# Service difficulty reports: N272SK, cancelled Sep 19, 2018 A list on [N272SK, cancelled Sep 19, 2018](https://openairdocs.org/deregistered/N272SK-2018-09-19.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 · 51 reports - [SDR UHLA201606140329](https://openairdocs.org/sdr/UHLA201606140329.md): Bracket · bent · Jun 14, 2016 · N272SK · Emb EMB145LR · Passenger/Crew Doors > MED STEPS WILL NOT DEPLOY. R & R BENT ROLLER BRACKET AND OPS CHECK GOOD IAW 52-13-02. - [SDR UHLA201602260084](https://openairdocs.org/sdr/UHLA201602260084.md): Stop · damaged · Feb 26, 2016 · N272SK · Emb EMB145LR · Passenger/Crew Doors > AIR STAIRS DO NOT DEPLOY. R & R MAIN DOOR STEP FOLD-OUT BACKSTOP IAW AMM 52-13-02. OPS CHECKED GOOD. - [SDR UHLA201602260075](https://openairdocs.org/sdr/UHLA201602260075.md): Stop · damaged · Feb 26, 2016 · N272SK · Emb EMB145LR · Passenger/Crew Doors > AIR START DOES NOT DEPLOY. R & R MAIN DOOR STEP FOLD-OUT BACKSTOP IAW AMM 52-13-02. OPS CHECK GOOD. - [SDR UHLA201512040896](https://openairdocs.org/sdr/UHLA201512040896.md): Fitting · cracked · Dec 4, 2015 · N272SK · Emb EMB145LR · Engine Mount Section > LEFT ENGINE LOWER FWD YOKE LINKAGE FITTING CRACKED. R & R LT ENGINE LOWER FWD YOKE LINKAGE FITTING IAW ETD2015-145-112035, REV A. - [SDR UHLA201510060759](https://openairdocs.org/sdr/UHLA201510060759.md): Rod · not reported · Oct 6, 2015 · N272SK · Emb EMB145LR · Passenger/Crew Doors > THE MAIN ENTRY DOOR AIRSTAIRS WOULD NOT RETRACT WHEN THE DOOR WAS CLOSED. MAINTENANCE R & R THE DOOR STEP ACTUATING ROD IAW AMM 52-10-03 AND ALL OPS CHECKS WERE GOOD. - [SDR UHLA201509100696](https://openairdocs.org/sdr/UHLA201509100696.md): Inverter · inoperative · Sep 10, 2015 · N272SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE EMERGENCY EXIT SIGNS OVER THE LT OVERWING EMERGENCY EXIT, FORWARD BULKHEAD, AND SERVICE DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 2, 3, AND 5 INVERTERS IAW AMM 33-50-11 AND ALL OPS CHECKS WERE GOOD; NO FURTHER DEFECTS - [SDR UHLA201505040343](https://openairdocs.org/sdr/UHLA201505040343.md): Windshield · faulty · May 4, 2015 · N272SK · Emb EMB145LR · Flight Compartment Windows > THE CREW REPORTED A BURNING ODOR IN FLIGHT WHEN THE WINDSHIELD 1 HEAT WAS IN OPERATION. THE ACFT LANDED AT ITS INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WINDSHIELD 1. OPS AND PRESSURIZATION CHECKS WERE GOOD WITH NO FURTHER DEFECTS - [SDR UHLA201505030339](https://openairdocs.org/sdr/UHLA201505030339.md): Unknown · odor · May 3, 2015 · N272SK · Emb EMB145LR · Air Distribution System > THE CREW REPORTED THAT THEIR WAS A BURNING ODOR IN THE COCKPIT AND CABIN DURING FLIGHT. THE ACFT LANDED UNEVENTFULLY AT ITS INTENDED DESTINATION. MAINTENANCE INSPECTED THE ELECTRICAL DISTRIBUTION SYSTEM, THE CABIN AND COCKPIT LIGHTING, THE ELECTRIC HYDRAULIC - [SDR UHLA2015011400051](https://openairdocs.org/sdr/UHLA2015011400051.md): Frame · gouged · Jan 14, 2015 · N272SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A GOUGE WAS FOUND ON FRAME 15 BETWEEN STRINGERS 1R AND 2R. THE FRAME REPAIRED IAW SRM 53-00-04, SRM 51-40-02, AND CPM 51-21-04. - [SDR UHLA2015011300054](https://openairdocs.org/sdr/UHLA2015011300054.md): Frame · cracked · Jan 13, 2015 · N272SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, FRAME 10 ON THE FIRST OFFICERS SIDE WAS FOUND TO BE CRACKED UNDER THE DV WINDOW. THE FRAME SECTION WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015011300049](https://openairdocs.org/sdr/UHLA2015011300049.md): Frame · cracked · Jan 13, 2015 · N272SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, FRAME 10 ON THE CAPTAIN`S SIDE WAS FOUND TO BE CRACKED UNDER THE DV WINDOW. THE FRAME SECTION WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015011200056](https://openairdocs.org/sdr/UHLA2015011200056.md): Floor Support · corroded · Jan 12, 2015 · N272SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015011200055](https://openairdocs.org/sdr/UHLA2015011200055.md): Floor Support · corroded · Jan 12, 2015 · N272SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM SILL AT FRAME 24. THE SILL WAS REPAIRED IAW ETD 2015-145-004502. - [SDR UHLA2015011200052](https://openairdocs.org/sdr/UHLA2015011200052.md): Step · corroded · Jan 12, 2015 · N272SK · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER NUTPLATE FOR THE PASSENGER DOOR LOWER STEP. THE CENTER NUTPLATE STRIP FITTING WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015011200050](https://openairdocs.org/sdr/UHLA2015011200050.md): Frame · cracked · Jan 12, 2015 · N272SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 AND STRINGER 2R. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-00367 - [SDR UHLA201501110053](https://openairdocs.org/sdr/UHLA201501110053.md): Skin · damaged · Jan 11, 2015 · N272SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY, FOUND A LIGHTNING BURN. A REPAIR DOUBLER WAS INSTALLED AT FRAME 14 AND STRINGER 1R IAW ETD 2014-145-081088. - [SDR CHQA20140925283](https://openairdocs.org/sdr/CHQA20140925283.md): Angle · corroded · Sep 27, 2014 · N272SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT FRAME 20. THE RAM ANGLE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140925285](https://openairdocs.org/sdr/CHQA20140925285.md): Support · corroded · Sep 25, 2014 · N272SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE RT RAMP SUPPORT WAS FOUND TO BE CORRODED. THE RT RAMP ANGLE WAS REPLACED IAW SRM 51-40-02 & ETD 2014-145-08-1412. - [SDR CHQA20140925284](https://openairdocs.org/sdr/CHQA20140925284.md): Profile · corroded · Sep 25, 2014 · N272SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE PROFILE FWD OF THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. THE PROFILE WAS REPAIRED IAW SRM 53-21-10. - [SDR CHQA20140705206](https://openairdocs.org/sdr/CHQA20140705206.md): Switch · faulty · Jul 5, 2014 · N272SK · Emb EMB145LR · Pneumatic Distribution System > CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 VLV FAIL MSG. THE ACFT WAS DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE BLEED SYS 1 PUSH BUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20140608187](https://openairdocs.org/sdr/CHQA20140608187.md): Flapper Valve · broken · Jun 8, 2014 · N272SK · Emb EMB145LR · Cabin Pressure Control System > CREW REPORTED THAT THE AUTO PRESSURIZATION SYS WAS INOPERATIVE DURING FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX FOUND THE MANUAL PRESSURIZATION SYS TO BE WORKING & DEFERRED THE AUTO PRESSURIZATION. THE DEFERRAL WAS CLEARED ON 6/11/14 - [SDR CHQA20140521152](https://openairdocs.org/sdr/CHQA20140521152.md): Battery · discharged · May 21, 2014 · N272SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20140213053](https://openairdocs.org/sdr/CHQA20140213053.md): Unknown · odor · Feb 13, 2014 · N272SK · Emb EMB145LR · Air Distribution System > CREW REPORTED THAT DURING FLIGHT, PACK 1 HAS AN ODOR WHEN SELECTED ON. INSPECTED THE PACK AREA WITH NO DEFECTS. OPERATIONS CHECKED GOOD WITH NO DEFECTS OR ODORS NOTED. - [SDR CHQA20131121437](https://openairdocs.org/sdr/CHQA20131121437.md): Controller · erratic · Nov 21, 2013 · N272SK · Emb EMB145LR · Cabin Pressure Controller > CREW REPORTED THAT THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT IN THE AUTO PRESSURIZATION MODE. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE AUTO PRESSURIZATION FUNCTION WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 11/21/2013 WHEN MX REPLACED THE - [SDR CHQA20131114410](https://openairdocs.org/sdr/CHQA20131114410.md): Icu · faulty · Nov 14, 2013 · N272SK · Emb EMB145LR · VHF Communications System > CREW REPORTED THAT AFTER TAKEOFF BOTH RADIO MANAGEMENT UNITS SHOWED DASHES IN THE TRANSPONDER AND TCAS FIELDS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 INTEGRATED COMMUNICATIONS UNIT. OPS CHECKS WERE GOOD WITH - [SDR CHQA20131104381](https://openairdocs.org/sdr/CHQA20131104381.md): Battery · inoperative · Nov 4, 2013 · N272SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, FORWARD WING TO FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD. - [SDR CHQA20131104380](https://openairdocs.org/sdr/CHQA20131104380.md): Battery · inoperative · Nov 4, 2013 · N272SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND ALL OPERATIONAL CHECKS WERE GOOD. - [SDR CHQA20130724188](https://openairdocs.org/sdr/CHQA20130724188.md): Wire · damaged · Jul 24, 2013 · N272SK · Emb EMB145LR · Light System Wiring > MX REPORTED THAT THE MAIN ENTRY DOOR HANDRAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED WIRE W737-0034-20. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130213051](https://openairdocs.org/sdr/CHQA20130213051.md): Wire Harness · faulty · Feb 13, 2013 · N272SK · Emb EMB145LR · Landing Gear System Wiring > CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER ROTATION AND REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS. OPERATIONAL - [SDR CHQA20130127031](https://openairdocs.org/sdr/CHQA20130127031.md): Control Unit · faulty · Jan 27, 2013 · N272SK · Emb EMB145LR · Landing Gear Brake System > CREW REPORTED THAT ON LANDING THE CAPTAIN'S BRAKES SEEMED TO LOSE PRESSURE FOR APPROXIMATELY ONE SECOND AND THEN WOULD GRAB. THE AIRCRAFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD - [SDR CHQA20120929364](https://openairdocs.org/sdr/CHQA20120929364.md): Light · inoperative · Sep 29, 2012 · N272SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 3 AND 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE OVERHEAD EMERGENCY LIGHTS AT ROWS 3 AND 12. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120919361](https://openairdocs.org/sdr/CHQA20120919361.md): Door Frame · corroded · Sep 19, 2012 · N272SK · Emb EMB145LR · Service Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR STRUCTURE AROUND THE FASTENERS AT THE BOTTOM OF THE DOOR. THE SERVICE DOOR STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013524. - [SDR CHQA20120919360](https://openairdocs.org/sdr/CHQA20120919360.md): Door Frame · corroded · Sep 19, 2012 · N272SK · Emb EMB145LR · Service Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR STRUCTURE AROUND THE FASTENERS AT THE BOTTOM OF THE DOOR. THE SERVICE DOOR STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013524. - [SDR CHQA20120918362](https://openairdocs.org/sdr/CHQA20120918362.md): Support · corroded · Sep 18, 2012 · N272SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK SUPPORT AT FRAME 50. THE SEAT TRACK SUPPORT AT FRAME 50 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20120609183](https://openairdocs.org/sdr/CHQA20120609183.md): Ballast · failed · Jun 8, 2012 · N272SK · Emb EMB145LR · Passenger Compartment Lighting > CREW REPORTED AN ELECTRICAL ODOR FROM THE CEILING LIGHT AT SEAT 1A. REMOVED AND REPLACED CEILING LIGHT BALLAST. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120218054](https://openairdocs.org/sdr/CHQA20120218054.md): Smoke Detector · false indication · Feb 18, 2012 · N272SK · Emb EMB145LR · Smoke Detection > CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A LAVATORY SMOKE WARNING MESSAGE. FLIGHT ATTENDANT VERIFIED THAT THERE WAS NO SMOKE OR ODOR IN THE CABIN. DECLARED AN EMERGENCY AND RETURNED TO FIELD. MESSAGE CLEARED ON LANDING. MAINTENANCE INSPECTED THE - [SDR CHQA201100395](https://openairdocs.org/sdr/CHQA201100395.md): Engine · leaking · Sep 30, 2011 · N272SK · Emb EMB145LR · Engine (Turbine/Turboprop) > CREW REPORTED THAT DURING TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT-HAND ENGINE. ALL LEAK CHECKS AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFEC - [SDR CHQA201100391](https://openairdocs.org/sdr/CHQA201100391.md): Unknown · smoke · Sep 28, 2011 · N272SK · Emb EMB145LR · Air Distribution System > CREW REPORTED THAT DURING CLIMB THERE WAS SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO KDTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT ELECTRICAL SYSTEM, THE WINDSHIELD HEATING SYSTEM, OPERATED BOTH COOLING PACKS, AND PERFORMED ENGINE - [SDR CHQA201100182](https://openairdocs.org/sdr/CHQA201100182.md): Inverter · inoperative · May 20, 2011 · N272SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE UPPER AFT ILLUMINATED PLACARD FOR THE RIGHT OVERWING ESCAPE HATCH WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 5 DC TO AC INVERTER. OPERATIONAL CHECKS OF THE UPPER AFT ILLUMINATED PLACARD FOR THE RIGHT OVERWING ESCAPE HATCH - [SDR CHQA201000145](https://openairdocs.org/sdr/CHQA201000145.md): Light · inoperative · Jul 23, 2010 · N272SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT SEAT 6A WAS INOP. MAINTENANCE REPLACED THE LIGHT STRIP. - [SDR CHQA200900255](https://openairdocs.org/sdr/CHQA200900255.md): Fixture · inoperative · Dec 3, 2009 · N272SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOP. THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA200900154](https://openairdocs.org/sdr/CHQA200900154.md): Bleed Valve · closed · Jul 9, 2009 · N272SK · Emb EMB145LR · Compressor Bleed Valve > FLIGHT 6030 FROM CMH TO JFK. THE FLIGHT CREW RECEIVED A BLEED 2 VALVE CLOSED MESSAGE DURING FLIGHT. THE CREW CYCLED THE VALVE BUT THE MESSAGE REMAINED. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 PRSOV AND THE BL - [SDR CHQA200900103](https://openairdocs.org/sdr/CHQA200900103.md): Connector · unsecure · Apr 8, 2009 · N272SK · Emb EMB145LR · Door System Wiring > FLIGHT 6033, CVG TO MSY. AFTER TAKE-OFF THE CREW RECEIVED A CABIN SERVICE DOOR WARNING ON EICAS AND RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE SERVICE DOOR EICAS INDICATION AND RELEASED THE AIRCRAFT FOR SERVICE. THE DEFERRAL WAS CL - [SDR CHQA200900082](https://openairdocs.org/sdr/CHQA200900082.md): Windshield · cracked · Mar 14, 2009 · N272SK · Emb EMB145LR · Flight Compartment Windows > FLIGHT 6042, CVG TO JAX - THE FLIGHT CREW REPORTED THAT DURING CLIMB AT FL230 THEY HEARD A POP FROM THE CAPTAIN'S WINDSCREEN AND THE OUTSIDE PANE WAS CRACKED. THE FLIGHT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. THE CAPTAIN'S WINDSHIELD WAS REPLACED IAW A - [SDR CHQA200800118](https://openairdocs.org/sdr/CHQA200800118.md): Contactor · faulty · Jun 19, 2008 · N272SK · Emb EMB145LR · Light System Wiring > FLIGHT 6312, CVG TO FWA. WHILE CLIMBING THROUGH 1,000 FT, AN EMERGENCY LIGHTS NOT ARMED WAS DISPLAYED. THE EMERGENCY LIGHTS WERE RESET AND LIGHTS CAME BACK ON ALONG WITH AN ELECTRICAL EMERGENCY ABNORMAL MESSAGE. THE ELECTRICAL PAGE ON THE MFD SHOWED NORMAL - [SDR CHQA200800048](https://openairdocs.org/sdr/CHQA200800048.md): Actuator · out of adjust · Mar 9, 2008 · N272SK · Emb EMB145LR · Engine Thrust Reverser > CMH TO CMH - DURING CLIMB-OUT FROM CMH, THE CREW RECEIVED AN E1 REVERSER DISAGREE MESSAGE ON EICAS. THE CREW LEVELED OFF, FOLLOWED THE APPROPRIATE QRH CHECKLISTS, AND E1 WAS SHUTDOWN. THE AIRCRAFT THEN LANDED AT CMH WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT - [SDR CHQA200600133](https://openairdocs.org/sdr/CHQA200600133.md): Battery Pack · discharged · Oct 8, 2006 · N272SK · Emb EMB145LR · Emergency Lighting > FOUND OVERWING EMERGENCY LIGHT ON RIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 30-50-04-4. - [SDR CHQA200600129](https://openairdocs.org/sdr/CHQA200600129.md): Light · inoperative · Oct 3, 2006 · N272SK · Emb EMB145LR · Emergency Lighting > AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY LIGHT BULB IAW MM 33-50-00. OPS CHECK GOOD. - [SDR CHQA200500160](https://openairdocs.org/sdr/CHQA200500160.md): Starter · smoke · Sep 9, 2005 · N272SK · Emb EMB145LR · Engine Starter > ON PUSHBACK & ENG START, NORMAL UNTIL START OF NR 1 ENG, WHEN START/STOP SELECTOR ENGAGED RECEIVED NO INDICATION OF NORMAL START. NO ROTATION, NO OIL PRESSURE, NO FUEL FLOW, AND NO ITT RISE. ABORTED START, ATTEMPTED A CROSS BLEED START, SAME RESULTS. TAXIED - [SDR CHQA200500100](https://openairdocs.org/sdr/CHQA200500100.md): Battery Pack · unserviceable · May 17, 2005 · N272SK · Emb EMB145LR · Emergency Lighting > ON INITIAL WALK OUT TO THE AIRCRAFT THE EMERGENCY LIGHTS WERE ALL ON. FOUND THE SWITCH IN THE COCKPIT TO BE IN THE OFF POSITION. INSPECTED AIRCRAFT AND FOUND IT TO BE SAFE FOR FERRY FLIGHT FROM TPA TP CMH. REMOVED AND REPLACED ALL FOUR EMERGENCY BATTERY PAC Next page: https://openairdocs.org/deregistered/N272SK-2018-09-19/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 = 'N272SK' AND deregistration_id = 'N272SK-2018-09-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N272SK-2018-09-19/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.