Boeing 737-130
Service difficulty reports · 287
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 = '737130' 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 = '737130' 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 CALA9700651Clip · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE CLIP TIE AT STA 300, STRINGER 29L. THE CLIP WAS REMOVED, A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700649Stringer · crackedINSPECTION FOUND A 1 INCH CRACK AT FORWARD FASTENER HOLE OF STRINGER 23L AND FAIL SAFE CHORD WAS BULGED AT BS 727. A STRINGER CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9700650Hinge · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT WING NR 3 SPOILER INBOARD HINGE. THE HINGE WAS REMOVED, A NEW HINGE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9700537Accessory Unit · inoperativeTHE LEFT GEAR GREEN DOWN AND LOCKED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. ALL OTHER INDICATIONS WERE NORMAL. THE GEAR WAS VISUALLY INSPECTED WHILE IT WAS EXTENDED AND RETRACTED, BUT THE GREEN LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO EWR WSDR CALA9700504Actuator · leakingTHE A-SYSTEM HYDRAULIC QUANTITY WAS LOST AFTER TAKEOFF. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 SPOILER ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-61-11, PAGE 401. LEAK AND OPERATSDR CALA9700442Fuel Module · inoperativeELECTRICAL SMOKE AND FUMES WERE OBSERVED IN THE COCKPIT WHILE EN ROUTE. ALSO, THE MASTER CAUTION FUEL LIGHT ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO DCA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FUEL SYSTEM MODULE AT FAULT. THE FUEL SYSTEM MSDR CALA9700299Thermo Valve · inoperativeTHE RT PACKED TRIPPED AT 6,000 FEET LEAVING EWR AND SMOKE BEGAN TO ENTER THE CABIN. SHORTLY AFTERWARDS THE BLEED TRIPPED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE 450 DEGREE THERMO VALVE WAS REMOVED AND REPLACED, AN ENGINE BLEESDR CALA9700231Hyd Line · chafedTHE A-SYSTEM HYDRAULIC QUANTITY WAS LOST AFTER TAKEOFF. THE SYSTEM A-HYDRAULIC FAILURE CHECKLIST WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A-HYDRAULIC PRESSURE CHAFED THROUGH. THE HYDRAULIC LINE WASDR CALA9700229Duct · rupturedTHE NR 1 ENGINE HAD A FIRE WARNING WHILE EN ROUTE. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A NR 1 ENGINE PNEUMATIC DUCT RUPTURED. THE DUCT WAS REMOVED AND REPLACED, LEAK AND OPERASDR CALA9700183Stringer · corrodedINSPECTION FOUND STRINGER 22L CORRODED AT STA 987. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-1.SDR CALA9700185Stringer · corrodedINSPECTION FOUND STRINGER 23L CORRODED IN SEVERAL SPOTS FROM STA 908 TO 1016. THE STRINGER SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 53-10-3.SDR CALA9700187Stringer · corrodedINSPECTION FOUND STRINGER 22L CORRODED FORWARD OF NEGATIVE PRESSURE RELIEF VALVE AT STA 950. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-20-10.SDR CALA9700182Frame · crackedINSPECTION FOUND FORWARD GALLEY DOOR LOWER AFT CORNER FRAME CRACKED. THE CRACKED SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-1.SDR CALA9700180Frame · corrodedINSPECTION FOUND FRAME CORRODED AT STA 285, STRINGER 27L. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-4.SDR CALA9700186Skin · corrodedINSPECTION FOUND FUSELAGE LOWER SKIN AT STA 727A BETWEEN STRINGERS 27L AND 27R BULGED AND RIVETS DISHED DUE TO CORROSION. A KEEL BEAM SPLICE WAS INSTALLED PER BOEING SERVICES EO SKCALR970203 AND SKIN DOUBLERS WERE INSTALLED IAW SRM 53-30-3, PAGE 11.SDR CALA9700181Frame · corrodedINSPECTION FOUND CORROSION ON FRAME LOWER CHORD AT STA 360 BETWEEN STRINGER 28L AND 28R. THE CORRODED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-10-1 AND 51-10-6.SDR CALA9700156Shear Tie · corrodedINSPECTION FOUND FRAME SHEAR TIE CORRODED AT STA 987, STRINGER 23 TO 24. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9700184Skin · disbondedINSPECTION FOUND TRAILING EDGE OF NR 1 L/E SLAT DISBONDED ALONG ENTIRE LOWER TRAILING EDGE SECTION. THE SLAT WAS REMOVED AND REPAIRED IAW SRM 51-40-5 AND REINSTALLED.SDR CALA9700071Hyd Line · leakingTHE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHTS FLICKERED AND THE A-SYSTEM HYRDAULIC QUANTITY GAUGE READ ZERO ON APPROACH PRIOR TO GEAR AND FLAP EXTENSION. THE HYDRAULIC FAILURE CHECKLIST WAS COMPLETED AND A MANUAL GEAR EXTENSION WAS PERFORMED. THE AIRCRAFT LANDESDR CALA9700067Gcu · inoperativeSMOKE AND FUMES MOMENTARILY APPEARED IN THE COCKPIT DURING A STANDBY POWER CHECK WHILE AIRCRAFT WAS AT GATE. MAINTENANCE FOUND THE APU GENERATOR CONTROL UNIT AT FAULT. THE APU GCU WAS REMOVED AND REPLACED, GROUND CHECK WAS GOOD.SDR CALA9700066Prox Sensor · inoperativeTHE LEFT MLG RED UNSAFE LIGHT ILLUMINATED AFTER GEAR WAS EXTENDED ON APPROACH. EMERGENCY PROCEDURES WERE COMPLIED WITH PER AIRCRAFT FLIGHT MANUAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG DOWNLOCK PROXIMITY SENSOR AT FAULT. THE SDR CALA9700056Fan · inoperativeTHE FLIGHT ATTENDANTS REPORTED, A BURNING ODOR IN CABIN WHILE EN ROUTE. THE SMOKE CHECKLIST PROCEDURE WAS ACCOMPLISHED AND THE ODOR DISSIPATED AFTER THE RT PACK WAS SHUTDOWN. THE AIRCRAFT LANDED AT PVD WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE SDR CALA9700055Hyd Line · crackedTHE A-SYSTEM HYDRAULIC FLUID QUANTITY WAS LOST WHILE EN ROUTE. THE AIRCRAFT LANDED AT CAE WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM HYDRAULIC SUPPLY LINE FOR NR 1 ENGINE CRACKED. THE SUPPLY LINE WAS REPLACED. IN ADDITION, BOTH A-SYSTEM ENGINE DRIVEN HYDSDR CALA9700046Stiffener · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING VERTICAL STIFFENER AT STRINGER 13R. THE STIFFENER WAS REPAIRED IAW ECRA 5710-01773 AND IN REFERENCE TO BOEING DRAWING 65C34533.SDR CALA9601911Hydraulic Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP DURING CLIMBOUT. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC SUPPLY FLEX LINE IN RIGHT ENGINE PYLON AREA LEAKING. THE LINE WAS REMOVED AND REPLACED AND LEAK CHESDR CALA9601876Hyd Line · leakingTHE A HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT INTO EWR. THE A SYSTEM PUMPS WERE TURNED OFF AND THE HYDRAULIC LOSS CHECKLIST WAS ACCOMPLISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT ENGINE A SYSTEM PRESSURE LISDR CALA9700049Spar · tornINSPECTION FOUND A 3 BY .375 INCH TEAR IN LOWER FLANGE OF LT HORIZONTAL STABILIZER FORWARD LEADING EDGE SPAR. THE TEAR WAS LOCATED THREE FEET FROM OUTBOARD EDGE. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-5, FIGURE 1.SDR CALA9700047Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 328, BL 0 TO RBL 55. A FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 51-10-3.SDR CALA9601797Window Frame · corrodedINSPECTION FOUND FORWARD LOWER CORNER OF NR 4 RT CABIN WINDOW FRAME CORRODED. THE WINDOW FRAME WAS REMOVED AND A NEW FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.SDR CALA9601796Skin · crackedINSPECTION FOUND .5 INCH CRACKS IN LT FUSELAGE SKIN AT BS 188 TO 251, WL 207 TO 234. THE AREA WAS REPAIRED IAW SRM 51-30-2, BAC DRAWING NR 65-18420, AND EA 5310-01188.SDR CALA9601791Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED ON UPPER CHORD AT STA 294.5 FROM RBL 20 TO LBL 20. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2 AND 51-30-2.SDR CALA9601790Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 755, STRINGER 19R. THE CRACKED AREA WAS REMOVED IAW SRM 53-30-3. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2.SDR CALA9601789Skin · corrodedINSPECTION FOUND EXTERNAL FUSELAGE SKIN LAP BULGED AND ONE FASTENER SHEARED AT FS 380, STRINGER 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2, 53-30-2 AND 51-30-2.SDR CALA9601788Stringer · corrodedINSPECTION FOUND FUSELAGE STRINGER 24L CORRODED FROM FS 970 TO 1000. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-10-6. STRINGER REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-2.SDR CALA9601787Skin · corrodedINSPECTION FOUND NLG WHEEL WELL UPPER SKIN CORRODED AFT OF ACCESS, STA 240. THE SKIN WAS REPAIRED IAW ECRA 5310-03378.SDR CALA9700050Support · corrodedINSPECTION FOUND CENTER FLOORBEAM SUPPORT CORRODED UNDER PANEL NR 8 BETWEEN STA 312 AND 328. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2.SDR CALA9700048Skin · crackedINSPECTION FOUND A 2.25 INCH CRACK IN RT FUSELAGE SKIN AT STA 745 BETWEEN STRINGERS 15R AND 16R. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2.SDR CALA9601846Bear Strap · corrodedINSPECTION FOUND E AND E DOOR CUTOUT BEAR STRAP CORRODED AT FORWARD SIDE OF CUTOUT. STRINGER 29 WAS REMOVED AND CORROSION WAS REMOVED FROM SKIN AND BEAR STRAP IAW SRM 51-10-6. A REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.SDR CALA9601845Skin · corrodedINSPECTION FOUND NOSE WHEEL WELL CUTOUT AFT RT CORNER HAD CORRODED SKIN AND STRESSED FASTENERS. LOWER LOBE SKINS WERE CUT AND REMOVED FROM STA 253 TO 312. THE LOWER CHORD AT STA 294.5 WAS REMOVED AND REPLACED IAW BAC DRAWING 65-45808. A SPLICE WAS FABRICATESDR CALA9601786Stringer · crackedINSPECTION FOUND A 1 INCH CRACK AT STRINGER 7R FASTENER ON RT WING UPPER SURFACE, WBL 200. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND ECRA 5710-01765.SDR CALA9700051Skin · corrodedINSPECTION FOUND LT WING ROOT LOWER SKIN PANEL CORRODED. THE SKIN WAS REPAIRED IAW ECRA 5730-01471.SDR CALA9601844Skin · corrodedINSPECTION FOUND FUSELAGE EXTERIOR SKIN LAP CORRODED AT STA 540, STRINGER 26L. REPAIR FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9601772Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 328, RBL 10 TO RBL 46. THE UPPER T-CAP WAS REMOVED, A NEW UPPER T-CAP WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.SDR CALA9601771Intercostal · crackedINSPECTION FOUND A 1.5 INCH CRACK IN INTERCOSTAL AT STA 357, STRINGER 16L. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.SDR CALA9601769Web · corrodedINSPECTION FOUND AFT LAV LT PAN CORRODED AROUND DUMP CHUTE AND CENTER SUBSTRUCTURE CHANNEL CORRODED AT UPPER SURFACE. THE FLOOR WEB AND CENTER CHANNEL WERE REMOVED, A REPLACEMENT WEB AND CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND 51-10SDR CALA9601770Stiffener · corrodedINSPECTION FOUND STA 285.62 NOSE WHEEL WELL RT VERTICAL STIFFENER CORRODED 3 INCHES FROM LOWER END AND 2 INCHES FROM UPPER END. THE VERTICAL STIFFENER WAS REMOVED, A REPLACEMENT STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND BAC DRAWING 6SDR CALA9601724Sensor · out of adjustTHE GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION AFTER TAKEOFF FROM PHL. CYCLING OF THE GEAR LIGHT CIRCUIT BREAKER MADE NO CHANGE. THE AIRCRAFT WAS RETURNED TO PHL WHERE IT LANDED WITHOUT INCIDENT (THE AIRCRAFT HAD AIR RETURNED THE DAY BEFORE FOR THE GEASDR CALA9601713Hyd Line · leakingTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC PRESSURE LINE ON TOP OF NR 2 ENGINE LEAKING. THE LINE WAS REPLACED USING A FLEX LINE ANSDR CALA9601842Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED BETWEEN RIVETS AT BS 964, STRINGER 20L. THE CORRODED AREA OF SKIN WAS CUT OUT, DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9601843Skin · crackedINSPECTION FOUND A 1.75 INCH CRACK IN FUSELAGE SKIN AT BS 775, STRINGER 19R. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
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