# Service difficulty reports: N17928, cancelled Feb 12, 2016

A list on [N17928, cancelled Feb 12, 2016](https://openairdocs.org/deregistered/N17928-2016-02-12.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 · 118 reports

- [SDR ASOA20140710094](https://openairdocs.org/sdr/ASOA20140710094.md): Inverter · inoperative · Jul 10, 2014 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING PREFLIGHT, THE CREW REPORTED THAT 2 SECTIONS OF AISLE PATH EMERGENCY LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS.
- [SDR ASOA20140315044](https://openairdocs.org/sdr/ASOA20140315044.md): Battery Pack · discharged · Mar 15, 2014 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT LIGHT AT ROW 18 WAS FOUND TO BE INOPERATIVE. MAINTENNACE R & R BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140203018](https://openairdocs.org/sdr/ASOA20140203018.md): Inverter · inoperative · Feb 3, 2014 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHT ON THE FORWARD BULKHEAD WAS NOT WORKING. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131217222](https://openairdocs.org/sdr/ASOA20131217222.md): Acm · failed · Dec 17, 2013 · N17928 · Emb EMB145EP · Cabin Cooling System
  > THE CREW REPORTED A STRONG ELECTRICAL ODOR AS NR 1 PACK WAS RUNNING, AND ODOR STOPPED WHEN NR 1 PACK TURNED OFF. ACFT LANDED WITHOUT INCIDENT. MAINTENNACE INSPECTED AND FOUND NR 1 ACM FROZEN. R & R NR 1 ACM, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR
- [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 ASOA20130611087](https://openairdocs.org/sdr/ASOA20130611087.md): Battery Pack · discharged · Jun 11, 2013 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING MX INSPECTION THE AISLE PATH LIGHTING AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130209009H](https://openairdocs.org/sdr/ASOA20130209009H.md): Light · inoperative · Feb 9, 2013 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING SCHEDULED MX, THE PASSENGER DOOR BOTTOM EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY, OPERATIONALLY TESTED THE SYS AND CLEARED THE DISCREPANCY.
- [SDR ASOA20121210156](https://openairdocs.org/sdr/ASOA20121210156.md): Firewall · cracked · Dec 10, 2012 · N17928 · Emb EMB145EP · APU Cowling/Containment
  > DURING MAINTENANCE INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED APPROXIMATELY 1.25" TOTAL LENGTH AT THE 9 O'CLOCK POSITION WITH A RIVET IN THE MIDDLE. MAINTENANCE PEFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121208155](https://openairdocs.org/sdr/ASOA20121208155.md): Skin · cracked · Dec 8, 2012 · N17928 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > SUPPLEMENTAL, DURING A-CHECK INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 5 SEPARATE CRACKS AT 3 DIFFERENT RIVETS AT FRAME 75. THESE INCLUDE 2 CRACKS MEASURING.07" AND.25" ON EITHER SIDE OF 1 RIVET DIRECTLY ABOVE STRINGER 2 LT, 2 CRACKS MEASURING.1
- [SDR ASOA20121127143](https://openairdocs.org/sdr/ASOA20121127143.md): Light · unsecure · Nov 27, 2012 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING A-CHECK INSPECTION, THE PAX DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX RESECURED THE LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120304030H](https://openairdocs.org/sdr/ASOA20120304030H.md): Relay · burned · Mar 4, 2012 · N17928 · Emb EMB145EP · Electrical Power System
  > DURING PREFLIGHT, THE CREW REPORTED A BURNING ODOR FROM THE COAT CLOSET. MX INSPECTED THE ACFT AND R & R RELAY K0454, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20111202008](https://openairdocs.org/sdr/ASOA20111202008.md): Actuator · weak · Dec 2, 2011 · N17928 · Emb EMB145EP · Landing Gear Actuator
  > DURING CLIMB THE CREW REPORTED THAT THE RIGHT MLG WOULD NOT LOCK IN THE UP POSITION. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT WHERE MX REPLACED THE RT MAIN GEAR MANUEVERING ACTUATOR, PERFORMED OPS TESTS AND CLEARED THE DISCREPANCY.
- [SDR C2XA11SH125](https://openairdocs.org/sdr/C2XA11SH125.md): Door Frame · corroded · Aug 29, 2011 · N17928 · Emb EMB145LR · Passenger/Crew Doors
  > SHV - DURING C-CHECK THE BOTTOM FRAME OF THE MAIN CABIN DOOR WAS FOUND TO BE CORRODED AROUND THE DOOR LINING MOUNT NUT PLATES. MAINTNENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE
- [SDR C2XA11IA159](https://openairdocs.org/sdr/C2XA11IA159.md): Electronic Unit · inoperative · Jul 21, 2011 · N17928 · Emb EMB145EP · Landing Gear Position and Warning
  > IAH - FLIGHT 2705 THE CREW REPORTED AN AIR/GRND FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE OT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT (LGEU), OPERATIONALLY TESTED WITH NO DEFECTS, AND T
- [SDR C2XA11IA158](https://openairdocs.org/sdr/C2XA11IA158.md): Wire Harness · burned · Jul 19, 2011 · N17928 · Emb EMB145EP · Light System Wiring
  > DURING MAINTENANCE INSPECTION, AN ELECTRICAL ODOR WAS NOTICED IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIDEWALL LIGHT HARNESS AT SEAT 10BC TO BE BURNED. MAINTENANCE DISCONNECTED THE LIGHT AND PLACED IT ON MEL 33-20-00-1 CAT C, AND THE AIR
- [SDR C2XA11IA019](https://openairdocs.org/sdr/C2XA11IA019.md): Light · inoperative · Jan 19, 2011 · N17928 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB IN THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN T
- [SDR C2XA10IA285](https://openairdocs.org/sdr/C2XA10IA285.md): Engine · odor · Nov 8, 2010 · N17928 · Emb EMB145EP · Engine (Turbine/Turboprop)
  > FLIGHT 2719, REPORTED A PROMINENT TURBINE CASE OIL BURNED ODOR DURING ALL PHASES OF FLT. ACFT LANDED WHERE MX INSPECTED AND PLACED NR 1 PACK ON MEL, AND AIRCRAFT RETURNED TO SERVICE. MX REMOVED AND REPLACED THE NR 1 ENGINE, OPERATIONALLY TESTED WITH NO DEF
- [SDR C2XA10IA213](https://openairdocs.org/sdr/C2XA10IA213.md): Battery · overtemp · Jul 28, 2010 · N17928 · Emb EMB145EP · Battery/Charger System
  > IAH - FLIGHT 2163, THE CREW REPORTED A MAIN BATTERY TWO OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA165](https://openairdocs.org/sdr/C2XA10IA165.md): Skin · corroded · Jun 1, 2010 · N17928 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > IAH - DURING MAINTENANCE INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 72 & 73 AT STRINGER 21R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN PANEL, OPERATIONAL CHECKS COMPLETED WITHOUT DEFECT. AIRCRAFT WAS APPROVED FOR RETUR
- [SDR C2XA10IA143](https://openairdocs.org/sdr/C2XA10IA143.md): Skin · cracked · May 9, 2010 · N17928 · Emb EMB145EP · Wing, Plate/Skin
  > IAH - DURING MAINTENANCE INSPECTION THE LEFT UPPER WING SKIN WAS FOUND TOP BE CRACKED AT THE SPEED BRAKE CENTER HINGE POINT CUTOUT. MAINTENANCE PLACED THE ITEM ON DEFERRED MAINTENANCE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE INSTALLED
- [SDR C2XA09IA331](https://openairdocs.org/sdr/C2XA09IA331.md): Inverter · inoperative · Dec 29, 2009 · N17928 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE LEFT EMERGENCY EXIT TOP LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09IA181](https://openairdocs.org/sdr/C2XA09IA181.md): Light · inoperative · Jul 17, 2009 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING ROUTINE INSP, RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09CL051](https://openairdocs.org/sdr/C2XA09CL051.md): Turbine Wheel · cracked · Apr 25, 2009 · N17928 · Emb EMB145EP · Turbine Section
  > DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.
- [SDR C2XA08IA152](https://openairdocs.org/sdr/C2XA08IA152.md): Light · inoperative · Jul 5, 2008 · N17928 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING A-CK INSPECTION THE LT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)
- [SDR C2XA08CL063](https://openairdocs.org/sdr/C2XA08CL063.md): Ballast · faulty · May 29, 2008 · N17928 · Emb EMB145EP · Passenger Compartment Lighting
  > CLE FLIGHT NR 2401, THE CREW REPORTED A STRONG BURNING SMELL COMING FROM THE LAVATORY. MAINTENANCE INSPECTED AND REPLACED THE LAV LIGHT BALLAST.
- [SDR C2XA07CL074](https://openairdocs.org/sdr/C2XA07CL074.md): Wire · loose · Sep 4, 2007 · N17928 · Emb EMB145EP · Light System Wiring
  > DURING ROUTINE MAINTENANCE THE RIGHT EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECTED THE WIRE AT THE EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07CL033](https://openairdocs.org/sdr/C2XA07CL033.md): Coffeemaker · smoke · Mar 18, 2007 · N17928 · Emb EMB145EP · Buffet/Galleys
  > CMH FLIGHT 2930 THE CREW REPORTED THE COFFEE POT WAS SMOKING WHEN TURNED ON.THE COFFEE POT WAS PLACED ON MEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 COFFEE POT BREWER.OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07CL010](https://openairdocs.org/sdr/C2XA07CL010.md): Controller · burned · Jan 22, 2007 · N17928 · Emb EMB145EP · Windshield/Door Rain/Ice Removal
  > CLE FLIGHT NR 2676, THE CREW REPORTED A BURNING ODOR IN THE COCKPIT AND CABIN DURING ICE CONDITIONS THROUGHOUT DESCENT. MAINTENANCE INSPECTED AND FOUND THE TERMINAL BURNED ON THE CAPTAINS WINDSHIELD TEMP CONTROLLER. THE TEMP CONTROLLER WAS REPLACED AND OPERA
- [SDR C2XA06SH129](https://openairdocs.org/sdr/C2XA06SH129.md): Floorbeam · corroded · Nov 14, 2006 · N17928 · Emb EMB145EP · Fuselage Main, Floor Beam
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FR 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH130](https://openairdocs.org/sdr/C2XA06SH130.md): Frame · corroded · Nov 11, 2006 · N17928 · Emb EMB145EP · Fuselage Main, Frame
  > SHV - DURING C-CHECK THE SERVICE DOOR AFT FRAME 22 WAS FOUND TO BE CORRODED AROUND THE NUT PLATE HOLE, BETWEEN STR 15R AND 16R. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER
- [SDR C2XA06CL078](https://openairdocs.org/sdr/C2XA06CL078.md): Battery · inoperative · Sep 25, 2006 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE LT FRONT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR1 EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06CL074](https://openairdocs.org/sdr/C2XA06CL074.md): Light · faulty · Sep 18, 2006 · N17928 · Emb EMB145EP · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE LT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06CL051](https://openairdocs.org/sdr/C2XA06CL051.md): Ballast · burned · May 18, 2006 · N17928 · Emb EMB145EP · Passenger Compartment Lighting
  > CLE FLIGHT 3156 THE CREW REPORTED A ELECTRICAL BURNING SMELL IN THE REAR OF THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BALLAST AT ROW 18. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06IA057](https://openairdocs.org/sdr/C2XA06IA057.md): Light · inoperative · Apr 13, 2006 · N17928 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING 3A INSPECTION THE RIGHT HAND INTERIOR EMERGENCY EXIT LIGHT BY THE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05TY013](https://openairdocs.org/sdr/C2XA05TY013.md): Rivet · loose · Feb 7, 2005 · N17928 · Emb EMB145ER · Vertical Stabilizer, Plate/Skin
  > TYS, DURING A SCHEDULE INSPECTION, SMOKING RIVETS WHERE FOUND ON THE BASE OF THE VERTICAL STAB (LEFT AND RIGHT SIDES). MAINTENANCE REMOVED THE OLD RIVETS, FABRICATED AND INSTALLED DOUBLERS, (4 ON EACH SIDE) I/A/W-EC5510-01109, EMB145-SRM-51-40-02, IC2005-145/
- [SDR C2XA05TY010](https://openairdocs.org/sdr/C2XA05TY010.md): Spar · cracked · Feb 3, 2005 · N17928 · Emb EMB145ER · Wing Spar
  > TYS DURING THE ACCOMPLISHMENT OF A NDI TASK(57-28-00) A CRACK INDICATION WAS DISCOVERED. MAINTENANCE FAB`D AND INSTALLED A REPAIR DOUBLER IAW EA5710-01041. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA04CL129](https://openairdocs.org/sdr/C2XA04CL129.md): Switch · faulty · Dec 22, 2004 · N17928 · Emb EMB145ER · Cabin Cooling System
  > CLE - THE CREW REPORTED IN FLIGHT, IN ICING HAD A VERY HOT RUBBER SMELL AND PACK 2 AIR WAS VERY HOT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PACK DUCT OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA04CL122](https://openairdocs.org/sdr/C2XA04CL122.md): Noise Attenuator · ruptured · Dec 1, 2004 · N17928 · Emb EMB145ER · Air Distribution Fan
  > DURING APPROACH THE CREW REPORTED A BURNING PLASTIC SMELL. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RUPTURED NR 2 RECIRCULATION FAN NOISE ATTENUATOR. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA04CL114](https://openairdocs.org/sdr/C2XA04CL114.md): Smoke · detected · Nov 7, 2004 · N17928 · Emb EMB145ER · Air Distribution System
  > CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF THE APU AND ENGINES WITH THE BLEED AND PACKS ON. NO DEFECTS NOTED.
- [SDR C2XA04TY142](https://openairdocs.org/sdr/C2XA04TY142.md): Floor Support · corroded · Aug 3, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION
- [SDR C2XA04TY132](https://openairdocs.org/sdr/C2XA04TY132.md): Support · corroded · Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FORWARD FLOOR SILL SUPPORT IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR SILL SUPPORT IAW SRM 51-40-02.
- [SDR C2XA04TY134](https://openairdocs.org/sdr/C2XA04TY134.md): Channel · corroded · Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED 4C INSPECTION THE RT SIDE STEPUP BRACKET AFT OF PAX DOOR WAS FOUND CORRODED. MAINT. REMOVED AND REPLACED THE STEP UP BRACKET AND CENTER OMEGA BEAM IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL 4C WORK.
- [SDR C2XA04TY135](https://openairdocs.org/sdr/C2XA04TY135.md): Sill · corroded · Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED 4C INSPECTION THE RT FLOOR SILL WAS FOUND CORRODED AT FR 70. MAINT REMOVED AND REPLACED A NEW COUNTERSUNK FLOOR SILL ALLODINED AND INSTALL IAW 135/145 SRM 51-40-02;51-40-06 AND CPM 51-21-04.
- [SDR C2XA04TY130](https://openairdocs.org/sdr/C2XA04TY130.md): Support Beam · corroded · Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Main, Structure
  > DURING A SCHEDULED 4C INSPECTION SIGNS OF CORROSION WERE FOUND ON SEVERAL NUTPLATES ON SUPPORT BEAM IN THE GALLEY. MAINT. REMOVED AND REPLACED ALL TOP CAPS IN THE GALLEY AREA IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLET
- [SDR C2XA04TY133](https://openairdocs.org/sdr/C2XA04TY133.md): Floorbeam · corroded · Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Main, Floor Beam
  > TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER AREA OF THE FLOORBEAM AT FR 20>23. REMOVED AND REPLACED THE FLOORBEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL 4C INSPECTION.
- [SDR C2XA04TY131](https://openairdocs.org/sdr/C2XA04TY131.md): Floor Support · corroded · Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FR 25. REMOVED AND REPLACED THE OMEGA BEAM BETWEEN FR 22 AND FR 25. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-40-02 AND WILL BE RELEASED UPON COMPLETION OF ALL 4C W
- [SDR C2XA04TY128](https://openairdocs.org/sdr/C2XA04TY128.md): Sill · corroded · Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FLOORBOARD SILL ON THE LT SIDE AT FR 53-58. REMOVED AND REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE COMPLETION OF THE 4C INSPECT
- [SDR C2XA04TY139](https://openairdocs.org/sdr/C2XA04TY139.md): Floor Support · corroded · Jul 31, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 23 TO 30. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION
- [SDR C2XA04TY138](https://openairdocs.org/sdr/C2XA04TY138.md): Floor Support · corroded · Jul 31, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 61 TO FRAME 65. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
- [SDR C2XA04TY120](https://openairdocs.org/sdr/C2XA04TY120.md): Support · corroded · Jul 26, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RT FWD FLOORBOARD SUPPORT SILL IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR BOARD SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF THE 4C INSPECTION.

Next page: https://openairdocs.org/deregistered/N17928-2016-02-12/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 = 'N17928' AND deregistration_id = 'N17928-2016-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17928-2016-02-12/reports

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