# Service difficulty reports: N11548, cancelled Feb 23, 2022

A list on [N11548, cancelled Feb 23, 2022](https://openairdocs.org/deregistered/N11548-2022-02-23.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 ASOA2019121945118](https://openairdocs.org/sdr/ASOA2019121945118.md): Yoke · cracked · Dec 14, 2019 · N11548 · Emb EMB145LR · Engine Mount Section
  > DURING MX INSPECTION THE #1 ENGINE FORWARD UPPER YOKE FITTING WAS FOUND CRACKED. MX R&R THE #1 ENGINE FORWARD UPPER YOKE FITTING IAW STS EA26-2014-063. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201908305098](https://openairdocs.org/sdr/ASOA201908305098.md): Light · inoperative · Aug 30, 2019 · N11548 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE RIGHT OVER WING EMERGENCY LIGHT WAS NOT ILLUMINATING. MX REMOVED AND REPLACED RT OVER WING EMERGENCY LIGHT IAW AMM 33-50-07 OPS CHECKED GOOD AT THIS TIME. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201908305097](https://openairdocs.org/sdr/ASOA201908305097.md): Light · inoperative · Aug 30, 2019 · N11548 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE EMERGENCY LIGHT SYSTEM BATTERY POWERED FLOOR PROXIMITY STRIP AT SEATS 18 THROUGH 20 NOT ILLUMINATING ( EMERGENCY LIGHTING SYSTEM (BATTERY POWERED) FLOOR PROXIMITY STRIPS ITEM MOVED TO DMIL OPERATE PER MEL 33-50-00-2 EXP 09-50-00-2 CAT
- [SDR ASOA2019021974006](https://openairdocs.org/sdr/ASOA2019021974006.md): Light · inoperative · Feb 17, 2019 · N11548 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE R/H EMERGENCY OVERWING EXTERIOR LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201802144010](https://openairdocs.org/sdr/ASOA201802144010.md): Engine · failed · Feb 14, 2018 · N11548 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > THE CREW REPORTED AN UINCOMMANDED SHOUTDOWN OF THE NR 2 ENGINE DURING FLIGHT. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVE
- [SDR ASOA201711064058](https://openairdocs.org/sdr/ASOA201711064058.md): Wire · broken · Nov 6, 2017 · N11548 · Emb EMB145LR · Light System Wiring
  > THE AISLE EMERGENCY LIGHT STRIP BETWEEN SEATS 8A - 9A WAS FOUND TO HAVE A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP, OPS TESTED WITH NO DEFECTS, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201710047019](https://openairdocs.org/sdr/ASOA201710047019.md): Frame · damaged · Oct 2, 2017 · N11548 · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 62 DAMAGED BETWEEN STRINGERS 4R & 5R. REMOVED AND REPLACED THE DAMAGED SECTION OF THE FRAME. RETURNED TO SERVICE
- [SDR ASOA201710047020](https://openairdocs.org/sdr/ASOA201710047020.md): Fuse · blown · Sep 30, 2017 · N11548 · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT ON COCKPIT CEILING PANEL 225CTC INOPERATIVE. REMOVED AND REPLACED THE FUSE IN THE NR 1 EMERGENCY LIGHT BATTERY TRAY. OPS CHECKED GOOD.
- [SDR ASOA201709107013](https://openairdocs.org/sdr/ASOA201709107013.md): Frame · damaged · Sep 10, 2017 · N11548 · Emb EMB145LR · Fuselage Main, Frame
  > A/C IS IN FOR A C-CHECK INSPECTION WHEN THE INSPECTOR FOUND FRAME 62 DAMAGED BETWEEN STRINGER 4R AND 5R. MAINTENANCE R&R THE DAMAGED SECTION OF FRAME 62 AT STR. 5R TO 1R IAW SRM 53-00-04. ALL WORK COMPLETED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA201611054107](https://openairdocs.org/sdr/ASOA201611054107.md): Drag Angle · cracked · Nov 5, 2016 · N11548 · Emb EMB145LR · Vertical Stabilizer
  > DURING AN A CHECK INSPECTION, THE RIGHT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED AT FRAME 76, MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611054105](https://openairdocs.org/sdr/ASOA201611054105.md): Skin · cracked · Nov 5, 2016 · N11548 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING AN A CHECK INSPECTION, THE RIGHT AFT FUSELAGE SKIN WAS FOUND TO HAVE A 20MM CRACK AT FRAME 75 STRINGER 1R, MAINTENANCE PERFORMED A DOUBLER REPAIR TOP THE AFFECTED AREA, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20161004054C](https://openairdocs.org/sdr/ASOA20161004054C.md): Lamp · inoperative · Oct 4, 2016 · N11548 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, THE RIGHT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LAMPS. OPS CHECKED GOOD.
- [SDR ASOA201704044016](https://openairdocs.org/sdr/ASOA201704044016.md): Skin · gouged · Apr 4, 2016 · N11548 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE INSPECTION, THE AIRCRAFT SKIN WAS FOUND TO BE GOUGED UNDER THE GPU DOOR. MAINTENANCE CUT OUT THE DAMAGE AND INSTALLED A DOUBLER AND FILLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160306008R](https://openairdocs.org/sdr/ASOA20160306008R.md): Charger · inoperative · Mar 6, 2016 · N11548 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 BATTERY CHARGER ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150611033](https://openairdocs.org/sdr/ASOA20150611033.md): Battery · discharged · Jun 11, 2015 · N11548 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 18. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA20141118132](https://openairdocs.org/sdr/ASOA20141118132.md): Outflow Valve · faulty · Nov 18, 2014 · N11548 · Emb EMB145LR · Pressure Regulator/Outflow Valve
  > CREW REPORTED LOSS OF PRESSURIZATION AND CABIN ALTITUDE EXCEEDED 10000 FT ALONG WITH O2 MASKS DEPLOY. MAINTENANCE R & R THE PNUEMATIC OUTFLOW VALVE AND MANUAL PRESSURE CONTROLLER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140910098](https://openairdocs.org/sdr/ASOA20140910098.md): Battery Pack · inoperative · Sep 10, 2014 · N11548 · Emb EMB145LR · Emergency Lighting
  > BOTH OF THE AFT EXTERIOR EMERGENCY LIGHTS AND LAST TWO EMERGENCY FLOOR PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT SYSTEM BATTERY PACK WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140109003](https://openairdocs.org/sdr/ASOA20140109003.md): A/C Pack · smoke · Jan 9, 2014 · N11548 · Emb EMB145LR · Cabin Cooling System
  > THE CREW REPORTED NR 2 PACK INOPERATIVE. WHEN RUNNING, SMOKE IN CABIN. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS. NO DEFECTS OR SMOKE NOTED.
- [SDR ASOA20131127133](https://openairdocs.org/sdr/ASOA20131127133.md): Valve · faulty · Nov 27, 2013 · N11548 · Emb EMB145LR · Cabin Pressure Control System
  > PILOT REPORTED BLEED VALVE NR 2 CLOSED ADVISORY MESSAGE PRESENT DURING CLIMBOUT, HIGH ALTITUDE WARNING PRESENT AT 17,000 FT, UNABLE TO REMAIN PRESSURIZED, DESCENDED TO 10,000FT TO REMAIN PRESSURIZED. MX R & R NR 1 HIGH STAGE VALVE, PRESSURE SWITCH, AND THE DIG
- [SDR ASOA20131029123](https://openairdocs.org/sdr/ASOA20131029123.md): Bulb · blown · Oct 29, 2013 · N11548 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE CEILING EMERGENCY LIGHT ABOVE SEAT ROW 12BC WAS FOUND INOPERATIVE. MX R & R THE 12BC LIGHT ASSY BULB WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201228111](https://openairdocs.org/sdr/ASOA201228111.md): Lamp · inoperative · Nov 28, 2012 · N11548 · Emb EMB145LR · Emergency Lighting
  > DURING A-CHECK INSPECTION, IT WAS FOUND THAT THE LT OVERWING AND ROW 12 EMERGENCY LIGHTS WERE INOPERATIVE. MX R & R THE LIGHT BULBS IN BOTH THE LT OVERWING AND ROW 12 EMERGENCY LIGHTS WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121002109](https://openairdocs.org/sdr/ASOA20121002109.md): Seal · damaged · Oct 2, 2012 · N11548 · Emb EMB145LR · Passenger/Crew Doors
  > CABIN ALTITUDE CLIMBED TO 11900 IN AUTO MODE, AND CONTINUED IN MANUAL MODE TO 12100. DIVERTED. MX FOUND CARGO DOOR SEAL DAMAGED, REMOVED AND INSTALLED CARGO DOOR SEAL WITH INSERTION REPAIR IAW AMM 52-00-04. PRESSURIZATION OPS CHECKED GOOD IAW AMM 21-30-00.
- [SDR ASOA20120831072](https://openairdocs.org/sdr/ASOA20120831072.md): Gcu · faulty · Aug 31, 2012 · N11548 · Emb EMB145 · AC Generator-Alternator
  > THE CREW REPORTED SMOKE IN THE COCKPIT & SPARKS COMING OUT OF APU STARTER GENERATOR APU OUTLET. MAINTENANCE REPLACED THE APU GENERATOR CONTROL UNIT AND REPLACED THE APU STARTER GENERATOR. OPS CHECKS WERE GOOD.
- [SDR ASOA20120604081](https://openairdocs.org/sdr/ASOA20120604081.md): Stiffener · cracked · Jun 4, 2012 · N11548 · Emb EMB145LR · APU Cowling/Containment
  > DURING A-CHECK INSPECTION, APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP OF THE RT VERTICLE STIFFENER. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120605083](https://openairdocs.org/sdr/ASOA20120605083.md): Firewall · cracked · Jun 3, 2012 · N11548 · Emb EMB145LR · APU Cowling/Containment
  > DURING A-CHECK INSPECTION, THE APU FIREWALL WAS FOUND TO BE CRACKED ON THE RT STIFFENER. MX PERFORMED A DOUBLER REPAIR AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120602082](https://openairdocs.org/sdr/ASOA20120602082.md): Skin · dented · Jun 2, 2012 · N11548 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING A-CK INSPECTION, A DENT WAS FOUND IN THE LT REAR FUSELAGE BETWEEN FRAMES 77 AND 78 AND STRINGERS 15L & 16L. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201201310011](https://openairdocs.org/sdr/ASOA201201310011.md): Light · inoperative · Jan 31, 2012 · N11548 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX, THE AFT AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MX REPLACED THE AFT EMERGENCY LIGHT STRIP. OPS CHECKS WERE GOOD.
- [SDR ASOA201201016004](https://openairdocs.org/sdr/ASOA201201016004.md): Controller · intermittent · Jan 9, 2012 · N11548 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED THAT DURING FLIGHT THE CABIN EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. THE ACFT LANDED WITHOUT INCIDENT WHERE MX REPLACED THE EMERGENCY LIGHT CONTROLLER, OPERATIONALLY TESTED THE SYS AND CLEARED THE DISCREPANCY.
- [SDR ASOA20111215021](https://openairdocs.org/sdr/ASOA20111215021.md): Light · malfunctioned · Dec 15, 2011 · N11548 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED THE EMERGENCY LIGHTS COME ON IN NORMAL POSITION. MX INSPECTED AND REPLACED RELAY KO275, REPLACED NR 2 AND NR 4 EMERGENCY LIGHT BATTERY CHARGERS AND REPLACED NR 1, 2, 3, 4 EMERGENCY LIGHT BATTERIES. OPS CHECKED GOOD.
- [SDR ASOA2011121300015](https://openairdocs.org/sdr/ASOA2011121300015.md): Control Module · faulty · Dec 13, 2011 · N11548 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED THE EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MX INSPECTED AND REPLACED THE EMERGENCY LIGHT CONTROL MODULE AND THE NR 2 EMERGENCY LIGHT BATTERY.
- [SDR ASOA20111212013](https://openairdocs.org/sdr/ASOA20111212013.md): Light · intermittent · Dec 12, 2011 · N11548 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED THE CABIN EMEREGENCY LIGHTS COME ON INTERMITENTLY. MX INSPECTED AND PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS. NO DEFECTS FOUND.
- [SDR ASOA20111208008](https://openairdocs.org/sdr/ASOA20111208008.md): Diode · failed · Dec 8, 2011 · N11548 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX INSPECTION, IT WAS DISCOVERED ALL THE EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN THE ARM POSITION. MX R & R DIODE CR0220 AND THE F/A CONTROL PANEL IAW WM 28-23-50 AND 25-27-09 WITH OPS CHECKED SUCCESSFULLY. ACFT WAS APPROVED FOR RETURNED T
- [SDR ASOA20111205010](https://openairdocs.org/sdr/ASOA20111205010.md): Control Module · faulty · Dec 5, 2011 · N11548 · Emb EMB145LR · Emergency Lighting
  > WHEN THE EMERGENCY LIGHT SWITCH WAS SELECTED TO THE "ARM" POSITION THE EMERGENCY LIGHTING ILLUMINATED. MX REPLACED THE EMERGENCY LIGHT CONTROL MODULE, OPERATIONALLY TESTED THE SYS AND CLEARED THE DISCREPANCY.
- [SDR C2XA11TY168](https://openairdocs.org/sdr/C2XA11TY168.md): Controller · malfunctioned · Nov 7, 2011 · N11548 · Emb EMB145LR · Windshield/Door Rain/Ice Removal
  > FLIGHT CREW SMELLED SMOKE. REMOVED AND REPLACED WINDSHIELD HEATER CONTROLLER IAW EMB 145 30-42-01. OPS CHECK GOOD.
- [SDR C2XA11CL105](https://openairdocs.org/sdr/C2XA11CL105.md): Connector · corroded · Apr 25, 2011 · N11548 · Emb EMB145 · Flight Control System Wiring
  > THE CREW REPORTED A TAKEOFF CONFIG WARNING MESSAGE FOR SPOILERS OPEN ON TAKEOFF ROLL.SPOILERS THEN KEPT ALTERNATING OPEN/CLOSED. THE CREW ABORTED TAKEOFF. MX INSPECTED AND REPLACED RT INBD SPOILER PROXIMITY SWITCH CONNECTOR. THE CONNECTOR WAS CORRODED AND WI
- [SDR C2XA11CL103](https://openairdocs.org/sdr/C2XA11CL103.md): Proximity Switch · faulty · Apr 25, 2011 · N11548 · Emb EMB145 · Drag Control System
  > CREW REPORTED A SPOILER FAIL MESSAGE IN LEVEL CRUISE FLIGHT, THEN PERFORMED THE CFM CHECK LIST AND THE MESSAGE CONTINUED WITH A NOTED CHANGE IN OPEN/CLOSED MESSAGE FREQUENCY ON EICAS DISPLAY. NO CHANGES WITH OPEN/CLOSED MESSAGES ON DESCENT OR LANDING WERE NOT
- [SDR C2XA11IA040](https://openairdocs.org/sdr/C2XA11IA040.md): Electronic Unit · inoperative · Mar 2, 2011 · N11548 · Emb EMB145LR · Landing Gear Position and Warning
  > OMA - FLIGHT 3044, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL EICAS MESSAGE AND THE GEAR WOULD NOT RETRACT ON CLIMB. THE AIRCRAFT RETURNED TO OMA WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS SUBSEQUENTLY FERRIED TO MCI WHERE MAINTENANCE REMOVED AND
- [SDR C2XA10RI083](https://openairdocs.org/sdr/C2XA10RI083.md): Battery · overtemp · Jun 18, 2010 · N11548 · Emb EMB145LR · Battery/Charger System
  > FLIGHT 3073 - GRR - FLIGHT CREW REPORTED NR 2 MAIN BATTERY OVERTEMP INDICATION ON EICAS. CREW LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED NR 2 MAIN BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09CL134](https://openairdocs.org/sdr/C2XA09CL134.md): Wire · faulty · Oct 12, 2009 · N11548 · Emb EMB145XR · Electrical Power System Wiring
  > YYZ - FLT 2305 - THE CREW REPORTED A BAG SMOKE WARNING MESSAGE ON THE EICAS. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 26-15-00. MAINTENANCE REPAIRED WIRE SPLICE SP5189. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09RI168](https://openairdocs.org/sdr/C2XA09RI168.md): Smoke Detector · false activation · Oct 2, 2009 · N11548 · Emb EMB145LR · Smoke Detection
  > FLIGHT 2897 - YQB - FLIGHT CREW REPORTED BAG SMOKE INDICATION ON EICAS. MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09IA245](https://openairdocs.org/sdr/C2XA09IA245.md): Smoke Warning · false activation · Sep 29, 2009 · N11548 · Emb EMB145LR · Smoke Detection
  > CAE - FLIGHT 2622, THE CREW REPORTED A BAG SMOKE INDICATION. THE CREW PLACED THE BAGGAGE SMOKE DETECTOR ON MEL. THE AIRCRAFT SUBSEQUENTLY LANDED AT IAH WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY TESTED THE BAGGAGE SMOKE DETECTORS ALL WITH NO
- [SDR C2XA09TY240](https://openairdocs.org/sdr/C2XA09TY240.md): Radar · defective · Sep 18, 2009 · N11548 · Emb EMB145LR · Weather Radar System
  > TYS - AIRCRAFT DIVERTED INTO TYS FROM CLE DUE TO RADAR FAILING IN FLIGHT. A/C WAS SWAPPED TO ANOTHER A/C AND CONTINUED ON. MAINTENANCE REMOVED AND REPLACED THE WEATHER RTA ASSEMBLY IAW EMB 145 AMM 34-42-01. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.
- [SDR C2XA09CL086](https://openairdocs.org/sdr/C2XA09CL086.md): Smoke Detector · malfunctioned · Jun 16, 2009 · N11548 · Emb EMB145LR · Smoke Detection
  > THE CREW REPORTED A BAGGAGE SMOKE DETECTION LIGHT REMAINS ON. MX CONFIRMED NO SMOKE AND PLACED ON MEL 26-15-00. FLT NR 2600 MX RESET BAGGAGE SMOKE DETECTOR. OPS CHECKS WERE GOOD AND REMOVED FROM MEL.
- [SDR C2XA09TY114](https://openairdocs.org/sdr/C2XA09TY114.md): Smoke Detector · malfunctioned · Jun 16, 2009 · N11548 · Emb EMB145LR · Smoke Detection
  > TYS FOR IAH - THE BAGGAGE SMOKE DETECTOR LIGHT REMAINS ON ALL THE TIME. THE AIRCRAFT WAS RELEASED IAW MEL 26-15-00 CAT (C) CONTROL NUMBER 171219.
- [SDR C2XA09TY099](https://openairdocs.org/sdr/C2XA09TY099.md): Frame Splice · corroded · May 27, 2009 · N11548 · Emb EMB145LR · Fuselage Main, Frame
  > TYS - AIRCRAFT CURRENTLY IN A C-CHECK STATUS, INSPECTION FOUND CORROSION AT FR 65 UNDER CARGO SEAL. MAINTENANCE REPAIRED FR 65 UNDER CARGO SEAL IAW EC 5330-01458. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA09TY100](https://openairdocs.org/sdr/C2XA09TY100.md): Sill · corroded · May 26, 2009 · N11548 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TYS - AIRCRAFT CURRENTLY GOING INTO C-CHECK, INSPECTION FOUND THE CARGO SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO SILL IAW EMB 145SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C-CHECK.
- [SDR C2XA09TY097](https://openairdocs.org/sdr/C2XA09TY097.md): Sill · corroded · May 23, 2009 · N11548 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TYS - DURING C-CHECK THE LT FLOOR SILL UNDER FRAME 18 WAS FOUND CORRODED. THE LT FLOOR SILL WAS REMOVED AND REPLACED IAW EMB 135/145 SRM 51-40-02.
- [SDR C2XA09TY096](https://openairdocs.org/sdr/C2XA09TY096.md): Threshold · corroded · May 23, 2009 · N11548 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TYS - DURING C-CHECK CORROSION WAS FOUND UNDER THE PAX DOOR THRESHOLD. SMALL SURFACE CORROSION WAS BLENDED OUT AND PRIMED AND PAINTED IAW EMB 135/145 SRM 51-10-03 AND CPM 51-21-04, 05, AND 06.
- [SDR C2XA09TY095](https://openairdocs.org/sdr/C2XA09TY095.md): Sill · corroded · May 23, 2009 · N11548 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TYS - DURING C-CHECK CORROSION WAS FOUND AT THE LT WALL FLOOR SILL AT FRAME 30 TO FRAME 35. THE SILL WAS REMOVED AND REPLACED IAW EMB 135/145 SRM 51-40-02.
- [SDR C2XA09TY094](https://openairdocs.org/sdr/C2XA09TY094.md): Floor Support · corroded · May 22, 2009 · N11548 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TYS - DURING C-CHECK, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT NUT PLATE AT PAX DOOR ENTRY WAY. THE AREA WAS REPAIRED IAW EC5320-01449. A/C STILL IN C-CHECK.

Next page: https://openairdocs.org/deregistered/N11548-2022-02-23/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 = 'N11548' AND deregistration_id = 'N11548-2022-02-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N11548-2022-02-23/reports

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