Boeing 737-217
Service difficulty reports · 308
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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 = '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 CA960214007Bushing · worn(CAN)DURING CLIMB, ONCE FLAPS RETRACTED AND ESTABLISHED IN CLIMB, STRONG VIBRATION AND RUMBLE FELT THROUGHOUT AIRCRAFT. STRONG IN AFT GALLEY THAN FORWARD. FELT THROUGH MAIN FLOOR AND SEATS IN COCKPIT AND R UMBLE NOISE QUITE PRONOUNCED. VIBRATION AND NOISE SUDDSDR CA960214006Window · delaminated(CAN)AFTER TAKEOFF THE CAPTAINS SIDE WINDOW APPEARED CRACKED IN THE UPPER RH CORNER AS IF ARCING. AIRCRAFT RETURNED. CAPTAINS SLIDING WINDOW REPLACED.SDR CA960212103Actuator · broken(CAN)NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. NOSE GEAR DOWN LOCK ACTUATOR REPLACED. ONE INCH OF BEARING RETAINING CASTING BROKEN OFF.SDR CAL960088Connectors · looseFLT NR 1517 - MDW - THE APU FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF FROM MDW. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO MDW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AREA AND FOUNDSDR CA960111012Module · intermittent(CAN)AFTER TAKEOFF AT 170 KTS AND 600 FT THE STICK SHAKER CAME ON AND STAYED ON UNTIL 230 KTS. THEN SHAKER CAME BACK ON AT 250 KTS. STALL WARNING TESTED WITH NO CHANGES. WHILE RETURNING TO YUL SHAKER STOPPED AND NEVER CAME BACK ON. MODULE REPLACED.SDR CA960119101Skin Doubler · cracked(CAN)FUSELAGE INNER BONDED DOUBLER CRACKED AT BBL 70.85 RH STA. 663. CRACK IS AT THE LOWER AFT FASTENER HOLE. CRACK POSITION 12 O'CLOCK, GOING UPWARDS. REPAIRED AS PER SRM.SDR CAL951175Hyd Line · leakingFLT NR 1084 - EWR - THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. MAINTENANCE FOUND THE HYDRAULIC RETURN LINE ON NLG UPLOCK ACTUATOR LEAKING. THE HYDRAULIC LINE WAS REMOVED AND REPLASDR CA951229003Switch · failed(CAN)THE #1 ENGINE START VALVE OPEN LIGHT CAME ON IN FLIGHT. THE #1 ENGINE WAS SHUTDOWN AS PER THE CHECKLIST. POST FLIGHT THE #1 ENGINE START VALVE AND THE PRESSURE SWITCH WERE REPLACED.SDR CA951214103Tab · broken(CAN)WHILE IN FLIGHT THE RH ELEVATOR TAB BROKE 10 INCHES FROM THE INBOARD END, A PIECE 24 INCHES LONG IS MISSING FROM THE TAB. THE PILOT REPORTED AT APPROXIMATELY FL330 IN THE CLIMB TO 370. SEVERE AIRFRAMEVIBRATION. DESCEND AND RETURN TO BLOCKS.SDR CAL951078Duct · rupturedFLT NR 1495 - BOS - THE NR 2 ENGINE SURGED ON TAKEOFF ROLL AT V1. THE TAKEOFF WAS CONTINUED AND ENGINE POWER WAS REDUCED TO KEEP EGT BELOW REDLINE. THE NR 2 ENGINE WOULD ONLY DEVELOP ABOUT 50 PERCENT POWER. THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WSDR CA951219102Stud · sheared(CAN)DURING BRAKE CHANGE FOUND BRAKE STUD SHEARED.SDR CAL951082Doubler · crackedGSO - INSPECTION FOUND A 1.25 INCH CRACK IN THIRD LAYER OF FUSELAGE INTERNAL DOUBLER AT AFT GALLEY DOOR FORWARD LOWER CORNER. THE CRACKED AREA WAS CUTOUT. A DOUBLER AND TRIPLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. (M)SDR CAL951073Shear Beam Web · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK IN LOWER INBOARD RADIUS OF SHEAR BEAM WEB JUST FORWARD OF STATION 727 AT S18A, LEFT SIDE. THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED IAW BAC DRAWING 65C29228. (M)SDR CAL951072Bulkhead · crackedGSO - INSPECTION FOUND A 4.05 INCH CRACK IN WEB ON LEFT SIDE OF NOSE WHEEL WELL AFT BULKHEAD AT LBL 6.12 AND A 3.25 INCH CRACK ON RIGHT SIDE OF NOSE WHEEL WELL AFT BULKHEAD AT RBL 7.50. THE CRACKS WERE LOCATED AT STATION 294.5. THE CRACKS WERE STOP DRILLED. SDR CAL951071Skin · creasedGSO - INSPECTION FOUND A CREASE IN SKIN PANEL ON RIGHT SIDE OF FUSELAGE AT STATION 350 AFT OF R-1 DOOR BETWEEN S18R AND S20R. THE DAMAGED AREA WAS CUTOUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. (M)SDR CAL951070Floor Beam · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK IN CENTER FLOOR BEAM OF MAIN CABIN AT STATION 660, BL 0. A REPAIR WAS FABRICATED AND INSTALLED IAW BAC DRAWING 65C34537 AND EA 5710-01322. (M)SDR CAL951069Battery Pack · inopGSO - INSPECTION FOUND THE L-1 AND R-1 EXTERIOR EMEREGNCY EXIT SLIDE LIGHTS INOPERATIVE. THE BATTERY PACK FOR THE L-1 AND R-1 EMERGENCY EXIT SLIDE LIGHTS WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M)SDR CA951110001Relay · failed(CAN)ON CLIMB FLIGHT ATTENDANT NOTICED SMOKE IN CABIN, #2 FUEL BOOST PUMP CIRCUIT BREAKER POPPED. GALLEY POWER OFF, GASPER FAN OFF, AIR CONDITIONING SMOKE CHECKLIST ACCOMPLISHED AND SMOKE DISPATCHED. REPLA CED R4 TRANSFER RELAY DUE PHASE C UNSERVICEABLE, HIGH SDR CAL951074Chord · crackedGSO - INSPECTION FOUND A 1 INCH CRACK AT FASTENERS IN LEFT STATION 727 OUTBOARD CHORD, STRINGER 18A. THE CRACKED CHORD SEGMENT WAS REMOVED AND REPLACED IAW EA 5310-01638 AND BAC DRAWING 65C33722. (M)SDR CAL950944Overheat Light · illuminatedFLT NR 1444 - EWR - AIRCRAFT INBOUND, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATES WITH THROTTLE ADVANCE. RETURNED TO BASE. MAINTENANCE REPLACED CONNECTOR AND ELEMENTS. (M)SDR CAL950860Chord · crackedGSO - INSPECTION FOUND A 2 INCH CRACK FROM FORWARD HOLE TO AFT HOLE OF RT CHORD AT STA 727, STR 18A. A REPAIR WAS ACCOMPLISHED IAW ECRA 5310-03165 AND EA 5310-02918. (X)SDR CAL950788Harness · chafedFLT NR 1588 - EWR - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED ON APPROACH TO EWR. THE NR 2 ENGINE WAS SHUT DOWN AND BOTH LEFT AND RIGHT FIRE BOTTLES WERE DISCHARGED. THE LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY ANOTHER EIGHT MINUTES AND THEN EXTINGUISHESDR CAL950802Web · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN NOSE WHEELWELL UPPER WEB AT THE INBOARD AFT CORNER ON LT SIDE AND CORROSION FOUND AT THE INBOARD FORWARD CORNER ON LT SIDE. THE WEB AREA WAS REPAIRED IAW EA 5310-02452 AND BAC DRAWING 65C35749. (X)SDR CAL950801Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN FUSELAGE FRAME AT RIGHT BS 664, WL 191.5, STRINGER 18A SHEAR BEAM. THE AREA WAS REPAIRED IAW ECRA 5310-03156 AND IAW BAC SERVICE BULLETIN 737-53-1082, REV 3, FIG 1. (M)SDR CAL950798Blkhd Chord · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK IN BS 727 BULKHEAD LEFT OUTBOARD CHORD AT STRINGER 18A. THE CHORD WAS REMOVED AND REPLACED IAW EA 5310-01638, OPERATION NR 2. (M)SDR CAL950797Stringer · corrodedGSO - INSPECTION FOUND CORROSION ON FORWARD LOWER AND UPPER AFT END OF STRINGER 26R AT STATION 1006. THE STRINGER WAS REMOVED AND A NEW STRINGER AND SPLICE WERE INSTALLED IAW SRM 53-10-3, FIGURE 1. (M)SDR CAL950796Beam · corrodedGSO - INSPECTION FOUND THE RIGHT NOSE WHEEL WELL STATION 251.6 VERTICAL SUPPORT BEAM AND ATTACHING WEB CORRODED. THE RIGHT VERTICAL BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. THE CORRODED ANGLES AND FRAME WEB WERE REPAIRED IAW SRM 51-40-1 AND 51-40-2. (SDR CAL950795Blkhd Chord · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK IN BS 727 BULKHEAD RIGHT OUTBOARD CHORD AT STRINGER 18A. THE RIGHT OUTBOARD CHORD WAS REMOVED AND REPLACED IAW EA 5310-01638. (M)SDR CAL950765Prox Sensor · inoperativeFLT NR 1580 - GSO - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR/GROUND PROXIMITY SENSOR AT FAULT. THE SENSOR WAS REPLACED AND GEAR RETRACTION WAS NORSDR CAL950749Stringer · corrodedMIA - INSPECTION FOUND CORROSION ON STRINGER 27L FROM STATION 947.5 TO 967. A STRINGER SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-3. (M)SDR CAL950748Stringer · corrodedMIA - INSPECTION FOUND CORROSION ON STRINGER 27R IN AFT BILGE INTERIOR AREA FROM STATION 947.5 TO 986. THE CORRODED AREA WAS CUT OUT. FILLER AND SPLICES WERE FABRICATED AND INSTALLED PER SRM 53-10-3. (M)SDR CALA950524Line · chafedDFW - FLT 1648 - LOSS OF A-SYSTEM HYD QUANTITY. REQUIRED BRAKE REPLACEMENT TO REMOVE FROM RUNWAY DUE TO OVERTEMP ON LANDING. FOUND LINE ON NR 2 ENGINE DRIVEN PUMP CHAFED. REPLACED LINE, FLUSHED, OPERATION AND LEAK CHECKED SYSTEM. REMOVED AND REPLACED NR 1,SDR CAL950553Battery · failedGSO - FLT 1551 - A FAINT ELECTRICAL SMELL WAS OBSERVED IN THE COCKPIT AND CABIN DURING TAXI IN AT GSO. THE AIR STARTED TO CLEAR AFTER THE PACKS AND BLEEDS WERE TURNED OFF. MAINTENANCE FOUND ACFT BATTERY BURNED. THE BATTERY WAS REMOVED AND REPLACED. THE BATSDR CAL950548Battery · failedGSO - FLT 1551 - A FAINT ELECTRICAL SMELL WAS OBSERVED IN THE COCKPIT AND CABIN DURING TAXI IN AT GSO. THE AIR STARTED TO CLEAR AFTER THE PACKS AND BLEEDS WERE TURNED OFF. MAINTNANCE FOUND THE ACFT BATTERY BURNED. THE BATTERY WAS REMOVED AND REPLACED. THE SDR CAL950484Cargo Door · crackedCLE - FLT 1639 - MAINTENANCE FOUND TWO CRACKS IN THE FORWARD CARGO DOOR AT THE SEAL RETAINER WHILE UNDERGOING A DECAY CHECK FOR PRESSURIZATION PROBLEMS. THE CRACKS WERE 8 INCHES AND 4.5 INCHES LONG. THE FORWARD CARGO DOOR WAS REMOVED AND REPLACED IAW MM 52-3SDR CAL950431Line · rupturedMCO - FLT 1594 - THE A-SYSTEM HYDRAULIC FLUID QUANTITY WAS LOST IN-FLIGHT. THE LANDING GEAR AND FLAPS WERE EXTENDED MANUALLY AND THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A RUPTURED HYDRAULIC LINE AT THE LT REAR SPASDR CAL950429Eel Fuse · blownSDF - FLT 1679 - INSPECTION FOUND A FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. TROUBLESHOOTING FOUND BAD FUSE ON FORWARD BATTERY CHARGER. THE FUSE WAS REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (X)SDR CAL950339Fan Blade · bentFLT NR 1464 - IAH - ON MAINTENANCE WALKAROUND, FOUND NR 2 ENGINE FAN BLADE BENT OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE ENGINE C1 DISK FAN ASSY. CHANGE COMPLETED, OPS CHECK GOOD. (W)SDR CAL950273Hyd Module · failedGSO - FLT 1735 - THE A-HYDRAULIC SYSTEM PRESSURE DROPPED TO ZERO DURING CLIMB OUT OF GSO. CHECK LIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CHECK VALVE FAILURE OF THE A-HYDRAULSDR CAL950235Hyd Module · inoperativeMSY - FLT 1275 - THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF WITH THE GEAR HANDLE IN THE UP POSITION. THE GEAR WAS CYCLED AND RED LIGHT EXTINGUISHED. THE RED LIGHT ILLUMINATED AGAIN WHEN THE GEAR HANDLE WAS PLACED IN THE OFF POSITION, BUT SDR CAL950177Eel Wiring · brokenFLT NR 1828 - EWR - A PREFLIGHT CHECK FOUND THE EMERGENCY AISLE PATH LIGHTING FROM ROWS 7-12 INOPERATIVE. MAINTENANCE FOUND WIRING BROKEN ON TRACK LIGHTING AT ROW 12. THE WIRING WAS SPLICED AND THE FUSE ON FORWARD BATTERY PACK WAS REPLACED. OPERATION OF THESDR CAL950120Hyd Valve · leakingBWI - FLT 1555 - THE AIRCRAFT LOST THE 'A' SYSTEM HYDRAULIC QUANTITY SHORTLY AFTER TAKEOFF FROM BWI. THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM HYDRAULIC MANUAL SHUT-OFF VALVE IN THE TAIL COMPARTMENT LSDR CAL950111Skin · crackedGSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES ON RT SIDE OF FUSELAGE BETWEEN BS 188 AND BS 251.6. ALL CRACKS WERE APPROXIMATELY 1 INCH LONG. THE CRACKS WERE REPAIRED IAW EA 5310-01188, PART 3. (X)SDR CAL950110Skin · crackedGSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES BETWEEN BS 188 AND BS 251.6 ON THE LT SIDE OF FUSELAGE. ALL CRACKS WERE APPROXIMTELY .25 INCH LONG. THE CRACKS WERE REPAIRED IAW EA 5310-01188, PART 3. (X)SDR CAL950109Skin · corrodedGSO - INSPECTION FOUND CORROSION ON RT EXTERNAL SKIN AND DOUBLER AT STA 727 BETWEEN STR 17R AND STR 18R. THE CORROSION WAS REMOVED AND A DOUBLER IN INSTALLED IAW EC 5330-02227. (X)SDR CAL950108Skin · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN THE LT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN AT STA 66. THE CRACK WAS STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 55-10-3 AND SRM 51-30-2. (X)SDR CAL950107Intercostal · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BEHIND AFT FORMER IN E AND E BAY. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-30-2. (X)SDR CAL950106Frame · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT BS 500 BETWEEN STR 21L AND STR 20L. THE CRACKED BELT FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2. (X)SDR CAL950100Frame · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN BELT FRAME AT BS 480 BETWEEN STR 21L AND STR 20L. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-30-0. (X)SDR CAL950099Frame · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT BS 500A BETWEEN STR 21L AND STR 20L. THE CRACKED FRAME WAS CUT OUT IAW BOEING DRAWING 65C225113 AND A REPAIR WAS INSTALLED IAW SRM 51-30-0. (X)
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