# Service difficulty reports: N271SK, cancelled Aug 6, 2019 A list on [N271SK, cancelled Aug 6, 2019](https://openairdocs.org/deregistered/N271SK-2019-08-06.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 · 71 reports - [SDR UHLA2015030600152](https://openairdocs.org/sdr/UHLA2015030600152.md): Solenoid · faulty · Mar 6, 2015 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension System > THE CREW REPORTED THAT THEIR WAS A NOISE IN THE COCKPIT DURING CLIMB AND SUSPECTED THE NLG DOORS WERE OPEN. THE CREW DIVERTED THE ACFT AND LANDED WITHOUT INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY FLIGHT AND WAS FERRIED FOR MAINTENANCE. MAINTENANCE REPLACE - [SDR CHQA20141201342](https://openairdocs.org/sdr/CHQA20141201342.md): Pressure Switch · faulty · Dec 1, 2014 · N271SK · Emb EMB145LR · Rudder Control System > THE CREW REPORTED THAT ON CLIMB OUT, THEY RECEIVED A RUDDER OVER BOOST MSG. THE CREW RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE RUDDER SYS 1 PRESS SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20141028325](https://openairdocs.org/sdr/CHQA20141028325.md): Floor Support · corroded · Oct 28, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20 UNDER THE RAMP ANGLE. THE CTR OMEGA BEAM WAS REPAIRED IAW SRM 51-40-02. - [SDR CHQA20141028322](https://openairdocs.org/sdr/CHQA20141028322.md): Fitting · cracked · Oct 28, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE SHEAR CLIP AT FRAME 62 & STRINGERS 6R & 8R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 53-31-04. - [SDR CHQA20141027327](https://openairdocs.org/sdr/CHQA20141027327.md): Fitting · cracked · Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE SHEAR CLIP AT FRAME 80 & STRINGER 8L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141027326](https://openairdocs.org/sdr/CHQA20141027326.md): Floor Support · corroded · Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SUPPORT FROM FRAME 44 TO 50. THE SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141027324](https://openairdocs.org/sdr/CHQA20141027324.md): Support · cracked · Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE LT WING BOX ANGLE SUPPORT WAS FOUND TO BE CRACKED BETWEEN FRAME 44 & 45. THE SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141027323](https://openairdocs.org/sdr/CHQA20141027323.md): Doubler · corroded · Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM PREVIOUS REPAIR AT THE CARBON CROSS MEMBER. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10 & 51-40-02. - [SDR CHQA20131231472](https://openairdocs.org/sdr/CHQA20131231472.md): Battery · discharged · Dec 31, 2013 · N271SK · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE NR 1 EMERGENCY LIGHT BATTERY WAS NOT CHARGING. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130823325](https://openairdocs.org/sdr/CHQA20130823325.md): Ballast · inoperative · Aug 23, 2013 · N271SK · Emb EMB145LR · Passenger Compartment Lighting > DURING TAXI, CREW REPORTED A BURNING ODOR AND VISIBLE SMOKE IN THE CABIN COMING FROM THE CABIN LIGHTING BALLAST AT ROW 1. RETURNED TO GATE, REPLACED BALLAST. NO FURTHER DEFECTS HAVE BEEN NOTED. - [SDR CHQA20130728196](https://openairdocs.org/sdr/CHQA20130728196.md): Flap System · malfunctioned · Jul 28, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control System > DURING CRUISE, RECEIVED A FLAP FAIL MESSAGE. FOLLOWED QUICK REF HANDBOOK AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MX RESET THE FLAP SYS. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130726195](https://openairdocs.org/sdr/CHQA20130726195.md): Control Unit · failed · Jul 26, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control System > DURING FLIGHT, RECEIVED A FLAP LOW SPEED MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLAP ELECTRONIC CONTROL UNIT AND LT VELOCITY SENSOR REPLACED. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130726194](https://openairdocs.org/sdr/CHQA20130726194.md): Velocity Sensor · faulty · Jul 26, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control System > DURING FLIGHT, RECEIVED A FLAP LOW SPEED MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLAP ELECTRONIC CONTROL UNIT AND LT VELOCITY SENSOR WERE REPLACED. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130516165](https://openairdocs.org/sdr/CHQA20130516165.md): Gcu · failed · May 16, 2013 · N271SK · Emb EMB145LR · AC Regulator > CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE GENERATORS DID NOT COME BACK ONLINE. DURING THE RETURN TO FIELD FOR THIS ISSU - [SDR CHQA20130516164](https://openairdocs.org/sdr/CHQA20130516164.md): Generator · failed · May 16, 2013 · N271SK · Emb EMB145LR · DC Generator-Alternator > CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE GENERATORS DID NOT COME BACK ONLINE. DURING THE RETURN TO FIELD FOR THIS ISSU - [SDR CHQA20130416117](https://openairdocs.org/sdr/CHQA20130416117.md): Proximity Switch · faulty · Apr 16, 2013 · N271SK · Emb EMB145LR · Landing Gear Position and Warning > CREW REPORTED THAT ON CLIMBOUT THE LANDING GEAR WOULD NOT RETRACT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE ABLE TO RETRACT THE LANDING GEAR BUT RECEIVED SEVERAL WARNING MESSAGES. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTE - [SDR CHQA20130416116](https://openairdocs.org/sdr/CHQA20130416116.md): Electronic Unit · faulty · Apr 16, 2013 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension System > CREW REPORTED THAT ON CLIMBOUT THE LANDING GEAR WOULD NOT RETRACT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE ABLE TO RETRACT THE LANDING GEAR BUT RECEIVED SEVERAL WARNING MESSAGES. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTE - [SDR CHQA20130326091](https://openairdocs.org/sdr/CHQA20130326091.md): Proximity Sensor · faulty · Mar 26, 2013 · N271SK · Emb EMB145LR · Landing Gear Position and Warning > CREW REPORTED THAT THE LEFT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED WHEN THE LANDING GEAR LEVER WAS SELECTED DOWN. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH LEFT MAIN LANDING GEAR DOWNLOCK PROXI - [SDR CHQA20130324090](https://openairdocs.org/sdr/CHQA20130324090.md): Light · defective · Mar 24, 2013 · N271SK · Emb EMB145LR · Passenger Compartment Lighting > CREW REPORTED THAT DURING LANDING THERE WAS AN ELECTRICAL SMELL COMING FROM THE LIGHTING BALLAST AT ROWS 5 AND 6. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BULBS AT ROWS 5 AND 6. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTE - [SDR CHQA20130126030](https://openairdocs.org/sdr/CHQA20130126030.md): Switch · inoperative · Jan 26, 2013 · N271SK · Emb EMB145LR · Pneumatic Distribution System > CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 VALVE CLOSED MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE DID NOT CLEAR. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED SYSTEM 1 PU - [SDR CHQA20130125029](https://openairdocs.org/sdr/CHQA20130125029.md): Bleed Valve · faulty · Jan 25, 2013 · N271SK · Emb EMB145LR · Compressor Bleed Valve > CREW REPORTED THAT DURING CLIMB, THEY RECEIVED A BLEED 1 VALVE CLOSED MESSAGE ON THE EICAS. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK. THE CREW DIVERTED TO KEVV AND LANDED WITHOUT INCIDENT. MAINTENANCE LOCKED THE BLEED VALVE CLOSED AND DEFERRED THE ITE - [SDR CHQA20121229004](https://openairdocs.org/sdr/CHQA20121229004.md): Thermostat · faulty · Dec 29, 2012 · N271SK · Emb EMB145LR · Pneumatic Distribution System > CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR VALVE THERMOSTAT AND THE FAN AIR VALVE. OPERATIONAL CHECKS WERE GO - [SDR CHQA20121229003](https://openairdocs.org/sdr/CHQA20121229003.md): Valve · faulty · Dec 29, 2012 · N271SK · Emb EMB145LR · Pneumatic Distribution System > CREW REPORTED, DURING FLIGHT THEY RECEIVED A BLEED 1 LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR VALVE THERMOSTAT AND THE FAN AIR VALVE. OPERATIONAL CHECKS WERE GOOD W - [SDR CHQA20121126446](https://openairdocs.org/sdr/CHQA20121126446.md): Strut · low · Nov 26, 2012 · N271SK · Emb EMB145LR · Main Landing Gear Strut/Axle/Truck > CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20121126445](https://openairdocs.org/sdr/CHQA20121126445.md): Strut · low · Nov 26, 2012 · N271SK · Emb EMB145LR · Main Landing Gear Strut/Axle/Truck > CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20121126444](https://openairdocs.org/sdr/CHQA20121126444.md): Strut · low · Nov 26, 2012 · N271SK · Emb EMB145LR · Nose/Tail Landing Gear Strut/Axle > CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120917352](https://openairdocs.org/sdr/CHQA20120917352.md): Engine · failed · Sep 17, 2012 · N271SK · Emb EMB145LR · Engine (Turbine/Turboprop) > CREW REPORTED THAT DURING FLIGHT THAT THE ENGINE 2 OIL PRESSURE DROPPED INTO THE AMBER RANGE AND THE ENGINE ITT ROSE INTO THE RED. THE CREW SHUT DOWN THE ENGINE IN FLIGHT, RAN THE CHECKLIST, AND DECLARED AN EMERGENCY. THE PASSENGER O2 MASKS WERE ALSO DEPLOYE - [SDR CHQA20120907331](https://openairdocs.org/sdr/CHQA20120907331.md): Skin · dented · Sep 7, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING INSPECTION, A DENT WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGERS 10R AND 11R. THE DENT ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGERS 10R AND 11R WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-02. - [SDR CHQA20120906336](https://openairdocs.org/sdr/CHQA20120906336.md): Skin · damaged · Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 12 AND FRAME 13 AND BETWEEN STINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012394 REVISION B, DETAIL H. - [SDR CHQA20120806330](https://openairdocs.org/sdr/CHQA20120806330.md): Skin · damaged · Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 10 AND FRAME 11 ON STRINGERS 21L AND 20L WAS COMPLETED IN ACCORDANCE WITH ETD2012-145-012394 REVISION B, DETAIL E. - [SDR CHQA20120906329](https://openairdocs.org/sdr/CHQA20120906329.md): Skin · damaged · Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 10 AND FRAME 11 ON STRINGERS 21R AND 20R WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012394 REVISION B, DETAIL D. - [SDR CHQA20120906328](https://openairdocs.org/sdr/CHQA20120906328.md): Skin · damaged · Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 11 AND FRAME 12 AND STRINGERS 21L AND 20L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-012394 REVISION B, DETAILS B AND C. - [SDR CHQA20120906327](https://openairdocs.org/sdr/CHQA20120906327.md): Skin · damaged · Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 16 AND FRAME 18 AND STRINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012320A DETAILS E AND F. - [SDR CHQA20120906326](https://openairdocs.org/sdr/CHQA20120906326.md): Skin · damaged · Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 19 AND FRAME 21 AND STRINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012320A. - [SDR CHQA20120903345](https://openairdocs.org/sdr/CHQA20120903345.md): Floor Support · corroded · Sep 3, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT FRAME 23. THE RIGHT OMEGA BEAM AT FRAME 23 WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10. - [SDR CHQA20120830344](https://openairdocs.org/sdr/CHQA20120830344.md): Frame · damaged · Aug 30, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 31 AT STRINGER 15R. FRAME 31 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04. - [SDR CHQA20120829343](https://openairdocs.org/sdr/CHQA20120829343.md): Frame · damaged · Aug 29, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 30 AT STRINGER 15R. FRAME 30 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04. - [SDR CHQA20120829342](https://openairdocs.org/sdr/CHQA20120829342.md): Frame · damaged · Aug 29, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 25 AT STRINGER 15R. FRAME 25 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04. - [SDR CHQA20120827341](https://openairdocs.org/sdr/CHQA20120827341.md): Floor Support · corroded · Aug 27, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE CENTER OMEGA BEAM AROUND THE ANCHOR NUT WAS FOUND CORRODED BETWEEN FRAME 24 AND FRAME 25. THE CENTER OMEGA BEAM AROUND ANCHOR NUT BETWEEN FRAME 24 AND FRAME 25 WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012075. - [SDR CHQA20120824340](https://openairdocs.org/sdr/CHQA20120824340.md): Structure · corroded · Aug 24, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012053. - [SDR CHQA20120824339](https://openairdocs.org/sdr/CHQA20120824339.md): Structure · corroded · Aug 24, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012053. - [SDR CHQA20120823338](https://openairdocs.org/sdr/CHQA20120823338.md): Beam · corroded · Aug 23, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED AND THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20120822346](https://openairdocs.org/sdr/CHQA20120822346.md): Skin · cracked · Aug 22, 2012 · N271SK · Emb EMB145LR · Wing, Plate/Skin > DURING INSPECTION, A CRACK WAS FOUND ON THE LEFT WING UPPER SKIN AT THE GROUND SPOILER CENTER HINGE CUTOUT. THE LEFT WING UPPER SKIN AT THE GROUND SPOILER HINGE CUTOUT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-011887. - [SDR CHQA20120822337](https://openairdocs.org/sdr/CHQA20120822337.md): Floor Support · corroded · Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 HAD AND EXISTING REPAIR THAT WAS FOUND TO BE CORRODED. THE LEFT OMEGA BEAM AT FRAME 20 EXISTING REPAIR WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20120822335](https://openairdocs.org/sdr/CHQA20120822335.md): Angle · cracked · Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA20120822334](https://openairdocs.org/sdr/CHQA20120822334.md): Angle · cracked · Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA20120822333](https://openairdocs.org/sdr/CHQA20120822333.md): Angle · cracked · Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA20120822332](https://openairdocs.org/sdr/CHQA20120822332.md): Angle · cracked · Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA20120822325](https://openairdocs.org/sdr/CHQA20120822325.md): Uplock Bracket · cracked · Aug 22, 2012 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension System > DURING INSPECTION, THE NOSE LANDING GEAR UPLOCK HOLDING BOX LEFT AND RIGHT WALL WAS FOUND CRACKED. THE NOSE LANDING GEAR UPLOCK HOLDING BOX WAS REPAIRED IN ACCORDANCE WITH SRM 53-11-08, 51-40-02, AND AMM 32-33-07. - [SDR CHQA20120822324](https://openairdocs.org/sdr/CHQA20120822324.md): Uplock Bracket · cracked · Aug 22, 2012 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension System > DURING INSPECTION, THE NOSE LANDING GEAR UPLOCK HOLDING BOX LEFT AND RIGHT WALL WAS FOUND CRACKED. THE NOSE LANDING GEAR UPLOCK HOLDING BOX WAS REPAIRED IN ACCORDANCE WITH SRM 53-11-08, 51-40-02, AND AMM 32-33-07. Next page: https://openairdocs.org/deregistered/N271SK-2019-08-06/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 = 'N271SK' AND deregistration_id = 'N271SK-2019-08-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N271SK-2019-08-06/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.