# Service difficulty reports: N16501

A list on [N16501](https://openairdocs.org/aircraft/N16501.md).

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

- [SDR C2XA07RI078](https://openairdocs.org/sdr/C2XA07RI078.md): Light · malfunctioned · Sep 10, 2007 · N16501 · Emb EMB135BJ · Emergency Lighting
  > FLT 2154 - EWR - CREW REPORTED EMERGENCY EXIT ROW 9A LIGHTS INOPERATIVE. EWR MX RESET ACFT ELECTRIC POWER, AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA06CL080](https://openairdocs.org/sdr/C2XA06CL080.md): Rmu · smoke · Oct 1, 2006 · N16501 · Emb EMB135ER · Audio/Video Monitoring
  > CLE FLIGHT NR 2786, CREW REPORTED SMOKE COMING FROM THE CO-PILOTS RMU WHILE TAXIING TO THE GATE. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE CO-PILOTS RMU. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA06SH089](https://openairdocs.org/sdr/C2XA06SH089.md): Stringer · corroded · Sep 10, 2006 · N16501 · Emb EMB135ER · Fuselage Main, Longeron/Stringer
  > SHV - DURING C-CHECK STRINGER 20R WAS FOUND TO BE CORRODED AT FRAME 51. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01393. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH088](https://openairdocs.org/sdr/C2XA06SH088.md): Floorbeam · corroded · Sep 6, 2006 · N16501 · Emb EMB135ER · Fuselage Main, Floor Beam
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 24. MAINTENANCE REMOVED THE DAMAGED AREA AND SPLICED IN A NEW BEAM SECTION IAW EC5320-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR CSXA06SH088](https://openairdocs.org/sdr/CSXA06SH088.md): Floor Support · corroded · Sep 6, 2006 · N16501 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK LT OMEGA BEAM FROM FR 20 TO 24 HAS CORROSION. MAINTENANCE SPLICED IN NEW LT OMEGA BEAM AT FR 18 TO 24 IAW EC5320-01229.
- [SDR C2XA06SH086](https://openairdocs.org/sdr/C2XA06SH086.md): Skin Panel · corroded · Sep 1, 2006 · N16501 · Emb EMB135ER · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK CENTER FUSELAGE 3 EXTERNAL SKIN HAS AREA OF CORROSION AT STR 19R FR 50 HYDRAULIC LINE PASS THROUGH. MAINTENANCE REPAIRED CENTER 3 EXTERNAL SKIN AT STR R19 FR 50 IAW EC5330-01624. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA06CL009](https://openairdocs.org/sdr/C2XA06CL009.md): Pdu · failed · Jan 18, 2006 · N16501 · Emb EMB135ER · Trailing Edge Flap Control System
  > CLE FLIGHT 2056 - THE CREW REPORTED A -FLAP FAIL- MESSAGE ON THE EICAS UPON SELECTING FLAPS -22- DEGREES. FLAPS WERE STUCK AT THE -18- DEGREE POSITION. THE CREW DECLARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE
- [SDR C2XA05CL017](https://openairdocs.org/sdr/C2XA05CL017.md): Heater · burned · Mar 16, 2005 · N16501 · Emb EMB135ER · Windshield/Door Rain/Ice Removal
  > CLE - FLIGHT 2226 THE CREW REPORTED A HOT BURNING SMELL IN THE CABIN AND COCKPIT. MAINTENANCE REPLACED THE NR 1 WINDSHIELD HEAT CONTROL BOX AND OPERATIONAL CHECKS GOOD.
- [SDR C2XA04CL011](https://openairdocs.org/sdr/C2XA04CL011.md): Light · inoperative · Feb 9, 2004 · N16501 · Emb EMB135ER · Emergency Lighting
  > CLE FLIGHT 2683 THE CREW REPORTED THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FIRST FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA04TY006](https://openairdocs.org/sdr/C2XA04TY006.md): Attach Fitting · gouged · Jan 10, 2004 · N16501 · Emb EMB135ER · Vertical Stabilizer, Attach Fittings
  > DURING A SCHEDULED INSPECTION, GOUGES WERE FOUND ON THE INNER BEARING MATING SURFACES AT THE HORIZONTAL STABILIZER ATTACH POINT. MAINTENANCE ACCOMPLISHED A REAM TO FIRST OVERSIZE REPAIR IAW EC5530-01062, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELE
- [SDR C2XA04TY005](https://openairdocs.org/sdr/C2XA04TY005.md): Angle · corroded · Jan 10, 2004 · N16501 · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR RAMP ANGLE AT THE COMPOSITE CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR RAMP ANGLE IAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPL
- [SDR C2XA01CL081](https://openairdocs.org/sdr/C2XA01CL081.md): Solenoid Valve · failed · Apr 17, 2001 · N16501 · Emb EMB135ER · Landing Gear Door Retract Section
  > CLE FLIGHT 3960 AFTER LANDING GEAR RETRACTION CREW REPORTED LOUD AIR NOISE COMING FROM NOSE LANDING GEAR AREA. NOISE INCREASED WITH AIRSPEED. AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITH OUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED NOSE LANDIN
- [SDR C2XA01CL050](https://openairdocs.org/sdr/C2XA01CL050.md): Window · leaking · Mar 6, 2001 · N16501 · Emb EMB135ER · Flight Compartment Windows
  > CLE FLIGHT 3971 AFTER DEICING OF AIRCRAFT THE CREW REPORTED A HISS AND POP SOUND FOLLOWED BY SMOKE COMING FROM FIRST OFFICER''S SIDE PANEL. THE ENGINES WERE SHUT DOWN AND ALL ELECTRICAL POWER WAS TURN OFF. MAINTENANCE INSPECTED AND FOUND DEICE FLUID HAD LEAK
- [SDR C2XA01CL025](https://openairdocs.org/sdr/C2XA01CL025.md): Light · inoperative · Feb 15, 2001 · N16501 · Emb EMB135ER · Emergency Lighting
  > CLE - FLT 3949 - THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE AT ROWS 3 THROUGH 6. MAINTENANCE REPLACED THE LIGHT STRIP ASSEMBLY NR 3. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)
- [SDR C2XA01CL001](https://openairdocs.org/sdr/C2XA01CL001.md): Charger · inoperative · Jan 8, 2001 · N16501 · Emb EMB135ER · Emergency Lighting
  > CLE - FLT 4135 - THE CREW REPORTED THAT THE 2ND AND 3RD SEAT OF AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE DURING THERE PREFLIGHT CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IAW EMB135 MM 33-50-04. MAINTENANCE
- [SDR C2XAOOCL087](https://openairdocs.org/sdr/C2XAOOCL087.md): Unknown · odor · Oct 27, 2000 · N16501 · Emb EMB135ER · Air Distribution System
  > CREW REPORTED A STRONG SMELL OF JET FUMES WHEN THE APU RUNS PACK NR 1. MX RAN APU AND CHECKED FOR LEAKS, NO LEAKS FOUND ALSO RAN PACK AND NO FUMES WERE NOTED. A/C WAS RELEASED FOR SERVICE.
- [SDR C2XA00BT085](https://openairdocs.org/sdr/C2XA00BT085.md): Starter · failed · Oct 2, 2000 · N16501 · Emb EMB135ER · Engine Start Valves/Controls
  > ROA - FLT 4009 - EN ROUTE CLE FROM RDU, CREW REPORTED NR 1 ENGINE INFLIGHT SHUTDOWN, OIL PRESSURE ERRATIC, OIL QUANTITY AT TWO QUARTS AIRCRAFT DIVERTED TO ROA AND LANDED UNEVETFULLY. MAINTNANCE DISPATCHED TO TROUBLESHOOT AND FOUND LEAKING NR 1 ENGINE AIR STAR
- [SDR C2XA00BT070](https://openairdocs.org/sdr/C2XA00BT070.md): Starter Gen · leaking · Oct 2, 2000 · N16501 · Emb EMB135ER · Starter-Generator
  > ROA - FLT 4009 - EN ROUTE CLE FROM RDU, CREW REPORTED NR 1 ENGINE IN FLIGHT SHUTDOWN, OIL PRESSURE ERRATIC, OIL QUANTITY AT TWO QUARTS AIRCRAFT DIVERTED TO ROA AND LANDED UNEVENTFULLY. MAINTENANCE DISPATCHED TO T/S AND FOUND LEAKING NR 1 ENGINE AIR STARTER.
- [SDR C2XA00CL074](https://openairdocs.org/sdr/C2XA00CL074.md): Starter · failed · Sep 30, 2000 · N16501 · Emb EMB135ER · Engine Oil Indicating System
  > RDU-CLE - FLT 4009 - THE CREW REPORTED THE NR 1 ENGINE OIL QUANTITY DROPPED TO 2 QUARTS INDICATED. THE CREW PERFORMED AN INFLIGHT SHUTDOWN AND DIVERTED INTO ROA. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE A
- [SDR C2XA99TY002](https://openairdocs.org/sdr/C2XA99TY002.md): Engine · failed · Oct 26, 1999 · N16501 · Emb EMB135ER · Engine (Turbine/Turboprop)
  > TYS - DURING A SCHEUDLED INSPECTION, THE LEFT ENGINE WAS FOUND TO BE PRODUCING METAL THAT WAS BEYOND MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW EMB-135 MM 71-00-00, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELE

## 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 = 'N16501' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N16501/reports

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