# Service difficulty reports: N106US, cancelled May 28, 2009

A list on [N106US, cancelled May 28, 2009](https://openairdocs.org/deregistered/N106US-2009-05-28.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR USAA2009011690084](https://openairdocs.org/sdr/USAA2009011690084.md): Engine · bird ingestion · Jan 15, 2009 · N106US · Airbus A320214 · Engine (Turbine/Turboprop)
  > FLT 1549 LGA-CLT - EMERGENCY DITCHING - DUAL ENGINE FAILURE - CREW REPORTED BIRD INGESTION SHORTLY AFTER TAKEOFF AND REQUESTED TO RETURN TO FIELD. ACFT MADE AN EMERGENCY DITCHING IN THE HUDSON RIVER. DETAILED DISASSEMBLY & EXAMINATION OF ENGINES AT MANUFACTU
- [SDR SA07034](https://openairdocs.org/sdr/SA07034.md): Bottle · reads low · Jun 6, 2007 · N106US · Airbus A320214 · Escape Slide
  > DCA - THE RIGHT HAND OVERWING EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS FOUND LOW DURING INSPECTION. MAINTENANCE ACCOMPLISHED REPLACEMENT OF THE RIGHT HAND OVERWING SLIDE BOTTLE CYLINDER ASSEMBLY. INSPECTED, OK FOR SERVICE.
- [SDR SA07017](https://openairdocs.org/sdr/SA07017.md): Slide · faulty · Feb 28, 2007 · N106US · Airbus A320214 · Escape Slide
  > PHL - THE FRONT ENTRY DOOR WAS OPENED INADVERTENTLY AFTER IT WAS ARMED. THE SLIDE DID NOT DEPLOY. MAINTENANCE REPLACED THE FORWARD, LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.
- [SDR SA07023](https://openairdocs.org/sdr/SA07023.md): Epsu · faulted · Mar 20, 2006 · N106US · Airbus A320214 · Emergency Lighting
  > RIC - THE MID CABIN, RIGHT HAND EMERGENCY POWER SUPPLY UNIT FAILED THE WEEKLY CHECK. MAINTENANCE REPLACED THE MID CABIN, RIGHT HAND EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.
- [SDR SA05088](https://openairdocs.org/sdr/SA05088.md): Lanyard · missing · Jul 21, 2005 · N106US · Airbus A320214 · Escape Slide
  > PIT - THE LEFT FORWARD DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND INCORRECTLY ROUTED. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARD. OK FOR SERVICE.
- [SDR SA05087](https://openairdocs.org/sdr/SA05087.md): Lanyard · missing · Jul 21, 2005 · N106US · Airbus A320214 · Escape Slide
  > PIT - THE AFT RIGHT DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND INCORRECTLY ROUTED. MAINTENANCE CORRECTLY ROUTED THE AFT RIGHT DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD.
- [SDR SA05086](https://openairdocs.org/sdr/SA05086.md): Lanyard · missing · Jul 21, 2005 · N106US · Airbus A320214 · Escape Slide
  > PIT - THE AFT LEFT EMERGENCY EXIT DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND NOT IN VIEW. MAINTENANCE INSTALLED SURVIVAL KIT LANYARD. OK FOR SERVICE.
- [SDR USAA050477](https://openairdocs.org/sdr/USAA050477.md): Floorbeam · corroded · Apr 10, 2005 · N106US · Airbus A320214 · Fuselage Main, Floor Beam
  > PIT - FOUND FLOORBEAM CORRODED 2.5 INCHES DIAMETER AREAS, FLOORBEAM GALLEY MOUNTING HOLES OUTBOARD FLOORBEAM, BETWEEN RT SIDE C68-69. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA050496](https://openairdocs.org/sdr/USAA050496.md): Floorbeam · corroded · Apr 10, 2005 · N106US · Airbus A320214 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM CORRODED 1 SQUARE INCH, AROUND NUT PLATE HOLES, FLOORBEAM C66-C69 LEFT OUTBOARD. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA 260-53500. (M)
- [SDR USAA050479](https://openairdocs.org/sdr/USAA050479.md): Floorbeam · corroded · Apr 10, 2005 · N106US · Airbus A320214 · Fuselage Main, Floor Beam
  > PIT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES BY.060 INCH DEEP AREA, FLOOR SUPPORT AT Y750 ABOVE C68. CORROSION LEVEL 1, TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-72-11. (M)
- [SDR USAA050478](https://openairdocs.org/sdr/USAA050478.md): Floorbeam · corroded · Apr 10, 2005 · N106US · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED.5 INCH DIAMETER AREA, FLOORBEAM AT FRAME 20, 9 INCH RIGHT OF CENTER. REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-11-14. CORROSION LEVEL 1, TASK JA-220-53300. REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-11-14. (M)
- [SDR USAA050522](https://openairdocs.org/sdr/USAA050522.md): Floorbeam · corroded · Apr 5, 2005 · N106US · Airbus A320214 · Fuselage Main, Floor Beam
  > PIT - FOUND FLOORBEAM CORRODED 2 INCH BY 2 INCH AREA, LEFT INBOARD AFT FLOORBEAM Y765 FRAME C64-C70. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14. CORROSION LEVEL 1, TASK JA-260-53500. (M)
- [SDR USAA050465](https://openairdocs.org/sdr/USAA050465.md): Floorbeam · corroded · Apr 5, 2005 · N106US · Airbus A320214 · Fuselage Main, Floor Beam
  > PIT - FOUND FLOORBEAM CORRODED 1 BY.5 BY.030 INCH,.75 INCH BY.5 INCH BY.030 INCH,.75 BY.3750 BY.05, FLOOR BEAM 10 INCHES LEFT OF CENTER LINE BETWEEN C16 AND C22. DEFECTIVE PART REPLACED WITH IDENT PART. (M)
- [SDR SA05016](https://openairdocs.org/sdr/SA05016.md): Proximity Sensor · faulty · Feb 6, 2005 · N106US · Airbus A320214 · Landing Gear Position and Warning
  > EN ROUTE MSY TO CLT - AFTER TAKEOFF, THE LANDING GEAR INDICATES DOWN AFTER THE LANDING GEAR LEVER WAS MOVED UP. UPON ARRIVAL, THE LANDING GEAR HAD AMBER -X- INDICATIONS ON THE WHEEL PAGE. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR EXTENSION PROX SENSOR,
- [SDR USAASA04034](https://openairdocs.org/sdr/USAASA04034.md): Power Supply · inoperative · Apr 3, 2004 · N106US · Airbus A320214 · Emergency Lighting
  > THE LEFT AFT EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)
- [SDR USAASA03036](https://openairdocs.org/sdr/USAASA03036.md): Proximity Switch · inoperative · May 1, 2003 · N106US · Airbus A320214 · Landing Gear Position and Warning
  > AFTER TAKEOFF, CREW RECEIVED ECAM INDICATIONS OF 'GEAR NOT UPLOCKED', 'ENG 2 REVERSER FAULT', AND 'CAPT PITOT'. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A PROXIMITY SWITCH, FIN 23GA. LANDING GEAR SYSTEMS CHECK W
- [SDR USAASA03016](https://openairdocs.org/sdr/USAASA03016.md): Power Supply · malfunctioned · Feb 16, 2003 · N106US · Airbus A320214 · Emergency Lighting
  > DCA - DURING THE EMERGENCY LIGHT SYSTEM TEST, RECEIVED 'EPSU INT LOAD FWD LT FAULT' MESSAGE. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)
- [SDR USAASA03010](https://openairdocs.org/sdr/USAASA03010.md): Girt Bar · lack of lube · Jan 28, 2003 · N106US · Airbus A320214 · Escape Slide
  > LGA - THE L1 DOOR WAS DIFFICULT TO KEEP IN THE ARMED POSITION. MAINTENANCE CLEANED AND LUBRICATED THE GIRT BAR ASSEMBLY AND LOCKING MECHANISM, AND REPLACED THE L-1 DOOR EMERGENCY EVACUATION SLIDE. OK FOR SERVICE. (M)
- [SDR USAADUPE](https://openairdocs.org/sdr/USAADUPE.md): Girt Bar · dirty · Jan 28, 2003 · N106US · Airbus A320214 · Escape Slide
  > LGA - THE L1 DOOR WAS DIFFICULT TO KEEP IN THE ARMED POSITION. MAINTENANCE CLEANED AND LUBRICATED THE GIRT BAR ASSEMBLY AND LOCKING MECHANISM, AND REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE. OK FOR SERVICE. (M)
- [SDR USAASA02105](https://openairdocs.org/sdr/USAASA02105.md): Flap · out of position · Dec 7, 2002 · N106US · Airbus A320214 · Escape Slide
  > THE SLIDE FOR DOOR L1 WOULD NOT REMAIN ARMED. MAINTENANCE REPOSITIONED THE GIRT FLAP ON THE GIRT BAR TO ELIMINATE FRICTION. THE SLIDE ARMING OF THE L1 DOOR NOW OPERATIONALLY CHECKS OK.
- [SDR USAASA02101](https://openairdocs.org/sdr/USAASA02101.md): Battery Pack · discharged · Nov 20, 2002 · N106US · Airbus A320214 · Emergency Lighting
  > BOS - THE LEFT OVERWING BATTERY PACK EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M)
- [SDR USA2002F00057](https://openairdocs.org/sdr/USA2002F00057.md): Slide · intermittent · Jun 21, 2002 · N106US · Airbus A320214 · Escape Slide
  > THE FORWARD CABIN, RIGHT SIDE, EMERGENCY ESCAPE SLIDE WAS DIFFICULT TO ARM AND INTERMITTENTLY INDICATED DISARMED. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. OPERATIONAL CHECKED OK.
- [SDR USAA020157](https://openairdocs.org/sdr/USAA020157.md): Skin · cracked · May 2, 2002 · N106US · Airbus A320214 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED.150 INCH, FRAME 30 STRINGER 8L. INSTALLED DOUBLER AND FILLER PER SRM 53-21-11 AND 53-00-11. (M)
- [SDR USAASA01037](https://openairdocs.org/sdr/USAASA01037.md): Engine · failed · Jul 20, 2001 · N106US · Airbus A320214 · Engine (Turbine/Turboprop)
  > JFK - FLT 6808 - EN ROUTE LGA-BOS, WHILE CLIMBING THROUGH FL080, FELT MULTIPLE COMPRESSION STALLS AND OBSERVED SHOTS OF FLAME FROM THE LEFT SIDE OF THE AIRCRAFT. THE NR 1 ENGINE THROTTLE WAS MOVED TO IDLE, HOWEVER, THE ENGINE INDICATED SHUTDOWN. THE FLIGHT D

## 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 = 'N106US' AND deregistration_id = 'N106US-2009-05-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N106US-2009-05-28/reports

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