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 CALA9601707Skin · dentedINSPECTION FOUND LOWER 6 SECTION OF C-1 CARGO DOOR SKIN DENTED, SCRATCHED AND GOUGED AT STA 178. THE DAMAGED SKIN WAS REMOVED AND REPLACED WITH NEW SKIN IAW SRM 52-30-2 AND 51-30-2.SDR CALA9601644Relay Module · burntSMOKE WITH FUMES WAS OBSERVED COMING FROM ELECTRICAL PANEL BY THE JUMP SEAT ON AIRCRAFT RIGHT ON APPROACH. THE M181 MODULE WAS HOT TO TOUCH, THE MODULE WAS REMOVED AND SMELLED BURNT. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLASDR CALA9601653Bulkhead · crackedINSPECTION FOUND A 6 INCH CRACK IN BULKHEAD AT STA 178, RT SIDE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11.SDR CALA9601652Bulkhead · crackedINSPECTION FOUND A 6 INCH CRACK IN BULKHEAD AT STA 178, LT SIDE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11.SDR CALA9601651Keel Beam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN KEEL BEAM SKIN AT STA 700. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9601601Hyd Line · brokenTHE A-HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO WHEN GEAR WAS LOWERED ON FINAL APPROACH TO CLE. THE FLAPS WERE LOWERED TO 15 DEGREES ELECTRICALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 4 SLAT ACTUATOR HYDRAULIC LINE BSDR CALA9601603Skin · crackedINSPECTION FOUND A 1 INCH CRACK AT AFT LOWER CORNER OF C-2 DOOR AFT CUTOUT. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLERS WERE INSTALLED IAW ECRA 5330-02460.SDR CALA9601561Bulkhead Skin · crackedINSPECTION FOUND A 6 INCH AND 7 INCH CRACK IN SKIN AT B.S. 178 BULKHEAD. THE CRACKED AREA WAS CUT OUT. DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-11.SDR CALA9601560Shear Web · crackedINSPECTION FOUND A 1 INCH CRACK IN INBOARD RADIUS OF SHEAR WEB AT S18A, LT B.S. 664. NEW REPAIR ANGLES WERE INSTALLED IAW BOEING DRAWING NR 65C29228 AND SRM 51-30-2.SDR CALA9601555Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN INBOARD SKIN AT LOWER AFT CORNER OF C-2 DOOR CUTOUT. THE CRACKED SECTION OF SKIN WAS REMOVED. A DOUBLER AND TRIPLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND ENGINEERING ORDER REO-02348.SDR CALA9601554Bulkhead Skin · crackedINSPECTION FOUND A 6.5 INCH CRACK IN STA 178 BULKHEAD SKIN PANEL ALONG HORIZONTAL STIFFENER AT WL 218, ON LT SIDE. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2.SDR CALA9601553Bulkhead Skin · crackedINSPECTION FOUND A .50 INCH CRACK IN STA 178 BULKHEAD SKIN AT WL 233.5 AND A 6 INCH CRACK WAS FOUND AT HORIZONTAL STIFFENER AT WL 218, RT SIDE. THE CRACKED AREAS WERE CUT OUT. FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2SDR CALA9601542Hyd Line · leakingTHE A-HYDRAULIC SYSTEM QUANTITY GRADUALLY DECREASED TO 1 GALLON WHILE EN ROUTE. THE A-SYSTEM HYDRAULIC PUMPS WERE TURNED OFF. WHEN THE PUMPS WERE TURNED ON TO LOWER FLAPS THE SYSTEM FAILED AND SMOKE ENTERED THE CABIN. THE AIRCRAFT LANDED AT EWR WITHOUT INCISDR CALA9601556Frame · crackedINSPECTION FOUND A 1 INCH CRACK THROUGH NUTPLATE HOLE AT LOWER AFT CORNER OF LT STA 520 WING TO BODY ATTACH FRAME. THE FASTENERS AND EXISTING ANGLE WERE REMOVED. AN ATTACH ANGLE, REPAIR ANGLE, AND CLIPS WERE FABRICATED AND INSTALLED IAW ECRA 5350-01227, SRM SDR CALA9601521Skin · crackedINSPECTION FOUND CRACKS IN SECTION 41 RT FUSELAGE EXTERNAL SKIN FROM BS 188 TO 251.6, WL 207 TO 234. THE CRACK LENGTHS WERE NOT IDENTIFIED. THE SKIN WAS REPAIRED IAW EA 5310-01188.SDR CALA9601519Fitting · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FRAME FITTING AT BS 685, WL 208, LBL 62. THE FASTENER HOLE WAS COLD WORKED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5310-03346.SDR CALA9601517Frame · crackedINSPECTION FOUND A 2 INCH CRACK EXTENDING AFT OF SECOND FASTENER HOLE IN LT BS 727 FRAME CHORD. THE LOWER CHORD SEGMENT WAS REMOVED AND REPLACED IAW CAL WORK CARD JA5310-0163802001.SDR CALA9601518Floorbeam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LOWER RADIUS OF FLOORBEAM AT STA 675, BBL 0. THE LOWER T-CHORD WAS REMOVED, A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 51-20-2, 51-30-2 AND BOEING DRAWING NR 65-45410.SDR CALA9601520Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT FUSELAGE SKIN AT BS 747 AND AT BS 727A. BOTH CRACKED AREAS WERE CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED OVER EACH CRACK FROM STA 725 TO 790 IAW SRM 53-30-3.SDR CALA9601516Bulkhead · crackedINSPECTION FOUND A 6 INCH CRACK IN BULKHEAD BEHIND STIFFENER ON RT SIDE AT STA 178, WL 218. ALSO, A 1 INCH CRACK WAS FOUND AT WL 230.5, RT SIDE. THE CRACKED AREA AT WL 218 WAS REMOVED AND THE CRACK AT WL 230.5 WAS STOP DRILLED IAW SRM 53-10-11. REPAIR DOUBLSDR CALA9601447Line · leakingLOSS OF A-SYSTEM HYDRAULICS. FOUND PRESSURE LINE FROM NR 2 ENGINE LEAKING. REPLACED LINE AND BOTH ENGINE DRIVEN AND ELECTRIC HYDRAULIC PUMPS AND REPLACED ALL FILTERS PER MM 29-11-32 AND 29-12-21.SDR CALA9601445Line · leakingLOSS OF A-SYSTEM HYD ON SHORT FINAL. A-SYSTEM PUMPS TURNED OFF. FOUND BLOWN PRESSURE LINE AT FORWARD WHEEL WELL WALL. REMOVED AND REPLACED LINE AND NR 1 ENGINE HYD PUMP PER MM 29-11-32 AND REPLACED SYSTEM CASE DRAIN FILTERS PER MM 29-11-41.SDR CALA9601423Wire · burnedSMOKE DEVELOPED FROM BEHIND COCKPIT OVERHEAD PANEL AFTER TURNING ON ENGINE ANTI-ICE WHILE CRUISING AT FL 240 EN ROUTE FROM EWR TO CAE. THE SMOKE CEASED WHEN ANTI-ICE WAS TURNED OFF. THE FLIGHT WAS CONTINUED TO CAE WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAISDR CALA9601385Actuator · inoperativeTHE NR 2 LEADING EDGE SLAT DID NOT RETRACT AFTER TAKEOFF. THE LEADING EDGE TRANSIT LIGHT WAS ON AFTER FLAP RETRACTION AND A VISUAL CHECK CONFIRMED THE NR 2 SLAT WAS STILL EXTENDED. A RECYCLE WAS PERFORMED, BUT THE SLAT REMAINED EXTENDED. THE AIRCRAFT WAS RESDR CALA9601376Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 380, STRINGER 21R. THE CRACK WAS STOP DRILLED IAW SRM 53-10-4. A DOUBLER, FILLER AND CLIP WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9601374Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT FS 765, STRINGER 19R. THE CRACKED AREA OF SKIN WAS REMOVED, REPAIR DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2.SDR CALA9601373Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN ATTACH ANGLE AT STA 360, STRINGER 21R. THE ATTACH ANGLE WAS REMOVED IAW SRM 51-30-2, REPAIR ANGLES AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9601372Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STRINGER 22L STA 360. THE CRACKED SECTION WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.SDR CALA9601377Angle · crackedINSPECTION FOUND A .75 INCH CRACK FROM LAST FASTENER HOLE OF RT UPPER RAM AIR ATTACH ANGLE AT STA 540, STRINGER 14R. THE CRACKED SECTION OF ANGLE WAS CUT OUT, A NEW SECTION AND SPLICE ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-50-1, 51-40-3 AND 51-10-2.SDR CALA9601371Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BETWEEN STRINGER 19L AND 20L AT STA 727. A MOD AND REPAIR WAS ACCOMPLISHED IAW BOEING DRAWING 65C28086 AND EA 5330-01198, OP 1 AND OP 2.SDR CALA9601325Air Dist Fan · inoperativeA STRONG ELECTRICAL ODOR WAS SMELLED IN THE COCKPIT AFTER TAKEOFF. THE FLIGHT ATTENDANT'S REPORTED SMOKE IN THE AFT/MID CABIN. THE AIR DISTRIBUTION FAN WAS TURNED OFF AND THE SMOKE APPEARED TO DISSIPATE. THE AIRCRAFT WAS DIVERTED TO IAD WHERE IT LANDED WITHSDR CALA9601375Angle · corrodedINSPECTION FOUND EXFOLIATION CORROSION AND SHEARED FASTENERS AT LT AFT CORNER OF E AND E DOOR CUTOUT SUPPORT STRUCTURE. THE T-ANGLE WAS REMOVED AND REPLACED IAW EC 5310-01233.SDR CALA9601314Seal · leakingTHE NR 2 ENGINE OIL QUANTITY DROPPED TO .5 GALLON WHILE EN ROUTE. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE OIL LEAKING FROM HYDRAULIC PUMP CAVITY DRAIN. THE CARBONSDR CALA9601305Hyd Line · rupturedTHE AIRCRAFT LOST A-SYSTEM HYDRAULICS AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC PRESSURE LINE FROM NR 1 ENGINE PYLON TO WING ROOT RUPTURED. THE HYDRAULIC PRESSURE LINE WAS REPLSDR CALA9601261Drive Mechanism · worn bearingWHEN FLAPS WERE SELECTED TO 30 DEGREES ON APPROACH, THE AIRCRAFT ROLLED LEFT. THE FLAPS WERE SET TO 25 DEGREES AND THE ROLL STOPPED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT INBOARD AFT FLAP STICKING IN THE UP POSITION WITH FLAPS LOWSDR CALA9601251Hyd Line · chafedTHE AIRCRAFT WAS RETURNED TO EWR AFTER LOSS OF THE A-HYDRAULIC SYSTEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM RETURN LINE IN LT MLG WHEEL WELL CHAFED AGAINST ANOTHER HYDRAULIC LINE. BOTH HYDRAULIC LINES WERE REMOVED AND REPLACED ANSDR CALA9601136Fireloop · malfunctionedTHE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMB OUT OF EWR. BOTH FIRE BOTTLES WERE DISCHARGED, THE NR 1 ENGINE WAS SHUTDOWN, AND AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE BOTTOM FIRE DSDR CALA9601110Harness · failedMAINTENANCE FOUND FEEDER HARNESS BURNT WHILE TROUBLESHOOTING THE APU. A STRINGER AT BELLY OF AIRCRAFT ABOUT 15 INCHES FORWARD OF APU COMPARTMENT AFT OF AFT PRESSURE BULKHEAD WAS FOUND BURNED DUE TO THE FEEDER HARNESS ARCING. A NEW HARNESS WAS SPLICED IN AND SDR CALA9601017Tire · failedA LOUD BANG WAS HEARD AFTER TAKEOFF, WHILE CLIMBING THROUGH 3,000 FEET. THE FLIGHT CONTINUED TO BOS WHERE IT LANDED SAFELY. MAINTENANCE FOUND THAT THE NR 3 TIRE HAD BLOWN RESULTING IN DAMAGE TO RT OUTBOARD SIDE OF WHEEL WELL. THE RT I/B FLAP TRACK FAIRING ASDR CALA9601005Stiffener · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING VERTICAL STIFFENER AT LEADING EDGE UNDER PANEL 6526. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-5.SDR CALA9601003Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE OF C-2 DOOR INTERIOR SKIN. THE CRACK WAS STOP DRILLED, A WEB REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-30-2 AND 51-40-2.SDR CALA9601000Skin · corrodedINSPECTION FOUND LOWER FUSELAGE SKIN AND STRINGER CORRODED WITH RIVETS POPPED AT STA 312 TO 328, STRINGER 27L TO 26R. THE CORRODED AREA OF SKIN WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-2. STRINGER 28 WAS REMOVED AND REPLACED ISDR CALA9600999Stiffener · damagedTWO STIFFENERS AND AFT SIDE OF WEB ON RT WING AT STA 180.36 SUSTAINED DAMAGE FROM TOOLING. THE STIFFENERS WERE REMOVED AND THE DAMAGED AREA WAS BLENDED IAW SRM 51-30-2 AND 57-10-1. STIFFENERS AND REPAIR PLATES WERE FABRICATED AND INSTALLED IAW SRM 57-10-2 ANSDR CALA9601006Floor Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN FLOOR BEAM UPPER CHORD AT STA 660, BL 07. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01322, OPERATION 2 AND ECRA 5710-01743.SDR CALA9601004Skin · crackedINSPECTION FOUND TWO .25 INCH CRACKS IN RT WING LEADING EDGE SKIN AT ANTI-ICE DUCT CUTOUT, NR 5 SLAT. THE CRACKED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2.SDR CALA9601002Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 277, STRINGER 26R. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 53-30-3 AND 51-10-2.SDR CALA9601001Skin · dentedINSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 400, S18L. THE DENTED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-2.SDR CALA9600859Gearbox · leakingTHE NR 1 ENGINE OIL PRESSURE ROSE TO OVER 60 PSI AFTER TAKEOFF. WHEN THE NR 1 THROTTLE WAS RETARDED, THE OIL TEMPERATURE ROSE BEYOND THE RED LINE. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ESDR CALA9600858Fuel Heat Valve · inoperativeTHE NR 1 ENGINE OIL TEMPERATURE WENT INTO THE YELLOW BAND AFTER DEPARTURE FROM EWR. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FUEL HEAT VALVE NOT SEATING PROPERLY. THE FUEL HEAT VALSDR CALA9600827Hyd Line · chafedTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE EN ROUTE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC SUPPLY LINE IN THE RT REAR SPAR ARE
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