# Service difficulty reports: N14974, cancelled Jul 31, 2021

A list on [N14974, cancelled Jul 31, 2021](https://openairdocs.org/deregistered/N14974-2021-07-31.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 · 120 reports

- [SDR ASOA20141012128](https://openairdocs.org/sdr/ASOA20141012128.md): Control Module · overheated · Oct 12, 2014 · N14974 · Emb EMB145LR · Passenger Compartment Lighting
  > THE CREW REPORTED A BURNING ODOR COMING FROM THE CABIN LIGHT MODULE. LANDED WITHOUT INCIDENT AND MAINTENANCE R & R THE CABIN LIGHT CONTROL MODULE, OPS TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201400711219](https://openairdocs.org/sdr/ASOA201400711219.md): Skin · corroded · Jul 11, 2014 · N14974 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE FUSELAGE SKIN AT FRAME 65 AND STRINGERS 21L-21R WAS FOUND TO BE CORRODED UNDER THE RA NR 2 ANTENNA. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-02922. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201400711218V](https://openairdocs.org/sdr/ASOA201400711218V.md): Floor Skin · corroded · Jul 11, 2014 · N14974 · Emb EMB145LR · Fuselage Floor Panel
  > DURING C-CHECK THE GALLEY FLOOR SKIN WAS FOUND TO BE CORRODED FROM FRAMES 17-19 AND STRINGERS 21R-21L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-02921. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201400711217](https://openairdocs.org/sdr/ASOA201400711217.md): Stiffener · cracked · Jul 11, 2014 · N14974 · Emb EMB145LR · Vertical Stabilizer
  > DURING C-CHECK THE VERTICAL STABILIZER RT AFT T/E LOWER SKIN STIFFENER WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5530-01283. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201400710216](https://openairdocs.org/sdr/ASOA201400710216.md): Stringer · corroded · Jul 10, 2014 · N14974 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 19L WAS FOUND TO BE CORRODED BETWEEN FRAMES 60-65. MAINTENANCE R & R THE STRINGER IAW EC5330-02919. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201400710215](https://openairdocs.org/sdr/ASOA201400710215.md): Beam · corroded · Jul 10, 2014 · N14974 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201400710214V](https://openairdocs.org/sdr/ASOA201400710214V.md): Skin · corroded · Jul 10, 2014 · N14974 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, SKIN SPLICE AT FRAMES 71-72 AND STRINGERS 19-20L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140704199](https://openairdocs.org/sdr/ASOA20140704199.md): Fitting · corroded · Jul 4, 2014 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FRAME 75 VERTICAL FITTING IS FRETTING. REPAIRED FRAME 75 FITTING IAW EC5330-02918. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130602044](https://openairdocs.org/sdr/ASOA20130602044.md): Inverter · inoperative · Jun 2, 2013 · N14974 · Emb EMB145LR · Emergency Lighting
  > DURING MX THE GALLEY OVERHEAD AND COCKPIT STEP EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.
- [SDR ASOA20120806069V](https://openairdocs.org/sdr/ASOA20120806069V.md): Bushing · migrated · Aug 6, 2012 · N14974 · Emb EMB145LR · Ailerons
  > DURING C-CHECK, TWO MIGRATED HAT BUSHINGS ON RT AILERON PCA FITTING. MX R & R PCA FITTING IAW EC5750-01177. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120806068V](https://openairdocs.org/sdr/ASOA20120806068V.md): Support · corroded · Aug 6, 2012 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LT UPPER SEAT TRACK SUPPORT FRM 50, LWR ATTACH FASTENERS CORRODED. MX PERFORMED REPAIR IAW SRM 51-40-02 AND EC5320-01522, REV A. WET INSTALLED FASTENERS, EDGE SEALED, ALODINE, PRIMERED AND RESTORED ORIGINAL FINISH IAW CPM 51-21-06. ACFT A
- [SDR ASOA20120806067V](https://openairdocs.org/sdr/ASOA20120806067V.md): Frame · damaged · Aug 6, 2012 · N14974 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, STRUCTURE AT FRM 50, STR 15R HAS 1 MISDRILLED HOLE. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120806066V](https://openairdocs.org/sdr/ASOA20120806066V.md): Frame · damaged · Aug 6, 2012 · N14974 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, STRUCTURE AT FRM 48, STR 15R HAS 2 MISDRILLED HOLES. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120806065V](https://openairdocs.org/sdr/ASOA20120806065V.md): Frame · damaged · Aug 6, 2012 · N14974 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 48 HAS 2 MISDRILLED HOLES AT STR 15R. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120806064V](https://openairdocs.org/sdr/ASOA20120806064V.md): Beam · corroded · Aug 6, 2012 · N14974 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT BEAM HAS CORROSION. MX R & R BAGGAGE DOOR LOWER CUTOUT BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2011CL008](https://openairdocs.org/sdr/ASOA2011CL008.md): Wire · loose · Nov 30, 2011 · N14974 · Emb EMB145 · Light System Wiring
  > THE CREW REPORTED THE AFT CABIN EMERGENCY LIGHT STAYS ILLUMINATED WHEN ACFT POWER WAS TURNED OFF. MX INSPECTED AND RESECURED WIRE W776-8515-20 ON CONNECTOR P8104. OPS CHECKS WERE GOOD.
- [SDR C2XA11IA126](https://openairdocs.org/sdr/C2XA11IA126.md): Unknown · odor · Jun 21, 2011 · N14974 · Emb EMB145LR · Air Distribution System
  > BHM - FLIGHT 2824 THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE, AND SMELLED ELECTRICAL TYPE SMOKE. THE AIRCRAFT LANDED AT BHM WITHOUT INCIDENT WHERE CONTRACT MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION WITH NO DEFECTS NOTED, FOUND NO EVIDENCE OF SMOK
- [SDR C2XA11IA113](https://openairdocs.org/sdr/C2XA11IA113.md): Fan · inoperative · Jun 12, 2011 · N14974 · Emb EMB145LR · Air Distribution Fan
  > AFTER TAKE OFF FROM DFW CREW REPORTED SMOKE IN COCKPIT. FLIGHT AIR RETURNED BACK TO DFW. LANDING WAS UNEVENTFUL. MAINTENANCE COMPLIED WITH FIM 21-20-00-810-801-A AND DETERMINED SMOKE IN COCKPIT WAS DUE TO PACK NR 1 FAILURE. AIRCRAFT RELEASED IAW MEL 21-51-
- [SDR C2XA11TY088](https://openairdocs.org/sdr/C2XA11TY088.md): Control Valve · dragging · Jun 12, 2011 · N14974 · Emb EMB145LR · Landing Gear Brake System
  > TYS - A/C WAS TAXIING FROM IAH GATE WHEN CREW FELT THE BRAKES DRAGGING. UPON FURTHER INSPECTION FOUND THE RT INBOARD BRAKE DRAGGING. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE AND OPS CHECK GOOD LP(2818684). ACFT WAS RELEASED TO SERVICE.
- [SDR C2XA11TY037](https://openairdocs.org/sdr/C2XA11TY037.md): Structure · damaged · Mar 25, 2011 · N14974 · Emb EMB145LR · Wing Miscellaneous Structure
  > TYS - A/C WAS EN ROUTE TO BNA FROM EWR WHEN LIGHTNING STRUCK THE A/C. THE A/C LANDING AT BNA WITHOUT ANY INCIDENT. MAINTENANCE COMPLIED WITH TASKCARD 6232012, WHICH IS THE LIGHTNING STRIKE TASKCARD. THE A/C WAS THEN FERRIED TO TYS WHERE MAINTENANCE REMOVED A
- [SDR C2XA10SH311](https://openairdocs.org/sdr/C2XA10SH311.md): Skin · dented · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK SKIN DENTED BETWEEN FRAMES 65-66 STRINGER 4R-5R ON EXTERNAL FUSELAGE. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 65-66 STRINGER 4R-5R IAW ETD 2010-145/07996. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH310](https://openairdocs.org/sdr/C2XA10SH310.md): Floor Support · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT RADIUS AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM BETWEEN FRAMES 18-23 IAW EMB-145 SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH309](https://openairdocs.org/sdr/C2XA10SH309.md): Crossbeam · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 29 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM CARBON CROSSBEAM ATTACHMENT AREA AT FRAME 29 IAW EMB-145 SRM 53-00-00. THE AIRCRAFT WAS APPROVED FOR RET
- [SDR C2XA10SH308](https://openairdocs.org/sdr/C2XA10SH308.md): Crossbeam · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 33 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CARBON CROSSBEAM AT FRAME 33 IAW EMB-145 SRM 51-40-02, SRM 53-00-10 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED
- [SDR C2XA10SH307](https://openairdocs.org/sdr/C2XA10SH307.md): Floorbeam · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Main, Floor Beam
  > SHV - DURING C-CHECK LT OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 54 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CARBON CROSSBEAM AT FRAME 54 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH306](https://openairdocs.org/sdr/C2XA10SH306.md): Floor Support · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR TO CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV
- [SDR C2XA10SH305](https://openairdocs.org/sdr/C2XA10SH305.md): Floor Support · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 33 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM CARBON CROSSBEAM ATTACHMENT AREA AT FRAME 33 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RET
- [SDR C2XA10SH304](https://openairdocs.org/sdr/C2XA10SH304.md): Floor Support · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CARBON CROSSBEAM AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH303](https://openairdocs.org/sdr/C2XA10SH303.md): Floor Support · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAMES 59-61. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 59-61 IAW EC5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH302](https://openairdocs.org/sdr/C2XA10SH302.md): Door Frame · corroded · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK BAGGAGE DOOR LOWER CUTOUT FRAMES 65 TO 68 INTERIOR AND EXTERIOR HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED THE CARGO LOWER BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH301](https://openairdocs.org/sdr/C2XA10SH301.md): Stringer · damaged · Sep 15, 2010 · N14974 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > SHV - DURING C-CHECK STRINGER 5R DAMAGED FRAMES 65-66. MAINTENANCE PERFORMED REPAIR OF STRINGER 5R AT FRAME 65 IAW ETD 2010-145/07996. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH300](https://openairdocs.org/sdr/C2XA10SH300.md): Support Fitting · cracked · Sep 15, 2010 · N14974 · Emb EMB145LR · Nacelle/Pylon Miscellaneous Structure
  > SHV - DURING C-CHECK ANGLE SUPPORT CLIP CRACKED IN PYLON AT FRAME 73 STRINGER 8R. MAINTENANCE REMOVED AND INSTALLED NEW FABRICATED ANGLE SUPPORT CLIP IN PYLON AT FRAME 72-74 STRINGER 8R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC
- [SDR C2XA10SH299](https://openairdocs.org/sdr/C2XA10SH299.md): Support Fitting · cracked · Sep 15, 2010 · N14974 · Emb EMB145LR · Nacelle/Pylon Miscellaneous Structure
  > SHV - DURING C-CHECK ANGLE SUPPORT CLIP CRACKED IN PYLON FRAME 73 STRINGER 8L. MAINTENANCE REMOVED AND FABRICATED NEW ANGLE SUPPORT CLIP IN PYLON AT FRAME 72-73 STRINGER 8L. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH293](https://openairdocs.org/sdr/C2XA10SH293.md): Hinge Bracket · gouged · Sep 15, 2010 · N14974 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > SHV - DURING C-CHECK LT SPEED BRAKE CENTER HINGE I/B ATTACHMENT BRACKET (ON WING) HAS GOUGES INSIDE & AROUND BOLT HOLE. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE CENTER HINGE ATTACHMENT BRACKET IAW EMB-145 AMM 20-10-01 AND CPM 51-21-06. THE AIRCRAFT WA
- [SDR C2XA10SH292](https://openairdocs.org/sdr/C2XA10SH292.md): Fitting · worn · Sep 15, 2010 · N14974 · Emb EMB145LR · Ailerons
  > SHV - DURING C-CHECK RT AILERON PCA O/B ROD FITTING O/B HAT BUSHING ON AILERON MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON PCA BRACKET FITTING IAW EC5750-01177 REV C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH291](https://openairdocs.org/sdr/C2XA10SH291.md): Hinge Bracket · worn · Sep 15, 2010 · N14974 · Emb EMB145LR · Ailerons
  > SHV - DURING C-CHECK ON RT AILERON 2ND FROM I/B HINGE BRACKET O/B SIDE HAT BUSHING MISSING. MAINTENANCE REMOVED AND REPLACED I/B HINGE BRACKET O/B SIDE FOR RT AILERON IAW EMB-145 SRM 51-40-02 AND CPM 51-21-05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI
- [SDR C2XA10TY096](https://openairdocs.org/sdr/C2XA10TY096.md): Battery · overtemp · Jun 27, 2010 · N14974 · Emb EMB145LR · Battery/Charger System
  > BATTERY NR 2 OVERTEMP UP TO 64C. REMOVED AND REPLACED BATTERY IAW EMB 145AMM 24-36-01, OPS CHECK GOOD.
- [SDR C2XA10IA156](https://openairdocs.org/sdr/C2XA10IA156.md): Inverter · inoperative · May 17, 2010 · N14974 · Emb EMB145LR · Emergency Lighting
  > MCI - DURING POST FLIGHT INSPECTION THE CREW REPORTED THE RIGHT EMERGENCY DOOR EXIT LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR C2XA10CL062](https://openairdocs.org/sdr/C2XA10CL062.md): O-Ring · deteriorated · Apr 2, 2010 · N14974 · Emb EMB145LR · Pneumatic Distribution System
  > CLE FLT 2556 THE CREW REPORTED A BLEED 1 LEAK MESSAGE IN CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED LINE GAMMA JOINT O-RINGS AT LEFT UPPER DUCT IN CARGO BAY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10IA100](https://openairdocs.org/sdr/C2XA10IA100.md): Inverter · inoperative · Mar 21, 2010 · N14974 · Emb EMB145LR · Emergency Lighting
  > EXTERIOR EXIT MARKER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP INVERTER AND OPERATIONAL CHECKED GOOD.
- [SDR C2XA09CL166](https://openairdocs.org/sdr/C2XA09CL166.md): Control Unit · faulty · Dec 21, 2009 · N14974 · Emb EMB145LR · Landing Gear Brake System
  > CLE FLT 2841 THE CREW REPORTED A INBOARD BRAKE INOP MESSAGE WHEN THE GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09IA267](https://openairdocs.org/sdr/C2XA09IA267.md): Light · malfunctioned · Oct 22, 2009 · N14974 · Emb EMB145LR · Flight Compartment Lighting
  > IAH - FLIGHT 2117, THE CREW REPORTED AN ELECTRIC SMELL IN THE COCKPIT ON DESCENT INTO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CENTER PROJECTOR LAMP UNDER THE GLARE SHIELD, OPERATIONALLY TESTED WITH NO DEFECT
- [SDR C2XA09IA206](https://openairdocs.org/sdr/C2XA09IA206.md): Actuator · malfunctioned · Aug 13, 2009 · N14974 · Emb EMB145LR · Drag Control Actuator
  > OMA - FLIGHT 2593, ON DESCENT THE CREW REPORTED THAT THE SPOILER FAILED TO CLOSE SYMMETRICALLY, AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT OMA WITHOUT INCIDENT. MCI MX REMOVED AND REPLACED THE RIGHT SPEED BRAKE ACTUATOR, OPERATIONALLY AND LEAK CHECKED
- [SDR C2XA09IA116](https://openairdocs.org/sdr/C2XA09IA116.md): Magnetic Seal · leaking · May 2, 2009 · N14974 · Emb EMB145LR · Turbine Engine Oil System
  > IAH - FLIGHT 3108, THE CREW REPORTED THAT APPROXIMATELY ONE HOUR INTO FLIGHT THEY STARTED LOSING OIL PRESSURE AND QTY ON THE NUMBER TWO ENGINE. THE CREW SHUT DOWN THE NUMBER TWO ENGINE AS A PRECAUTION, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENA
- [SDR C2XA08CL096](https://openairdocs.org/sdr/C2XA08CL096.md): Battery · inoperative · Aug 8, 2008 · N14974 · Emb EMB145LR · Emergency Equipment
  > CLE FLIGHT 2522, THE CREW REPORTED THE CAPTAIN` S EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE INSPECTED AND REPLACED THE CAPTAIN`S FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. (S)
- [SDR C2XA08SH082](https://openairdocs.org/sdr/C2XA08SH082.md): Floor Support · corroded · Jun 11, 2008 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK IT WAS FOUND THAT THE RT OMEGA BEAM HAT SECTION WAS CORRODED AROUND NUT PLATE HOLES AT FRAME 18. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC532001411. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (
- [SDR C2XA08SH083](https://openairdocs.org/sdr/C2XA08SH083.md): Floor Support · corroded · Jun 11, 2008 · N14974 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK IT WAS FOUND THAT THE LT OMEGA SHAPE WAS CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)
- [SDR C2XA08SH084](https://openairdocs.org/sdr/C2XA08SH084.md): Skin · dented · Jun 11, 2008 · N14974 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK IT WAS FOUND THAT THE LT REAR FUSELAGE SKIN WAS DENTED AT FRAME 65/STRINGER 16L, DIRECTLY BELOW THE FORWARD LOWER CORNER OF THE CARGO DOOR CUTOUT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR
- [SDR C2XA07RI084](https://openairdocs.org/sdr/C2XA07RI084.md): Inverter · inoperative · Sep 24, 2007 · N14974 · Emb EMB145LR · Emergency Lighting
  > EWR - DURING ROUTINE MAINTENANCE, MX FOUND FIRST EMERGENCY LIGHT STRIP INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07RI085](https://openairdocs.org/sdr/C2XA07RI085.md): Inverter · inoperative · Sep 19, 2007 · N14974 · Emb EMB145LR · Emergency Lighting
  > EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT FLOOR STRIPS 6, 7 AND 8 INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N14974-2021-07-31/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 = 'N14974' AND deregistration_id = 'N14974-2021-07-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14974-2021-07-31/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.