N572RP, cancelled Oct 18, 2019
Service difficulty reports · 43
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 = 'N572RP' AND deregistration_id = 'N572RP-2019-10-18' 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.
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 = 'N572RP' AND deregistration_id = 'N572RP-2019-10-18' 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 CHQA20140501136Fitting · corrodedDURING INSPECTION, THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CRACKED AT STRINGERS 18L & 19L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140427142Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FWD PAX DOOR STRUCTURE. THE LOWER FWD PAX DOOR STRUCTURE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140425132Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140425131Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423144Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER AFT CORNER OF THE MAIN ENTRY DOOR. THE LOWER AFT CORNER STRUCTURE OF THE LOWER MAIN ENTRY DOOR WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423143Reinforcement · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE DOOR STOP REINFORCEMENT INSIDE OF THE FWD FRAME OF THE MAIN ENTRY DOOR. THE DOOR STOP REINFORCEMENT WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423141Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND & A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT ON THE MAIN ENTRY DOOR. THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423140Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR. THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423139Reinforcement · corrodedDURING INSPECTION, CORROSION WAS FOUND AROUND THE THE REINFORCEMENT FOR THE BOTTOM DOOR STOP INSIDE THE AFT STRUCTURE OF THE MAIN ENTRY DOOR. THE DOOR STOP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140423138Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE CARGO DOOR FRAME JUST BELOW THE DOOR BUMPER PLATE. THE FRAME WAS REPAIRED IAW ETD 2014-145-034902.SDR CHQA20140423137Fitting · damagedDURING INSPECTION, THE LT AILERON ACTUATOR ATTACH LUG OTBD HAT BUSHING WAS FOUND TO BE MIGRATING AWAY FROM THE LUG. THE LT AILERON PCA FITTING WAS REPLACED IAW SRM 51-20-01 & SRM 51-40-02.SDR CHQA20140423133Door · chafedDURING INSPECTION, A CHAFE WAS FOUND ON THE INNER AFT FACE OF THE MAIN ENTRY DOOR FOLDING FLAP. THE CHAFE WAS REPAIRED IAW ETD 2014-145-034319.SDR CHQA20140422135Support · corrodedDURING INSPECTION, THE LT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED AT FRAME 45. THE SEAT TRACK SUPPORT WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140422134Doubler · corrodedDURING INSPECTION, A PREVIOUS REPAIR DOUBLER ON THE LT FWD OMEGA BEAM FWD CAP AT FRAME 20 WAS FOUND TO BE CORRODED. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131206442Smoke Detector · false activationCREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE MESSAGE ON CLIMB OUT. THE CREW FURTHER REPORTED NO VISIBLE SMOKE. THE SMELL OF DE-ICING FLUID WAS REPORTED AS PRESENT IN THE AIRCRAFT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX RAN THE ENGS WSDR CHQA20130831331Light · inoperativeDURING INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT OVERWING LIGHT ASSY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130708261Control Valve · faultyCREW REPORTED THAT ON GEAR EXTENSION, RECEIVED A BRAKE DEGRADED MESSAGE ON THE EICAS DISPLAY. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REPLACED THE RT BRAKE CONTROL VALVE. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130405105Switch · dirtyCREW REPORTED THAT THEY RECEIVED A BAGGAGE DOOR INDICATION IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE BAGGAGE DOOR INDICATION. THE DEFERRAL WAS CLEARED ON 4/12/2013 WHEN THE DOOR INDICATION MICROSWITCHES WERESDR CHQA20130117020Tire · separatedCREW REPORTED DURING TAKEOFF THE RIGHT INBOARD MAIN LANDING GEAR TIRE SEPARATED. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT INBOARD MAIN LANDING GEAR TIRE. A TIRE TREAD SEPARATION INSPECTION WAS ALSSDR CHQA20120727247Support Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT STEP SUPPORT FITTING AT THE STEP BUSHING AREAS. MAINTENANCE REPLACED THE FORWARD AND AFT SUPPORT FITTINGS.SDR CHQA20120727246Support Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT STEP SUPPORT FITTING AT THE STEP BUSHING AREAS. MAINTENANCE REPLACED THE FORWARD AND AFT SUPPORT FITTINGS.SDR CHQA20120726242Shear Plate · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR FOOT FRAME 68 BETWEEN STRINGER 6L-7L. MAINTENANCE REPLACED THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L.SDR CHQA20120726241Shear Plate · crackedDURING INSPECTION A CRACK WAS FOUND IN SHEAR FOOT FRAME 61 BETWEEN STRINGER 6R-7R. MAINTENANCE REPLACED THE SHEAR FOOT AT FRAME 61.SDR CHQA20120725240Door Frame · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE MAIN PASSENGER LOWER DOOR FRAME AT THE AFT STOP, SECOND FROM THE BOTTOM, WITH THE DOOR IN THE OPEN POSITION. MAINTENANCE REPAIRED THE DAMAGED AREA IN ACCORDANCE WITH ETD 2012-145-010458.SDR CHQA201100389Wire Harness · defectiveCREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE CREW FOLLOWED ALL CHECKLISTS AND RETURNED TO KDCA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FOUND TO SAFE FOR A FERRY FLIGHT TO KSDF WITH THE LANDING GEAR DOWN AND THE GESDR CHQA201100367Proximity Switch · dirtyCREW REPORTED, COULD NOT LIFT THE LANDING GEAR LEVER AND THE LANDING GEAR WOULD NOT RETRACT. RETURNED TO KIAD AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBRICATED ALL PROXIMITY SWITCHES IN THE LANDING GEAR SYSTEM. OPERATIONAL CHECKS WERE GOOD WITSDR CHQA201100344Skin · scratchedDURING INSPECTION, SEVERAL SCRATCHES WERE FOUND ON THE FUSELAGE UPPER SKIN UNDERNEATH ADF ANTENNA NUMBER 1 AND NUMBER 2. MAINTENANCE REPAIRED THE SCRATCHES ON THE FUSELAGE UPPER SKIN UNDER THE NUMBER 1 AND NUMBER 2 ADF ANTENNA IN ACCORDANCE WITH ETD 2011-145-SDR CHQA201100347Stop Fitting · damagedDURING INSPECTION, THE PASSENGER DOOR STOP WAS FOUND TO BE DAMAGED. MAINTENANCE BLENDED THE PASSENGER DOOR STOPS IN ACCORDANCE WITH SRM 53-21-15. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED IN ACCORDANCE WITH NDI MANUAL, INTRODUCTION PAGE 17E, WITSDR CHQA201100346Bonding Strap · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT AND RIGHT AILERON UPPER SHROUD BONDING STRAP. MAINTENANCE REWORKED THE LEFT AND RIGHT AILERON UPPER SHROUD BONDING STRAP IN ACCORDANCE WITH CPM 51-14-02.SDR CHQA201100345Skin · damagedDURING INSPECTION, THE SKIN WAS FOUND TO BE DAMAGED AND AN ANCHOR NUT MISSING ON RUDDER II, BETWEEN X27083 AND X27621 AS WELL AS BETWEEN ZV1932 AND ZV2277. MAINTENANCE REPAIRED THE SKIN (PN: 120-21755-001) AND ANCHOR NUT ON RUDDER II (PN: 120-20808-509) BETWESDR CHQA201100343Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MIDDLE BEAM AT Y0.0. MAINTENANCE REPLACED THE MIDDLE BEAM AT Y0.0 IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA201100342Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR LOWER STRUCTURE FORWARD AND AFT U-SHAPE. MAINTENANCE REPLACED THE FORWARD (PN:145-24131-009) AND AFT (PN:145-24131-011) U-SHAPE ON THE PASSENGER DOOR LOWER STRUCTURE IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA201100340Beam · corrodedDURING INSPECTION, AN EXISTING REPAIR ON THE LEFT BEAM Y479.0 AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT BEAM, Y479.0 AT FRAME 20 IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA201100314Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGERS 15L AND 16L. MAINTENANCE REPAIRED THE FORWARD FRAME OF THE CARGO DOOR CUT-OUT LOWER PORTION IN ACCORDANCE WITH ETD 2011-145-103278. THE FINAL CORRECTIVE ACTION IS SDR CHQA201100313Shear Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE AFT AND FORWARD L-SHAPE SHEAR CLIP. MAINTENANCE REPAIRED THE FORWARD AND AFT L-SHAPE SHEAR CLIPS IN ACCORDANCE WITH ETD2011-145-103275 REVISION A. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS CARRIED OUT ON THE CSDR CHQA201100348Skin · dentedDURING C-CHECK, A DENT, FORWARD OF THE SERVICE DOOR, ON THE CENTER FUSELAGE I, BETWEEN STRINGERS 12R AND 13R, WAS REPAIRED. THE DENT WAS PREVIOUSLY DEFERRED (DMI 67032/1). THE FINAL REPAIR OF THE DENT, FORWARD OF THE SERVICE DOOR, ON THE CENTER FUSELAGE I, BSDR CHQA201100026Unknown · contaminatedPRIOR TO TAKEOFF THE AIRCRAFT WAS DE-ICED, AND AT APPROXIMATELY 500FT ON TAKEOFF, THE FLIGHT ATTENDANT REPORTED HAZE IN THE CABIN THAT SMELLED LIKE GLYCOL. THERE WERE NO WARNING MESSAGES ON EICAS, AND THE HAZE DISSIPATED QUICKLY. IT WAS DECIDED TO CONTINUE TSDR CHQA200900202Battery Pack · dischargedDURING INSPECTION WHILE TESTING EMERGENCY LIGHT SYSTEM THE OVERWING EMERGENCY LIGHTS WERE INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND THE EMERGENCY LIGHTS OPERATED NORMALLY.SDR CHQA200900061Strut · underservicedUPON GEAR RETRACTION THE CREW RECEIVED A L/G AIR/GND FAIL MESSAGE ON THE EICAS. FOLLOWED SHORTLY BY E1-2 REVERSE DISAGREE MESSAGE. THE CREW RETURNED TO THE FIELD AND BOTH MESSAGES CLEARED ON GEAR EXTENSION. A NORMAL LANDING WAS MADE. UPON INSPECTION BY MAISDR CHQA200700090Warning Message · false activationIND TO CVG - DURING CLIMB-OUT OF IND IN ICING CONDITIONS THE CREW RECEIVED A BLEED 1 LEAK EICAS MESSAGE WITH LEAK ILLUMINATED ON THE ENGINE BLEED VALVE SELECTOR SWITCH. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE SDR CHQA200700010O-Ring · brokenFLIGHT 6218 - CVG-CMH - ON DESCENT INTO CMH, RECEIVED NR 2 ENGINE BLEED LEAK. SHUT OFF ENGINE PER QRH. INTERMITTENTLY IN AND OUT OF ICING CONDITIONS, SHUTTING OFF THE BLEED CAUSED THE WING ANTI-ICE TO FAIL. DECLARED AN EMERGENCY. MAINTENANCE FOUND LEAK AT SDR CHQA200600005Bulb · missingFLOOR PROXIMITY LIGHT STRIP MISSING. INSTALLED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 MM 33-50-12.SDR CHQA200500049Light · inoperativeAFT EMERGENCY FLOOR PROXIMITY LIGHT STRIP IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12-4. OPS CHECK GOOD.
Back to N572RP, cancelled Oct 18, 2019