Boeing 737-232
Service difficulty reports · 1,700
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 = '737232' 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 = '737232' 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 DL73S040462Wire · pinchedROW 11-16 EMERGENCY LIGHTS INOPERATIVE. FOUND WIRE PINCHED UNDER FLOOR TRACK COVER, REPLACED FUSE IN POWER PACK AND REPAIRED WIRE UNDER SEAT TRACK COVER.SDR DL73S040562Floorbeam · crackedFLOORBEAM TEE CAP UPPER FLANGE CRACKED STA 328 AT LBL 12. INSTALLED REPAIR PER SRM 53-10-9D.SDR DL73S040454Connector · not seatedEMERGENCY EXIT LIGHT COME ON AND GO OUT OFF WITHOUT A POWER FAILURE. RESET PLUG ON E-PATH POWER SUPPLY. NO OCCURRENCE NOTED.SDR DL73S040451Coffeemaker · malfunctionedDURING FLIGHT AFT CABIN ATTENDANTS NOTICE ELECTRICAL SMELL IN THE AFT GALLEY. SHORTLY AFTER SMELL STARTED SMOKE DETECTOR IN AFT LAV STARTED TO SOUND. THE C/B FOR THE AFT GALLEY COFFEEMAKER POPPED AND THE SMELL WENT AWAY. THE AFT LAV SMOKE DETECTOR CONTINUEDSDR DL73S040434Battery Pack · dischargedR1 EXIT DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK.SDR DL73S040430Skin · delaminatedNR 2 AFT FLAP AFT SKIN SEPARATED/DELAMINATED AT IB END. REPAIRED IAW SRM 51-40-20 FIG 10.SDR DL73S040418Skin · delaminatedWHILE WORKING N/R 13 FOUND LT ELEVATOR UPPER SURFACE DELAMINATED UNDER CONDUCTIVE FRAME REPAIRED PER SRM 55-20-03 FIG 1 TABLE 1.SDR DL73S040412Battery · inoperativeFWD BULLNOSE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY. CHECKS OK.SDR DL73S040411Fuse · failedAFT LT BULLNOSE EMERGENCY LIGHTS INOPERATIVE, REPLACED BATTERY. NO HELP. REPLACED FUSES ON CHARGER. CHECKS GOOD.SDR DL73S040402Rmi · smokeNR 2 RMI STARTED TO SMOKE. REPLACED SAMESDR DL73S040401Housing · crackedLOST A HYDRAULIC SYSTEM ON TAXI IN TO GATE AT ORD. FOUND NR 8 GROUND SPOILER ACTUATOR BODY CRACKED. REPLACED NR 8 GROUND SPOILER PER AMM 27-62-101, PB 401. LEAK AND OP. CHECK GOOD. RII PERFORMED.SDR DL73S040426Skin · cracked3/16 INCH CRACK IN FUSELAGE OUTER SKIN AT C2 DOOR CUTOUT UPPER AFT CORNER , FASTENER REPAIR PER SRM 53-30-3 FIG 6SDR DL73S040395Skin · crackedDENT & CRACK ON LWR SIDE OF I/B GROUND SPOILER 1.5 INCH FWD OF T/E AFT OF INBOARD ACTUATOR.SDR DL73S040372Bulkhead · crackedINSPECTION OF THE AFT P-DOME WEB PER AD 99-08-23 REVEALED CRACKS IN THE WEB COMMON TO THE BULKHEAD Y-CHORD NEAR STRINGER 5R. THE CRACKED AREA OF WEB WAS REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PESDR DL73S040359Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 727B+2 ALONG THE BONDED DOUBLER LINE JUST BELOW STRINGER 18L. THE CRACK IS TYPICAL OF BAC S/B 737-53-1065. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PESDR DL73S040349Power Supply · failedEMERGENCY INSEAT LIGHTING SEATS 21-24 INOP. REPLACED FUSE IN PWR SUPPLY M9013. CHECKS OK.SDR DL73S040346Skin · crackedINSPECTION OF THE STRINGER 10R SKIN LAP JOINT FROM FS 360 TO 540 PER AD 2003-08-15, REVEALED A SINGLE CRACK AT FS 370. THE CRACK WAS REMOVED WITH A 1 X 4.25 INCH CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3 AND PER ER/A 0SDR DL73S040345Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 540 & 727 PER AD 2003-08-15, REVEALED 15 CRACK INDICATIONS. THE ENTIRE LAP JOINT WAS CUT OUT AND REPLACED WITH ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53A1177 AND ER/A 089523-14AD.SDR DL73S040320Skin · crackedINSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15, REVEALED A TOTAL OF 9 CRACKED FASTENER HOLES AT THREE LOCATIONS IN THE JOINT. THE CRACKS WERE REMOVED WITH CUTOUTS OF 15.5 X 1 INCH AND TWO CUTOUTS OF 7.25 X 1 INCH. THE CUTOUTS WERE REPAIRED WISDR DL73S040319Skin · crackedINSPECTION OF THE STRINGER 10L LAP JOINT BETWEEN FS 360 & 540 REVEALED A CRACKED FASTENER HOLE AT FS 380. THE CRACKED HOLE WAS REMOVED WITH A 1 X 4 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER BAC 737 SRM 53-30-3, FIG 42. THE REPAIR SDR DL73S040318Skin · crackedINSPECTION OF THE STRINGER 14L SKIN LAP JOINT PER AD 2003- 08-15, REVEALED A CRACKED FASTENER HOLE AT FS 500A+10 & ANOTHER AT FS 500B+15. THE CRACKS WERE REMOVED WITH SKIN CUTOUTS (1 X 4 & 1 X 7 INCH RESPECTIVELY). THE CUTOUTS WERE REPAIRED WITH ALUMINUM DOSDR DL73S040314Engine · malfunctionedABORTED T/O DCA DUE TO NR 2 ENG EPR HUNG AT 1.6, N1, N2, EGT, FF LOWER THAN NR 1. CLEARED RUNWAY, RAN ENG TO FULL POWER OK. SUSPECT CROSSWIND FOR THE LEFT AFFECTED NR 2. DID STATIC RUNUP PRIOR TO 2ND T/O, NR 2 SLOWER TO ACCEL TO T/O THAN NR 1, BUT DID REACHSDR DL73S040283Frame · corrodedCORROSION ON AFT SIDE OF FORMER STA 827 O/B OF STR 27R. INSTALLED PERMANENT REPAIR PER SRM 53-10-4 FIG 6. COMPLETED AND SENT SSI DATA RETRIEVAL.SDR DL73S040273Skin · damagedTHE FUSELAGE WAS INSPECTED AND FOUND TO HAVE EVIDENCE OF SCRIBING ALONG THE LOWER SKIN OF SEVERAL SKIN LAP JOINTS BETWEEN FS 360 & 1016 IN THE UPPER FUSELAGE BETWEEN STRINGERS 14L & 14R. THE BUTT JOINTS OF THE FUSELAGE WERE ALSO FOUND WITH SCRIBE INDICATIONS.SDR DL73S040254Battery · inoperativeFOUND AFT UPPER LT EMERGENCY LIGHTS 3 EACH INOP. REPLACED BATTERY ASSY, OPS NORMAL.SDR DL73S040259Skin · crackedINSPECTION OF THE SKIN LAPS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 10R SKIN LAP SPLICE AT FS 432. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKIN TO REMOVE THE CRACKED AREA. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER BSDR DL73S040258Skin · crackedINSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 14R SKIN LAP JOINT. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKIN TO REMOVE THE DAMAGED AREA AND AN ALUMINUM REPAIR DOUBLER INSTALLED PER B737 SRM AND DOCUMENTED PSDR DL73S040241Csd · failedON TAKEOFF RT GEN LOW OIL PRESS LIGHT ON WITH GEN DROPPING OFF LINE WITH APU POWERING LEFT BUS DUE TO MCO ON LEFT GEN. AFTER FIVE MINUTES LOW OIL PRESSURE LIGHT OUT AND RIGHT GEN BACK ON RIGHT BUS, FREQS LOW AT 390, RIGHT GEN FELL OFF BUS AGAIN FOR REMAINDER SDR DL73S040248Stringer · crackedSTRINGER 4L DAMAGED IN LWR RADIUS AT STA 797. REPAIRED PER SRM 53-10-3 FIG 4.SDR DL73S040229Relief Valve · failedDURING APPROACH PHASE AFTER PLACING THE FLAP LEVER TO 5 SYSTEM A PRESSURE WENT TO ZERO WITH ASSOCIATED SYSTEM A LOW PRESSURE LIGHTS ILLUMINATED. REPLACED SEVERAL LINES AND RESERVOIR PRESSURE RELIEF VALVE.SDR DL73S040234Skin · scratchedTHE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH SCRIBE DAMAGE. THE LAP JOINT WAS CUTOUT FROM FS 727 TO FS 908 TO REMOVE THE JOINT AND THE DAMAGE. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53A1177 AND ERSDR DL73S040233Skin · scratchedTHE LOWER SKIN OF THE STRINGER 4L SKIN LAP SPLICE WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 540-727. THE ENTIRE LAP JOINT WAS CUT AWAY TO REMOVE THE DAMAGE. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53A117SDR DL73S040220Skin · gougedTHE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND DENTED AND GOUGED AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT STRINGER 22R. THE DAMAGE WAS REMOVED WITH A 1 X .75 INCH CUTOUT FROM THE DOOR CUTOUT EDGE. THE DAMAGE WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOSDR DL73S040206Skin · crackedTHE STRINGER 4L & 4R SKIN LAP JOINTS WERE FOUND WITH SEVERAL CRACKS BETWEEN FS 540 & 727 WHEN INSPECTED PER AD 2003-08-15. THE CRACKED LAP JOINTS WERE CUTOUT IN THEIR ENTIRETY AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53A1177 AND PER ER/A 3SDR DL73S040197Power Supply · inoperativeEMERGENCY PATH LIGHTS AT ROWS 22-25D INOP. REMOVED AND REPLACED POWER SUPPLY.SDR DL73S040193Accessory Unit · failedON T/O WHEN GEAR HANDLE RAISED LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ON. NO OTHER ABNORMAL INDICATIONS. REPLACED LANDING GEAR ACCESSORY UNIT.SDR DL73S040191Regulator · leakingLOSS OF A-SYSTEM HYDRAULIC PRESSURE. FOUND NO RESERVOIR HEAD PRESSURE. REPLACED RESERVOIR PRESSURE REGULATOR AND BOTH CHECK VALVES.SDR DL73S040178Start Valve · contaminatedRIGHT ENGINE START VALVE OPEN LIGHT CAME ON DURING CLIMBOUT ISOLATION VALVE AND ENGINE BLEED VALVE WERE CLOSED. LIGHT WENT OUT AT LOW PWR SETTING. LIGHT STAYED OUT AT LOW PWR. FOUND F/F XMTR LEAKING AT HI PWR SETTING. REPLACED PACKING AND BACK UP RINGS. RSDR DL73S040172Clevis · corrodedCORROSION DAMAGE WAS NOTED ON THE NR 5, NR 6 AND NR 11 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW 386170-14.SDR DL73S040170Skin · dentedTHE UPPER SKIN OF THE S19R WAS FOUND DENTED. DENTED WAS REMOVED AND REPAIR INSTALLED IAW 386089-14.SDR DL73S040169Support Fitting · corrodedCORROSION WAS NOTED ON BOTH THE LT AND RT BS 685 MLG SUPPORT FITTINGS IN THE LUG BORES AND FACES. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW ERA 386114-14.SDR DL73S040166Actuator · leakingON TAXI TO GATE POSTFLIGHT LOST A-SYSTEM HYDRAULICS, QUANTITY ZERO AND PRESSURE ZERO. REPLACED LEFT OUTBOARD SPOILER ACTUATOR FOR LEAKAGE.SDR DL73S040155Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 4 INCH TYPICAL CRACK IMMEDIATELY ABOVE STRINGER 16L. THE CRACK RAN ALONG THE EDGE OF THE BONDED INTERNAL DOUBLER AT THE STRINGER. THE CRACK WAS REMOVED WITH A CUTOUT THROUGH THE SKIN AND BONDED DOUBLER AND REPAIRED WITH AN SDR DL73S040152Bulkhead · corrodedCORROSION WAS NOTED AT BS 1016 PRESSURE BLKHD, AT BL 0 AND AFFECTED THE WEB/GORE AND CHANNEL STIFFENERS. REPAIRED PER ERA 386069-14AD.SDR DL73S040149Frame · crackedDURING INSPECTION OF THE BS 663 FRAME CRACKS WERE NOTED IN THE FRAME AT S3L, S2L AND S1. DURING INSTALLATION OF THE SRM FRAME REPAIR IT WAS NECESSARY TO CUT THE FUSELAGE SKIN TO ACCOMMODATE FRAME REPAIR FASTENERS. FRAME WAS REPAIRED PER SRM, SKIN REPAIRED PESDR DL73S040146Actuator · leakingNR 2 FLT SPOILER LEAKING. LOSS OF A-SYSTEM HYD. REMOVED NUMBER 1 SPOILER ACTUATOR.SDR DL73S040144Flap Track · corrodedTHE REAR ENGINE MOUNT ATTACH HOLES, LOCATED AT THE NR 2 AND NR 3 T/E FLAPS, OUTBOARD TRACKS WERE NOTED WITH CORROSION IN THE BORES. CORROSION WAS REMOVED AND TRACKS WERE REWORKED PER ERA 386130-14.SDR DL73S040143Control Cable · stiffDURING CLIMB TO 370 FROM 330 NR 1 THROTTLE POPPED BACK AND FORTH. A/T DISCONNECTED AND THROTTLE STIFF. AFTER DESCENT BELOW 330 THROTTLE WORKED NORMAL AND NOT AS STIFF. REPLACED NR 1 ENGINE THROTTLE PUSH-PULL CABLE. RAN ENGINE PER PFHB. OPS GOOD.SDR DL73S040131Bulkhead · canningTHE WEB OF THE FS 1016 AFT P-DOME WAS FOUND WITH AN OIL-CAN CONDITION BETWEEN S-3L & S-5L. THE DAMAGED AREA OF WEB WAS CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 088351-14AD.SDR DL73S040115Attach Fitting · corrodedTHE STABILZER ATTACHMENT LUGS WERE FOUND WITH DAMAGE EXCEEDING THE LIMITS OF SB 737-55-1033. DAMAGE WAS REMOVED BY BLENDING AND OVERSIZING BORES PER ER/A 386108-14AD.
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