# Service difficulty reports: N11535

A list on [N11535](https://openairdocs.org/aircraft/N11535.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 · 71 reports

- [SDR ASOA202004027033](https://openairdocs.org/sdr/ASOA202004027033.md): Door Sill · corroded · Apr 2, 2020 · N11535 · Emb EMB145 · Fuselage Miscellaneous Structure
  > CARGO DOOR CUT-OUT SILL HAS CORROSION. REMOVED AND REPLACED CARGO DOOR CUT-OUT SILL. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA202003307033](https://openairdocs.org/sdr/ASOA202003307033.md): Floor Support · corroded · Mar 30, 2020 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RH OMEGA BEAM CORRODED BETWEEN FRAMES 59-60 AT NUTPLATE. REPAIRED RH OMEGA BEAM BETWEEN FRAMES 56-60 AT NUTPLATE IAW EMB 145 SRM 53-24-10.
- [SDR ASOA202003307032](https://openairdocs.org/sdr/ASOA202003307032.md): Stringer Splice · cracked · Mar 30, 2020 · N11535 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 6R SPLICE IS CRACKED @ FWD END @ FRAME 19 (MARKED). REMOVED AND REPLACED CRACKED STIFFENER IAW EMB 145 SRM 51-40-02.
- [SDR ASOA202003257029](https://openairdocs.org/sdr/ASOA202003257029.md): Skin Panel · cracked · Mar 24, 2020 · N11535 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > CRACK IN SKIN PANEL @ FRAME 75 BETWEEN 1L & 2L. CUT OUT CRACKED SECTION, FABRICATED AND INSTALLED FILLER AND DOUBLER. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA202001287015](https://openairdocs.org/sdr/ASOA202001287015.md): Wire Harness · damaged · Jan 28, 2020 · N11535 · Emb EMB145LR · Landing Gear System Wiring
  > TYS A/C ONCE AIRBORNE THE AIR-GROUND FAIL AND CREW RETURN TO BASE. MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXY SWITCH HARNESS IAW EMB 145AMM 20-10-01 AND OPS CHECK GOOD IAW EMB 145 AMM 32-30-00. A/C RELEASED TO SERVICE.
- [SDR ASOA2019041745055](https://openairdocs.org/sdr/ASOA2019041745055.md): Battery Pack · inoperative · Apr 14, 2019 · N11535 · Emb EMB145LR · Emergency Lighting
  > MX REPORTED THE EMERGENCY FLOOR LIGHT BY WING EMERGENCY EXIT INOP. REMOVED AND REPLACED THE #3 PSU BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2019041745054](https://openairdocs.org/sdr/ASOA2019041745054.md): Battery Pack · inoperative · Apr 14, 2019 · N11535 · Emb EMB145LR · Emergency Lighting
  > MX REPORTED THE EMERGENCY LIGHTS BY WING EMERGENCY EXIT NOT WORKING. REMOVED AND REPLACED THE #3 PSU BATTERY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201805257093](https://openairdocs.org/sdr/ASOA201805257093.md): Control Unit · failed · May 25, 2018 · N11535 · Emb EMB145LR · Flight Control System
  > DURING CLIMB OUT, WHILE ACTIVATING MAIN PITCH TRIM SWITCH, ICAS WENT TO INOPERATIVE, THE MASTER WARNING WENT TO INOPERATIVE, THE MESSAGE REMAINED AFTER THE TRIM SWITCH WAS RELEASED.. MESSAGE ALSO REMAIN WAS RELEASED. ACFT RETURNED TO BASE AND MAINTENANCE R
- [SDR ASOA201703213051](https://openairdocs.org/sdr/ASOA201703213051.md): Charger · inoperative · Mar 21, 2017 · N11535 · Emb EMB145LR · Emergency Lighting
  > LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY CHARGER IAW AMM 33-50-04. OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA201702017002](https://openairdocs.org/sdr/ASOA201702017002.md): Engine · malfunctioned · Jan 27, 2017 · N11535 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > ENGINE NR 1 OUT IN FLIGHT. REMOVED AND REPLACED NR 1 ENG. OPS AND LEAK CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA201701163002](https://openairdocs.org/sdr/ASOA201701163002.md): Battery Pack · discharged · Jan 16, 2017 · N11535 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EXTERNAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY CHARGER AND BATTERY PACK. OPERATIONAL CHECKED GOOD.
- [SDR ASOA20160502020](https://openairdocs.org/sdr/ASOA20160502020.md): Battery Pack · discharged · May 2, 2016 · N11535 · Emb EMB145LR · Emergency Lighting
  > DURING SCHEDULED MAINTENANCE INSPECTION THE AFT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160429028](https://openairdocs.org/sdr/ASOA20160429028.md): Wire · burned · Apr 29, 2016 · N11535 · Emb EMB145 · Flight Control System Wiring
  > THE CREW REPORTED CLIMBING OUT THROUGH 6000 FT, THEY SMELLED A FOUL ODOR AND RECEIVED A PITCH TRIM MAIN FAIL MESSAGE. NONE OF THE TRIM SWITCHES WOULD WORK. PITCH TRIM BREAKER POPPED AND SMELL WENT AWAY. MAINTENANCE INSPECTED AND REPAIRED BURNED PITCH TRIM
- [SDR ASOA20160418022](https://openairdocs.org/sdr/ASOA20160418022.md): Power Supply · inoperative · Apr 18, 2016 · N11535 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD.
- [SDR ASOA20160325026](https://openairdocs.org/sdr/ASOA20160325026.md): Charger · inoperative · Mar 25, 2016 · N11535 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, MAINTENANCE DISCOVERED AN OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT CHARGER ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160224014](https://openairdocs.org/sdr/ASOA20160224014.md): Power Supply · inoperative · Feb 24, 2016 · N11535 · Emb EMB145 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE CABIN FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROW 18 TO ROW 24. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD.
- [SDR ASOA20160214009H](https://openairdocs.org/sdr/ASOA20160214009H.md): Battery Pack · discharged · Feb 14, 2016 · N11535 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION THE ALL OF THE EMERGENCY LIGHTS THAT OPERATE OFF OF BATTERY NR 4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160207010](https://openairdocs.org/sdr/ASOA20160207010.md): Battery · inoperative · Feb 7, 2016 · N11535 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, THE AFT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA201601070003](https://openairdocs.org/sdr/ASOA201601070003.md): Battery Pack · inoperative · Jan 7, 2016 · N11535 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, THE LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA20150323079](https://openairdocs.org/sdr/ASOA20150323079.md): Floor Support · corroded · Mar 23, 2015 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CK. CENTER OMEGA BEAM CORRODED AT FR 59. REPAIRED CENTER OMEGA BEAM IAW EC5320-02020. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150323078](https://openairdocs.org/sdr/ASOA20150323078.md): Skin · cracked · Mar 23, 2015 · N11535 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CK. RT FUSELAGE SKIN CRACKED AROUND RIVET FR 79. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150323077](https://openairdocs.org/sdr/ASOA20150323077.md): Skin · cracked · Mar 23, 2015 · N11535 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, RT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 75. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150323076V](https://openairdocs.org/sdr/ASOA20150323076V.md): Skin · cracked · Mar 23, 2015 · N11535 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, LEFT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 77-78. REPAIRED FUSELAGE SKIN IAW EC5330-02992. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131118081](https://openairdocs.org/sdr/ASOA20131118081.md): Charger · inoperative · Nov 18, 2013 · N11535 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED EMERGENCY LIGHT ON MAIN CABIN DOOR CEILING PANEL WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER ASSY. OPS CHECKED GOOD.
- [SDR ASOA20130825101](https://openairdocs.org/sdr/ASOA20130825101.md): Unknown · odor · Aug 25, 2013 · N11535 · Emb EMB145LR · Air Distribution System
  > ON DESCENT, CREW REPORTED A VERY STRONG ODOR OF BURNING IN FLIGHT DECK. F/A REPORTED BURNING ODOR ALSO AROUND ROW 11. SMOKE WAS NOT VISIBLE ONLY STRONG ODOR. MX INSPECTED AND FOUND EVIDENCE OF INGESTED BIRD IN NR 1 ENGINE. PERFORMED BORESCOPE AND BIRD STRI
- [SDR ASOA20130717075R](https://openairdocs.org/sdr/ASOA20130717075R.md): Flapper Valve · leaking · Jul 17, 2013 · N11535 · Emb EMB145LR · Fuel Storage
  > LIQUID VAPOR WAS REPORTED TO BE TRAILING OFF THROUGH RT WING AFTER TAKEOFF BY FLIGHT ATTENDANT. MX R & R THE RT WING OTBD FLAPPER VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR V0XR20130401J0186](https://openairdocs.org/sdr/V0XR20130401J0186.md): Stringer · chafed · Mar 29, 2013 · N11535 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 2L IS CHAFED AT FRAME 20. BLENDED OUT DAMAGE IAW SRM 51-10-03, NDT PERFORMED, NO DEFECTS NOTED, ALODINED DAMAGED AREA, FABRICATED REPAIR, ALODINED AND PRIMED FABRICATED PARTS, INSTALLED NEW FABRICATED REPAIR, DOUBLER. CLASSIFIED AS A MAJOR.
- [SDR V0XR201303270185](https://openairdocs.org/sdr/V0XR201303270185.md): Channel · corroded · Mar 25, 2013 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RT HAT BEAM AT FRAME 60 IS CORRODED. R & R RT HAT BEAM AT FRAME 60 IAW SRM 51-40-02, 53-24-10,51-20-03, 51-20-01, AND CPM 51-21-06,51-21-05,51-21-04, AND AMM 25-40-01.
- [SDR V0XR201303270184](https://openairdocs.org/sdr/V0XR201303270184.md): Sill · corroded · Mar 25, 2013 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RT SILL AT FRAME 61 CABIN BOTTOM IS CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R SILL IAW SRM 51-10-03,51-40-02, 51-40-06, 53-31-10, AND CPM 51-21-06.
- [SDR V0XR201303270183](https://openairdocs.org/sdr/V0XR201303270183.md): Sill · corroded · Mar 25, 2013 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LT SILL AT FRAME 61 CABIN BOTTOM IS CORRODED. REMOVED THE CORROSION,THE REMAINING MATERIAL WAS OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R LT SILL AT FRAME 61 IAW SRM 51-10-03,51-40-02,51-40-06,53-31-10, AND CPM 51-21-06.
- [SDR V0XR201303270182](https://openairdocs.org/sdr/V0XR201303270182.md): Sill · corroded · Mar 25, 2013 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LT SILL AT FRAME 58 CABIN BOTTOM IS CORRODED. REMOVED THE CORROSION,THE REMAINING MATERIAL WAS OUT OF LIMITS IAW SRM 51-10-03 & 53-31-10. R & R LT SILL AT FRAME 58 IAW SRM 51-10-03, 51-40-02,51-40-06, 53-31-10, AND CPM 51-21-06.
- [SDR V0XR20130325J0181](https://openairdocs.org/sdr/V0XR20130325J0181.md): Gusset · corroded · Mar 22, 2013 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > GUSSET ON CENTER HAT LT BEAM AT FRAME 60 CORRODED. R & R CENTER HAT GUSSET AT FRAME 60 IAW SRM 51-40-02, 53-24-10, 51-20-03,51-20-01, AND CPM 51-21-04,51-21-05.
- [SDR V0XR20130325J0180](https://openairdocs.org/sdr/V0XR20130325J0180.md): Angle · corroded · Mar 22, 2013 · N11535 · Emb EMB145LR · Cargo/Baggage Doors
  > CARGO DOOR TOP FRAME HAS CORROSION AROUND FORWARD FASTENER HOLE. INSTALLED NEW TOP CARGO DOOR ANGLE TO CARGO DOOR. PN 145-31544-001 IAW SRM 51-40-02, 51-20-03, AND 52-30-01.
- [SDR V0XR20130325J0179](https://openairdocs.org/sdr/V0XR20130325J0179.md): Sill · corroded · Mar 22, 2013 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO DOOR SILL AROUND 2 FASTENER HOLES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. R & R AFT CARGO LOWER DOOR SILL IAW SRM 51-10-03, 53-31-15, 51-20-03, CPM 51-21-04, 51-21-05, AND 51-21-06.
- [SDR ASOA20130117003C](https://openairdocs.org/sdr/ASOA20130117003C.md): Light · inoperative · Jan 17, 2013 · N11535 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED LT EXTERNAL FORWARD EMERGENCY LIGHT INOPERATIVE. MX INSPECTED AND REPLACED THE LT WING FORWARD EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.
- [SDR ASOA20121217120](https://openairdocs.org/sdr/ASOA20121217120.md): Unknown · odor · Dec 17, 2012 · N11535 · Emb EMB145LR · Air Distribution System
  > CREW REPORTED A FUEL ODOR IN COCKPIT DURING POWER CHANGES. MX PERFORMED ENGINE RUNS AT HIGH POWER AND VARIABLE SETTINGS WITH BOTH PACKS ON AND COULD NOT DUPLICATE ANY FUEL ODOR IN COCKPIT OF CABIN. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11RI139](https://openairdocs.org/sdr/C2XA11RI139.md): Light · inoperative · Aug 22, 2011 · N11535 · Emb EMB145LR · Emergency Lighting
  > RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND CEILING EXIT LIGHT NOT WORING DURING TEST. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA11RI135](https://openairdocs.org/sdr/C2XA11RI135.md): Light · inoperative · Aug 15, 2011 · N11535 · Emb EMB145LR · Emergency Lighting
  > RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND ROW 7 FLOOR PROXIMITY STRIP INOPERATIVE. MX REMOVED AND REPLACED STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA11IA076](https://openairdocs.org/sdr/C2XA11IA076.md): Transponder · inoperative · Apr 25, 2011 · N11535 · Emb EMB145LR · Navigation System
  > DURING CLIMB THE CREW REPORTED THE NR 2 TRANSPONDER. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE INTEGRATED COMM /TRANSPONDER UNIT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH082](https://openairdocs.org/sdr/C2XA11SH082.md): Skin · cracked · Apr 3, 2011 · N11535 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK EXTERNAL SKIN CRACKED AT FRAME 50 STRINGER 15R. MAINTENANCE PERFORMED REPAIR ON EXTERNAL SKIN AT FRAME 50 STRINGER 15R IAW EMB-145 EC5330-02393. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10RI052](https://openairdocs.org/sdr/C2XA10RI052.md): Computer · faulty · Apr 26, 2010 · N11535 · Emb EMB145LR · Ground Proximity System
  > FLIGHT 2985 - EWR - FLIGHT CREW REPORTED BURNING SMELL IN COCKPIT, GPWS/WINDSHEAR/TCAS INOP, THEN MESSAGE CLEAR. CREW RETURNED TO GATE UNEVENTFULLY. EWR MX REMOVED AND REPLACED GPWS COMPUTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO
- [SDR C2XA09RI153](https://openairdocs.org/sdr/C2XA09RI153.md): Strut · low · Aug 27, 2009 · N11535 · Emb EMB145LR · Nose/Tail Landing Gear Strut/Axle
  > FLIGHT 2767 - EWR - FLIGHT CREW DIVERTED TO EWR DUE TO LANDING GEAR NOT RETRACTING (ORIGINAL FLIGHT WAS ALB TO CLE). EWR MX VERIFIED GAP IN ALL WOW SWITCHES, SERVICED NOSE LANDING GEAR STRUT AND PERFORMED LANDING GEAR OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS
- [SDR C2XA09RI146](https://openairdocs.org/sdr/C2XA09RI146.md): Proximity Switch · corroded · Aug 17, 2009 · N11535 · Emb EMB145LR · Landing Gear Position and Warning
  > FLIGHT 2007 - RIC - AFTER TAKING OFF OF DCA TO CLE, FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. CREW DIVERTED FLIGHT TO RIC AND LANDED ACFT UNEVENTFULLY. RIC MX FOUND CORROSION ON NOSE DOWN PROX SWITCH. MX CLEANED CORROSION AND PERFO
- [SDR C2XA09CL079](https://openairdocs.org/sdr/C2XA09CL079.md): Coupling · blown · Jun 8, 2009 · N11535 · Emb EMB145LR · Cabin Cooling System
  > CLE FLIGHT 2351 - CREW REPORTED BOTH ENGINE BLEEDS CLOSED ADVISORY MESSAGE AND BOTH PACKS CLOSED, ADVISORY MESSAGE ON EICAS AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED TWO PACK COUPLINGS FOR PAC
- [SDR C2XA09IA148](https://openairdocs.org/sdr/C2XA09IA148.md): Proximity Switch · inoperative · Jun 5, 2009 · N11535 · Emb EMB145LR · Landing Gear Position and Warning
  > THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON CLIMB. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE NLG WOW PROX SWITCH, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH148](https://openairdocs.org/sdr/C2XA09SH148.md): Panel · corroded · May 3, 2009 · N11535 · Emb EMB145LR · Passenger/Crew Doors
  > SHV - DURING C-CHECK PAX DOOR BOTTOM FOUR NUT PLATE HOLES FOR MAIN LINER PANEL CORRODED. MAINTENANCE REPAIRED PAX DOOR LOWER FOUR NUT PLATE ATTACHMENT HOLES FOR MAIN LINER PANEL IAW EC5210-01154 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH146](https://openairdocs.org/sdr/C2XA09SH146.md): Skin · corroded · May 3, 2009 · N11535 · Emb EMB145LR · Horizontal Stabilizer, Plate/Skin
  > SHV - DURING C-CHECK HORIZONTAL STAB LT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER AND LOWER SURFACES. MAINTENANCE REPAIRED LT HORIZONTAL STABILIZER LEADING EDGE IAW EMB-145 EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH147](https://openairdocs.org/sdr/C2XA09SH147.md): Skin · corroded · May 3, 2009 · N11535 · Emb EMB145LR · Horizontal Stabilizer, Plate/Skin
  > SHV - DURING C-CHECK HORIZONTAL STAB RT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER AND LOWER SURFACES. MAINTENANCE REPAIRED RT HORIZONTAL STAB LEADING EDGE IAW EMB-145 EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH145](https://openairdocs.org/sdr/C2XA09SH145.md): Floor Support · corroded · May 3, 2009 · N11535 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FRAME 38. MAINTENANCE REMOVED CORROSION AT FR 38 IAW EMB-145 SRM 53-23-10 AND REPAIRED LT OMEGA BEAM AT FR 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH144](https://openairdocs.org/sdr/C2XA09SH144.md): Floor Support · corroded · May 3, 2009 · N11535 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV-DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FRAME 29. MAINTENANCE REMOVED CORROSION IAW EMB-145 SRM 53-22-10 AND INSTALLED FABRICATED REPAIR AT FRAME 29 IAW EMB-145 SRM 53-00-10 AND CPM 51-21-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/aircraft/N11535/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 = 'N11535' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N11535/reports

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