Boeing 737-7CT

Service difficulty reports · 2,415

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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 aircraft_model_key = '7377CT'
  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.

SDR SWAA2015021036496Frame · crackedFRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.Jan 13, 2015 · N566WN · Boeing 7377CT · Fuselage Main, FrameSDR SWAA2015021036495Frame · crackedFRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.Jan 13, 2015 · N566WN · Boeing 7377CT · Fuselage Main, FrameSDR SWAA1933050137163Floorbeam · crackedFORWARD FLOORBEAM UPPER FLANGE CRACKED AT BS 727B, RBL 25. REPAIRED FLANGE IAW ER & EA.Jan 12, 2015 · N566WN · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2015030537159Floorbeam · crackedFORWARD FLOORBEAM UPPER FLANGE CRACKED AT BS 727B, RBL 45. REPAIRED FLANGE IAW ER & EA.Jan 12, 2015 · N566WN · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2015030337056Support Channel · crackedLEFT HORIZONTAL STABILIZER ON SUPPORT CHANNEL FOR ELEVATOR BALANCE PANEL AT REAR SPAR FAIL SAFE CHORD BETWEEN STAB STATION 129.50 TO 138.70. REPAIRED CHANNEL IAW EA.Jan 12, 2015 · N566WN · Boeing 7377CT · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2015021236582Floorbeam · crackedFLOORBEAM UPPER FLANGE CRACKED FWD OF BS 727B, LBL 25. REPAIRED FLOORBEAM IAW ER & EA.Jan 12, 2015 · N566WN · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2015021236581Floorbeam · crackedFLOORBEAM UPPER FLANGE CRACKED FWD OF BS 727B, LBL 45. REPAIRED FLOORBEAM IAW ER & EA.Jan 12, 2015 · N566WN · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2015021036439Seat Track · crackedAFT SEAT TRACK CRACKED AT BS 727B, LBL 45 OTBD FLANGE. REPAIRED SEAT TRACK IAW EA.Jan 12, 2015 · N566WN · Boeing 7377CT · Fuselage, Seat/Cargo Attach FittingsSDR CA150112014Actuator · failed(CAN) ON CLIMB THROUGH FL200 THERE WAS A BURNING ODOR THROUGH THE CABIN FOLLOWED BY RIGHT PACK TRIP OFF LIGHT. THE NON-NORMAL CHECKLIST WAS CARRIED OUT, THE RIGHT PACK TRIP OFF LIGHT STAYED ON. THE AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE FOUND CONSTANJan 9, 2015 · Boeing 7377CT · Cabin Cooling SystemSDR SWAA2015022436854Frame · corrodedAFT CARGO BAY ON FRAME INBD FLANGE CORRODED AT BS 792, STRINGER 25R. REPAIRED FLANGE IAW ER & EA.Jan 9, 2015 · N566WN · Boeing 7377CT · Fuselage Main, FrameSDR SWAA2015021036447Threshold · corrodedAFT CARGO BAY ON SUB THRESHOLD WEB, LOWER SURFACE AT NUTPLATE CORRODED BETWEEN BS 807 - 827, BETWEEN RBL 20 - RBL 27. R & R WEB IAW SRM & DWG.Jan 9, 2015 · N566WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2015021036446Frame Splice · corrodedAFT CARGO BAY ON FRAME SPLICE CORRODED AT BS 787, STRINGER 25R. R & R SPLICE IAW SRM.Jan 9, 2015 · N566WN · Boeing 7377CT · Fuselage Main, FrameSDR SWAA2015021036445Plate · corrodedAFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727+4 - 767, RBL 21. R & R PLATE IAW SRM & DWG.Jan 9, 2015 · N566WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2015021036444Plate · corrodedAFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727+4 - 847, LBL 21. R & R PLATE IAW SRM.Jan 9, 2015 · N566WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2015021036438Support Channel · crackedAFT CARGO BAY BULKHEAD LINER SUPPORT CHANNEL CRACKED AT BS 727+4, RBL 4. R & R CHANNEL IAW SRM & DWG.Jan 9, 2015 · N566WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2015021936726Post · crackedLEFT NR 3 WINDOW FRAME E - F POST, SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.Jan 8, 2015 · N566WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR CA150112006Line · ruptured(CAN) CREW REPORTED THAT THE "ELEC 1" LOW PRESSURE LIGHT ILLUMINATED ON TAXI-IN. SYSTEM B HYDRAULIC QUANTITY INDICATED ZERO, UPON INSPECTIONTHE "B" SYSTEM ACOUSTIC FILTER FLEX LINE IN THE WHEEL WELL WAS FOUND RUPTURED. MAINTENANCE REPLACED THE LINE IAW AMM 20-Jan 7, 2015 · Boeing 7377CT · Hydraulic System, MainSDR SWAA2019031930752Floor Panel · damagedFLOOR PANEL 221BF OUTBOARD EDGE AND OUTBOARD AFT CORNER DAMAGED. REPAIRED PANEL IAW SRM.Jan 6, 2015 · N566WN · Boeing 7377CT · Fuselage Floor PanelSDR CA150106004Window · failed(CAN) WHILE SITTING AT THE GATE THE CAPT`S NR 2 WINDOW SHATTERED. THE WINDOW WAS REPLACED IAW AMM 56-12-11.Jan 6, 2015 · Boeing 7377CT · Flight Compartment WindowsSDR SWAA2015020436330Floorbeam · crackedFLOOR SUPPORT CRACKED AT BS 540, BETWEEN RBL 25 TO 45 ATBD AFT FASTENER. R & R SUPPORT IAW SRM.Jan 6, 2015 · N566WN · Boeing 7377CT · Fuselage Main, Floor BeamSDR CA150108013Transmitter · failed(CAN) TRAILING EDGE FLAPS DID NOT EXTEND PAST POSITION 5. USED ALTERNATE FLAPS SYSTEM TO EXTEND FLAPS TO 15 AS PER TRAILING EDGE FLAPS DISAGREE CHECKLIST. PER FIM 27-51 TASK 820, RIGHT FLAP POSITION TRANSMITTER REPLACED IAW AMM 27-58-01. REPAIR CONFIRMATION Jan 5, 2015 · Boeing 7377CT · Trailing Flap Position Indicating SystemSDR SWAA2015022536883Doubler · crackedELECTRICAL GND POWER RECEPTACLE SURROUND DOUBLER DOOR 114AR CUT OUT CRACKED, FWD SIDE BELOW LOWER DOOR HINGE. REPAIRED DOUBLER IAW EA.Jan 5, 2015 · N566WN · Boeing 7377CT · Fuselage Main, Plate/SkinSDR CA150105008Toilet · inoperative(CAN) AFTER DEPARTING FROM MCO IT WAS DISCOVERED THAT BOTH THE FORWARD AND AFT LAVATORY TOILETS WOULD NOT FLUSH. PRIOR TO DISPATCH THE LAVATORY MOTOR BLOWER WAS MEL IN THIS CONFIGURATION THE VACUUM WASTE SYSTEM USES NEGATIVE PRESSURE AT ALTITUDE TO FLUSH THE TJan 4, 2015 · Boeing 7377CT · Waste Disposal SystemSDR CA141110010Window · cracked(CAN) JUST AFTER TAKEOFF, A SPARK WAS NOTICED IN THE TOP R/H CORNER OF THE L1 WINDOW. A SECOND SPARK WAS FOLLOWED 5-10 SECONDS LATER AND THE OUTER PANE OF WINDOW CRACKED. ATC WAS ADVISED AND THE FLIGHT ENTERED A HOLDING PATTERN TO MEET MAX LANDING WEIGHT BEFORNov 9, 2014 · Boeing 7377CT · Flight Compartment WindowsSDR CA141031010Motor · failed(CAN) AFTER TAKEOFF THE ELECTRIC STAB TRIM FAILED, MANUAL STAB TRIM WAS STILL OPERABLE. THERE WAS A SPEED TRIM FAIL AND STAB OUT OF TRIM ANNUNCIATION. THE CREW CARRIED OUT AN AIR TURN BACK AND LANDED WITHOUT INCIDENT. YYC MAINTENANCE IN ACCORDANCE WITH FAULT IOct 31, 2014 · Boeing 7377CT · Stabilizer Control SystemSDR CA141031018Control Box · odor(CAN) THE FLIGHT CREW REPORTED A BURNING PLASTIC ODOR AROUND ROW 21. MAINTENANCE ISOLATED FAULT TO LTV BOX AT ROW 21 D-E-F. LIVE TV SYSTEM WAS DEACTIVATED AND SYSTEM PLACED ON MEL. FURTHER TROUBLESHOOTING IS REQUIRED TO IDENTIFY THE UNIT THAT CAUSED THE ISSUE Oct 27, 2014 · Boeing 7377CT · Entertainment SystemSDR CA141021007Video Display · failed(CAN) CREW NOTICED STRONG BURNING ODOR FROM ROW 18A, ASSOCIATED WITH LIVE TV SCREEN FAILURE. ODOR DISSIPATED QUICKLY. VIDEO DISPLAY UNIT AND VDU CABLES WHERE REMOVED. SYSTEM TESTED SERVICEABLE AND NO OTHER DEFECTS WERE NOTED.Oct 17, 2014 · Boeing 7377CT · Entertainment SystemSDR CA141014019Regulator · failed(CAN) DURING CRUISE THERE WAS A NR 2 ENGINE BLEED TRIP INDICATION AND EXTINGUISHED AFTER RESET. THE AIRCRAFT HAD HISTORY OF THIS DEFECT. THE AIRCRAFT WAS DIVERTED FOR COMPANY CONVENIENCE. MAINTENANCE FOUND A FAILED BLEED AIR REGULATOR AND A FAILED HIGH STAGE ROct 12, 2014 · Boeing 7377CT · Pneumatic Distribution SystemSDR CA141010017Outlet · shorted(CAN) DURING AIRCRAFT CLEANING, ON THE GROUND IN POS, WHEN THE GROOMER PLUGGED IN HIS VACUUM AT THE AFT RIGHT HAND DOOR AC OUTLET, SMOKE AND SPARKS WERE SEEN COMING FROM THE OUTLET. FLIGHT CREW WAS INFORMED AND NO BARKERS WHERE FOUND POPPED. SYSTEM WAS DEACTIVOct 9, 2014 · Boeing 7377CT · Equipment/Furnishings WiringSDR CA141006020Window · overheated(CAN) DURING PRE-TAXI, CREW REPORT A L2 WINDOW OVERHEAT LIGHT ILLUMINATED. THE WINDOW WAS HOT TO TOUCH AND AN ACRID BURNING SMELL WAS PRESENT. TROUBLESHOOTING WAS CARRIED OUT IAW FIM 30-41, TASK 811 AND FOUND THE LT SIDE WINDOW TO BE AT FAULT. WINDOW WAS FOUOct 3, 2014 · Boeing 7377CT · Flight Compartment WindowsSDR CA140909006Connector · shorted(CAN) CREW REPORTED THEY COULD NOT START NR 1 ENGINE. THEY HAD FUEL FLOW BUT NO EGT. ACFT RETURN TO GATE. MAINTENANCE FOUND NR 1 ENGINE ELECTRONIC ENGINE CONTROL CHANNEL A ALT POWER BREAKER POPPED AND WILL NOT RESET WHEN ELECTRONIC ENGINE CONTROL POWERED, ADSep 5, 2014 · Boeing 7377CT · Turbine Engine System WiringSDR CA140829004Connector · shorted(CAN) CREW REPORTED THAT ON TAXI NR 2 ENGINE COWL ANT-ICE LIGHT CAME ON, ACCOMPANIED BY A BUZZING NOISE AND AN ELECTRICAL SMELL, SUBSEQUENTLY THE COWL ANT-ICE BULBS BURNT OUT. DURING TROUBLESHOOTING MAINTENANCE FOUND THE NR 2 ENGINE LT IGNITION CB OUT. INVESTIAug 28, 2014 · Boeing 7377CT · Equipment/Furnishings WiringSDR CA140825001Switch · failed(CAN) WHEN THE LANDING GEAR WAS SELECTED UP, ALL 3 LANDING GEAR GREEN LIGHTS EXTINGUISHED, HOWEVER, THE 3 RED LANDING GEAR LIGHTS REMAINED ILLUMINATED. THE CREW FOLLOWED THE "GEAR DISAGREE" CHECKLIST INCLUDING CYCLING THE MAIN GEAR EXTENSION HANDLE A SECOND TIAug 24, 2014 · Boeing 7377CT · Landing Gear Retraction/Extension SystemSDR CA140822008Wire Harness · failed(CAN) DURING CRUISE THE ENGINE 2, ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED. THE ENGINE 2 IDG DRIVE LIGHT ALSO ILLUMINATED. THE CREW CARRIED OUT AN AIR TURN BACK. MAINTENANCE CARRIED OUT A FUNCTION CHECK OF THE ENGINE DRIVEN HYDRAULIC PUMPAug 22, 2014 · Boeing 7377CT · Electrical Power System WiringSDR CA140822007Controller · failed(CAN) AUGUST 20 2014. SHORTLY AFTER LEVELING OFF AT CRUISE ALT OF FL390 LEVELING OFF AT FL390 THE AUTO FAIL AMBER ANNUNCIATOR ILLUMINATED, CREW RAN THE NON-NORMAL CHECKLIST AND POSITIONED THE MODE SELECTOR TO ALTN HOWEVER FAULT STILL REMAINED AND SYSTEM DID NOAug 20, 2014 · Boeing 7377CT · Cabin Pressure ControllerSDR CA140717008Tire · failed(CAN) DURING THE TAKEOFF ROLL THERE WAS A VIBRATION FELT IN THE AIRFRAME. A HIGH ENERGY STOP WAS CARRIED OUT. THE NR 2 MAIN WHEEL TIRE BLEW. THE WHEEL ASSEMBLY & ASSOCIATED BRAKE WERE REPLACED. A HIGH ENERGY STOP INSPECTION CARRIED OUT & THE FIXED TRAILINGJul 16, 2014 · Boeing 7377CT · TireSDR CA140729007Control Panel · failed(CAN) DURING CLIMB OUT WITH AUTOPILOT "A" OR "B" ENGAGED, ENCOUNTERED CONSTANT TRIMMING OF AIRCRAFT NOSE UP AND THEN NOSE DOWN ALMOST CONTINUOUSLY. MAINTENANCE ADVISED A RETURN. DURING RETURN OCCURED AGAIN IN LEVEL FLIGHT AND HELD AT 12000FT. THE MODE CONTROL Jul 12, 2014 · Boeing 7377CT · Autopilot SystemSDR CA140714003Outflow Valve · failed(CAN) CREW PERFORMED AN AIR TURN BACK DUE TO UPON LEVEL OFF AT FL400 CABIN ALT WARNING HORN SOUNDED. CABIN ALT AT 10000 FT AND CLIMBING AT 500 FPM. THEN EQUIP COOLING "OFF" ILLUMINATED. WHEN POWER REDUCED FOR DESCENT, CABIN CLIMB INCREASED TO 2000FPM. NOTE: OUJul 11, 2014 · Boeing 7377CT · Pressure Regulator/Outflow ValveSDR CA140709006Transceiver · failed(CAN) DURING TAKEOFF, THE AIRCRAFT EXPERIENCE A FAILURE OF THE WEATHER RADAR AND PREDICTIVE WIND SHEAR SYSTEMS. AIRCRAFT PERFORMED AN AIR TURNBACK. THE SYSTEM WAS TESTED IAW FIM 34-43-801, NO DEFECT WERE FOUND. IT WAS NOTED THAT THE COOLING FAN WAS FOUND TOJul 8, 2014 · Boeing 7377CT · Weather Radar SystemSDR CA140630027Radar · failed(CAN) PREFORMED AN AIR TURN BACK DUE TO THE WEATHER RADAR NOT WORKING. CREW NOTED THAT THE WEATHER RADAR DISPLAY WAS BLANK ON BOTH SIDES. CIRCUIT BREAKER P6-1, D13 WAS FOUND EXTENDED. ACFT RETURNED FOR MAINTENANCE. THE CIRCUIT BREAKER WAS RESET AND OPS TESJun 28, 2014 · Boeing 7377CT · Weather Radar SystemSDR CA140624005Switch · loose(CAN) DURING TAKEOFF, THE FLIGHT CREW REPORTED THE GEAR WOULD NOT RETRACT WHEN SELECTED UP. THE APPLICABLE CHECKLIST WAS CARRIED OUT AND THE GEAR RETRACTED ON THE SECOND ATTEMPT. AFTER AN UNEVENTFUL LANDING, MAINTENANCE CARRIED OUT THE FOLLOWING ACTIONS BEFOJun 24, 2014 · Boeing 7377CT · Door Warning SystemSDR CA140716010Ground Wire · damaged(CAN) WJ IS EXPERIENCED NUMEROUS FDR LIGHT ILLUMINATED ON ONE OF IT`S A/C. BITE AND SYSTEM TESTED AS PER FIM AND AMM DID NOT REVEAL ANY FAULTS WITH THE SYSTEM. AFTER THE ORIGINAL NFF, WJ PROACTIVELY REPLACED THE PROBABLE CAUSE UNITS (FDR, FDAU, RELAYS). AFTER Jun 15, 2014 · Boeing 7377CT · Instrument System WiringSDR CA140604012Bumper · detached(CAN) WHILE AT THE GATE, CREW REPORTED THAT L2 DOOR OPENS ONLY HALF WAY. UPON INVESTIGATION MAINTENANCE FOUND ON THE L2 DOOR THE RUBBER BUMPER THAT IS LOCATED ON THE LOWER LINK HINGE AND HINGE ARM HAD WAS FOUND DETACHED AND IN THE CUTOUT. THE BUMPER WAS REINSTMay 30, 2014 · Boeing 7377CT · Passenger/Crew DoorsSDR CA140602027Actuator · failed(CAN) DURING CRUISE THE FLIGHT CREW NOTICED THE FUEL CROSS FEED CIRCUIT BREAKER HAD TRIPPED. A DIVERSION WAS CARRIED OUT AND THE ACFT LANDED WITH A MINOR FUEL IMBALANCE BUT WITHOUT INCIDENT. MAINTENANCE CARRIED OUT THE FOLLOWING ACTIONS BEFORE SUCCESSFULLY RMay 29, 2014 · Boeing 7377CT · Aircraft Fuel Distribution SystemSDR CA140602029Guide Arm · binding(CAN) CREW REPORTED L2 DOOR JAMS HALFWAY DURING OPENING. MAINTENANCE REPLACED THE GUIDE ARM ASSY AND ROLLER AND CARRIED OUT DOOR RIGGING IAW AMM 52-13-00.May 27, 2014 · Boeing 7377CT · Passenger/Crew DoorsSDR CA140606010Blade · cracked(CAN) ENGINE WAS REMOVED FOR A CORE OVERHAUL. DURING THE INSPECTION OF THE HPT BLADES, IT WAS FOUND THAT QTY 1 BLADE HAD CRACKING IN THE TRANSITION ZONE.May 26, 2014 · Boeing 7377CT · Turbine SectionSDR CA140605010Blade · cracked(CAN) ENGINE WAS REMOVED FOR A PROACTIVE O/H. DURING THE FLOURESCENT PENETRANT INSPECTION OF THE HIGH PRESSURE TURBINE ROTOR BLADES, IT WAS DISCOVERED THAT QUANTITY 3 BLADES EXHIBITED CRACKING AT THE MINIMUM NECK POINT ON THE FIRTREE AT THE CONVEX LOWER POINTMay 10, 2014 · Boeing 7377CT · Turbine SectionSDR CA140429002Adiru · failed(CAN) DID AN AIR TURNBACK DUE TO PROBLEMS WITH THE F/O NAVIGATION SYS. CREW REPORTED THAT THE TCAS FAIL ANNUNCIATED ON F/O NR 2 NAVIGATION DISPLAY, FOLLOWED BY LOSS OF HEADING DATA ON NR 2 PRIMARY FLIGHT DISPLAY, UPON LANDING LOSS OF ALL MAP DATA ON F/O NR 2 NApr 26, 2014 · Boeing 7377CT · Attitude and Direction Data SystemSDR CA140421009Switch · failed(CAN) THE CREW REPORT THAT THE "STABILIZER OUT OF TRIM" LIGHT ILLUMINATED. THEY COULD ELECTRICALLY TRIM THE STABILIZER NOSE DOWN BUT NOT NOSE UP. SINCE THEY COULDN`T TRIM THE STABILIZER PROPERLY, THE CREW DECLARED AN EMERGENCY AND LANDED WITH FLAPS AT 15 UNIApr 18, 2014 · Boeing 7377CT · Stabilizer Control SystemSDR CA140421004Wire · disconnected(CAN) DIVERTED DUE TO BOTH LAVATORYS NOT FLUSHING. UPON INSPECTION, MAINTENANCE FOUND A WIRE ON CONNECTOR DISCONNECTED FROM THE BLOWER MOTOR. WIRE WAS RECONNECTED AND SYS TESTED SERVICEABLE IAW AMM 38-32-00.Apr 18, 2014 · Boeing 7377CT · Water/Waste System Wiring
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