# Service difficulty reports: N294SK, cancelled Jan 11, 2018 A list on [N294SK, cancelled Jan 11, 2018](https://openairdocs.org/deregistered/N294SK-2018-01-11.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 · 63 reports - [SDR UHLA201509130722](https://openairdocs.org/sdr/UHLA201509130722.md): Switch · dirty · Sep 13, 2015 · N294SK · Emb EMB145LR · Door Warning System > THE MAIN ENTRY DOOR WAS UNABLE TO BE OPERATED WITH THE HYDRAULIC SYSTEM. MAINTENANCE FOUND AND CLEANED DEBRIS FROM THE MAIN ENTRY DOOR SWITCHES AND ALL OPS CHECKS WERE GOOD. - [SDR UHLA201507170566](https://openairdocs.org/sdr/UHLA201507170566.md): Ballast · failed · Jul 17, 2015 · N294SK · Emb EMB145LR · Passenger Compartment Lighting > THE LIGHT BALLAST OVER THE LAVATORY TOILET WAS FOUND TO BE SMOKING. MAINTENANCE DEACTIVATED THE BALLAST AND DEFERRED IT. MAINTENANCE LATER DETERMINED THE FAULT TO BE DUE TO A FAULTY HARNESS. THE BALLAST REMAINS ON DEFERRAL. - [SDR UHLA201506190445](https://openairdocs.org/sdr/UHLA201506190445.md): Frame · corroded · Jun 19, 2015 · N294SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, CORROSION WAS FOUND ON THE DOUBLER AT LT OMEGA FRAME 20. THE DOUBLER, FILLER, AND 2 OF EACH SHIMS WERE R & R IAW SRM 53-00-10. - [SDR UHLA201506190456](https://openairdocs.org/sdr/UHLA201506190456.md): Threshold · corroded · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND IN THE CARGO DOOR CUTOUT THRESHOLD AT FRAMES 65-68. THE THRESHOLD WAS R & R IAW SRM 51-40-02. - [SDR UHLA201506190455](https://openairdocs.org/sdr/UHLA201506190455.md): Floor Support · corroded · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT THE NUTPLATE HOLES AT FRAMES 59-61. THE OMEGA BEAM WAS R & R IAW SRM 51-40-02. - [SDR UHLA201506190454](https://openairdocs.org/sdr/UHLA201506190454.md): Shear Tie · cracked · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Internal Mounting Structure > DURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR TIE AT FRAME 67 BETWEEN STRINGERS 6L AND 7L. THE SHEAR TIE AND STIFFNER WERE R & R IAW SRM 53-31-04. - [SDR UHLA201506190453](https://openairdocs.org/sdr/UHLA201506190453.md): Structure · corroded · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Main, Structure > DURING INSPECTION, CORROSION WAS FOUND THE THE L SHAPE FRAME 65 AT THE CARGO DOOR STOP. THE DAMAGE WAS REPAIRED IAW SRM 53-31-04. - [SDR UHLA201506190452](https://openairdocs.org/sdr/UHLA201506190452.md): Floor Support · corroded · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AT THE LOWER HOLE AT THE UPRIGHT STANTION AT FRAME 20 AND THE LT OMEGA BEAM. THE STANTION WAS R & R IAW SRM 51-40-02. - [SDR UHLA201506190451](https://openairdocs.org/sdr/UHLA201506190451.md): Floor Support · corroded · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND IN THE GUSSET CENTER OMEGA AT FRAMES 20, 21, 22, 23. THE CENTER OMEGA BEAM WAS R & R IAW SRM 51-40-02. - [SDR UHLA201506190450](https://openairdocs.org/sdr/UHLA201506190450.md): Floor Support · cracked · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO HAVE A CRACK AT THE AFT NUTPLATE BETWEEN FRAMES 60 AND 61. THE BEAM WAS REPAIRED IAW ETD2014-145-05099. - [SDR UHLA201506190449](https://openairdocs.org/sdr/UHLA201506190449.md): Floor Support · cracked · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO HAVE CRACKS AT THE FWD AND AFT NUTPLATES AT FRAMES 59, 60, 61. NEW OMEGA BEAM INSTALLED - [SDR UHLA201506190448](https://openairdocs.org/sdr/UHLA201506190448.md): Hinge Fitting · worn · Jun 15, 2015 · N294SK · Emb EMB145LR · Rudder Structure > DURING INSPECTION, THE RUDDER BOTTOM HINGE FITTING BUSHING BORES WERE FOUND TO BE OUT OF LIMITS. THE BOTTOM HINGE FITTING WAS REPLACED IAW SRM 55-40-02. - [SDR UHLA201506190447](https://openairdocs.org/sdr/UHLA201506190447.md): Hinge Fitting · out of limits · Jun 15, 2015 · N294SK · Emb EMB145LR · Rudder Structure > DURING INSPECTION, THE RUDDER TOP HINGE FITTING BUSHING BORE'S WERE FOUND TO BE OUT OF LIMITS. THE TOP HINGE FITTING WAS REPLACED IAW SRM 55-40-02. - [SDR UHLA201506190446](https://openairdocs.org/sdr/UHLA201506190446.md): Tee Fitting · corroded · Jun 15, 2015 · N294SK · Emb EMB145LR · Fuselage Main, Attach Fittings > DURING INSPECTION, CORROSION WAS FOUND AT THE TEE FITTING AT FRAME 65. THE TEE FITTING WAS R & R IAW SRM 51-40-02. - [SDR UHLA201505210380](https://openairdocs.org/sdr/UHLA201505210380.md): Fan · failed · May 21, 2015 · N294SK · Emb EMB145LR · Air Distribution Fan > IN FLIGHT, THE CREW NOTICED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND FORWARD CABIN. NO SMOKE WAS VISIBLE. THE CREW DECLARED AN EMERGENCY AND MADE A SUCCESSFUL UNSCHEDULED LANDING. MAINTENANCE DETERMINED THE ODOR TO BE FROM A FAULTY FORWARD ELECTRICAL COM - [SDR CHQA20140624194](https://openairdocs.org/sdr/CHQA20140624194.md): Tire · separated · Jun 24, 2014 · N294SK · Emb EMB145LR · Tire > CREW REPORTED DURING TAKEOFF THERE WAS A VIBRATION IN THE ACFT. ATC REPORTED THAT THE ACFT HAS LT TIRE DEBRIS ON THE RUNWAY. THE CREW DECLARED AN EMER & RETURNED TO FIELD. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED A TREAD SEPARATION INSPECTION - [SDR CHQA20130427137](https://openairdocs.org/sdr/CHQA20130427137.md): Fitting · cracked · Apr 27, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, A CRACKED SHEAR CLIP WAS FOUND AT FRAME 10 UNDER THE RIGHT DIRECT VISION WINDOW. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130426136](https://openairdocs.org/sdr/CHQA20130426136.md): Fitting · damaged · Apr 26, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, FRAME 10 WAS FOUND TO BE ELONGATED AND THE HOLES MISALIGNED ON THE UPPER ATTACH SHEAR CLIP. THE SHEAR CLIP WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02 AND 53-00-04. - [SDR CHQA20130424141](https://openairdocs.org/sdr/CHQA20130424141.md): Floor Support · damaged · Apr 24, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, A MISDRILLED HOLE IN THE OMEGA BEAM SPLICE AT THE CENTER OMEGA BEAM LEFT SIDE WAS REPORTED. THE FINAL CORRECTIVE ACTION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT. - [SDR CHQA20130423132](https://openairdocs.org/sdr/CHQA20130423132.md): Skin · corroded · Apr 23, 2013 · N294SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING INSPECTION, CORROSION WAS FOUND ON THE INNER SKIN AT THE POTABLE WATER NIPPLE FILL. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-007598. - [SDR CHQA20130422133](https://openairdocs.org/sdr/CHQA20130422133.md): Fitting · corroded · Apr 22, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LATERAL L SHAPE AT THE BOTTOM OF FRAME 65. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 53-31-04. - [SDR CHQA20130420131](https://openairdocs.org/sdr/CHQA20130420131.md): Floor Support · corroded · Apr 20, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE RIGHT OMEGA BEAM FROM FRAME 59 TO FRAME 61 WAS FOUND TO BE CORRODED. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-007501. - [SDR CHQA20130419140](https://openairdocs.org/sdr/CHQA20130419140.md): Reinforcement · cracked · Apr 19, 2013 · N294SK · Emb EMB145LR · Fuselage Main, Longeron/Stringer > DURING INSPECTION, A CRACK WAS FOUND ON THE STRINGER REINFORCEMENT FRAME 20 STRINGER 3L. THE STRINGER REINFORCEMENT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130419139](https://openairdocs.org/sdr/CHQA20130419139.md): Floor Support · corroded · Apr 19, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE ON THE LEFT OMEGA INBOARD FLOOR SUPPORT BETWEEN FRAMES 24 AND 25. THE FLOOR SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-30-01 AND 53-00-10. - [SDR CHQA20130419138](https://openairdocs.org/sdr/CHQA20130419138.md): Floor Support · corroded · Apr 19, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE CENTER OMEGA LEFT FLOOR SUPPORT BETWEEN FRAMES 24 AND 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-007499. - [SDR CHQA20130419135](https://openairdocs.org/sdr/CHQA20130419135.md): Seat Track · corroded · Apr 19, 2013 · N294SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > DURING INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK SUPPORT AT FRAME 50. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130419134](https://openairdocs.org/sdr/CHQA20130419134.md): Doubler · corroded · Apr 19, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER AT THE LEFT OMEGA FRAME 20. THE REPAIR DOUBLER WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20130419130](https://openairdocs.org/sdr/CHQA20130419130.md): Doubler · corroded · Apr 19, 2013 · N294SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND IN THE DOUBLER AT THE POTABLE WATER FILL NIPPLE. THE DOUBLER WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-007598. - [SDR CHQA20130226066](https://openairdocs.org/sdr/CHQA20130226066.md): Computer · faulty · Feb 26, 2013 · N294SK · Emb EMB145LR · Central Computers > CREW REPORTED THAT THERE WAS ELECTRICAL SMOKE SMELL AND HAZE IN THE COCKPIT IN FLIGHT. THE CREW DIVERTED TO KUNV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE IC-600 NUMBER 1 AND THE DATA ACQUISITION UNIT 1. OPERATIONAL CHECKS WERE GOOD AND NO SMELL - [SDR CHQA20130226065](https://openairdocs.org/sdr/CHQA20130226065.md): Dau · faulty · Feb 26, 2013 · N294SK · Emb EMB145LR · Central Computers > CREW REPORTED THAT THERE WAS ELECTRICAL SMOKE SMELL AND HAZE IN THE COCKPIT IN FLIGHT. THE CREW DIVERTED TO KUNV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE IC-600 NUMBER 1 AND THE DATA ACQUISITION UNIT 1. OPERATIONAL CHECKS WERE GOOD AND NO SMELL - [SDR CHQA20120831304](https://openairdocs.org/sdr/CHQA20120831304.md): Light · inoperative · Aug 31, 2012 · N294SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE LEFT AFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120825300](https://openairdocs.org/sdr/CHQA20120825300.md): Wire · damaged · Aug 25, 2012 · N294SK · Emb EMB145LR · Light System Wiring > MAINTENANCE REPORTED THAT THE AFT FLOOR PROXIMITY STRIP WIRING WAS DAMAGED AT THE PROXIMITY STRIP. THE AFT FLOOR PROXIMITY STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201200028](https://openairdocs.org/sdr/CHQA201200028.md): Clamp · broken · Jan 27, 2012 · N294SK · Emb EMB145LR · Cabin Cooling System > CREW REPORTED THAT DURING CLIMB THERE WAS A LOUD RUSHING AIR NOISE IN THE PASSENGER CABIN. THE CREW SELECTED PACK NUMBER 1 OFF AND THE NOISE CLEARED. PACK NUMBER 2 WAS ALREADY ON DEFERRAL AND THE CREW DECIDED TO RETURN TO KLGA. THE AIRCRAFT LANDED WITHOUT I - [SDR CHQA201100491](https://openairdocs.org/sdr/CHQA201100491.md): Battery · discharged · Dec 16, 2011 · N294SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS CONNECTED TO THE NUMBER 2 EMERGENCY BATTERY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100490](https://openairdocs.org/sdr/CHQA201100490.md): Battery · discharged · Dec 16, 2011 · N294SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS CONNECTED TO THE NUMBER 4 EMERGENCY BATTERY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100394](https://openairdocs.org/sdr/CHQA201100394.md): Module · activated · Sep 29, 2011 · N294SK · Emb EMB145LR · Cabin Pressure Control System > CREW REPORTED, LOST THE CABIN ALTITUDE INDICATION IN MANUAL PRESSURIZATION MODE. AUTO-PRESSURIZATION WAS ALREADY ON MEL. THE AIRCRAFT RETURNED TO KPIT AND LANDED WITHOUT INCIDENT. MAINTENANCE LOCKED BOTH OUTFLOW VALVES OPEN AND DEFERRED AUTO AND MANUAL PRES - [SDR CHQA201100049](https://openairdocs.org/sdr/CHQA201100049.md): Wire · broken · Mar 4, 2011 · N294SK · Emb EMB145LR · Light System Wiring > DURING INSPECTION THE NR 1 FLOOR PROXIMITY EMERGENCY LIGHT WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REPLACED THE NR 1 FLOOR PROXIMITY LIGHT STRIP WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000198](https://openairdocs.org/sdr/CHQA201000198.md): Wire · pulled · Oct 9, 2010 · N294SK · Emb EMB145LR · Light System Wiring > WHILE REMOVING THE AFT CENTER FLOORBOARD, THE AFT FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A WIRE PULLED FROM THE STRIP. THE FLOOR PROXIMITY STRIP AT ROWS 17/18 WAS REPLACED PER EMB 145 AMM 33-50-12 WITH NO FURTHER DEFECTS NOTED AT THAT TIME. - [SDR CHQA201000153](https://openairdocs.org/sdr/CHQA201000153.md): Light · inoperative · Aug 8, 2010 · N294SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT THE EXIT ROW WAS INOP WHEN TESTED. MAINTENANCE REPLACED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD. - [SDR CHQA201000115](https://openairdocs.org/sdr/CHQA201000115.md): Proximity Switch · faulty · Jun 5, 2010 · N294SK · Emb EMB145LR · Landing Gear Position and Warning > CREW REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE GEAR WAS CYCLED SEVERAL TIMES BEFORE THE NOSE GEAR DOORS FINALLY CLOSED. THE FLIGHT CONTINUED TO CMH AND LANDED WITHOUT INCIDENT. WHILE TROUBLESHOOTING THE FAULT, MAINTENANCE - [SDR CHQA201000111](https://openairdocs.org/sdr/CHQA201000111.md): Lever · failed · Jun 2, 2010 · N294SK · Emb EMB145LR · Landing Gear Selector > AFTER TAKEOFF, CREW RETRACTED MLG & AFTER RETRACTION, NLG DOORS REMAINED OPEN. ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX FOUND A GROUND AT PIN X2 ON K0642 RELAY SOCKET. CONNECTOR P0774 DISCONNECTED ON W014 HARNESS & PIN X2, NO LONGER GROUNDED. - [SDR CHQA201000109](https://openairdocs.org/sdr/CHQA201000109.md): Connector · shorted · Jun 1, 2010 · N294SK · Emb EMB145LR · Landing Gear System Wiring > AFTER TAKEOFF, GEAR SELECTED UP, CREW REPORTED NORMAL RETRACTION & EICAS INDICATIONS, BUT A LOUD NOISE HEARD FROM NLG AREA. ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED LGEU, NLG DOOR RELAY K0642, & NLG DOOR SOLENOID. FAULT RETURNED ON 6/2/ - [SDR CHQA201000107](https://openairdocs.org/sdr/CHQA201000107.md): Proximity Sensor · faulty · May 29, 2010 · N294SK · Emb EMB145LR · Landing Gear Position and Warning > AFTER TAKEOFF, WHEN THE LANDING GEAR WAS UP AND LOCKED, THE CREW NOTICED A LOUD RUSHING AIR NOISE FROM THE NOSE. THERE WERE NO UNUSUAL INDICATIONS ON EICAS AND AS A PRECAUTION THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. THE ACFT WAS THEN FER - [SDR CHQA201000103](https://openairdocs.org/sdr/CHQA201000103.md): Unknown · malfunctioned · May 27, 2010 · N294SK · Emb EMB145LR · Landing Gear Door Retract Section > CREW REPORTED THAT AFTER SELECTING THE LANDING GEAR UP, THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE CREW VERIFIED WITH TOWER THAT THE NOSE GEAR DOORS WERE STILL OPEN WITH NO ABNORMAL INDICATIONS ON EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT - [SDR CHQA201000093](https://openairdocs.org/sdr/CHQA201000093.md): Connector · damaged · May 4, 2010 · N294SK · Emb EMB145LR · Light System Wiring > DURING INSPECTION A FLOOR PROXIMITY LIGHT STRIP WAS FOUND WITH DAMAGED CONNECTORS. THE FLOOR LIGHT STRIP WAS REPLACED BY MAINTENANCE IAW AMM 33-50-12. - [SDR CHQA201000082](https://openairdocs.org/sdr/CHQA201000082.md): Control Lever · faulty · Apr 17, 2010 · N294SK · Emb EMB145LR · Trailing Edge Flap Control System > CREW REPORTED THAT THE AIRCRAFT WOULD NOT ACCELERATE AND A RUMBLE COULD BE HEARD AND FELT. THE CREW INSPECTED THE WINGS DURING FLIGHT AND FOUND THE FLAPS SLIGHTLY EXTENDED WITH A ZERO INDICATION IN THE COCKPIT. THE FLAP HANDLE WAS CYCLED AND THE FLAPS FULLY - [SDR CHQA201000079](https://openairdocs.org/sdr/CHQA201000079.md): Solenoid Valve · faulty · Apr 15, 2010 · N294SK · Emb EMB145LR · Landing Gear Door Retract Section > CREW RETURNED TO FIELD DUE TO A RUMBLING NOISE FROM THE NOSE LANDING GEAR AREA AFTER GEAR RETRACTION. THE AIRCRAFT WAS FERRIED TO SDF FOR FURTHER TROUBLESHOOTING. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR SOLENOID, ALL THREE HYDRAULIC MANIFOLD FILTERS, - [SDR CHQA201000078](https://openairdocs.org/sdr/CHQA201000078.md): Landing Gear · malfunctioned · Apr 14, 2010 · N294SK · Emb EMB145LR · Landing Gear Retraction/Extension System > ON DEPARTURE THE CREW REPORTED THAT IT TOOK THE NOSE LANDING GEAR ALMOST 1 MINUTE TO RETRACT AFTER SELECTING THE GEAR UP. A LANDING GEAR DISAGREE MESSAGE WAS ALSO REPORTED. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM - [SDR CHQA201000034](https://openairdocs.org/sdr/CHQA201000034.md): Battery Pack · discharged · Feb 11, 2010 · N294SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND LAMP WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000033](https://openairdocs.org/sdr/CHQA201000033.md): Light · inoperative · Feb 10, 2010 · N294SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOP DURING TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10, OPS CHECK GOOD. Next page: https://openairdocs.org/deregistered/N294SK-2018-01-11/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 = 'N294SK' AND deregistration_id = 'N294SK-2018-01-11' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N294SK-2018-01-11/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.