N563RP, cancelled Jul 11, 2018
Service difficulty reports · 39
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 = 'N563RP' AND deregistration_id = 'N563RP-2018-07-11' 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.
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 = 'N563RP' AND deregistration_id = 'N563RP-2018-07-11' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UHLA201512210838Arm · failedTHE MAIN ENTRY DOOR WAS UNABLE TO BE OPENED FROM THE EXTERIOR AND MAINTENANCE FOUND THE LT HINGE AT THE BASE OF THE DOOR INOPERATIVE. MAINTENANCE R & R THE RT MAIN DOOR ROTATING ARM IAW AMM 52-11-03 AFTER WHICH ALL OPERATIONAL CHECKS WERE GOOD. NO FURTHER DESDR UHLA201510230774Step · brokenTHE MAIN ENTRY DOOR STEPS WERE FOUND TO BE BROKEN. MAINTENANCE ADJUSTED THE SPRINGS ON THE MAIN ENTRY DOOR STEPS IAW AMM 52-10-01 AND ALL OPS CHECKS WERE GOOD. NO FURTHER DEFECTS HAVE BEEN NOTED.SDR UHLA201506120495Skin · dentedDURING INSPECTION, THE BAGGAGE COMPARTMENT DOOR WAS FOUND TO BE DENTED. THE DENT WAS REPAIRED IAW SRM 52-30-01.SDR UHLA201506050490Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE UPRIGHT AT FRAME 20 ON THE LT OMEGA BEAM. THE STANTION WAS R & R IAW SRM 51-40-02.SDR UHLA201506040489Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAMES 20-23. THE OMEGA BEAM WAS R & R IAW SRM 51-40-02.SDR UHLA201506010494Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE CAPTAIN'S OTBD FLOOR SILL AT FRAMES 09-12. THE CORROSION WAS REPAIRED IAW ETD 2015-145-053918A.SDR UHLA201506010491Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CAPTAIN'S INBD SEAT TRACK FLOOR GUSSET AT FRAME 08-09. THE CORROSION WAS REPAIRED IAW ETD 2015-145-053918.SDR UHLA201506010488Bushing · migratedDURING INSPECTION, THE RT AILERON DAMPER ATTACH FITTING, OTBD HAT BUSHING WAS FOUND TO BE MIGRATED AND GOUGED. THE FITTING WAS R & R IAW SRM 51-40-02.SDR UHLA201506010487Bushing · migratedDURING INSPECTION, THE RT AILERON PCA ATTACH FITTING HAT BUSHINGS WERE FOUND TO BE MIGRATED AND GOUGED. THE FITTING WAS R & R IAW SRM 51-40-02.SDR UHLA201506010486Bushing · migratedDURING INSPECTION, THE LT AILERON DAMPER ATTACH FITTING, OTBD HAT BUSHING WAS FOUND TO HAVE MIGRATED. THE FITTING WAS R & R IAW SRM 51-21-06.SDR UHLA201506010485Bushing · migratedDURING INSPECTION, THE LT AILERON PCA ATTACH FITTING HAT BUSHINGS WERE FOUND TO HAVE MIGRATED OUT. THE FITTING WAS R & R IAW SRM 51-40-02.SDR UHLA201505310492Stringer · crackedDURING INSPECTION, THE STRINGER STIFFENER 3L WAS FOUND TO BE CRACKED BETWEEN FRAMES 18 AND 19. THE STRINGER STIFFENER WAS R & R IAW SRM 51-40-02.SDR CHQA20141121331Switch · faultyTHE CREW REPORTED THAT THE GUST LOCK LIGHT CAME ON IN CRUISE FLIGHT. THE CREW DECLARED AN EMER & LANDED WITHOUT INCIDENT AT ITS INTENDED DESTINATION. THE GUST LOCK SYS WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 11/22/2014 WHEN MX REPLACED MICRO SWITCH S0658.SDR CHQA20140508146Light · brokenDURING INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10A WAS FOUND TO BE BROKEN. THE FLOOR STRIP WAS REPLACED & ALL OPERATIONAL CHECKS WERE GOOD.SDR CHQA20131229470Battery · dischargedDURING INSPECTION, THE FWD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130608211Frame · damagedFRAME WAS CREASED. THE FRAME WAS REPLACED IAW SRM 51-40-02.SDR CHQA20130608219Stringer · bentDURING INSPECTION, A STRINGER 12L WAS FOUND TO BE BENT BETWEEN FRAMES 71 AND 72. THE STRINGER WAS REPLACED IAW ETD 2012-145-017997-A.SDR CHQA20130608218Frame · damagedDURING INSPECTION, A FINAL REPAIR WAS COMPLETED FOR A DEFERRED MX ITEM ON FRAME 62 AT STRINGER 13L WHICH WAS CREASED. THE FRAME WAS REPAIRED IAW ETD2012-145-017869-D AND SRM 53-00-04.SDR CHQA20130608216Stringer · damagedDURING INSPECTION, A FINAL REPAIR FOR STRINGER 13L DAMAGE BETWEEN FRAME 62 AND FRAME 62A WAS COMPLETED. THE STRINGER WAS REPLACED IAW ETD 2012-145-017997.SDR CHQA20130607217Floor Support · crackedDURING INSPECTION, THE RT SIDE OMEGA BEAM AT FRAME 59 HAS A CRACK IN THE NUT PLATE HOLE. THE BEAM WAS REPAIRED IAW ETD 2013-145-011759.SDR CHQA20130603210Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR LOWER FRAME AROUND THE NUT PLATE HOLES. THE FRAME WAS REPAIRED IAW ETD 2013-145-011762.SDR CHQA20130602213Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR ANGLE AT FRAME 23. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20130601214Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE LOWER DOOR PLATE. THE FRAME WAS REPAIRED IAW SRM 53-31-04 AND SRM 51-40-02.SDR CHQA20130601212Frame · corrodedDURING INSPECTION, A GOUGE WAS FOUND ON FRAME 60 BETWEEN STRINGERS 4L AND 5L. THE FRAME WAS REPAIRED IAW SRM 53-00-04.SDR CHQA20130531215Skin · damagedDURING INSPECTION, THE LEFT HAND ENGINE PYLON WAS FOUND TO HAVE DAMAGE AROUND THE DRILLED SCREW SHANK ON THE UPPER FORWARD SURFACE. THE DAMAGE WAS REPAIRED IAW SRM 54-50-01 AND ETD 2013-145-011772.SDR CHQA20121205451Engine · leakingCREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THEY REPORTED NO VISIBLE SMOKE WAS PRESENT, HOWEVER AN ODOR WAS PRESENT IN THE CABIN. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TASDR CHQA201100496Wire · damagedCREW REPORTED THAT DURING CLIMB, AT 17,000 FEET, THEY RECEIVED A HIGH OIL PRESSURE INDICATION FOR THE NUMBER 2 ENGINE. AFTER LEVELING, THE CREW RAN THE QUICK REFERENCE HANDBOOK AND SET THE NUMBER 2 ENGINE TO IDLE THRUST. THE ENGINE OIL PRESSURE STOPPED INCRESDR CHQA201100489Battery · dischargedDURING INSPECTION, THE EMERGENCY LIGHT POWER SUPPLY IN POSITION 4 FAILED THE FUNCTIONAL CHECK. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100265Floor Support · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OMEGA BEAM BETWEEN FRAMES 23 AND 24 IN CENTER FUSE I. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM BETWEEN FRAME 14 AND FRAME 25 IN ACCORDANCE WITH ETD2011-145-101741.SDR CHQA201100262Spar Cap · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING FRONT SPAR LOWER CAP FROM THE CAP EDGE THROUGH THE SCREW HOLE. THE AIRCRAFT IS CURRENTLY IN C-CHECK INSPECTION.SDR CHQA201100042Inverter · inoperativeDURING INSPECTION, THE FORWARD OVERWING EXIT LOCATOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER FOR THE FORWARD OVERWING EXIT LIGHT LOCATOR. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000007Battery · dischargedDURING INSPECTION THE LAST 4 EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04 AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR CHQA200900138Connector · looseDURING INSPECTION, THE EMERGENCY LIGHT OVER THE MAIN DOOR AND FRONT SIDE OF THE EXIT ROW SIGN WERE INOP WHEN TESTED. MAINTENANCE RE-SECURED ALL CONNECTORS ON THE EMERGENCY LIGHT BATTERY PACKS PER AMM 33-50-00, ALL LIGHTS OPS CHECKED GOOD.SDR CHQA200900085Seal · leakingFLIGHT 6123, MKE TO CVG - CREW REPORTED THAT THE AUTO PRESSURIZATION SYSTEM WAS INOP, BUT DID NOT TRY THE MANUAL MODE BEFORE RETURNING TO MKE. THEY ALSO REPORTED THAT THE MAIN ENTRY DOOR WAS SQUEALING IN FLIGHT. THE AIRCRAFT WAS PRESSURIZED ON THE GROUND ANDSDR CHQA200800156Control Unit · faultyFLIGHT 6349, CVG TO LIT. DURING INITIAL CLIMB THE FLIGHT CREW RECEIVED A PTRIM MAIN INOP MESSAGE ON EICAS. THE CREW PERFORMED THE APROPRIATE QRH CHECKLIST ITEMS AND THE ACFT LANDED WITHOUT INCIDENT BACK AT CVG. MAINTENANCE TROUBLESHOT THE FAULT TO THE HORIZSDR CHQA200800036Engine · making metalCVG TO GSP - AFTER TAKEOFF, THE FLIGHT CREW REPORTED SMOKE IN THE CABIN AND THE AUTO SHUTDOWN OF ENGINE NR 1. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE CMC FOR FAULT CODES AND FOUND MESSAGES FOR OIL DEBRIS, CONTROL SSDR CHQA200600130Battery · dischargedEMERGENCY LIGHTS IN BACK HALF OF AIRPLANE (INSIDE) WERE ON WHEN ARRIVED AT THE AIRCRAFT. AIRPLANE WAS COMPLETELY POWERED DOWN. REMOVED AND REPLACED EMERGENCY BATTERIES.SDR CHQA200600007Bulb · burned outRIGHT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB ON RIGHT AFT EMERGENCY LIGHT IAW EMB MM 33-50-10.SDR CHQA200500174Static Inverter · inoperativeLEFT OVERWING EMERGENCY EXIT MARKER LIGHT INOPERATIVE. REMOVED AND REPLACED NR 4 STATIC INVERTER IAW EMB 145 MM 33-50-11. OPS CHECK GOOD.
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