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 DL73S952203Skin · delaminatedRUDDER DELAMINATED AT TOP LEFT SIDE T/E NEXT TO PREV REPAIR. ACCOMPLISHED REPAIRS PER SRM 51-40-9 FIG 1 AND ERA 301817-14.May 19, 1995 · N329DL · Boeing 737232 · Rudder, Plate/SkinSDR DL73S952122Control Panel · shortedON TAXI OUT, HAD SMOKE AND SPARKS COMING FROM CABIN LIGHT CONTROL PANEL AT FWD ENTRY DOOR. REPAIRED SHORTED WIRES, RETURNED TO SERVICE.May 13, 1995 · N327DL · Boeing 737232 · Passenger Compartment LightingSDR DL73S952021Skin · gougeFOUND SMALL .25 INCH BY .125 INCH GOUGE IN LOWER SKIN OF LEFT ELEV APPROX 6 INCHS FWD OF TAB. INSTALLED REPAIR PER SRM 55-20-03 FIG 01.May 10, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S952830Skin · delaminatedON INITIAL SHOP INSPECTION, 2 AREAS OF DELAMINATION WERE FOUND. THE FIRST AREA OF DAMAGE IS ON BOTTOM SKIN, APPROX 12 INCHES FROM I/B END. THE DAMAGED AREA IS DELAMINATED APPROX 8 INCH BY 2 INCH. THIS DAMAGE WAS REPAIRED IN ACCORDANCE WITH SRM 57-50-6 WITH May 9, 1995 · N303DL · Boeing 737232 · Aileron TabsSDR DL73S952116Skin · crackedLT ELEV TAB O/B HINGE UPPER AND LOWER SKIN CRACKED, COMPLIED WITH SRM 55-20-3.May 9, 1995 · N328DL · Boeing 737232 · Elevator, Tab StructureSDR DL73S952115Skin · crackedLT ELEV TAB CRACKED AT BOTH ENDS. BAL AFTER REPAIR. REPAIRED TAB PER ARM 55-20-01.May 8, 1995 · N328DL · Boeing 737232 · Elevator, Tab StructureSDR DL73S952455Skin · damagedDURING INITIAL SHOP INSPECTION, MAINTENANCE FOUND A ONE INCH HOLE IN UPPER IB SKIN, 10 INCHES FROM THE INBOARD END AND 2 INCHES FROM THE TRAILING EDGE. REPAIR WAS ACCOMPLISHED PER ERA 270848-14. ALSO, A 4 INCH DELAMINATED AREA WAS FOUND 14 INCHES FROM INBOARMay 2, 1995 · N328DL · Boeing 737232 · Elevator, Tab StructureSDR DL73S951971Le Skin · dentedDURING SHOP INSPECTION, VERTICAL STABILIZER LEADING EDGE PANEL WAS REPAIRED FOR A DENT AT 51 INCHES FROM THE LOWER END OF PANEL. DAMAGE WAS REPAIRED PER SRM 55-30-6.May 1, 1995 · N316DL · Boeing 737232 · Vertical Stabilizer, Plate/SkinSDR DL73S951950Skin · damageFOUND DURING INSP DFW, RT ELEVATOR DAMAGED JUST OUTBD OF TRIM TAB APPROXIMATE STATION 121.59, APPROX 3.0 INCHES FROM TRAILING EDGE 1.5 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951949Skin · damagedFOUND DURING INSP DFW, RT ELEVATOR DAMAGED INBD OF STA 149.12, 15.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951948Elevator · damagedFOUND DURING INSP DFW, RT ELEVATOR DAMAGED OUTBD OF STA 39.02 APPROXIMATELY 20.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3 INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951947Skin · damagedFOUND DURING INSP DFW, RT ELEVATOR DAMAGED OUTBD OF STA 66.54 APPROX 15.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951946Skin · damagedFOUND DURING INSP DFW, RT ELEVATOR DAMAGED INDB OF STA 66.54 APPROX 10.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951945Skin · damagedFOUND DURING INSP DFW, LT ELEVATOR DAMAGE OUTBOARD OF STA 176.64, 6 INCHES FROM TRAILING EDGE 1.25 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951944Skin · damagedFOUND DURING INSP DFW, LT ELEVATOR DAMAGE BETWEEN STA 176.64 AND 149.12, 13 INCHES FROM TRAILING EDGE 2 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951943Skin · damagedFOUND DURING INSP DFW, LT ELEVATOR DAMAGE BETWEEN STA 149.12 AND 121.59, 12 INCHES FROM TRAILING EDGE 2.5 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951942Skin · damagedFOUND DURING INSP DFW, LT ELEVATOR DAMAGED BETWEEN STA 94.27 AND 66.54, 15 INCHES FROM TRAILING EDGE 2.5 INCH DAMAGE STARTED REPAIR PER SRM 55-20-3. REPAIRED ELEV PER SRM 55-20-3. INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301711-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951941Skin · damagedFOUND ON INSP DFW, LT ELEVATOR DAMAGE JUST OUTBOARD OF STA 3902, 4 INCHES FROM TRAILING EDGE 1 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301771-14.Apr 30, 1995 · N328DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S951842Flap Skin · damagedDURING SHOP INSP, RT WING NR 4 AFT FLAP WAS FOUND WITH A TIME LIMITED REPAIR 10 INCHES FROM THE IN/B END ON THE L/E OF FLAP. INSTALLED PERMANENT REPAIR PER SRM 57-50-4 FIG 5.Apr 24, 1995 · N332DL · Boeing 737232 · Trailing Edge FlapsSDR DL73S952137Te Wedge · delaminatedDURING SHOP INSPECTION, NR 4 AFT FLAP T/E WEDGE WAS FOUND DELAMINATED 10 FROM THE INBD END OF FLAP. REPAIRED PER SRM 51-70-10.Apr 22, 1995 · N332DL · Boeing 737232 · Trailing Edge FlapsSDR DL73S952136Te Wedge · damagedDURING SHOP INSPECTION, NR 4 AFT FLAP WAS FOUND WITH T/E WEDGE WITH DAMAGE TO O/B AFT CORNER. REPAIRED PER SRM 57-53-01.Apr 22, 1995 · N332DL · Boeing 737232 · Trailing Edge FlapsSDR DL73S952135Le Skin · damagedDURING SHOP INSPECTION, NR 4 AFT FLAP WAS FOUND WITH TIME LIMITED REPAIR ON L/E AT 16 FROM THE I/B END OF FLAP. REPAIRED PER SRM 57-50-4 FIG 5.Apr 22, 1995 · N332DL · Boeing 737232 · Trailing Edge FlapsSDR DL73S951641Computer · failedON CLIMBOUT HAD ELEV, FEEL DIFF. PRESSURE LITE ON. RETURNED DFW, REPLACED FEEL COMPUTER, FOR RETURN TO SERVICE.Apr 19, 1995 · N332DL · Boeing 737232 · Elevator Control SystemSDR DL73S951251Vane · crackedDURING INSPECTION, RT WING NR 3 FLAP VANE WAS FOUND WITH CRACKED UPPER SKIN. REPAIRED PER SRM 57-53-00 FIG 806.Mar 24, 1995 · N311DL · Boeing 737232 · Trailing Edge FlapsSDR DL73S951630Nose Cowl · damagedDURING SHOP INSPECTION, A DEEP NICK WAS FOUND IN THE LEADING EDGE LIP OF NR 2 ENGINE NOSE COWL. REPAIRED PER SRM 54-30-3 FIG. 4.Mar 17, 1995 · N314DA · Boeing 737232 · Engine Cowling SystemSDR DL73S951629Nose Cowl · crackedDURING SHOP INSPECTION, A .5 INCH CRACK WAS FOUND IN THE LEADING EDGE LIP OF NR 2 NOSE COWL. REPAIRED PER SRM 54-30-3 FIG. 4.Mar 17, 1995 · N314DA · Boeing 737232 · Engine Cowling SystemSDR DL73S951091Windshield · failedDURING CRUISE, HEARD BURNING NOISE AND HAS ACRID SMELL IN FLT DECK, THEN HAD SMOKE AT R-1 WINDOW TERMINAL BLOCK, LANDED BNA, FOUND R-1 WINDOW TERMINAL BURNED. RELACED R-1 WINDOW, CONTROLLER AND CIRCUIT BREAKER. OPERATION NORMAL.Mar 13, 1995 · N332DL · Boeing 737232 · Flight Compartment WindowsSDR DL73S951104Web · crackedDURING INSPECTION, A 6 INCH CRACK WAS FOUND AT THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL AT STATION 270. IN ACCORDANCE WITH S/B 727-53-145, THE WEB WAS TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED.Mar 12, 1995 · N311DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR DL73S951035Coffee Maker · failedDURING CLIMB-OUT, HAD SMOKE AND FUMES COMING FROM FORWARD GALLEY. ALSO, WATER LEAKING AT COFFEE MAKER. DEACTIVATED POWER AND RETURNED ICT. FOUND COFFEE MAKER DRAIN VALVE STUCK OPEN. REPLACED MAKER OPERATION NORMAL.Mar 9, 1995 · N313DL · Boeing 737232 · Buffet/GalleysSDR DL73S950870Engine · failedAFTER TAKOFF, RDU NR 1 ENGINE FLAMED-OUT AT TOP OF CLIMB. OFF LANDED GSO. FOUND METAL ON CHIP DETECTOR AND OIL SCREEN, N1 FAN BINDING AND UNABLE TO TURN N2. REPLACED ENGINE AND ROUTED TO SHOP FOR REPAIRS (SUPPLEMENT 5-18-95). UPON DISASSEMBLY IN SHOP, FOUFeb 26, 1995 · N303DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR DL73S951109Skin · corrodedDURING HMV INSPECTION, THE SKIN AT STA 480 WAS FOUND CORRODED IN TWO LOCATIONS BETWEEN STR 26R-28R. THE DAMAGE CONSISTED OF A 1.125 INCH CUTOUT NEAR STR 27R AND A 3.25 INCH BY 2.5 INCH CUTOUT AT THE STA 480 BUTT SPLICE. IN ACCORDANCE WITH B727 SRM 53-30-3, FFeb 22, 1995 · N310DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S950846Floor Beam · crackedTHE BL 0.07 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT STATION 663. THE UPPER CAP OF THE BEAM IS CRACKED ON THE RIGHT HAND FLANGE ONLY, STARTING FROM AN EXISTING FASTENER HOLE. NO CRACKS WERE FOUND ON THE WEB. THE PANEL ATTACH HOLE WAS ALSO FOUND CFeb 20, 1995 · N322DL · Boeing 737232 · Fuselage Main, Floor BeamSDR DL73S950757Valve · leakingON TAXI OUT LOST ALL HYDRAULIC FLUID. FOUND BRAKE SHUTTLE VALVE LEAKING. REPLACED VALVE, OPERATION NORMAL.Feb 19, 1995 · N310DA · Boeing 737232 · Landing Gear Brake SystemSDR DL73S950555Cowl · dentedDURING A ROUTINE INSPECTION A 3 INCH BY 4 INCH DENT WAS FOUND ON THE NR 1 ENGINE SIDE COWL NEXT TO THE OIL ACCESS DOOR. THE DENT WAS CUT OUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER SRM 54-10-3. THE AUTHORITY USED TO REPLACE THE FLUSH REPAIR WITH AN EXTERNAFeb 8, 1995 · N328DL · Boeing 737232 · Engine Cowling SystemSDR DL73S950642Skin · crackedDURING LETTER CHECK, THE R-1 DOORWAY FRAME WAS FOUND CRACKED AT LOWER AFT CORNER APPROXIMATELY 1.75 INCH. THE CRACK ENDS IN A NUTPLATE HOLE. REPAIRED PER ERA, 301125-14.Feb 4, 1995 · N309DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR DL73S950489Air Data Comp · failedDURING CLIMB-OUT AT 10,000 FT, 32 AIR DATA COMPUTER FAILED. RETURNED ATL. REPLACED ADC OPERATION NORMAL.Feb 1, 1995 · N315DL · Boeing 737232 · Air Data ComputerSDR DL73S950481Floor Beam · crackedDURING ROUTINE INSPECTION, THE BL 0.07 FLOORBEAM OF THE WING CENTER SECTION WAS FOUND CRACKED AT STA 657. THE UPPER CAP WAS COMPLETELY CRACKED, BUT NO CRACKS WERE FOUND IN THE WEB. PER B737 S/B 737-57-1210, THE CAP WILL BE REPAIRED.Feb 1, 1995 · N319DL · Boeing 737232 · Fuselage Main, Floor BeamSDR DL73S950440Skin · puncturedDURING LETTER CHECK M-1, FOUND RT ELEVATOR HAS A HOLE IN LOWER SURFACE. REPAIRED AS PER SRM 51-40-13.Jan 30, 1995 · N325DL · Boeing 737232 · Elevator, Plate/SkinSDR DL73S950439Aft Clevis · crackedDURING LETTER CHECK M-1, FOUND L1 DOOR UPPER GATE AFT CLEVIS CRACKED. MANUFACTURED AND INSTALLED NEW ANGLE PER ERA 274058-14, REF SRM 52-10-2.Jan 30, 1995 · N325DL · Boeing 737232 · Passenger/Crew DoorsSDR DL73S950425Eel · inoperativeDURING SERVICE CHECK, THE R-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOP. REPLACED REFLECTOR AND BULB OPERATION NORMAL.Jan 30, 1995 · N318DL · Boeing 737232 · Emergency LightingSDR DL73S950844Floorbeam · crackedTHE BL 0.07 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT STA 663, AND THE UPPER CAP OF THE BEAM IS COMPLETELY CRACKED. THE WEB AND WEB DOUBLER ARE CRACKED APPROXIMATELY 4 INCHES AT THE SAME LOCATION. THE CRACKS ARE TYPICAL PER BOEING SERVICE BULLETIN RJan 26, 1995 · N312DL · Boeing 737232 · Fuselage Main, Floor BeamSDR DL73S950386Skin · lightning strikeFOUND DURING LETTER CHECK, L2 LIGHTNING STRIKES ON LEFT FWD FUSELAGE BETWEEN STA 211 TO 259. BLENDED AREAS PER SRM 53-30-3. DYE CHECK OK, TREATED AREA PER SRM 53-30-3Jan 26, 1995 · N328DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S950385Door · crackedFOUND DURING LETTER CHECK, L2 MLG INNER DOOR CRACKED AT T/E. REPAIRED PER SRM 51-40-13.Jan 26, 1995 · N328DL · Boeing 737232 · Landing Gear DoorsSDR DL73S950384Skin · puncturedFOUND DURING LETTER CHECK, L2 SMALL HOLE IN RUDDER. APPROXIMATELY .5 INCHES DIAMETER, 7 FEET FROM TOP OF RUDDER, AND APPROXIMATELY 7 INCHES AFT OF HINGE LINE. REPAIRED PER SRM 55-40-5.Jan 26, 1995 · N328DL · Boeing 737232 · Rudder, Plate/SkinSDR DL73S950373Duct · crackedDURING CLIMB-OUT, HAD NR 1 ENGINE OVERHEAT LIGHT. RETURNED SLC, AND FOUND CRACKED BLEED DUCT. REPLACED DUCT, OPERATION NORMAL.Jan 26, 1995 · N324DL · Boeing 737232 · Pneumatic Distribution SystemSDR DL73S950395Skin · damagedDURING SHOP INSPECTION, FOUND LEFT ELEVATOR TAB WITH DAMAGE TO COMPOSITE SKIN AT TAB HINGE CUTOUTS. REPAIRED PER SRM 55-20-1.Jan 21, 1995 · N327DL · Boeing 737232 · Elevator, Tab StructureSDR DL73S953104Skin · damagedDURING LAYOVER IN ATLANTA, THE FUSELAGE SKIN WAS DAMAGED JUST AFT OF STATION 360 AND JUST ABOVE STRINGER 19R WHEN STRUCK BY A BAGGAGE CONTAINER. DAMAGE WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER IN ACCORDANCE WITH B737-200 SRM 53-30-3 FIG 1 PER ER/A 30Jan 19, 1995 · N302DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S950279Psu · faultyAFTER TAKEOFF FLIGHT ATTENDANTS REPORTED STRONG BURING ODOR IN MID CABIN AND AFT. NO SMOKE OR FIRE NOTED. RETURNED HSV. TRACED SOURCE OF ODOR TO PSU AT ROW 17ABC. REPLACED PSU OPERATION NORMAL.Jan 18, 1995 · N324DL · Boeing 737232 · Passenger Compartment EquipmentSDR DL73S950260Dome · dislodgedON TAKEOFF NR 1 ENGINE HAD COMPRESSOR STALL, ABORTED TAKOFF. UPON RETURNING TO GATE FOUND INTAKE DOME ASSEMBLY DISLODGED, WITH DAMAGE TO N-1 ACCESSORY GEARCASE, AND 5 FAN BLADES. SUSPECT CAUSE OF COMPRESSOR STALL WAS WHEN THE DOME ASSEMBLY MOUNT FAILED AND Jan 17, 1995 · N320DL · Boeing 737232 · Turbine Engine Air Inlet SectionSDR DL73S950161Eel Rack · failedDURING INSPECTION, FOUND AFT CABIN FLOOR EMERGENCY TRACK LIGHTS INOP. REPLACED RACK M9222, OPERATION NORMAL.Jan 13, 1995 · N311DL · Boeing 737232 · Emergency Lighting
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