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 DL73S040104Attach Fitting · corrodedNUMEROUS ATTACHMENT FITTING LUGS ON THE HORIZ STAB TO FUSELAGE JOINT REQUIRED MACHINING BEYOND PUBLISHED LIMITS IN ORDER TO REMOVE CORROSION. CORROSION WAS REMOVED AND LUGS REWORKED IAW ERA 386108-14AD.SDR DL73S040102Floorbeam · crackedDURING INSPECTION THE BS 520 FLOORBEAM WAS NOTED WITH CRACKS IN THE RADIUS, ALONG THE UPPER CHORD TO WEB RADIUS AT LBL 24.75, LBL 45.5 AND RBL 24.75. UPPER CAP WAS REMOVED AND A NEW SECTION SPLICED IN PER ERA 386080-14.SDR DL73S040105Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 2.75 INCH CRACK RUNNING ALONG THE BONDED DOUBLER LINE JUST ABOVE STRINGER 19L BETWEEN FS 776 & 787. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER BAC S/B 737-53-106SDR DL73S040087Blade · brokenAT TOP OF DESCENT UPON THROTTLE RETARD NR 2 ENGINE VIBRATION. ALL ENGINE PARAMETERS NORMAL. AT 75 PERCENT VIBRATION DISCONTINUED. LEFT ENGINE AT 75 PERCENT. FOUND TURBINE BLADE DAMAGE. REPLACED ENGINE.SDR DL73S040127Skin · crackedTHE UPPER AFT CORNER OF THE L2 DOOR CUTOUT WAS FOUND WITH 2 SMALL CRACKS IN THE BONDED SKIN AND UNDERLYING BEAR STRAP. THE CRACKS WERE REMOVED WITH 1 INCH CUTOUTS. THE CUTOUTS WERE REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3 AND ER/SDR DL73S040045Charger · inoperativeMCO OVERHEAD EMERGENCY LIGHT BULLNOSE INOP 19D. FOUND BATTERY CHARGER RACK AT M1134 STA 629L INOP. REPLACED CHARGER RACK.SDR DL73S040025Hose · leakingLOSS OF A-SYSTEM HYDRAULICS IN FLIGHT. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE LEAKING. REPLACED NR 2 ENG HYDRAULIC PRESSURE HOSE. HOSE LEAK CHECKS GOOD. SERVICED A-SYSTEM HYDRAULICS TO FULL. SPUN & RAN ENGINE PRESSURE AND LEAK CHECK GOOD.SDR DL73S040018Battery Pack · inoperativeON PREFLIGHT FOUND FWD ESCAPE PATH LIGHTING INOP. REPLACED BATTERY PACK AND RACK.SDR DL73S040012Engine · failedAT CRUISE FROM YYZ - ATL NR 02 ENGINE OIL PRESS DROPPED TO 28 PSI ALL OTHER INDICATIONS NORM. NR 02 OIL QTY ON MCO NO LOW OIL PRESS LIGHT. AFTER CONSULTING WITH ATL DIVERT TO CVG AND NR 02 ENGINE SHUTDOWN. ENGINE SHUTDOWN REPORT COMPLETED. CHECKED OIL QTY SDR DL73S031146Engine · malfunctionedAFTER T/O, NR 2 ENGINE WENT TO FULL THEN DROVE TO IDLE. ENGINE DATA READ ON FDR. REPLACED NR 2 ENGINE.SDR DL73S031139Line · chafedA SYSTEM HYDRAULIC FAILURE ON FINAL, PRESSURE AND QUANTITY WENT TO ZERO. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE LINE CHAFED THROUGH. REPLACED LINE.SDR DL73S031132Skin · dentedDAMAGE FOUND ON LOWER SKIN PANEL OF RIGHT WING AT STA 525 NEAR OUTBOARD TIP. REPAIRED PER ERA 426849-14.SDR DL73S031131Attach Fitting · corrodedCORROSION WAS NOTED DURING INSPECTION OF THE HORIZ STAB ATTACH LUGS PER 03-069697-03 AND 03-053025-03AD. THE RIGHT SIDE OUTBOARD HORIZ STAB REAR SPAR UPPER ATTACH LUG WAS BEYOND PUBLISHED ALLOWABLE LIMITS. CORROSION WAS REMOVED AND LUG REWORKED PER ERA 38598SDR DL73S031129Skin · damagedDAMAGED FASTENER HOLES WERE REPORTED DURING PERMANENT REPAIR ACCOMPLISHMENT TO THE R2 DOOR UPPER HINGE CUTOUT. AREA WAS REWORKED/REPAIRED PER ERA 360517-14, REV A.SDR DL73S031128Skin · dentedA DENT WAS FOUND ABOVE S19L NEAR THE LWR AFT CORNER OF THE DOOR LOCATED NEAR BS 985. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385887-14.SDR DL73S031127Frame · dentedA DENT WAS FOUND IN THE INNER CHORD OF THE BS 767 FRAME JUST ABOVE S24L. DENT WAS REMOVED AND REPAIRED PER ERA 385960-14.SDR DL73S031126Clevis · corrodedCORROSION DAMAGE FOUND WHICH EXCEEDED LIMITS COVERED IN 03-085220-03. CORROSION WAS FOUND IN THE NR 6 AND NR 12 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND REWORKED PER ERA 386007-14.SDR DL73S031123Skin · crackedCRACK DAMAGE WAS NOTED ON THE KEEL BEAM LOWER SKIN PANEL. SKIN PANEL WAS REPLACED PER ERA 385927-14.SDR DL73S031112Skin · crackedINSPECTIONS REQUIRED PER AD 2003-08-15 REVEALED SEVERAL CRACKS IN THE STRINGER 4R SKIN LAP JOINT BETWEEN FS 380 & 420. THE CRACKS WERE REMOVED WITH CUTOUTS AND REPAIRED PER B737 SRM 53-30-3, 42. THE REPAIR WAS DOCUMENTED PER ER/A 087961-14AD.SDR DL73S031109Skin · crackedINSPECTION OF THE STRINGER 4R SKIN LAP JOINT REVEALED 15 CRACK INDICATIONS IN THE SKIN PANEL BETWEEN FS 540 & 727. THE INSPECTIONS WERE PERFORMED PER AD 2003-08-15. THE ENTIRE LAP JOINT WAS TRIMMED OUT AND REPAIRED PER BAC S/B 737-53A1177. THE REPAIR WAS DOSDR DL73S031108Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 867. THE CRACK WAS REMOVED WITH A CUTOUT TO THE SKIN WITH ADDITIONAL INSPECTIONS TO ENSURE NO FURTHER CRACKS. THE AREA WAS REPAIRED PER B737 SRM 53-30-3SDR DL73S031099Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT THE FWD INBD CORNER OF THE AFT LAV SERVICE DOOR CUTOUT NEAR FS 987 AND STRINGER 27R. THE DAMAGE WAS REMOVED WITH A 4 X 4 INCH CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED SDR DL73S031097Doubler · damagedFOUND ON W-2 LETTER CK, STRINGER 22RT CUT AT STA 957, 977, 996 FOR OUTFLOW VALVE DOUBLER REPLACEMENT. REPAIR PER SRM 53-10-3 FIG 1.SDR DL73S031096Frame · corrodedFOUND ON W2 LETTER CK, CORROSION ON FORMER STA 967 O/B OF STR 27 RIGHT. REPAIRED PER SRM 53-10-4 FIG 11.SDR DL73S031095Frame · corrodedFOUND ON W-2 LETTER CK, CORROSION ON FORMER STA 967 AT SKIN ATTACH ANGLE BETWEEN STR 27 LEFT AND 27 RIGHT. REPAIRED PER SRM 53-10-4 FIG 11.SDR DL73S031094Frame · corrodedFOUND ON W-2 LETTER CK, SKIN BULGED/ RIVETS SHEARED AT FRAME STA 847 BETWEEN STR 27 LEFT AND 27 RIGHT. FOUND FORMER CORRODED AT THIS LOCATION. REPAIRED PER SRM 53-10-4 FIG 9A.SDR DL73S031089Bulkhead · corrodedCORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD AT BS 1016 AND BL 0, BETWEEN S26L AND 26R. CORROSION WAS REMOVED THEN REPAIRED PER ERA 385921-14AD.SDR DL73S031078Skin · dentedDENTS WERE NOTED IN THE SKIN PANEL AT APPROXIMATELY BS 380 AND BETWEEN S15L AND S18L. DENTS WERE CUTOUT AND REPAIRED PER ERA 385947-14.SDR DL73S031058Gyro · defectiveON ROTATION, AIRPLANE PITCHED UP CAPTS GYRO WHICH WAS SELECTED TO AUX. PER MEL DID NOT OPERATE NORMAL, STRAIGHT AND LVL BUT DID NOT WORK WITH PITCH CHANGES. REPLACED NR 3 VG AS PER M/M, CKS GOOD.SDR DL73S031040Skin Panel · crackedDURING ACCOMPLISHMENT OF 03-058543-03, ME-01 EXISTING REPAIRS AND NEW CRACK DAMAGE WERE NOTED ON THE KEEL BEAM LOWER SKIN PANEL. THE SUBJECT SKIN PANEL WAS REPLACED PER INSTRUCTIONS CONTAINED IN ERA 385772-14.SDR DL73S031039Attach Fitting · corrodedDURING ACCOMPLISHMENT OF 03-069697-03 NUMEROUS ATTACHMENT LUGS REQUIRED MACHINING BEYOND THE LIMITS PROVIDED, IN ORDER TO REMOVE ALL CORROSION DAMAGE FOUND. LUGS WERE REWORKED PER INSTRUCTIONS CONTAINED IN ERA 385802-14AD.SDR DL73S031033Floorbeam · corrodedDURING MODIFICATION OF THE BL 24 FLOORBEAMS PER EO 03-056673-03AD ADDITIONAL WORK WAS REQUIRED DUE TO ADDITIONAL DAMAGE INCURRED. ERA 385831-14AD IMPLEMENTS THE LBL 24 BEAM MOD, PROVIDES NEW REPAIRS FOR THE BEAM WEBS AND ADDRESSES INCURRED DAMAGE.SDR DL73S031028Fitting · corrodedCORROSION DAMAGE WAS FOUND ON THE VERTICAL STAB NR 2 FIN LUG AND THE NR 11 BODY CLEVIS LUG. CORROSION WAS REMOVED AND REWORKED PER ERA 385810-14.SDR DL73S031036Skin · damagedTHE FUSELAGE SKIN WAS FOUND DAMAGED AROUND 2 NUT PLATE HOLES USED FOR ATTACHMENT OF A WING TO FUSELAGE FAIRING PANEL AT FS 760 BETWEEN STRINGERS 19R & 20R. THE DAMAGED HOLES WERE REMOVED WITH 1.5 X 1 INCH LOCAL CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLSDR DL73S031035Skin · gougedTHE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED NEAR FS 178 AND STRINGER 24R. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 087582-14, REV A.SDR DL73S031025Skin · dentedA DENT WAS NOTED IN THE FUSELAGE SKIN AT BS 380, BETWEEN S17L AND S18-L. THE DENT WAS CUT OUT AND REPAIRED PER ERA 385827-14.SDR DL73S031024Wire · shortedON L/O FOUND EMERGENCY LIGHTS AT SEAT ROWS 22-25 INOP AND L2 EXIT IDENTIFIER INOP. REPAIRED DAMAGED WIRE.SDR DL73S031010Floorbeam · crackedTHE FS 520 FLOORBEAM WAS FOUND WITH 1 INCH TO 2 INCH CRACKS NEAR THE UPPER CAP FLANGE AT RBL & LBL 24 & 45. THE CRACKS WERE TYPICAL OF BAC S/B 737-53-1120. THE UPPER CAP WAS TRIMMED OFF TO REMOVE ALL CRACKS. A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSIONSDR DL73S031002Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 2.5 INCH CRACK JUST BELOW STRINGER 18R AT FS 750. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385880-14, REV A.SDR DL73S031001Bulkhead · crackedA SMALL CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE FS 1016 AFT P-DOME WEB AT BL 0, WL 244. THE CRACK EMANATED IN 2 DIRECTIONS FROM THE HOLE AND WAS TOTAL OF .625 INCH LONG (INCLUDING HOLE DIA). THE CRACK WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLESDR DL73S030984Panel · delaminatedFOUND ON W-1 LETTER CHECK, VERTICAL STAB COMPOSITE T/E PANEL DELAMINATED 2 PLACES LEFT SIDE, 1 PLACE RIGHT SIDE. REPAIRED PER SRM 55-30-3 FIG 3.SDR DL73S030983Wedge · dentedFOUND ON W-1 LETTER CK, REPAIR LIFTING NUMBER 6 L/E SLAT T/E WEDGE 6 INCHES FROM O/B EDGE. REPAIRED PER SRM 51-40-20 AND OPERATION 1000.SDR DL73S030975Stop Fitting · damagedDURING ACCOMPLISHMENT OF EO 3-059252-3AD, OPN 0301, (S/B 737-52A1100), A 65-46861-0) FITTING WAS FOUND. EO INSTRUCTIONS REQUIRE ENGINEERING EVALUATION. EVALUATION FOUND THAT FITTING REQUIRED REPLACEMENT PER S/B 737-52-1065. FITTING REPLACED PER S/B 737-52-1SDR DL73S030970Attach Fitting · corrodedDURING INSPECTIONS PER EO 03-069697-03 AND 03-053025-03AD THE HORIZ STAB ATTACH FITTINGS, SEVERAL LUG BORES WERE OVERSIZED TO REMOVE CORROSION. CORROSION DAMAGE WAS CLEANED UP AND REWORKED PER ERA 38580314AD.SDR DL73S030969Skin · dentedA DENT WAS FOUND IN THE FUSELAGE SKIN AT BS 380 BETWEEN S17L AND S17A. DENT WAS REPAIRED PER ERA 385801-14.SDR DL73S030967Frame · damagedDURING REPAIR OF STA 663 FRAME AT S3L AN EXISTING FASTENER LOCATION WAS NOTED TO HAVE SHORTED ALONG WITH STANDOFFS THAT INTERFERED WITH REPAIR ACCOMPLISHMENT. REPAIR INSTRUCTIONS WERE ISSUED VIA ERA 385749-14.SDR DL73S030972Proximity Switch · failedATB LANDING MAIN RED LIGHT ON WITH GEAR RETRACTED. FOUND LEFT MAIN GEAR UPLOCK PROX SWITCH BAD S-72. REMOVED SAME, INSTALLED NEW PROX SENSOR AND ADJUSTED. CHECK GOOD ON GEAR SWING.SDR DL73S030918Gasper Fan · failedGASPER FAN C/B POPPED IN CLIMB WITH A BURNED METAL ODOR. REPLACED FAN.SDR DL73S030925Stiffener · corrodedINSPECTION OF THE FS 1016 AFT PRESSURE BULKHEAD PER AD 2002-10-11 REVEALED CORROSION ON THE RT BL 0 STIFFENER. NO OTHER DAMAGE WAS FOUND. THE DAMAGED AREA OF STIFFENER WAS TRIMMED AWAY AND REPAIRED PER BAC S/B 737-53A1075 AND ER/A 087493-14AD.SDR DL73S030924Skin · crackedA TYPICAL CRACK WAS FOUND IN THE LOWER FORWARD CORNER OF THE L2 DOOR CUTOUT THROUGH THE SKIN, BONDED DOUBLER, AND UNDERLYING BEAR STRAP. THE CRACK WAS REMOVED WITH A 1 X 2 INCH CUTOUT THROUGH THE STACK-UP. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REP
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