Douglas DC-9-32

Service difficulty reports · 12,755

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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 = 'DC932'
  ORDER BY difficulty_date DESC"

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SDR MWEA96473Door Frame · crackedDURING INSP, VENTRAL DOOR JAMB FRAME IS CRACKED AT UPPER RT STRIKER PLATE FOR DOOR STOP. REPLACED DOOR JAMB FRAME IAW SRM 51-30-2.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96472Jamb · crackedDURING INSP, VENTRAL DOOR JAMB PAN WAS CRACKED IN UPPER LT CORNER AND LWR FWD EDGE WAS EXFOLIATED. REPLACED DOOR PAN IAW SRM 51-30-2.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96471Door Pan · crackedDURING INSP, AFT CABIN DOOR PAN ON LT SIDE WAS FOUND CRACKED AT BEAM NR 2. ALSO, SUPPORT ANGLE WAS CRACKED. REPAIRED THE PAN IAW DAC TELEX MSP-SVC-643/DAI DATED 2 AUG 96. ANGLE INSTALLED IAW SRM 51-30-5.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA96470Lav Service Pnl · crackedDURING INSP, THE LAV SERVICE PANEL PAN WAS FOUND CRACKED AT THE RT DRAIN HANDLE BOSS. REPAIRED CRACK IAW SRM 53-01 FIG 2, SHEET 3.Sep 12, 1996 · N209ME · Doug DC932 · Water and Waste SystemSDR MWEA96469Clips · corrodedDURING INSP, LONG 20 AND 21L HAD CORROSION AT STA 992 AND AT SHOVEL CLIPS. REPLACED CLIPS AND LONGERON IAW SRM 53-11-3.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96468Longeron · corrodedDURING INSP, LONGERON 20 AND 21R WERE FOUND CORRODED AT STA 965 TO 996 AND 970. REPLACED LONGERONS IAW SRM 53-11-3.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA96467Frame · corrodedDURING INSP, LIGHT CORROSION WAS FOUND ON FRAME AFT SIDE AFT CARGO COMPT FROM LONG 24R TO 29R. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-03, PAGE 4A FIG 2A.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Main, FrameSDR MWEA96466Clip · corrodedDURING INSP, EXFOLIATION CORROSION FOUND ON INTERCOSTAL ATTACH CLIP AFT CARGO COMPT STA 965, LONG 29R. INSTALLED A FABRICATED ATTACH CLIP IAW SRM 51-30-5.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96465Panel · corrodedDURING INSP, LT WHEEL WELL SLANT PRESSURE PANEL WAS FOUND TO HAVE MODERATE CORROSION AROUND A BOTTOM ROW FASTENER AND WIRE BUNDLE ATTACH CLIP. FABRICATED A NEW PANEL AND CLIP, INSTALLED IAW SRM 53-11-3, FIG 12.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96464Angle · damagedDURING INSP, FLOOR BEAMS AT STA 389 AND 408 LOWER FLANGE WERE DAMAGED FROM FWD CARGO DOOR HITTING THEM. FABRICATED PARTS FOR REPAIRS AND INSTALLED IAW SRM 53-05 FIG 86, SHEET 2.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96463Former · crackedDURING INSP, TWO FORMERS FOUND CRACKED IN WING CENTER SECTION AREA LT AND RT OUTBD END AT STA 660. FABRICATED TWO NEW PARTS, HEAT TREATED AND INSTALLED IAW 53-03 PG 31, FIG 12.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96462Hinge · wornDURING INSP, LT MAIN GEAR DOOR ATTACH HINGE WAS FOUND TO HAVE EXCESSIVE PLAY AND CRACKED LOBE. REPLACED HINGE IAW SRM 52-05, FIG 15.Sep 12, 1996 · N209ME · Doug DC932 · Landing Gear DoorsSDR MWEA96461Doublers · not installedDURING INSP, STRUCTURAL HARD POINTS TO BE INSTALLED IN FWD BAG PIT PER DAC DRAWING NR 5911412 AT BELLY STATIONS 396, 339, 453 AND 510. INSTALLED ALL FOUR ANTENNA ATTACH DOUBLERS IAW DAC DWG 5911412.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96460Floor Beam · corrodedDURING INSPECTION, TWO SMALL SPOTS OF EXFOLIATION CORROSION WERE FOUND ON THE UPPER FLANGE OF CABIN FLOOR BEAM AT STA 389. REPAIRED FLOOR BEAM IAW SRM 53-05.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA96459Clip · hole in radiusDURING INSPECTION, AN ATTACH CLIP HAD A HOLE IN RADIUS IN FORWARD CARGO PIT FORWARD DOOR JAMB INTERCOSTAL AT STA 380. FABRICATED A NEW CLIP AND INSTALLED IAW SRM 53-01.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96458Skin · tornDURING INSPECTION, VENTRAL STAIR EXTERNAL SKIN WAS FOUND TORN AT THE TOE PLATE. COMPLETED A REPAIR IAW SRM 52--01, FIG. 2, SHEET 3.Sep 12, 1996 · N209ME · Doug DC932 · Entrance StairsSDR MWEA96457Skin · chafedDURING INSPECTION, THE PYLON LEADING EDGE WAS FOUND CHAFED INTO THE FUSELAGE SKIN. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM'S 51-10-3, 51-30-2, 53-04, FIG. 3A, SHEET 1, PG 6A.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA96456Center Hinge · crackedDURING INSPECTION, VERTICAL STAB REAR SPAR CENTER HINGE FOR THE RUDDER FOUND CORRODED ON RT ATTACH LEG. REMOVED THE HINGE AND FOUND CORRODED LEG CRACKED. REPLACED HINGE IAW DAC MM 20-16-0, PG. 209, FIG. 205.Sep 12, 1996 · N209ME · Doug DC932 · Vertical StabilizerSDR MWEA96455Doubler · corrodedDURING INSPECTION, A DOUBLER PLATE UNDER THE TOP STEP OF THE VENTRAL STAIR DOOR WAS FOUND EXFOLIATED. FABRICATED A NEW ANGLE AND INSTALLED IAW SRM 52-01.Sep 12, 1996 · N209ME · Doug DC932 · Entrance StairsSDR MWEA96454Angle · corrodedDURING INSPECTION, AN ANGLE AT STA 1089 (CANTED FRAME) WAS FOUND EXFOLIATED ON AFT SIDE AT LONGERON 12L. MANUFACTURED AND INSTALLED A NEW ANGLE IAW DC9 SRM 53-11-4.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96453Spar Cap · crackedDURING INSPECTION, A .3750 INCH CRACK WAS FOUND IN THE ELEVATOR UPPER SPAR CAP AT STA XE68 AND A .75 INCH CRACK AT STA XE 121. REPAIRED IAW SRM 55-02, FIG. 9, CONFIGURATION -501.Sep 12, 1996 · N209ME · Doug DC932 · Elevator, Spar/RibSDR MWEA96452Spar Cap · crackedDURING INSPECTION, A 1 INCH CRACK WAS FOUND IN RT ELEVATOR LOWER SPAR CAP AT STA XE25 AND A .75 INCH CRACK ON UPPER SPAR CAP AT XE25. COMPLETED REPAIR PER DAC TELEX SVC-MSP-0677/RMK DATED 11 AUG 96.Sep 12, 1996 · N209ME · Doug DC932 · Elevator, Spar/RibSDR MWEA96451Fitting · crackedDURING INSPECTION, RT FLAP CENTER HINGE MOUNT INBD CASTING WAS FOUND CRACKED IN TWO PLACES ALONG THE BOTTOM FLANGE. REPLACED RT FLAP CENTER HINGE FITTING IAW SRM 57-09, PARA 13, AND DAC DRAWING 5914508.Sep 12, 1996 · N209ME · Doug DC932 · Trailing Edge FlapsSDR MWEA96450Doubler · crackedDURING INSPECTION, THE MLG INBD DOOR OUTER SKIN WAS FOUND CRACKED AT FORWARD EDGE NEAR THE OTBD END, APPROX 1.50 INCHES. FABRICATED AND INSTALLED REPAIR IAW SRM 52-05, FIG. 4, PG 5, AND 51-30.Sep 12, 1996 · N209ME · Doug DC932 · Landing Gear DoorsSDR MWEA96449Support Beam · crackedDURING INSPECTION, RT WING INBD SPOILER TORSION BAR BEARING UPPER SUPPORT BEAM IS CRACKED AT LOWER END. INSTALLED A NEW SUPPORT BEAM IAW SRM 57-01, PG 1.Sep 12, 1996 · N209ME · Doug DC932 · SpoilersSDR MWEA96448Spar Cap · corrodedDURING INSPECTION, LT REAR SPAR CAP LOWER HORIZONTAL LEG WAS FOUND TO HAVE SEVERE EXFOLIATION CORROSION. COMPLETED REPAIR IAW SRM 57-09, FIG. 11.Sep 12, 1996 · N209ME · Doug DC932 · Wing SparSDR MWEA96447Fitting · crackedDURING INSPECTION, LT FLAP CENTER HINGE MOUNT INBD FITTING WAS FOUND CRACKED. REPLACED FITTING IAW SRM 57-09, PARA 13, AND DRWG NR 5914508.Sep 12, 1996 · N209ME · Doug DC932 · Trailing Edge FlapsSDR MWEA96446Doubler · scratchedDURING INSPECTION, LT WING OTBD SPOILER PANEL WAS FOUND TO HAVE A DEEP SCRATCH ON LOWER SURFACE. COMPLETED A REPAIR IAW SRM 51-70-2, PG. 83, PARA C.Sep 12, 1996 · N209ME · Doug DC932 · SpoilersSDR MWEA96445Floor Beam · corrodedDURING INSPECTION, EXFOLIATION CORROSION WAS FOUND ON A FLOOR BEAM UPPER FLANGE LOWER SURFACE INBD OF SEAT TRACK NR 1 AT STA 218. REPAIRED THE FLOOR BEAM IAW SRM 53-05, FIG. 20A.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA96444Seat Track · corrodedDURING INSPECTION, SEAT TRACKS NR 2 AND NR 3 WERE FOUND TO HAVE CORROSION FROM STA 180 TO STA 229. REPAIRED THE SEAT TRACKS IAW SRM 53-05, FIG. 4D.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA96443Longeron · exfoliatedDURING INSPECTION, LONGERON 30 WAS FOUND EXFOLIATED IN E/E COMPT AT STA 180. MAINTENANCE SPLICED IN A NEW SECTION OF LONGERON IAW SRM 53-02, FIG. 2.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA96442Angle · brokenDURING INSPECTION, RADAR RT RACK INBD AFT MOUNT BRACKET BROKEN. FABRICATED REPAIR ANGLES IAW SRM 53-01, FIG. 2, SHEET 4, AND INSTALLED IAW SRM 51-30-2.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96441Blkhd Fitting · corrodedDURING INSPECTION, FOUND CABLE ATTACH FITTING EXFOLIATED IN NLG WHEELWELL ON UPPER PRESSURE BULKHEAD. FABRICATED A FITTING AND INSTALLED IAW SRM 51-30-5.Sep 12, 1996 · N209ME · Doug DC932 · Fuselage Main, BulkheadSDR GTIA96NK199Pressure System · failedAIRCRAFT LOG PAGE NR 028813, ITEM NR P744 - PRESSURIZATION FAILED ON TAKEOFF OUT OF ACY. RETURNED ON TAKEOFF, OUT OF ACY. RETURNED FOR MAINTENANCE INSPECTION. DEFERRED PRESSURIZATION IAW MEL 21-24, DMI NR 2595. (M)Sep 12, 1996 · N12505 · Doug DC932 · Cabin Pressure Control SystemSDR 96520Slide · fell offCREW REPORTS FWD ENTRY DOOR EVACUATION SLIDE FELL OFF. MAINTENANCE REINSTALLED FWD ENTRY DOOR EVACUATION SLIDE.Sep 12, 1996 · N207ME · Doug DC932 · Emergency EquipmentSDR 9619769613Circuit Breaker · malfunctionedDURING FLIGHT, EMERGENCY LIGHTS IN MAIN CABIN REMAINED ON WHILE SWITCH WAS IN ARMED POSITION. REPLACED B1-41 CIRCUIT BREAKER 061641, OPERATIONAL CHECK NORMAL.Sep 12, 1996 · N613NW · Doug DC932 · Emergency LightingSDR MWEA96518Striker Plate · out of adjustPILOT REPORTS AFT CARGO DOOR LIGHT ON ANNUNCIATOR PANEL ILLUMINATED DURING TAKEOFF. ABORTED TAKEOFF, RETURNED TO GATE. MTCE CHECKED DOOR SECURITY AND DEFERRED SYSTEM FOR FLT TO MKE. IN MKE RESHIMMED LIGHT STRIKER PLATE, OPS CHECK GOOD.Sep 11, 1996 · N502ME · Doug DC932 · Door Warning SystemSDR MWEA96440Light · inoperativeDURING SERVICE CHECK, FOUND FORWARD ENTRY EMERGENCY LIGHT DOES NOT ILLUMINATE DURING TEST. REPLACED FORWARD ENTRY EMERGENCY LIGHT ASSY. OPS CHECK GOOD.Sep 11, 1996 · N301ME · Doug DC932 · Emergency LightingSDR ABXA9700656Beam · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND TOP HORIZONTAL BEAM CRACKED ON SERVICE DOOR. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.Sep 11, 1996 · N902AX · Doug DC932 · Service DoorsSDR ABXA9700655Longeron · damagedDURING C-CHECK AND COMPLIANCE WITH AD 96-07-51, FOUND LONGERON 2L DAMAGED AT STA 256. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2.Sep 11, 1996 · N902AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9619759991Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS VERY DIM. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Sep 11, 1996 · N8957E · Doug DC932 · Emergency LightingSDR MWEA96517Switch · out of adjustPILOT REPORTS SPOILER DEPLOYED LIGHT ON ANNUNCIATOR PANEL ILLUMINATED DURING TAKEOFF ROLL. RETURNED TO GATE. ADJUSTED LT OUTBD SPOILER PANEL SWITCH IAW ME EO 1-27-014R2, OPS CHECK GOOD.Sep 10, 1996 · N401ME · Doug DC932 · Drag Control SystemSDR CALA9601298Relay · crackedTHE AIRCRAFT HAD A HISTORY OF THE GPWS GIVING A TOO LOW GEAR WARNING AT LOW ALTITUDES DURING LANDING, WHICH RESULTED IN TWO INSTANCES OF A GO-AROUND. THE WARNING WAS ACCOMPANIED BY DIM LOWER HALF OF GREEN DOWN AND LOCKED LIGHTS. TROUBLESHOOTING BY MAINTENANCSep 10, 1996 · N43537 · Doug DC932 · Ground Proximity SystemSDR ABXA9701007Tab · crackedFOUND RUDDER TAB TRAILING EDGE CRACKED AND DENTED. REPAIRED TRAILING EDGE SKINS PER DC9 SRM 51-70-2.Sep 10, 1996 · N902AX · Doug DC932 · Rudder, Tab StructureSDR ABXA9700928Beam · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SECOND FROM TOP HORIZONTAL BEAM CRACKED ON SERVICE DOOR. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.Sep 10, 1996 · N902AX · Doug DC932 · Service DoorsSDR 9619699613Switch · malfunctionedDURING FLIGHT, THE FLOOR PROXIMITY EMERGENCY LIGHTS IN MAIN CABIN FLICKERED ON AND OFF. REPLACED FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH. OPERATIONAL CHECK OK.Sep 10, 1996 · N613NW · Doug DC932 · Emergency LightingSDR ABXA9700475Vortilon · dentedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING VORTILON LEADING EDGE WITH PIN HOLES AND DENTS. REPAIRED IAW ABX REA 953-16330.Sep 9, 1996 · N902AX · Doug DC932 · Wing Miscellaneous StructureSDR 9619519604Actuator · looseVIBRATION FROM NOSE GEAR AREA OCCURRED ON GEAR RETRACTION AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT NOSE GEAR DOOR OPEN AND ACTUATOR LOOSE. REPLACED ACTUATOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO Sep 9, 1996 · N604NC · Doug DC932 · Landing Gear Door ActuatorSDR MWEA96434Power Supply · inoperativeDURING C-CHECK, FOUND EMERGENCY OVERHEAD LIGHT IN AFT ACCESSORY COMPARTMENT VERY DIM. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.Sep 7, 1996 · N502ME · Doug DC932 · Emergency LightingSDR MWEA96433Beam · crackedDURING C-CK, FOUND AFT ENTRANCE DOOR HAS CRACK AT LOWER LEFT BEAM END AND AT RADIUS OF UPPER BEAM NEAR HINGE POINT. MAINT INSTALLED DOUBLER REPAIR ON UPPER BEAM IAW SRM 52-05 PG 201 FIG 34. REMOVED AND REPLACED LOWER BEAM IAW SRM 51-30.Sep 7, 1996 · N502ME · Doug DC932 · Passenger/Crew Doors
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