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 DL73K990283Power Supply · inopON S/C, FOUND LT OVERWING SLIDE LIGHT, RT OVERWING EXIT SIGN, AISLE LIGHT SEAT 4DEF AND AISLE LIGHT SEAT 8ABC INOP ON EMERGENCY LIGHTS TEST. REPLACED BATTERY CHARGER M01135.SDR DL73K990280Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT THE LOWER FWD CORNER OF THE L2 DOOR SURROUND LOWER HINGE CUTOUT. THE CRACK WAS .25 INCH LONG IN THE SKIN ONLY. THE CRACK WAS ROUTED OUT, THE UNDERLYING BEAR STRAP INSPECTED, AND AN EXTERNAL REPAIR DOUBLER INSTALLED PERSDR DL73K990271Fitting · corrodedFUSELAGE RT AND LT MLG SIDE STRUT SUPPORT FITTINGS, FS 685, REPAIR FOR LUG BORE CORROSION. THE LOWER LUGS OF THE LT AND RT MLG SIDE STRUT SUPPORT FITTINGS WERE FOUND TO HAVE CORROSION IN THE LOWER LUG BORES. THE LUG BORES WERE OVERSIZED TO REMOVE THE CORROSISDR DL73K990233Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 1 INCH LONG CRACK JUST ABOVE STRINGER 16R AT FS 522. THE CRACK WAS ROUTED OUT AND A REPAIR DOUBLER INSTALLED PER B737 SRM 53-30-3, FIG 1. BECAUSE THE REPAIR EXTENDED UNDR A WING-TO-FUSELAGE PANEL THE REPAIR WAS DOCUMENTEDSDR DL73K990170Skin · crackedTHE AFT ENTRY DOOR CUTOUT WAS FOUND WITH A .25 INCH LONG TYPICAL CRACK IN THE LOWER DOOR HINGE CUTOUT. THE CRACK WAS IN THE SKIN AND BONDED DOUBLER ONLY. THE DAMAGED SKIN ASSY WAS CUT AWAY AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND STEEL TRIPLER PERSDR DL73K990077Wire · shortedLEFT AND RIGHT FWD DOORS EMERGENCY LIGHT EXIT IDENTIFIERS DO NOT ILLUMINATE WHEN TESTED. POWER SUPPLY FUSE BLOWN DUE TO LEFT LIGHT ASSY WIRE SHORTED. REPLACED FUSE IN POWER SUPPLY AND REPLACED LEFT LIGHT ASSY.SDR DL73K982655Skin · crackedDURING RTN VISUAL INSPECTIONS, A CRACK WAS FOUND IN THE LWR BONDED SKIN PANEL AT THE LWR HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) SURROUND. TRIMMING OUT THE DAMAGE IN THE LWR BONDED SKIN REVEALED A CRACK IN THE BEAR STRAP. TRIM OUT IN BEAR STRAP IS APPROX 1 SDR DL73K982610Fitting · corrodedFUSELAGE LT AND RT MLG SIDE STRUT SUPPORT FITTING, BS 685. REPAIR FOR OVERSIZE LUG BORES. THE LUG BORES OF THE LT AND RT MLG SIDE STRUT SUPPORT FITTINGS AT BS 685 WERE FOUND CORRODED. THE LUG BORES WERE OPENED A MAX OF .11 IN DIAMETER. STEEL REPAIR SLEEVES SDR DL73S982592Floorbeam · crackedFUSELAGE/OVERWING FLOORBEAM,BL 0 FS 660-664, REPAIR FOR CRACKS. THE OVERWING LONGITUDINAL FLOORBEAM UPPER CAP AT BL 0 WAS SEVERED AT FS 660 AND HAD AN ADDITIONAL CRACK FS 664. THE BEAM WEB WAS NOT DAMAGED. THE FLOORBEAM CAP WAS REPAIRED PER THE PROCEDURES OSDR DL73K982593Floorbeam · crackedFUSELAGE OVERWING FLOORBEAM, UPPER CAP BL 0 FS 66, REPAIR FOR CRACKED CAP. THE OVERWING FLOORBEAM AT BL 0 WAS FOUND WITH A SEVERED UPPER CAP AT FS 662 WITH AN ADDITIONAL CRACK IN THE CAP AT FS 666. THE UPPER CAP WAS REPAIRED PER THE GUIDELINES OF BAC S/B SDR DL73K982578Electrical Syst · lostON BASE LEG, SELECTED GEAR DOWN AND FLAPS 15, LOST ALL ELECTRICAL POWER, INCLUDING STBY PWR, HAD NO COMM/NAV. FLEW WITH STBY INST ON LANDING BLEW NR 1 TIRE DUE TO NO ROTATION. REPLACED NR 1 GCU P/N 948F458-2 S/N NF4063, NR 2 GCU S/N 3934, BATT P/N 23168 S/N SDR DL73K982533Skin · crackedTHE FUSELAGE SKIN ASSY AND BEAR STRAP WERE FOUND WITH AN APPROX 1 INCH LONG CRACK AT THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND BEAR STRAP AND REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS. THE REPAIR WAS SDR DL73K982498Actuator · failedLEADING EDGE AMBER LIGHT ON SLAT NR 5. REPLACED NR 5 SLAT AND ACTUATOR.SDR DL73K982421Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 2 INCH CRACK AT FS 747 JUST BELOW S-18R. THE CRACK WAS ROUTED OUT OF THE EXISTING SKIN AND AN EXISTING, ADJACENT SKIN REPAIR WAS REMOVED AND THE UNDERLYING EXISTING SKIN CUTOUT INSPECTED. BOTH AREAS WERE INCORPORATED INTOSDR DL73S982349Battery Pack · dischargedTHE 4 AFT EMERGENCY PATHWAY LIGHTS INOP. REPLACED BATTERY PACK.SDR DL73K982285Module · failedCOCKPIT FIRE CONTROL PANEL SHORTED. POPPING NOISE COMING FROM PEDESTAL AREA. REMOVED AND REPLACED ENG/APU FIRE CONTROL MODULE.SDR DL73K982268Hinge · crackedTHE LOWER GATE HINGE ON THE R1 DOOR WAS FOUND CRACKED. THE CRACKED HINGE WAS REMOVED AND REPLACED PER THE REQUIREMENTS OF BAC S/B 737-52A1124. THE REPAIR WAS DOCUMENTED PER ER/A 366007-14AD.SDR DL73K982264Skin · crackedTHE FUSELAGE SKIN AT FS 740 WAS FOUND WITH A 1.25 INCH LONG CRACK BELOW STRINGER 18R. THE CRACK WAS REPAIRED PER THE B737-200 SRM 53-30-3 FIG 1. THE REPAIR DOUBLER EXTENDS UNDER THE WING TO BODY FAIRING, SO INFRINGES ON SSI F-41. THE REPAIR HAS BEEN DOCUMENSDR DL73K982266Skin · crackedTHE FUSELAGE SKIN AND DOUBLER WERE FOUND TO HAVE A 1.5 INCH TYPICAL CRACK AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT. THE CRACK WAS REPAIRED PER THE B737-200 SRM 53-30-3 FIG 26, EXCEPT BLIND BOLTS WERE AUTHORIZED ON A TIME LIMITED BASIS. THE REPAIR WAS ACSDR DL73K982229O-Ring · failedLOSS OF HYD SYS A QTY IN FLT. REPL NO3 FLT SPOILER ACTUATOR. O-RING RUPTURED ON ACTUATOR. ALL LEAK AND OPN TEST NML.SDR DL73K982223Control Cable · frayedRT AILERON BINDING AT FULL RT TRAVEL. INSP FOUND AILERON CABLE SEGMENT ABSB-4 FRAYED. MANUFACTURED & INSTLD NEW CABLE SEGMENT ABSB-4 PER M/M. REPLD 2 EA AILERON BUS CABLE PULLEYS AT APPROX STA RBL 60. RIGGED AILERON BUS CABLES AND OPS CKD, ADJUSTED FIRST OSDR DL73K982186Skin · crackedFUSELAGE SKIN, FS 520, S-16L SKIN CRACK REPAIR. THE FUSELAGE SKIN WAS FOUND WITH A CRACK ABOVE STRINGER 16L AT FS 520. THE CRACK WAS CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 1. THE REPAIR WAS DOCUMENTED PER ER/A 365917-14. THESDR DL73K982183Fitting · corrodedFUSELAGE, RT AND LT MLG SIDE STRUT SUPPORT FITTING, BS 685, REPAIR FOR O/S HOLE BORES. THE LT AND RT MLG SIDE STRUT SUPPORT FITTINGS WERE FOUND WITH CORROSION IN THE LOWER HOLE BORES OF THE FITTINGS. THE HOLES WERE OVERSIZED TO REMOVE THE CORROSION AND LARGESDR DL73K982137Bulkhead Web · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH A CRACK AT LBL 5.7, WL 212. THE WEB HAD A PREVIOUS REPAIR IN THE AREA FOR 3 OTHER CRACKS WHICH WERE CUTUOUT OF THE WEB. THE EXISTING REPAIR DOUBLER WAS REMOVED, THE NEW CRACK CUTOUT, THE WEB INSPECTED FURTHER AND A NESDR DL73S982090Fitting · damagedTHE LT MLG SIDE STRUT SUPPORT FITTING AT BS 685 WAS DAMAGED BY TOOL MARKS. REPAIRED PER ERA 332329-14.SDR DL73S982089Skin · damagedC2 DOOR CUTOUT WAS WITH AN EXISTING REPAIR ALONG THE FWD EDGE. UPON REMOVAL OF THE REPAIR ADDITIONAL DAMAGE WAS FOUND. REPAIRED PER ERA 332286-14.SDR DL73S982088Frame · crackedCRACK FOUND IN THE FAIL/SAFE CHORD OF THE STA 907 FRAME AT APPROX S13R. REPAIRED PER ERA 332297-14.SDR DL73S982087Frame · damagedDURING MODIFICATION OF THE FUSELAGE FRAMES SEVERAL WERE DAMAGED. THE DAMAGE REQUIRED TRIMMING OFF/OUT THE TOOLING DAMAGE. REPAIRED PER ERA 332294-14.SDR DL73S982086Frame · crackedSTA 440 FRAME WEB FOUND CRACKED AT A TOOLING HOLE BETWEEN S13R - 14R. REPAIRED PER ERA 332298-14.SDR DL73K982051Fuel Control · malfunctionedNR 1 ENGINE COMPRESSOR STALLS AT FL370. AC YAWED LT EACH TIME AND N1 AND F/FLOW GAUGES FLUXED. N1 GAUGE WOULD SPIKE 5PC DROP. 5 SPIKES AT 1 SECOND INTERVALS. FLT DIVERSION TO MCO. INSP ENG COMPRESSOR AND EXH WITH BOROSCOPE. NO TROUBLE FOUND. CKED PS3 FISDR DL73K982054Skin · crackedFUSELAGE/SKIN ASSY/R1 DOOR CUTOUT/LOWER AFT CORNER: REPAIR FOR SKIN CRACK. A .5 TYPICAL CRACK WAS FOUND IN THE SKIN AND BONDED DOUBLER AT THE LOWER AFT CORNER OF THE R1 (FWD GALLEY) DOOR CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN ALUMINUM DOUBLERSDR DL73K981951Temp Bulb · failedSHUT DOWN NR 1 ENGINE IN FLIGHT DUE TO HIGH OIL TEMP. FOUND NR 1 ENG OIL TEMP BULB OPEN. REPLACED TEMP BULB PER M/M, OPN CKD GOOD. LK CK GOOD. RAN ENG PER PFHB. ALL CKS GOOD.SDR DL73K981927Line · leakingHYD LEAK A-SYS TOTAL LOSS. FOUND LEAK NR 1 ENG. REPLACED HYD PUMP PRESS AND CASE DRAIN LINES. REPLACED HYD PUMP AS PRECAUTION. CHECKED CASE DRAIN FILTER FOR CONTAMINATION, NONE FOUND. REPLACED SAME. SERVICED SYS RAN ENGS AND FLT CONTROLS TO BLEED. ALL CKSDR DL73K981870Battery Pack · dischargedAFT RIGHT SERVICE DOOR SLIDE LIGHT INOP. REPLACED BATTERY PACK. CKS GOOD.SDR DL73S981844Bolt · missingAPU FIRE WARNING WHILE ON APPROACH. FOLLOWED CHECKLIST. FIRED BOTTLE, FIRE WARNING EXTINGUISHED. FOUND BOLT MISSING FROM FUEL ATOMIZER CAUSING HEAT TO REACH FIRE LOOP.SDR DL73S981794Actuator · failedRUNAWAY STAB TRIM ON SHORT FINAL. GO-AROUND MADE. REPLACED STAB TRIM ACTUATOR.SDR DL73K981793Power Supply · inoperativeMID PATH LIGHTS INOP. REPLACED POWER SUPPLY.SDR DL73K981778Skin · crackedA CRACK WAS FOUND IN THE SKIN AT FS 520 AND STR 16L. THE UNDERLYING STRINGER WAS FOUND WITH A TYPICAL CRACK AT THE END OF THE STRINGER AS OUTLINED IN BAC S/B 737-53-1145. THE SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER PER SRM PROCEDURE AND THE STRINGER WAS RSDR DL73S981712Battery Pack · dischargedRT O/W EMERGENCY SIGN INOP. REPLACED BATT PK.SDR DL73S981665Power Supply · inoperativeON L/O-2 CHECK FOUND EMERGENCY EXIT LIGHT ABOVE RT OVERWING DOOR INOP, M1135 POSITION. REPLACED POWER SUPPLY.SDR DL73K981632Bulkhead Chord · crackedA 0.5 INCH CRACK WAS FOUND IN THE MLG WHEEL WELL BLKHD AT STA 727. THE CRACK WAS LOCATED IN THE UPPER FLANGE OF THE COMPRESSION CHORD AT BL 0.0 AND RUNS THRU A FASTENER HOLE. REPAIRED PER ERA 365406-14.SDR DL73K981643Floorbeam · crackedCRACKS WERE FOUND IN THE UPPER CHORD OF THE LBL 24 AND RBL 24 OVERWING FLOORBEAMS AT APPROX STA 670 TO 675. THE CRACKS EMINATED FROM THE SEAT TRACK FASTENER CUTOUTS. CRACKING IS DUE TO FATIGUE. REPAIRED PER ERA 332012-14.SDR DL73K981637Skin · crackedAFT EDGE OF C2 DOOR CUTOUT WAS FOUND CRACKED AT APPROX 10 BELOW THE SKIN LAP SPLICE. REPAIRED PER ERA 332013-14.SDR DL73K981636Frame · gougedFS 380 FRAME WAS GOUGED APPROX 3 ABOVE S27L IN THE UPPER FREE FLANGE. REPAIRED PER ERA 332007-14.SDR DL73K981635Floorbeam · crackedBL 0 FLOORBEAM OF THE WING CENTER SECTION IS CRACKED AT BS 664. NO CRACKS FOUND IN THE WEB. REPAIRED PER ERA 331996-14.SDR DL73K981634Strap · corrodedTHE REINFORCEMENT STRAP FOR THE C2 DOOR CUTOUT FWD FRAME WAS CORRODED AT THE NUT PLATE HOLES AT APPROX S25R. REPAIRED PER ERA 332025-14.SDR DL73K981633Floorbeam · crackedLBL AND RBL 24 CABIN FLOORBEAMS OVERLYING THE MAIN WHEEL WELL AT APPROX STA 678 WERE FOUND WITH CRACKS IN THE WEB AND WEB DOUBLER. REPAIRED PER ERA 332046-14.SDR DL73K981610Power Supply · inoperativeEMERGENCY LIGHTS FLASHING RT AISLE AND AFT BULKHEAD. REPLACED POWER SUPPLY.SDR DL73K981566Door · not latchedFWD CARGO DOOR LIGHT ILLUMINATE UPON TOUCH DOWN. FOUND DOOR OPEN, CHECKED DOOR LATCHES AND ALL WARNING SYS ALL CKS NML.SDR DL73K981567Battery · dischargedFOUND LAST THREE LEFT SIDE AISLE EMERGENCY LIGHTS INOP. FOUND BATTERY BAD FOR PWR SUPPLY. REPLACED PWR SUPPLY, AND NEW BATTERY.
Back to Boeing 737-232