N561RP, cancelled Sep 25, 2019
Service difficulty reports · 57
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 = 'N561RP' AND deregistration_id = 'N561RP-2019-09-25' 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 = 'N561RP' AND deregistration_id = 'N561RP-2019-09-25' 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 UHLA201507170565Light · inoperativeDURING INSPECTION, THE EMERGENCY LIGHT STRIP AT ROW 16 WAS FOUND TO BE INOPERATIVE. R & R IAW AMM 33-50-12. NO FURTHER DEFECTS HAVE BEEN NOTED.SDR UHLA2015042000273Solenoid Valve · faultyTHE CREW REPORTED THAT THERE WAS A LOUD AIR NOISE FROM THE FRONT OF THE ACFT AND PRESUMED THAT THE LANDING GEAR DOORS REMAINED OPEN IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NLG DOOR SOLENOID VALVE. OPS CHECSDR CHQA20140515158Floor Support · corrodedDURING INSPECTION, THE CTR OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. THE FRAME WAS REPAIRED IAW SRM 51-40-02.SDR CHQA20140514173Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE FRAME WAS REPLACED IAW SRM 53-0010 & SRM 51-40-02.SDR CHQA20140514162Floor Support · corrodedDURING INSPECTION, THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 & 60. THE BEAM WAS REPAIRED IAW ETD 2014-145-040625.SDR CHQA20140514157Frame · crackedDURING INSPECTION, FRAME 23 AT STRINGER 15L WAS FOUND TO BE CRACKED. FRAME 23 WAS REPAIRED IAW SRM 53-00-04.SDR CHQA20140512161Fitting · damagedDURING INSPECTION, THE LT AILERON PCA ROD END ATTACH FITTING ON THE AILERON OTBD ROD INBD HAT BUSHING WAS FOUND TO BE MIGRATED OUTWARD. THE LT AILERON PCA ROD END ATTACH FITTING WAS REPLACED IAW SRM 51-40-02, 51-20-03 & CPM 51-21-04.SDR CHQA20150512160Fitting · damagedDURING INSPECTION, THE RT AILERON DAMPER ROD END ATTACH FITTING WAS ON THE AILERON INBD HAT BUSHING WAS FOUND TO BE MIGRATED OUT. THE FITTING WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140512159Fitting · gougedDURING INSPECTION, THE LT AILERON DAMPNER ROD END FITTING WAS FOUND TO BE GOUGED ON THE INBD SIDE. THE LT AILERON DAMPNER ROD END FITTING WAS REPLACED IAW SRM 51-60-02.SDR CHQA20140512156Hinge Fitting · damagedDURING INSPECTION, THE RT AILERON OTBD HINGE ATTACH FITTING ON THE AILERON HAT BUSHING WAS FOUND TO BE MIGRATED & THE INBD SIDE HOLE ELONGATED. THE RT AILERON OTBD HINGE FITTING WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140510174Floor Support · corrodedDURING INSPECTION, THE RT OMEGA BEAM REPAIR AT FRAME 23 HAS CORROSION. THE REPAIR DOUBLER WAS REPLACED IAW ETD 2014-145-041404.SDR CHQA20140510168Floor Support · corrodedDURING INSPECTION, THE LT OMEGA BEAM CTR FLOOR FLANGE WAS FOUND TO BE CORRODED AT FRAME 24 & FRAME 25. THE BEAM WAS REPAIRED IAW SRM 53-00-10 & 51-40-02.SDR CHQA20140510166Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 12L. THE Z RIB & L ANGLE WERE REPLACED IAW SRM 51-40-02.SDR CHQA20140510165Rib · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 12L. THE Z RIB & L ANGLE WERE REPLACED IAW SRM 51-40-02.SDR CHQA20140510164Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & MID FRAME AT STRINGER 14L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140510163Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 15L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140510155Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 28 BETWEEN STRINGERS 15R & 16R WERE FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140509172Profile · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STEP SUPPORT BRACKET ON THE MAIN ENTRY DOOR. THE PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140509171Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE AFT FRAME & STRINGER 10L. THE PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140509169Door Frame · corrodedDURING INSPECTION, THE MAIN ENTRY DOOR STRUCTURE AT THE MID AFT FRAME & STRINGER 14 WAS FOUND TO BE CORRODED. THE MID AFT FRAME WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140509167Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE STRUCTURE OF THE MAIN ENTRY DOOR AT THE AFT FRAME AT STRINGER 12L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140509154Nut Plate · corrodedDURING INSPECTION, MULTIPLE AREAS OF CORROSION WERE FOUND ON THE NUTPLATE HOLES IN THE AFT FRAME OF THE MAIN ENTRY DOOR. THE NUTPLATE WAS REPAIRED IAW ETD 2014-145-040679.SDR CHQA20140507170Doubler · gougedDURING INSPECTION, THE DOUBLER AT THE FWD NOSE SECTION BELOW THE EXTERNAL POWER RECEPTACLE ON THE LT SIDE AT FRAME 8 WAS FOUND TO BE GOUGED. THE DOUBLER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140204040Isis · faultedCREW REPORTED THAT DURING FLIGHT THE STANDBY ATTITUDE INDICATOR WENT BLANK & WENT TO, ATT CAGE. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT.. RESET THE ISIS CB, ALL INDICATIONS RETURNED TO NORMAL & NO FURTHER DEFECTS WERE NOTED.SDR CHQA20130520187Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21 AT FRAME 13. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-03.SDR CHQA20130520186Attach Bolt · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FLAP POWER DRIVE UNIT ATTACH POINTS. THE ATTACH POINTS WERE REPAIRED IN ACCORDANCE WITH ETD 2013-145-010207.SDR CHQA20130519191Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT. THE SERVICE DOOR CUT OUT WAS REPAIRED IAW SRM 53-21-02.SDR CHQA20130519190Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT THE SCREW HOLE FRAME 23. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-010149.SDR CHQA20130519189Floor Support · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OUTBOARD OMEGA BEAM SUPPORT BETWEEN FRAMES 47 AND 48. THE OMEGA BEAM SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130519188Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON A REPAIR DOUBLER ON THE INBOARD SIDE OF THE LEFT OMEGA BEAM AT FRAME 20. THE DOUBLER WAS REPLACED IN ACCORDANCE WITH 53-00-10.SDR CHQA20130213049Electronic Unit · faultyCREW REPORTED THAT AFTER TAKEOFF, DURING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR DID NOT SHOW UP AND LOCKED. THE OTHER GEAR HAD GREEN INDICATIONS AND SHOWED UP AND LOCKED. THE CREW ALSO RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE. THEY FOLLOWED THE SDR CHQA20120423131Duct · crackedCREW REPORTED, RECEIVED A BLEED 1 LEAK MESSAGE AFTER TAKEOFF. THE CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE T-DUCT JUST BELOW JOINT 17. OPERATIONAL AND LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120229068Valve · inoperativeCREW REPORTED THAT THERE WAS AN ELECTRICAL BURNING SMELL IN THE COCKPIT UPON ARRIVING AT THE GATE. MAINTENANCE REPLACED THE GASPER VALVE FOR THE LEFT ELECTRICAL FLIGHT INSTRUMENT SYSTEMS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100419Light · inoperativeDURING INSPECTION, THE NUMBER 3 FLOOR PROXIMITY EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 3 FLOOR PROXIMITY EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100366Warning System · false activationCREW REPORTED THAT DURING CLIMB RECEIVED A BLEED 1 LEAK MESSAGE. THE CREW RETURNED TO KDCA AND LANDED WITHOUT INCIDENT. MAINTENANCE EXPOSED ALL JOINTS IN THE BLEED 1 SYSTEM WITH NO LEAKS NOTED. HIGH POWER ENGINE RUNS WERE ALSO PERFORMED WITH NO DEFECTS NOTESDR CHQA201100199Warning System · false activationFLIGHT CREW REPORTED THAT WHILE CLIMBING THROUGH 9,000FT, THE HAD A BLEED 1 LEAK MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT THEN RETURNED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OPS CHECK OF THE SDR CHQA201100179Reinforcement · corrodedDURING INSPECTION, THE TOILET CUP ON THE LOWER AFT FUSELAGE WAS FOUND CORRODED. THE TOILET CUP WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100149Battery Pack · dischargedDURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100126Outflow Valve · inoperativeCREW REPORTED THAT DURING DESCENT FROM FL320 TO FL240 CABIN ALTITUDE STARTED INCREASING. THE CREW DECLARED AN EMERGENCY AND INCREASED THERE DESCENT RATE. THE AIRCRAFT LANDED KCLT WITHOUT INCIDENT. MAINTENANCE FOUND THE MANUAL PRESSURIZATION MODE TO BE OPERASDR CHQA201000211Warning System · false activationDURING GEAR EXTENSION ON FINAL APPROACH, THE CREW REPORTED A BRAKE DEGRADED MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE BRAKE SYSTEM, AND THE BRAKES WERE OPERATING SDR CHQA201000207Light · inoperativeDURING INSPECTION THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. THE BULB WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000138Unknown · malfunctionedCREW REPORTED THAT THE CABIN FAILED TO PRESSURIZE AFTER TAKEOFF. CREW ATTEMPTED MANUAL AND AUTO MODES WITH NO SUCCESS, AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED NUMEROUS OPS CHECKS OF THE CABIN PRESSURIZATION SYSTEM IN BOTH SDR CHQA201000068Battery Pack · dischargedDURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000040Battery Pack · dischargedDURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK PER AMM 33-50-04. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA200900260Light · inoperativeDURING INSPECTION THE NR 2 EMERGENCY LIGHT FLOOR STRIP WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT FLOOR STRIP AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR CHQA200900242Wire · brokenDURING INSPECTION THE NR 4 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REPLACED THE #4 PROXIMITY LIGHT STRIP IAW EMB 145 AMM 32-50-12. OPERATIONAL CHECK GOOD.SDR CHQA200900140Proximity Sensor · crackedFLIGHT 6094, CMH TO BOS. UPON GEAR RETRACTION THE CREW RECEIVED A LG AIR/GND FAIL EICAS MESSAGE. THIRTY SECONDS LATER RECEIVED A TAKEOFF FLAPS MESSAGE WITH NO OTHER MESSAGES. THE GEAR RETRACTED NORMALLY, AND THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TOSDR CHQA200900098Battery Pack · dischargedDURING INSPECTION THE LEFT-HAND OVER WING EMERGENCY LIGHT WAS INOP WHEN TESTED. THE NR 4 EMERGENCY LIGHT POWER SUPPLY WAS REPLACED AND THE SYSTEM OPERATED NORMALLY.SDR CHQA200900077Proximity Switch · faultyFLIGHT 6115, CVG TO CMH, CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE CREW DID NOT ATTEMPT TO RETRACT THE LANDING GEAR AND RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE DOWNLOADED THE CMC AND FOUND CMC MESSAGES FOR THE LSDR CHQA200900052Battery Pack · inoperativeDURING INSPECTION THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOP WHEN TESTED. THE NR 4 EMERGENCY BATTERY WAS REPLACED ALONG WITH THE INVERTER AND THE EMERGENCY LIGHTS OPERATED NORMALLY.
Back to N561RP, cancelled Sep 25, 2019