N295SK, cancelled Jan 18, 2017

Service difficulty reports · 41

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N295SK' AND deregistration_id = 'N295SK-2017-01-18'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CHQA20140908267Trunnion · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT MLG FWD UPPER TRUNNION. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-075943A.Sep 8, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach SectionSDR CHQA20140908266Trunnion · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE RT MLG UPPER FWD TRUNNION. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-075943A.Sep 8, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach SectionSDR CHQA20140827269Bracket · chafedDURING INSPECTION THE LT EMER EXIT DOOR WAS FOUND TO BE CHAFED & BENT ON THE BRACKET ON THE AFT SIDE. THE DOOR WAS REPAIRED IAW ETD 2014-145-073270.Aug 27, 2014 · N295SK · Emb EMB135KL · Emergency ExitsSDR CHQA20140827260Fitting · damagedDURING INSPECTION THE LT AILERON PCA OTBD FITTING WAS FOUND TO HAVE AN ENLARGED HOLE. THE LT AILERON PCA OTBD FITTING WAS REPLACED IAW SRM 51-40-02.Aug 27, 2014 · N295SK · Emb EMB135KL · AileronsSDR CHQA20140826265Bearing · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT MLG UPPER AFT TRUNNION BEARING. THE TRUNNION BEARING WAS REPAIRED IAW ETD 2014-145-075943A.Aug 26, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach SectionSDR CHQA20140824271Skin · dentedDURING INSPECTION A DENT FROM STRIKE DAMAGE BETWEEN FRAME 70 - 72 & STRINGERS 13 - 14R WAS REPAIRED IAW ETD 2014-145-071479.Aug 24, 2014 · N295SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA20140826264Bearing · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE RT MLG UPPER AFT TRUNNION BEARING. THE TRUNNION BEARING WAS REPAIRED IAW ETD 2014-145-075943.Aug 24, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach SectionSDR CHQA20140822263Floor Support · corrodedDURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.Aug 22, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20140822261Repair · corrodedDURING INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM FLOOR FLANGE AT FRAME 20 WAS FOUND TO BE CORRODED. THE FLANGE WAS REPAIRED IAW SRM 53-00-10.Aug 22, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20140820270Skin · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE SKIN AT FRAME 25 & STRINGERS 20 - 21L. THE SKIN WAS REPAIRED IAW SRM 53-22-01.Aug 20, 2014 · N295SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA20140820268Skin · damagedDURING INSPECTION A LIGHTNING STRIKE REPAIR WAS COMPLETED ON NR 1 FRAME 27 - 28 AT STRINGER 21L & FRAME 28 AT STRINGER 18L - 19L. THE REPAIR WAS MADE IAW SRM 53-22-01.Aug 20, 2014 · N295SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA20140820262Repair · chafedDURING INSPECTION A PREVIOUS REPAIR WAS FOUND TO BE CHAFED BELOW ACCESS DOOR 113EL. THE PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM53-11-01.Aug 20, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20130123042Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON SUPPORT WEB FOR AILERON TORQUE TUBE BETWEEN FRAME 13 AND 14 AND STRINGERS 21R AND 20R. THE AILERON TORQUES TUBE SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 23, 2013 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20130123041Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 66 BETWEEN STRINGERS 8L AND 9L. THE DAMAGED SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 53-31-04 AND 51-40-02.Jan 23, 2013 · N295SK · Emb EMB135KL · Fuselage Main, Attach FittingsSDR CHQA20120309082Skin · crackedDURING INSPECTION, THE RIGHT ELEVATOR LEADING EDGE SKIN WAS FOUND TO BE CRACKED AT THE SERVO TAB CONTROL ROD AT STA YH 1310. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS CARRIED OUT WITH NO CRACK LIKE INDICATIONS FOUND. THE RIGHT ELEVATOR LEADING EDGE SKIN AMar 9, 2012 · N295SK · Emb EMB135KL · Elevator, Plate/SkinSDR CHQA20120308081Frame · crackedDURING INSPECTION, THE RIGHT FRAME 10 WAS FOUND TO BE CRACKED. THE RIGHT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Mar 8, 2012 · N295SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA20120308080Frame · crackedDURING INSPECTION, THE LEFT FRAME 10 WAS FOUND TO BE CRACKED. THE LEFT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Mar 8, 2012 · N295SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA20120308079Frame · crackedDURING INSPECTION, THE RIGHT FRAME 23, JUST BEHIND THE RIGHT SILL NUMBER 1 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE RIGHT FRAME 23 JUST BEHIND THE RIGHT SILL NUMBER 1 IN ACCORDANCE WITH ETD 2012-145-003386.Mar 8, 2012 · N295SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA20120308078Skin · gougedDURING INSPECTION, FOUR GOUGES WERE FOUND ON THE LEFT SKIN PANEL BETWEEN FRAME 20 AND FRAME 22 BETWEEN STRINGERS 19L AND 17L. THE LEFT SKIN BETWEEN FRAME 20 AND FRAME 22, AND BETWEEN STRINGERS 19L AND 17L WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-003415.Mar 8, 2012 · N295SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA20120308077Skin · dentedDURING INSPECTION, MULTIPLE DENTS WERE FOUND ON THE RIGHT SKIN BETWEEN FRAME 3 AND FRAME 4, SIX INCHES ABOVE THE NOSE LANDING GEAR DOOR CUTOUT. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH NO CRACK INDICATIONS FOUND. THE RIGHT SKIN BETWEEN FRAMar 8, 2012 · N295SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA201100492Battery · dischargedDURING INSPECTION, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT, CEILING AISLE EMERGENCY LIGHT 1 AND COCKPIT FLOOD LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTEDec 18, 2011 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA201100201Shear Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FRAMES BAGGAGE DOOR SHEAR CLIP. THE DAMAGED AREA OF THE SHEAR CLIP WAS REMOVED AND A NEW SECTION WAS INSTALLED.May 30, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100200Floor Support · damagedDURING INSPECTION THE CENTER FUSELAGE III OMEGA BEAM WAS FOUND TO BE DAMAGED. THE OMEGA BEAM WAS REPAIRED IAW SRM 53-23-02-RE AND EMBRAER ETD 2011-145-100373.May 30, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100215Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE RIGHT OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.May 28, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100214Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE MID OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.May 28, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100213Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.May 28, 2011 · N295SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100051Controller · inoperativeCREW REPORTED, AFTER TAKEOFF WERE UNABLE TO CONTROL THE CABIN ALTITUDE IN MANUAL MODE WHILE THE AUTO MODE WAS ON DEFERRAL. IT WAS REPORTED THAT THE CABIN ALTITUDE WAS CLIMBING AT APPROXIMATELY THE SAME RATE AS THE AIRCRAFT AT ALL SETTINGS. THE AIRCRAFT RETURMar 8, 2011 · N295SK · Emb EMB135KL · Cabin Pressure ControllerSDR CHQA201100034Light · inoperativeDURING INSPECTION, THE LEFT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IN THE LEFT AFT EMERGENCY EXIT LIGHT WITH NO FURTHER DEFECTS NOTED.Feb 8, 2011 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA200900212Light · brokenWHILE REMOVING FLOOR STRIP FOR REMOVAL OF GASPER FAN, THE FLOOR PROX LIGHT STRIP BROKE. THE LIGHT STRIP AT ROW 14A WAS REPLACED AND CHECKED NORMAL PER EMB AMM 33-50-12.Sep 30, 2009 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA200900095Heater · shortedFLIGHT 5323, MKE TO STL - DURING DESCENT INTO STL, AT AROUND 11,000 FT SMOKE WAS SMELLED AND SEEN IN THE COCKPIT. THE CREW FOUND THE SOURCE TO BE AT THE BASE OF THE FIRST OFFICER'S WINDSHIELD. THE APPROACH WAS EXPEDITED AND THE APPROPRIATE CHECK LISTS WERE FMar 31, 2009 · N295SK · Emb EMB135KL · Windshield/Door Rain/Ice RemovalSDR CHQA200900264Proximity Switch · dirtyIMMEDIATELY AFTER TAKEOFF THE CREW RECEIVED A LG AIR/GND FAIL EICAS MESSAGE. THE LANDING GEAR INDICATED 3 GREEN DOWN AND LOCKED WITH THE LEVER DOWN. THE QRH WAS FOLLOWED AND THE ACFT RETURNED AND LANDED WITHOUT INCIDENT. MX CLEANED AND INSPECTED THE LANDINGJan 2, 2009 · N295SK · Emb EMB135KL · Landing Gear Position and WarningSDR CHQA200800173Solenoid · faultyFLIGHT 5325 ICT TO STL. THE FLIGHT CREW REPORTED A LOUD AIR SOUND FROM THE NLG AREA DURING FLIGHT. THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND FOUND THE NLG DOOR COMMAND CIRCUIT BREAKER TRIPPED. THROUGH FURTHER TROUBLESHOOTING, IT WAS FOUNDSep 1, 2008 · N295SK · Emb EMB135KL · Landing Gear Door Retract SectionSDR CHQA200600134Bulb · inoperativeEMERGENCY LIGHT OVER WING EXIT INOPERATIVE. TESTED EMERGENCY LIGHT SYSTEM IAW EMB 140 MM 33-50-00. NO DEFECTS NOTED.Oct 16, 2006 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA200600096Battery · misinstalledPROXIMITY EMERGENCY LIGHT STRIP ON CENTER AISLE FLOOR FRONT HALF NOT WORKING. FOUND BATTERY INSTALLED INCORRECTLY. INSTALLED BATTERY IAW EMB 140 MM 30-50-04. LIGHTS WORK SATISFACTORY.Jul 31, 2006 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA200600095Connector · disconnectedLEFT OVERWING EMERGENCY LIGHT DOES NOT COME ON WHEN SWITCHED TO THE ON POSITION. FOUND LIGHT NOT PLUGGED IN. PLUGGED IN LIGHT AND OPS CHECK GOOD IAW EMB 140 MM 33-50-07.Jul 30, 2006 · N295SK · Emb EMB135KL · Light System WiringSDR CHQA200600094Battery · inoperativeAFT HALF OF EMERGENCY LIGHT ON CEILING PANEL BETWEEN PASSENGER CABIN EMERGENCY EXIT INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB 140 MM 33-50-04. OPS CHECK GOOD.Jul 27, 2006 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA200500136Bulb · burned outLEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IAW EMB 140 MM 33-50-10. OPS CHECK GOOD.Aug 4, 2005 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA200500076Warning System · false indicationWHILE CRUISING AT FL350 BOTH AMBER GUST LOCK WARNING LIGHTS ILLUMINATED. THE QRH PROCEDURES WERE RUN, WHICH AT THE END STATED TO LAND AT THE NEAREST SUITABLE AIRPORT. DISPATCH AND MAINTENANCE CONTROL WERE CONTACTED ABOUT THE PROBLEM AND ADVISED THEM ABOUT THApr 7, 2005 · N295SK · Emb EMB135KL · Gust Lock Damper SystemSDR CHQA200500064Bulb · burned outLEFT HAND AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT HAND AFT OVERWING EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW EMB 140 AMM 33-50-09.Mar 27, 2005 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA000565Battery · inoperativeEMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY IAW EMB 140 AMM 33-50-09. OPS CHECK GOOD.Oct 7, 2004 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA200500010Battery Pack · dischargedLEFT HAND OVERWING FORWARD EMERGENCY LIGHT IS INOP. AISLE EGRESS LIGHT AND CABIN FLOOD LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY EGRESS BATTERY PACK PER EMB 140 MM 33-50-04-5. OPS CHECK GOOD.Jan 21, 2004 · N295SK · Emb EMB135KL · Emergency Lighting
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