# Service difficulty reports: N16502

A list on [N16502](https://openairdocs.org/aircraft/N16502.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 · 57 reports

- [SDR FJTA2026072716502](https://openairdocs.org/sdr/FJTA2026072716502.md): Windshield · cracked · Jul 26, 2026 · N16502 · Emb EMB135ER · Flight Compartment Windows
  > WHILE CLIMBING THROUGH FL220 THE OUTER PANE OF THE FIRST OFFICER'S WINDSHIELD SHATTERED. THIS WINDSHIELD WAS RECENTLY REPLACED ON 7/18/2026 WITH AN OVERHAULED UNIT. TAT AT REPLACEMENT WAS 23586.9 AND TAC 25141.
- [SDR ASOA201703314015](https://openairdocs.org/sdr/ASOA201703314015.md): Floor Support · corroded · Mar 31, 2017 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE PERFORMED AN INSERTION REPAIR ON THE AFFECTED BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08RI070](https://openairdocs.org/sdr/C2XA08RI070.md): Module · inaccurate · May 12, 2008 · N16502 · Emb EMB135ER · Landing Gear Steering System
  > FLIGHT 1202 - EWR - FLIGHT CREW REPORTED STEERING PULLED TO LEFT AND SHAKING LEFT & RIGHT. CREW RETURNED AIRCRAFT TO GATE. EWR MX REMOVED AND REPLACED HYDRAULIC MODULE (STEERING MANIFOLD) AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. AIRCRAFT WAS APPROVED
- [SDR C2XA08RI067](https://openairdocs.org/sdr/C2XA08RI067.md): Smoke Detector · false activation · May 11, 2008 · N16502 · Emb EMB135ER · Smoke Detection
  > FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND LANDED AIRCRAFT UNEVE
- [SDR C2XA08RI061](https://openairdocs.org/sdr/C2XA08RI061.md): Smoke Detector · loose · May 2, 2008 · N16502 · Emb EMB135ER · Smoke Detection
  > FLIGHT 2424 - BAG SMOKE WARNING IN FLIGHT, BOTH LIGHTS AND EICAS MESSAGES STAYED FOR FEW SECONDS THEN WENT OFF. MX RESECURED LOOSE CONNECTOR PLUG AT AFT SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08CL053](https://openairdocs.org/sdr/C2XA08CL053.md): Wire · chafed · May 1, 2008 · N16502 · Emb EMB135ER · APU System Wiring
  > CLE FLIGHT 2419 - THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED AND REPAIRED A CHAFED WIRE ON THE APU HARNESS. PERFORMED OPERATIONAL CHECKS OF THE SYSTEM.
- [SDR C2XA08RI068](https://openairdocs.org/sdr/C2XA08RI068.md): Smoke Detector · intermittent · Jan 11, 2008 · N16502 · Emb EMB135ER · Smoke Detection
  > FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND LANDED AIRCRAFT UNEVE
- [SDR C2XA07CL077](https://openairdocs.org/sdr/C2XA07CL077.md): Shock Absorber · binding · Sep 13, 2007 · N16502 · Emb EMB135ER · Main Landing Gear Strut/Axle/Truck
  > CLE FLIGHT 2514 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR SHOCK ABSORBER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07CL069](https://openairdocs.org/sdr/C2XA07CL069.md): Wire Harness · faulty · Aug 16, 2007 · N16502 · Emb EMB135ER · Fire Protection System Wiring
  > CLE FLIGHT 2457 - THE CREW REPORTED A INTERMITTANT ENGINE NR 1 FIRE DETECT FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 1ENGINE HARNESS. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07RI002](https://openairdocs.org/sdr/C2XA07RI002.md): Seal · leaking · Jan 13, 2007 · N16502 · Emb EMB135ER · Passenger/Crew Doors
  > FLT 3031 - RIC - DURING FLIGHT, RIGHT OVERWING EMERGENCY EXIT DOOR AIR LEAK. RIC MX REMOVED THE DOOR, LUBRICATED DOOR SEAL, AND REINSTALLED IT. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA06CL085](https://openairdocs.org/sdr/C2XA06CL085.md): Battery · discharged · Oct 13, 2006 · N16502 · Emb EMB135ER · Emergency Equipment
  > DURING ROUTINE MAINTENANCE THE FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE INSPECTED AND REPLACED THE FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06CL072](https://openairdocs.org/sdr/C2XA06CL072.md): Splice · damaged · Sep 5, 2006 · N16502 · Emb EMB135ER · Light System Wiring
  > CLE - FLIGHT 2828, THE CREW REPORTED THE RIGHT SIDE EXIT ROW EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED DAMAGED WIRE SPLICE BEHIND LIGHT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA06SD015](https://openairdocs.org/sdr/C2XA06SD015.md): Smoke Detector · inoperative · Aug 22, 2006 · N16502 · Emb EMB135LR · Smoke Detection
  > SDF - BAGGAGE FIRE DETECTOR INOP. REMOVED AND REPLACED FWD BAGGAGE SMOKE DETECTOR IAW EMB 135 AMM 26-15-01. OPS CHECK GOOD.
- [SDR C2XA06SH069](https://openairdocs.org/sdr/C2XA06SH069.md): Stringer · corroded · Jun 21, 2006 · N16502 · Emb EMB135ER · Fuselage Main, Longeron/Stringer
  > SHV - DURING C-CHECK CORROSION DAMAGE WAS DISCOVERED ON STR 20L BETWEEN FRAME 59 AND 60. MAINTENANCE REMOVED CORROSION AND REPAIRED STR 20L BETWEEN FRAME 59 AND 60 IAW EC5310-01388. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA06SH064](https://openairdocs.org/sdr/C2XA06SH064.md): Floor Support · corroded · Jun 17, 2006 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 32 TO 35. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10, FIG 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH063](https://openairdocs.org/sdr/C2XA06SH063.md): Floor Support · corroded · Jun 17, 2006 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10, ITEM 3 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH062](https://openairdocs.org/sdr/C2XA06SH062.md): Floor Support · corroded · Jun 17, 2006 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 TO 32. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A FILLER REPAIR IAW EMB 135 SRM 53-00-10, ITEM 3 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH061](https://openairdocs.org/sdr/C2XA06SH061.md): Floor Support · corroded · Jun 17, 2006 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH065](https://openairdocs.org/sdr/C2XA06SH065.md): Floor Support · corroded · Jun 17, 2006 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-00-10 FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04BT089](https://openairdocs.org/sdr/C2XA04BT089.md): Tube · leaking · Aug 15, 2004 · N16502 · Emb EMB135LR · Turbine Engine Oil System
  > ENROUTE, DIVERTED, CREW REPORTED, ENGINE NR 1 LOST OIL INFLIGHT. PERFORMED SHUTDOWN IAW QRH. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED PRESSURE OIL CONTROL TUBE TO ENGINE GEARBOX, OPS AND LEAK CHECKED GOOD REFERENCE MM NR 71-00-01. AIR
- [SDR C2XA03TY161](https://openairdocs.org/sdr/C2XA03TY161.md): Floorbeam · corroded · Sep 11, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION THE RT HAND FORWARD DIGITAL UNDER THE GALLEY WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04,05AND 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMP
- [SDR C2XA03TY160](https://openairdocs.org/sdr/C2XA03TY160.md): Angle · corroded · Sep 11, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DUEING A SCHEDULED INSPECTION THE LEFT HAND FORWARD RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
- [SDR C2XA03TY159](https://openairdocs.org/sdr/C2XA03TY159.md): Floorbeam · corroded · Sep 11, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM TOP CAP WAS FOUND TO BE CORRODED UNDER SEAT TRACK LF1. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02 AND M.M. 53-01-06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON CO
- [SDR C2XA03TY158](https://openairdocs.org/sdr/C2XA03TY158.md): Sill · damaged · Sep 11, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE SERVICE DOOR FORWARD SILL AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 53-00-04, 51-40-02, 51-30-01 AND CPM 51-21-04, 05. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL
- [SDR C2XA03TY157](https://openairdocs.org/sdr/C2XA03TY157.md): Axle · damaged · Sep 10, 2003 · N16502 · Emb EMB135ER · Main Landing Gear Strut/Axle/Truck
  > DURING A SCHEDULED INSPECTION THE RIGHT MLG RETRACTION AXLE CHROME PLATED AREA DAMAGED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG RETRACTION AXLE I/A/W-EMB-135-AMM-32-10-03. OPS AND LEAK CHECKED GOOD.
- [SDR C2XA03TY156](https://openairdocs.org/sdr/C2XA03TY156.md): Sill · damaged · Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE MAIN DOOR SILL SKIN, MAINTENANCE REMOVED AND REPLACED THE SILL I/A/W-EMB-135-AMM-53-21-00.
- [SDR C2XA03TY155](https://openairdocs.org/sdr/C2XA03TY155.md): Skin · dented · Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION 2 DENTS WHERE FOUND AFT OF THE PAX DOOR BETWEEN FRAMES 19 AND 20, ABOVE STR 12L. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A FILLER AND DOUBLER, ALIDINED, INSTALLED THE PATCH, PRIMED AND PAINTED. I/A/W-EMB-135/145-SRM-53-21
- [SDR C2XA03TY153](https://openairdocs.org/sdr/C2XA03TY153.md): Bearing Cap · cracked · Sep 10, 2003 · N16502 · Emb EMB135ER · Main Landing Gear
  > DURING A SCHEDULED INSPECTION THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP IAW EMB M.M. 32-10-01, THE REPAIR WAS SATISFACTORY.
- [SDR C2XA03TY152](https://openairdocs.org/sdr/C2XA03TY152.md): Cap · cracked · Sep 10, 2003 · N16502 · Emb EMB135ER · Main Landing Gear
  > DURING A SCHEDULED INSPECTION THE LT MLG BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE BEARING CAP IAW EMB M.M. 32-10-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION
- [SDR C2XA03TY151](https://openairdocs.org/sdr/C2XA03TY151.md): Floorbeam · corroded · Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Floor Beam
  > DURING A SCHEDULED INSPECTION THE FLOORBEAM AT FRAME 22 RT, WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 22 IAW EMB SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPO
- [SDR C2XA03TY150](https://openairdocs.org/sdr/C2XA03TY150.md): Gusset · corroded · Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION THE GALLEY FLOOR AFT GUSSET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
- [SDR C2XA03TY149](https://openairdocs.org/sdr/C2XA03TY149.md): Plate · corroded · Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION THE GALLEY RIGHT HAND AFT CROSS BEAM PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CROSS BEAM PLATE IAW EMB SRM 51-10-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPE
- [SDR C2XA03TY148](https://openairdocs.org/sdr/C2XA03TY148.md): Cam · corroded · Sep 10, 2003 · N16502 · Emb EMB135ER · Nose/Tail Landing Gear
  > DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR STRUT MAIN HOUSING AND LOWER CAM WERE FOUND TO HAVE AREAS OF CORROSION AND PITTING. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR LEG ASSEMBLY IAW EMB MM 32-20-01, ALL OPERATIONAL AND LEAK CHECKS WE
- [SDR C2XA03TY147](https://openairdocs.org/sdr/C2XA03TY147.md): Bracket · corroded · Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING A SCHEDULE INSPECTION THE MAIN PASSENGER DOOR THRESHOLD BRACKETS WERE FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD BRACKETS IAW EMB SRM 51-40/02, 51-30-02 AND CPM 51-21-04,05 AND 06. THE REPAIR WAS FOUND TO SAT
- [SDR C2XA03TY145](https://openairdocs.org/sdr/C2XA03TY145.md): Sill · corroded · Sep 4, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
- [SDR C2XA03TY144](https://openairdocs.org/sdr/C2XA03TY144.md): Buttstrap · corroded · Aug 30, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 2C INSPECTION THE FWD DIGITAL BUTTSTRAP WAS CORRODED. MAINT REMOVED THE FWD DIGITAL, FAB A DOUBLER AND INSTALL A NEW FWD DOUBLER, ALLODINED, PRIMED AND PAINTED. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.
- [SDR C2XA03TY142](https://openairdocs.org/sdr/C2XA03TY142.md): Floorbeam · corroded · Aug 28, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Floor Beam
  > TYS DURING A SCHEDULED 2C INSPECTION THE FLOORBEAM AT FR 22 RT SIDE WAS FOUND CORRODED IN SEVERAL AREAS. MAINT R&R THE FLOOR BEAM AT FR 22 IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.
- [SDR C2XA03TY141](https://openairdocs.org/sdr/C2XA03TY141.md): Plate · corroded · Aug 28, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 2C INSPECTION THE RT AFT CROSS BEAM PLATE WAS CORRODED. MAINT R&R THE AFT CROSS BEAM PLATE IAW EMB 135/145 SRM 51-10-02 ALLODINED, PRIMED AND PAINTED REWORK AREA IAW EMB 135/145 CPM 51-21-04'05'06. ALL WORK WAS ACCOMPLISHED AND WILL B
- [SDR C2XA03TY140](https://openairdocs.org/sdr/C2XA03TY140.md): Gusset · corroded · Aug 28, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 2C INSPECTION THE AFT GUSSET WAS FOUND WITH SEVERAL AREAS THAT WAS CORRODED. MAINT R&R THE AFT GUSSET IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.
- [SDR C2XA03BT038](https://openairdocs.org/sdr/C2XA03BT038.md): Bearing · seized · Mar 14, 2003 · N16502 · Emb EMB135ER · Wheel/Ski/Float
  > EWR ACFT PULLS RIGHT ON T/O. ABORTED T/O AND TAXI BACK TO GATE. ACFT CONTINUED TO PULL RIGHT DURING TAXI. REMOVED AND REPLACED NOSE TIRE/WHEEL ASSYS. FOUND SEIZED BEARING. ALL IAW EMB MM 32-49-05. OPS CHECK GOOD.
- [SDR C2XA02CL105](https://openairdocs.org/sdr/C2XA02CL105.md): Receptacle · burned · Apr 24, 2002 · N16502 · Emb EMB135ER · Buffet/Galleys
  > CLE FLIGHT 3180 THE CREW REPORTED ELECTRICAL SMELL COMING FROM THE COFFEE WARMERS. MAINTENANCE INSPECTED AND REPLACED BOTH LEFT AND RIGHT COFFEE WARMER RECEPTACLES. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA02CL102](https://openairdocs.org/sdr/C2XA02CL102.md): Light · inoperative · Apr 20, 2002 · N16502 · Emb EMB135ER · Emergency Lighting
  > CLE MAINTENANCE FOUND THE CABIN EMERGENCY AISLE LIGHT INOPERATIVE DURING ROUTINE MAINTENANCE. MAINTENANCE REPLACED THE EMERGENCY AISLE LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA01CL228](https://openairdocs.org/sdr/C2XA01CL228.md): Actuator · failed · Nov 12, 2001 · N16502 · Emb EMB135ER · Stabilizer Actuator
  > MSN FLIGHT#3110 THE CREW REPORTED THE HORIZONTAL STABILIZER PITCH TRIM FAILED AFTER TAKEOFF.THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR AND THE HORIZONTAL STABILIZER CONT
- [SDR C2XA01TY090](https://openairdocs.org/sdr/C2XA01TY090.md): Bracket · chafed · Apr 25, 2001 · N16502 · Emb EMB135ER · Passenger/Crew Doors
  > TYS DURING A SCHEDULED INSPECTION THE MAIN CABIN DOOR, HANDLE BRACKET WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB-GST-1405/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
- [SDR C2XA01TY089](https://openairdocs.org/sdr/C2XA01TY089.md): Plate · corroded · Apr 25, 2001 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE JUST AFT OF FLIGHT DECK WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A SLICE REPAIR IAW EMB-GST-1266/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTI
- [SDR C2XA01TY088](https://openairdocs.org/sdr/C2XA01TY088.md): Floorbeam · corroded · Apr 24, 2001 · N16502 · Emb EMB135ER · Fuselage Main, Floor Beam
  > TYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM AFT OF FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A SPLICE REPAIR IAW EMB-135 SRM-53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
- [SDR C2XA01TY087](https://openairdocs.org/sdr/C2XA01TY087.md): Angle · corroded · Apr 23, 2001 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM AFT RAMP ANGLE FORWARD OF FRAME 20 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM-51-30-01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF
- [SDR C2XA01TY086](https://openairdocs.org/sdr/C2XA01TY086.md): Mount · chafed · Apr 23, 2001 · N16502 · Emb EMB135ER · Nacelle/Pylon, Attach Fittings
  > TYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE PYLON FORWARD YOKE MOUNT WAS FOUND CHAFED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1365/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
- [SDR C2XA01TY085](https://openairdocs.org/sdr/C2XA01TY085.md): Floorbeam · corroded · Apr 22, 2001 · N16502 · Emb EMB135ER · Fuselage Main, Floor Beam
  > TYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION AT FRAME 20. MAINTENANCE REPAIRED THE OMEGA BEAM IAW EMB-GST-3120/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSP
- [SDR C2XA01TY084](https://openairdocs.org/sdr/C2XA01TY084.md): Fitting · gouged · Apr 22, 2001 · N16502 · Emb EMB135ER · Stabilizer Actuator
  > TYS DURING A SCHEDULED INSPECTION THE RIGHT HORIZONTAL ACTUATOR SUPPORT FITTING WAS FOUND GOUGED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1340/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Next page: https://openairdocs.org/aircraft/N16502/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 = 'N16502' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N16502/reports

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