N550NN
Service difficulty reports · 89
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 = 'N550NN' 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 = 'N550NN' 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 VNAA20251004007Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 BTWN STGR 26RH TO 26LH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-21-23-101-003-A02. INTERCSDR VNAA20251004003Support Angle · crackedCRACK ON ANGLE SUPPORT ON FS1098.20 AND STGR24RH ON INTERNAL FUSELAGE STRUCTURE AT AFT EQUIPMENT COMPARTMENT. ANGLE SUPPORT ON FS1098.20 AND STGR24RH ON INTERNAL FUSELAGE STRUCTURE AT AFT EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR VNAA20251005014Skin · damagedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUSDR VNAA20251005013Skin · crackedDISCREPANCY: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% RESDR VNAA20251005011Fitting · gougedIN REFERENCE TO CARD TRFKE00BNCEY': 690-55-31-079-PERM REPAIR BEFORE 25,579.22 FH - GOUGE DAMAGE ON V/STAB TRIM ACTUATOR FITTING THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 4200 FLIGHT HOURS FROM THE EXPIRY OF E.A. 23-C9-55-1132 REV "IR" TIMESDR VNAA20251004013Fitting · damagedIN REFERENCE TO CARD TRFKE00BNCEY': 690-55-31-079-PERM REPAIR BEFORE 25,579.22 FH - GOUGE DAMAGE ON V/STAB TRIM ACTUATOR FITTING THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 4200 FLIGHT HOURS FROM THE EXPIRY OF E.A. 23-C9-55-1132 REV "IR" TIMESDR VNAA20251005010Fitting · damagedIN REFERENCE TO CARD TRFKE00AYDYV': REO 690-55-11-175-4300FH PERM REPAIR - TEMPORARY DISPOSITION FOR BLENDED NICK DAMAGE TO H/S TRIM ACTUATOR FITTING ASSY, RHS (PREVIOUSLY REPAIRED PER E.A. 23-C9-55-1131 REVISION IR) WITHIN 4300FH, REPAIR THE DISCREPANT ITEM ISDR VNAA20251004012Fitting · corrodedPERM REPAIR - TEMPORARY DISPOSITION FOR BLENDED NICK DAMAGE TO H/S TRIM ACTUATOR FITTING ASSY, RHS (PREVIOUSLY REPAIRED PER E.A. 23-C9-55-1131 REVISION IR) WITHIN 4300FH, REPAIR THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES.// ENGINEERING COMMENTSSDR VNAA2024032111101Holder · sparksFO CHART HOLDER LIGHT SPARKED. CBP-2 G6 POPPED OUT. / REMOVED AND INSTALLED FO CHART HOLDER LIGHT ASSEMBLY IAW CRJ 900 AMM 25-18-13-000/400-801-A01-PSA. OPS CHECK GOOD.SDR VNAA202206071111Actuator · unserviceableIN DESCENT JUST PASSED THROUGH 10,000 INTO CLT SLIGHT OSCILLATION, TWO SECONDS LATER PITCH SEAL CAUTION CAME UP, RAN CHECKLISTS DECLARED EMERGENCY SINCE FLIGHT CONTROL RELATED. FOLLOWED QRH, DID NOT LAND OVERWEIGHT, EMS RESPONDED FOR PRECAUTIONARY MEASURES. PISDR V0XD20220405002Skin · damagedRH FUSE SKIN LIGHTNING STRIKES FS202.75 TO FS 661.00 STR 16-20 R- CORRECTIVE ACTION: PERFORMED PERMANT REPAIR TO AREAS AFFECTED IAW OLIVER WYMAN CAVOK EA 21-C953-0640 REB B DATE 03/28/2022 REPAIRS REQUIRE DTE WITHIN 12 MONTHS OF RTS DATE FOR THE SECTION III RESDR V0XD20220405001Skin · damagedRH WING INBD FIXED LE PANEL APPX SS48, CORRECTIVE ACTION: DRESS BACK TO ORIGINAL CONTOUR PERFORMED HFEC TO REWORKED AREA NO FURTHER DEFECTS NOTED. THIS IS CONSIDERED AS PERMANANT REPAIR IAW O;LIVER WYMAN CAVOK EA 21-C9-57-1296 NO DTE REQUIREDSDR V0XD20220324001Skin · gougedGOUGE IN FUSELAGE SKIN FS 913 STR 27, CORRECTIVE ACTION: BLENDED AREA AND INSTALLED REPAIR DOUBLER IAW OLIVER WYMAN CAVOK EA 22-C9-53-0309 REV B DATED 3/23/2022 - DTE TO BE ACCOMPLISHED WITHIN 12 MO OF RETURN TO SERVICE DATE FOR THE SECTION III REPAIR IAW AC SDR V0XD20220327002Arm · gougedCENTER CARGO DOOR FWD INNER ARM HAS GOUGES. CORRECTIVE ACTION: BLEND OUT DAMAGE, SHOT PEEN REWORKED AREAS AND RESTORED FINISHED IAW OLIVER WYMAN CAVOK EA 22-C9-52-0359 REV. IR DATE 03/23/2022.SDR V0XD20220327001Arm · gougedFWD CARGO DOOR AFT INNER ARM HAS GOUGES. CORRECTIVE ACTION: BLEND OUT DAMAGE, SHOT PEEN REWORKED AREAS AND RESTORED FINISHED IAW OLIVER WYMAN CAVOK EA 22-C9-52-0354 REV. IR DATE 3/17/2022.SDR V0XD20220321003None · noneFWD EQUIPMENT COMPARTMENT RH SIDE FLOOR WEB IS CRACKED AT FR. 202 AFT SIDE. CORRECTIVE ACTION: PERFORM REPAIR AT FWD EQUIPMENT COMPARTMENT RH SIDE FLOOR WEB AT FR. 202 AFT SIDE IAW BOMBARDIER REO 670-53-11-509.SDR V0XD20220329001Slider · gougedNUMBER 2 ENGINE UPPER THRUST REVERSER INBOARD SLIDER GOUGED. CORRECTIVE ACTION: BLENDED AREA OF THE NUMBER 2 ENGINE UPPER THRUST REVERSER INBOARD SLIDER REMAINING THICKNESS REMAINING .145MM WITH IN LIMITS IAW BOMBARDIER REO 670-78-34-384 REV D DATE 11/27/2018.SDR V0XD20220324002Frame · corrodedFRAME 349 IS CORRODED BETWEEN STR. 26L AND STR. 27. CORRECTIVE ACTION: REMOVED AND REPLACED FRAME 349 BETWEEN STR. 24R. TO STR. 24L IAW CRJ 900 SRM 51-42-06, SRM 51-42-21.SDR V0XD20220407003Strap · wornNUMBER 2 ENGINE UPPER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP WORN. CORRECTIVE ACTION: REMOVED AND REPLACED (P/N: 2219-T81) NUMBER 2 ENGINE UPPER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP IAW CRJ 900 SRM 54-23-00.SDR V0XD20220407002Strap · wornNUMBER 1 ENGINE UPPER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP WORN. CORRECTIVE ACTION: REMOVED AND REPLACED (P/N: 2219-T81) NUMBER 1 ENGINE UPPER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP.SDR V0XD20220407001Strap · wornNUMBER 1 ENGINE LOWER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP WORN. CORRECTIVE ACTION REMOVED AND REPLACED (P/N: 2219-T81.040) NUMBER 1 ENGINE LOWER COWLING AFT OUTBOARD TRAILING EDGE INTERNAL CHAF STRAP.SDR V0XD20220321004None · noneAFT CARGO FLIP STEP HINGES ARE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CARGO FLIP STEP HINGES IAW CRJ 900 SRM 51-42-06.SDR V0XD20220323001None · noneLIGHTNING STRIKE DAMAGE AT STA 477.4 STR. 16L AND 18L. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR OLIVER WYMAN CAVOK EA 22-C9-53-0268 REV. IR DATE 03/10/2022.SDR V0XD20220328001None · noneDENT IN FUSELAGE BELLY SKIN AT FS 270 BETWEEN STR 23L AND STR 24 L. CORRECTIVE ACTION: DRESS BACK TO ORIGINAL CONTOUR AT FS 270 BETWEEN STR 23L AND STR 24 L AND RESTOR TO FINISH IAW OLIVER WYMAN CAVOK EA 22-C9-53-0355 REV A DATE 03/27/2022.SDR VNAA2020080511102Controller · failedON APPROACH TO TLH AT 5000 FT THE CAPTAIN'S SIDE WIND SHIELD SHATTERED. REMOVED AND REPLACED L/H WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED L/H FWD CAPTAINS HEATER CONTROLLER IAW CRJ 900 AMM 30-41-06-SDR VNAA2020070211104Battery · dischargedROW 16 FLOOR LEVEL EMERGENCY EXIT SIGNS NOT ILLUMINATED. REMOVED AND REPLACED POWER SUPPLY BATTERY. OPS CHECKS GOOD.SDR VNAA20200215101Hose · failedDURING CLIMB THE CREW RECEIVED A NOSE WHEEL STEERING MSG AND THE GEAR WOULD NOT RETRACT. THEY RETURNED TO IAD. THE AIRCRAFT LANDED SAFELY BUT IS BEING TOWED TO THE GATE AS A PRECAUTION. ATC DECLARED AN EMERGENCY AND TRUCKS ROLLED. THE AIRCRAFT IS CURRENTLY SDR VNAA2019102951101Acm · failedUPON LANDING R. PACK AUTOFAIL CAUTION MESSAGE ILLUMINATED WITH SMOKE IN THE CABIN. DEFERRED RH AIRCONDITIONING PACK. REMOVED AND REPLACED RH AIR CYCLE MACHINE IAW CRJ-900 AMM. OPS AND LEAK CHECKS GOOD.SDR VNAA201910121106Light · not reportedR&R PAX DOOR EMERGENCY LIGHT IAW CRJ900 AMM 33-51-15-000/400-801. OPS TEST GOOD AT THIS TIME.SDR VNAA2019022611101Lever · failedDURING CLIMB THE CREW RECEIVED A GEAR DISAGREE MSG. THEY RAN THE QRH, DECLARED AN EMERGENCY AND RETURNED TO CLT. TRUCKS ROLLED. THE AIRCRAFT LANDED SAFELY AND WAS ABLE TO TAXI TO THE GATE WITH NO ISSUES. REMOVED AND REPLACED THE LANDING GEAR SELECT HANDLE ASDR VNAA2019022291101Warning Message · false activationAIRCRAFT GOT GEAR DISAGREE MESSAGE SHORTLY AFTER TAKE-OFF. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. MAINTENANCE REPLACED THE PSEU AND PERFORMED GEAR SWINGS, OPS CHECK GOOD.SDR VNAA2018083011101Spoiler Sys · unknownTHE CREW HAD A FLIGHT SPOILERON ISSUE DURING APPROACH, SO THEY DECLARED AN EMERGENCY SO THEY COULD LAND ON THE LONGEST RWY IN ATL. EMERGENCY VEHICLES DID ROLL. THE CREW DID NOT INSTRUCT THE PASSENGERS TO BRACE. LANDED WITH NO ISSUES AND IS NOW AT THE GATE. SDR VNAA2017061700003Hose · disconnectedLOUD NOISE AND ODOR COMING FROM ROWS 18-20. RECONNECTED THE PASSENGER SERVICE UNIT AIR HOSE.SDR VNAA2017011400016Cable · brokenPASSENGER DOOR ASSIST CABLE BROKEN. REMOVED AND REPLACED PASSENGER DOOR ASSIST MOTOR.SDR VNAA2016071200013Rivet · corrodedBS 280, TWO RIVETS ON LEFT CORROSION PLATE CORRODED AT LBL 9. MAINTENANCE REMOVED AND REPLACED TWO RIVETS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY MAINTENANCE CHECKS.SDR VNAA2016071200012Angle · corrodedBS 280 FWD J-ANGLE CORRODED. MAINTENANCE REMOVED CORROSION IAW THE AMM.SDR VNAA2016053100032Detector · faultyFLAPS FAIL C-MESSAGE. THE CREW DECLARED AN EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RT OTBD FLAP SKEW DETECTOR IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.SDR VNAA2016012500025Controller · failedCREW REPORTED CABIN ALTITUDE RED MESSAGE AROUND FLIGHT LEVEL 350. CABIN ALTITUDE WAS 5900. CREW FOLLOWED PROCEDURES, INITITIATED EMERGENCY DESCENT AND DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL. CREW STOPPED DESCENT AFTER MESSAGE EXTINGUISHED AND CANCELSDR VNAA2015062400036Connector · looseCREW REPORTED RED BRAKE OVERHEAT MESSAGE AT APPROXIMATELY 200 FT AGL AFTER TAKEOFF AND REPORTED LT INBD BRAKE INDICATION HIGH. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT BRAKE SYS, TIGHTENED THE CONNECTORS AND PERFORMED CHE
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