# Service difficulty reports: N276SK, cancelled Feb 22, 2023 A list on [N276SK, cancelled Feb 22, 2023](https://openairdocs.org/deregistered/N276SK-2023-02-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 4VAA20211216003](https://openairdocs.org/sdr/4VAA20211216003.md): Inverter · failed · Dec 16, 2021 · N276SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS THREE AND FOUR. MAINTENANCE REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS FAILED. MAINTENANCE THEN REPLACED THE NUMBER 3 INVERTER. OPERATIONAL CHECKS WERE GOOD WIT - [SDR 4VAA202111190002](https://openairdocs.org/sdr/4VAA202111190002.md): None · none · Nov 19, 2021 · N276SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INTERMITTENTLY INOPERATIVE IN THE FRONT SECTION OF THE AIRCRAFT. A LOOSE CONNECTOR WAS RESECURED AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. *NOTE* THE FINAL CORRECTIVE ACTION I - [SDR UHLA201607140363](https://openairdocs.org/sdr/UHLA201607140363.md): Stop · inoperative · Jul 14, 2016 · N276SK · Emb EMB145LR · Passenger/Crew Doors > MAIN ENTRY DOOR STEPS WILL NOT DEPLOY. R & R MAIN DOOR FOLD OUT BACK STOP IAW AMM 52-13-02. OPS TEST GOOD. - [SDR UHLA201605140239](https://openairdocs.org/sdr/UHLA201605140239.md): Control Panel · malfunctioned · May 14, 2016 · N276SK · Emb EMB145LR · Emergency Lighting > SIDE WALL LIGHT BUTTON TURNS ON EMERGENCY LIGHTS. R & R ATTENDANT CONTROL PANEL IAW AMM 25-27-09. OPS CHECK GOOD. - [SDR UHLA2015020100068](https://openairdocs.org/sdr/UHLA2015020100068.md): Seat Track · corroded · Feb 1, 2015 · N276SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > DURING INSPECTION, THE INBD AND OTBD FLOOR FLANGES WERE FOUND TO BE CORRODED ON THE CAPTAINS SEAT TRACK LOCATIONS. THE FLANGES WERE REPAIRED IAW ETD 2015-145-010166. - [SDR UHLA2015020100067](https://openairdocs.org/sdr/UHLA2015020100067.md): Floor Support · corroded · Feb 1, 2015 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE COCKPIT INBD AND OTBD FLOOR FLANGES WERE FOUND TO BE CORRODED ON THE F/O SEAT TRACKS. THE INBD AND OTBD FLOOR FLANGES WERE REPAIRED IAW ETD 2015-145-010166. - [SDR UHLA2015012300070](https://openairdocs.org/sdr/UHLA2015012300070.md): Attach Fitting · corroded · Jan 23, 2015 · N276SK · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD PASSENGER DOOR ATTACH FITTING BELOW THE HINGE ARM. THE ATTACH FITTING WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-008649. - [SDR UHLA2015012200069](https://openairdocs.org/sdr/UHLA2015012200069.md): Structure · corroded · Jan 22, 2015 · N276SK · Emb EMB145LR · Cargo/Baggage Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR BOTTOM SIDE STRUCTURE, THE STRUCTURE WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015012200066](https://openairdocs.org/sdr/UHLA2015012200066.md): Attach Angle · cracked · Jan 22, 2015 · N276SK · Emb EMB145LR · Fuselage Main, Attach Fittings > DURING INSPECTION, THE ATTACH ANGLE ON THE FORWARD SIDE OF THE APU FIREWALL WAS FOUND TO BE CRACKED AT FRAME 80 AND STRINGERS 5R-7R. THE ATTACH ANGLE WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015012200065](https://openairdocs.org/sdr/UHLA2015012200065.md): Attach Angle · cracked · Jan 22, 2015 · N276SK · Emb EMB145LR · Fuselage Main, Attach Fittings > DURING INSPECTION, THE ATTACH ANGLE ON THE FORWARD SIDE OF THE APU FIREWALL WAS FOUND TO BE CRACKED AT FRAME 80 AND STRINGERS 5L-7L. THE ATTACH ANGLE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140705207](https://openairdocs.org/sdr/CHQA20140705207.md): Pump · leaking · Jul 5, 2014 · N276SK · Emb EMB145LR · Hydraulic Pump (Electric/Engine), Main > CREW REPORTED THAT THEY RECEIVED A HYD 1 LOW QTY MSG FOLLOWED BY A HYD SYS 1 FAIL MSG. THE CREW PERFORMED A MANUAL EXTENSION ON THE LG. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE HYD SYS 1 ENG DRIVEN PUMP & PERFORMED THE LG FREE FALL CHECK. - [SDR CHQA20140306082](https://openairdocs.org/sdr/CHQA20140306082.md): Floor Support · corroded · Mar 6, 2014 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE FRAME WAS REPAIRED IAW SRM 53-0010 & SRM 51-40-02. - [SDR CHQA20140306081](https://openairdocs.org/sdr/CHQA20140306081.md): Floor Support · corroded · Mar 6, 2014 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 23. THE LT OMEGA BEAM WAS REPAIRED IAW ETD 2014-145-014567. - [SDR CHQA20140306080](https://openairdocs.org/sdr/CHQA20140306080.md): Service Door · corroded · Mar 6, 2014 · N276SK · Emb EMB145LR · Service Doors > DURING INSPECTION THE SERVICE DOOR BOTTOM STRUCTURE ATTACHMENT FOR THE LINER NUT PLATE AREAS WAS FOUND TO BE CORRODED. THE SERVICE DOOR WAS REPAIRED IAW ETD 2014-145-019393-A. - [SDR CHQA20131016371](https://openairdocs.org/sdr/CHQA20131016371.md): Switch · faulty · Oct 16, 2013 · N276SK · Emb EMB145LR · Pneumatic Distribution System > CREW REPORTED THAT THEY RECEIVED A "BLEED 2 VALVE CLOSED" MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED SYSTEM 2 PUSH BUTTON. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130706260](https://openairdocs.org/sdr/CHQA20130706260.md): Wire Harness · inoperative · Jul 6, 2013 · N276SK · Emb EMB145LR · Light System Wiring > DURING INSPECTION, EMERGENCY LIGHT ON MAIN ENTRY DOOR HANDRAIL WAS FOUND TO BE INOPERATIVE. MX REPLACED THE CAUTION INDICATION HARNESS OPS CHECKED GOOD. - [SDR CHQA20130208046](https://openairdocs.org/sdr/CHQA20130208046.md): Display · inoperative · Feb 8, 2013 · N276SK · Emb EMB145LR · Central Display > CREW REPORTED THE PRIMARY FLIGHT DISPLAY NUMBER 1 FAILED IN FLIGHT WITH AN ELECTRICAL ODOR PRESENT IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED THE NUMBER 1 PRIMARY FLIGHT DISPLAY WITH NUMBER 2 MULTI-FUNCTION DISPLAY AND - [SDR CHQA20121207475](https://openairdocs.org/sdr/CHQA20121207475.md): Beam · corroded · Dec 7, 2012 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT THRESHOLD BEAM. THE THRESHOLD BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20121207474](https://openairdocs.org/sdr/CHQA20121207474.md): Threshold · corroded · Dec 7, 2012 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR THRESHOLD BEAM AT THE SCREW HOLES. THE SERVICE DOOR THRESHOLD WAS REPLACED IN ACCORDANCE WITH SRM 53-21-02. - [SDR CHQA20121207473](https://openairdocs.org/sdr/CHQA20121207473.md): Gusset · corroded · Dec 7, 2012 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT RIGHT OMEGA FRAME 61. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND SRM 51-20-03. - [SDR CHQA20121207472](https://openairdocs.org/sdr/CHQA20121207472.md): Gusset · corroded · Dec 7, 2012 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT LEFT OMEGA FRAME 59. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20121207471](https://openairdocs.org/sdr/CHQA20121207471.md): Sill · corroded · Dec 7, 2012 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SILL AT FRAME 20 TO FRAME 21. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-00. - [SDR CHQA20121207470](https://openairdocs.org/sdr/CHQA20121207470.md): Angle · corroded · Dec 7, 2012 · N276SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RAMP ANGLE FRAME 20 AT THE CENTER OMEGA BEAM. THE ANGLE AT FRAME 20 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-03. - [SDR CHQA20120801229](https://openairdocs.org/sdr/CHQA20120801229.md): Pressure Switch · faulty · Aug 1, 2012 · N276SK · Emb EMB145LR · Rudder Control System > CREW REPORTED THAT DURING CLIMBOUT, AT 10,000 FEET, THEY RECEIVED A RUDDER SYSTEMS 1/2 INOP MESSAGE, AUTO-PILOT FAIL, AND YAW DAMPER FAIL MESSAGES. THE CREW FURTHER REPORTED THAT THE AUTO-PILOT FAIL AND YAW DAMPER FAIL MESSAGES CLEARED WHILE THE RUDDER SYS 1/ - [SDR CHQA20120801228](https://openairdocs.org/sdr/CHQA20120801228.md): Pressure Switch · faulty · Aug 1, 2012 · N276SK · Emb EMB145LR · Rudder Control System > CREW REPORTED THAT DURING CLIMBOUT, AT 10,000 FEET, RECEIVED A RUDDER SYSTEMS 1/2 INOP MESSAGE, AUTO-PILOT FAIL, AND YAW DAMPER FAIL MESSAGES. THE CREW FURTHER REPORTED THAT THE AUTO-PILOT FAIL AND YAW DAMPER FAIL MESSAGES CLEARED WHILE THE RUDDER SYSTEM 1/2 - [SDR CHQA201100286](https://openairdocs.org/sdr/CHQA201100286.md): Carbon Seal · leaking · Jul 24, 2011 · N276SK · Emb EMB145LR · Turbine Engine Oil System > CREW REPORTED THAT DURING TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT. THE CREW ABORTED TAKE-OFF AND REPORTED THAT THEY RECEIVED NO FIRE INDICATIONS AND ALL ENGINE INDICATIONS WERE GOOD. AS SOON AS THE TAKEOFF WAS ABORTED THE SMOKE BEGAN TO CLEAR. MAIN - [SDR CHQA201100046](https://openairdocs.org/sdr/CHQA201100046.md): Light · inoperative · Feb 24, 2011 · N276SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000113](https://openairdocs.org/sdr/CHQA201000113.md): Unknown · malfunctioned · Jun 3, 2010 · N276SK · Emb EMB145LR · Landing Gear Retraction/Extension System > AFTER TAKEOFF, CREW ATTEMPTED TO RETRACT LANDING GEAR, RECEIVED A LDG AIR/GND FAIL MESSAGE ON EICAS AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE AIRCRAFT ON JACKS AND CYCLED THE LANDING GE - [SDR CHQA201000081](https://openairdocs.org/sdr/CHQA201000081.md): Solenoid Valve · faulty · Apr 16, 2010 · N276SK · Emb EMB145LR · Landing Gear Door Retract Section > CREW REPORTED THAT DURING CLIMBOUT A VIBRATION AND LOW RUMBLE COULD BE HEARD AND FELT. AFTER LEVELING OFF, THE AIRCRAFT WOULD NOT ACCELERATE PAST 0.70 MACH IN CLIMB MODE. THE AIRCRAFT DIVERTED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOS - [SDR CHQA200900261](https://openairdocs.org/sdr/CHQA200900261.md): Battery Pack · discharged · Dec 11, 2009 · N276SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT AND THE NR 4 BATTERY PACK WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA200900148](https://openairdocs.org/sdr/CHQA200900148.md): Battery Pack · discharged · Jun 28, 2009 · N276SK · Emb EMB145LR · Emergency Lighting > DURING INSP, THE LT AND RT OVER-WING EMERGENCY EXTERIOR LIGHTS WERE FOUND TO BE INOP. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND THE EXTERIOR LIGHTS OPERATED NORMALLY. - [SDR CHQA200900114](https://openairdocs.org/sdr/CHQA200900114.md): Wire · broken · Apr 25, 2009 · N276SK · Emb EMB145LR · Door System Wiring > FLIGHT 7822, IAD TO IND - SHORTLY AFTER TAKEOFF, AT APPROXIMATELY 400 FT THE CREW RECEIVED A SERVICE DOOR OPEN EICAS MESSAGE. THE QRH CHECKLIST WAS COMPLETED AND IT WAS DECIDED TO RETURN TO IAD WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. THE SERVICE DOOR IND - [SDR CHQA200900017](https://openairdocs.org/sdr/CHQA200900017.md): Battery Pack · inoperative · Jan 13, 2009 · N276SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE INOP ON THE LEFT AND RIGHT SIDES. THE NR 3 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY. - [SDR CHQA200700029](https://openairdocs.org/sdr/CHQA200700029.md): Flap System · malfunctioned · Jun 20, 2007 · N276SK · Emb EMB145LR · Trailing Edge Flap Control System > FLIGHT 3438 - ATL-CLE - ON DESCENT WHEN FLAPS SELECTED TO 9, EICAS MESSAGES SPS ADV AND FLAP FAIL APPEARED. PERFORMED THE QRH AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE RESET FLAPS AND CYCLED THROUGH, OPS CHECK GOOD. - [SDR CHQA200600119](https://openairdocs.org/sdr/CHQA200600119.md): Inverter · inoperative · Sep 14, 2006 · N276SK · Emb EMB145LR · Emergency Lighting > FLOOR PROXIMITY LIGHT NR 2 AND NR 2 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW MM 33-50-00. OPS CHECK GOOD. - [SDR CHQA200600114](https://openairdocs.org/sdr/CHQA200600114.md): Bulb · burned out · Sep 1, 2006 · N276SK · Emb EMB145LR · Emergency Lighting > NR 1 EMERGENCY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT IAW MM 33-26-06. - [SDR CHQA200600112](https://openairdocs.org/sdr/CHQA200600112.md): Battery · inoperative · Aug 30, 2006 · N276SK · Emb EMB145LR · Emergency Lighting > EMERGENCY LIGHTING PROXIMITY STRIPS 2 AND 3 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB 145 MM 33-50-06. OPS CHECK GOOD. - [SDR CHQA200600091](https://openairdocs.org/sdr/CHQA200600091.md): Windshield · malfunctioned · Jul 25, 2006 · N276SK · Emb EMB145LR · Flight Compartment Windows > DURING DESCENT THROUGH FL200, THERE WAS A THIN CLOUD LAYER WITH ICING CONDITIONS. HEARD WHAT SOUNDED LIKE WATER DROPLETS SIZZLING. THEN SMELLED ELECTRICAL SMOKE AND AFTER A FEW SECONDS, SAW SMOKE COMING FROM THE FRONT OF THE GLARESHIELD WHERE THE HEATING ELEM - [SDR CHQA200500215](https://openairdocs.org/sdr/CHQA200500215.md): Hub Cap · missing · Dec 20, 2005 · N276SK · Emb EMB145LR · Wheel/Ski/Float > FLIGHT 900 - LAN-OKC - DURING INITIAL CLIMBOUT, RETRACTED GEAR DURING NORMAL SCHEDULE. RIGHT MAIN SHOWED IN TRANSITION (AMBER BOX) FOR APPROXIMATELY 10 SECONDS, THEN WENT TO RED. RAN QRH, RECYCLED GEAR PER QRH. WHILE PUTTING GEAR IN THE UP POSITION AGAIN, S - [SDR CHQA200500171](https://openairdocs.org/sdr/CHQA200500171.md): Odor · detected · Oct 1, 2005 · N276SK · Emb EMB145LR · Air Distribution System > FLIGHT 6320 - FLL-MCO - ON FINAL APPROACH, NOTICED SMOKE AND AN ODOR OF SMOKE. THE ELECTRIC PAGE INDICATED GEN 3 AMP 105. PERFORMED GENERAL VISUAL INSPECTION OF COMPONENTS IN THE FORWARD AVIONICS BAY. NO BURNS OR ODOR OF SMOKE. RAN BOTH ENGINES FOR 20 MINUT - [SDR CHQA200500115](https://openairdocs.org/sdr/CHQA200500115.md): Light · inoperative · Jun 17, 2005 · N276SK · Emb EMB145LR · Emergency Lighting > LEFT HAND OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. - [SDR CHQA200500042](https://openairdocs.org/sdr/CHQA200500042.md): Lamp · burned out · Feb 25, 2005 · N276SK · Emb EMB145LR · Emergency Lighting > LEFTHAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REPLACED THE LEFTHAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. - [SDR 00050](https://openairdocs.org/sdr/00050.md): Gasket · leaking · Nov 29, 2001 · N276SK · Emb EMB145 · Pneumatic Distribution System > RT ENGINE ITT 50 DEGREES HOTTER THAN LT ITT. INSPECTED AIRCRAFT NR 2 ENG, PERFORMED BORESCOPE OF COMPRESSOR TURBINE SECTION HOT SECTION WITHIN LIMITS. PERFORMED LEAK CHECK OF BLEED LINE, FOUND LEAKS AND REPLACED GASKETS. ALL CHECK GOOD AT THIS TIME. ## 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 = 'N276SK' AND deregistration_id = 'N276SK-2023-02-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N276SK-2023-02-22/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.