# Service difficulty reports: N15555, cancelled Oct 5, 2023

A list on [N15555, cancelled Oct 5, 2023](https://openairdocs.org/deregistered/N15555-2023-10-05.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 · 64 reports

- [SDR ASOA2019082145096](https://openairdocs.org/sdr/ASOA2019082145096.md): Bearing · seized · Aug 14, 2019 · N15555 · Emb EMB145LR · Cabin Cooling System
  > PILOT REPORTED "INTERMITTENT STRONG ELECTRICAL BURNING SMELL IN FLIGHT. THE SMELL WOULD COME AND GO. BECAME STRONG STARTING AT DESCENT FROM CRUISE. R & R NR 1 AIR CYCLE MACHINE WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2019061314028](https://openairdocs.org/sdr/ASOA2019061314028.md): Bulb · burned out · Jun 11, 2019 · N15555 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION THE LEFT HAND EXTERNAL EMERGENCY LIGHT FWD OF THE LEFT WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NPO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO
- [SDR ASOA2018060217095](https://openairdocs.org/sdr/ASOA2018060217095.md): Stringer · cracked · Jun 1, 2018 · N15555 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 2R CRACKED AT FRAME 75. REPAIRED THE STRINGER IAW ETD 2018-145-054192.
- [SDR ASOA201805167081](https://openairdocs.org/sdr/ASOA201805167081.md): Skin · cracked · May 16, 2018 · N15555 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING A C CHECK, FOUND THE LT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 1L TO 2L, VERIFIED BY SOP 5711, NDT. REPAIRED IAW SRM 53-31-01.
- [SDR ASOA201805167080](https://openairdocs.org/sdr/ASOA201805167080.md): Skin · cracked · May 16, 2018 · N15555 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING A C CHECK INSPECTION, FOUND THE RT FUSELAGE SKIN AT FRAME 75, STRINGER 1R CRACKED. VERIFIED WITH NDT.SOP 5711. REPAIRED THE SKIN IAW SRM 53-31-01.
- [SDR ASOA20805057083](https://openairdocs.org/sdr/ASOA20805057083.md): Frame · cracked · May 15, 2018 · N15555 · Emb EMB145LR · Fuselage Main, Frame
  > COCKPIT FRAME IS CRACKED BETWEEN FRAME 13, STRINGER 8L-10L. CUTOUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER TO FRAME 13 STRINGER 8L AND 10L PER SRM 53-00-04.
- [SDR ASOA201803174016](https://openairdocs.org/sdr/ASOA201803174016.md): Acm · failed · Mar 17, 2018 · N15555 · Emb EMB145LR · Cabin Cooling System
  > AIR RETURN DUE TO SMOKE AND HAZE IN THE COCKPIT. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT ACM, OPS TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201802227020](https://openairdocs.org/sdr/ASOA201802227020.md): Hinge · damaged · Feb 21, 2018 · N15555 · Emb EMB145LR · Trailing Edge Flaps
  > A BROKEN LUG WAS DISCOVERED ON THE LEFT HAND INBOARD FLAP SHROUD PIANO HINGE. REMOVED AND REPAIRED DAMAGED LEFT HAND INBOARD FLAP SHROUD PIANO HINGE PER EC5750-01468.
- [SDR ASOA201801234005](https://openairdocs.org/sdr/ASOA201801234005.md): Battery Pack · inoperative · Jan 23, 2018 · N15555 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHTS AT THE EMERGENCY EXIT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS TESTED GOOD. AIRCRATF WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201710243301](https://openairdocs.org/sdr/ASOA201710243301.md): Fitting · cracked · Oct 24, 2017 · N15555 · Emb EMB145LR · Nacelle/Pylon, Main Frame
  > DURING A NR 2 ENGINE CHANGE, FOUND THE LOWER FORWARD PYLON FITTING CRACKED. MAINTNENACE REPLACED THE LOWER FORWARD PYLON YOKE FITTING.
- [SDR ASOA201710233300](https://openairdocs.org/sdr/ASOA201710233300.md): Engine · failed · Oct 23, 2017 · N15555 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > THE CREW REPORTED ENGINE NR 2 EXCEEDANCE AND AUTO SHUT DOWN IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NR 2 ENGINE FAILED WITH INTERNAL DAMAGE. THE NR 2 ENGINE WAS REPLACED.
- [SDR ASOA20160812020](https://openairdocs.org/sdr/ASOA20160812020.md): Skin · damaged · Aug 11, 2016 · N15555 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > RIGHT NOSE SKIN DAMAGED BETWEEN FRAMES 3 AND 5, STRINGERS 4 AND 9R. REMOVED AND REPLACED THE DAMAGED SKIN.
- [SDR ASOA20151204203](https://openairdocs.org/sdr/ASOA20151204203.md): Beam · corroded · Dec 4, 2015 · N15555 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, BAGGAGE DOOR CUTOUT LOWER BEAM HAS CORROSION FRAME 65-68. INSTALLED NEW LOWER BEAM IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151204202](https://openairdocs.org/sdr/ASOA20151204202.md): Door Sill · corroded · Dec 4, 2015 · N15555 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FWD SERVICE DOOR SILL IS CORRODED. REPAIRDED FWD SERVICE DOOR SILL IAW SRM 53-21-10. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151204201](https://openairdocs.org/sdr/ASOA20151204201.md): Door Sill · corroded · Dec 4, 2015 · N15555 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, AFT SERVICE DOOR SILL IS CORRODED. REPAIRED AFT SERVICE DOOR SILL IAW SRM 53-21-10. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151120194](https://openairdocs.org/sdr/ASOA20151120194.md): Bracket · corroded · Nov 20, 2015 · N15555 · Emb EMB145LR · Fuselage Main, Attach Fittings
  > DURING C-CHECK, FOUND CARGO DOOR LOWER ANGLE BRACKET IS CORRODED AROUND NUTPLATE HOLES. INSTALLED NEW CARGO DOOR LOWER ANGLE BRACKET IAW SRM 51-40-02. APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2015728026](https://openairdocs.org/sdr/ASOA2015728026.md): Handle · inoperative · Jul 25, 2015 · N15555 · Emb EMB145LR · Fire Detection
  > NR 1 ENGINE FIRE TEE HANDLE DOES NOT ILLUMINATE ON FIRE DETECTION TEST. R & R NR 1 ENGINE FIRE TEE HANDLE. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20150707034R](https://openairdocs.org/sdr/ASOA20150707034R.md): Pressure Switch · faulty · Jul 7, 2015 · N15555 · Emb EMB145LR · Landing Gear Brake System
  > PILOT REPORTED THE BRAKES PULSING BADLY DURING LANDING ROLL AT HIGHER SPEEDS WITH LOW SPEEDS NORMAL. MX R & R THE OTBD BRAKE PRESSURE SWITCH AND BLED BRAKES WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150101003](https://openairdocs.org/sdr/ASOA20150101003.md): Inverter · inoperative · Jan 1, 2015 · N15555 · Emb EMB145LR · Emergency Lighting
  > DURING FLIGHT, CREW INSPECTION THE EMERGENCY LIGHT SIGN AT EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE ROW 18 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140917105](https://openairdocs.org/sdr/ASOA20140917105.md): Brake Assy · malfunctioned · Sep 17, 2014 · N15555 · Emb EMB145LR · Landing Gear Brake System
  > PILOT REPORTED DURING BRAKE APPLICATION, BRAKES WILL ALTERNATE BETWEEN GRABBING AND RELEASING, RESULTING IN DEGRADED BRAKING AND ACFT SHUDDERING. MAINTENANCE R & R NR 1 BRAKE ASSY WITH OPS AND TAXI CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140119008](https://openairdocs.org/sdr/ASOA20140119008.md): Mount · cracked · Jan 19, 2014 · N15555 · Emb EMB145LR · Engine Mount Section
  > DURING C-CHECK, NR 1 ENGINE FWD LOWER MOUNT CRACKED. R & R NR 1 ENGINE FWD LOWER YOKE FITTING IAW EC5450-01073, REV B. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140119007](https://openairdocs.org/sdr/ASOA20140119007.md): Firewall · cracked · Jan 19, 2014 · N15555 · Emb EMB145LR · APU Cowling/Containment
  > DURING C-CHECK. APU FIREWALL CRACKED. R & R APU FIREWALL IAW EC5310-01072. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130727197](https://openairdocs.org/sdr/ASOA20130727197.md): Bolt · broken · Jul 25, 2013 · N15555 · Emb EMB145LR · Fuselage Main, Structure
  > DURING SCHEDULED MX A BROKEN BOLT WAS FOUND IN THE LT AFT HOLE OF THE WINDSHIELD CENTER POST LOWER FITTING WHERE IT ATTACHES TO THE FORWARD PRESSURE BULKHEAD NEAR FRAME 7 AT THE 12 O'CLOCK POSITION. MX R & R THE BOLT IAW EC5310-01715, REV A. THE ACFT WAS AP
- [SDR ASOA20120423064](https://openairdocs.org/sdr/ASOA20120423064.md): Skin · dented · Apr 23, 2012 · N15555 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SKIN DENTED NEXT TO MAIN CABIN DOOR LOWER RT CORNER. MX INSPECTED THE DENT AND PERFORMED A FILLER REPAIR, LEAK CHECKS PERFORMED SATISFACTORILY, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120309024](https://openairdocs.org/sdr/ASOA20120309024.md): Skin · dented · Mar 5, 2012 · N15555 · Emb EMB145LR · Cargo/Baggage Doors
  > CARGO DOOR HAS SIX DENTS. RECONTOURED THE DENTS WITHOUT DIRECT IMPACT. PERFORMED NDT NO DEFECTS NOTED, FABRICATED DOUBLER AND INSTALLED.
- [SDR C2XA11TY161](https://openairdocs.org/sdr/C2XA11TY161.md): Radome · damaged · Oct 20, 2011 · N15555 · Emb EMB145LR · Aerodynamic Fairings
  > LIGHTNING STRIKE ON NOSE WITH BURNS AND RADOME COATING DAMAGE. UPON LIGHTNING STRIKE INSPECTION FOUND SEVERAL AREAS OF DAMAGE. REPAIRED LT AILERON, LT WING TIP, REPLACED LWR TDR ANTENNA, REPLACED VHF 2 ANTENNA, REPLACED DME 2 ANTENNA, REPLACED RADOME, REPAIR
- [SDR C2XA11CL200](https://openairdocs.org/sdr/C2XA11CL200.md): Fan · faulty · Sep 2, 2011 · N15555 · Emb EMB145LR · Air Distribution Fan
  > ORD FLT 6128 THE CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT AFTER ENGINE NR 2 START. MAINTENANCE INSPECTED AND REPLACED BOTH NR 1 AND NR 2 RECIRCULATION FANS. PERFORMED OPERATIONAL CHECKS WITH NO FURTHER SMELL NOTED.
- [SDR C2XA11TY034](https://openairdocs.org/sdr/C2XA11TY034.md): Skin · dented · Mar 22, 2011 · N15555 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > TWO DENTS ADJACENT TO EXTERNAL POWER RECEPTACLE. CUT OUT DAMAGE, RECONTOURED, INSTALLED DOUBLER IAW EC5330-02389.
- [SDR C2XA11CL050](https://openairdocs.org/sdr/C2XA11CL050.md): Controller · intermittent · Feb 16, 2011 · N15555 · Emb EMB145LR · Cabin Pressure Controller
  > THE CREW REPORTED A LOSS OF PRESSURIZATION ON DESCENT IN AUTO MODE. MAINTENANCE INSPECTED AND RELEASED IAW MEL 21-30-00-3. MAINTENANCE REPLACED THE PRESSURIZATION DIGITAL CONTROLLER AND ELECTRO-PNEUMATIC OUTFLOW VALVE. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11CL017](https://openairdocs.org/sdr/C2XA11CL017.md): Unknown · smoke · Jan 18, 2011 · N15555 · Emb EMB145LR · Air Distribution System
  > MHT FLT 2190 THE CREW REPORTED SMOKE IN LAV AND THE CABIN HAD A ELECTRICAL SMELL. THE AIRCRAFT DIVERTED INTO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES AND PERFORMED BLEED AIR SYSTEM OPERATIONAL CHECKS. NO SMOKE OR ELECTRICAL SME
- [SDR C2XA10R057](https://openairdocs.org/sdr/C2XA10R057.md): Adc · inoperative · May 6, 2010 · N15555 · Emb EMB145LR · Air Data Computer
  > FLIGHT 3110 - EWR - FLIGHT CREW REPORTED ADC NR 2 INOPERATIVE IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED ADC NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10SH060](https://openairdocs.org/sdr/C2XA10SH060.md): Frame · cracked · Feb 17, 2010 · N15555 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK FR 10 CRACKED AT STR 10R. REPAIRED FR 10 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09TY012](https://openairdocs.org/sdr/C2XA09TY012.md): Battery · defective · Jan 15, 2009 · N15555 · Emb EMB145 · Emergency Equipment
  > FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WILL NOT CHARGE. R&R THE BATTERY IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD ACFT RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09TY011](https://openairdocs.org/sdr/C2XA09TY011.md): Shear Tie · damaged · Jan 15, 2009 · N15555 · Emb EMB145 · Fuselage Internal Mounting Structure
  > FUSELAGE DENT LOWER RT OF THE MAIN DOOR. R&R DAMAGED SHEAR CLIP AT FRAME 20 BETWEEN STR 14L & 15L, REPAIRED DAMAGE IAW EC5330-01879. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA08IA118](https://openairdocs.org/sdr/C2XA08IA118.md): Light · inoperative · Apr 17, 2008 · N15555 · Emb EMB145LR · Emergency Lighting
  > AUS - DURING MAINTENANCE INSPECTION THE 4TH AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT STRIP. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08ON093](https://openairdocs.org/sdr/C2XA08ON093.md): Vent Line · chafed · Feb 16, 2008 · N15555 · Emb EMB145LR · Fuel Storage
  > FLT 0119 - ONT - MX PERSONNEL REPORTED LT WING FUEL PANEL LEAKING. MX PERSONNEL REMOVED AND REPLACED VENT VALVE LINE, OPERATIONALLY & LEAK CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE.
- [SDR C2XA08SH001](https://openairdocs.org/sdr/C2XA08SH001.md): Striker · corroded · Jan 15, 2008 · N15555 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK CARGO DOOR CUTOUT LINER DOOR STRIKER PLATE HAS CORROSION ON 2 SIDE. MX REPAIRED CARGO DOOR CUTOUT LINER DOOR STRIKER PLATE AT FR 65 IAW EC 5330-01767. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA07ON034](https://openairdocs.org/sdr/C2XA07ON034.md): Smoke Detector · inoperative · Dec 5, 2007 · N15555 · Emb EMB145LR · Smoke Detection
  > FLT 0108 - ONT TO BOI - DURING FLIGHT, FLIGHT CREW REPORTED BAG SMOKE MESSAGE DID NOT APPEAR ON EICAS. MX AT LAX REMOVED AND REPLACED NR 1 BAGGAGE BIN SMOKE DETECTOR, OPERATIONALLY CHECK GOOD AND A/C WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.
- [SDR C2XA07ON015](https://openairdocs.org/sdr/C2XA07ON015.md): Flapper Valve · worn · Jul 30, 2007 · N15555 · Emb EMB145LR · Fuel Transfer Valve
  > FLT 41 - GEG TO ONT - PASSENGER REPORTED STREAM OF FUEL COMING FROM LEFT WING. MX PERSONNEL INSPECTED THE LEFT WING FLAPPER VALVE LEAKING. MX REMOVED AND REPLACED LEFT WING FLAPPER VALVE AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. THE A/C WAS APPROVED TO
- [SDR C2XA07ON011](https://openairdocs.org/sdr/C2XA07ON011.md): Valve · leaking · Jul 15, 2007 · N15555 · Emb EMB145LR · Fuel Transfer Valve
  > FLT 403 - BOI TO BOI - AFTER TAKEOFF FROM BOI TOWER ADVISED FUEL LEAKING FROM LEFT WING, RETURNED TO BOI. FUEL FOUND ON UPPER AND LOWER SURFACE OF LEFT WING. MX DISPATCHED MX CREW TO BOI AND INSPECTED AND FOUND LEFT VENT VALVE LEAKING. MX REMOVED AND REPLAC
- [SDR C2XA07CL037](https://openairdocs.org/sdr/C2XA07CL037.md): Wire Harness · shorted · Apr 8, 2007 · N15555 · Emb EMB145LR · Landing Gear System Wiring
  > CLE FLIGHT 2133 - THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT UNTIL THE DOWNLOCK RELEASE WAS USED ON THE LGEU. MAINTENANCE INSPECTED AND REPLACED THE LEFT WOW PROXIMITY SENSOR HARNESS. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07CL031](https://openairdocs.org/sdr/C2XA07CL031.md): Relay · faulty · Mar 15, 2007 · N15555 · Emb EMB145LR · Landing Gear Door Retract Section
  > CLE FLIGHT 2736 THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT RETRACT AFTER TAKEOFFF. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR SEQUENCE DOOR RELAY KO642. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07IA031](https://openairdocs.org/sdr/C2XA07IA031.md): Light · inoperative · Feb 11, 2007 · N15555 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI
- [SDR C2XA06IA162](https://openairdocs.org/sdr/C2XA06IA162.md): Electronic Unit · inoperative · Oct 18, 2006 · N15555 · Emb EMB145LR · Landing Gear Retraction/Extension System
  > BPT - FLIGHT 3059, THE CREW REPORTED AN AIR GROUND FAILURE ON CLIMB, AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO BPT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LAND GEAR ELECTRONIC UN
- [SDR C2XA06CL082](https://openairdocs.org/sdr/C2XA06CL082.md): Circuit Breaker · tripped · Sep 30, 2006 · N15555 · Emb EMB145LR · Landing Gear System Wiring
  > CLE FLIGHT NR 2783, CREW REPORTED THAT AFTER TAKEOFF FROM GRR THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CREW PRESSED RED DOWNLOCK RELEASE AND THE GEAR RETRACTED NORMALLY. AIRCRAFT LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FO
- [SDR C2XA06SH013](https://openairdocs.org/sdr/C2XA06SH013.md): Firewall · chafed · Feb 3, 2006 · N15555 · Emb EMB145LR · APU Cowling/Containment
  > SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5310-01359 SECTION 1.2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH014](https://openairdocs.org/sdr/C2XA06SH014.md): Floor Support · corroded · Feb 3, 2006 · N15555 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05BT062](https://openairdocs.org/sdr/C2XA05BT062.md): Sensor · faulty · Aug 20, 2005 · N15555 · Emb EMB145LR · Landing Gear Position and Warning
  > CREW REPORTED, "LANDING GEAR AIR/GROUND FAIL AFTER TAKEOFF, GEAR WOULD NOT RETRACT." MAINTENANCE REMOVED AND REPLACED THE LEFT TRAILING ARM PROXIMITY SWITCH IAW EMB145 MM NR 32-63-01. OPS CHECKED OF LANDING GEAR AIR/GROUND SYSTEM AND LANDING GEAR SWING GOOD
- [SDR C2XA04SH231](https://openairdocs.org/sdr/C2XA04SH231.md): Skin · gouged · Apr 17, 2004 · N15555 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV- DURING C-CHECK THE EXTERIOR SKIN WAS FOUND TO BE GOUGED AT FRAME 11 BETWEEN STRINGERS 20L AND 21L. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 53-10-01, STEP 6 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER
- [SDR C2XA04SH229](https://openairdocs.org/sdr/C2XA04SH229.md): Sill · corroded · Apr 15, 2004 · N15555 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N15555-2023-10-05/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 = 'N15555' AND deregistration_id = 'N15555-2023-10-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N15555-2023-10-05/reports

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