# Service difficulty reports: N12122

A list on [N12122](https://openairdocs.org/aircraft/N12122.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 · 59 reports

- [SDR RAIA2019083028001](https://openairdocs.org/sdr/RAIA2019083028001.md): Fuel Cap · unsecure · Aug 28, 2019 · N12122 · Emb EMB145XR · Fuel Storage
  > R/H WING FUEL CAP UNSECURED IN FLIGHT. SECURED FEUL CAP AND INSPECTED FOR DAMAGE. NONE FOUND.
- [SDR RAIA201901130001](https://openairdocs.org/sdr/RAIA201901130001.md): Pump · inoperative · Jan 13, 2019 · N12122 · Emb EMB145XR · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC SYSTEM NR 1 LOW QUANITY FOLLOWED BY HYDRAULIC SYSTEM NR 1 FAILURE. (HYD SYS PRESSURE WAS NOTED AT ZERO WHEN THE FAILURE MESSAGE CAME UP ALONG WITH NR 1 QTY BEING AT ZERO. HYD PUMPS WERE SHUT OFF IAW QRH. LANDING GEAR EXTENSION WAS NORMAL. WHEN THE GE
- [SDR RAIA201812200008](https://openairdocs.org/sdr/RAIA201812200008.md): Proximity Switch · malfunctioned · Dec 20, 2018 · N12122 · Emb EMB145XR · Landing Gear Position and Warning
  > LANDING GEAR AIR GROUND FAIL EICAS MESSAGE. R&R BOTH AIR/GROUND PROX SWITCHES. CHECKED CONNECTORS AND HARNESSES FOR ALL LANDING GEAR. NO DEFECTS NOTED.
- [SDR RAIA2018101980001](https://openairdocs.org/sdr/RAIA2018101980001.md): Unknown · malfunctioned · Oct 18, 2018 · N12122 · Emb EMB145XR · Pneumatic Indicating System
  > HIGH STAGE VALVE 1 FAIL ON TAKE OFF ROLL. SWAPPED HIGH STAGE VALVE FROM E1 TO E2 AND E2 TO E1. OPS CHECK GOOD ON BOTH HIGH STAGE VALVES.
- [SDR RAIA201810090001](https://openairdocs.org/sdr/RAIA201810090001.md): Valve · malfunctioned · Oct 9, 2018 · N12122 · Emb EMB145XR · Pneumatic Distribution System
  > BLEED 2 OVERTEMP. R2 FAN AIR VALVE. OPS CHECK GOOD.
- [SDR RAIA2018082530001](https://openairdocs.org/sdr/RAIA2018082530001.md): Rmu · burned out · Aug 23, 2018 · N12122 · Emb EMB145XR · Communications System
  > RMU 1 WENT BLANK WITH BURING SMELL IN COCKPIT. R & R THE NR 1 RMU. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR RAIA201807250001](https://openairdocs.org/sdr/RAIA201807250001.md): Control Unit · malfunctioned · Jul 25, 2018 · N12122 · Emb EMB145XR · Stabilizer Control System
  > MAIN PITCH TRIM INOP IN FLIGHT. REMOVED/REPLACED HORIZONTAL STAB CONTROLLER UNIT IAW AMM 27-40-01. OPS TEST GOOD AT THIS TIME.
- [SDR RAIA2018053130001](https://openairdocs.org/sdr/RAIA2018053130001.md): Panel · detached · May 23, 2018 · N12122 · Emb EMB145XR · Wing, Plate/Skin
  > TWO WING PANELS FELL OFF IN FLT ON LT AND RT WINGS. REPLACED THE INSPECTION PANELS.
- [SDR RAIA201803130001](https://openairdocs.org/sdr/RAIA201803130001.md): Light · inoperative · Mar 13, 2018 · N12122 · Emb EMB145XR · Emergency Lighting
  > PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE LIGHT ASSEMBLY. OPS CHECKED GOOD.
- [SDR RAIA201801100001](https://openairdocs.org/sdr/RAIA201801100001.md): Line · disconnected · Jan 10, 2018 · N12122 · Emb EMB145XR · Cabin Cooling System
  > NR 2 PACK FAILED WITH NO WARNING IN FLT. INSPECTED THE NR 2 PACK AND FOUND THE SENSE LINE DISCONNECTED. CONNECTED THE SENSE LINE, OPS CHECKED GOOD.
- [SDR RAIA201708310002](https://openairdocs.org/sdr/RAIA201708310002.md): Bulb · inoperative · Aug 31, 2017 · N12122 · Emb EMB145XR · Emergency Lighting
  > LEFT AFT EMERGENCY EXIT DOOR LIGHT NR 23 INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.
- [SDR RAIA201701100001](https://openairdocs.org/sdr/RAIA201701100001.md): Bulb · inoperative · Jan 10, 2017 · N12122 · Emb EMB145XR · Emergency Lighting
  > PAX DOOR SWING ARM EMERGENCY LIGHT IS INOPERATIVE AND LENS IS CRACKED. REMOVED AND REPLACED THE BULB AND LENS OPS CHECKED GOOD.
- [SDR RAIA201608170001](https://openairdocs.org/sdr/RAIA201608170001.md): Valve · inoperative · Aug 17, 2016 · N12122 · Emb EMB145XR · Cabin Cooling System
  > THE NR 1 PACK VALVE CLOSED MESSAGE ON EICAS WITH CB F7 TRIPPED. R & R THE NR 1 PACK VALVE OPS CHECK GOOD.
- [SDR RAIA201607240001](https://openairdocs.org/sdr/RAIA201607240001.md): Cradle · inoperative · Jul 24, 2016 · N12122 · Emb EMB145XR · Emergency Equipment
  > AFT FA FLASHLIGHT HOLDER NOT CHARGING THE FLASHLIGHT.
- [SDR RAIA201605020001](https://openairdocs.org/sdr/RAIA201605020001.md): Strut · underserviced · May 2, 2016 · N12122 · Emb EMB145XR · Nose/Tail Landing Gear Strut/Axle
  > LANDING GEAR WOULD NOT RETRACT. LANDING GEAR AIR, GROUND FAIL MSG ON EICAS. DURING INSPECTION, TROUBLESHOOTING FOUND NLG LEG NOT CENTERING. PERFORMED SERVICING OF NLG SHOCK ABSORBER PERFORMED EXTENSION AND RETRATION OF ACFT LANDING GEAR. NO DEFECTS NOTED.
- [SDR RAIA201602220002](https://openairdocs.org/sdr/RAIA201602220002.md): Bulb · inoperative · Feb 22, 2016 · N12122 · Emb EMB145XR · Emergency Lighting
  > PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD.
- [SDR RAIA201601210001](https://openairdocs.org/sdr/RAIA201601210001.md): Bulb · inoperative · Jan 21, 2016 · N12122 · Emb EMB145XR · Emergency Lighting
  > PASSENGER DOOR EMERGENCY LIGHT NR 1 INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR ASOA20150706024](https://openairdocs.org/sdr/ASOA20150706024.md): Inverter · inoperative · Jul 5, 2015 · N12122 · Emb EMB145XR · Emergency Lighting
  > NR 1 & NR 3 INVERTER FOR EMERGENCY LIGHTS INOPERATIVE. R & R NR 1 & NR 3 INVERTER. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20150521118](https://openairdocs.org/sdr/ASOA20150521118.md): Door Sill · corroded · May 21, 2015 · N12122 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140909106](https://openairdocs.org/sdr/ASOA20140909106.md): Fadec · unknown · Sep 5, 2014 · N12122 · Emb EMB145XR · Fuel Controlling System
  > NR 1 ENGINE HAD UNCOMMANDED THRUST REDUCTION DURING FLIGHT. R & R NR 1 FADEC. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20140513071](https://openairdocs.org/sdr/ASOA20140513071.md): Engine · smoke · May 13, 2014 · N12122 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > THE CREW REPORTED THAT THE CABIN AND FLT DECK FILLED WITH SMOKE DURING CLIMB. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130924171](https://openairdocs.org/sdr/ASOA20130924171.md): Acm · seized · Sep 24, 2013 · N12122 · Emb EMB145XR · Cabin Cooling System
  > CREW REPORTED SMOKE IN THE COCKPIT AND FWD CABIN IN FLIGHT, SMOKE SMELLED ELECTRICAL AND DISSIPATED AFTER A COUPLE OF MINUTES. NO ABNORMAL INDICATIONS IN FLIGHT. PACK 1 OVERHEAT MESSAGE APPEARED MOMENTARILY AFTER LANDING. LANDED WITHOUT INCIDENT, MX INSPECT
- [SDR ASOA20130222264](https://openairdocs.org/sdr/ASOA20130222264.md): Light · inoperative · Feb 22, 2013 · N12122 · Emb EMB145XR · Emergency Lighting
  > LEFT OVERWING EXIT LIGHT INOPERATIVE. R & R LT OVERWING EMERGENCY EXIT LIGHT.
- [SDR ASOA20130209260](https://openairdocs.org/sdr/ASOA20130209260.md): Doubler · corroded · Feb 9, 2013 · N12122 · Emb EMB145XR · Nacelle/Pylon, Main Frame
  > ACFT IS FOR A ESCALATION WORK WHEN THE FUSELAGE WAS FOUND CHAFED FROM CONTACT FROM A LANYARD INSIDE RT PYLON. MX INSTALL A DOUBLER OVER BLENDED AREA THAT WAS CHAFED FROM STRINGER 67 TO 68 IAW EC 5330-02698. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END O
- [SDR ASOA20120117002](https://openairdocs.org/sdr/ASOA20120117002.md): Power Supply · inoperative · Jan 17, 2012 · N12122 · Emb EMB145XR · Emergency Lighting
  > DURING SCHEDULED MX INSPECTION, IT WAS FOUND THAT THE AFT LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04 WITH OPS CHECK SUCCESSFUL. THE ACFT WAS APPROVED FOR RETURN TO SERVI
- [SDR C2XA11TY081](https://openairdocs.org/sdr/C2XA11TY081.md): Charger · inoperative · Jun 9, 2011 · N12122 · Emb EMB145XR · Emergency Lighting
  > RT EMERGENCY LIGHT ON PANEL 191 INOP. REMOVED AND REPLACED POWER SUPPLY CHARGER NR 2 IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11CL100](https://openairdocs.org/sdr/C2XA11CL100.md): Switch · faulty · Apr 21, 2011 · N12122 · Emb EMB145XR · Rudder Control System
  > THE CREW REPORTED A RUDDER 1 & 2 INOP MESSAGE IN CLIMB AT FL340. SWITCHING SYS 2 OFF CAUSED SYS 1 TO WORK NORMALLY. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX REPLACED THE RUDDER 2 PRESSURE SWITCH AND OPS CHECKS WERE GOOD.
- [SDR C2XA11RI021](https://openairdocs.org/sdr/C2XA11RI021.md): Acm · defective · Feb 13, 2011 · N12122 · Emb EMB145XR · Cabin Cooling System
  > FLIGHT 2746 - EWR - FLIGHT CREW REPORTED AUTO PRESS ERRACTIC AND FAIL. EWR MX REMOVED AND REPLACED NR 1 ACM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10R1155](https://openairdocs.org/sdr/C2XA10R1155.md): Adc · failed · Dec 18, 2010 · N12122 · Emb EMB145XR · Air Data Computer
  > FLIGHT 2746 EWR-YQB FLIGHT CREW REPORTED NR 1 AIR DATA COMPUTER FAILED WITH A RED X OVER NR 1 TAPE. CREW PERFORMED AIR RETURN TO EWR AND LANDED ACFT UNEVENFULLY. EWR MX REMOVED AND REPLACED NR 1 ADC AND PERFORMED OPERATIONAL CHECK SUCESSFULLY WITH THE ACFT B
- [SDR C2XA10CL132](https://openairdocs.org/sdr/C2XA10CL132.md): Smoke Detector · malfunctioned · Aug 13, 2010 · N12122 · Emb EMB145XR · Smoke Detection
  > THE CREW REPORTED A BAG SMOKE INOP MESSAGE ON THE EICAS. MAINTENANCE INSPECTED AND REPLACED THE BAG SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10IA227](https://openairdocs.org/sdr/C2XA10IA227.md): Smoke Detector · malfunctioned · Aug 12, 2010 · N12122 · Emb EMB145XR · Smoke Detection
  > IAH - FLIGHT 2274, DURING PREFLIGHT INSPECTION A BAGGAGE SMOKE INDICATION ON EICAS WAS REPORTED. THE BOTTLES WERE BLOWN AS PRECAUTION. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED BOTH FIRE BOTTLES, AND BOTH SMOKE DETECTORS IN THE CARGO. OPERATI
- [SDR C2XA10IA226](https://openairdocs.org/sdr/C2XA10IA226.md): Smoke Detector · malfunctioned · Aug 12, 2010 · N12122 · Emb EMB145XR · Smoke Detection
  > IAH - FLIGHT 2274, DURING PREFLIGHT INSPECTION A BAGGAGE SMOKE INDICATION ON EICAS WAS REPORTED. THE BOTTLES WERE BLOWN AS PRECAUTION. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED BOTH FIRE BOTTLES, AND BOTH SMOKE DETECTORS IN THE CARGO. OPERATI
- [SDR C2XA10TY075](https://openairdocs.org/sdr/C2XA10TY075.md): Battery · failed · Apr 29, 2010 · N12122 · Emb EMB145XR · Battery/Charger System
  > BACK-UP BATTERY FAILED FUNCTION CHECK. REMOVED AND REPLACED BACK-UP BATTERY IAW EMB 145 AMM 24-35-01. OPS CHECK GOOD.
- [SDR C2XA10IA057](https://openairdocs.org/sdr/C2XA10IA057.md): Pressure System · malfunctioned · Feb 7, 2010 · N12122 · Emb EMB145XR · Cabin Pressure Control System
  > FLIGHT 2010 - CLIMBING THROUGH FL320 PRESSURIZATION ^P WAS 8 AND CABIN ALTITUDE WAS 8000. THE AIRCRAFT DESCENDED TO FL240 AT WHICH TIME THE ^P WAS 6.6 AND CABIN ALTITUDE WAS 4800. THROUGHOUT DESCENT THE CABIN ALTITUDE WAS REPORTED TO BE MUCH HIGHER THAN NORM
- [SDR C2XA10RI007](https://openairdocs.org/sdr/C2XA10RI007.md): Unknown · odor · Jan 6, 2010 · N12122 · Emb EMB145XR · Air Distribution System
  > FLIGHT 2279 - EWR - FLIGHT CREW REPORTED ON THE GROUND IN EWR, DURING APU START, SMELL OF FUEL COMING OUT OF THE PACKS. EWR MX PERFORMED OPERATIONAL CHECK OF APU AND COULD NOT DUPLICATE THE SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09229](https://openairdocs.org/sdr/C2XA09229.md): Engine · smoke · Dec 27, 2009 · N12122 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > FLIGHT 3060 - EWR - FLIGHT CREW REPORTED NR 1 ENGINE EMITTING AN UNUSUAL AMOUNT OF SMOKE AFTER BEING SHUTDOWN. EWR MX RAN ENGINE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. NO SMOKE NOTICED AFTER SHUTDOWN.
- [SDR C2XA09SH371](https://openairdocs.org/sdr/C2XA09SH371.md): Support Bracket · corroded · Oct 21, 2009 · N12122 · Emb EMB145XR · Aileron Control System
  > SHV - DURING C-CHECK FWD AILERON QUADRANT TORQUE TUBE SUPPORT BRACKET HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 12A-13 AND BETWEEN STRINGERS 21R-20R. MAINTENANCE REMOVED AND REPLACED FWD AILERON QUADRANT TORQUE TUBE SUPPORT BRACKET AT FRAME 12A-13 BETWEEN STRING
- [SDR C2XA09SH370](https://openairdocs.org/sdr/C2XA09SH370.md): Skin · dented · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK DENT BETWEEN FRAMES 25 AND 26 BETWEEN STRINGER 14R AND 15R. MAINTENANCE PERFORMED REPAIR OF DENT BETWEEN FRAMES 25 AND 26 BETWEEN STRINGERS 14R AND 15R IAW EMB-145XR SRM 53-22-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH369](https://openairdocs.org/sdr/C2XA09SH369.md): Rivet · missing · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Main, Longeron/Stringer
  > SHV - DURING C-CHECK MISSING 7 RIVETS IN STRINGER 21L AT FRAME 15 (WHERE SHORING SUPPORT WAS PLACED). MAINTENANCE INSTALLED 7 RIVETS IN STRINGER 21L AT FRAME 15 (WHERE SHORING SUPPORT WAS PLACED) IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN
- [SDR C2XA09SH368](https://openairdocs.org/sdr/C2XA09SH368.md): Support Bracket · corroded · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SUPPORT BRACKET BETWEEN FRAMES 12-13, BETWEEN STRINGERS 21L-20L HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET BETWEEN FRAMES 12-13 AND STRINGERS 21L-20L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVE
- [SDR C2XA09SH367](https://openairdocs.org/sdr/C2XA09SH367.md): Support Bracket · corroded · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SUPPORT BRACKET BETWEEN FRAME 12-13, BETWEEN STRINGER 21R-20R HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET AT FRAMES 12-13 BETWEEN STRINGERS 21R AND 20R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROV
- [SDR C2XA09SH366](https://openairdocs.org/sdr/C2XA09SH366.md): Fitting · corroded · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SHEAR CLIP AT FRAME 11 BETWEEN STRINGERS 21L AND 21R HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF SHEAR CLIP AT FRAME 11 BETWEEN STRINGERS 21L AND 21R IAW EMB-145XR SRM 51-10-03 AND CPM 51-21-07. THE AIRCRAFT WAS APPROV
- [SDR C2XA09SH365](https://openairdocs.org/sdr/C2XA09SH365.md): Skin · corroded · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK FUSELAGE SKIN INTERNAL PITTING CORROSION (LEVEL 2 LOCAL) AT FRAME 12 STRINGER 21R. MAINTENANCE PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 12 STRINGER 21R IAW EC5330-01996. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH364](https://openairdocs.org/sdr/C2XA09SH364.md): Support Bracket · corroded · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SUPPORT BRACKET BETWEEN FRAME 12-13, BETWEEN STRINGERS 21R-20R HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET AT FRAME 12-13 BETWEEN STRINGER 21R-20R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FO
- [SDR C2XA09SH362](https://openairdocs.org/sdr/C2XA09SH362.md): Floor Support · corroded · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) ON I/B SIDE FRAME 19-23. MAINTENANCE NEW REPAIR ON LT OMEGA BEAM AT FRAME 20 I/B SIDE IAW EMB-145 SRM 51-40-02. PREPPED, PRIMED AND PAINTED LT OMEGA BEAM I/B FRAME 19-23 IAW EMB-145 CPM 51-21-0
- [SDR C2XA09SH361](https://openairdocs.org/sdr/C2XA09SH361.md): Doubler · corroded · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK RT OMEGA BEAM DOUBLER AT FRAME 22 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED RT OMEGA BEAM DOUBLER AT FRAME 22 IAW EMB-145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH360](https://openairdocs.org/sdr/C2XA09SH360.md): Skin · cracked · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK RIVETS AT FRAME 79 STRINGER 4L TO 6L SHOW VISIBLE EVIDENCE OF CRACKS. MAINTENANCE PERFORMED CORRECTIVE ACTION REPAIR OF CRACKS ON FUSELAGE SKIN AROUND RIVET HEADS AT FRAME79 STRINGER 4L TO 6L IAW EC5330-01990, REV ORIG. REPAIR BUSHING IN
- [SDR C2XA09SH359](https://openairdocs.org/sdr/C2XA09SH359.md): Skin · cracked · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK RIVETS AT FRAME 78 STRINGER 4L TO 6L SHOW VISIBLE EVIDENCE OF CRACKS. MAINTENANCE PERFORMED CORRECTIVE ACTION REPAIR FOR CRACKS ON FUSELAGE SKIN AROUND RIVETS AT FRAME 78 STRINGER 4L TO 6L IAW EC5330-01990, REV ORIG. REPAIR BUSHINGS INST
- [SDR C2XA09SH358](https://openairdocs.org/sdr/C2XA09SH358.md): Skin · cracked · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK RIVETS AT FRAME 79 STRINGER 4R SHOWS VISIBLE EVIDENCE OF CRACKS. MAINTENANCE PERFORMED CORRECTIVE ACTION REPAIR FOR CRACKS ON FUSELAGE SKIN AROUND RIVET HEADS AT FRAME 79 STRINGER 4R IAW EC5330-01990, REV ORIG REPAIR BUSHINGS INSTALLED. A
- [SDR C2XA09SH357](https://openairdocs.org/sdr/C2XA09SH357.md): Skin · cracked · Oct 21, 2009 · N12122 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK RIVETS AT FRAME 78 STRINGER 6R SHOWS VISIBLE EVIDENCE OF CRACKS. MAINTENANCE PERFORMED CORRECTIVE ACTION REPAIR FOR CRACKS ON FUSELAGE SKIN AROUND RIVET HEADS AT FRAME 78 STRINGER 6R IAW EC5330-01990 REV ORIG. REPAIR BUSHINGS INSTALLED.

Next page: https://openairdocs.org/aircraft/N12122/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 = 'N12122' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N12122/reports

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