# Service difficulty reports: N16510

A list on [N16510](https://openairdocs.org/aircraft/N16510.md).

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

- [SDR C2XA07CL018](https://openairdocs.org/sdr/C2XA07CL018.md): Power Supply · inoperative · Feb 2, 2007 · N16510 · Emb EMB135ER · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EMERGENCY LIGHT AND THE FORWARD AISLE PATH LIGHT STRIP WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06SH104](https://openairdocs.org/sdr/C2XA06SH104.md): Firewall · chafed · Oct 21, 2006 · N16510 · Emb EMB135LR · APU Cowling/Containment
  > SHV - MAJOR - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED. MAINTENANCE CLEANED UP THE DAMAGED AREA AND INSTALLED A SHIM IAW EC5310-01359. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06BT019](https://openairdocs.org/sdr/C2XA06BT019.md): Sensor · odor · May 1, 2006 · N16510 · Emb EMB135LR · Pitot/Static Anti-Ice System
  > CREW REPORTED, PITOT 3 INOPERATIVE CAUTION LIGHT ON EICAS AND STRONG BURNING SMELL ON CABIN AND COCKPIT. FOUND PITOT NR 3 CURRENT SENSOR MELTED. REMOVED AND REPLACED PITOT NR 3 CURRENT SENSOR K0057 IAW EMB135 AMM 30-31-00, OPS CHECKED GOOD. NO BURNING SMELL
- [SDR C2XA06CL047](https://openairdocs.org/sdr/C2XA06CL047.md): Windshield · failed · Apr 21, 2006 · N16510 · Emb EMB135ER · Flight Compartment Windows
  > CLE FLIGHT 2805, THE CREW REPORTED UPON ENTERING ICING CONDITIONS, WINDSHIELD HEAT SELECTED, A STRONG ELECTRICAL SMELL WAS DETECTED. THE AIRCRAFT DIVERTED INTO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPER
- [SDR C2XA04TY051](https://openairdocs.org/sdr/C2XA04TY051.md): Sill · corroded · Mar 13, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CUTOUT LOWER SILL IAW EMB-135 SRM 51-40-02.
- [SDR C2XA04TY049](https://openairdocs.org/sdr/C2XA04TY049.md): Channel · corroded · Mar 12, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 2C INSPECTION A GOUGE WAS FOUND AT FR 15, STR 16L. MAINT REPAIRED CENTER FUSELAGE 1 AT LT FLOOR CROSSBEAM. ALODINED, PRIMED AND PAINTED IAW IC 2004-145/0816 AND CPM 51-21-04;05;06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON
- [SDR C2XA04TY048](https://openairdocs.org/sdr/C2XA04TY048.md): Sill · corroded · Mar 12, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 2C INSPECTION THE SERVICE DOOR FWD SILL WAS FOUND CORRODED. MAINT BLENDED AND MEASURED AREA, FAB AND INSTALL DOUBLER IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
- [SDR C2XA04TY047](https://openairdocs.org/sdr/C2XA04TY047.md): Floorbeam · corroded · Mar 12, 2004 · N16510 · Emb EMB135ER · Fuselage Main, Floor Beam
  > TYS DURING A SCHEDULED 2C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE GALLEY AREA. MAINT REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
- [SDR C2XA04TY041](https://openairdocs.org/sdr/C2XA04TY041.md): Bracket · corroded · Mar 4, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 2C INSPECTION THE PAX DOOR SILL BRACKETS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE FORWARD AND AFT PAX DOOR SILL BRACKETS IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WO
- [SDR C2XA04TY040](https://openairdocs.org/sdr/C2XA04TY040.md): Sill · corroded · Mar 4, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 2C INSPECTION THE LT WALL FLOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE LT FLOOR SILL AFT OF PAX DOOR IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
- [SDR C2XA04BT008](https://openairdocs.org/sdr/C2XA04BT008.md): Battery Pack · discharged · Jan 19, 2004 · N16510 · Emb EMB135LR · Emergency Lighting
  > DURING SERVICE CHECK MAINTENANCE FOUND NR 3 EMERGENCY LIGHT BATTERY WILL NOT CHARGE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB135 33-50-04. OPS CHECKED GOOD.
- [SDR C2XA04BT006](https://openairdocs.org/sdr/C2XA04BT006.md): Battery Pack · faulty · Jan 18, 2004 · N16510 · Emb EMB135LR · Emergency Lighting
  > DURING RON CHECK MAINTENANCE FOUND THE FORWARD RIGHTHAND OVERWING EMERGENCY LIGHT DOES NOT WORK AND FLOOR PROXIMITY LIGHTS ARE NOT WORKING. MAINTENANCE REMOVED AND REPLACED BATTERY PACK NR 1 IAW EMB135 AMM 33-50-04. EMERGENCY LIGHTS OPS. CHECKED GOOD IAW EM
- [SDR C2XA03BT123](https://openairdocs.org/sdr/C2XA03BT123.md): Battery · malfunctioned · Dec 28, 2003 · N16510 · Emb EMB135LR · Emergency Lighting
  > CREW REPORTED, (VARIOUS EMERGENCY LIGHTS IN FORWARD CABIN ARE INOPERATIVE.) MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB135 AMM NR 33-50-04. OPS. CHECKED GOOD.
- [SDR C2XA03CL212](https://openairdocs.org/sdr/C2XA03CL212.md): Battery · discharged · Dec 26, 2003 · N16510 · Emb EMB135ER · Emergency Lighting
  > CLE FLIGHT 2026 THE CREW REPORTED THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA03CL217](https://openairdocs.org/sdr/C2XA03CL217.md): Battery · discharged · Dec 25, 2003 · N16510 · Emb EMB135ER · Emergency Lighting
  > THE CREW REPORTED THE EMERGENCY EXIT LIGHTING WOULD NOT REMAIN ILLUMINATED DURING TESTING. MAINTENANCE RECHARGED THE EMERGENCY EXIT LIGHTING BATTERIES. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA03CL203](https://openairdocs.org/sdr/C2XA03CL203.md): Battery Pack · discharged · Dec 18, 2003 · N16510 · Emb EMB135ER · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE SECOND AND THIRD EMERGENCY AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA03BT111](https://openairdocs.org/sdr/C2XA03BT111.md): Switch · out of position · Nov 22, 2003 · N16510 · Emb EMB135LR · Fuel Storage
  > CREW REPORTED, FUEL NR 1 LOW LEVEL MESSAGE CAME ON INFLIGHT ON ARRIVAL INTO EWR. NR 1 FUEL QTY INDICATOR SHOWS ZERO FUEL. DECLARED EMERGENCY AND LANDED UNEVENTFULLY IN EWR. MAINTENANCE FOUND REFUELING SWITCH TO BE IN THE OPEN POSITION ON THE REFUELING PANEL
- [SDR C2XA02CL191](https://openairdocs.org/sdr/C2XA02CL191.md): Odor · detected · Oct 1, 2002 · N16510 · Emb EMB135LR · Air Distribution System
  > CLE FLIGHT NR 3160 THE CREW REPORTED THE CABIN SMELLS OF FUMES WITH THE APU BLEED ON. MAINTENANCE INSPECTED AND RAN APU WITH BLEED ON AND OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA02CL027](https://openairdocs.org/sdr/C2XA02CL027.md): Engine · failed · Jan 29, 2002 · N16510 · Emb EMB135ER · Engine (Turbine/Turboprop)
  > CLE FLIGHT 3052 THE CREW REPORTED THE NR 2 ENGINE SHUT DOWN IN FLIGHT UNCOMMANDED. THEY REPORTED A LOUD BANG AND HIGH ITT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONAL CHECKS WERE GOOD. THE AIR
- [SDR C2XA02CL012](https://openairdocs.org/sdr/C2XA02CL012.md): Switch · out of adj · Jan 18, 2002 · N16510 · Emb EMB135ER · Door Warning System
  > DURING A 2A INSPECTION MAINTENANCE FOUND THE RIGHT HAND OVERWING EMERGENCY EXIT DID NOT PRODUCE A MESSAGE ON THE EICAS WHEN THE DOOR WAS OPEN. MAINTENANCE ADJUSTED THE MICROSWITCH ON THE RIGHT HAND EMERGENCY EXIT DOOR. OPERATIONAL CHECKS WERE GOOD. THE AIRC
- [SDR C2XA01TY171](https://openairdocs.org/sdr/C2XA01TY171.md): Skin · chafed · Oct 29, 2001 · N16510 · Emb EMB135ER · Cargo/Baggage Doors
  > TYS DURING A SCHEDULED 1C INSPECTION,THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE HANDLE CUTOUT. MAINTENANCE BLENDED OUT THE AREA IAW EC5230-01068--5120-04--5120-05 AND 5120-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE SCHEDULED M
- [SDR C2XA01TY](https://openairdocs.org/sdr/C2XA01TY.md): Skin · chafed · Oct 29, 2001 · N16510 · Emb EMB135ER · Cargo/Baggage Doors
  > TYS DURING A SCHEDULED 1C INSPECTION,THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE HANDLE CUTOUT. MAINTENANCE BLENDED OUT THE AREA IAW EC5230-01068--5120-04--5120-05 AND 5120-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE SCHEDULED M
- [SDR C2XA01TY170](https://openairdocs.org/sdr/C2XA01TY170.md): Firewall · damaged · Oct 29, 2001 · N16510 · Emb EMB135ER · Fuselage Main, Bulkhead
  > TYS DURING A SCHEDULE 1-C INSPECTION,MAINTENANCE FOUND A HOLE RUBBED INTO THE FIREWALL BLANKET. MAINTENANCE USED EC5330-01166 FOR THE REPAIR. ALL WORK WAS DONE IAW THE EC AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL SCHEDULE MAINTENANCE.
- [SDR C2XA01TY169](https://openairdocs.org/sdr/C2XA01TY169.md): Floor Support · broken · Oct 29, 2001 · N16510 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED INSPECTION A FAIRLEAD FLOOR SUPPORT AT THE CENTER OMEGA BEAM WAS FOUND BROKEN AT FR21. MAINTENANCE R/R THE FAIRLEAD FLOOR SUPPORT AND THE WORK WAS FOUND SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL SCHEDULED MAIN
- [SDR C2XA01TY168](https://openairdocs.org/sdr/C2XA01TY168.md): Switch · inoperative · Oct 28, 2001 · N16510 · Emb EMB135ER · Oxygen System
  > TYS During a scheduled inspection, When doing inspection task card # 35-20-00-720-001-A00, the cabin oxygen masks did not deploy in auto mode. Maintenance removed and replaced the altitude sensing switch. I.A.W.-EMB-135-AMM-51-40-02. operational checked good.
- [SDR C2XA01TY167](https://openairdocs.org/sdr/C2XA01TY167.md): Floor Support · corroded · Oct 28, 2001 · N16510 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED INSPECTION, SEVERAL AREAS OF CORROSION WAS FOUND ON THE CENTER FLOORBEAM GUSSET BETWEEN FRAMES 18-22. MAINTENANCE REMOVED AND REPLACED GUSSET TOP CAP. IAW-EMB-135/145-SRM-51-40-02. REPAIR PROCEDURES WERE SATISFACTORY, AIRCRAFT WILL BE
- [SDR C2XA01TY166](https://openairdocs.org/sdr/C2XA01TY166.md): Gusset · corroded · Oct 28, 2001 · N16510 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS During a scheduled inspection, corrosion was found on the floor gussets at the entrance to the cockpit, between frames 15 and 18. Maintenance removed and replaced gusset and center section of forward digital plate (fabricated doubler, shims and cockpit st
- [SDR C2XA01TY165](https://openairdocs.org/sdr/C2XA01TY165.md): Seal · corroded · Oct 28, 2001 · N16510 · Emb EMB135ER · Fuselage Floor Panel
  > TYS During a scheduled inspection, corrosion was found on the right floor seal at frame 18. Maintenance removed surface corrosion, alodined, primed and painted. I.A.W.-EMB135/145-CMP-51-21-04,05 and 06. Repair procedure was satisfactory and the aircraft will
- [SDR C2XA01TY164](https://openairdocs.org/sdr/C2XA01TY164.md): Antenna · corroded · Oct 28, 2001 · N16510 · Emb EMB135ER · Air Collision Avoidance System
  > TYS During a scheduled inspection the lower TCAS antenna was found with corrosion on the base. Maintenance removed and replaced the antenna, operational checked good. I.A.W.-EMB-AMM-34-43-03. Repair procedure was satisfactory and the aircraft will be released
- [SDR C2XA01TY163](https://openairdocs.org/sdr/C2XA01TY163.md): Floor Support · corroded · Oct 28, 2001 · N16510 · Emb EMB135ER · Fuselage Main, Floor Beam
  > TYS Several areas of corrosion were found on the aft side of service door aft of frame 22.Maintenance removed floor support and replaced it with a new part IAW emb135/145 SRM 51-40-02 and 51-10-02-Work was satisfactory and aircraft will be released upon comple
- [SDR C2XA01TY162](https://openairdocs.org/sdr/C2XA01TY162.md): Bushing · backed out · Oct 28, 2001 · N16510 · Emb EMB135ER · Passenger/Crew Doors
  > TYS DURING A SCHEDULED INSPECTION THE PAX-DOOR HOLD OPEN PIN LOWER BUSHING WAS FOUND TO BE MIGRATING OUT. MAINTENANCE INSTALLED BUSHING FROM THE BOTTOM IN REFERENCE TO GST-1662/01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED ON COMPLETION OF AIRCRAFT MAIN
- [SDR C2XA00CL072](https://openairdocs.org/sdr/C2XA00CL072.md): Tube · broken · Sep 24, 2000 · N16510 · Emb EMB135ER · Compressor Bleed Control
  > MDW-EWR - FLT 3620 - THE CREW REPORTED THE LEFT ENGINE ITT WAS HIGHTER THAN THE RIGHT (APPROX 100 DEGREES) WHILE IN CRUISE. THE AIRCRAFT DIVERTED INTO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT ENGINE AIR TUBE ASSY FOR

## 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 = 'N16510' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N16510/reports

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