MARKED. FABRICATED, LOCTED, DRILLED, ALODINED AND PRIMED 2(EA) DOUBLERS ON RH WING PANEL 198.
- [SDR JJBA2020032015010](https://openairdocs.org/sdr/JJBA2020032015010.md): Doubler · corroded · Mar 15, 2020 · N11181 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION - COCKPIT FLOOR DOUBLER Y=+607.0 FR 9/10. REMOVED AND REPLACED RH OB COCKPIT GUSSET
- [SDR JJBA2020032015009](https://openairdocs.org/sdr/JJBA2020032015009.md): Doubler · corroded · Mar 15, 2020 · N11181 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION - COCKPIT FLOOR DOUBLER Y=-293.0 FR9/11. SPLICED IN NEW PILOT INBD FLOOR DOUBLER AND DOUBLERS
- [SDR JJBA2020032614017](https://openairdocs.org/sdr/JJBA2020032614017.md): Skin · not reported · Mar 14, 2020 · N11181 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > LOCATE THE CIRCULAR DOUBLER REPAIR AT FRAMES 19-20, STRINGERS 15L-17L REMOVE THE DOUBLER, REPORT THE SKIN CONDITION TO RTS FOR PERMANENT REPAIR INSTRUCTIONS AND DAMAGE TOLERANCE-BASED SUPPLEMENTAL INSPECTION REQUIREMENTS, AS NEEDED. ACCOMPLISH THE PERMANENT RE
- [SDR JJBA2020032005008](https://openairdocs.org/sdr/JJBA2020032005008.md): Floor Support · corroded · Mar 5, 2020 · N11181 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LH OMEGA BEAM CORRODED AS MARKED FROM FR 50-45. REMOVED AND REPLACED LH OMEGA BEAM FR45-52. CORROSION FOUND TO BE LEVEL 2
- [SDR JJBA2020032003007](https://openairdocs.org/sdr/JJBA2020032003007.md): Floor Support · corroded · Mar 3, 2020 · N11181 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > R/H OMEGA BEAM CORRODED ON FR23 AS MARKED. REPAIRED RH OMEGA BEAM CORRODED ON FR23 BY CUTTING OUT THE DAMAGE AND INSTALLING A DOUBLER. CORROSION FOUND TO BE LEVEL 2.
- [SDR JJBA202001064001](https://openairdocs.org/sdr/JJBA202001064001.md): Muffler · unsecure · Jan 4, 2020 · N11181 · Emb EMB145XR · Cabin Cooling System
  > RETURN TO FIELD DUE TO PAX COMPLAINTS OF EXTREME AMOUNTS OF CONDENSATION AND BANGING NOISES AROUND ROW 9 RIGHT SIDE. R&R PACK MUFFLER. OPS CHECK SAT.
- [SDR JJBA201912264010](https://openairdocs.org/sdr/JJBA201912264010.md): Control Module · failed · Dec 24, 2019 · N11181 · Emb EMB145XR · Electrical Power System Wiring
  > SMOKE COMING FROM FA PANEL. PERFORMED GVI OF COMPONENTS & CONNECTORS AROUND FA PANEL. FOUND CONTROL MODULE UNIT BURNED OUT. R&R CONTROL MODULE UNIT. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.
- [SDR JJBA201910185007](https://openairdocs.org/sdr/JJBA201910185007.md): Light · missing · Oct 15, 2019 · N11181 · Emb EMB145XR · Emergency Lighting
  > ISLE PATH EMERGENCY STRIP FO SIDE NEXT TO GALLEY WITH RED DOTS IS MISSING. INSTALLED EMERGENCY STRIP NEXT TO GALLEY AS REQUIRED.
- [SDR JJBA201910185006](https://openairdocs.org/sdr/JJBA201910185006.md): Light · misinstalled · Oct 15, 2019 · N11181 · Emb EMB145XR · Emergency Lighting
  > ISLE PATH EMERGENCY STRIP ON CAPTAIN SIDE NEXT TO MAIN CABIN DOOR BACKWARDS. CORRECTLY INSTALLED EMERGENCY STRIP ON CAPTAINS SIDE NEXT TO MAIN CABIN DOOR AS REQUIRED.
- [SDR JJBA20190808003](https://openairdocs.org/sdr/JJBA20190808003.md): Latch · no test · Aug 8, 2019 · N11181 · Emb EMB145XR · Fixed Inner Doors
  > THE PRESSURE RELIEF LATCH ON THE COCKPIT DOOR FAILED FUNCTIONAL TEST, REQUIRED TOO MUCH FORCE TO OPEN AND CLOSE PAST DETENT. CLEANED PRESSURE RELIEF LATCH BOLT. OPS CHECK SAT.
- [SDR JJBA20190718016](https://openairdocs.org/sdr/JJBA20190718016.md): Battery Pack · discharged · Jul 18, 2019 · N11181 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOPERATIVE. R&R EMERGENCY EXIT LIGHT AND R&R BATTERY #2. OPS CHECK SAT.
- [SDR JJBA20190129038](https://openairdocs.org/sdr/JJBA20190129038.md): Ecs · contaminated · Jan 29, 2019 · N11181 · Emb EMB145XR · Air Distribution System
  > SMOKE IN THE COCKPIT ON TAKE-OFF ROLL. ON TAKE-OFF ROLL ADVANCED THROTTLES COCKPIT FILLED WITH SMOKE. NO SMOKE IN CABIN, DID NOT DECLARE EMERGENCY, APU NOT ON, WHEN THROTTLES DECREASED SMOKE CLEARED. PERFORMED VISUAL CHECK OF AIRCRAFT. FOUND LARGE AMOUNTS OF D
- [SDR JJBA201811095003](https://openairdocs.org/sdr/JJBA201811095003.md): Receptacle · damaged · Nov 5, 2018 · N11181 · Emb EMB145XR · Fuselage Main, Structure
  > GPU EXTERNAL SOCKET DAMAGED. RECONTOURED DENTED AREA AFT OF FR 06. ACCOMPLISHED 30X DET VISUAL INSPECTION ON AND AROUND REWORKED AREA. FABRICATED REPAIR PARTS. PERFORMED REPAIR. R&R EXT POWER BOX ASSY AND DOOR ASSY. R&R POWER RECEPTACLE. OPS CHECK SAT.
- [SDR JJBA20180927012](https://openairdocs.org/sdr/JJBA20180927012.md): Solenoid Valve · failed · Sep 27, 2018 · N11181 · Emb EMB145XR · Landing Gear Retraction/Extension System
  > NOSE GEAR DOOR OPENED INFLIGHT ON DECENT AT 6000 FT. R&R NLG DOOR SOLENOID VALVE. OPS & LEAK CHECK SAT.
- [SDR JJBA20180827013](https://openairdocs.org/sdr/JJBA20180827013.md): Sign · detached · Aug 27, 2018 · N11181 · Emb EMB145XR · Emergency Lighting
  > FORWARD OVERHEAD EMERGENCY EXIT SIGN DETACHED. ATTACHED THE FORWARD OVERHEAD EMERGENCY EXIT SIGN. OPS CHECKED SAT.
- [SDR ASOA201701103001](https://openairdocs.org/sdr/ASOA201701103001.md): Clamp · worn · Jan 10, 2017 · N11181 · Emb EMB145XR · Pneumatic System
  > THE CREW REPORTED BLEED NR 1 LEAK WARNING IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE CLAMP ON LEFT PRECOOLER FORWARD DUCT. OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA201610100726](https://openairdocs.org/sdr/ASOA201610100726.md): Beam · corroded · Oct 10, 2016 · N11181 · Emb EMB145XR · Fuselage Main, Structure
  > DURING C-CHECK. CARGO DOOR CUTOUT LOWER BEAM CORRODED. REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160508029](https://openairdocs.org/sdr/ASOA20160508029.md): Battery Pack · inoperative · May 8, 2016 · N11181 · Emb EMB145XR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, MULTIPLE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA20150426038H](https://openairdocs.org/sdr/ASOA20150426038H.md): Inverter · inoperative · Apr 26, 2015 · N11181 · Emb EMB145XR · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE F/A HEADSET WAS INOPERATIVE. MAINTENANCE R & R THE NR 1 INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20141220154H](https://openairdocs.org/sdr/ASOA20141220154H.md): Light · intermittent · Dec 20, 2014 · N11181 · Emb EMB145XR · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD F/A SEAT WAS INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140801083](https://openairdocs.org/sdr/ASOA20140801083.md): Smoke Warning · false activation · Aug 1, 2014 · N11181 · Emb EMB145XR · Smoke Detection
  > CREW REPORTED LAVATORY SMOKE WARNING INTERMITTENTLY ALARMS. MX PERFORMED LAV SMOKE OPS CHECKS IAW SUPPLEMENT 26-14-00, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140702052](https://openairdocs.org/sdr/ASOA20140702052.md): Battery · discharged · Jul 2, 2014 · N11181 · Emb EMB145XR · Emergency Lighting
  > THE CREW REPORTED GALLEY AND ROW 3 EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.
- [SDR ASOA20140509058](https://openairdocs.org/sdr/ASOA20140509058.md): Door Sill · corroded · May 8, 2014 · N11181 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE FORWARD SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140509057](https://openairdocs.org/sdr/ASOA20140509057.md): Door Sill · corroded · May 8, 2014 · N11181 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140506056V](https://openairdocs.org/sdr/ASOA20140506056V.md): Yoke · cracked · May 6, 2014 · N11181 · Emb EMB145XR · Engine Mount Section
  > DURING C-CHECK, THE NR 1 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED, VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5450-01087. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130829159](https://openairdocs.org/sdr/ASOA20130829159.md): Controller · smoke · Aug 29, 2013 · N11181 · Emb EMB145XR · Autopilot System
  > THE CREW REPORTED ELECTRICAL SMOKE COMING FROM THE VS BUTTON OF THE FLIGHT GUIDANCE PANEL. MX R & R THE FLIGHT GUIDANCE CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130808146H](https://openairdocs.org/sdr/ASOA20130808146H.md): Relay · inoperative · Aug 8, 2013 · N11181 · Emb EMB145XR · Cabin Cooling System
  > THE CREW REPORTED THAT PACK 1 AND 2 VALVES CLOSED IN FLIGHT. THE ACFT RETURNED TO WHERE IT LANDED WITHOUT INCIDENT. MX R & R RELAY K0435, OPS TESTED BOTH PACKS WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130116236](https://openairdocs.org/sdr/ASOA20130116236.md): Inverter · inoperative · Jan 16, 2013 · N11181 · Emb EMB145XR · Emergency Lighting
  > AFT OVERWING EXIT LOCATOR LIGHT INOPERATIVE. R & R NR 4 INVERTER. OPS CHECKED GOOD.
- [SDR ASOA20120723063](https://openairdocs.org/sdr/ASOA20120723063.md): Battery · discharged · Jul 23, 2012 · N11181 · Emb EMB145XR · Emergency Lighting
  > DURING ROUTINE MX, THE AFT OVERHEAD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX ARMED AND RECHARGED THE EMERGENCY LIGHT SYS. OPS CHECKED GOOD.
- [SDR ASOA20120531042](https://openairdocs.org/sdr/ASOA20120531042.md): Battery Pack · failed · May 31, 2012 · N11181 · Emb EMB145XR · Emergency Lighting
  > DURING MX INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO NOT BE HOLDING CHARGE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH OPS CHECKED SUCCESSFUL. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120406021](https://openairdocs.org/sdr/ASOA20120406021.md): Stringer · corroded · Apr 6, 2012 · N11181 · Emb EMB145XR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 21R CORRODED BETWEEN FRAME 12-13. R & R STRINGER WITH NEW STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120406020](https://openairdocs.org/sdr/ASOA20120406020.md): Stringer · corroded · Apr 6, 2012 · N11181 · Emb EMB145XR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 21L CORRODED BETWEEN FRAMES 12-13. R & R STRINGER WITH NEW STRINGER 21L, FRAME 9-13 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20111211014](https://openairdocs.org/sdr/ASOA20111211014.md): Electronic Unit · faulty · Dec 11, 2011 · N11181 · Emb EMB145XR · Landing Gear Position and Warning
  > THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. MX INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPS CHECKS WERE GOOD.
- [SDR C2XA11TY169](https://openairdocs.org/sdr/C2XA11TY169.md): Sensor · defective · Nov 9, 2011 · N11181 · Emb EMB145XR · Engine Vibration Analyzer
  > TYS - A/C WAS EN ROUTE FROM ORD TO CHS WHEN THE E1 HP SHOWED A HIGH VIBE INDICATION/SHUT DOWN IN FLIGHT. NO OTHER ABNORMAL CONDITIONS OCCURRED. A/C DIVERTED TO TYS. MAINTENANCE REMOVED AND REPLACED THE COMPRESSOR VIBRATION SENSOR IAW RRMM 77-41-10. IPC 77
- [SDR C2XA11RI171](https://openairdocs.org/sdr/C2XA11RI171.md): Actuator · faulty · Oct 19, 2011 · N11181 · Emb EMB145XR · Landing Gear Door Actuator
  > FLT 5862 IAD CREW REPORTED LG AIR/GRND FAIL MESSAGE ON EICAS DURING GEAR EXTENSION. GEAR OPERATED NORMALLY AND A/C LANDED WITHOUT INCIDENT. IAD MX REMOVED AND REPLACED LT NOSE DOOR ACTUATOR IAW EMB145 32-33-05 WITH OPERATIONAL AND LEAK CHECKS SUCCESSFUL. A/
- [SDR C2XA11RI136](https://openairdocs.org/sdr/C2XA11RI136.md): Fuel Line · leaking · Aug 16, 2011 · N11181 · Emb EMB145XR · APU Engine Fuel and Control
  > FLIGHT 2566 - EWR - FLIGHT CREW REPORTED STRONG FUEL SMELL IN COCKPIT DURING TAXI. EWR MX PERFORMED GVI ON APU AREA AND FOUND FCU LINES LEAKING. SUSPECT SMELL IS COMING FROM FCU LEAKING. APU MEL`ED. ACFT RELEASED FOR FLIGHT. (SDR FILED OPEN PENDING FINAL C

Next page: https://openairdocs.org/aircraft/N11181/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 = 'N11181' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N11181/reports

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