# Service difficulty reports: N11107

A list on [N11107](https://openairdocs.org/aircraft/N11107.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 · 71 reports

- [SDR JJBA20220304004](https://openairdocs.org/sdr/JJBA20220304004.md): Lamp · inoperative · Mar 4, 2022 · N11107 · Emb EMB145XR · Emergency Lighting
  > SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECK FAIL. UPON FURTHER INVESTIGATION FOUND BROKEN SPLICE IN WIRE BUNDLE ON DOOR HINGE. REPAIRED SPLICE. OPS CHECK SAT.
- [SDR JJBA20220304003](https://openairdocs.org/sdr/JJBA20220304003.md): Lamp · inoperative · Mar 4, 2022 · N11107 · Emb EMB145XR · Emergency Lighting
  > LH EXTERNAL EMERGENCY WING FAIRING LIGHT FOUND TO BE DIM. REMOVED AND REPLACED LH EXTERNAL EMERGENCY WING FAIRING LIGHT. OPS CHECK FAILED. FOUND HOUSING TO HAVE A BAD GROUND. REMOVED LH EXTERNAL EMERGENCY WING LIGHT HOUSING. INSTALLED LH EXTERNAL EMERGENCY WIN
- [SDR JJBA20210217018](https://openairdocs.org/sdr/JJBA20210217018.md): Not Reported · not reported · Feb 17, 2022 · N11107 · Emb EMB145XR · Emergency Lighting
  > FLOOR PATH LIGHTING STRIP "EXIT" PLACARDS ARE MISPOSITIONED. CORRECTLY ORIENTED FLOOR PATH LIGHTING STRIPS "EXIT" PLACARDS.
- [SDR JJBA2022020431033](https://openairdocs.org/sdr/JJBA2022020431033.md): Coffeemaker · odor · Jan 31, 2022 · N11107 · Emb EMB145XR · Buffet/Galleys
  > FA REPORTS BURNING SMELL FROM COFFEE MAKERS. CLEANED UP COFFEE BREW WARMER, PERFORMED VISUAL INSPECTION COFFEE BREW CRACKS, WIRES. NO DEFECTS NOTED. OPS CHECK GOOD
- [SDR JJBA20211213009](https://openairdocs.org/sdr/JJBA20211213009.md): Lamp · inoperative · Dec 13, 2021 · N11107 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY EXIT LIGHT FORWARD OF WING INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK SAT.
- [SDR JJBA20210603008](https://openairdocs.org/sdr/JJBA20210603008.md): Inverter · inoperative · Jun 3, 2021 · N11107 · Emb EMB145XR · Emergency Lighting
  > FWD CEILING CABIN EMERGENCY EXIT LOCATOR LIGHT INOPERATIVE. R&R EMERGENCY LIGHT INVERTER 6. OPS CHECK SAT.
- [SDR JJBA20210517015](https://openairdocs.org/sdr/JJBA20210517015.md): Bulb · burned out · May 17, 2021 · N11107 · Emb EMB145XR · Emergency Lighting
  > ENTRYWAY EMERGENCY LIGHT BULB BURNT OUT. R&R ENTRYWAY LIGHT BULB. OPS CHECK SAT.
- [SDR ASOA2020071304016](https://openairdocs.org/sdr/ASOA2020071304016.md): Display · inoperative · Jul 10, 2020 · N11107 · Emb EMB145XR · Central Display
  > IAH - FLIGHT 3980, THE CREW REPORTED PFD#1 FAIL "SMOKED SMELL". THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PFD#1, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2020030433020](https://openairdocs.org/sdr/ASOA2020030433020.md): Skin · chafed · Feb 3, 2020 · N11107 · Emb EMB145XR · Elevator, Plate/Skin
  > DURING C CHECK INSPECTION FOUND LEFT ELEVATOR LEADING EDGE SKIN WAS CHAFED INTERNALLY JUST FORWARD OF CUTOUT REINFORCEMENT BETWEEN RIB YH983.4 AND YH1280. MAINTENANCE REPLACED LEADING EDGE SKIN I/A/W SRM 51-10-04 AND SB 145-27-0034.
- [SDR ASOA2020030693026](https://openairdocs.org/sdr/ASOA2020030693026.md): Rib · corroded · Jan 29, 2020 · N11107 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C CHECK INSPECTION FOUND VENTRAL TANK FORWARD FACE OF RIB 1 HAS CORROSION AT LOWER CENTER SUPPORT BRACKET. MAINTENANCE REPAIRED VENTRAL TANK RIB 1 I/A/W ETD 2020-145-004783 REVISION C
- [SDR ASOA202002193015](https://openairdocs.org/sdr/ASOA202002193015.md): Skin · corroded · Jan 9, 2020 · N11107 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C CHECK INSPECTION FOUND CORROSSION ON FUSELAGE SKIN AT AFT RADIO ALTIMETER AT FRAME 65 STRINGER 21L-21R. MAINTENANCE REPAIRED I/A/W ETD2020-145-001101
- [SDR ASOA2020030463025](https://openairdocs.org/sdr/ASOA2020030463025.md): Floor Support · corroded · Jan 6, 2020 · N11107 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C CHECK INSPECTION FOUND FLOOR BOARD SUPPORT CORRODED FRAME 18-23 STRINGER 15L-16L. MAINTENANCE REPLACED FLOOR BOARD SUPPORT
- [SDR ASOA202002193016](https://openairdocs.org/sdr/ASOA202002193016.md): Doubler · corroded · Jan 5, 2020 · N11107 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C CHECK INSPECTION FOUND CORROSSION AND MISSING RIVET ON AFT RADIO ALTIMETER BASE FRAME 68-69 AND STRINGER 21L-21R. MAINTENANCE PERFROMED REPAIR I/A/W ETD 2020-145-001101
- [SDR ASOA2020020353006](https://openairdocs.org/sdr/ASOA2020020353006.md): Bearing Cap · corroded · Jan 5, 2020 · N11107 · Emb EMB145XR · Main Landing Gear
  > DURING C CHECK INSPECTION FOUND RIGHT FORWARD MAIN LANDING GEAR BEARING CAP HAD CORROSION/PITTING. MAINTENANCE REPLACED THE RIGHT FORWARD MAIN LANDING GEAR BEARING CAP.
- [SDR ASOA2020021903017](https://openairdocs.org/sdr/ASOA2020021903017.md): Skin Splice · corroded · Jan 3, 2020 · N11107 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C CHECK INSPECTION SKIN SPLICE WAS FOUND CORRODED AT FRAME 60-61 STRINGER 20R-21R. MAINTENANCE REPAIRED I/A/W SRM 53-00-02 AND 51-40-02.
- [SDR ASOA2020020633014](https://openairdocs.org/sdr/ASOA2020020633014.md): Gusset · corroded · Jan 3, 2020 · N11107 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C CHECK INSPECTION FOUND LAV FLOOR CENTER GUSSET AT FRAME 61 HAS SURFACE CORROSION. MAINTENANCE REPLACED LAV FLOOR CENTER GUSSET.
- [SDR ASOA2020020633013](https://openairdocs.org/sdr/ASOA2020020633013.md): Gusset · corroded · Jan 3, 2020 · N11107 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C CHECK INSPECTION FOUND CENTER FUSELAGE IV FLOOR GUSSET HAT BEAM AT FRAME 61 HAD CORROSION. MAINTENANCE REPLACED GUSSET HAT BEAM AT FRAME 61
- [SDR ASOA202002033008](https://openairdocs.org/sdr/ASOA202002033008.md): Bearing Cap · corroded · Jan 3, 2020 · N11107 · Emb EMB145XR · Main Landing Gear
  > DURING C CHECK INSPECTION FOUND LEFT AFT MAIN LANDING GEAR BEARING CAP HAD CROSSION PITTING IN 1 AREA. MAINTENANCE INSPECTED AND REMOVED CORROSION IA/W SRM 57-51-07.
- [SDR ASOA202002033007](https://openairdocs.org/sdr/ASOA202002033007.md): Bearing Cap · corroded · Jan 3, 2020 · N11107 · Emb EMB145XR · Main Landing Gear
  > DURING C CHECK INSPECTION FOUND LEFT FORWARD MAIN LANDING GEAR BEARING CAP HAD 3 AREAS OF CORROSION/PITTING. MAINTENANCE REPLACED LEFT FORWARD MAIN LANDING GEAR BEARING CAP.
- [SDR ASOA202001313005](https://openairdocs.org/sdr/ASOA202001313005.md): Floor Support · corroded · Jan 3, 2020 · N11107 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK INSPECTION FOUND CORROSION ON CENTER LAV FLOORBOARD SUPPORT AT FRAME 60-61. MAINTENANCE REPLACED LAV CENTER FLOOR BOARD SUPPORT. (GUSSET)
- [SDR ASOA202001313004](https://openairdocs.org/sdr/ASOA202001313004.md): Gusset · corroded · Jan 3, 2020 · N11107 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE CHECK CORROSSION WAS FOUND ON RIGHT SIDE LAV FLOORBOARD SUPPORT. AT FRAME 60 THRU61. MAINTENANCE REPLACED HAT BEAM GUSSET AT FRAME 60 TO 61.
- [SDR ASOA202002263018](https://openairdocs.org/sdr/ASOA202002263018.md): Channel · corroded · Jan 2, 2020 · N11107 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C CHECK INSPECTION FOUND SERVICE DOOR SILL CORRODED@HOLES FOR SCREWS. MAINTENANCE REPLACED THE SERVICE DOOR SILL CHANNEL.
- [SDR ASOA2020030313019](https://openairdocs.org/sdr/ASOA2020030313019.md): Door Frame · corroded · Dec 31, 2019 · N11107 · Emb EMB145XR · Fuselage Main, Structure
  > DURING C CHECK INSPECTION CARGO DOOR CUTOUT SILL BEAM CORRODED AT FORWARD CORNER. MAINTENANCE REPLACED THE LOWER FRAME DOOR CARGO DOOR BEAM.
- [SDR ASOA2020030403024](https://openairdocs.org/sdr/ASOA2020030403024.md): Skin · damaged · Dec 30, 2019 · N11107 · Emb EMB145XR · Trailing Edge Flaps
  > DURING C CHECK INSPECTION RIGHT INBOARD FLAP UPPER SURFACE HAS DAMAGED COMPOSITE AT INBOARD EDGE. MAINTENANCE REPAIRED COMPOSITE DAMAGE AT UPPER SKIN INBOARD EDGE I/A/W SRM 57-52-00.
- [SDR ASOA202002063012](https://openairdocs.org/sdr/ASOA202002063012.md): Rod · corroded · Dec 26, 2019 · N11107 · Emb EMB145XR · APU Cowling/Containment
  > DURING C CHECK INSPECTION FOUND LEFT APU LOWER MOUNTING ROD END CORRODED.MAINTENANCE REPLACED LEFT LOWER ROD ASSEMBLY.
- [SDR ASOA20200206311](https://openairdocs.org/sdr/ASOA20200206311.md): Support Rod · corroded · Dec 26, 2019 · N11107 · Emb EMB145XR · APU Cowling/Containment
  > DURING C CHECK INSPECTION FOUND UPPER APU MOUNTING RODENDS CORRODED. MAINTENANCE REPLACED APU UPPER SUPPORT RODS.
- [SDR ASOA2020304223022](https://openairdocs.org/sdr/ASOA2020304223022.md): Rib · cracked · Dec 22, 2019 · N11107 · Emb EMB145XR · Wing, Rib/Bulkhead
  > DURING C CHECK INSPECTION THE LEFT WING RIB 21 WAS FOUND CRACKED. MAINTENANCE PERFORMED REPAIR I/A/W SRM 57-20-07.
- [SDR ASOA20200203009](https://openairdocs.org/sdr/ASOA20200203009.md): Doubler · corroded · Dec 20, 2019 · N11107 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C CHECK INSPECTION FOUND CENTER FUSELAGE IV DRAIN PLUG DOUBLER HAD CORROSION, FRAME 53-FRAME 54 STRINGER 21 LH TO 21 RH. MAINTENANCE REPLACED DOUBLER I/A/W ETD2020-145-001840
- [SDR ASOA2020030493023](https://openairdocs.org/sdr/ASOA2020030493023.md): Rib · cracked · Dec 19, 2019 · N11107 · Emb EMB145XR · Wing, Rib/Bulkhead
  > DURING C CHECK INSPECTION FOUND RIGHT WING RIB 21 CRACKED. MAINTENANCE REPAIRED RIGHT WING RIB 21 I/A/W SRM 57-20-07.
- [SDR ASOA2020030453021](https://openairdocs.org/sdr/ASOA2020030453021.md): Skin · gouged · Dec 15, 2019 · N11107 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C CHECK INSPECTION FOUND GOUGE ON FORWARD FUSELAGE SKIN II BELOW GPU ACCESS DOOR. MAINTENANCE REPAIRED DAMAGED SKIN I/A/W SRM 53-12-01 AND ETD2020-145-002945
- [SDR ASOA201906294038](https://openairdocs.org/sdr/ASOA201906294038.md): Light · inoperative · Jun 29, 2019 · N11107 · Emb EMB145XR · Emergency Lighting
  > IAH - FLIGHT 4197, THE CREW REPORTED THAT THE EMERGENCY LIGHT NEAR THE EXIT DOOR IN THE CEILING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE
- [SDR ASOA201902264007](https://openairdocs.org/sdr/ASOA201902264007.md): Battery Pack · discharged · Feb 26, 2019 · N11107 · Emb EMB145XR · Emergency Lighting
  > ** SUPPLEMENTAL TO ASOA201802264007 CONTROL NUMBER SHOULD HAVE BEEN ASOA201902264007*** IAH- DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHTS WEER FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND TWO EMERGENCY LIGHT BATTERY PA
- [SDR ASOA201902264008](https://openairdocs.org/sdr/ASOA201902264008.md): Battery Pack · discharged · Feb 26, 2019 · N11107 · Emb EMB145XR · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHTS WEER FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND TWO EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS NOTRED AND THE AIRCRAFT WAS APPROVED FOR RETU
- [SDR ASOA201802177017](https://openairdocs.org/sdr/ASOA201802177017.md): Skin · dented · Feb 17, 2018 · N11107 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FOUND A CREASED AREA AFT OF A RECENT REPAIR BETWEEN FRAMES 19 - 20 AND STRINGERS 11L AND 12L. MAINTENANCE REMOVED THE OLD DOUBLER AND CUT OUT THE DAMAGE AREA AND INSTALL A FILLER AND A NEW DOUBLER ENCOMPASSING ALL OF THE DAMAGE IAW ETD2018-145-019052.
- [SDR ASOA20140529087](https://openairdocs.org/sdr/ASOA20140529087.md): Bracket · worn · May 29, 2014 · N11107 · Emb EMB145XR · Ailerons
  > DURING C-CHECK, INSPECTION FOUND THE LT AILERON PCA BRACKET INBD HAT BUSHING FOR INBD ATTACH POINT HAS NO INTERFERENCE FIT. MAINTENANCE R & R THE LT AILERON PCA BRACKET IAW AMM 27-10-00. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA20140219019](https://openairdocs.org/sdr/ASOA20140219019.md): Switch · malfunctioned · Feb 19, 2014 · N11107 · Emb EMB145XR · Ignition Power Supply
  > THE CREW REPORTED AT FL350 WITH THRUST SET FOR CRUISE FLIGHT, THEY EXPERIENCED TWO AUTO RELIGHT SEQUENCES WITH NO ASSOCIATED CAUTION AND WARNING MESSAGES BUT DID FEEL THE EFFECT OF THE ASSOCIATED POWER LOSS AND SUCCESSFUL RELIGHT. MAINTENANCE INSPECTED AND RE
- [SDR ASOA20130610057](https://openairdocs.org/sdr/ASOA20130610057.md): Unknown · odor · Jun 10, 2013 · N11107 · Emb EMB145XR · Air Distribution System
  > CREW REPORTED A ODOR OF SMOKE IMMEDIATELY AFTER THE ACFT WAS POSSIBLY STRUCK BY LIGHTNING. MX INSPECTED ACFT, RAN AIR CONDITIONING PACKS, TAXIED, AND HAD ELECTRICAL POWER ON ACFT FOR HOURS WITH NO ODOR OF SMOKE OR LIGHTNING STRIKE DAMAGE NOTED. ACFT WAS APPRO
- [SDR ASOA20130424039](https://openairdocs.org/sdr/ASOA20130424039.md): Oil System · overserviced · Apr 24, 2013 · N11107 · Emb EMB145XR · APU Oil System
  > CREW REPORTED A STRONG ELECTRICAL ODOR IN COCKPIT AND CABIN AT FL220. MX PERFORMED FAULT ISOLATION TASK 21-20-00-810-801A AND 21-20-00-810-803A WITH NO DEFECTS NOTED, NO FAILED ELECTRICAL COMPONENTS OR FLUID LEAKS NOTED. RAN ENGINES, APU, AND AIR CONDITIONIN
- [SDR ASOA20121224182](https://openairdocs.org/sdr/ASOA20121224182.md): Wire · shorted · Dec 21, 2012 · N11107 · Emb EMB145XR · Light System Wiring
  > MAIN DOOR EMERGENCY LIGHT AND MAIN ENTRANCE EMERGENCY LIGHT INOPERATIVE. REPAIRED SHORTED WIRE AT OVERHEAD LIGHT. OPS CHECK GOOD.
- [SDR ASOA20121025085](https://openairdocs.org/sdr/ASOA20121025085.md): Engine · leaking · Oct 25, 2012 · N11107 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > THE CREW REPORTED SMOKE IN THE COCKPIT & CABIN AFTER TAKE-OFF, ALONG WITH LAVATORY SMOKE MESSAGE WARNING. AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.
- [SDR ASOA20120508096](https://openairdocs.org/sdr/ASOA20120508096.md): Fuel Tank · gouged · May 8, 2012 · N11107 · Emb EMB145XR · Fuel Storage
  > BOTTOM CENTER OF THE VENTRAL TANK WAS FOUND GOUGED. MX REPAIRED VENTRAL TANK BY INSTALLING A DOUBLER IAW EC 2810-01053. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK
- [SDR ASOA20120405037](https://openairdocs.org/sdr/ASOA20120405037.md): Battery · discharged · Apr 5, 2012 · N11107 · Emb EMB145XR · Emergency Lighting
  > DURING ROUTINE MX, EMERGENCY LIGHT INOPERATIVE AT EXIT ROW 12 A, B, C. REPLACED NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.
- [SDR ASOA20120229028](https://openairdocs.org/sdr/ASOA20120229028.md): Unknown · odor · Feb 29, 2012 · N11107 · Emb EMB145XR · Air Distribution System
  > AFTER SHUTTING DOWN THE APU ON ARRIVAL CREW REPORTED AN ELECTRICAL BURNING ODOR. MX INSPECTED THE ACFT WITH NO DEFECTS NOTED, OPS TESTED APU WITH NO DEFECTS NOTED, THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2012180003](https://openairdocs.org/sdr/ASOA2012180003.md): Skin · gouged · Feb 18, 2012 · N11107 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > ACFT HAD GROUND DAMAGE AND WAS FERRIED FOR THE REPAIRS. THE FUSELAGE BETWEEN FR 65 TO FR 66 AND BETWEEN STR 17L AND 18L WERE DAMAGED. THE WORK WAS ACCOMPLISHED IAW EC5300-01025. ALSO THE TEMPORARY REPAIRS WERE COMPLIED WITH IAW THE REPAIR ETD2012-145-001697C
- [SDR C2XA11CL211](https://openairdocs.org/sdr/C2XA11CL211.md): Trim Switch · faulty · Sep 20, 2011 · N11107 · Emb EMB145XR · Stabilizer Control System
  > THE CREW REPORTED A PITCH TRIM BACK-UP FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BACK-UP PITCH TRIM SWITCH.OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11RI131](https://openairdocs.org/sdr/C2XA11RI131.md): Warning System · malfunctioned · Aug 9, 2011 · N11107 · Emb EMB145XR · Landing Gear Position and Warning
  > FLIGHT 3124 - EWR - FLIGHT CREW REPORTED L/G AIR GROUND FAIL INDICATION ON EICAS. EWR MX PERFORMED AIR GROUND SYSTEM RESET AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA11RI078](https://openairdocs.org/sdr/C2XA11RI078.md): Audio Panel · defective · May 12, 2011 · N11107 · Emb EMB145XR · Audio Integrating System
  > FLIGHT 4940 - EWR - FLIGHT CREW REPORTED FO AUDIO CONTROL PANEL GAVE OUT ELECTRICAL SMELL. EWR MX REMOVED AND REPLACED FO AUDIO CONTROL PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10RI156](https://openairdocs.org/sdr/C2XA10RI156.md): Switch · inoperative · Dec 12, 2010 · N11107 · Emb EMB145XR · Airfoil Anti/De-ice System
  > FLIGHT 2640 - MSN - FLIGHT CREW REPORTED WING ANTI-ICE FAIL IN ICE CONDITION - ANTI ICE INOPERATIVE. EWR MX REMOVED AND REPLACED NR 2 WING LOW PRESSURE SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10SH323](https://openairdocs.org/sdr/C2XA10SH323.md): Skin · cracked · Oct 4, 2010 · N11107 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK EXTERNAL FUSELAGE HAS POSSIBLE CRACKS AROUND FASTENER HEAD AT FRAME 78 STR 5L. MAINTENANCE PERFORMED REPAIR ON FRAME 78-79 STR 5L-6L IAW EC5330-02251. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH322](https://openairdocs.org/sdr/C2XA10SH322.md): Crossbeam · corroded · Oct 4, 2010 · N11107 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CROSSBEAM AT FRAME 23 FROM CENTER OMEGA BEAM TO RT AFT FLOOR SILL HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSBEAM AT FRAME 23 FROM CENTER OMEGA BEAM TO RT AFT FLOOR SILL. THE AIRCRAFT WAS APPROVED FOR RETURN TO

Next page: https://openairdocs.org/aircraft/N11107/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 = 'N11107' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N11107/reports

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