Boeing 737-232

Service difficulty reports · 1,700

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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"

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SDR DL73K001276Frame · crackedA CRACK WAS FOUND IN THE LOWER FASTENER OF THE INBOARD CHORD OF THE FS 616 JUST BELOW THE CABIN FLOOR. THE CRACK IS SIMILIAR TO THAT OF S/B 737-53-1182. ADDITIONALLY, A PILOT HOLE FROM THE FACTORY WAS FOUND AT THE LOWER EDGE OF THE SIXTH FASTENER FROM THJul 7, 2000 · N305DL · Boeing 737232 · Fuselage Main, FrameSDR DL73K001254Acm · seizedDUCT TEMP HIGH WITH NR PACK MIX VALVE IN FULL COLD. INTERMITTENT BURNING SMELL PRESENT IN AFT GALLEY AREA. NR 2 PACK APPEARS TO WORK FINE. - FOUND LT ACM FROZEN - REPLACED SAMEJul 3, 2000 · N308DL · Boeing 737232 · Cabin Cooling SystemSDR DL73K001248Seal · tornVERY LOUD SQUEAL AT 1L DOOR. FOUND DOOR PRESSURE SEAL RIPPED ALL THE WAY ACROSS BOTTOM OF L1 DOOR - REPLACED SAME.Jul 2, 2000 · N315DL · Boeing 737232 · Passenger/Crew DoorsSDR DL73K001234Bulkhead · damagedINSPECTIONS OF THE FS 178 BULKHEAD STRUCTURE PER AD 2000-05-19, REVEALED CRACKS IN THE BULKHEAD STRUCTURE COMMON TO THE COCKPIT FLOOR (REF. DAL ER/A 377636-14AD). IN ORDER TO ACCESS THE AREA FOR REPAIR, AN ACCESS HOLE HAD TO BE CUT IN THE BULKHEAD WEB AT Jun 29, 2000 · N329DL · Boeing 737232 · Fuselage Main, BulkheadSDR DL73K001232Attach Fitting · corrodedCORROSION WAS FOUND ON THE HORIZONTAL STABILIZER FRONT AND REAR SPAR ATTACH FITTING LUGS. THE LUGS WERE SPOT FACED AND THE BORES OVERSIZED PER ERA 334517-14 AT HMV.Jun 29, 2000 · N305DL · Boeing 737232 · Horizontal Stabilizer, Attach FittingsSDR DL73K001231Fitting · corrodedDURING HMV CORROSION WAS FOUND ON THE AFT FACES OF THE LEFT AND RIGHT VERTICAL STABILIZER PRIMARY REAR SPAR TERMINAL FITTING. THE AREA WAS BLENDED AND TREATED PER ERA 334527-14AT HMV.Jun 29, 2000 · N305DL · Boeing 737232 · Empennage Flight Control Surfaces, Attach FittingsSDR DL73K001221Web · crackedWHILE ACCOMPLISHING AD 2000-05-29 INSPECTIONS OF THE FS 178 BULKHEAD AND ADJACENT STRUCTURE, A 1 INCH CRACK WAS FOUND EMANATING FROM A LIGHTNING HOLE IN THE WEB OF THE HORIZONTAL FLOOR CLOSEOUT AT WL 207 ON BOTH THE LT AND RT SIDES OF THE AIRCRAFT. THE LT Jun 28, 2000 · N329DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR DL73K001222Bulkhead · crackedA TYPICAL CRACK WAS FOUND IN THE FS 178 BULKHEAD WEB AT WL 233.5, RBL 7 DURING INSPECTIONS MANDATED PER AD 2000-05-29. THE CRACK WAS REPAIRED PER B737-200 SRM 53-10-11, FIG. 1 AND DOCUMENTED PER ER/A 377622-14AD.Jun 27, 2000 · N329DL · Boeing 737232 · Fuselage Main, BulkheadSDR DL73K001198Skin · crackedTHE SKIN AROUND THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE LOWER DOOR HINGE CUTOUT. THE CRACK WAS REMOVED WITH A 1 INCH X 1 INCH CUT OUT THROUGH THE SKIN AND BONDED SURROUND DOUBLER. THE DAMAGE WAS REPAIRED WITH AN EXTERNAL STJun 21, 2000 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K001187Acm · leakingAFTER LANDING, CABIN FILLED WITH SMOKE. SHUTOFF APU BLEED AND BOTH PACKS, SMOKE DISSIPATED. FOUND OIL COMING OUT OF LT ACM INTO DUCT. REPLACED ACM, BOTH LT AND RT WATER COALESCER BAGS. RAN BOTH PACKS WITH APU AND ENGS, LEAK CHECK OK. NO SMOKE IN CABIN NOTJun 19, 2000 · N301DL · Boeing 737232 · Air Distribution SystemSDR DL73K001174Coffeemaker · burnedON T/O, STRONG SMELL OF SMOKE/ELECTRICAL/SULFUR. RETURN TO LAND MCO OVERWEIGHT LANDING AT 200 FPM, LANDING WEIGHT 112.8. REPLACED BOTH COALESCER BAGS. BOTH CLEAN, NO ODOR. PULLED FLIGHT INSTRUMENTS, NO SMELL. OPENED C/B PANELS, NO SMELLS. FOUND BURNT COFJun 18, 2000 · N302DL · Boeing 737232 · Buffet/GalleysSDR DL73K001161Receiver · inoperativeIN CLIMB LVL OFF AT 330, .74M AP-A ENGDG HEARD AND FELT MUFFLED BANG ASSOC W/ROLLING A/P DISENGAGED BANKED SEVERAL TIMES BEFORE STABILIZED BANK NEARED 30 DEGREES. NO OBSERVED ABNML ENG OR SYS INDICATIONS AFTER STABILIZING ACFT, NO OTHER ABNORMALTIES OCCURED Jun 15, 2000 · N303DL · Boeing 737232 · Visual Omnirange (VOR) SystemSDR DL73K001144Beam · crackedA CRACK WAS FOUND IN THE RT S18A SHEAR BEAM WEB AT BS 727. SUBJECT CRACK IS TYPICAL OF THOSE DEPICTED IN S/B 737-53-1066. THE CRACK IS LOCATED AT THE AFT, I/B MOST FASTENER LOCATION. THE SUBJECT SB IS NOT EFFECTIVE FOR AC 316. DAMAGE REPAIRED PER ERA 377513Jun 13, 2000 · N316DL · Boeing 737232 · Fuselage Main, StructureSDR DL73K001113Unknown · odorF/A REPORTS ELECTRICAL ODOR IN AFT GALLEY. CREW S/O GALLEY PWR AND SMELL DISSIPATED. DIVERTING TO RIC. CONTRACT MTC CHECKED AIRCRAFT INCLUDING RUNNING BOTH ENGS, ALL CKS OK. IT APPEARS PAX MAY HAVE HAD A PLANT THAT WAS PUTTING OUT SAME KIND OF ODOR THAT F/Jun 6, 2000 · N334DL · Boeing 737232 · Air Distribution SystemSDR DL73K001089Smoke Detector · will not testAFT LAV SMOKE DETECTOR WOULD NOT TEST. REPLACED SMOKE DETECTOR.Jun 3, 2000 · N302DL · Boeing 737232 · Smoke DetectionSDR DL73K001081Antenna · inoperativeWEATHER RADAR INOP, CON/IND FAULT. REPLACED R/T AND ANT PER MM, PUSHED OUT INTO RAMP AND PAINTED ACTUAL WEATHER, OPS NORMAL IN ALL MODES.Jun 2, 2000 · N319DL · Boeing 737232 · Weather Radar SystemSDR DL73K001037Engine · malfunctionedON T/O ROLL, LT ENG WOULD ONLY ACHIEVE 2.02 EPR. DISCONTINUEDT/O ROLL AT 60 KTS. TRIMMED 01/02 ENGS PER PFHB. PART PWR AND T/O PWR CHECKS GOOD. ALL ENG PARAMETERS NORMAL ON ENG RUN.May 26, 2000 · N331DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR DL73K001034Stringer · corrodedSTR 27L WAS FOUND CORRODED FROM FS 907 TO FS 947. THE STR WAS CUT AND REMOVED FROM FS 907 TO FS 1016 AND SPLICED IN PER ERA 3-53-11.May 26, 2000 · N303DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR DL73K001036Indicator · malfunctionedON T/O 03 SLAT LED SLAT REMAINED INTRANSIT ON T/O AFTER FLAP RETRACTION. RETURNED TO MCO. ON EXTENSION 02 SLAT REMAINED INTRANSIT. INSPECTED SLATS, RAN SLATS THRU SEVERAL CYCLES. SLAT OPERATE NORMAL. UNABLE TO DUPLICATE PROBLEM.May 25, 2000 · N318DL · Boeing 737232 · Leading Edge Slat Position Indicating SystemSDR DL73K001021Bulkhead · crackedTWO CRACKS WERE FOUND THE THE FS 178 BULKHEAD WEB AT APPROX WL 233.5. ONE WAS AT LBL 12 AND THE OTHER AT RBL 12. THE CRACKS WERE ROUTED OUT AND DOUBLERS WERE INSTALLED ON THE FORWARD SIDE OF THE WEB PER ERA 334418-14AD AT HMV.May 25, 2000 · N303DL · Boeing 737232 · Fuselage Main, BulkheadSDR DL73K001008Floorbeam · crackedA 2.2 INCH CRACK WAS FOUND AT RBL 24.75 IN THE VERTICAL WEB OF THE FS 520 FLOORBEAM. ADDITIONALLY, A CHANNEL ON THE AFT SIDE OF THE BEAM AT LBL 24.75 WAS FOUND TO HAVE A .5 INCH CRACK. THE CHANNEL WAS REPLACED AND THE BEAM WAS REPAIRED SIMILIAR TO THAT OF SBMay 23, 2000 · N303DL · Boeing 737232 · Fuselage Main, Floor BeamSDR DL73K001006Smoke · detectedTAXIING TO GATE, APU BLEED SOURCE SELECTED. RT PACK TURNED ON AND LITE SMOKE ENTERED CABIN. CONTRACT MTC. RAN APU FOR OVER AN HOUR WITH NO FURTHER FUMES/SMOKING. INSPECTED PACK BAY FOR ANY EVIDENCE OF HYDRAULIC LEAKS, NONE FOUND. UNABLE TO DUPLICATE PROBLMay 22, 2000 · N301DL · Boeing 737232 · Air Distribution SystemSDR DL73K000962Battery · failedAFT UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY.May 15, 2000 · N328DL · Boeing 737232 · Emergency EquipmentSDR DL73K000978Transformer · failedC/B POPPED, CREW REPORTED SMOKE AND BURNING SMELL BEFORE C/B POPPED. FOUND SHORTED TRANSFORMER IN OIL QTY INDICATOR. REPLACED SAME.May 14, 2000 · N305DL · Boeing 737232 · Engine Oil QuantitySDR DL73K000897Attach Fitting · corrodedTHE HORIZONTAL STABILIZER REAR SPAR ATTACH LUGS WERE FOUND CORRODED. THE DAMAGE WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED PER ERA 334311-14 AT HMV.May 5, 2000 · N304DL · Boeing 737232 · Horizontal Stabilizer, Attach FittingsSDR DL73K000896Fitting · corrodedCORROSION WAS FOUND ON THE LHS MLG SIDE STRUT SUPPORT FITTING. THE BORE WAS OVERSIZED AND A BUSHING INSTALLED PER ERA 334372-14 AT HMV.May 5, 2000 · N304DL · Boeing 737232 · Fuselage, Landing Gear Attach FittingsSDR DL73K000895Attach Fitting · corrodedSEVERAL OF THE FIN ATTACHMENT LUGS WERE FOUND CORRODED AT THE AFT SPAR. THE CORROSION WAS REMOVED AND THE BUSHINGS WERE RE-MANUFACTURED PER ERA 334313-14 AT HMV.May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR DL73K000894Stringer · crackedA 4 INCH CRACK WAS FOUND IN THE OUTBOARD SKIN FLANGE OF THE S27R KEEL CHORD AT FS 727A. THE EXISTING FACTORY SPLICE ANGLES WERE MODIFIED TO REPAIR THE DAMAGE PER ERA 334332-14 AT HMV.May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR DL73K000893Bulkhead · crackedTHE WEB OF THE FS 178 BULKHEAD WAS FOUND CRACKED AT RBL 1 AND WL 190. THE CRACK WAS REMOVED BY A 1.0 X 2.0 CUTOUT AND A DOUBLER WAS INSTALLED PER ERA 334328-14.May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, BulkheadSDR DL73K000892Stringer · crackedCRACKS WERE DISCOVERED ON THE WEB OF STR 18AL AT FS 727. ERA 334331-14 REPAIRS THE DAMAGE SIMILIARLY TO THAT OF S/B 737-53-1170. THE DAMAGE WAS FOUND AT HMV.May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR DL73K000891Frame · misinstalledTHE FS 440 FRAME INSTALLATION DID NOT MATCH THE CONFIGURATION FOUND IN S/B 737-53-1125. THE S/B REQUIRES INSTALLATION OF .2187 INCH FASTENERS AND THE FACTORY INSTALLATION INSTALLS .25 INCH FASTENERS. ERA 334319-14 ADDRESSES THIS CONDITION AND INSTALLSMay 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, FrameSDR DL73K000890Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A .375 INCH CRACK AT THE R2 DOOR UPPER HINGE CUTOUT. THE DAMAGE WAS LIMITED TO THE SKIN ONLY. THE DAMAGE WAS REPAIRED PER ERA 259665-14 AT HMV.May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000889Skin · corrodedCORROSION WAS FOUND ON THE FUSELAGE SKIN AT FS 967 BETWEEN STR 27L AND 27R. THE FRAME SHEAR TIE AND STR 27R WAS ALSO CORRODED AT THIS LOCATION. THE STRINGER WAS REPAIRED PER B737-200 SRM 53-10-3, FIGURE 1, THE FRAME SHEAR TIE REPLACED AND THE SKIN WAS REPAMay 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000860Floorbeam · crackedCRACKING FOUND IN BL 0 LONGITUDINAL FLOORBEAM WEB AFT OF STA 717. RESULTED IN TRIMOUT OF BEAM WEB BETWEEN STA 700 AND 721. CORRECTIVE ACTION: ER/A 334337-14.Apr 27, 2000 · N304DL · Boeing 737232 · Fuselage Main, Floor BeamSDR DL73K000810Battery Pack · inoperativeL1 DOOR SLIDE LIGHT DIM DURING TEST. REMOVED AND REPLACED L1 SLIDE LIGHT BATTERY PACK AND RACK, OPS CKS OK.Apr 25, 2000 · N307DL · Boeing 737232 · Emergency LightingSDR DL73K000791Warning Light · false indicationLEFT, RIGHT AND APU FAULT DET ILLUMINATED. REPLACED COCKPIT FIRE CONTROL PANEL. GROUND CHECKS NORMAL. REPLACED FIRE DETECTOR MODULE PRECAUTIONARY OPS NORMAL. RAN ENGS, NO FAULT DET LIGHTS. OK FOR SERVICE.Apr 23, 2000 · N329DL · Boeing 737232 · Detection SystemSDR DL73K000794Support Fitting · corrodedTHE LUG BORE OF THE RT MLG SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE BORE HOLE. A STEEL BUSHING WAS INSTALLED TO RESTORE THE BORE DIA TO THE BLUEPRINT DIAMETER. THE REPAIR WAS ACCOMPLISHED PER Apr 21, 2000 · N307DL · Boeing 737232 · Fuselage, Landing Gear Attach FittingsSDR DL73K000752Power Supply · inoperativeOVERHEAD EMERGENCY LIGHT INOP AT SEAT ROW 6 DEF. REPLACED BATTERY PACK POWER SUPPLY.Apr 18, 2000 · N318DL · Boeing 737232 · Emergency LightingSDR DL73K000729Keelbeam · corrodedTHE LOWER SKIN OF THE KEEL BEAM WAS FOUND CORRODED BETWEEN FS 661 AND FS 727. THE SKIN PANEL WAS REMOVED AND REPLACED PER ERA 334318-14 AT HMV.Apr 16, 2000 · N304DL · Boeing 737232 · Fuselage Main, KeelSDR DL72L001013Spar · crackedAFT SPAR RAIL CRACKED. REPAIRED PER MM 57-52-0 FIG 802, ON S/O A34369.Apr 14, 2000 · N509DA · Boeing 737232 · Trailing Edge FlapsSDR DL73K000705Skin · crackedTHE FUSELAGE SKIN ASSY BELOW THE L1 DOOR CUTOUT LOWER SILL NEAR THE AFT CORNER WAS FOUND WITH A 1 INCH CRACK. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE CRACK WAS ROUTED OUT AND REPAIRED WITH TWO REPAIR STRAPS ON A TIME-LIMITED BASIS PER THE S/B. THApr 13, 2000 · N311DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000706Skin · dentedTHE AFT EDGE OF THE CARGO DOOR CUTOUT WAS STRUCK BY GROUND EQUIPMENT BETWEEN STRINGERS 20R & 21R. THE DAMAGE WAS REMOVED WITH A 1 WIDE X 9 TALL CUTOUT IN THE SKIN ASSY AND BEARSTRAP. THE DAMAGE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS INApr 12, 2000 · N332DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000703Light · inoperativeDURING LAYOVER, FOUND L2 SLIDE LIGHT INOP. RELAMPED LIGHT, CHECKS GOOD PER MM.Apr 12, 2000 · N312DL · Boeing 737232 · Emergency LightingSDR DL73K000686Controller · malfunctionedON APPROACH WITH B A/P ENGAGED UPON DEPLOYMENT OF SPEEDBRAKES HAD UNCOMMANDED ROLL. REPLACED SPOILER MIXER PER M/M AND TESTED YAW DAMP SYSTEM AS PRECAUTION.Apr 9, 2000 · N321DL · Boeing 737232 · Drag Control SystemSDR DL73K000674Seat · crackedSEAT ROW 3 DEF LOOSE ON MOUNTS LIKE A ROCKING CHAIR. FOUND SEAT FRAME CRACKED. REPLACED SEAT ASSEMBLY.Apr 8, 2000 · N330DL · Boeing 737232 · Passenger Compartment EquipmentSDR DL73K000669Beam · crackedTHE WEB OF THE STR 18A SHEAR BEAM AT FS 727, RT WAS FOUND WITH A CRACK AT AN ATTACH FASTENER ON THE AFT END. THE CRACK IS TYPICAL OF CRACKS NOTED IN S/B 737-53-1066, THOUGH THE S/B IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK TERMINATED IN AN ADJACENT FASTEApr 5, 2000 · N324DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR DL72L000634Beam · crackedTHE RT VENTRAL STAIR TORQUE BOX WAS FOUND WITH TWO TYPICAL CRACKS IN THE UPPER HORIZONTAL BEAM MEMBERS AT FS 1263 AND FS 1273. THE CRACKS ARE TYPICAL OF S/B 727-53-0129. THE CRACKED MEMBERS WERE REMOVED AND REPLACED WITH NEW PARTS PER ER/A 369707-14AD.Apr 4, 2000 · N501DA · Boeing 737232 · Fuselage Miscellaneous StructureSDR DL73K000630Light · inoperativeEMERGENCY AISLE LIGHT INOP. REPLACED PWR SUPPLY M1135, OPS NORMAL.Apr 2, 2000 · N318DL · Boeing 737232 · Emergency LightingSDR DL73K000625Controller · malfunctionedON DESCENT INTO TPA PASSING THROUGH 15000 FT, RECEIVED A WHEEL WELL FIRE INDICATION. AFTER PERFORMING APPROPRIATE PROCEDURE WHEEL WELL FIRE LIGHT BECAME INTERMITTENT. T/S PER MM. UNABLE TO DUPLICATE DISCREPANCY. REPLACED COMP OVHT CONTROLLER MODUEL AS PApr 2, 2000 · N319DL · Boeing 737232 · Overheat DetectionSDR DL73K000618Bleed Valve · malfunctionedON TAKEOFF, RT BLD TRIPPED OFF AT 60 KTS, LEFT ONE OFF AT ROTATION. RESET BOTH AND BOTH TRIPPED OFF AGAIN. RETURNED TO MCO. REPLACED S21490 DEGREE SW ON RT ENG, REPLACED PRESS REG AND 13TH STAGE MOD VLV ON LT ENG. PERFORMED TEST PER PFHB AND RAN TO TAKEOFFApr 2, 2000 · N306DL · Boeing 737232 · Pneumatic Distribution System
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