# Service difficulty reports: N26549 A list on [N26549](https://openairdocs.org/aircraft/N26549.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 · 54 reports - [SDR ASOA2018101654055](https://openairdocs.org/sdr/ASOA2018101654055.md): Floor Support · not reported · Oct 15, 2018 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > IAH- MAINTENANCE REMOVED AND REPLACED A REPAIR DOUBLER ON THE CENTER OMEGA BEAM BETWEEN FR 60-61 IAW TECHNICAL DISPOSITION ETD2018-145-107152. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA2018101654054](https://openairdocs.org/sdr/ASOA2018101654054.md): Doubler · dented · Oct 15, 2018 · N26549 · Emb EMB145LR · Fuselage Main, Plate/Skin > IAH- MAINTENANCE REMOVED AND REPLACED A REPAIR DOUBLER BETWEEN FR2-4 STRINGERS 9R-13R IAW SRM 53-10-01. AIRCRAFT RETURNED TO SERVICE. - [SDR ASOA201803267041](https://openairdocs.org/sdr/ASOA201803267041.md): Proximity Switch · broken · Mar 26, 2018 · N26549 · Emb EMB145LR · Landing Gear Position and Warning > AFTER TAKEOFF, THE LANDING GEAR WOULDN'T RETRACT. RETURNED TO DEPARTURE. FOUND A BAD PROXIMITY SWITCH. REPLACED THE PROXIMITY SWITCH IAW WITH WO:542630. PERFORMED GEAR RETRACTIONS AND WAS RELEASED BACK TO SERVICE. - [SDR ASOA20180317012](https://openairdocs.org/sdr/ASOA20180317012.md): Display · faulty · Mar 17, 2018 · N26549 · Emb EMB145LR · Central Display > THE CREW REPORTED STRONG ODOR IN COCKPIT. MAINTENANCE INSPECTED AND FOUND THE ODOR TO BE COMING FROM THE CAPTAIN`S MFD. THE MFD WAS REPALCED AND OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR ASOA201702123007](https://openairdocs.org/sdr/ASOA201702123007.md): Control Unit · malfunctioned · Feb 12, 2017 · N26549 · Emb EMB145LR · Rudder Control System > THE CREW REPORTED A RUDDER OVERBOOST MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RUDDER POWER CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. - [SDR ASOA201610293063](https://openairdocs.org/sdr/ASOA201610293063.md): Battery · inoperative · Oct 29, 2016 · N26549 · Emb EMB145LR · Emergency Lighting > EMERGENCY LIGHTS IN GALLEY INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD. - [SDR ASOA20160602032](https://openairdocs.org/sdr/ASOA20160602032.md): Floor Support · corroded · Jun 2, 2016 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 60-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-24-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140822095](https://openairdocs.org/sdr/ASOA20140822095.md): Valve · stuck · Aug 22, 2014 · N26549 · Emb EMB145LR · Cabin Pressure Control System > ACFT WAS BEING VECTORED WHEN THE PRESSURIZATION BECAME ERRATIC, COULDN'T GET IT UNDER CONTROL MANUALLY AND FINALLY PRESSURIZATION DEPRESSURIZED AT 5000 FEET. ACFT LANDED AND MAINTENANCE, R THE ELECTROMAGNETIC OUTFLOW VALVE IAW AMM 21-31-03; IPC 21-30-00, FIGUR - [SDR ASOA20140706079](https://openairdocs.org/sdr/ASOA20140706079.md): Fan · failed · Jul 6, 2014 · N26549 · Emb EMB145LR · Air Distribution Fan > PILOT REPORTED AFTER TAKE OFF AND GEAR RETRACTION, A STRANGE ODOR PERCEIVED IN THE FLIGHT DECK. MX PERFORMED AN OPS CHECK OF APU BLEED SYS AND PERFORMED A GVI OF FWD AVIONICS BAY FOR ODOR AND ABNORMALITIES. NO DEFECTS NOTED. AN ASSOCIATED ELECTRONIC BAY EXA - [SDR ASOA20140704050](https://openairdocs.org/sdr/ASOA20140704050.md): Fuse · blown · Jul 4, 2014 · N26549 · Emb EMB145 · Emergency Lighting > DURING ROUTINE MAINTENANCE, THE LT FORWARD EXTERNAL EMERGENCY AISLE LIGHT, AND COCKPIT FLOODLIGHT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE FUSE ON THE NR 1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKED GOOD. - [SDR ASOA20140517075](https://openairdocs.org/sdr/ASOA20140517075.md): Flange · cracked · May 16, 2014 · N26549 · Emb EMB145LR · Rudder Structure > DURING C-CHECK, THE RUDDER II UPPER ATTACHMENT POINT NUTPLATE FLANGE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FLANGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130326045H](https://openairdocs.org/sdr/ASOA20130326045H.md): Battery Pack · inoperative · Mar 26, 2013 · N26549 · Emb EMB145LR · Emergency Lighting > DURING MX INSPECTION THE FORWARD LT EXTERNAL EMERGENCY LIGHT AND FWD CABIN CEILING LIGHT WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY, OP TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201111211002](https://openairdocs.org/sdr/ASOA201111211002.md): Detection Sys · malfunctioned · Nov 21, 2011 · N26549 · Emb EMB145LR · Central Warning > DURING CLIMB THE EICAS DISPLAY INDICATED A SYS NR 1 BLEED AIR LEAK. THE ACFT RETURNED AND LANDED AT WITHOUT INCIDENT WHERE MX PERFORMED TROUBLESHOOTING, PERFORMING SYS OPS CHECKS, HOWEVER THE CONDITION COULD NOT BE DUPLICATED, NOR DID THE WARNING INDICATION IL - [SDR C2XA11RI152](https://openairdocs.org/sdr/C2XA11RI152.md): Control Unit · faulty · Sep 17, 2011 · N26549 · Emb EMB145LR · Stabilizer Control System > AFTER TAKEOFF, DURING CLIMB THE CREW REPORTED MAIN PITCH INOP WARNING ON EICAS. CREW PERFORMED AIR RETURN BACK TO IAD. IAD MX REMOVED AND REPLACED HORIZONTAL STABLIZER CONTROL UNIT IAW EMB145 AMM 27-40-01 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT - [SDR C2XA11CL150](https://openairdocs.org/sdr/C2XA11CL150.md): Fire Loop · chafed · Jun 21, 2011 · N26549 · Emb EMB145LR · Fire Detection > ORF FLT 5867 THE CREW REPORTED A ENGINE FIRE DETECT FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE LOOP. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11RI014](https://openairdocs.org/sdr/C2XA11RI014.md): O-Ring · worn · Jan 30, 2011 · N26549 · Emb EMB145LR · Pneumatic Distribution System > FLIGHT 4936 - JAX - FLIGHT CREW REPORTED NR 1 BLEED LEAK ON CLIMB. CREW PERFORMED AIR RETURN AND LANDED SAFELY. MX REMOVED AND REPLACED SEVERAL O-RINGS FWD OF LAV NR 1 BLEED SIDE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO S - [SDR C2XA10TY123](https://openairdocs.org/sdr/C2XA10TY123.md): Engine · malfunctioned · Sep 9, 2010 · N26549 · Emb EMB145LR · Engine (Turbine/Turboprop) > TYS - IN BNA THE CREW EXPERIENCED A FUNNY SMELL AND VIBES AT 5000 FEET ON DESCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE AND WILL BE RELEASED AT THE END OF THE CHANGE AND OPS CHECKS. - [SDR C2XA10IA234](https://openairdocs.org/sdr/C2XA10IA234.md): Smoke Detector · malfunctioned · Aug 18, 2010 · N26549 · Emb EMB145LR · Smoke Detection > IAH - FLIGHT 2493, DURING CLIMB THE CREW REPORTED THAT THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT S - [SDR C2XA10IA233](https://openairdocs.org/sdr/C2XA10IA233.md): Smoke Detector · false activation · Aug 18, 2010 · N26549 · Emb EMB145LR · Smoke Detection > IAH - FLIGHT 2493, DURING CLIMB THE CREW REPORTED THAT THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT S - [SDR C2XA10SH260](https://openairdocs.org/sdr/C2XA10SH260.md): Frame · cracked · Aug 9, 2010 · N26549 · Emb EMB145LR · Fuselage Main, Frame > SHV - DURING C-CHECK THE RT FRAME 10 SEGMENT AT STRINGER 10R WAS FOUND TO BE CRACKED DIRECTLY BELOW THE F/O DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH259](https://openairdocs.org/sdr/C2XA10SH259.md): Frame · cracked · Aug 9, 2010 · N26549 · Emb EMB145LR · Fuselage Main, Frame > SHV - DURING C-CHECK LT FRAME 10 WAS FOUND TO BE CRACKED AT STRINGER 10L DIRECTLY BELOW THE PILOT DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH258](https://openairdocs.org/sdr/C2XA10SH258.md): Floor Support · corroded · Aug 9, 2010 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA210](https://openairdocs.org/sdr/C2XA09IA210.md): Windshield · cracked · Aug 22, 2009 · N26549 · Emb EMB145LR · Flight Compartment Windows > IAH - FLIGHT 2550, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD SHATTERED ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS N - [SDR C2XA09TY120](https://openairdocs.org/sdr/C2XA09TY120.md): Fastener · loose · Jun 19, 2009 · N26549 · Emb EMB145XR · Engine Mount Section > NR 2 ENGINE FWD MOUNT YOKE O/B PLATE HAS SEVERAL LOOSE FASTENERS. REMOVED AND REPLACED 13 LOOSE JO-BOLTS IAW EMB 145 SRM 51-40-02. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA09RI006](https://openairdocs.org/sdr/C2XA09RI006.md): Inverter · inoperative · Jan 5, 2009 · N26549 · Emb EMB145LR · Emergency Lighting > FLIGHT CREW REPORTED EMERGENCY LIGHT STRIP ROW 8 TO 12 INOPERATIVE. MX REMOVED AND REPLACED AC INVERTER AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA08IA255](https://openairdocs.org/sdr/C2XA08IA255.md): Light · malfunctioned · Dec 15, 2008 · N26549 · Emb EMB145LR · Emergency Lighting > IAH - DURING A-CK INSPECTION THE EMERGENCY LIGHT STRIPS BETWEEN ROWS 8 & 9 WERE FOUND TO BE INOPERATIVE. MX INSPECTED THE LIGHTING SYSTEM, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE - [SDR C2XA08TY116](https://openairdocs.org/sdr/C2XA08TY116.md): Stringer · torn · Oct 5, 2008 · N26549 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > A/C WAS GROUND DAMAGED IN JAX AND FERRY FLOWN TO TYS FOR REPAIR. STR 21L AT FRM 66 WAS FOUND TORN. THE DAMAGED SECTION OF STR 21L AT FRM 64-68 WAS REMOVED AND A NEW SECTION WAS CUT AND DRILLED. THE NEW SECTION OF STR 21L AND STR SPLICE AT FRAMES 61-62 WERE - [SDR C2XA08TY114](https://openairdocs.org/sdr/C2XA08TY114.md): Stringer · torn · Oct 5, 2008 · N26549 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > A/C WAS GROUND DAMAGED IN JAX AND FERRY FLOWN TO TYS FOR REPAIR. STR 19L AT FRM 66 WAS FOUND TORN. THE DAMAGED SECTION OF STR 19L FRM 67 TO FRM 61 WAS REMOVED AND A NEW SECTION WAS CUT AND DRILLED. FWD SECTION OF STR 19L AND STR SPLICE AT FRM`S 66-67 WERE I - [SDR C2XA08ON173](https://openairdocs.org/sdr/C2XA08ON173.md): Handle · out of adjust · Aug 23, 2008 · N26549 · Emb EMB145LR · Doors > FLT 0053 RNO FLIGHT CREW REPORTED AFTER LANDING IN RNO PAX DOOR DIFFICULT TO OPEN FROM INSIDE. REPO ACFT 188 ONT RNO TO COVER FLIGHT 53 AND ROUTE MECHANICS AND PARTS TO REPAIR 549. MX PERSONNEL ADJUSTED PAX DOOR INTERNAL HANDLE. OPS CHECK SATISFACTORY AND A - [SDR C2XA08TY066](https://openairdocs.org/sdr/C2XA08TY066.md): Light · inoperative · Jun 18, 2008 · N26549 · Emb EMB145LR · Emergency Lighting > EMERGENCY LIGHT FLOOR STRIP WILL NOT ILLUMINATE BETWEEN ROWS 8A AND 10A. REMOVED AND REPLACED EMERGENCY LIGHT FLOOR STRIP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. (S) - [SDR C2XA08TY047](https://openairdocs.org/sdr/C2XA08TY047.md): Light · inoperative · Apr 29, 2008 · N26549 · Emb EMB145LR · Emergency Lighting > SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB ON SERVICE DOOR IAW EMB 145AMM 33-50-10, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA08SH005](https://openairdocs.org/sdr/C2XA08SH005.md): Floor Support · corroded · Jan 16, 2008 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION AT FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA08SH004](https://openairdocs.org/sdr/C2XA08SH004.md): Skin · corroded · Jan 16, 2008 · N26549 · Emb EMB145LR · Horizontal Stabilizer, Plate/Skin > SHV - DURING C-CHECK RIGHT HORIZONTAL STAB L/E HAS PITTING CORROSION. MX REPAIRED RIGHT HORIZONTAL L/E IAW EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA08SH003](https://openairdocs.org/sdr/C2XA08SH003.md): Attach Bracket · damaged · Jan 16, 2008 · N26549 · Emb EMB145LR · Ailerons > SHV - DURING C-CHECK LEFT WING AILERON HAS EXCESSIVE PLAY AT PCA RODS AND MIGRATED HAT BUSHING AT ATTACHMENT LUG. MX REMOVED AND REPLACED LEFT AILERON PCA BRACKET IAW EMB 145 SRM 51-40-02 & EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA08SH002](https://openairdocs.org/sdr/C2XA08SH002.md): Door Frame · corroded · Jan 16, 2008 · N26549 · Emb EMB145LR · Doors > SHV - DURING C-CHECK MAIN DOOR LOWER FRAME HAVE CORROSION AROUND NUT PLATE HOLES. MX REPAIRED MAIN DOOR LOWER FRAME IAW EMB 145 EC 5210-01154. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA07CL007](https://openairdocs.org/sdr/C2XA07CL007.md): Static Port · inoperative · Jan 13, 2007 · N26549 · Emb EMB145LR · Pitot/Static System > CLE FLIGHT 2061 THE CREW REPORTED A PITOT NR 2 INOPERATIVE MESSAGE ON THE ECIAS WITH A BURNING SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 STATIC PORT ASSEMBLY. OPERATIONAL CHE - [SDR C2XA06IA108](https://openairdocs.org/sdr/C2XA06IA108.md): Heater · odor · Jul 8, 2006 · N26549 · Emb EMB145LR · Windshield/Door Rain/Ice Removal > IAH - FLIGHT 2392, THE CREW REPORTED AN ACRID ODOR IN THE COCKPIT DURING APPROACH INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE PACKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR - [SDR C2XA06SH006](https://openairdocs.org/sdr/C2XA06SH006.md): Beam · corroded · Jan 23, 2006 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV-DURING C CHECK THE BAGGAGE DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA05CL048](https://openairdocs.org/sdr/C2XA05CL048.md): Engine · failed · Jun 16, 2005 · N26549 · Emb EMB145LR · Engine (Turbine/Turboprop) > CLE FLIGHT 2668 THE CREW REPORTED A LOUD BANG FOLLOWED BY NR 1 ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA04IA055](https://openairdocs.org/sdr/C2XA04IA055.md): Fuel Nozzle · faulty · May 25, 2004 · N26549 · Emb EMB145LR · Fuel Injector Nozzle > CREW REPORTED THAT THERE WERE FUMES IN THE CABIN AND COCKPIT DURING ANTI-ICE OPERATION. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. THE ENGINES WERE RUN AND THE ANTI-ICE SYSTEM OPERATED WITH NO FURTHER SMELL NOTED. THE DISCREPANCY WAS THE - [SDR C2XA04SH145](https://openairdocs.org/sdr/C2XA04SH145.md): Rib · gouged · Mar 8, 2004 · N26549 · Emb EMB145LR · Nacelle/Pylon, Frame/Spar/Rib > SHV - DURING C-CHECK THE LEFT UPPER COWLING OUTBOARD REINFORCEMENT ANGLE WAS FOUND TO BE GOUGED BETWEEN STATION XN 2355 AND XN 3168. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR R - [SDR C2XA04SH142](https://openairdocs.org/sdr/C2XA04SH142.md): Floorbeam · corroded · Mar 4, 2004 · N26549 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH141](https://openairdocs.org/sdr/C2XA04SH141.md): Sill · corroded · Mar 4, 2004 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH143](https://openairdocs.org/sdr/C2XA04SH143.md): Firewall · cracked · Mar 4, 2004 · N26549 · Emb EMB145LR · APU Cowling/Containment > SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER END OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 6, FIGURE 205. THE AIRCRAFT WAS APPROVED FO - [SDR C2XA04SH140](https://openairdocs.org/sdr/C2XA04SH140.md): Buttstrap · corroded · Mar 4, 2004 · N26549 · Emb EMB145LR · Fuselage Main, Structure > SHV - DURING C-CHECK, THE L-BRACKET AFT OF THE CENTER BUTTSTRAP AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH138](https://openairdocs.org/sdr/C2XA04SH138.md): Firewall · cracked · Mar 3, 2004 · N26549 · Emb EMB145LR · Fuselage Main, Bulkhead > SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH137](https://openairdocs.org/sdr/C2XA04SH137.md): Stiffener · chafed · Mar 3, 2004 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH135](https://openairdocs.org/sdr/C2XA04SH135.md): Firewall · cracked · Mar 2, 2004 · N26549 · Emb EMB145LR · Fuselage Main, Bulkhead > SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND UPPER APU SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH134](https://openairdocs.org/sdr/C2XA04SH134.md): Doubler · corroded · Mar 2, 2004 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- DURING C-CHECK THE RIGHT HAND FORWARD OMEGA BEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH133](https://openairdocs.org/sdr/C2XA04SH133.md): Crossbeam · corroded · Mar 2, 2004 · N26549 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 23 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV Next page: https://openairdocs.org/aircraft/N26549/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 = 'N26549' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N26549/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.