N552NN
Service difficulty reports · 98
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 = 'N552NN' AND registry_match = 'registration' 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 = 'N552NN' AND registry_match = 'registration' 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 VNAA202308180009Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1574 REV.--SDR VNAA202308180008Skin · wornWEAR ON FUSELAGE SKIN BTW STA 897.70 AND STA 913 STGR 27 ALSO WEAR ON SEVERAL FASTENER HEADS BTW STA. 913 AND STA 927 STGR 27. FUSELAGE SKIN BTW STA 897.70 AND STA 913 STGR 27 BTW STA 913 AND STA 927 STGR 27 WAS REPAIRED PER EA 23-C9-53-0988 REV. IR SECTION ISDR VNAA202308180007Skin · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ/900 SRM 51-2SDR VNAA202308180006Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN BTW FS280.00 AND FS 295.00 AND STGR 26RH AND 25RH. INTERNAL FUSELAGE SKIN BTW FS280.00 AND FS 295.00 AND STGR 26RH AND 25RH WAS REPAIRED PER EA 23-C9-53-0904 REV. IR SECTION III - PERMANENT REPAIRSDR VNAA202308180005Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FS 280.00 AND 295.00 AND STGR 25RH AND 24RH. INTERNAL FUSELAGE SKIN BETWEEN FS 280.00 AND 295.00 AND STGR 25RH AND 24RH WAS REPAIRED PER EA 23-C9-53-0904 REV. IR SECTION III - PERMANENT REPAIRSDR VNAA202308180004Door Sill · corrodedCORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH. CORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 ANSDR VNAA202308180003Drip Tray · corrodedCORROSION ON DRIP TRAY RH AT CROSSBEAM FS:280. EVALUATED, DUE TO EXCESSIVE CORROSION ON DRIP TRAY RH AT CROSSBEAM FS:280 PER CRJ-900 SRM 53-21-43-101-001-A03 AND REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.SDR VNAA202308180002Hinge Fitting · corrodedCORROSION ON HINGE BRACKETS (2EAS) AND HINGE (1 EA) OF AFT LAVATORY SERVICE DOOR. HINGE BRACKETS (2EAS) AND HINGE (1 EA) OF AFT LAVATORY SERVICE DOOR WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01.SDR VNAA202308180001Skin · unknownBURN MARK BY LIGHTNING STRIKE IN TRAILING EDGE OF RH ELEVATOR LOCATED BETWEEN RIB NO. 19./ RIB NO. 20. LIGHTNING STRIKE IN TRAILING EDGE OF RH ELEVATOR LOCATED BETWEEN RIB NO. 19./ RIB NO. 20 WAS REPAIRED PER EA 23-C9-55-0930 REV IR SECTION III PERMANENT REPASDR VNAA202308170007Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% REAR SPAR DATUM (OML TRACE). FWD DRAG ANGLE LH BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% WAS REPAIREDSDR VNAA202308170006Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (642BB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (642BB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WERE BLENDED OUT, EVALUATED WITHIN LIMITS AND REPAIRED PER EA 23SDR VNAA202308170005Skin · nickedSEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND BTW FLS15.00 AND FLS42.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SDR VNAA202308170004Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (542BB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (542BB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER EA 23-C9-57-1085 REV IR, EA 23-C9-57-1084 REV SDR VNAA202308170003Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN, ON STA 1000 TO STA 1096.75 AND BTW STGR 17LH TO STGR 11LH. SEVERAL NICKS ON FUSELAGE SKIN, ON STA 1000 TO STA 1096.75 AND BTW STGR 17LH TO STGR 11LH WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED IS WITHISDR VNAA202308170002Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN, ON STA 977.00 TO STA 1069.75 AND BTW STGR 21LH TO STGR 22RH.SDR VNAA202308170001Hinge · wornPERM REPAIR BEFORE 20,786.18 FH - PAX DOOR PIANO HINGE FUSELAGE SIDE WITHIN 1401.1 FHS FROM IRSDR VNAA202206271113Skin · corrodedPOSSIBLE CORROSION R/H FUSELAGE SKIN BETWEEN FS295.00 AND FS310.00 AND BETWEEN STGR24RH AND STGR25RH / C/W REPAIR TO FUSELAGE SKIN PANEL BTW FS295.00 - FS310.00 @ BTW STR23R - STR26R IAW REO 690-53-21-1525 INSTRUCTIONS. SUBMITTED 2 FORM 337'S AND RECEIVED AIRSDR V0XD20220421001Arm · gougedFWD BAGGAGE DOOR FWD INNER ARM IS GOUGED. CORRECTIVE ACTION: ROTO PEENED AND RESTORED SURFACE JINISH IAW CAVOK EA 21-C9-52-840 REV C, DATED 04-19-2022.SDR V0XD20220419001Hinge · out of tolerancePASSENGER DOOR FUSELAGE HINGE DID NOT PASS THE "GO-NO-GO" GAUGE TEST (IAW BOMBARDIER REO 670-53-21-582 REV. E DATED 2017-06-05). CORRECTIVE ACTION: REMOVED AND REPLACED THE PASSENGER DOOR FUSELAGE HINGE (PN: SH670-31876-13S) IAW CRJ 900 SRM 51-42-06. WORK DOSDR VNAA202201311111Actuator · misriggedEMERGENCY DECLARED GOING INTO JAX DUE TO A REPEAT PITCH FAIL MESSAGE. TRUCKS WERE ROLLED AND FLIGHT LANDED SAFELY. MX HAS BEEN ADVISED. / INTERROGATED MDC FOUND B1 007975. TROUBLESHOT IAW CRJ 900 FIM 27-31-23-810-802-A01. FOUND ACTUATOR TO BE OUT OF RIG. REMOSDR VNAA202106041111Sensor · false indicationDURING FLIGHT, FROM CAK-CLT, CREW HAD INTERMITENT BRAKE OVERHEAT MESSAGE AT FL350. EMERGENCY WAS DECLARED WITH ATC, HOWEVER, ALL INDICATIONS WERE NORMAL DURING APPROACH AND EMERGENCY WAS CANCELLED. NO EMERGENCY VEHICLES WERE ROLLED, NO ANNOUNCEMENT TO BRACE. MSDR VNAA202105131111Windshield · crackedAT FL350, CA NOTICED WINDSHIELD WAS CRACKING IN FRONT OF HIM. HE TOOK THE FLIGHT CONTROLS FROM THE FO, DECLARED AN EMERGENCY, AND DESCENDED INTO SDF. AT SDF, THE EMERGENCY RESPONSE VEHICLES ROLLED, HOWEVER ONCE THE CREW OBSERVED NO FURTHER INCIDENT AT LANDING,SDR VNAA202102031111Anti-Ice Valve · warning messageAT 120KTS, THEY REJECTED TAKEOFF FOR WING ANTI-ICE CAUTION MESSAGE. MX DEFERRED WING ANTI-ICE TEMP SENSOR. WHILE PERFORMING RT WING ANTI-ICE VALVE OPS CHECK, NOTED RT MODULATING AND S/O VALVE OPERATING VERY DELAYED AND SLOW. R & R RT MODULATING AND S/O VALVSDR VNAA2020040911101Battery Pack · dischargedEMERGENCY LIGHT BATTERY NOT CHARGING. REMOVED & REPLACED #3 EPSU BATTERY PACK IAW CRJ900 AMM. OPS CHECK GOOD AT THIS TIME.SDR VNAA2020032811101Ecu · failedFLAPS FAIL AMBER MESSAGE CAME ON DURING CRUISE. REMOVED AND REPLACED SFECU1 IAW CRJ-900 AMM 27-51-05-000/400-801. FLAPS/SLATS OPS CHECK GOOD. SFECU SELF TEST GOOD.SDR VNAA2020032041101Unknown · noisyLOUD BANGING NOISE COMING FROM NOSE AFTER GEAR RETRACTION.GEAR INDICATIONS NORMAL.NO ISSUES NOTED DURING GEAR EXTENSION OR TAXI. C/W EXTERNAL ZONAL INSPECTION OF THE NLG AND DOORS IAW CRJ900 AMM.NO DAMAGE/DEFECTS NOTED. DEFERRED LANDING GEAR RETRACTION SYSTEM.SDR VNAA2020022071101Target · missingAFTER TAKEOFF CREW REPORTED VIA ACARS THAT THE NOSE GEAR DOOR RED MESSAGE HAD APPEARED. CREW RAN QRH WHICH INSTRUCTED THEM TO RETURN TO FIELD. CREW REPORTED VIA ACARS THAT THEY WOULD NOT BE DECLARING AN EMERGENCY. CHARLOTTE OPERATIONS REPORTED THAT EMERGENCY VSDR VNAA2020021281102Hose · cutAFT PORTABLE OXYGEN MASK NOT CONNECTED/HOSE CUT. REMOVED AND REPLACED AFT PORTABLE OXYGEN MASK.SDR VNAA2019121899906Door Frame · corrodedCORROSION AT BOTTOM OF FLIGHT DECK DOOR SURROUND AT FS 280 RBL 11. D.FIGHT 11/22/19 (ROSEM) M/A: 1. NEDD REMOVED ANGLE TO ACCESS CORROSION. R.HENRIQUEZ 11/22/19 C/A: 1. REMOVED ANGLE TO ACCESS CORROSION IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001SDR VNAA2019121899905Seat Track · corrodedRH SIDE SEAT TRACK FS 785-847+8.4 SEGMENT IS CORRODED. FOUND RH SIDE SEAT TRACK TO BE CORRODED BEYOND LIMITS, REQUIRING REPLACEMENT IAW CRJ 900 SRM 53-41-49-101-001-A02. RECEIVED PARTS FROM STORES, READY FOR INSTALLATION. REMOVED RH SIDE SEAT TRACK IAW CRJSDR VNAA2019121899904Seat Track · corrodedLH SIDE SEAT TRACK FS 785-847+8.4 SEGMENT IS CORRODED. F.HENRY 11/16/19 (PCC) M/A: 1. FOUND LH SIDE SEAT TRACK TO BE CORRODED BEYOND LIMITS, REQUIRING REPLACEMENT IAW CRJ 900 SRM 53-41-49-101-001-A02. J.CROSSON,S.SHARTZ 11/18/19 C/A: 1. RECEIVED PARTS FROM STOSDR VNAA2019121899903Drag Angle · crackedLEFT VERTICAL STAB DRAG ANGLE CRACKED. J.SWINK 11/12/19(JW) M/A: 1. L/H VERTICAL STAB DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. J.BARTLETT 11/16/19 C/A: 1. UPON FURTHER INVESTIGATION, FOUND LH AFT DRAG ANGLE TO REQUIRE REPLACEMENT IAW CRJSDR VNAA2019121899902Drag Angle · crackedRIGHT VERTICAL STAB DRAG ANGLE CRACKED. J.SWINK 11/12/19(JW) M/A: 1. R/H VERTICAL STAB DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. J.BARTLETT 11/16/19 C/A: 1. UPON FURTHER INVESTIGATION, FOUND RH AFT DRAG ANGLE TO REQUIRE REPLACEMENT IAW CRSDR VNAA2019121299905Floor Support · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE AT FS 280. ANGLE CORRODED BEYOND LIMITS IAW CRJ900 SRM FIG 53-00-00-901-803. REMOVED FWD J-ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. P/N: CC670-34095-3. NEW SERVICEABLE J-SDR VNAA2019121299904Seat Track · corrodedRH SIDE SEAT TRACK FS 785-847+8.4 SEGMENT IS CORRODED. FOUND RH SIDE SEAT TRACK TO BE CORRODED BEYOND LIMITS, REQUIRING REPLACEMENT IAW CRJ 900 SRM 53-41-49-101-001-A02. RECEIVED PARTS FROM STORES, READY FOR INSTALLATION. REMOVED RH SIDE SEAT TRACK IAW CRJ SDR VNAA2019121299903Seat Track · corrodedLH SIDE SEAT TRACK FS 785-847+8.4 SEGMENT IS CORRODED. FOUND LH SIDE SEAT TRACK TO BE CORRODED BEYOND LIMITS, REQUIRING REPLACEMENT IAW CRJ 900 SRM 53-41-49-101-001-A02. RECEIVED PARTS FROM STORES, READY FOR INSTALLATION. REMOVED LH SIDE SEAT TRACK IAW CRJ SDR VNAA2019121299902Drag Angle · crackedLEFT VERTICAL STAB DRAG ANGLE CRACKED. L/H VERTICAL STAB DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. UPON FURTHER INVESTIGATION, FOUND LH AFT DRAG ANGLE TO REQUIRE REPLACEMENT IAW CRJ900 SRM 55-31-00-201-001-A01. REMOVED LH AFT DRAG ANGLESDR VNAA2019121299901Drag Angle · crackedRIGHT VERTICAL STAB DRAG ANGLE CRACKED. R/H VERTICAL STAB DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. UPON FURTHER INVESTIGATION, FOUND RH AFT DRAG ANGLE TO REQUIRE REPLACEMENT IAW CRJ900 SRM 55-31-00-201-001-A01. REMOVED RH AFT DRAG ANGSDR VNAA2018041311101A/C Pack · malfunctionedSMOKE IN THE CABIN. MX VERIFIED RT PACK RUNNING VERY HOT (FIRE DEPT VERIFIED IT WAS 100 DEG HOTTER THAN THE LEFT WHEN THEY CHECKED IN AFT EQUIP BAY) CAUSING SMOKE AND AUTO-SHUTDOWN. DEFERRED CABIN TEMP CONTROL SYSTEM AND RT PACK. MX REPLACED RH ACM. OPS CHECKSDR VNAA2018011611101Oxygen Mask · unwanted deployDURING LANDING, THE OXYGEN MASK AT ROW 23AC DEPLOYED AND ACTIVATED THE OXYGEN GENERATOR CAUSING A BURNING SMOKE ODOR IN THE AFT LAV. MAINTENANCE REPLACED THE OXYGEN GENERATOR AT ROW 23AC AND WAS RETURNED TO SERVICE.SDR VNAA2017090211101Cooling Fan · failedTHE CREW RECEIVED A DISPLAY COOL CAUTION MESSAGE. FOLLOWED QRH, DECLARED AN EMERGENCY AND RETURNED TO FIELD FOR MAINTENANCE. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIIED TO GATE. MX REMOVED AND REPLACED THE NR 2 DISPLAY FAN, OPS CHECKED GOOD.SDR VNAA2017051700008Spoiler Sys · malfunctionedOUTBOARD FLIGHT SPOILER AND SPOILERON CAUTION MESSAGE, AN EMERGENCY WAS DECLARED. PERFORMED A SYSTEM RESET.SDR VNAA2017051100006Warning Message · illuminatedINBOARD, & OUTBOARD SPOILERONS AND INBOARD, & OUTBOARD FLIGHT SPOILERS MESSAGE, AN EMERGENCY WAS DECLARED.SDR VNAA2017041400012Warning Message · false activationOUTBOARD SPOILERON AND SPOILER CAUTION MESSAGES DURING APPROACH. AN EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED SPOST 2 AND OPS CHECKS, OPS CHECKED GOOD.SDR VNAA2017022500032Unknown · vibrationAT 60 AND 80 KNOTS THE AIRCRAFT SHUTTERED AND PULLED TO THE LEFT. THE CREW REJECTED THE TAKE-OFF FOR SAFETY REASONS. PERFORMED OPERATIONAL TEST OF THE BRAKE SYSTEM AND PERFORMED TAXI CHECK OF THE AIRCRAFT. NO DEFECTS NOTED.SDR VNAA201608120001Acm · smokeSMOKE IN COCKPIT AND CABIN, LEFT PACK TEMPERATURE CAUTION MESSAGE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED AIR CYCLE MACHINE AND PERFORMED CHECKS IAW THEAMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA2016081200010Acm · smokeSMOKE IN COCKPIT AND CABIN, LEFT PACK TEMPERATURE CAUTION MESSAGE. THE CREW DECLARED AND EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, DEFERED LEFT HAND AIR CONDITIONING PACK AND THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENANCE TROUBLESHOTSDR VNAA2016051500010Warning Message · false activationSLATS HALF SPEED ON DEPARTURE WOW, FLAP OVERSPEED, AND STABILIZER TRIM RUNAWAY. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, PERFORMED ELECTRICAL RIGGING OF SLATS, CLEARED INHIBITS, AND PERFORMED CHECKS IAW THE AMM. THE ACF
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