# Service difficulty reports: N16951, cancelled Sep 10, 2015

A list on [N16951, cancelled Sep 10, 2015](https://openairdocs.org/deregistered/N16951-2015-09-10.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 · 126 reports

- [SDR ASOA20141203357](https://openairdocs.org/sdr/ASOA20141203357.md): Bowl · corroded · Dec 3, 2014 · N16951 · Emb EMB145LR · Lavatories
  > DURING C-CHECK, TOILET BOWL IS CORRODED. MAINTENANCE R & R TOILET BOWL SUPPORT ASSY IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20141203356V](https://openairdocs.org/sdr/ASOA20141203356V.md): Floor Support · corroded · Dec 3, 2014 · N16951 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, RT OMEGA BEAM HAS CORROSION, LOCAL LEVEL 2, FRAME 18. MAINTENANCE PERFORMED REPAIR OF RT OMEGA BEAM IAW EC5320-01991 FRAME 18. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20141203355](https://openairdocs.org/sdr/ASOA20141203355.md): Door Sill · corroded · Dec 3, 2014 · N16951 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK BAGGAGE DOOR LOWER SILL CORRODED, LOCAL LEVEL 2, FROM FRAME 65-68. MAINTENANCE R & R BAGGAGE DOOR LOWER SILL AT FRAME 65-68 IAW SRM 51-40-02 AND CPM 51-40-02. THE ACFT WAS APPROVED FOR RETURN T0 SERVICE.
- [SDR ASOA20141126350](https://openairdocs.org/sdr/ASOA20141126350.md): Skin · dented · Dec 3, 2014 · N16951 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK 4 PROTRUDING DENTS IN SAME BAY AT FRAME 24-25, STRINGER 21R-21L. MAINTENANCE PERFORMED REPAIR OF 4 PROTRUDING DENTS BETWEEN FRAME 24-25 STRINGER 21L-21R IAW SRM 53-22-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20141126349](https://openairdocs.org/sdr/ASOA20141126349.md): Skin · dented · Dec 3, 2014 · N16951 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK 4, PROTRUDING DENTS IN SAME BAY AT FRAME 20-21, STRINGER 19L-20L. MAINTENANCE PERFORMED REPAIR OF 4 PROTRUDING DENTS BETWEEN FRAME 20-21 STRINGER 19L-20L IAW SRM 53-21-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140717056](https://openairdocs.org/sdr/ASOA20140717056.md): Power Supply · faulty · Jul 17, 2014 · N16951 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE FWD OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD.
- [SDR ASOA20130709098](https://openairdocs.org/sdr/ASOA20130709098.md): Light · inoperative · Jul 9, 2013 · N16951 · Emb EMB145LR · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, CREW REPORTED THAT THE LAST TWO ROWS OF AISLE PATH LIGHTING WERE INOPERATIVE. MX RESET THE EMERGENCY LIGHT SYS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130614088](https://openairdocs.org/sdr/ASOA20130614088.md): Acm · failed · Jun 14, 2013 · N16951 · Emb EMB145LR · Cabin Cooling System
  > THE CREW REPORTED SMOKE IN THE CABIN. THE ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. MX OPERATED THE APU AND ENGINES WITH THE FLIGHT CREW, VERIFIED THE SMOKE WAS COMING FROM THE NR 1 PACK, PLACED THE NR 1 PACK ON MEL, AND THE ACFT WAS APPROVED FOR RETU
- [SDR ASOA20130120004](https://openairdocs.org/sdr/ASOA20130120004.md): Lamp · inoperative · Jan 20, 2013 · N16951 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED LAMP. OPS CHECKED GOOD.
- [SDR ASOA20130118032](https://openairdocs.org/sdr/ASOA20130118032.md): Attach Fitting · damaged · Jan 18, 2013 · N16951 · Emb EMB145LR · Vertical Stabilizer, Attach Fittings
  > DURING C-CHECK, FRAME 75 STR 2L-2R IS FRETTING AT BOLTS FOR VERTICAL STAB TO FUSELAGE BRACKET. MX PERFORMED REPAIR AT FRM 75 STR 2L-2R AT VERTICAL STAB TO FUSELAGE BRACKET IAW EC5310-01317. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118031](https://openairdocs.org/sdr/ASOA20130118031.md): Skin · damaged · Jan 18, 2013 · N16951 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK SMOKING RIVETS AT FRM 77, BETWEEN STRS 3R-5R. MX PERFORMED REPAIR OF FUSELAGE SKIN AT FRM 77 BETWEEN STRS 3R-5R IAW EC5330-02673, REV ORIGINAL. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118030](https://openairdocs.org/sdr/ASOA20130118030.md): Skin · cracked · Jan 18, 2013 · N16951 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK RIVET AT FRM 78, STR 5R SHOWS VISUAL INDICATION OF CRACKS. MX REPAIRED FUSELAGE SKIN AT FRM 78, STR 5R IAW EC5330-02673, REV ORIGINAL. THE AVFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118029](https://openairdocs.org/sdr/ASOA20130118029.md): Skin · damaged · Jan 18, 2013 · N16951 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK SMOKING RIVETS AT FRM 78 STR 3R. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRM 78 STR 3R IAW EC5330-02673. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118028](https://openairdocs.org/sdr/ASOA20130118028.md): Door Frame · corroded · Jan 18, 2013 · N16951 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, MAIN DOOR LOWER FRAME HAS CORRODED SCREW HOLES. MX PERFORMED REPAIR ON MAIN DOOR LOWER FRAME SCREW HOLES IAW EC5210-01154, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118027](https://openairdocs.org/sdr/ASOA20130118027.md): Structure · corroded · Jan 18, 2013 · N16951 · Emb EMB145LR · Service Doors
  > DURING C-CHECK CORROSION AROUND LOWER NUTPLATE ON AFT SIDE OF SERVICE DOOR. MX PERFORMED REPAIR AROUND LOWER NUTPLATE ON AFT SIDE OF SERVICE DOOR IAW EC5210-01154, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118026](https://openairdocs.org/sdr/ASOA20130118026.md): Structure · corroded · Jan 18, 2013 · N16951 · Emb EMB145LR · Service Doors
  > DURING C-CHECK CORROSION AROUND LOWER NUTPLATES ON SERVICE DOOR. MX PERFORMED REPAIR AROUND LOWER NUTPLATES ON SERVICE DOOR IAW EC5210-01154. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118025](https://openairdocs.org/sdr/ASOA20130118025.md): Hinge Bracket · worn · Jan 18, 2013 · N16951 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > DURING C-CHECK, RT GROUND SPOILER INBD HINGE OTBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER INBD HINGE BRACKET IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118024](https://openairdocs.org/sdr/ASOA20130118024.md): Bushing · migrated · Jan 18, 2013 · N16951 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > DURING C-CHECK RT WING SPEED BRAKE CENTER HINGE ATTACHMENT INBD LOBE HAS MIGRATED HAT BUSHING. MX R & R CENTER HINGE INBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118023](https://openairdocs.org/sdr/ASOA20130118023.md): Hinge · worn · Jan 18, 2013 · N16951 · Emb EMB145LR · Spoilers
  > DURING C-CHECK, LT GROUND SPOILER CENTER HINGE INBD HAT BUSHING MIGRATED. MX R & R LT WING GROUND SPOILER CENTER HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118022](https://openairdocs.org/sdr/ASOA20130118022.md): Hinge · worn · Jan 18, 2013 · N16951 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > DURING C-CHECK LT WING GROUND SPOILER INBD HINGE ATTACHMENT OTBD LOBE HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER INBD HINGE ATTACHMENT BRACKET IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118021](https://openairdocs.org/sdr/ASOA20130118021.md): Hinge · worn · Jan 18, 2013 · N16951 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > DURING C-CHECK LT WING GROUND SPOILER CENTER HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER CENTER HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118020](https://openairdocs.org/sdr/ASOA20130118020.md): Hinge · worn · Jan 18, 2013 · N16951 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > DURING C-CHECK LT WING GROUND SPOILER OTBD HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT WING GROUND SPOILER OTBD HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118019](https://openairdocs.org/sdr/ASOA20130118019.md): Bushing · migrated · Jan 18, 2013 · N16951 · Emb EMB145LR · Spoilers
  > DURING C-CHECK, LT WING SPEED BRAKE CENTER HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT SPEED BRAKE CENTER HINGE INBD HAT BUSHING IAW EC5750-01415, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118016](https://openairdocs.org/sdr/ASOA20130118016.md): Attach Angle · corroded · Jan 18, 2013 · N16951 · Emb EMB145LR · Horizontal Stabilizer Structure
  > DURING C-CHECK, PANEL 321DR ATTACHMENT FLANGE HAS CORRODED SCREW HOLES. MX PERFORMED REPAIR AT PANEL 321DR ATTACHMENT FLANGE SCREW HOLES IAW EC5510-01297. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118015](https://openairdocs.org/sdr/ASOA20130118015.md): Skin · cracked · Jan 18, 2013 · N16951 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK RIVET AT FRAME 79, STRINGER 3L SHOWS VISUAL INDICATION OF CRACKS. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 79, STRINGER 3L IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118014](https://openairdocs.org/sdr/ASOA20130118014.md): Skin · cracked · Jan 18, 2013 · N16951 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, RIVET AT FRAME 79, STRINGER 3R SHOWS VISUAL INDICATION OF CRACKS. MX PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 79, STRINGER 3R IAW EC 5330-02673. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118013](https://openairdocs.org/sdr/ASOA20130118013.md): Floor Support · corroded · Jan 18, 2013 · N16951 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK RT OMEGA BEAM CORRODED AT FRAME 23. MX R & R RT OMEGA BEAM BETWEEN FR 16-24 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118018](https://openairdocs.org/sdr/ASOA20130118018.md): Stringer · damaged · Jan 17, 2013 · N16951 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK DAMAGE, AT FRM 77, STR5R, MX PERFORMED REPAIR AT FRM 77, STR 5R IAW EMB-145 EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118017](https://openairdocs.org/sdr/ASOA20130118017.md): Hinge · damaged · Jan 17, 2013 · N16951 · Emb EMB145LR · Rudder Structure
  > DURING C-CHECK, RUDDER NR 1 AFT CENTER UPPER HINGE DAMAGE GOUGED. MX R & R RUDDER NR 1 AFT CTR UPPER HINGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120808105H](https://openairdocs.org/sdr/ASOA20120808105H.md): Acm · seized · Aug 8, 2012 · N16951 · Emb EMB145LR · Cabin Cooling System
  > AFTER TAKEOFF, THE CREW REPORTED SMOKE IN THE CABIN AND ELECTED TO RETURN TO DEPARTURE WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION, MX FOUND THE SOURCE OF THE SMOKE TO BE A SEIZED NR 1 AIR CYCLE MACHINE (ACM). MX REPLACED THE ACM, PERFORMED O
- [SDR C2XA11TY159](https://openairdocs.org/sdr/C2XA11TY159.md): Pump · overheated · Oct 19, 2011 · N16951 · Emb EMB145LR · Hydraulic Pump (Electric/Engine), Main
  > HYD SYSTEM 2 OVERHEAT/FAIL IN FLIGHT. REMOVED AND REPLACED ENG NR 2 HYD PUMP AND MANIFOLD IAW EMB145 AMM 29-10-03 & 29-10-07. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11TY050](https://openairdocs.org/sdr/C2XA11TY050.md): Adc · malfunctioned · Apr 28, 2011 · N16951 · Emb EMB145LR · Air Data Computer
  > DIVERTED FOR EICAS AIRSPEED MESSAGE IN AMBER AT CRUISE. TYS R & R ADC NR1, OPS AND LEAK CHECKS GOOD. (CLOSED)
- [SDR C2XA11IA052](https://openairdocs.org/sdr/C2XA11IA052.md): Proximity Sensor · faulty · Mar 11, 2011 · N16951 · Emb EMB145LR · Spoilers
  > DURING FLIGHT THE CREW RECEIVED SPOILER FAIL AND SPOILER OPEN MESSAGES. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REPLACED A SPOILER PROXIMITY SENSOR. OPERATIONAL CHECKS WERE PERFORMED AND THE DISCREPANCY WAS CLEARED.
- [SDR C2XA11IA050](https://openairdocs.org/sdr/C2XA11IA050.md): Actuator · leaking · Mar 9, 2011 · N16951 · Emb EMB145LR · Landing Gear Door Actuator
  > ON APPROACH INTO FAR THE CREW RECEIVED A GEAR AIR/GROUND FAIL MESSAGE. THE CREW ELECTED TO ABORT THE APPROACH AND THE MESSAGE EXTINGUISHED HOWEVER ON THE SECOND GEAR EXTENSION THE MESSAGE APPEARED AGAIN. THE AIRCRAFT LANDED IN FAR WITHOUT INCIDENT. THE AIRC
- [SDR C2XA11SH028](https://openairdocs.org/sdr/C2XA11SH028.md): Skin · cracked · Jan 17, 2011 · N16951 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK - SKIN CRACKS AROUND RIVETS BETWEEN FR 77-79 STR 4L TO 8L. REPAIRED CRACKS IAW EC5330-02342. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH027](https://openairdocs.org/sdr/C2XA11SH027.md): Fitting · damaged · Jan 17, 2011 · N16951 · Emb EMB145LR · Ailerons
  > SHV - DURING C-CHECK - LT AILERON 2ND FROM I/B HINGE I/B HAT BUSHING MIGRATED. REPLACED FITTING IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH026](https://openairdocs.org/sdr/C2XA11SH026.md): Hinge Fitting · damaged · Jan 17, 2011 · N16951 · Emb EMB145LR · Spoilers
  > SHV - DURING C-CHECK - LT GROUND SPOILER O/B HINGE O/B HAT BUSHING MIGRATED. REPLACED HINGE FITTING BRACKET IAW EMB 145 SRM 51-20-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH025](https://openairdocs.org/sdr/C2XA11SH025.md): Bracket · cracked · Jan 16, 2011 · N16951 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK FRAME 10 L BRACKET AT STRINGER 10L AND 9L CRACKED. MAINTENANCE REMOVED AND REPLACED FRAME 10 L BRACKET AT STRINGER 10L-9L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH024](https://openairdocs.org/sdr/C2XA11SH024.md): Frame · cracked · Jan 16, 2011 · N16951 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK FRAME 10 AT STRINGER 10L AND 9L CRACKED. MAINTENANCE REMOVED AND REPLACED FRAME 10 AT STRINGER 10L AND 9L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH023](https://openairdocs.org/sdr/C2XA11SH023.md): Stringer · corroded · Jan 16, 2011 · N16951 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > SHV - DURING C-CHECK STRINGER 21R BETWEEN FRAMES 12 AND 13 IS CORRODED. MAINTENANCE PERFORMED REPAIR OF STRINGER 21R BETWEEN FRAMES 12 AND 13 BY INSTALLING STRINGER REPAIR AT FRAMES 10-12 IAW EMB-145 SRM 53-00-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV
- [SDR C2XA10CL199](https://openairdocs.org/sdr/C2XA10CL199.md): Controller · malfunctioned · Dec 15, 2010 · N16951 · Emb EMB145LR · Windshield/Door Rain/Ice Removal
  > CLE FLT 2629 THE CREW REPORTED A STRONG ELECTRICAL SMELL AND A WINDSHIELD HEAT NR 2 FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10IA327](https://openairdocs.org/sdr/C2XA10IA327.md): Acm · seized · Dec 13, 2010 · N16951 · Emb EMB145LR · Cabin Cooling System
  > IAH - FLIGHT 2380, THE CREW REPORTED NOISE AND A SMOKE SMELL COMING FROM THE NUMBER ONE PACK. MAINTENANCE FOUND THE NR 1 ACM TO BE SEIZED, AND PLACED THE LEFT COOLING PACK ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. LATER ON 12/13/10 THE AIR
- [SDR C2XA10IA122](https://openairdocs.org/sdr/C2XA10IA122.md): Ballast · overheated · Apr 15, 2010 · N16951 · Emb EMB145LR · Lighting System
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL AT ROW 4. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED CEILING LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED OF RETURN TO SERVICE.
- [SDR C2XA09IA225A](https://openairdocs.org/sdr/C2XA09IA225A.md): Valve · leaking · Sep 9, 2009 · N16951 · Emb EMB145LR · Fuel Storage
  > MEM - FLIGHT 2291, THE CREW REPORTED FUEL LEAKING FROM THE LEFT WING ON CLIMB. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT WING FLAPPER VALVE, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS
- [SDR C2XA09RI116](https://openairdocs.org/sdr/C2XA09RI116.md): Light · malfunctioned · Jun 4, 2009 · N16951 · Emb EMB145LR · Emergency Lighting
  > FLIGHT CREW REPORTED THAT EMERGENCY LIGHTS WERE INOPERATIVE. MX PERFORMED SYS RESET SUCCESSFULLY AND ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09RI076](https://openairdocs.org/sdr/C2XA09RI076.md): Unknown · malfunctioned · Apr 27, 2009 · N16951 · Emb EMB145LR · Stabilizer Control System
  > FLIGHT 3134 - EWR - FLIGHT CREW REPORTED NOSE EXCESSIVELY HEAVY ON TAKE OFF AND LANDING AND CREW HAD TO USE FULL NOSE UP TRIM ON LANDING. CREW DECLARED EMERGENCY AND LANDED ACFT UNEVENTFULLY. EWR MX CHECKED CABLE TENSION AND FOUND TO BE WITHIN LIMITS. FLIGHT C
- [SDR C2XA09TY062](https://openairdocs.org/sdr/C2XA09TY062.md): Stop Fitting · defective · Apr 14, 2009 · N16951 · Emb EMB145LR · Passenger/Crew Doors
  > MAIN CABIN DOOR WILL NOT CLOSE. REMOVED AND REPLACED FWD AND AFT DOOR STOP HARDWARE, REPOSITIONED DOOR SEAL AND RIGGED DOOR. REMOVED AND REPLACED FWD AND AFT UPPER DOOR STOPS, CHECKED AND ADJUSTED AS REQUIRED IAW EMB 145 AMM 52-18-00-820-808. AIRCRAFT RELEA
- [SDR C2XA09IA061](https://openairdocs.org/sdr/C2XA09IA061.md): Inverter · inoperative · Feb 22, 2009 · N16951 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING BETWEEN ROWS 6-8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRC
- [SDR C2XA09IA038](https://openairdocs.org/sdr/C2XA09IA038.md): Inverter · inoperative · Feb 9, 2009 · N16951 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING POST-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE SLOW TO CHARGE, AND SOME BLINK ON AND OFF. MX R&R THE NR 3 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09IA039](https://openairdocs.org/sdr/C2XA09IA039.md): Battery Pack · discharged · Feb 8, 2009 · N16951 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 3097, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE LT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MX CHARGED THE NR 3 EMERGENCY LIGHT BATTERIES, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N16951-2015-09-10/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 = 'N16951' AND deregistration_id = 'N16951-2015-09-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16951-2015-09-10/reports

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