# Service difficulty reports: N14945, cancelled Jan 16, 2019

A list on [N14945, cancelled Jan 16, 2019](https://openairdocs.org/deregistered/N14945-2019-01-16.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 · 85 reports

- [SDR ASOA20130921170](https://openairdocs.org/sdr/ASOA20130921170.md): Smoke Detector · inoperative · Sep 21, 2013 · N14945 · Emb EMB145EP · Smoke Detection
  > AFTER TAKEOFF, CREW REPORTED A LAVATORY SMOKE INDICATION. RAN QRH ITEMS AND MESSAGE WENT AWAY, NO SMOKE NOTED. ACFT LANDED WITHOUT INCIDENT. MX R & R LAVATORY SMOKE DETECTOR, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130505066](https://openairdocs.org/sdr/ASOA20130505066.md): Skin · cracked · May 5, 2013 · N14945 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 3A INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED NEAR FR 77 AT 1 RIVET AT STR9R. MX PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02501 (SMALL CIRCLE REPAIR) AND THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA20130308287](https://openairdocs.org/sdr/ASOA20130308287.md): Skin · corroded · Mar 8, 2013 · N14945 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > ACFT IS IN A C-CHECK POSITION WHEN INSPECTION FOUND CORROSION WAS FOUND ON A SKIN PANEL AT FRAME 13 AT STRINGERS 20R AND 19R. MX R & R THE SKIN PANEL IAW SRM 53-00-02. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA20130308206](https://openairdocs.org/sdr/ASOA20130308206.md): Skin · corroded · Mar 8, 2013 · N14945 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > ACFT IS IN C-CHECK WHEN INSPECTION FOUND CORROSION ON THE SKIN AFT OF FRAME 18, BETWEEN STRINGERS 20L AND 19R. MX R & R THE SKIN IAW EMB 145 EC 5330-02715. THE RVSM REMAP WAS GOOD AS WELL AS PRESSURE CHECKS. ACFT WILL BE RELEASED AT THE END OF ALL CHECKS.
- [SDR C2XA11TY149](https://openairdocs.org/sdr/C2XA11TY149.md): Skin · damaged · Sep 23, 2011 · N14945 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > AIRCRAFT SUSTAINED GROUND DAMAGE TO THE RT REAR FUSELAGE BETWEEN FRAMES 63 AND 68. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSPECTION, FABRICATED FILLERS AND DOUBLERS. REPLACED FRAME 66 INTERNAL SKIN SPLICE BETWEEN STRINGERS 8R & 9R AND 14R & 15R. GENERATED
- [SDR C2XA11IA083](https://openairdocs.org/sdr/C2XA11IA083.md): Display · shorted · May 6, 2011 · N14945 · Emb EMB145EP · Central Display
  > XNA - FLIGHT 2619 THE CREW REPORTED A SMOKE SMELL FOLLOWED BY THE CAPTAINS PFD CIRCUIT BREAKER POPPING. THE PFD WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE CAPT
- [SDR C2XA11IA030](https://openairdocs.org/sdr/C2XA11IA030.md): Unknown · odor · Feb 7, 2011 · N14945 · Emb EMB145EP · Air Distribution System
  > IAH - THE CREW REPORTED THAT THE COCKPIT SMELLED LIKE BURNING ELECTRICAL WIRE. MAINTENANCE INSPECTED THE AIRCRAFT POWERED UP THE AIRCRAFT WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH315](https://openairdocs.org/sdr/C2XA10SH315.md): Skin · damaged · Sep 20, 2010 · N14945 · Emb EMB145EP · Rudder, Plate/Skin
  > SHV - DURING C-CHECK 2 OBLONG HOLES IN RUDDER II SKIN, LT SIDE, ABOUT 1/2 WAY UP. MAINTENANCE PERFORMED REPAIR TO RUDDER II SKIN, LT SIDE, HALFWAY UP IAW EC5540-01141. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH314](https://openairdocs.org/sdr/C2XA10SH314.md): Housing · damaged · Sep 20, 2010 · N14945 · Emb EMB145EP · Vertical Stabilizer
  > SHV - DURING C-CHECK VERTICAL STABILIZER RT SPERICAL BEARING HOUSING FOUND TO BE OUT OF LIMITS. MAINTENANCE PERFORMED REPAIR ON RT SPERICAL BEARING HOUSING IAW ETD 2010-145/084787. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH313](https://openairdocs.org/sdr/C2XA10SH313.md): Beam · corroded · Sep 15, 2010 · N14945 · Emb EMB145ER · Fuselage Main, Structure
  > SHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) FRAMES 19 TO 23. MAINTENANCE REMOVED AND REPLACED RT OMEGA BEAM AT FRAME 18-24 IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA241](https://openairdocs.org/sdr/C2XA10IA241.md): Connector · burned · Aug 31, 2010 · N14945 · Emb EMB145EP · Light System Wiring
  > IAH - FLIGHT 2012, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE CABIN BEFORE BOARDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIDEWALL LIGHT ASSY AT SEAT 1A TO HAVE A BURNED CONNECTOR. MAINTENANCE PLACED THE LIG
- [SDR C2XA10SH201](https://openairdocs.org/sdr/C2XA10SH201.md): Warning Light · false activation · Jun 11, 2010 · N14945 · Emb EMB145EP · Pneumatic Distribution System
  > FLT 2213 DIVERT - E1 BLEED LK MSG-E1 COMMANDED SHUTDOWN INFLT. MAINTENANCE DOWNLOADED DFDR AND CMC - NO FAULTS FOUND, RAN AC, NO LEAKS. PERFORMED BLEED OPERATIONAL CHECKS IAW EMB-145 AMM 36-00-00 AND 36-11-09, ALL OPERATIONAL CHECKS GOOD. TEST FLIGHT GOOD.
- [SDR C2XA10IA107](https://openairdocs.org/sdr/C2XA10IA107.md): Skin · cracked · Mar 27, 2010 · N14945 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > IAH - FLIGHT 2820, DURING POST FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH100](https://openairdocs.org/sdr/C2XA10SH100.md): Light · inoperative · Mar 21, 2010 · N14945 · Emb EMB145EP · Emergency Lighting
  > SHV - GALLEY EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY EMERGENCY LIGHT IAW EMB 145 AMM 33-50-09. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08IA261](https://openairdocs.org/sdr/C2XA08IA261.md): Unknown · odor · Dec 21, 2008 · N14945 · Emb EMB145EP · Air Distribution System
  > FLIGHT 2195 MOB - IAH. THE CREW REPORTED A BURNING PLASTIC SMELL AT PASSENGER SEAT ROWS 9 THROUGH 11. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE PASSENGER CABIN. ALL CONDITIONS WERE FOUND TO BE NORMAL
- [SDR C2XA08IA142](https://openairdocs.org/sdr/C2XA08IA142.md): Smoke Detector · false activation · Jun 19, 2008 · N14945 · Emb EMB145EP · Smoke Detection
  > BTR - FLIGHT 2010, THE CREW REPORTED A LAV SMOKE DETECTOR INDICATION. THE ACFT DIVERTED TO BETWEEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONALLY CHECKED WITH NO DEFECTS, AND
- [SDR C2XA08CL067](https://openairdocs.org/sdr/C2XA08CL067.md): Bulb · faulty · Jun 8, 2008 · N14945 · Emb EMB145EP · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE AFT OVERHEAD WHITE EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AFT OVERHEAD WHITE EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. (S)
- [SDR C2XA08RI075](https://openairdocs.org/sdr/C2XA08RI075.md): Ballast · defective · May 16, 2008 · N14945 · Emb EMB145EP · Passenger Compartment Lighting
  > FLIGHT 2404 - EWR - FLIGHT CREW REPORTED SIDE LIGHTS AT 2A AND 3A INOPERATIVE WITH BURNING SMELL COMING FROM BALLAST. EWR MX REMOVED AND REPLACED BALLAST IAW WMB 145 AMM 33-21-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN T
- [SDR C2XA08RI074](https://openairdocs.org/sdr/C2XA08RI074.md): Coffeemaker · malfunctioned · May 16, 2008 · N14945 · Emb EMB145EP · Buffet/Galleys
  > FLIGHT 2404 - EWR - FLIGHT CREW REPORTED COFFEEMAKERS EMITTING BURNING SMELL WHEN TURNED ON. EWR MX PERFORMED OPERATIONAL CHECK OF BOTH COFFEEMAKERS IAW EMB 145 VCMM 25-30-39 SUCCESSFULLY AND COULD NOT DUPLICATE BURNING SMELL. NO ABNORMALITIES WERE FOUND. A
- [SDR C2XA08CL024](https://openairdocs.org/sdr/C2XA08CL024.md): Proximity Switch · faulty · Mar 3, 2008 · N14945 · Emb EMB145EP · Landing Gear Position and Warning
  > YQB FLIGHT 3072 - THE CREW REPORTED AFTER TAKEOFF A LOUD CLUNK ALONG WITH VIBRATION FELT IN FLIGHT CONTROLS. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR UPLOCK PROXIMITY SWITCH "A" OPEN. THE PROXIMITY SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA08IA045](https://openairdocs.org/sdr/C2XA08IA045.md): Nozzle · dirty · Feb 2, 2008 · N14945 · Emb EMB145EP · Cabin Cooling System
  > IAH - FLIGHT 2818, THE CREW REPORTED FOG DENSE IN COCKPIT DURING TAKEOFF ROLL, NO BURNING SMELL JUST FOGGED ALL WINDOWS. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE CLEANED WATER SPRAY NOZZLE ON NR 1 PACK IAW EMB145 AMM 21-51-1
- [SDR C2XA08SH014](https://openairdocs.org/sdr/C2XA08SH014.md): Frame · corroded · Feb 2, 2008 · N14945 · Emb EMB145EP · Fuselage Main, Frame
  > SHV - DURING C-CHECK FRAME 65 HAS CORROSION AT STR 17L. MX REPAIRED FR 65 STR 17 IAW EC 5310-01432. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA08SH016](https://openairdocs.org/sdr/C2XA08SH016.md): Shear Tie · corroded · Feb 2, 2008 · N14945 · Emb EMB145EP · Fuselage Internal Mounting Structure
  > SHV - DURING C-CHECK SHEAR CLIP AT FR 65 HAS CORROSION. MX REPAIRED FR 65 SHEAR CLIP IAW EC 5330-01458. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA08SH015](https://openairdocs.org/sdr/C2XA08SH015.md): Beam · corroded · Feb 2, 2008 · N14945 · Emb EMB145EP · Fuselage Main, Structure
  > SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SECTION HAS VARIOUS ARES OF CORROSION. MX REMOVED AND REPLACED LOWER BEAM AT CARGO DOOR CUTOUT FR 65-68 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA07IA202](https://openairdocs.org/sdr/C2XA07IA202.md): Connector · burned · Sep 13, 2007 · N14945 · Emb EMB145EP · Light System Wiring
  > IAH FLT 2302, MX WORKING MEL 33-20-001/C PLASTIC BURNT SMELL IN AIRCRAFT. MAINTENANCE REMOVED AND REPLACED CONNECTOR TO OVERHEAD LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA07IA146](https://openairdocs.org/sdr/C2XA07IA146.md): Nozzle · clogged · Jun 19, 2007 · N14945 · Emb EMB145EP · Cabin Cooling System
  > FLIGHT 2553 - CREW REPORTED A BURNING SMELL IN THE COCKPIT AND CABIN WHEN THE AIR CONDITIONING PACKS WERE SELECTED TO MANUAL. MAINTENANCE CLEANED THE LEFT AIR CONDITIONING PACK SPRAY NOZZLE, OPERATIONALLY CHECKED THE SYSTEM AND CLEARED THE DISCREPANCY.
- [SDR C2XA06IA045](https://openairdocs.org/sdr/C2XA06IA045.md): Windshield · damaged · Mar 22, 2006 · N14945 · Emb EMB145EP · Flight Compartment Windows
  > IAH - FLIGHT 2537, DURING DESCENT INTO IAH, THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, WHERE MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS
- [SDR C2XA05SH131](https://openairdocs.org/sdr/C2XA05SH131.md): Support · cracked · Nov 9, 2005 · N14945 · Emb EMB145EP · Cargo/Baggage Doors
  > SHV - DURING C-CHECK, MAINTENANCE FOUND FS 68 CARGO DOOR ROD SUPPORT BRACKET(AFT SECTION) CRACKED. MAINTENANCE REPAIRED FS 68 (AFT SECTION) OF CARGO DOOR SUPPORT BRACKET IAW EC 5230-01123. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH130](https://openairdocs.org/sdr/C2XA05SH130.md): Bushing · gouged · Nov 8, 2005 · N14945 · Emb EMB145EP · Trailing Edge Flaps
  > SHV - DURING C-CHECK, MAINTENANCE FOUND LT I/B FLAP O/B BUSHING GOUGED (ON FLAP). MAINTENANCE REMOVED AND REPLACED LT I/B FLAP O/B BUSHING (ON FLAP) IAW EMB 145 EC5710-01096. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH129](https://openairdocs.org/sdr/C2XA05SH129.md): Firewall · chafed · Nov 7, 2005 · N14945 · Emb EMB145EP · APU Cowling/Containment
  > SHV-DURING C-CHECK MAINTENANCE FOUND AFT LOWER SIDE OF APU FIREWALL RIVET HEAD WITH DAMAGE. MAINTENANCE REPAIRED APU LOWER FIREWALL SKIN DAMAGE I/A/W EC 5330-01521. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA04IA125](https://openairdocs.org/sdr/C2XA04IA125.md): Control Unit · malfunctioned · Sep 30, 2004 · N14945 · Emb EMB145ER · Stabilizer Control System
  > IAH- FLIGHT 2225, DURING CRUISE, THE CREW REPORTED A/P FAIL & AUTO TRIM FAIL MESSAGES, WITH PITCH TRIM INDICATIONS BEING ERRATIC, WITH BOTH SYSTEMS STILL FUNCTIONING. THE CREW ALSO REPORTED CONTROLLABILITY ISSUES ABOVE 240KTS WITH ROLLING 20 DEGREES TO EITHER
- [SDR C2XA04BT075](https://openairdocs.org/sdr/C2XA04BT075.md): Light · deactivated · Jul 8, 2004 · N14945 · Emb EMB145ER · Emergency Lighting
  > CREW REPORTED, NR 2 EMERGENCY LIGHT STRIP IN CABIN INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS IAW EMB145 AMM 33-50-00, OPS CHECKED EMERGENCY LIGHTS GOOD.
- [SDR C2XA04IA079](https://openairdocs.org/sdr/C2XA04IA079.md): Control Panel · contaminated · Jun 5, 2004 · N14945 · Emb EMB145ER · Emergency Lighting
  > DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MIDDLE EMERGENCY LIGHTS ON THE FLOOR WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTION AT THE FLIGHT ATTENDANTS LIGHTING CONTROL PANEL, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY.
- [SDR C2XA03CL156](https://openairdocs.org/sdr/C2XA03CL156.md): Light · malfunctioned · Aug 30, 2003 · N14945 · Emb EMB145ER · Emergency Lighting
  > CLE FLIGHT NR 2115 THE CREW REPORTED TWO EMERGENCY AISLE LIGHTS OUT OF SERVICE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST OF AISLE PATH EMERGENCY LIGHTS OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA03IA082](https://openairdocs.org/sdr/C2XA03IA082.md): Light · inoperative · Aug 9, 2003 · N14945 · Emb EMB145ER · Emergency Lighting
  > IAH - FLIGHT 2573 - THE FORWARD SECTION OF EMERGENCY PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA03BT079](https://openairdocs.org/sdr/C2XA03BT079.md): Battery · discharged · Aug 9, 2003 · N14945 · Emb EMB145ER · Emergency Lighting
  > EWR---CO2573, CREW REPORTED DURING PREFLIGHT, EMERGENCY LIGHTS WERE INOPERATIVE......MAINTENANCE REMOVED AND REPLACED BATTERY AND REPAIRED BROKEN WIRE. (IAW EMB145 MM NR 33-50-01) OPS.CHECKED SYSTEM GOOD.
- [SDR C2XA03CL129](https://openairdocs.org/sdr/C2XA03CL129.md): Light · malfunctioned · Jul 27, 2003 · N14945 · Emb EMB145ER · Emergency Lighting
  > EWR FLIGHT NR 2568 THE CREW REPORTED THE AISLE PATH LIGHTING WAS INOPERATIVE STARTING FROM ROW 8. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA03CL121](https://openairdocs.org/sdr/C2XA03CL121.md): Wire · loose · Jul 8, 2003 · N14945 · Emb EMB145ER · Light System Wiring
  > THE CREW REPORTED FLOOR EMERGENCY LIGHTS BURNED OUT IN TWO SECTIONS. MAINTENANCE RESECURED LOOSE WIRE ON EMERGENCY LIGHT STRIP.
- [SDR C2XA03SH164](https://openairdocs.org/sdr/C2XA03SH164.md): Squat Switch · failed · May 29, 2003 · N14945 · Emb EMB145ER · Landing Gear Position and Warning
  > DURING TEST FLIGHT 3160 A CAUTION MESSAGE CAME UP ON THE EICAS AND WOULD NOT CLEAR. PILOT USED DOWNLOCK RELEASE BUTTON TO RAISE AND LOWER GEAR. THE AIRCRAFT COMPLETED FLIGHT WITH NO OTHER INCIDENTS. MAINTENANCE ADJUSTED LEFT HAND MAIN LANDING GEAR WOW SWITC
- [SDR C2XA03SH163](https://openairdocs.org/sdr/C2XA03SH163.md): Floorbeam · corroded · May 29, 2003 · N14945 · Emb EMB145ER · Fuselage Main, Floor Beam
  > DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED BEAM IAW EMB 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA03SH165](https://openairdocs.org/sdr/C2XA03SH165.md): Proximity Switch · out of adjust · May 28, 2003 · N14945 · Emb EMB145ER · Landing Gear Position and Warning
  > SHV - DURING TEST FLIGHT 3160, A CAUTION MESSAGE CAME UP ON THE EICAS AND WOULD NOT CLEAR. THE PILOT USED THE DOWNLOCK RELEASE TO CYCLE THE GEAR. THE AIRCRAFT COMPLETED THE TEST FLIGHT AND RETURNED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUST
- [SDR C2XA03SH162](https://openairdocs.org/sdr/C2XA03SH162.md): Floorbeam · corroded · May 28, 2003 · N14945 · Emb EMB145ER · Fuselage Main, Floor Beam
  > SHV DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO HAVE CORROSION AT RAMP SUPPORT ANGLE BETWEEN FRAMES 19 AND 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR ON AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN T
- [SDR C2XA03SH161](https://openairdocs.org/sdr/C2XA03SH161.md): Floorbeam · corroded · May 28, 2003 · N14945 · Emb EMB145ER · Fuselage Main, Floor Beam
  > SHV-DURING C-CHECK THE LEFT HAND FLOORBEAM HAS CORROSION UNDER THE COMPOSITE CROSSBEAM BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA03SH160](https://openairdocs.org/sdr/C2XA03SH160.md): Stop · cracked · May 28, 2003 · N14945 · Emb EMB145ER · Cargo/Baggage Doors
  > DURING C-CHECK THE CARGO DOOR STOP LIP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED STOP IAW EMB 145 SRM 52-30-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA03SH156](https://openairdocs.org/sdr/C2XA03SH156.md): Buttstrap · corroded · May 25, 2003 · N14945 · Emb EMB145ER · Fuselage Main, Structure
  > DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA03SH155](https://openairdocs.org/sdr/C2XA03SH155.md): Angle · cracked · May 25, 2003 · N14945 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE LOWER ATTACH ANGLE FOR THE CARGO RAMP AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA03SH154](https://openairdocs.org/sdr/C2XA03SH154.md): Support · corroded · May 25, 2003 · N14945 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE AFT PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA03SH153](https://openairdocs.org/sdr/C2XA03SH153.md): Support · corroded · May 25, 2003 · N14945 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE FORWARD PASSANGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA03SH152](https://openairdocs.org/sdr/C2XA03SH152.md): Crossbeam · corroded · May 25, 2003 · N14945 · Emb EMB145ER · Fuselage Main, Structure
  > DURING C-CHECK THE LOWER CROSSBEAM ANGLE FROM THE CENTER BEAM TO THE RIGHT HAND BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA03SH151](https://openairdocs.org/sdr/C2XA03SH151.md): Floorbeam · corroded · May 25, 2003 · N14945 · Emb EMB145ER · Fuselage Main, Floor Beam
  > SHV-DURING C-CHECK THE SUPPORT RAMP ON THE CENTER FLOORBEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECT SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N14945-2019-01-16/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 = 'N14945' AND deregistration_id = 'N14945-2019-01-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14945-2019-01-16/reports

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