# Service difficulty reports: N21537, cancelled Aug 16, 2022

A list on [N21537, cancelled Aug 16, 2022](https://openairdocs.org/deregistered/N21537-2022-08-16.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 · 63 reports

- [SDR ASOA201906045074](https://openairdocs.org/sdr/ASOA201906045074.md): Battery Pack · inoperative · May 30, 2019 · N21537 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE #3 EMERGENCY LIGHT BATTERY WAS FOUND DEAD. MX R/R #3 BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201905075068](https://openairdocs.org/sdr/ASOA201905075068.md): Light · inoperative · May 7, 2019 · N21537 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE CEILING EXIT LIGHT AT ROW 23 WAS INOP. REMOVED AND REPLACED AISLE CEILING EXIT LIGHT AT ROW 23 IAW AMM 33-50-08, OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE
- [SDR ASOA201901145013](https://openairdocs.org/sdr/ASOA201901145013.md): Connector · disconnected · Jan 14, 2019 · N21537 · Emb EMB145LR · Light System Wiring
  > DURING MX INSPECTION THE EMERGENCY LIGHTS WERE INOP AT COCKPIT, MAIN ENTRANCE, AND SIGN ABOVE FLIGHT ATTENDANT SEAT. MX FOUND IN MAIN DOOR CEILING PANEL THE ELECTRICAL CONNECTOR DISCONNECTED. RECONNECTED AND PERFORMED OPS CHECK GOOD. A/C WAS APPROVED FOR RETU
- [SDR ASOA201705264028](https://openairdocs.org/sdr/ASOA201705264028.md): Seat Track · corroded · May 26, 2017 · N21537 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK INSPECTION, THE LEFT OUTBOARD SEAT TRACK NR 5 AND RIGHT NR 4 WERE FOUND TO BE CORRODED BEYOND LIMITS. THE AFFECTED SEAT TRACKS WERE REMOVED AND REPLACED.
- [SDR ASOA201705264026](https://openairdocs.org/sdr/ASOA201705264026.md): Floor Support · corroded · May 26, 2017 · N21537 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, THE RT INBD FLOOR SUPPORT BETWEEN FRAMES 59-61 WAS FOUND TO BE CORRODED BEYOND LIMITS. THE DAMAGE WAS REMOVED AND A DOUBLER REPAIR WAS PERFORMED.
- [SDR ASOA201705254032](https://openairdocs.org/sdr/ASOA201705254032.md): Bearing Cap · corroded · May 25, 2017 · N21537 · Emb EMB145LR · Wing, Landing Gear Attach Fittings
  > DURING C-CHECK INSPECTION, THE FORWARD AND AFT MLG LOWER BEARING CAPS WERE FOUND TO BE CORRODED BEYOND LIMITS. THE AFFECTED BEARING CAPS WERE REMOVED AND REPLACED.
- [SDR ASOA201705254031](https://openairdocs.org/sdr/ASOA201705254031.md): Bearing Cap · corroded · May 25, 2017 · N21537 · Emb EMB145LR · Wing, Landing Gear Attach Fittings
  > DURING C-CHECK INSPECTION, THE FORWARD AND AFT MLG LOWER BEARING CAPS WERE FOUND TO BE CORRODED BEYOND LIMITS. THE AFFECTED BEARING CAPS WERE REMOVED AND REPLACED.
- [SDR ASOA201705254027](https://openairdocs.org/sdr/ASOA201705254027.md): Doubler · corroded · May 25, 2017 · N21537 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, THE INTERNAL DOUBLE FOR THE FORWARD RADIO ALTIMETER 2 WAS FOUND TO BE CORRODED. A DOUBLER REPAIR WAS ACCOMPLISHED ON THE AFFECTED AREA.
- [SDR ASOA201705243174](https://openairdocs.org/sdr/ASOA201705243174.md): Crossbeam · cracked · May 24, 2017 · N21537 · Emb EMB145LR · Fuselage Main, Attach Fittings
  > NOSE LANDING GEAR UPLOCK FORWARD CROSSBEAM CRACKED. REPLACED FORWARD CROSSBEAM AS PER SRM 51-40-02.
- [SDR ASOA201705243173](https://openairdocs.org/sdr/ASOA201705243173.md): Angle · cracked · May 24, 2017 · N21537 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE NR 3 OMEGA BEAM ANGLE CRACKED. OMEGA BEAM ANGLE REPLACED.
- [SDR ASOA201705243172](https://openairdocs.org/sdr/ASOA201705243172.md): Angle · cracked · May 24, 2017 · N21537 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE 3 OMEGA BEAM ANGLE CRACKED. OMEGA BEAM ANGLE REPLACED.
- [SDR ASOA201705243171](https://openairdocs.org/sdr/ASOA201705243171.md): Angle · cracked · May 24, 2017 · N21537 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE 3 R/H OMEGA ANGLE CRACKED. OMEGA ANGLE REPLACED.
- [SDR ASOA201705243170](https://openairdocs.org/sdr/ASOA201705243170.md): Angle · cracked · May 24, 2017 · N21537 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE 3 RT OMEGA ANGLE CRACKED. OMEGA ANGLE REPLACED.
- [SDR ASOA201705233169](https://openairdocs.org/sdr/ASOA201705233169.md): Angle · cracked · May 23, 2017 · N21537 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE 3 FRAME 46 LT FLOOR LEVEL FUSELAGE TO REAR SPAR ANGLE CRACKED. ANGLE REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201705233168](https://openairdocs.org/sdr/ASOA201705233168.md): Angle · cracked · May 23, 2017 · N21537 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE 3 FRAME 46 RT FLOOR LEVEL FUSELAGE TO REAR ANGLE CRACKED. ANGLE REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201703275028](https://openairdocs.org/sdr/ASOA201703275028.md): Control Unit · faulty · Mar 27, 2017 · N21537 · Emb EMB145LR · Landing Gear Brake System
  > PILOT REPORTED INBOARD BRAKES DID NOT WORK ON LANDING BOTH TEMP PROBES SHOWING COLD AND COLD TO THE TOUCH. MX REMOVED AND REPLACED BCU WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160326027](https://openairdocs.org/sdr/ASOA20160326027.md): Light · inoperative · Mar 26, 2016 · N21537 · Emb EMB145LR · Emergency Lighting
  > DURING CREW INSPECTION AN EMERGENCY LIGHT WAS FOUND TO BE DIMLY LIT. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151028055](https://openairdocs.org/sdr/ASOA20151028055.md): Light · arced · Oct 28, 2015 · N21537 · Emb EMB145LR · Passenger Compartment Lighting
  > CREW REPORTED AN ACRID BURNING ODOR OBSERVED AROUND ROW 10A. MAINTENANCE R & R PASSENGER CABIN LIGHT ASSY AT SEAT 10A WITH OPS CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151008077](https://openairdocs.org/sdr/ASOA20151008077.md): Connector · loose · Oct 8, 2015 · N21537 · Emb EMB145LR · Light System Wiring
  > DURING MAINTENANCE INSPECTION THE FORWARD EXIT ROW CEILING EMERGENCY EXIT SIGN, LABEL, WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE ACFT AND FOUND A LOOSE CONNECTION TO THE AFFECTED SIGN, LABEL. MAINTENANCE RESET THE CONNECTION, OPERATIONALLY TESTED
- [SDR ASOA20150225057](https://openairdocs.org/sdr/ASOA20150225057.md): Skin · cracked · Feb 25, 2015 · N21537 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK FUSELAGE SKIN AT FRAME 75, STRINGER 1R-2R CRACKS AT RIVET HOLE. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 75, STRINGER 1R-2R IAW EC5330-02978. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150225056V](https://openairdocs.org/sdr/ASOA20150225056V.md): Skin · cracked · Feb 25, 2015 · N21537 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK FUSELAGE SKIN AT FRAME 75 AT STRINGER 1L-2L CRACKED RIVET HOLE SKIN. MAINTENANCE COMPLETED REPAIR ON FUSELAGE SKIN AT FRAME 75 STRINGER 1L-2L IAW EC5330-02978. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150218055](https://openairdocs.org/sdr/ASOA20150218055.md): Support · corroded · Feb 18, 2015 · N21537 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CARGO LOWER BEAM CORRODED BETWEEN FRAMES 65-68. R & R LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130601043](https://openairdocs.org/sdr/ASOA20130601043.md): Inverter · inoperative · Jun 1, 2013 · N21537 · Emb EMB145LR · Emergency Lighting
  > DURING MX THE AFT CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MX REPLACED THE AFT EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.
- [SDR ASOA20130531042](https://openairdocs.org/sdr/ASOA20130531042.md): Socket · burned · May 31, 2013 · N21537 · Emb EMB145LR · Passenger Compartment Lighting
  > CREW REPORTED A BURNED ODOR AT ROW 16A, 17A, 18A. MX INSPECTED AND FOUND BURNED LIGHT SOCKETS.
- [SDR ASOA20121227093C](https://openairdocs.org/sdr/ASOA20121227093C.md): Light · inoperative · Dec 27, 2012 · N21537 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX, THE LAST AFT EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. MX REPLACED THE AISLE PATH LIGHT STRIP AND OPS CHECKED GOOD.
- [SDR ASOA20120930079](https://openairdocs.org/sdr/ASOA20120930079.md): Light · burned · Sep 30, 2012 · N21537 · Emb EMB145 · Passenger Compartment Lighting
  > THE CREW REPORTED SMOKE ODOR IN COCKPIT. MX INSPECTED AND FOUND CABIN SIDE WALL LIGHT ASSY BURNED. THE LIGHT ASSY WAS DISCONNECTED. MX INSPECTED AND REPLACED 6A SIDEWALL LIGHT ASSY. OPS CHECKS WERE GOOD.
- [SDR ASOA20120507035](https://openairdocs.org/sdr/ASOA20120507035.md): Unknown · odor · May 7, 2012 · N21537 · Emb EMB145LR · Air Distribution System
  > CREW REPORTED A STRONG ELECTRICAL ODOR ON CLIMBOUT. FLIGHT CONTINUED. MX RAN ENGINES IAW AMM 71-00-01 AND PERFORMED OPS CHECKS OF THE APU, PACK SYS, AND PNEUMATIC SYS SUCCESSFULLY. COULD NOT DUPLICATE ANY ELECTRICAL BURNING ODOR OR DEFECTS AT THIS TIME. ACF
- [SDR ASOA20120420041](https://openairdocs.org/sdr/ASOA20120420041.md): Wire Harness · odor · Apr 20, 2012 · N21537 · Emb EMB145LR · Light System Wiring
  > CREW REPORTED A CHEMICAL OR ELECTRICAL ODOR IN FRONT OF CABIN NEAR ROW 3 AND 4. MX INSPECTED AND REPLACED THE CABIN CEILING LIGHT ELECTRICAL HARNESS. OPS CHECKED GOOD.
- [SDR C2XA11TY124](https://openairdocs.org/sdr/C2XA11TY124.md): Battery · overtemp · Jul 20, 2011 · N21537 · Emb EMB145LR · Battery/Charger System
  > TYS - A/C DIVERTED INTO BNA (LOGPAGE 2825614) WITH A OVERTEMP NR 2 BATTERY. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY IAE EMB 145 AMM 24-36-001, OPS CHECK GOOD AND WAS RELEASED.
- [SDR C2XA10CL123](https://openairdocs.org/sdr/C2XA10CL123.md): Starter Gen · failed · Aug 3, 2010 · N21537 · Emb EMB145LR · APU Start/Ignition System
  > CLE FLT 2785 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT FOLLOWED BY APU FAIL. MAINTENANCE INSPECTED AND REPLACED THE APU STARTER/GENERATOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10IA202](https://openairdocs.org/sdr/C2XA10IA202.md): O-Ring · blown · Jul 17, 2010 · N21537 · Emb EMB145LR · Pneumatic Distribution System
  > IAH - FLIGHT 2226, THE CREW REPORTED A BLEED ONE LEAK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE O-RINGS ON THE NR 1 BLEED SYSTEM JOINT NUMBER 7, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND TH
- [SDR C2XA10IA189](https://openairdocs.org/sdr/C2XA10IA189.md): Thermostat · faulty · Jul 3, 2010 · N21537 · Emb EMB145LR · Pneumatic Distribution System
  > TUL - DURING CLIMB, AT FL250 IN ICING CONDITIONS THE CREW REPORTED A BLEED NR 2 OVERTEMP WARNING WITH INDICATIONS IN THE UPPER RED RANGE. THE CREW DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO FAN AIR THERM
- [SDR C2XA10IA186](https://openairdocs.org/sdr/C2XA10IA186.md): Clamp · loose · Jul 3, 2010 · N21537 · Emb EMB145LR · Cabin Cooling System
  > TUL - FLIGHT 2752, ON DESCENT INTO TUL THE CREW RECEIVED A PACK 1 FAIL AND PACK 2 INOP MESSAGE. THE CREW PERFORMED AN EMERGENCY DESCENT AND THE AIRCRAFT LANDED AT TUL WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND SECURED A LOOSE CLAMP ON THE LEFT
- [SDR C2XA10CL054](https://openairdocs.org/sdr/C2XA10CL054.md): Probe · inoperative · Apr 4, 2010 · N21537 · Emb EMB145LR · Outside Air Temperature Indicator/Sensor
  > CLE FLIGHT 2659 THE CREW REPORTED A NR 1 TAT HEAT INOP MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 TAT PROBE. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10CL027](https://openairdocs.org/sdr/C2XA10CL027.md): Lead · loose · Feb 14, 2010 · N21537 · Emb EMB145LR · Light System Wiring
  > DURING ROUTINE MAINTENANCE THE AFT OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RE-SECURED THE POSITIVE POWER LEAD ON THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09CL120](https://openairdocs.org/sdr/C2XA09CL120.md): Battery · discharged · Sep 21, 2009 · N21537 · Emb EMB145LR · Emergency Equipment
  > CLE - FLT 2999 - THE CREW REPORTED THE CAPTAINS FLASHLIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BATTERY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09TY081](https://openairdocs.org/sdr/C2XA09TY081.md): Skin · chafed · Apr 28, 2009 · N21537 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > CHAFE ON AIRCRAFT SKIN INSIDE PANEL 414DB FROM LANYARD. FABRICATED AND INSTALLED DOUBLER IAW IC2009-145/03078A.
- [SDR C2XA09TY076](https://openairdocs.org/sdr/C2XA09TY076.md): Skin · dented · Apr 28, 2009 · N21537 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DENT LOCATED BETWEEN FR8 AND FR9 BETWEEN STR 20R AND 21R. REPAIRED DENTED AREA ON FUSELAGE SKIN IAW EMB 135/145 SRM 53-10-01. AIRCRAFT STILL IN C CHECK.
- [SDR C2XA09TY067](https://openairdocs.org/sdr/C2XA09TY067.md): Frame · corroded · Apr 22, 2009 · N21537 · Emb EMB145LR · Fuselage Main, Structure
  > TYS - DURING C-CHECK CORROSION WAS FOUND AROUND THE SERVICE DOOR LOWER FRAME NUT PLATES. THE AREA WAS CUT OUT AND REPAIRED IAW EC 5310-01373. A/C STILL IN C-CHECK.
- [SDR C2XA09TY065](https://openairdocs.org/sdr/C2XA09TY065.md): Yoke · cracked · Apr 21, 2009 · N21537 · Emb EMB145LR · Nacelle/Pylon Miscellaneous Structure
  > TYS - DURING C-CHECK THE NR 1 ENGINE FWD LOWER YOKE WAS FOUND CRACKED AT THE FWD ATTACH POINT. A DYE PEN TEST WAS PERFORMED IAW EMB NDT PTO 1 AND PTO 2 AND THE CRACK WAS CONFIRMED. THE NR 1 ENG FWD LOWER YOKE INNER PIECE WAS REMOVED AND REPLACED IAW EMB 145
- [SDR C2XA08CL038](https://openairdocs.org/sdr/C2XA08CL038.md): Light · inoperative · Mar 24, 2008 · N21537 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA08IA020](https://openairdocs.org/sdr/C2XA08IA020.md): Wheel · worn · Jan 9, 2008 · N21537 · Emb EMB145LR · Wheel/Ski/Float
  > IAH - FLIGHT 2431, THE CREW REPORTED AN EXCESSIVE NW VIBRATION ON T/O. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08IA019](https://openairdocs.org/sdr/C2XA08IA019.md): Wheel · worn · Jan 9, 2008 · N21537 · Emb EMB145LR · Wheel/Ski/Float
  > IAH - FLIGHT 2431, THE CREW REPORTED AN EXCESSIVE NW VIBRATION ON T/O. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA07SH043](https://openairdocs.org/sdr/C2XA07SH043.md): Case · corroded · Aug 4, 2007 · N21537 · Emb EMB145LR · Turbine Engine Compressor Section
  > SHV - DURING C-CHECK MAINTENANCE FOUND NR 1 ENGINE FAN CASE ASSY & ENGINE INLET MOUNTING ATTACHMENT BOLTS HOLES WITH CORROSION. MAINTENANCE REPAIRED NR 1 ENGINE FAN CASE ASSY & ENGINE INLET ATTACHMENT BOLT HOLES IAW EC5420-01097. AIRCRAFT WAS APPROVED TO RET
- [SDR C2XA06CL086](https://openairdocs.org/sdr/C2XA06CL086.md): Inverter · inoperative · Oct 16, 2006 · N21537 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHTS BELOW EMERGENCY EXIT DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06IA159](https://openairdocs.org/sdr/C2XA06IA159.md): Control Unit · malfunctioned · Sep 28, 2006 · N21537 · Emb EMB145LR · Cabin Temperature Control System
  > IAH-2394, ON TAXI OUT OF BNA, THE CREW REPORTED A PACK TWO OVERHEAT ON TAXI OUT. THE SYSTEM WAS RESET SUCCESSFULLY, AND ON TAKEOFF HAD A STRONG ELECTRICAL ODOR LASTING APPROXIMATELY FIVE MINUTES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT.
- [SDR C2XA06CL043](https://openairdocs.org/sdr/C2XA06CL043.md): Proximity Switch · faulty · Apr 15, 2006 · N21537 · Emb EMB145LR · Landing Gear Position and Warning
  > CLE FLIGHT 3233, THE CREW REPORTED A VIBRATION FROM THE NOSE AREA AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS STAYING OPENED. MAINTENANCE REPLACED THE NOSE GEAR DOOR PROXIMITY
- [SDR C2XA06IA030](https://openairdocs.org/sdr/C2XA06IA030.md): Connector · loose · Mar 6, 2006 · N21537 · Emb EMB145LR · Landing Gear System Wiring
  > IAH - ON TAKEOFF FROM SDF THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT WITHOUT PRESSING THE DOWNLOCK RELEASE BUTTON. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT IN
- [SDR C2XA06BT011](https://openairdocs.org/sdr/C2XA06BT011.md): Control Lever · faulty · Mar 2, 2006 · N21537 · Emb EMB145LR · Landing Gear Selector
  > CREW REPORTED AFTER TAKEOFF IN YYZ, -DOWNLOCK RELEASE- BUTTON HAD TO BE PUSHED TO GET THE GEAR HANDLE TO COME UP, NO EICAS MESSAGE NOTED. FLIGHT CONTINUE TO NEWARK THE LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IA
- [SDR C2XA06IA028](https://openairdocs.org/sdr/C2XA06IA028.md): Battery Pack · discharged · Feb 27, 2006 · N21537 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FO

Next page: https://openairdocs.org/deregistered/N21537-2022-08-16/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 = 'N21537' AND deregistration_id = 'N21537-2022-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N21537-2022-08-16/reports

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