Boeing 737-217
Service difficulty reports · 308
Newest first. General aviation reporting is voluntary.
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 = '737217' 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 aircraft_model_key = '737217' 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 CA140908023Overheat Loop · open(CAN) AT THE TOP OF DECENT, OUR ACFT ILLUMINATED AN ENGINE OVERHEAT INDICATION ON NR 1 ENGINE. THE CREW FOLLOWED THEIR NON-NORMAL CHECKLIST WHICH SAID TO RETURN THE ENGINE TO IDLE, WHICH IT ALREADY WAS, CUT FUEL TO THE ENGINE AND FIRE THE BOTTLE. THE OVERHEASDR CA140806001Line · leaking(CAN) 1 ENGINE OVERHEAT ILLUMINATED. SHUTDOWN NR 1 ENGINE BOTH EXTINGUISHER BOTTLES DISCHARGED. UPON INVESTIGATION MAINTENANCE FOUND NR 1 ENGINE, 13TH STAGE BLEED AIR AND MODULATING VALVE SENSE LINE, PN BACH7D0137DD, BRAIDED HOSE ASSY LEAKING BLEED AIR ONTO SDR CA110520002Window · brokenDURING CRUISE, THE FLIGHT CREW REPORTED THAT THE OUTER PANE OF THE L-1 WINDOW HAD SHATTERED. THE ACFT RETURNED TO POINT OF DEPARTURE, WHERE THE WINDOW WAS REPLACED.SDR CA100526002Gearbox · leakingENGINE WAS LEAKING OIL FROM AROUND THE BANJO FITTING, ENGINE APPROX 70HRS SINCE SHOP VISIT - GEARBOX TO BE REPLACED. THIS IS A PRELIMINARY REPORT ONLYSDR CA090514001Window · cracked(CAN) DURING CRUISE AT 35,000, THE NR 4 WINDOW CRACKED, CREW DESCENDED TO 14,000 AND CONTINUED THE FLIGHT. WINDOW WAS REPLACED AND ACFT RETURNED TO SERVICE.SDR CA100215002Gcu · smoke(CAN) DURING ENGINE START THE GCU STARTED TO SMOKE, THE CREW REMOVED THE GCU, MX INSTALLED A SERVICEABLE GCU. (TC 20100215002)SDR CA090323005Turbine · failed(CAN) AFTER TAKEOFF, THE CREW OBSERVED A SUDDEN LOSS OF POWER ON NR 2 ENGINE COINCIDENT WITH AN UNUSUAL VIBRATION AND NOISE. THE CREW CARRIED OUT AN INFLIGHT SHUTDOWN OF NR 2 ENGINE. THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER DIFFICULTYSDR CA080630001Engine · failed(CAN) - ON DESCENT, A "BUZZING" SOUND WAS HEARD IN THE FLIGHT DECK FOR APPROX 5-10 SEC. THIS WAS FOLLOWED BY 1 OR 2 "POPS" AND THEN A LOUD "BANG" AT WHICH TIME THE NR 2 ENGINE LOST THRUST. NR 2 ENG TEMP CLIMBED BUT THERE WAS NO ENG OVERHEAT OR FIRE WARNING. ASDR CA080121003Wire · inoperative(CAN) TAIL 523 ON JAN 2ND APPROACH BACK COURSE ON RWY 15 YELLOWKNIFE 1040FT ASL 350FT AGL LEVEL FLIGHT 140K IN THIS CASE THE FLIGHT CREW EXPERIENCED A TAWS GENERATED A PICTORIAL DISPLAYED IMPACT WARNING. THE CREW WAS IN VISUAL CONDITIONS AND SAW NO DANGER OF SDR CA070911003Valve · malfunctioned(CAN) APPROXIMATELY 25 MINUTES AFTER DEPARTING, THE CREW OBSERVED THE NR 1 ENGINE OIL TEMPERATURE CLIMBING THROUGH THE YELLOW BAND. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE NR 1 FUEL HEAT VALVE AND CONDUSDR CA060829004Bearing · seized(CAN) AIRCRAFT ENCOUNTERED INTERMITTENT REPEAT SNAGS FOR STIFF ELEVATOR MOVEMENT. FINAL RECTIFICATION CAME ON AUGUST 5 2006 WHEN THE REFERENCED BEARING AND RETAINER WERE REPLACED. REFERENCED BEARING WAS FOUND SEIZED. CURRENT MAINTENANCE PROGRAM WAS REVIEWESDR CA040625004Actuator · inoperative(CAN) NR 6 LEADING EDGE SLAT WAS SLOW TO RETRACT ON DEPARTURE. AFTER IT DID RETRACT IT RE-EXTENDED FOR ABOUT 5 MINUTES THEN RETRACTED AGAIN. CREW WAS ALERTED BY SLAT INDICATION OF THE REDEPLOYMENT AND VISUALLY CONFIRMED THE EXTENSION AND RETRACTION. NO OTHER ASDR CA040519014Actuator · failed(CAN) DURING TAXI TO GATE LOSS OF NOSE WHEEL STEERING OCCURRED WITH TOTAL LOSS OF HYDRAULIC A PRESSURE AND QUANTITY AT ZERO. MAINTENANCE FOUND THE NR 8 GROUND SPOILER ACTUATOR TO BE THE CAUSE. THE ACTUATOR BODY HAD STRUCTURAL FAILURE CAUSING FLUID LOSS. ACTUSDR CA040510004Ring · damagedHAVE HAD SEVERAL OCCURRENCES OF FUEL LEAKS FROM THE JT8D FUEL FLOW TRANSMITTERS. THE LEAKS ARE EVIDENT AT VERY HIGH POWER SETTINGS. A FLEET CAMPAIGN HAS BEEN COMPLETED WHICH CHECKED ALL ENGINES FOR LEAKS AND RECTIFIED DEFECTS. AN EXTENSIVE INVESTIGATION IS BESDR CA031218008Fitting · broken(CAN) ON WALK AROUND, MAINTENANCE FOUND THE RT OB FOREFLAP OB LINK BROKEN. MAINTENANCE REPLACED THE FOREFLAP AND AIRCRAFT RETURNED TO SERVICE. CAUSE UNKNOWN. WILL UPDATE IF ADDITIONAL INFORMATION AVAILABLE.SDR CA031027005Module · failed(CAN) ON DECENT NR1 A SYS LOW PRESSURE LIGHT ILLUMINATED. SHORTLY, NR 2 A SYS LOW PRESSURE LIGHT ILLUM. CREW ACCOMPLISHED QRH FOR LOSS OF SYS A. EMERGENCY DECLARED & LANDED. MAINT CHECKED SERVICEABLE HYD SYS RES STANDPIPE & PRESSURE. ENG RAN AND HYD PRESSURE SSDR CA031015003Link · broken(CAN) A LOUD BANG WAS HEARD UPON GEAR RETRACTION. ONCE GEAR WAS RETRACTED A STRONG VIBRATION WAS FELT. WHEN GEAR EXTENTED, VIBRATION WENT AWAY. RETURNED TO YYC FOR A NORMAL LANDING. RT NOSE LANDING GEAR DOOR DOG LINK FOUND BROKEN. LINK REPLACED, SWING CARRIEDSDR CA030929006Actuator · malfunctioned(CAN) ON CLIMB OUT THE AIRCRAFT EXPERIENCED A TOTAL LOSS OF HYDRAULIC SYSTEM A FLUID. AIRCRAFT TURNED BACK TO YUL AND LANDED WITHOUT INCIDENT. THE NR 3 SPOILER ACTUATOR WAS FOUND TO BE THE CAUSE OF THE FLUID LEAK.ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERSDR CA030805001Landing Light · fire(CAN) DURING TROUBLESHOOTING OF AN OUTBOARD (LT HAND) LANDING LIGHT SNAG MAINTENANCENOTICED SMOKE ODOR IN THE COCKPIT AND THEN SEVERAL C/BS POPPED. MAINTENANCE SHUT ALL AIRCRAFT POWER DOWN. SMOKE WAS NOTICED BY MAINTENANCE COMING FROM THE LT PYLON AREA FWD. PSDR CA030318018Actuator · leaking(CAN) DURING CRUISE THE AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC FLUID. THE AIRCRAFT WAS DIVERTED TO WHERE EMERGENCY VEHICLES MET THE AIRCRAFT ON LANDING.THE LOSS OF FLUID WAS ATTRIBUTED TO THE NR 2 FLIGHT SPOILER ACTUATOR. THE ACTUATOR IS BEING TESTED AND ASSSDR CA030321011Control Unit · misoverhauled(CAN) UNSCHEDULED REMOVAL OF RUDDER PCU, OCCURRED ON FEB 25/26/2003 WAS IN RESPONSE TO A REQUEST FROM MATERIAL SERVICES BASED ON A FAA UNAPPROVED PARTS NOTIFICATION NR 2001-0089 DATED AUG 12,2002. SUSPECT PCU P/N 1U1150-3 S/N 737 WAS LISTED IN THE NOTIFICATIONSDR CA030224004Apu · failed(CAN) PRIOR TO PUSH BACK, AIRCRAFT RAPIDLY FILLED CABIN WITH SMOKE, AIRCRAFT DEPLANNED. CAUSED BY THE BLEED FROM THE APU (BURNED OIL CONTAMINATION) APU CHANGED AND COLLESTER BAGS REPLACED. AC SERVICEABLESDR CA030221010Cooling Fan · unsecure(CAN) JUST BEFORE PUSH BACK, CABIN RAPIDLY FILLED WITH SMOKE (NON ELECTRICAL IN NATURE). A/C WAS DEPLANED VIA THE LOADING BRIDGE AND SHUT DOWN TO BATTERY. MAINT FOUND THE APU OIL TANK EMPTY AND INLET PLENUM CONTAMINATED WITH OIL. FOUND APU COOLING FAN HAD DESDR CA030205011Strut · overserviced(CAN) AFTER TAKE OFF, NOSE GEAR DID NOT STOW. OLEO DID NOT EXTEND FULLY OR MADE CONTACT WITH SNUBBERS. THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED. GEAR WAS CYCLED WAS NORMAL. MAINT FIRST CHECKED NOSE OLEO SERVICING AND DISCOVERED OLEO TO BE OVERSERVSDR CA030108011Warning System · activated(CAN) DURING CRUISE, THE APU FIRE DETECT LIGHT FLICKERED 3 TIMES. MAINTENANCE GROUND TESTED, NO FAULTS FOUND AND AIRCRAFT RELEASED FOR SERVICE.THE NEXT DAY THE APU FIRE DETECT LIGHT CAME ON BEFORE LANDING. AFTER LANDINGTHE APU FIRE LIGHT AND BELL CAME ON AND TSDR CA030107016Computer · failed(CAN) MACH TRIM LIGHT CAME ON IN FLIGHT, CREW REPORTED ELEVATOR FEEL INOPERATIVE. AIRCRAFT RETURNED TO DEPARTURE STATION. ELEVATOR FEEL COMPUTER REPLACED AS PER AMM. AND OPERATION CHECKED SERVICEABLE.SDR CA021227005Cam · damaged(CAN) UPON ARRIVAL IN YEG, THE NOSE OLEO WAS FOUND LOW AND LEAKING FLUID. AIRCRAFT HAD SOME HISTORY OF HARD BOTTOMING SNAGS. AFTER INSPECTION BY MAINTENANCE IT WAS DETERMINED THE NOSE GEAR REQUIRED DIASSEMBLY FOR A SEAL CHANGE. AIRCRAFT WAS FERRIED TO YVR FOR SDR CA020904007Isolation Valve · malfunctioned(CAN) BOTH ENGINE SURGING AT CRUISE, BLEED SURGING FROM 20PSI TO 52 PSI. NR 2 ENGINE SURGING CONSIDERABLY MORE ON DESCENT.SDR CA020806008Engine · failed(CAN) WHEN ADDING THRUST FOR T/O, HEARD LOUD BANG AND NOTICED PARAMETERS DROPPING. SHUT DOWN AND SECURED NR 2 ENGINE. NR 2 ENGINE AND T/R REPLACED AS PER AMMSDR CA020731016Actuator · failed(CAN) L/E FLAP TRANSIT ON AFTER T/O. NR 5 RT WING SLAT FULLY EXTENDED FOR APPROX 2 MIN. WHEN IT RETRACTED AND BEFORE WE RECYCLED THE FLAPS. REPLACED NR 5 SLAT ACTUATOR AS PER AMM. SYSTEM CHECKED SERVICEABLE AND CERTIFIED.SDR CA020726007Indicator · failed(CAN) 30 MINUTES AFTER DEPARTURE, ELECTRICAL BURNING SMELL IN COCPIT, AIRCRAFT LANDED SAFELY, BURNING SMELL ORIGINATED BY WEATHER RADAR INDICATOR. INDICATOR REPLACED.SDR CA020801010Indicator · failed(CAN) FLIGHT WAS DIVERTED DUE TO BURNING SMELL IN COCKPIT FROM WEATHER RADAR INDICATOR. UNIT WAS REPLACED AND SHOP REPORT INDICATED CAUSE OF PROBLEM WAS BURNED OUT DIODES ON RECTIFIER AND FILTER ASSY.SDR CA020725014Adc · failed(CAN) AUTOPILOT ENGAGED IN CRUISE,UNABLE TO UNFREEZE MANUALLY,LEFT WING LEVEL TO A SLIGHT RIGHT BANK. AILERON CONTOL LOST-FROZEN TILL AUTO PILOT RELEASED.CENTRAL AIR DATA COMPUTER REPLACED P/N HG480B13 S/N P-529SDR CA020228001Adc · failed(CAN) JUST AFTER TAKEOFF CAPTAINS AIRSPEED, STANDBY AIRSPEED, GROUND PROX WARNING, AND MACH TRIM INDICATORS FAILED. AIRCRAFT RETURNED TO AIRPORT. NR 1 CENTRAL AIR DATA COMPUTER REPLACED AND OPERATION CHECKED SERVICEABLE.SDR CA020215007Arm · dislodged(CAN) MAINTENANCE FOUND NR 2 SLAT FOUND PROTRUDING 4 INCHES ON ONE SIDE ON WALKAROUND CHECK. SLAT MECHANISM FOUND OFF GUIDE TRACK. FLIGHT PERMIT (SPECIFIC PURPOSE, FERRY FLIGHT) ISSUED AND AIRCRAFT FLOWN TO BASE FOR REPAIRS. NR 2 LEADING EDGE SLAT DETENT ARM SDR CA020110002Transmitter · failed(CAN) ENGINE NR 1 OIL PRESSURE DROPPED TO 20 PSI AFTER TAKEOFF. ENGINE FAILURE AND SHUT DOWN COMPLETED. AIRCRAFT RETURNED TO VANCOUVER. OIL PRESSURE TRANSMITTER REPLACED.SDR CA020104010Gasper Fan · seized(CAN) AIRCRAFT ENROUTE FROM SAN FRANSISCO TO VANCOUVER, DIVERTED TO KLAMATH FALLS OREGON, DUE SMOKE IN THE CABIN. SMOKE DISIPATED WHEN GASPER FAN SELECTED OFF. GASPER FAN FOUND SEIZED. GASPER FAN REPLACED.SDR CA020121008Spar · cracked(CAN) RT ELEVATOR REAR SPAR AT TRIM TAB ATTACHMENT POINT FOUND CRACKED. ELEVATOR REMOVED FOR REPAIR, LOCATION OF DAMAGED LOCATED AT STATION 66.54 REPLACED ELEVATOR. DAMAGE REPAIRED AS PER SRMSDR CA011121010Accessory Unit · failed(CAN) SHORTLY AFTER TAKEOFF OUT OF YYC, THE CREW EXPERIENCED DIFFICULTY GETTING THE LANDING GEAR LEVER TO REMAIN IN THE 'UP' POSTION. THE CREW PERFORMED THE 'NON-NORMAL CHECKLIST', BUT WERE UNABLE TO RECTIFY THE PROBLEM. THE CREW ELECTED TO RETURN TO YYC ANSDR CA011114011Selector Valve · failed(CAN) LOUD NOISE AND ALL 3 GEAR INDICATION LIGHTS BOTH GREEN AND RED ILLUMINATED. A/C RETURNED TO YQR, LANDING GEAR EXTENDED AND ALL INDICATION NORMAL. RIGGING CHECK CARRIED OUT ALL NORMAL. LANDING GEAR SELECTOR VALVE REPLACED. LANDING GEAR SWING CARRIED OUT ASDR CA011019010Selector Valve · failed(CAN) AFTER NORMAL TAKEOFF, GEAR IN OFF POSITION, LIGHTS OUT, AT 29,000 FT. SPEED AT 290-300 LANDING GEAR CAME DOWN WITH THREE GREEN LIGHTS, AIR DID AN AIR TURN BACK TO REGINA. FOUND TO BE THE SELECTOR VALVE AT FAULT. LANDING GEAR SELECTOR VALVE REPLACED.SDR CA011114010Controller · failed(CAN) PRESSURE CONTROLLER FAILED ON CLIMB OUT FROM YYC. A/C RETURNED TO YYC. O2 MASKS DEPLOYED. CABIN PRESSURE CONTROLLER FAILED FUNCTION TEST ON GROUND. REPLACED O2 MASKS AND REPLACED PRESSURE CONTROLLER. FUNCTION CHECK CARRIED OUT AND A/C RETURNED TO SERVICESDR CA010906010Oven · failed(CAN) FORWARD GALLEY OVEN BURNING SMELL. OVEN REPLACED.SDR CA010522003Generator · failed(CAN) 20 MINUTES AFTER DEPARTURE, APU GENERATOR DROPPED OFF LINE. RETURNED DUE #2 CSD WAS ON MEL. REPLACED #2 GENERATOR AND CSD AS PER WORK CARDS 1177-2 AND 1182-2. GROUND RUNUP COMPLETED, APU AND NR 2 GENERATOR CHECKED SERVICEABLE.SDR CA010423002Gcu · failed(CAN) NR 1 ENGINE GENERATOR FAILED INBOUND, NR 1 GENERATOR CONTROL PANEL REPLACED AS PER WORK CARD.SDR CA010404007Engine · vibration(CAN) A/C 722, MAR 12/2001, YQX, LOG SEQUENCE 0295200. TOP OF DESCENT WHEN THRUST LEVERS RETARDED, NR 2 ENGINE VIBRATION WAS INDICATING 2 MILS ON INLET AND 3.5 ON TURBINE. NR 2 START LEVER WAS VIBRATING. TRIED ENGINE ANTI-ICE AND THROTTLE MOVEMENT, WITH NO CHASDR CA010105006Housing · broken(CAN) DURING INSPECTION, 17C CHECK OF NR 4 GROUND SPOILER, SPOILER FOUND TO BE LOOSE. FOUND NR 4 SPOILER ACTUATOR, BODY END THAT ENCLOSED THE BEARING, BROKEN AWAY. ACTUATOR REPLACED AS PER WORK CARD 51160.SDR CA001201006Engine · failed(CAN) A/C 723, NOV 13/2000, FLT 7012, YFC, LOG SEQUENCE 0298768. ON LANDING YFC, WITH REVERSE THRUST SELECTED, A BANG WAS FELT. FLIGHT CREW THOUGHT IT WAS A TIRE. NOTICED NR 1 ENGINE EPR AND OTHER PARAMETERS DECREASING, SHUTDOWN NR 1 ENGINE. INSPECTION OF ENSDR CA001122002Clamp · failed(CAN) NR 1 ENGINE SHUT DOWN, APPROXIMATELY 12 MINUTES INTO FLT. DUE TO ENGINE OVERHEAT AND START VALVE OPEN LIGHT ON. FOUND THERMAL ANTI-ICE DUCT CLAMP FAILED. REPLACED CLAMP, RT 8TH STAGE BLEED DUCT, AND 13TH STAGE BLEED DUCT TO EXPANSION BELLOWS. ENGINE RUNSDR CA001201013Gcu · failed(CAN) DEPARTED WITH MEL ON NR 2 GENERATOR, GENERATOR HAD BEEN DISCONNECTED. 50 MILES SOUTH WEST OF YQB, THE APU GENERATOR FAILED. NR 1 BUS TRANSFER DID NOT TAKE PLACE, FIRST OFFICER WAS WITHOUT INSTRUMENTS. REQUESTED LANDING TO YQB, LANDED WITHOUT INCIDENT. AP
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