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 CALA9801659Fairing · crackedINSPECTION FOUND A 4.5 INCH CRACK IN LOWER AFT END OF RT HORIZONTAL STABILIZER LOWER FAIRING. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 55-11-0 FIGURE 7, 55-01, FIGURE 2, 51-10-3, AND 51-30-2.Sep 8, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer StructureSDR CALA9801654Doubler · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN DOUBLER AT STA 945, LONGERON 14R. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 28.Sep 8, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801653Floor · crackedINSPECTION FOUND 1 INCH CRACKS AT CLIP NUT HOLES IN FLOOR PANEL NR 47 FORWAD OF STA 756. A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-21, 51-30-2, AND 53-05, FIGURE 1.Sep 8, 1998 · N70542 · Doug DC932 · Fuselage Floor PanelSDR 98ZZZX4001Ballast · shortedTWO POWER LAMPHOLDER ASSEMBLIES (BALLAST) WERE BURNED BY ARCING WITH THE ELECTRIC WIRE CONNECTOR WHICH WAS FABRICATED AND ASSEMBLED BY BRUCE INDUSTRIES (FAA PMA 400-067), AND DELIVERED TO AEROMEXICO FOR INTERIOR MODIFICATION OF DC9'S. THIS AIRCRAFT WAS MODIFISep 8, 1998 · N1003P · Doug DC932 · Passenger Compartment LightingSDR MWEA98955Slide · detachedTHE MAIN SLIDE ON FORWARD EXIT FELL OFF. MAINTENANCE REINSTALLED PASSENGER DOOR SLIDE.Sep 7, 1998 · N302ME · Doug DC932 · Emergency EquipmentSDR MWEA98954Battery Pack · dischargedFOUND LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK.Sep 6, 1998 · N302ME · Doug DC932 · Emergency LightingSDR MWEA98953Cover · crackedFOUND FORWARD PASSENGER DOOR EMERGENCY SLIDE COVER CRACKED. MTC RESECURED LAMINANT COVER TO EMERGENCY SLIDE COVER.Sep 6, 1998 · N302ME · Doug DC932 · Emergency EquipmentSDR MWEA98952Door · damagedFOUND TEAR IN WATER SERVICE PANEL DOOR ON AFT LOWER CORNER. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.Sep 6, 1998 · N302ME · Doug DC932 · Fluid Service DoorsSDR MWEA98951Battery Pack · dischargedFOUND RIGHT NACELLE EMERGENCY LIGHT VERY DIM. MTC REMOVED AND REPLACED NACELLE EMERGENCY LIGHT BATTERY PACK.Sep 6, 1998 · N302ME · Doug DC932 · Emergency LightingSDR MWEA98950Jamb · crackedFOUND CRACK ON AFT VENTRAL DOOR JAMB LEFT SIDE ANGLE. MTC FABRICATED AND INSTALLED DOUBLER.Sep 6, 1998 · N301ME · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800861Web · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CUSP WEB BETWEEN FS 218 AND 237 CORRODED. REPLACED CUSP WEB IAW DC9 SRM CHAPTERS 51-30-2 AND 51-30-5.Sep 6, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98949Bulkhead Support · crackedFOUND CRACK IN AFT PRESSURE BULKHEAD UPPER LEFT SUPPORT ATTACHED TO -13 DOUBLER. MTC REMOVED AND REPLACED DOUBLER.Sep 5, 1998 · N301ME · Doug DC932 · Fuselage Main, BulkheadSDR VJ9800469Channel · crackedLT LOWER CORNER AFT ENTRY DOOR CRACKED 1.875 INCHED IN LENGTH. REPLACED CRACKED CHANNEL AND REINSTALLED AFT ENTRY DOOR ATTENDANT SEAT IAW DC9 OHM 25-21-3, MM 25-23-2 AND DC9 SRM 51-30-1, 51-30-2, 51-30-4, 51-30-5 AND AIRTRAN RES 981367.Sep 4, 1998 · N933VV · Doug DC932 · Passenger/Crew DoorsSDR VJ9800317Life Vest · damagedAFT RT FLT ATTENDANTS LIFE VEST COVER TORN. INSTALLED SERVICEABLE LIFE VEST.Sep 4, 1998 · N940VV · Doug DC932 · Life JacketSDR CALA9801636Frame · crackedINSPECTION FOUND A 1 INCH CRACK AT UPPER MOUNT HOLE OF FRAME AT STA 980, LONGERON 16R. THE CRACKED AREA WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-1.Sep 4, 1998 · N70542 · Doug DC932 · Fuselage Main, FrameSDR ABXA9800883Fitting · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND VERTICAL ATTACH FITTING CRACKED AT FS 617 UNDER SEAT TRACK AT LBL 22. REPLACED ATTACH FITTING IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-5.Sep 3, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800874Longeron · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 RIGHT CRACKED AT FS 945 ON UPPER AND LOWER FLANGE. REPLACED LONGERON 17 RIGHT FROM FS 937 TO 996 IAW DC9 SRM.Sep 3, 1998 · N903AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800865Shear Tie · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND SHEAR TIE DOUBLER ON FUSELAGE FRAME AT FS 945 CRACKED AT LONGERON 14 RIGHT. REPLACED SHEAR TIE AT FS 945 BETWEEN LONGERON 14 RIGHT AND LONGERON 16 RIGHT IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-5.Sep 3, 1998 · N903AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9800859Angle · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ENTRY DOOR PAN CRACKED OUT IN LOWER FORWARD CORNER. REPAIRED CRACK IAW ABX REA D952-24779.Sep 3, 1998 · N903AX · Doug DC932 · Passenger/Crew DoorsSDR CALA9801621Web · corrodedINSPECTION FOUND WEB CORRODED AT FORWARD CARGO DOOR, STA 370, STRINGER 28R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.Sep 2, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801620Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT FASTENER IN TAIL SECTION SKIN AT STA 1062 APPROXIMATELY FOUR INCHES BELOW LONGERON 15L. THE FASTENER WAS REMOVED IAW SRM 51-30-2 AND THE CRACKED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 28. A DOUBLER REPAIR WAS INSTALLED IASep 2, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801619Bulkhead Strap · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER SUPPORT STRAP OF FORWARD BULKHEAD WALL IN AFT PIT, FS 737. THE SUPPORT STRAP WAS REMOVED AND A NEW SUPPORT STRAP WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3.Sep 2, 1998 · N70542 · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9800905Longeron · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 16 LEFT LOWER FLANGE CRACKED AT FS 965. REPLACED LONGERON 16 LEFT AT FS 965 IAW DC9 SRM DRAWING K05864.Sep 2, 1998 · N903AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800884Control Cable · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND NR 2 ENGINE FUEL SHUT-OFF CABLE NR 57 HEAVILY CORRODED BETWEEN STATION 658 AND 699. REPLACED NR 2 ENGINE FUEL SHUT-OFF CABLE IAW DC9 MM CHAPTER 76-12-00.Sep 2, 1998 · N903AX · Doug DC932 · Engine Emergency Shutdown SystemSDR ABXA9800882Fitting · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND VERTICAL ATTACH FITTING CRACKED AT FS 617 UNDER SEAT TRACK AT LBL 44. REPLACED ATTACH FITTING IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-5.Sep 2, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800875Longeron · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 LEFT CRACKED AT FS 945 ON THE LOWER FLANGE. REPLACED LONGERON SECTION 17 LEFT AT FS 945 IAW DC9 SRM DRAWING K05864.Sep 2, 1998 · N903AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800423Floor · corrodedE/E BAY FLIGHT COMPARTMENT FLOOR FS 161.0 CORRODED AND A PORTION IS MISSING. CLEANED CORROSION, 100 PERCENT MATERIAL LOSS AND CRACKED SKIN. FABBED REPAIR DOUBLER IAW DC-9 SRM 51-01, 53-01. DRILLED, DEBURRED AND COUTERSUNK IAW DC-9 SRM 53-11-1. TREATED AND Sep 1, 1998 · N933VV · Doug DC932 · Fuselage Floor PanelSDR MWEA98948Cover · detachedTHE FORWARD GALLEY SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED THE SLIDE COVER.Sep 1, 1998 · N204ME · Doug DC932 · Emergency EquipmentSDR CALA9801610Longeron · crackedINSPECTION FOUND A 2 INCH CRACK IN LONGERON 17L AT ANGLE MOUNT, STA 965. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02, FIGURE 18. A NEW LONGERON SECTION AND SPLICE WERE INSTALLED IAW SRM 51-30-5.Sep 1, 1998 · N70542 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801600Position Switch · inoperativeTHE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. QRH PROCEDURE WAS FOLLOWED, BUT GREEN LIGHT STILL DID NOT ILLUMINATE. THE NOSE GEAR WAS VISUALLY CONFIRMED DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NLG DOWNLOCSep 1, 1998 · N14534 · Doug DC932 · Landing Gear Position and WarningSDR ABXA9800886Rib · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND RIB CRACKED INSIDE LEFT FLAP AT OUTBOARD FLAP HINGE. REPLACED RIB INSIDE LT FLAP IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2.Sep 1, 1998 · N903AX · Doug DC932 · Trailing Edge FlapsSDR VJ9800468Floor · corrodedACCESS PANEL AND COVER FWD CARGO FLOOR PANEL CORRODED BEYOND LIMIT IAW DC9 SRM 53-01. FABRICATED NEW COVER PLATE, LOCATED NEW ACCESS PANEL, INSTALLED IAW DC9 SRM 51-10-2.Aug 31, 1998 · N933VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800467Splice · corrodedFWD PIT FS 484-503, L30, CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. REMOVED LONGERON IAW DC9 SRM 53-11-2, FIG 14, CUT, TRIMMED, DRILLED, INSTALLED NEW SECTION LONGERON AND SPLICES IAW DC9 SRM 51-30-3, 51-30-3. SPLICES MADE FROM 7075T7351..Aug 31, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800466Intercostal · corrodedFLOOR BRACKET BY NUTPLATES AT FS 560 -579, L27 -28R, CORRODED. FABRICATED NEW PANEL INTERCOSTAL FLANGE FROM 7075-80,.050, IAW DC9 SRM 51-30-1, 53-11-1, FIG 10. HEAT TREATED AND FABRICATED NEW INTERCOSTAL FLANGE FROM 7075-0,.050, IAW DC9 SRM 53-11-2 AND AIRTRAug 31, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800465Doubler · crackedFWD CARGO DOOR JAMB AFT WEB SUPPORT HAS FASTENER HOLE CRACKED TO EDGE OF WEB. FABRICATED REPAIR DOUBLER FROM 2024T3-.040 IAW DC9 SRM 53-01. FIG 2. DRILLED, DEBURRED, TRIMMED IAW DC9 SRM 51-30-2 AND AIRTRAN RES 981439.Aug 31, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800464Bracket · corrodedGILL LINER ATTACHING BRACKETS ALONG BOTTOM OF BULKHEAD AT STA 998 CORRODED. FABRICATED, HEAT TREATED, DRILLED, ALODINED AND PRIMED NEW ATTACH ANGLES IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4 AND AIRTRAN RES 981417.Aug 31, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800463Skin · corrodedSKIN AT FS 966, L30, CORRODED BEYOND LIMIT. CUT OUT CORRODED SKIN AREA IAW DC9 SRM 53-04, FIG 9. FABRICATED, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3 AND 53-04, FIG 9.Aug 31, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800388Skin · dentedDENTS OUT OF LIMIT AT AFT SECTION OF SKIN AT AFT ENTRY DOOR IAW DC9 SRM 51-50-1, FIG 1. CUT OUT DAMAGED AREA, FABRICATED SKIN REPAIR AND DOUBLER. FITTED, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-10-4, 51-10-3, 51-10-2 AND AIRTRAug 31, 1998 · N933VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800387Longeron · dentedTWO EACH DENTS LOCATED AT FS 250L, L18-17, OUT OF LIMIT. COLD WORKED DENTS AT STA 250-245L, BETWEEN L17-18L, IAW DC9 SRM 53-04, FIG 38. FABRICATED DOUBLER REPAIR IAW DC9 SRM 53-04, FIG 38. DRILLED, TRIMMED AND DEBURRED DOUBLER, TREATED AND PRIMED DOUBLER ANAug 31, 1998 · N933VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800386Longeron · dentedDENT .048X2X 18 INCHES AT FS 240R, L26-29, OUT OF LIMIT IAW 5304, FIG 38. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DC9 SRM 53-04, FIG 38.Aug 31, 1998 · N933VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800385Frame · crackedFRAME 699R AFT SIDE BELOW FLOOR LEVEL CRACKED. REPLACED CRACKED FRAME AT STA 699 RT IAW EO 12-5311-29-B1044.Aug 31, 1998 · N933VV · Doug DC932 · Fuselage Main, FrameSDR VJ9800384Skin · corrodedRT PYLON LOWER TRAILING EDGE SKIN CORRODED ON INBOARD SIDE. REMOVED CORRODED SKIN FROM RT PYLON LOWER TRAILING EDGE IAW DC9 SRM 51-10-2, 51-10-4. INSTALLED NEW SKIN IAW DC9 SRM 51-30-2 AND RES 981313, REINSTALLED TRAILING EDGE ON PYLON IAW DC9 SRM 51-30-1.Aug 31, 1998 · N933VV · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR VJ9800383Frame · corrodedFORWARD CARGO FRAME STA 218, L26L-L26R CORRODED. REMOVED NUTPLATES FOR ACCESS AND CORROSION IAW DC9 SRM 51-10-3. TREATED AND PRIMED FROM LBL 3 TO RBL 40 AND LBL 5 TO LBL29 IAW DC9 SRM 53-01, FIG 1. FABRICATED REPAIR FILLER AND DOUBLER, PRIMED AND INSTALLED Aug 31, 1998 · N933VV · Doug DC932 · Fuselage Main, FrameSDR VJ9800382Skin · corrodedFRAME TO SKIN ATTACHING CLIP AND SKIN IN AFT CARGO COMPARTMENT AT STA 945 HAS CORROSION BEYOND LIMIT. REMOVED CORROSION AT FRAME LOWER CAP IAW DC9 SRM 51-30-2 AND FOUND SHEAR TIE CRACKED IN TWO PLACES AND SKIN OUT OF LIMIT IAW DC9 SRM 53-01, FIG 1. FABRICATEAug 31, 1998 · N933VV · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98947Light · inoperativeFOUND FORWARD EMERGENCY ENTRANCE LIGHT INOP. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY ENTRANCE LIGHT ASSEMBLY.Aug 31, 1998 · N502ME · Doug DC932 · Emergency LightingSDR MWEA98944Pan · chafedFOUND CHAFE DAMAGE ON AFT LAV TOILET SERVICE DOOR PAN. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS.Aug 31, 1998 · N809ME · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800887Angle · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLAP OUTBOARD HINGE FITTING, INBOARD ATTACH ANGLE CRACKED. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2, AND 51-30-5.Aug 31, 1998 · N903AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9800885Angle · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND INTERCOSTAL LOWER SUPPORT ANGLE CORRODED AT FS 917 AND RBL 22. REPLACED ANGLE IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2.Aug 31, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800881Fitting · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND VERTICAL SUPPORT BRACKET UNDER SEAT TRACK AT FS 680 AND LBL 44 CRACKED. REPLACED SUPPORT BRACKET IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-5.Aug 31, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABAX9800888Angle · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLAP OUTBOARD HINGE FITTING, OUTBOARD ATTACH ANGLE CRACKED. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2, AND 51-30-5.Aug 31, 1998 · N903AX · Doug DC932 · Trailing Edge Flaps
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