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 GTIA9700202Mount · damagedYIP - LEFT NACELLE, ENGINE MOUNT: UPPER AFT VIBRATION ABSORBER ASSY LOOSE, STEM BENT. ALSO, SUSPECT THREADS DAMAGED. REMOVED AND REPLACED ABSORBER IAW DC-9 MM 71-20-3. THREADS IN PYLON YOKE ATTACH BOLT GOOD. (X)Feb 23, 1997 · N947ML · Doug DC932 · Engine Mount SectionSDR GTIA9700190Oxygen Line · leakingYIP - DURING FUNCTIONAL CHECK OF OXYGEN MASK DEPLOYMENT TEST, FOUND DEFECTIVE LEAKING LINE AT SUPPLY MANIFOLD (L13 OVERHEAD PANEL LOCATION). REQUIRES LEAK CHECK. SERVICEABLE LINE INSTALLED IAW DC-9 MM 35-20-2. NO LEAKS NOTED. (X)Feb 23, 1997 · N947ML · Doug DC932 · Passenger Oxygen SystemSDR CALA9700281Longeron · crackedINSPECTION FOUND LONGERON 7L CRACKED IN TWO PLACES AT STA 980. TOTAL LENGTH OF CRACKS WAS 3.25 INCHES. THE CRACKED SECTION OF LONGERON WAS REMOVED. A REPLACEMENT SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-5.Feb 23, 1997 · N12508 · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ970129Wire · failedAT SERVICE CHECK, FORWARD SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. REPAIRED BROKEN WIRE BETWEEN POWER SUPPLY AND LIGHT SECTION. REPAIR EFFECTED BY USING BUTT SPLICE IAW MM AND STANDARD MAINTENANCE PRACTICE (SMP). OPS CHECKED GOOD. (M)Feb 22, 1997 · N935VV · Doug DC932 · Light System WiringSDR MWEA97113Evac Slide · fell offCREW REPORTS, FWD ENTRY DOOR EVAC SLIDE FELL OFF DOOR. MAINTENANCE REINSTALLED EVAC SLIDE, RETURNED A/C TO SERVICE.Feb 22, 1997 · N302ME · Doug DC932 · Emergency EquipmentSDR VJ970128Indicator · shortedEN ROUTE ATL-VPS, FLT 147, LEFT MAIN LANDING GEAR 'GREEN' LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GROUND CHECKED NORMAL WITH GEAR HANDLE DOWN AND GEAR PINNED. TROUBLE SHOT SYSTEM PER WD32-61-00 AND REPLACED LEFT MLG DOWN GREEN LIGHT ASSEMBLY. ALL Feb 21, 1997 · N922VV · Doug DC932 · Landing Gear Position and WarningSDR GTIA9700189Splice · crackedYIP - FORWARD BELLY COMPARTMENT, NR 22 LONGERON CORRODED AND SPLICE PLATE CRACKED AT FS 229. REPAIRED LONGERON AT FS 229 PER DC-9 SRM 53-02. (X)Feb 21, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9700497Intercostal · crackedDURING C-INSPECTION, FOUND THE INTERCOSTAL BETWEEN FS 699 RIGHT AND 718 RIGHT CRACKED IN UPPER FORWARD CORNER. REPAIRED INTERCOSTAL IAW DC9 SUPPLEMENTAL SRM DRAWING K 05159 AND SRM CHAPTERS 51-30-2 AND 51-30-5.Feb 21, 1997 · N985AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9700495Frame · corrodedDURING C-INSPECTION, FOUND THE FUSELAGE FRAME AT FS 945 CORRODED FROM LONGERON 24 LEFT TO LONGERON 30. REPLACED ANGLE IAW DC9 51-10-3 AND 51-30-2.Feb 21, 1997 · N985AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9700487Bracket · corrodedDURING C-INSPECTION, FOUND UPPER RUDDER HINGE BRACKET CORRODED AT THE RIGHT AND LEFT ATTACH BOLTS. REPLACED RUDDER HINGE BRACKET IAW DC9 MAINTANCE MANUAL CHAPTERS 55-50-0 AND 20-16-0.Feb 21, 1997 · N985AX · Doug DC932 · Vertical StabilizerSDR ABXA00441Skin · dentedLEFT WING SPOILER HAS LARGE DENTS. REPLACED CORE, STIFFENERS AND SKIN PER SRM.Feb 21, 1997 · N985AX · Doug DC932 · SpoilersSDR VJ970127Dorsal Fin · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, TWO L-ANGLES CRACKED IN SIDE DORSAL FIN AT STATION 1074 BOTH APPROXIMATELY 1 INCH IN LENGTH. REMOVED CRACKED L-ANGLES FROM INTERIOR OF DORSAL FIN FS 1074, FABRICATED AND REPFeb 20, 1997 · N919VV · Doug DC932 · Vertical StabilizerSDR VJ970126Longeron · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, LONGERON 2 RIGHT STATION 1080 CRACKED AFT END, APPROXIMATELY 2 INCHES IN LENGTH. REMOVED CRACKED LONGERON 2R FS 1080, CUT AND TRIMMED NEW LONGERON, FABRICATED LONGERON SPLICFeb 20, 1997 · N919VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ970125Longeron · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, LONGERON 2 LEFT STATION 1080 CRACKED AFT END APPROXIMATELY 2 INCHES LONG. REMOVED CRACKED LONGERON 2L FS 1080, CUT AND TRIMMED NEW LONGERONS, FABRICATED LONGERON SPLICE, DOUFeb 20, 1997 · N919VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA9700224Control Cable · frayedYIP - LEFT WING - AILERON CABLE FRAYED NEAR FAIR LEAD AT APPROXIMATELY STA XRS 353. MANUFACTURED AND INSTALLED CABLE, TENSIONED AND SAFTIED IAW DC-9 MM CHAPTER 27-10-0 PAGES 9 AND 10, AND CABLE TENSION CHART. (X)Feb 20, 1997 · N947ML · Doug DC932 · Aileron Control SystemSDR ABXA9701117Vane · delaminatedRIGHT MIDDLE FIXED VANE DELAMINATED. REPLACED SKIN HONEYCOMB CORE AND INTERNAL DOUBLERS IAW DC9 SRM.Feb 20, 1997 · N985AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9700502Rib · crackedDURING C-INSPECTION, FOUND THE LEFT WING LEADING EDGE RIB IS CRACKED JUST OUTBOARD OF THE NR 11 SLAT TRACK. REPLACED LEFT WING LEADING EDGE RIB IAW DC9 SRM CHAPTERS 51-30-2 AND 51-30-55.Feb 20, 1997 · N985AX · Doug DC932 · Wing, Rib/BulkheadSDR ABXA9700500Link Assy · wornDURING C-INSPECTION, FOUND THE LEFT OUTBOARD SPOILER DRIVE LINK UPPER AND LOWER BEARINGS WORN. REPLACED LEFT OUTBOARD SPOILER DRIVE LINK IAW ABX EA 27-04047MA AND DC9 MAINTANCE MANUAL CHAPTER 27-61-02.Feb 20, 1997 · N985AX · Doug DC932 · Drag Control SystemSDR ABXA9700496Intercostal · crackedDURING C-INSPECTION, FOUND THE INTERCOSTAL BETWEEN FS 699 LEFT AND 718 LEFT UPPER FORWARD CORNER CRACKED. REPAIRED INTERCOSTAL IAW DC9 SUPPLEMENTAL SRM DRAWING K 05159 AND SRM CHAPTER 51-30-2 AND 51-30-5.Feb 20, 1997 · N985AX · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ970120Longeron · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, LONGERON 30 BETWEEN STATION 544-564 HAS A 5 INCH CRACK. REMOVE LONGERON FOR CRACK FABRICATED LONGERON AND SPLICE, DRILL AND DEBURRED. HOLD IN LONGERON SPLICE PART. INSTALLFeb 19, 1997 · N921VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ970119Sub Floor · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, SUB FLOOR CORRODED AT STATION 196 LBL 21. REMOVED CORROSION, DETERMINED OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1 (DEPTH GAUGE A-0299) MORE THAN 20 PERCENT MATERIAL LOSS. FABRFeb 19, 1997 · N921VV · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700216Skin · damagedYIP - REPAIR ON RIGHT FLAP TRAILING EDGE AT APPROXIMATELY STATION XRS 138-156 BE REMOVED AND REPLACED WITH NEW. REMOVED AND REPLACED RIGHT FLAP TRAILING EDGE WITH NEW PART IAW DC9 SRM 57-03 PAGE 11. (M)Feb 19, 1997 · N947ML · Doug DC932 · Trailing Edge FlapsSDR GTIA9700197Doubler · damagedYIP - EXTERNAL REPAIR DOUBLER FS 351 BETWEEN LONGERONS 18R AND 20R REQUIRES REWORK. REWORKED REPAIR DOUBLER AT RIGHT FUS 351 TO C/W REQUIREMENTS OF DC-9 SRM 53-04 FIG 12B (INSTALLATION OF FINGER DOUBLER AND PROPER FASTENERS). (X)Feb 19, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700476Doubler · corrodedINSPECTION FOUND DOUBLER CORRODED AT STA 897. THE DOUBLER WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-11-3 AND 51-30-2.Feb 19, 1997 · N17543 · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ970122Slide · malfunctionedCHECKED REAR EVACUATION SLIDE FOR PROPER SERVICING. AS PRECAUTIONARY MEASURE, REMOVED AND REPLACED TAILCONE SLIDE PER MM 25-60. (M)Feb 18, 1997 · N910VJ · Doug DC932 · Escape SlideSDR VJ970118Battery Charger · failedEMERGENCY PATH FLOOR LIGHTS BETWEEN SEAT ROWS 15-20 OUT. ALSO, LEFT SIDE INOP AFT ACCESSORY COMPARTMENT. REPLACED BATTRY CHARGER AT FUSELAGE STATION 936 AND REPAIRED WIRING TO CHARGER PER MM 33-53-0. OPS CHECKED GOOD. (M)Feb 18, 1997 · N912VV · Doug DC932 · Emergency LightingSDR VJ960121Slide Cover · fell offCOVER POPPED OFF R1 DOOR SLIDE. REINSTALLED SLIDE COVER PER MM 25-60. (M)Feb 18, 1997 · N924VV · Doug DC932 · Emergency EquipmentSDR GTIA9700200Bracket · crackedYIP - LEFT FLAP, INBOARD ATTACH BRACKET CRACKED. (CONFIRMED WITH EDDY CURRENT.) REMOVED AND REPLACED LEFT INBOARD ATTACH BRACKET WITH NEW BRACKET IAW DC-9 MM 20-16-0 PAGE 207. (X)Feb 18, 1997 · N947ML · Doug DC932 · Trailing Edge FlapsSDR VJ970116Spar · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, RIGHT WING AFT SPAR LOWER CAP HAD BLEND OUT AT STATION XRS 88 AND TWO CRACKS AT STATIONS XRS 88 AND XRS 73.5. RIGHT WING AFT SPAR CAP BLEND OUT AT STATION XRS 88 AND TWO CRAFeb 17, 1997 · N919VV · Doug DC932 · Wing SparSDR TWAA9712001Switch · failedSTL - FLT 251 - RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE DOWN. REMOVED AND REPLACED DOWNLOCK SWITCH, MFG P/N H14-6, MANUFACTURED BY EATON CORPORATION. OPERATIONAL CHECK NORMAL. (M)Feb 17, 1997 · N923L · Doug DC932 · Landing Gear Position and WarningSDR TWAA9711001Relief Valve · failedSTL - FLT 322 - DURING CLIMB, THE NR 2 ENGINE, S/N 3994 INDICATED HIGH OIL PRESSURE. REMOVED AND REPLACED OIL PRESSURE RELIEF VALVE, MFG P/N 811131, MANUFACTURED BY PWA. OPERATIONAL CHECK NORMAL. (M)Feb 17, 1997 · N920L · Doug DC932 · Turbine Engine Oil SystemSDR TWAA9710006Longeron · corrodedSTL - REMOVED CORROSION FROM TOP SURFACE OF LONGERON 27L AT STATION 862. (M)Feb 17, 1997 · N996Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9710005Bulkhead Skin · corrodedSTL - REMOVED AND REPLACED BULKHEAD SKIN BETWEEN LONGERON 30 TO 23R AND LONGERON 30 TO 26L DUE TO CORROSION. (M)Feb 17, 1997 · N996Z · Doug DC932 · Fuselage Main, BulkheadSDR GTIA9700227Trap Panel · crackedYIP - ULTRASONIC INDICATION FROM FORWARD MOST END OF UPPER ATTACH FLANGE THROUGH FIRST ATTACH HOLE TO FORWARD END OF SECOND ATTACH HOLE OF LEFT TRAP PANEL (APPROXIMATE LENGTH, 2 INCHES). REMOVED OUTBOARD PORTION OF CRACKED FLANGE AND CORROSION IAW DC-9 SRM 57Feb 17, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700199Fairing · corrodedYIP - LEFT HORIZONTAL STABILIZER LOWER SCRAPPER FAIRING: INTERIOR BOX CHANNEL HAS SURFACE CORROSION ALONG ATTACH EDGES. REMOVED MINOR SURFACE CORROSION IAW DC-9 SRM 51-10-3. (X)Feb 17, 1997 · N947ML · Doug DC932 · Horizontal Stabilizer StructureSDR MWEA97112Bulkhead Channel · crackedDURING INSPECTION, FOUND AFT PRESS BULKHEAD CHANNEL CRACKED UNDER TOP VENTRAL STAIR. MAINT REMOVED AND REPLACED CHANNEL IAW 53-05 FIG 40.Feb 16, 1997 · N401ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA97111Skin · crackedDURING INSPECTION, FOUND FWD CARGO DOOR LWR AFT CORNER HAS CRACKS FROM FASTENER HOLE ON DOOR PAN. MAINT INSTALLED DOUBLER REPAIR IAW SRM 52-03 FIG 8.Feb 16, 1997 · N401ME · Doug DC932 · Cargo/Baggage DoorsSDR 9703669610Retract Mech · out of adjustRIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT CONTINUED TO DTW AT REDUCED SPEED. ON GEAR EXTENSION, GEAR DOOR OPEN LIGHT REMAINED ON. CREW DECLARED AN EMERGENCY AND UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES ON LANDING. AIRCRAFT Feb 16, 1997 · N610NW · Doug DC932 · Landing Gear Door Retract SectionSDR 9703269618Fuse · blownDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT ROWS 5 THROUGH 7 AND AT FORWARD RIGHT OVERWING DOOR INOPERATIVE. REPLACED FUSE IN FORWARD RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK NORMAL.Feb 16, 1997 · N618NW · Doug DC932 · Emergency LightingSDR VJ970115Sensor · failedTAIL COMPARTMENT HIGH LIGHT CAME ON IN CLIMB, FLIGHT CREW ISOLATED PROBLEM TO LEFT PACK USING AIRCRAFT OPERATIONS MANUAL. FLIGHT DIVERTED TO MCO. TIGHTENED LOOSE CLAMP ON LT AUGMENTATION VALVE. SUBSEQUENTLY, ITEM REPEATED FOLLOWING DAY AND TAIL COMPARTMENT Feb 15, 1997 · N901VJ · Doug DC932 · Pneumatic Distribution SystemSDR 9703319941Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK, OPERATIONAL CHECK NORMAL.Feb 15, 1997 · N3324L · Doug DC932 · Emergency LightingSDR GTIA9700195Rivet · failedYIP - LEFT UPPER HORIZONTAL STABILIZER FAIRING - POPPED RIVET AT AFT ATTACH AND AFT CDCC AREA CRACKED. REPAIRED CRACK AND INSTALLED EXTERNAL DOUBLER AND FILLER PER DC-9 SRM 55-01 PAGE 7, 51-30-2 AND USING MATERIAL AS PRESCRIBED IN DC-9 SRM 55-10-0, PAGE 11, FFeb 14, 1997 · N947ML · Doug DC932 · Horizontal Stabilizer StructureSDR GTIA9700192Clip · brokenYIP - FS 148 CIRCUMFERENTIAL APPROXIMATELY 12 INCHES LEFT OF CENTER OVERHEAD, BROKEN ANGLE CLIP. MANUFACTURED REPAIR ANGLE IAW DC-9 SRM 51-10-1. INSTALLED ANGLE IAW DC-9 SRM 51-30-1. (X)Feb 14, 1997 · N947ML · Doug DC932 · Fuselage Miscellaneous StructureSDR 9703289917Batteries · dischargedDURING PERIODIC CHECK, FOUND OVERWING EMERGENCY LIGHTS AT ROWS 2 AND 3 DIM. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Feb 14, 1997 · N967N · Doug DC932 · Emergency LightingSDR VJ970124Splice · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, LONGERON 30 SPLICE BETWEEN STATION 408 AND 427 HAS 2 INCH CRACK BETWEEN FASTENERS. REMOVED CRACKED FITTING. FABRICATED AND INSTALLED SPLICE IAW DC-9 SRM 53-02 FIG 14 AND 51Feb 13, 1997 · N922VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ970113Slide Cover · fell offL1 DOOR SLIDE COVER FELL. RESECURED SLIDE. (M)Feb 13, 1997 · N932VV · Doug DC932 · Emergency EquipmentSDR VJ970110Spar Cap · corrodedDURNG A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT MAIN TANK XW 58.768 REAR SPAR LOWER CAP TO STRINGER 11 WAS CORRODED. XW 58.768 LEFT MAIN TANK REAR SPAR LOWER CAP TO STRINGER 11 CORROSION ON T-CAP COMPLIED IAW EO 9Feb 13, 1997 · N919VV · Doug DC932 · Wing SparSDR VJ970109Rear Spar · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT MAIN TANK REAR SPAR LOWER CAP XRS 70 HAS CORROSION AROUND 1 FASTENER. LEFT MAIN TANK REAR SPAR LOWER CAP XRS 70 CORROSION AROUND FASTENER COMPLIED WITH IAW EO 97-47Feb 13, 1997 · N919VV · Doug DC932 · Wing SparSDR VJ970108Stringer · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT MAIN TANK XRS 58-69 STRINGER 16 UPPER AND LOWER CAP IS CORRODED ON LOWER STRINGER. NR 4 MAIN TANK XRS 58-69 STRINGER 16 UPPER AND LOWER CAP CORROSION COMPLIED IAW EFeb 13, 1997 · N919VV · Doug DC932 · Wing, Longeron/StringerSDR VJ970107Stringer · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT MAIN TANK XRS 58-69 STRINGER 15 UPPER AND LOWER CAP IS CORRODED ON LOWER STRINGER. LEFT MAIN TANK XRS 58-69 STRINGER 15 UPPER AND LOWER CAP CORROSION ON LOWER STRINFeb 13, 1997 · N919VV · Doug DC932 · Wing, Longeron/Stringer
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