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 CALA9700135Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER RADIUS OF FLOORBEAM AT STA 685, BL 0. A 1 INCH CRACK WAS FOUND IN TRANSVERSE BEAM AT STA 675, BL 0. THE FLOORBEAM WAS REPAIRED IAW BAC DRAWING 65C19643. THE TRANSVERSE BEAM WAS REPAIRED IAW BAC DRAWING 65C17103.SDR CALA9700134Bulkhead · crackedINSPECTION FOUND AN 8 INCH CRACK IN BULKHEAD AT STA 178, RBL 29 AND A 10 INCH CRACK WAS FOUND IN BULKHEAD AT STA 178, LBL 29. THE CRACKED AREAS WERE CUT OUT, FILLER AND DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-11.SDR CALA9700133Stringer · crackedINSPECTION FOUND A .25 INCH CRACK IN STRINGER AT RT WING FS 465 LEADING EDGE SLAT WELL. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 51-20-1 AND 51-30-2.SDR CA970327005Coupler · failed(CAN) AT 5000FT DURING TURN AT 190 KTS AND AGAIN AT 29000, 220 KTS IN TURN HAD UNCOMMANDED YAW MOVEMENT, WITH AUTOPILOT ENGAGED MOVEMENT WAS NOT AS NOTICEABLE. RUDDER YAW DAMPER AND PCU REPLACED.SDR CA970109011Solenoid · failed(CAN) LANDING GEAR LEVER WOULD NOT MOVE TO GEAR UP POSITION WITHOUT USE OF OVERRIDE LEVER. LANDING GEAR LEVER LOCK SOLENOID REPLACED.SDR CA970109010Detector · shorted(CAN) PRIOR TO DEPARTURE APU FIRE WARN SOUNDED. AIRCRAFT EVACUATED USING REAR SLIDES AND FORWARD ENTRY DOORS. M515 LOOP FOUND SHORTED TO GROUND. REPLACED.SDR CA970109006Apu · failed(CAN) APU AUTO SHUTDOWN DUE LOW OIL PRESSURE. LOW OIL PRESSURE SWITCH REPLACED, NO FIX, SUSPECT OIL PUMP. APU REPLACED.SDR CA961217003Skin · cracked(CAN) 3/4 INCH CRACK IN THE LEFT HAND FUSELAGE SKIN, 4 INCHES AFT OF THE OVERWING LIGHT, AT STATION 520 STRINGER 16. REPAIRED AS PER SRM.SDR CA961220006Start Valve · intermittent(CAN) ON CLIMB RH STARTER VALVE OPEN LIGHT CAME ON. ENGINE SHUT DOWN. PNEUMATIC STARTER REGULATING AND SHUT OFF VALVE REPLACED.SDR CA961220005'B' Nut · loose(CAN) ON TAKEOFF 'A' SYSTEM QTY INDICATED ZERO. MAIN GEAR EVENTUALLY RETRACTED BECAUSE IT WAS ALREADY SELECTED UP. 'A' SYSTEM CYCLED ON AND OFF SEVERAL TIMES AND INDICATED 200 PSI. EMERGENCY DECLARED AND LANDING CARRIED OUT. PRESSURE LINE 'B' NUT LOOSE, TIGHTESDR CA961220003Switch · intermittent(CAN) TEN MINUTES AFTER TAKEOFF, CLIMBING THROUGH 20,000 FEET #2 START VALVE OPEN LIGHT ILLUMINATED. ENGINE SHUT DDOWN, LIGHT OUT AND DUCT PRESSURE UP. #2 START PRESSURE SWITCH REPLACED.SDR CA961220008Module · intermittent(CAN) ELECTRICAL SMELL COMING FROM FIRST OFFICER'S INSTRUMENT PANEL AREA. TURNING GASPER FAN, BACKGROUND LIGHTS OR FLOOD LIGHTS OFF HAS NO EFFECT. SMELL LIKE BURNT OUT LIGHT BALLEST. #2 ENGINE ANTI-ICE INOPERATIVE AND SMELL/HEAT COMING FROM MODULE. REPLACED.SDR CALA9601704Fuel Pump · inoperativeTHE NR 2 ENGINE FLAMED OUT DURING CLIMB AT 900 FEET AGL. THE AIRCRAFT WAS RETURNED TO CHS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE FUEL PUMP AT FAULT. THE FUEL PUMP WAS REMOVED AND REPLACED IAW MM 73-11-1. A POWER ASSURANCE RUN WSDR CALA9601628Solenoid · inoperativeTHE GEAR LATCH WOULD NOT RELEASE AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CIRCUIT BREAKERS WERE PULLED AND RESET IAW QRH PROCEDURES, BUT WITH NO CHANGE. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCESDR CA970212007Controller · intermittent(CAN) ON DESCENT AIRPLANE TOTALLY DEPRESSURIZED. DID NOT AUTO SWITCH TO STANDBY. NO TIME TO TROUBLESHOOT. DID NOT APPEAR TO WORK IN STANDBY. REPLACED.SDR CALA9601382Hyd Line · crackedTHE A-HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ON APPROACH. THE A-SYSTEM HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 SLAT ACTUATOR HYDRAULIC PRESSURE LINE CRACKED AT B-BUT. THE LISDR CALA9601320Hyd Line · crackedTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY UPON LANDING. THE AIRCRAFT STOPPED SAFELY AND WAS TOWED TO THE GATE. MAINTENANCE FOUND HYDRAULIC LINE JUST OUTBOARD OF NR 2 SLAT ACTUATOR CRACKED. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO RSDR CA960924012Computer · intermittent(CAN) ABORTED TAKEOFF ROLL AT 70 KTS DUE STAB OUT OF TRIM LGIHT ON. PITCH CHANNEL COMPUTER REPLACED.SDR CALA9601188Hyd Pump · leakingTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURE ON NR 2 ENGINE WHILE EN ROUTE. AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED SDR CA960801005Duct · cracked(CAN) OVERHEAT LIGHT AND LOW PNEUMATIC PRESSURE INDICATION. NOSE COWL ANTI-ICE DUCT FOUND CRACKED AT FORWARD WELD FORWARD OF BELLOWS. REPLACED.SDR CALA9600961Actuator · leakingTHE A-SYSTEM HYDRAULIC FLUID WAS LOST WHILE ON DESCENT INTO CHS. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE A-SYSTEM HYDRAULIC PUMP LIGHTS. THE LANDING GEAR WAS LOWERED MANUALLY AND THE FLAPS WERE EXTENDED ELECTRICALLY. THE AIRCRAFT LANDED WITHOUSDR CALA9600940Hyd Line · leakingTHE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM RDU. ALL GEAR WERE LOWERED AND VERIFIED DOWN. THE AIRCRAFT WAS RETURNED TO RDU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR LOCK ACTUATOR HYDRAULIC FLEX LINE LEAKING. THE LINE SDR CALA9601014Floor Beam · crackedINSPECTION FOUND FLOOR BEAM LOWER CHORD AND TRANSVERSE BEAM CRACKED AT STA 675, BL 0. THE TRANSVERSE BEAM AT STA 685, BL 0 WAS ALSO CRACKED. THE BEAMS WERE REPAIRED IAW ECRA 5710-01740 AND SRM 51-40-4.SDR CALA9600906Pcu · inoperativeTHE AIRCRAFT HAD AN UNCOMMANDED ROLL TO THE RIGHT ON TAKEOFF. FIFTEEN TO TWENTY DEGREES OF LEFT AILERON WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. ALL OTHER INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO CLE WHERE IT LANDED WITHOUT FURTHER PROBLEM. THE YAWSDR CALA9601012Skin · crackedINSPECTION FOUND A 1.75 INCH AND 5.75 INCH CRACK IN RT FUSELAGE SKIN BETWEEN BS 188 AND 251, WL 207 TO 234. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EA 5310-01188.SDR CALA9601010Skin · disbondingINSPECTION FOUND ONE AREA OF RT WINDOW BELT SKIN DISBONDING. THE WINDOW BELT SKIN WAS REPAIRED IAW SRM 53-30-08.SDR CALA9601013Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN WEB AT STA 358, STRINGER 17L. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW 51-40-3, 51-10-2 AND 53-10-2.SDR CALA9600806Fire Loop · burnedTHE APU FIRE WARNING LIGHT BEGAN TO FLASH INTERMITTENTLY APPROXIMATELY FIVE MINUTES INTO THE FLIGHT WITH THE APU SHUT DOWN. THE APU FIRE HANDLE WAS PULLED AND THE FIRE LIGHT FLASHING CEASED AFTER 45 SECONDS. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WSDR CALA9601011Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LT FUSELAGE SKIN BETWEEN BS 188 AND 251, WL 207 TO 234. THE CRACKED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW EA 5310-01188.SDR CALA9601009Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN RT WING UPPER SURFACE SKIN AT REAR SPAR, WBL 165, AFT OF INBOARD DRY BAY PANEL. THE CRACKED SECTION WAS CUT OUT AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5730-01449.SDR CALA9601008Skin · gougedINSPECTION FOUND A GOUGE IN FUSELAGE SKIN BELOW R-1 DOOR AT STRINGER 18R. THE GOUGED AREA WAS CUT OUT IAW SRM 53-30-3. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9601007Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN STA 1020 AND 1044, STRINGER 25R. THE DENTED AREA WERE CUT OUT IAW SRM 53-30-8. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2.SDR CA960827101Card · corroded(CAN) DURING APPROACH WITH FLAPS AT 40, AIRCRAFT YAWED UNTIL YAW DAMPER TURNED OFF. AUTOPILOT WAS OFF, ALTITUDE 1200 AGL, WIND 10 MPH, TEMP 18C, REPLACED COUPLER. EXTENSIVE CORROSION ON ANODE CONNECTOR LUG FOR CR3 ON A1A1 CARD.SDR CA960604015Yaw Damper · intermittent(CAN) ON APPROACH WITH 40 UNITS OF FLAPS SELECTED AIRCRAFT HAD EXCESSIVE YAW TO THE RIGHT AND LEFT. AIRCRAFT STABILIZED WHEN YAW DAMPER SELECTED OFF. AUTOPILOT OFF/ALT 1200 AGL/WIND 10/TEMP 18 DEGREES. REPLACED.SDR CA960528101Cell · melted(CAN) BATTERY CHARGER CIRCUIT BREAKER POPPED AND BATTERY HOT TO TOUCH. ON GROUND A VERY NOTICEABLE ELECTRICAL SMELL WAS NOTED. REPLACED 60 AMP BATTERY CHARGER. SMELL STILL EXISTS NEAR BATTERY. BATTERY ALSO RE PLACED.SDR CALA9600689Frame · crackedINSPECTION FOUND A 1 INCH AND 1.5 INCH CRACK IN FRAME AT STA 480 BETWEEN STRINGER 22L AND 23L. THE CRACKED FRAME SECTION WAS REMOVED, A NEW FRAME SECTION WAS FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C25113.SDR CA960827102Card · corroded(CAN) TAKEOFF REJECTED DUE TO VIOLENT LATERAL MOVEMENT. YAW DAMPER REPLACED. VISUAL INSPECTION OF A1A1 YAW INTERLOCK CARD REVEALED EXTENSIVE CORROSION ON ANODE CONNECTOR LUG FOR CR3. REPLACED.SDR CALA9600798Strap · corrodedINSPECTION FOUND STRAP AT C-1 DOOR THRESHOLD CORRODED, STA 420 TO 500. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.SDR CALA9600721Frame · crackedINSPECTION FOUND TWO, .5 INCH CRACKS IN FRAME AT BS 328 BETWEEN STRINGER 2OR AND 21R. THE CRACKED AREAS WERE REMOVED, FILLER AND REPAIR PLATES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.SDR CALA9600720Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 328, STRINGER 26L. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-40-3 AND 51-30-2.SDR CALA9600719Frame · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT NUTPLATE HOLES OF FRAME AT BS 440, LT SIDE. THE FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113.SDR CALA9600718Frame · crackedINSPECTION FOUND A 2 INCH CRACK AT NUTPLATE HOLE OF FRAME, BS 420, STRINGER 22L. THE FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113.SDR CALA9600706Frame · crackedINSPECTION FOUND A 1.5 CRACK AT NUTPLATE HOLE OF FRAME, BS 500A, RT SIDE. THE FRAME SEGMENT WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW BOEING DRAWING 65C25113.SDR CALA9600704Floorbeam · crackedINSPECTION FOUND A .75 CRACK IN FLOORBEAM AT STA 676, RBL 24. THE BEAM WAS REPAIRED IAW EA 5710-01638.SDR CALA9600700Frame · crackedINSPECTION FOUND A 1 INCH CRACK AT TWO NUTPLATE LOCATIONS ON FRAME AT BS 500, RT SIDE. THE CRACKED FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113.SDR CALA9600698Splice · crackedINSPECTION FOUND A 1.5 INCH CRACK IN STRINGER SPLICE AT STA 360, STRINGER 21R. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 53-30-2.SDR CALA9600695Skin · crackedINSPECTION FOUND SEVERAL CRACKS IN SECTION 41 FUSELAGE SKIN ON LT SIDE, BS 188 TO 251, WL 207 TO 234. THE CRACKS RANGED FROM .125 INCH TO .25 INCH IN LENGTH. THE CRACKED AREAS WERE CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW EA 5310-01188SDR CALA9600694Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AND CORROSION AT FASTENER HOLE OF STRINGER 26L, BS 323. THE CRACKED STRINGER WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-5 AND 51-10-2.SDR CALA9600688Stringer · corrodedINSPECTION FOUND STRINGER 22L CORRODED AT STA 727. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.SDR CALA9600801Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN UPPER SKIN OF RT WING INBOARD AFT FLAP. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND MM 51-20-0.
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