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 CA980415007Bearing · separated(CAN) ON APPROACH, TWO SELECTIONS WERE MADE IN ORDER TO INDICATE NOSE GEAR DOWN AND LOCKED. DOWNLOCK ACTUATOR LOWER BEARING SEPARATED FROM ACTUATOR HOUSING. REPLACED.SDR CA980415010Engine · failed(CAN) ON CLIMB, NR 2 ENGINE FAILED. AIRCRAFT RETURNED TO RAMP. ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE. ENGINEERING REPORT TO FOLLOW.SDR CA971216025Sensor · intermittent(CAN) AIRCRAFT RETURNED TO RAMP DUE TO RT MAIN GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. RT UPLOCK REPLACED.SDR CA971216022Tire · detached(CAN) AIRCRAFT ARRIVED WITH LT NOSE WHEEL OFF RIM. REPLACED BOTH NOSE WHEELS.SDR CA971216018Fitting · cracked(CAN) SECOND OBSERVER OXYGEN CONTROL PANEL FITTING CRACKED. PANEL REPLACED.SDR CALA9800039Control Cable · out of adjTHE LANDING GEAR HANDLE COULD NOT BE MOVED BEYOND THE OFF POSITION AFTER TAKEOFF. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG TELEFLEX CABLE OUT OF ADJUSTMENT. THSDR CALA9800017Solenoid · inoperativeTHE LANDING GEAR HANDLE WOULD NOT GO PAST THE OFF DETENT AFTER TAKEOFF. THE OVERRIDE DID NOT WORK EITHER. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE M241 LEVER LATCH SOLENOID AT FAULT. THE SOLENOID WAS REPLACEDSDR CALA9701782Cylinder · leakingTHE NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED AND HYDRAULIC QUANTITY DROPPED TO ZERO ON APPROACH TO EWR. ALL ABNORMAL AND EMERGENCY CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG HYDRAULIC TRANSSDR CALA9701652Sensor · out of adjustTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE HANDLE WOULD GO TO THE OFF POSITION AND STOP. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR SAFETY SENSOR ACTUATOR OUT OF RIG. THE SENSOR WAS ADJUSTED IAW SDR CA971015022Sensor · intermittent(CAN) LEFT HAND MAIN LANDING GEAR UNSAFE LIGHT FLASHING. REPLACED SENSOR.SDR CA971113017Bolt · corroded(CAN) BOLT SECURING LOCK BRACE SHAFT TO LOCK BRACE CORRODED APPROXIMATELY 50 PERCENT THROUGH SHANK. REPLACED.SDR CA971015016Bolt · corroded(CAN) BOLT SECURING LOCK BRACES SHAFT TO LOCK BRACE CORRODED APPROXIMATELY 50 PERCENT THROUGH SHANK. REPLACED.SDR CA971015013Wire · chafed(CAN) AFTER TAKEOFF NR1 START VALVE LIGHT CAME ON, AIRCRAFT RETURNED. FOUND WIRES CHAFED AT PRESSURE SWITCH. REPAIREDSDR CALA9701377Hyd Line · chafedTHE A-HYDRAULIC SYSTEM BEGAN TO LEAK SLOWLY WHILE EN ROUTE. THE HYDRAULIC PUMPS WERE TURNED OFF BEFORE LOW PRESSURE LIGHTS ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM HYDRAULIC PRESSURE LINE IN SDR CA970904014Valve · leaking(CAN) ON TAXI A HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED. INTERCONNECT OPENED AND 'B' SYSTEM QUANTITY DROPPED. MAIN LANDING GEAR ISOLATION VALVE REPLACED.SDR CALA9701161Slide · zero pressureINSPECTION FOUND THE R-2 DOOR ESCAPE SLIDE WITH ZERO PRESSURE. THE SLIDE WAS REMOVED AND REPLACED.SDR CA970715006Aural Warning Bx · malfunction(CAN) DURING CLIMB CONFIGURATION AURAL WARNING SOUNDED. AURAL WARNING BOX REPLACED.SDR CA970715004Transmitter · faulty(CAN) TAKEOFF ABORTED AT 70 KNOTS WHEN #2 ENGINE OIL PRESSURE DROPPED TO ZERO. OIL PRESSURE TRANSMITTER AND PRESSURE REGULATOR WERE REPLACED AND AFTER GROUND RUNUP THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CALA9700978Light · inoperativeINSPECTION FOUND FIRST CLASS EMERGENCY TRACK LIGHT AT L-1 DOOR INOPERATIVE. MAINTENANCE REPLACED SOCKET AND DAMAGED WIRE, OPERATIONAL CHECK WAS GOOD.SDR CALA9700891Hyd Line · leakingTHE B HYDRAULIC SYSTEM WAS LOST DURING CRUISE, EN ROUTE TO ATL. THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE FROM NR 1 ELECTRIC B PUMP TO THE NR 5 PORT ON THE FILTER MODULE LEAKING. THE HYDRAULIC LINE WAS REMOVED AND REPLACESDR CA970618004Element · failed(CAN) #2 ENGINE OVERHEAT ON DESCENT. AIRCRAFT DIVERTED. LOWER OVERHEAT DETECTION LOOP FAILED, REPLACED.SDR CA970528007Clamp · loose(CAN) #2 ENGINE HAD OVERHEAT INDICATION FLICKERING AND THEN STEADY IN CRUISE. FIRE BOTTLES ACTIVATED. POST FLIGHT INSPECTION FOUND UPSTREAM CLAMP LEAKING AND FLEX LINE TO 13TH STAGE BLEED VALVE LOOSE. LINE TIGHTENED AND CLAMP REPLACED. ENGINE GROUND RUN NO LEASDR CALA9700584Tr Unlock Light · illuminatedONTAKEOFF ROLL, CREW RECEIVED NR 1 THRUST REVERSER UNLOCK LIGHT ILLUMINATE. REJECTED TAKEOFF AT 100 KNOTS. RETURNED TO GATE WHERE MAINTENANCE PERFORMED INSPECTION PER MM 5-5-111 P201-208. ALSO, TESTED TR SYSTEM IAW B7373 MM 78-32-01, ALL CHECKED NORMAL.SDR CALA9700538Return Hyd Line · leakingTHE AIRCRAFT LOST A-HYDRAULIC SYSTEM QUANTITY ON APPROACH. CHECKLIST PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT WING SPOILER HYDRAULIC RETURN LINE ABOVE LEFT GEAR LEAKING. THE HYDRAULIC LINE WAS REMOVED ASDR CA970421018Valve · split(CAN) A AND B HYDRAULIC SYSTEMS PRESSURIZED WITH INTERCONNECT VALVE CLOSED AND ENGINES NOT RUNNING. INTERCONNECT VALVE BODY SPLIT, REPLACED.SDR CA970421016Pcu · failed(CAN) RUDDER PCU FAILED STEP 4A OF W/C 6026, AD 94-01-07 PCU FAILED TO CENTRE RUDDER ASSEMBLY WHEN JUMPERS REMOVED FROM PINS OF YAW DAMPER COUPLER, REPLACED.SDR CALA9700438Hyd Line · crackedTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY DURING CLIMBOUT. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AN A-SYSTEM HYDRAULIC PRESSURE LINE CRACKED. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. IN ADSDR CA970318003Fan · failed(CAN) ON APPROACH ATTENDANT REPORTED BURNING ELECTRICAL SMELL IN THE CABIN. SHORTLY AFTER CB POPPED FOR GASPER FAN. AIRCRAFT DISPATCHED UNDER MEL. FAN REPLACED AT YVRSDR CALA9700160Skin · crackedINSPECTION FOUND A 4.5 INCH CRACK IN RT WING LEADING EDGE SKIN AT WS 190. THE CRACKED AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30-2, FIGURE 2.SDR CALA9700176Angle · crackedINSPECTION FOUND A 2.5 INCH CRACK IN RIB LOWER CHORD ANGLE AT S3 IN FUEL ACCESS PANEL 7202 AT LT WING FUEL TANK, WBL 135.5. THE CRACKED AREA WAS REMOVED, A REPAIR TEE WAS INSTALLED IAW BOEING SERVICE BULLETIN 737-57-1186 AND REPAIR ENGINEERING ORDER NUMBER 02SDR CALA9700175Angle · crackedINSPECTION FOUND STA 540 WING TO BODY FRAME CRACKED LOWER AREA LBL 31, T-ANGLE WAS CRACKED INTO TWO PIECES. THE CRACKED SECTION WAS REMOVED, ANGLES AND T-CHORD WERE FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9700172Web · crackedINSPECTION FOUND THREE EACH CRACKS AT RIVETS OF WEB UNDER NR 3 SEAT TRACK AT BS 715. THE CRACKS WERE APPROXIMATELY 2 INCHES LONG. THE CRACKED AREAS WERE REMOVED, REPAIR SHIMS AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9700171Bulkhead Web · puncturedINSPECTION FOUND A .25 INCH DIAMETER PUNCTURE IN AFT PRESSURE BULKHEAD WEB AT 8:30 POSITION, TWO FEET FROM CENTER. THE DAMAGED AREA WAS REMOVED, A DOUBLER AND FASTENERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-30-0.SDR CALA9700170Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN SKIN PANEL AT LEADING EDGE STA 213 OF LT WING LOWER SURFACE. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-0 AND 51-30-2.SDR CALA9700169Stringer · crackedINSPECTION FOUND A 2 INCH CRACK IN STRINGER AT STA 907. THE CRACKED SECTION OF STRINGER WAS REMOVED IAW SRM 53-10-3, STRINGER SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-10-3 AND 51-30-2.SDR CALA9700168Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN RADIUS OF STRINGER 6L AT STA 787. THE CRACKED SECTION OF STRINGER WAS REMOVED, A STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-30-2, AND 51-20-4.SDR CALA9700167Fitting · crackedINSPECTION FOUND A 1 INCH CRACK AT BOTTOM AFT FACE OF VERTICAL STABILIZER LT AFT OUTBOARD FITTING TO LUG. THE CRACKED FITTING WAS REMOVED, A NEW FITTING WAS DRILLED AND INSTALLED IAW SRM 51-10-7 AND 51-30-2.SDR CALA9700166Support · brokenINSPECTION FOUND FORWARD CARGO PIT FLOOR SUPPORT BROKEN AT STA 490 ABOVE STRINGER 28L. THE BROKEN SECTION WAS REMOVED IAW SRM 53-10-1 AND 51-30-2, A NEW SECTION OF SUPPORT WAS TRIMMED, FITTED AND SPLICED IAW SRM 53-10-5. THE NEW SECTION AND SPLICES WERE INSTSDR CALA9700159Frame · corrodedINSPECTION FOUND STA 250 RT VERTICAL STIFFENER, STA 277 RT FRAME WEB, STA 270 RT SHEAR TIE ANGLE CHORD IN RT NOSE WHEEL WELL CORRODED. A VERTICAL BEAM, FRAME WEB REPAIR ANGLES, AND SHEAR TIE REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2SDR CALA9700158Frame · corrodedINSPECTION FOUND STA 270 LT FRAME, STA 277 LT CAP ANGLE, FRAME WEB, STIFFENER CHANNELS AT STA 270 AND 277, AND BEAR STRAP AT STA 277 LT CORRODED. FRAME ANGLES, WEB, REPAIR DOUBLER, STIFFENER CHANNELS, BEAR STRAP, FILLER AND DOUBLERS WERE FABRICATED AND INSTALSDR CALA9700157Bulkhead · crackedINSPECTION FOUND A 8.25 INCH CRACK AT RBL 7.5 AND A 5.25 INCH CRACK AT LBL 6.12 IN BULKHEAD, STA 294.5. THE CRACKED AREAS WERE CUT OUT, DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03410.SDR CALA9700146Frame · crackedINSPECTION FOUND FRAME CRACKED AND BENT AT STA 987, BL ZERO - RBL 10. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-30-2.SDR CALA9700145Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED BETWEEN SEAT TRACKS 2-13 AT STA 360. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9.SDR CALA9700144Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 744, RBL 15 TO LBL 15. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-2.SDR CALA9700143Floorbeam · corrodedINSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 980. THE UPPER FLANGE WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-2.SDR CALA9700142Support · crackedINSPECTION FOUND TWO 8 INCH CRACKS IN FORWARD CARGO PIT FLOOR SUPPORT AT STA 460, RBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-40-4.SDR CALA9700141Floorbeam · corrodedINSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 328, RBL 24 TO RBL 50. THE UPPER CHORD OF BEAM WAS REMOVED. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-2.SDR CALA9700138Skin · gougedINSPECTION FOUND AFT CARGO DOOR CUTOUT FORWARD LOWER CORNER SKIN GOUGED. THE GOUGED SKIN WAS CUT OUT, REPAIR FILLERS AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ECRA 5330-02484.SDR CALA9700137Angle · corrodedINSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 947 TO 970, ON RT SIDE. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED, A REPAIR SECTION AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.SDR CALA9700136Floorbeam · crackedINSPECTION FOUND A 2 INCH CRACK ON UPPER FLANGE OF FLOORBEAM AT BS 667, BL 0. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5710-01779.
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