# Service difficulty reports: N11539

A list on [N11539](https://openairdocs.org/aircraft/N11539.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 · 67 reports

- [SDR ASOA2019123045119](https://openairdocs.org/sdr/ASOA2019123045119.md): Unknown · odor · Dec 24, 2019 · N11539 · Emb EMB145LR · Air Distribution System
  > PILOT REPORTED SMOKE ODOR IN FLIGHT DECK AFTER STARTING APU. MX PERFORMED A FEW APU STARTS NO SMOKE OR ODOR DETECTED IN FLIGHT DECK. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2019121864066](https://openairdocs.org/sdr/ASOA2019121864066.md): Engine · failed · Dec 16, 2019 · N11539 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > IAH - FLIGHT 4047 THE CREW REPORTED THAT INITIATED CLIMB OUT AT 5000FT WHEN THRUST LEVER WAS ADVANCED #2 ENGINE FLAMED OUT. EICAS MESSAGE PRESENTED SHORTLY AFTER WITH NO ENGINE FIRE NOTED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENA
- [SDR ASOA20191115111](https://openairdocs.org/sdr/ASOA20191115111.md): Battery Pack · inoperative · Nov 11, 2019 · N11539 · Emb EMB145LR · Emergency Lighting
  > MX REPORTED CABIN EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED EMERGENCY BATTERIES 1&2 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20191115110](https://openairdocs.org/sdr/ASOA20191115110.md): Bulb · burned out · Nov 11, 2019 · N11539 · Emb EMB145LR · Emergency Lighting
  > MX REPORTED THE LEFT AND RIGHT FWD OVER WING EMERGENCY LIGHTS INOP. MX RE-LAMPED EMERGENCY LIGHTS WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2019081314044](https://openairdocs.org/sdr/ASOA2019081314044.md): Acm · inoperative · Aug 11, 2019 · N11539 · Emb EMB145LR · Cabin Cooling System
  > MAINTENANCE RECORDED THAT THE FLIGHT CREW COMPLAINED ABOUT SMOKE / ELECTRICAL BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE #2 ACM TO BE THE CAUSE OF THE ISSUE. MAINTENANCE REMOVED AND REPLACED THE #2 ACM, OPERATIONAL
- [SDR ASOA201908073041](https://openairdocs.org/sdr/ASOA201908073041.md): Muffler · dirty · Aug 3, 2019 · N11539 · Emb EMB145LR · Cabin Cooling System
  > FLIGHT 4478 THE CREW REPORTED A BURNING EXHAUST ODOR IN AC PACKS/GASPERS WITH THE SMELL OCCURRING MULTIPLE TIMES DURING DESCENT WITH THE ENGINES AT IDLE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE DISTRIBUTION SYSTEM
- [SDR ASOA201907207074](https://openairdocs.org/sdr/ASOA201907207074.md): Bushing · damaged · Jul 19, 2019 · N11539 · Emb EMB145LR · Horizontal Stabilizer Structure
  > LT HORIZONTAL STABILIZER I/B AND O/B HINGE PIN LUGS STATIONARY HAT BUSHINGS DAMAGED. REMOVED BUSHINGS, REAMED TO 1ST OVERSIZE AND INSTALLED NEW BUSHINGS. AIRCRAFT STILL IN MAINTENANCE.
- [SDR ASOA201907207073](https://openairdocs.org/sdr/ASOA201907207073.md): Bushing · damaged · Jul 19, 2019 · N11539 · Emb EMB145LR · Horizontal Stabilizer Structure
  > RT HORIZONTAL STAB I/B HINGE PIN LUGS STATIONARY BUSHING MIGRATED AND DAMAGED. REMOVED BUSHINGS AND REAMED TO 4TH REWORK AND INSTALLED NEW BUSHINGS.
- [SDR ASOA2019062195080](https://openairdocs.org/sdr/ASOA2019062195080.md): Bulb · inoperative · Jun 19, 2019 · N11539 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE ROW 23 CEILING EMERGENCY LIGHT WAS FOUND INOP. MX R/R LIGHT BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201905205070](https://openairdocs.org/sdr/ASOA201905205070.md): Controller · faulty · May 20, 2019 · N11539 · Emb EMB145LR · Windshield/Door Rain/Ice Removal
  > WINDSHIELD HEAT 2 FAIL ON T/O LOUD CLICKING FROM RELAY FOLLOWED BY STRONG BURNT SMELL. REMOVED AND REPLACED WINDSHIELD NR 2 TEMP CONTROLLER IAW AMM 30-42-01. OPS CHECK IS GOOD A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201812051323](https://openairdocs.org/sdr/ASOA201812051323.md): Battery Pack · discharged · Dec 1, 2018 · N11539 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE FIRST 3 SETS OF INTERIOR EMERGENCY LIGHTS AND RH LOWER EXTERIOR EMERGENCY LIGHT TURNS ON AND FADES OFF. MX REMOVED AND REPLACED #2 EMERGENCY BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2018090414046](https://openairdocs.org/sdr/ASOA2018090414046.md): Skin · cracked · Aug 31, 2018 · N11539 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > IAH - DURING MAINTENANCE INSPECTION A PREVIOUS REPAIR TO THE FUSELAGE SKIN AT FR21-22 STR 10L-11L WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REPAIR. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERV
- [SDR ASOA201807105162](https://openairdocs.org/sdr/ASOA201807105162.md): Light · malfunctioned · Jul 10, 2018 · N11539 · Emb EMB145LR · Emergency Lighting
  > PILOT REPORTED THE EMERGENCY LIGHT INSIDE EXIT ROW WAS NOT ILLUMINATING. MX PREFORMED A SYSTEM RESET AND PERFORMED OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201804134021](https://openairdocs.org/sdr/ASOA201804134021.md): Control Module · inoperative · Apr 13, 2018 · N11539 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT COME ON WITH THE F/A CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT CONTROL MODULE, OPS CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR ASOA201804124022](https://openairdocs.org/sdr/ASOA201804124022.md): Control Module · malfunctioned · Apr 12, 2018 · N11539 · Emb EMB145LR · Passenger Compartment Lighting
  > GRK - THE CREW REPORTED A BURNING SMELL ABOVE SEAT 1A. MAINTENANCE REMOVED AND REPLACED A LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS OR SMELL NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201711307028](https://openairdocs.org/sdr/ASOA201711307028.md): Uplock · failed · Nov 30, 2017 · N11539 · Emb EMB145LR · Landing Gear Position and Warning
  > NOSE GEAR WOULDN'T RETRACT AFTER TAKEOFF AND RETURNED TO DEPARTURE. FOUND THE NLG UPLOCK BOX AND NLG PROXIMITY SWITCHED BAD. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX AND PROXIMITY SWITCHES IAW AMM 32-33-07; 32-61-01; IPC32-33-07 PAGE 1, ITEM 30A,
- [SDR ASOA201711147027](https://openairdocs.org/sdr/ASOA201711147027.md): Bracket · cracked · Nov 13, 2017 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > A 2 INCH LONG CRACK WAS FOUND ON THE UPPER LATERAL BRACKET IN THE COCKPIT OVERHEAD. CUTOUT DAMAGED SECTION, SPLICED IN A NEW SECTION, FABRICATED AND INSTALLED DOUBLER. AIRCRAFT STILL IN C-CHECK.
- [SDR ASOA201709092009](https://openairdocs.org/sdr/ASOA201709092009.md): O-Ring · leaking · Sep 9, 2017 · N11539 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > NR 1 ENGINE PRODUCED SMOKE ON EXHAUST DURING WALK AROUND. REPLACE LPT SHAFT PLUG O-RING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201705154023](https://openairdocs.org/sdr/ASOA201705154023.md): Wire Harness · defective · May 15, 2017 · N11539 · Emb EMB145LR · Fire Protection System Wiring
  > FLIGHT 4189 THE CREW REPORTED AN ENGINE ONE FIRE DET FAIL MESSAGE ON EICAS DURING CLIMB AND DESCENT. THE AIRCRAFT LANDED IN JAN WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FIRE DETECTOR HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS,
- [SDR ASOA201612214114](https://openairdocs.org/sdr/ASOA201612214114.md): Light · inoperative · Dec 21, 2016 · N11539 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED ONE FLOOR EMERGENCY LIGHT STRIP OUT BETWEEN ROWS 8 & 9. REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160815044R](https://openairdocs.org/sdr/ASOA20160815044R.md): Connector · unsecure · Aug 15, 2016 · N11539 · Emb EMB145LR · Emergency Lighting
  > PILOT REPORTED UNABLE TO OPERATE EMERGENCY LIGHTS FROM THE FA PANEL. MX FOUND CONNECTOR ON F/A'S LIGHT CONTROL PANEL LOOSE. SECURED THE CONNECTER AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150427012](https://openairdocs.org/sdr/ASOA20150427012.md): Fitting · cracked · Apr 23, 2015 · N11539 · Emb EMB145LR · Trailing Edge Flaps
  > THE RT OTBD FLAP HAS A CRACK ON THE INBD ROOT FITTING. REPAIRED USING PRINCIPALES OF TECH INSTRUCTIONS TI-145-13-200, REV U. GENERATED A DMI TO PERFORM AN INTERNAL AND EXTERNAL DVI AT A 2C OR 10,000 FLT HRS WHICHEVER OCCURES FIRST.
- [SDR ASOA20140526044](https://openairdocs.org/sdr/ASOA20140526044.md): Flapper Valve · leaking · May 26, 2014 · N11539 · Emb EMB145LR · Fuel Storage
  > THE CREW REPORTED FUEL VENTING FROM RT WING ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE RT WING FLAPPER VALVE. OPS CHECKS WERE GOOD.
- [SDR ASOA20131203212](https://openairdocs.org/sdr/ASOA20131203212.md): Skin · cracked · Dec 6, 2013 · N11539 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING A-CHECK INSPECTION, LEFT FUSELAGE SKIN WAS FOUND TO HAVE A FREE FLOATING HORIZONTAL CRACK MEASURING 9.07 MM, 0.35", WITH A 3.47 MM, 0.13", CRACK TRAVELING UP FROM IT AT FRAME 75 ABOVE STRINGER 2L. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND PER
- [SDR ASOA20131203211](https://openairdocs.org/sdr/ASOA20131203211.md): Profile · cracked · Dec 6, 2013 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING A-CHECK INSPECTION, LEFT L-PROFILE, DRAG ANGLE WAS FOUIND TO BE CRACKED AT FRAME 76. MAINTENANCE R & R PROFILE, AND ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131203210](https://openairdocs.org/sdr/ASOA20131203210.md): Skin · cracked · Dec 6, 2013 · N11539 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING A-CHECK INSPECTION, RT SIDE FUSELAGE SKIN WAS FOUND TO BE CRACKED FRAME 75 BELOW STRINGER 2R. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131017119](https://openairdocs.org/sdr/ASOA20131017119.md): Unknown · odor · Oct 17, 2013 · N11539 · Emb EMB145LR · Buffet/Galleys
  > CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM COFFEEMAKER WHEN TURNED ON, ODOR WENT AWAY WHEN TURNED OFF. MX PERFORMED OPS CHECK OF THE COFFEEMAKER WITH NO FAULTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130628335](https://openairdocs.org/sdr/ASOA20130628335.md): Pressure Switch · defective · Jun 28, 2013 · N11539 · Emb EMB145LR · Aircraft Fuel Distribution System
  > ACFT WAS ON THE GROUND WHEN CREW SAW VISABLE SMOKE ON THE F/O SIDE OF ACFT. MX R & R THE NR 2 ENGINE FUEL LOW PRESSURE SWITCH IAW AMM 28-45-01, OPS CHECK GOOD IPC REFERENCE EMB 145 28-21-00, FIG 01 ITEM 110A. ACFT RELEASED TO SERVICE.
- [SDR ASOA20130626065R](https://openairdocs.org/sdr/ASOA20130626065R.md): Pressure Switch · inoperative · Jun 26, 2013 · N11539 · Emb EMB145LR · Aircraft Fuel Distribution System
  > PILOT REPORTED VISIBLE SMOKE IN COCKPIT ON THE F/O'S SIDE WITH THE FUEL PUMPS ON. MX PERFORMED A DETAILED VISUAL INSPECTION IN THE COCKPIT AND NO SMOKE NOTED. R & R THE NR 2 ENGINE LOW PRESSURE SWITCH WITH OPS CHECK SUCCESSFUL.
- [SDR ASOA20130601169V](https://openairdocs.org/sdr/ASOA20130601169V.md): Sill · corroded · Jun 1, 2013 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE CARGO DOOR CUTOUT CENTER SILL WAS FOUND TO BE CORRODED. BETWEEN FRAMES 65-68 AND STRINGERS 15-16L. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130601168](https://openairdocs.org/sdr/ASOA20130601168.md): Floor Support · corroded · Jun 1, 2013 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130601167](https://openairdocs.org/sdr/ASOA20130601167.md): Floor Support · corroded · Jun 1, 2013 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10, FIG 202. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130601166](https://openairdocs.org/sdr/ASOA20130601166.md): Floor Support · corroded · Jun 1, 2013 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 34. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-01, FIG 202. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130601165](https://openairdocs.org/sdr/ASOA20130601165.md): Floor Support · corroded · Jun 1, 2013 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 55. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10, FIG 202. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11CL232](https://openairdocs.org/sdr/C2XA11CL232.md): Actuator · faulty · Oct 13, 2011 · N11539 · Emb EMB145LR · Trailing Edge Flap Actuator
  > ORD FLT 5946 THE CREW REPORTED A FLAP FAIL MESSAGE AT 500 FT ON FINAL APPROACH WITH FLAPS SHOWING 45 DEGREES. MAINTENANCE INSPECTED AND REPLACED THE LEFT OUTBOARD FLAP INBOARD ACTUATOR. PERFORMED ZERO RIG OF THE FLAP SYSYTEM. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA20111002152](https://openairdocs.org/sdr/C2XA20111002152.md): Switch · faulty · Oct 2, 2011 · N11539 · Emb EMB145LR · Fire Detection
  > ACFT WAS IN FOR A SERVICE ROUTINE AND ON THE MORNING DEPARTURE CLIMBOUT THE CREW GOT A AURA WARNING OF A FIRE. ACFT RETURNED TO DEPARTURE WHERE MX FOUND THE NR1 ENG FIRE SWITCH WOULD NOT LOCK DOWN INT DOWN POSITION. MX R & R THE ENG FIRE SWITCH IAW MM 31-00-
- [SDR C2XA11CL184](https://openairdocs.org/sdr/C2XA11CL184.md): Potentiometer · faulty · Aug 6, 2011 · N11539 · Emb EMB145LR · Landing Gear Steering System
  > ORD FLT 5912 THE CREW REPORTED THE STEERING WAS UNRESPONSIVE WHILE TAXIING. THE AIRCRAFT STARTED PULLING RIGHT AND GRINDING NOISE CAME FROM THE NOSE WHEEL AREA. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR FEEDBACK POT
- [SDR C2XA11IA097](https://openairdocs.org/sdr/C2XA11IA097.md): Engine · leaking · May 19, 2011 · N11539 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > IAH - FLIGHT 3051, THE CREW REPORTED THAT AT FULL POWER SETTING DURING CLIMB PACK TWO EMITTED A BURNING SMELL. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO ENGINE,
- [SDR C2XA10IA091](https://openairdocs.org/sdr/C2XA10IA091.md): Isis · inoperative · Mar 8, 2010 · N11539 · Emb EMB145LR · Integrated Flight System
  > IAH - FLIGHT 2237, THE CREW REPORTED THAT ON LANDING THE ISIS FAILED WITH AN OUT OF ORDER MESSAGE FOLLOWED BY AN ELECTRICAL BURNING SMELL ON THE FLIGHT DECK. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE RESET THE ISIS, OPERATIONALLY TESTED WITH NO DEFECTS OR
- [SDR C2XA09RI206](https://openairdocs.org/sdr/C2XA09RI206.md): Starter Gen · inoperative · Dec 8, 2009 · N11539 · Emb EMB145LR · Starter-Generator
  > FLIGHT 2082 - IND - FLIGHT CREW REPORTED ELECTRIC BURN SMELL IN COCKPIT AND GALLEY FOLLOWED BY APU AUTO SHUTDOWN. MX REMOVED AND REPLACED APU STARTER GENERATOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09IA280](https://openairdocs.org/sdr/C2XA09IA280.md): Unknown · odor · Nov 2, 2009 · N11539 · Emb EMB145LR · Air Distribution System
  > ABQ - FLIGHT 2728, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT AND CABIN. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT ELECTRICAL AND PNEUMATIC SYSTEMS, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT W
- [SDR C2XA09SH203](https://openairdocs.org/sdr/C2XA09SH203.md): Skin · damaged · Jul 21, 2009 · N11539 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK LIGHTNING STRIKE BETWEEN FRAME 23 AND 24 STRINGER 14L (EXTERNAL). MX PERFORMED AND COMPLETED REPAIR IAW SRM 53-21-01 AND IC 2009-145/05374. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH211](https://openairdocs.org/sdr/C2XA09SH211.md): Fitting · corroded · Jul 20, 2009 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK (FR 65/STR 16L) SHEER CLIP AT CARGO DOOR CUTOUT BASE FWD CORNER HAS CORROSION. MAINTENANCE REMOVED CORROSION AND COMPLETED REPAIR AT FRAME 65 CLIP IAW EC5330-01458 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH210](https://openairdocs.org/sdr/C2XA09SH210.md): Skin · corroded · Jul 20, 2009 · N11539 · Emb EMB145LR · Horizontal Stabilizer, Plate/Skin
  > SHV - DURING C-CHECK LT HORIZONTAL L/E UPPER AND LOWER SURFACE HAS CORROSION AROUND ALL RIVET HEADS AND SCREW HEADS. MAINTENANCE REMOVED CORROSION BY POLISHING LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SURFACES IAW EC5530-01116. THE AIRCRAFT WAS APPROVED
- [SDR C2XA09SH209](https://openairdocs.org/sdr/C2XA09SH209.md): Door Frame · corroded · Jul 20, 2009 · N11539 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK SERVICE DOOR CUTOUT AFT STRUCTURE AT FRAME 22 BETWEEN STRINGER 15R AND 16R HAS CORROSION AT BOLT HOLE. MAINTENANCE REPAIRED SERVICE DOOR CUTOUT AFT STRUCTURE AT FRAME 22 BETWEEN STRINGER 15R AND 16R AT BOLT HOLE IAW EC5310-01373. THE AIR
- [SDR C2XA09SH208](https://openairdocs.org/sdr/C2XA09SH208.md): Floor Support · corroded · Jul 20, 2009 · N11539 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM I/B SIDE HAS CORROSION FRAME 58-59. MAINTENANCE PERFORMED AND COMPLETED REPAIR OF LT OMEGA BEAM FRM 59 AT CROSSBEAM ATTACHMENT POINT IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH207](https://openairdocs.org/sdr/C2XA09SH207.md): Fitting · corroded · Jul 20, 2009 · N11539 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK CORROSION FOUND AT FRAME 65 CLIP. MAINTENANCE PERFORMED AND COMPLETED REPAIR TO FRAME CLIP AT FR 65 IAW EC5330-01458 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH206](https://openairdocs.org/sdr/C2XA09SH206.md): Bushing · migrated · Jul 20, 2009 · N11539 · Emb EMB145LR · Spoilers
  > SHV - DURING C-CHECK HAT BUSHING MIGRATED ON LT SPEED BRAKE ACTUATOR ATTACHMENT BRACKET. MAINTENANCE REMOVED, MEASURED AND REINSTALLED HAT BUSHING ON LT SPEED BRAKE ATTACHMENT BRACKET FOR ACTUATOR IAW EMB-145 EC5740-01152 REV B. MEASURED WITHIN LIMITS. THE
- [SDR C2XA09SH205](https://openairdocs.org/sdr/C2XA09SH205.md): Rivet · loose · Jul 20, 2009 · N11539 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK 3 WORKING RIVETS FOUND AT FRAME 79 STRINGER 3R-6R. MAINTENANCE REMOVED AND REPLACED RIVETS AT FRAME 79 STRINGER 3R-6R IAW EC5330-01941 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH204](https://openairdocs.org/sdr/C2XA09SH204.md): Skin · dented · Jul 20, 2009 · N11539 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK DENT IN LT STATIC PORT AREA AT FRAME 14 STRINGER 15L. MAINTENANCE REPAIRED DENT IN LT STATIC PORT AREA AT FRAME 14 STRINGER 15L IAW IC2009-145/05429. INSPECTION PERFORMED RVSM CRITICAL REGION INSPECTION. RVSM WAS FOUND TO BE IN LIMITS.

Next page: https://openairdocs.org/aircraft/N11539/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 = 'N11539' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N11539/reports

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