# Service difficulty reports: N287SK, cancelled Oct 1, 2022 A list on [N287SK, cancelled Oct 1, 2022](https://openairdocs.org/deregistered/N287SK-2022-10-01.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR UHLA201603140109](https://openairdocs.org/sdr/UHLA201603140109.md): Pin · damaged · Mar 14, 2016 · N287SK · Emb EMB145LR · Light System Wiring > EMERGENCY LIGHT BROKEN, LAST STRIP NEEDS CONNECTOR PIN. REPINNED LAST ROW EMERGENCY STRIP LIGHTING IAW SWPM 20-21-00. OPS CHECK GOOD. - [SDR UHLA201602090107](https://openairdocs.org/sdr/UHLA201602090107.md): Strut · underserviced · Mar 9, 2016 · N287SK · Emb EMB145LR · Nose/Tail Landing Gear Strut/Axle > NLG DID NOT RETRACT, LT LEVER DISAGREE MESSAGE ON EICAS. RETURNED TO FIELD. VERIFIED NLG STRUT SERVICING AND CYCLED LANDING GEAR SEVERAL TIMES WITH NO DEFECTS NOTED. - [SDR UHLA201508270675](https://openairdocs.org/sdr/UHLA201508270675.md): Light · inoperative · Aug 27, 2015 · N287SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE EMERGENCY LIGHT AT SEATS 10-16A WERE FOUND TO BE INOPERATIVE. THE LIGHTS WERE R & R IAW AMM53-50-12 AND OPS CHECKED GOOD. - [SDR UHLA2015041100247](https://openairdocs.org/sdr/UHLA2015041100247.md): Uplock · malfunctioned · Apr 11, 2015 · N287SK · Emb EMB145LR · Landing Gear Retraction/Extension System > THE CREW REPORTED RECEIVING A LANDING GEAR LEVER DISAGREE FAIL MESSAGE AND THE NOSE GEAR FAILING TO RETRACT. THE CREW MADE AN UNSCHEDULED LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE NLG UPLOCK BOX AND LANDING GEAR SOLENOID VALVE. OPS CHECKS AND LANDI - [SDR UHLA2015041000246](https://openairdocs.org/sdr/UHLA2015041000246.md): Wire Harness · damaged · Apr 10, 2015 · N287SK · Emb EMB145LR · Landing Gear System Wiring > THE CREW REPORTED THAT THE NLG WOULD NOT RETRACT AFTER TAKEOFF. THE ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NLG WIRE HARNESS. OPS CHECKS AND LANDING GEAR SWINGS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR UHLA2015040600238](https://openairdocs.org/sdr/UHLA2015040600238.md): Wire Harness · damaged · Apr 6, 2015 · N287SK · Emb EMB145LR · Landing Gear System Wiring > THE CREW REPORTED THAT THEY RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NLG UPLOCK SWITCHES AND THE NOSE LANDING GEAR UPLOCK PROXIMITY SWITCH HARNESS. OPS - [SDR UHLA2015022300130](https://openairdocs.org/sdr/UHLA2015022300130.md): Frame · dented · Feb 23, 2015 · N287SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A DENT WAS FOUND ON FRAME 62 AT STRINGER 16R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-04. - [SDR UHLA2015021900131](https://openairdocs.org/sdr/UHLA2015021900131.md): Threshold · corroded · Feb 19, 2015 · N287SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR THRESHOLD STRINGER BEAM. THE THRESHOLD WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141209351](https://openairdocs.org/sdr/CHQA20141209351.md): Seal · dirty · Dec 9, 2014 · N287SK · Emb EMB145LR · Flight Compartment Windows > THE CREW REPORTED THAT DURING FLIGHT THE CAPTAIN'S DIRECT VISION WINDOW WAS LEAKING. THE ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. INSPECTED THE WINDOW & CLEANED THE WINDOW SEAL. PRESSURIZATION CHECKS WERE GOOD WITH NO LEAKS NOTED. - [SDR CHQA20140226070](https://openairdocs.org/sdr/CHQA20140226070.md): Downlock Bracket · broken · Feb 26, 2014 · N287SK · Emb EMB145LR · Landing Gear Position and Warning > CREW REPORTED THAT DURING CLIMB THE LG WOULD NOT RETRACT & A LG AIR & GND FAIL MSG APPEARED. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED THE NLG AIR & GND PROXIMITY SWITCH BRACKET. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS N - [SDR CHQA20131209464](https://openairdocs.org/sdr/CHQA20131209464.md): Fitting · corroded · Dec 9, 2013 · N287SK · Emb EMB145LR · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 & STRINGER 21R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20131207465](https://openairdocs.org/sdr/CHQA20131207465.md): Frame · dented · Dec 7, 2013 · N287SK · Emb EMB145LR · Fuselage Main, Frame > FRAME 72 WAS FOUND TO BE DENTED AT STRINGER 16R. THE FRAME WAS REPAIRED IAW SRM 51-40-02. - [SDR CHQA20131207463](https://openairdocs.org/sdr/CHQA20131207463.md): Threshold · corroded · Dec 7, 2013 · N287SK · Emb EMB145LR · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT LOWER BEAM. THE THRESHOLD PLATE WAS REPAIRED IAW SRM 53-21-02. - [SDR CHQA20131207462](https://openairdocs.org/sdr/CHQA20131207462.md): Fitting · cracked · Dec 7, 2013 · N287SK · Emb EMB145LR · Fuselage Miscellaneous Structure > A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16R & 15R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20131207461](https://openairdocs.org/sdr/CHQA20131207461.md): Fitting · cracked · Dec 7, 2013 · N287SK · Emb EMB145LR · Fuselage Miscellaneous Structure > A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R & 16R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20120909309](https://openairdocs.org/sdr/CHQA20120909309.md): Inverter · inoperative · Sep 9, 2012 · N287SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE CENTER CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 6 DC TO AC INVERTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120803231](https://openairdocs.org/sdr/CHQA20120803231.md): Battery · discharged · Aug 3, 2012 · N287SK · Emb EMB145LR · Emergency Lighting > CREW REPORTED THAT UPON ARRIVING AT THE AIRCRAFT, THE EMERGENCY LIGHT CIRCUIT BREAKER WAS POPPED AND THE FORWARD HALF OF THE EMERGENCY LIGHTS WERE ON AND THE BACK HALF WERE NOT. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WE - [SDR CHQA20120729227](https://openairdocs.org/sdr/CHQA20120729227.md): Switch · inoperative · Jul 29, 2012 · N287SK · Emb EMB145LR · Emergency Lighting > CREW REPORTED THAT THE EMERGENCY LIGHTS WERE TURNED ON AND WOULD NOT TURN OFF WHILE ON THE GROUND. MAINTENANCE REPLACED THE FLIGHT DECK EMERGENCY LIGHT SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120223063](https://openairdocs.org/sdr/CHQA20120223063.md): Battery · failed · Feb 23, 2012 · N287SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE NUMBER 4 EMERGENCY BATTERY FAILED ITS OPERATIONAL CHECK. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120217053](https://openairdocs.org/sdr/CHQA20120217053.md): Battery · faulty · Feb 17, 2012 · N287SK · Emb EMB145LR · Emergency Lighting > CREW REPORTED THAT THE EMERGENCY LIGHTS STAYED ON WHEN NOT COMMANDED TO BE ON. MAINTENANCE REPLACED THE NUMBER THREE BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201200035](https://openairdocs.org/sdr/CHQA201200035.md): Conditioner · faulty · Jan 29, 2012 · N287SK · Emb EMB145LR · Landing Gear Brake System > CREW REPORTED THAT UPON LANDING, THERE WAS NO BRAKING FROM EITHER THE CAPTAIN'S OR FIRST OFFICER'S BRAKE PEDALS. THE AIRCRAFT WAS SLOWED WITH USE OF THE THRUST REVERSERS AND AT APPROXIMATELY 10 KNOTS, THE BRAKES BECAME EFFECTIVE. MAINTENANCE REPLACED THE BRA - [SDR CHQA201100388](https://openairdocs.org/sdr/CHQA201100388.md): Engine · smoke · Sep 26, 2011 · N287SK · Emb EMB145LR · Engine (Turbine/Turboprop) > AFTER TAKEOFF, RECEIVED A LAVATORY SMOKE INDICATION ON EICAS. F/A VERIFIED SMOKE COMING FROM LAVATORY. RETURNED AND LANDED WITHOUT INCIDENT. FIRE DEPT. INFRARED IMAGING LOCATED HOT AREA IN FLOOR OF CARGO BAY TO FLOOR OF LAVATORY. MAINTENANCE FOUND RT ENG - [SDR CHQA201100228](https://openairdocs.org/sdr/CHQA201100228.md): Splice · broken · Jun 21, 2011 · N287SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE AFT FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN SPLICE. MAINTENANCE REPLACED THE SPLICE WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100127](https://openairdocs.org/sdr/CHQA201100127.md): Brake Sys · malfunctioned · Apr 3, 2011 · N287SK · Emb EMB145LR · Landing Gear Brake System > CREW REPORTED THAT DURING THE LANDING ROLL OUT, THE BRAKES INITIALLY WORKED NORMALLY, BUT WHILE DECELERATING FROM 90KTS TO 50KTS, THE BRAKES WERE INEFFECTIVE. REPORTED THAT THERE WAS STILL RESISTANCE IN THE PEDALS, BUT NO BRAKING FORCE WAS APPLIED. ONCE BELO - [SDR CHQA201000227](https://openairdocs.org/sdr/CHQA201000227.md): Pressure Switch · inoperative · Dec 12, 2010 · N287SK · Emb EMB145LR · Air Intake Anti/De-Ice System > DURING CLIMBOUT, THE CREW REPORTED AN E2 ANTI-ICE VALVE FAIL MESSAGE ON EICAS. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE E2 ANTI-ICE VALVE ON MEL AND RETURNED THE AIRCRAFT TO SERVICE. THE DEFERRAL WAS CLEARED ON 12/17/2010 - [SDR CHQA200900208](https://openairdocs.org/sdr/CHQA200900208.md): O-Ring · damaged · Sep 24, 2009 · N287SK · Emb EMB145LR · Pneumatic Distribution System > FLIGHT 5516, ATL TO CLE. AIRCRAFT RETURNED TO FIELD DUE TO A BLEED 1 LEAK MESSAGE ON EICAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A DAMAGED O-RING IN THE BLEED SYSTEM 1 DUCTING AT JOINT 19 BEHIND THE CARGO COMPARTMENT WALL. THE O-RINGS IN THE AFFECT - [SDR CHQA200900139](https://openairdocs.org/sdr/CHQA200900139.md): Relay · faulty · Jun 11, 2009 · N287SK · Emb EMB145LR · Exterior Lighting > FLIGHT 5876, CLE TO LGA. DURING CLIMBOUT THE FLIGHT CREW NOTICED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. NO VISIBLE SMOKE WAS REPORTED. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RELAY K0234 (RIGHT LANDING LIGHT CONTACT - [SDR CHQA200900039](https://openairdocs.org/sdr/CHQA200900039.md): Ballast · inoperative · Jan 30, 2009 · N287SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE MAIN DOOR EXIT SIGN WAS FOUND TO BE INOP. THE NR 1 EMERGENCY LIGHT BALLAST WAS REPLACED AND THE LIGHT OPERATED NORMALLY. - [SDR CHQA200900021](https://openairdocs.org/sdr/CHQA200900021.md): Battery Pack · inoperative · Jan 17, 2009 · N287SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE FORWARD EMERGENCY LIGHT ON THE OVERWING EXIT CEILING PANEL WAS FOUND TO BE INOPERATIVE ALONG WITH THE EMERGENCY LIGHTS AT THE LEFT AND RIGHT OVERWING HATCHES INSIDE THE FUSELAGE. THE CONNECTIONS FOR THE CEILING PANEL WERE CHECKED AND RE- - [SDR CHQA200800241](https://openairdocs.org/sdr/CHQA200800241.md): Inverter · inoperative · Dec 8, 2008 · N287SK · Emb EMB145LR · Emergency Lighting > EMERGENCY FLOOR STRIP LIGHTS 2 AND 3 WERE INOPERATIVE DURING TEST. THE NR 3 INVERTER WAS REPLACED IAW EMB 145 AMM 33-50-11 AND THE SYSTEMS CHECKED OPERATIONAL. - [SDR CHQA200800150](https://openairdocs.org/sdr/CHQA200800150.md): Hose · chafed · Jul 17, 2008 · N287SK · Emb EMB145LR · Hydraulic System, Main > FLIGHT 5923, GSO TO CLE. ON DESCENT INTO CLE, THE FLIGHT CREW RECEIVED AN E1 HYD PUMP FAIL MESSAGE. THE QRH WAS FOLLOWED AND IT WAS DETERMINED THAT THERE WAS NO QUANTITY INDICATING ON SYSTEM 1. LANDED WITHOUT INCIDENT, TAXIED CLEAR OF RUNWAY AND WAITED FOR - [SDR CHQA200800080](https://openairdocs.org/sdr/CHQA200800080.md): Pump · overheated · Apr 19, 2008 · N287SK · Emb EMB145LR · Hydraulic Pump (Electric/Engine), Main > FLIGHT 5901, CLE TO MSY - WHILE CRUISING AT FL360 THE FLIGHT CREW RECEIVED A MASTER CAUTION AND EICAS MESSAGE FOR HYD SYS 1 OVHT. THE CREW RAN THROUGH THE APPROPRIATE QRH CHECKLISTS AND SHUT OFF THE SYSTEM. AFTER WAITING THE QRH RECOMMENDED TIME, THE NR 1 HY - [SDR CHQA200600101](https://openairdocs.org/sdr/CHQA200600101.md): Battery · inoperative · Aug 18, 2006 · N287SK · Emb EMB145LR · Emergency Lighting > NR 2 AND NR 3 EMERGENCY STRIP AND AFT GALLEY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB 145 MM 33-50-04. OPS CHECK GOOD AT THIS TIME. - [SDR CHQA200600102](https://openairdocs.org/sdr/CHQA200600102.md): Battery · inoperative · Aug 18, 2006 · N287SK · Emb EMB145LR · Emergency Lighting > LEFT HAND OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY IAW EMB 145 MM 33-50-04. - [SDR CHQA200600019](https://openairdocs.org/sdr/CHQA200600019.md): Sign · inoperative · Jan 28, 2006 · N287SK · Emb EMB145LR · Emergency Lighting > FOUND FORWARD CABIN EXIT SIGN SERVICE DOOR OVERHEAD INOPERATIVE. REMOVED AND REPLACED SIGN IAW EMB 145 MM 33-50-15. - [SDR CHQA200400551](https://openairdocs.org/sdr/CHQA200400551.md): Battery Pack · discharged · Sep 4, 2004 · N287SK · Emb EMB145LR · Emergency Lighting > BOTH OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04. ## 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 = 'N287SK' AND deregistration_id = 'N287SK-2022-10-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N287SK-2022-10-01/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, except the copies of manufacturers’ service documents, which belong to their rights holders.