Douglas DC-9-32

Service difficulty reports · 12,755

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  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 MWEA00544Battery Pack · inoperativeOMA - TWO EMERGENCY LIGHTS AT TOP OF AFT EMERGENCY ESCAPE SLIDE AND ONE LIGHT ON LEFT SIDERAIL WERE INOPERATIVE. REMOVED AND REPLACED AFT BATTERY PACK. (M)Jul 3, 2000 · N205ME · Doug DC932 · Emergency LightingSDR AT0000368Skin · lightning strikeFOUND LIGHTNING STRIKE AT LEFT HAND WINDOW BELT PANEL AT BS 908 - 937. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 MM 25-21-0, 53-05 FIGURE 11 AND REO L00224.Jul 3, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000367Skin · lightning strikeFOUND LIGHTNING STRIKE AT LEFT HAND WINDOW BELT PANEL AT BS 832 - 870. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 MM 25-21-0, 53-05 FIGURE 11 AND REO L00224.Jul 3, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0010401Bulb · failedTHE EMERGENCY LIGHT ABOVE THE AFT FLIGHT ATTENDANT SEAT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 3-29-00 MCI. ---CLOSED---Jul 3, 2000 · N925L · Doug DC932 · Emergency LightingSDR MWEA00546Pan · crackedMKE - FORWARD CABIN ENTRY DOOR HAD AN APPROXIMATE 1 INCH CRACK AT EDGE OF OUTER PAN AT LOWER HINGE CUT OUT. MAINTENANCE REPAIRED CRACK IAW BOEING SRM 52-05, FIGURE 33. (X)Jul 2, 2000 · N501ME · Doug DC932 · Passenger/Crew DoorsSDR AT0000358Lap Joint · corrodedFOUND SKIN LAP FUSELAGE SKIN PITTED BEYOND LIMITS AT L24 - L26. CUT OUT CORRODED SECTION AND INSTALLED REPAIR IAW REO L00229.Jul 2, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/SkinSDR CA000721006Guard · missing(CAN) ON WALKAROUND, CREW NOTICED TAILCONE RELEASE HANDLE GUARD MISSING. GUARD REPLACED BY MAINTENANCE.Jul 1, 2000 · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000349Door · openFELT STRONG VIBRATION IN COCKPIT AFTER GEAR RETRACTION. SLOWED AIRCRAFT AND CYCLED GEAR, NO HELP. FOUND NOSE GEAR DOOR OPEN, INSPECTED NOSE GEAR FOR DAMAGE, NONE FOUND. CLOSED AND SECURED BOTH NOSE GEAR DOORS IAW DC9 MM 32-20-0.Jul 1, 2000 · N836AT · Doug DC932 · Landing Gear Door Retract SectionSDR MWEA00536Computer · failedMCI - EN ROUTE TO DFW, THE STALL INDICATION FAILURE ANNUNCIATOR LIGHT CAME ON AND THE NR 1 STALL C0MPUTER CIRCUIT BREAKER POPPED AND WOULD NOT RESET. FLIGHT DIVERTED TO MCI. MAINTENANCE REMOVED AND REPLACED NR 1 STALL COMPUTER BUT AT PUSH TIME, CIRCUIT BREAKJun 30, 2000 · N301ME · Doug DC932 · Stall Warning SystemSDR MWEA00538Floorboard · crackedMKE - FOUND CABIN FLOORBOARD BETWEEN SEAT TRACKS NR 1 AND NR 2 AT STATION 680 IS CRACKED IN NUMEROUS PLACES. FABRICATED AND INSTALLED NEW FLOORBOARD AREA. (M)Jun 30, 2000 · N502ME · Doug DC932 · Fuselage Floor PanelSDR MWEA00539Skin · dentedMKE - FUSELAGE IS DENTED AT STATION 113 LONGERON 19 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER. (M)Jun 30, 2000 · N502ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA00540Longeron · crackedMKE - LONGERON 4L IS CRACKED AT FRAME STATION 756. FABRICATED AND INSTALLED REPAIR SPLICES AND LONGERON. (M)Jun 30, 2000 · N502ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00541Longeron · crackedMKE - LONGERON 3 LEFT HAS A CRACK WHERE IT ATTACHES TO FRAME AT STATION 756. FABRICATED AND INSTALLED REPAIR SPLICES AND LONGERON. (M)Jun 30, 2000 · N502ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00542Clip · crackedMKE - FOUND CRACK IN SHEAR CLIP BETWEEN LONGERON 14, 15 AND 16 LEFT AT STATION 945. FABRICATED AND INSTALLED NEW SHEAR CLIPS. (M)Jun 30, 2000 · N502ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00543Clip · crackedMKE - FOUND CRACK IN SHEAR CLIP BETWEEN LONGERON 14, 15, AND 16 RIGHT AT STATION 945. FABRICATED AND INSTALLED NEW SHEAR CLIPS. (M)Jun 30, 2000 · N502ME · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0010705Skin · corrodedIN THE FORWARD CARGO COMPT, CORROSION WAS FOUND BETWEEN SKIN AND DOUBLER AT STA 598 TO 604, LONGERON 29L TO 29R, AND RIVETS POPPED ON THE SKIN. REMOVED CORRODED DOUBLER PER SRO-9530101. REPAIRED CORRODED SKIN PER DAC DRAWING SRO-9530101. CHECK-C 1-12-00 STL.Jun 30, 2000 · N924L · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000354Attach Angle · corrodedFOUND G-2 GALLEY ANGLES CORRODED AT RIGHT SIDE OF G-2. REMOVED CORRODED ANGLES, FABRICATED AND INSTALLED NEW ANGLES IAW DC9 51-10-2, 51-10-3, 51-10-4, 51-30-2.Jun 29, 2000 · N817AT · Doug DC932 · Fuselage Main, Attach FittingsSDR TWAA0010414Access Panel · damagedDURING OP 16 MAINT CHECK FOUND LT WING BOTTOM FUEL TANK ACCESS PLATE NR 1365, HAD 2 MOUNT RING SCREW HOLES ELONGATED. REPAIRED PER ARA 16924A. REAMING PER SRM 51-30-10, AND COLD WORKING PER SRM 51-30-9. ---CLOSED---Jun 29, 2000 · N921L · Doug DC932 · Wing, Plate/SkinSDR TWAA0010408Frame · damagedDURING CHECK-C MAINT AT STA 965 FOUND PREVIOUS FRAME REPAIR BETWEEN LONGERON 22 LT AND 25 LT, REQUIRED REPLACEMENT. REPAIRED FRAME AT STA 965 FROM LONGERON 26R TO 23L PER SRM 53-03 FIG 2A.Jun 29, 2000 · N924L · Doug DC932 · Fuselage Main, FrameSDR TWAA0010407Frame · corrodedDURING CHECK-C MAINT THE FUSELAGE FROM STA 965 AFT SIDE BETWEEN LONGERON 29R TO 28L, WAS CORRODED IN THE AFT CARGO BIN. REPAIRED FRAME AT STA 965 PER SRM 53-03, FIG 2A, LONG 26R TO 23L.Jun 29, 2000 · N924L · Doug DC932 · Fuselage Main, FrameSDR TWAA0010406Skin · corrodedDURING CHECK -C MAINT FOUND IN FWD CARGO COMPT AT STA 446, LONGERON 30, THE AFT SIDE OF FINGER DOUBLER HAD CORROSION. CUT OUT CORRODED SECTION OF SKIN AND INSTALLED DOUBLER REPAIR PER 53-04, FIG 44. ---CLOSED---Jun 29, 2000 · N924L · Doug DC932 · Fuselage Main, Plate/SkinSDR 0002279608Charger · failedBATTERY CHARGER LIGHT ILLUMINATED IN FLIGHT. CREW DECLARED AN EMERGENCY AND FLIGHT WAS CONTINUED TO DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BATTERY CHARGER AND BATTERIES. OPERATIONAL CHECK NORMAL.Jun 28, 2000 · N608NW · Doug DC932 · Battery/Charger SystemSDR GTIA000236Light · inoperativeMYR - FLT 541 - AFT OVERWING EMERGENCY LIGHTS INOP. FOUND 1 BAD BATTERY AT PACK B5-25. REMOVED AND REPLACED BATTERY. OPS CHECK GOOD PER DC9 MM 33-53-0. (M)Jun 27, 2000 · N12536 · Doug DC932 · Emergency LightingSDR GTIA000237Switch · malfunctionedMYR - FLT 541 - FOUND 3 EMERGENCY LIGHTS AT FORWARD ENTRANCE COME ON WITH ENTRY LIGHT SWITCH AND DO NOT TEST WITH COCKPIT EMERGENCY SWITCH. REPOSITIONED INSULATION ABOVE FORWARD ENTRANCE LIGHT ASSY. OPS CHECKS GOOD PER DC9 MM 33-53-0. (M)Jun 27, 2000 · N12536 · Doug DC932 · Emergency LightingSDR TWAA0010102Longeron · crackedFOUND A .5 INCH CRACK IN THE I/B FLANGE OF NUMBER 2 LONGERON 6L AT STA 639. SECTION CUT OUT, LONGERON REPAIR SPLICE PUT IN PER SRM 53-02-0, FIG 18 SHEET 1. CHECK-C 2-25-00 STL.Jun 27, 2000 · N931L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA0010101Longeron · crackedA .5 INCH CRACK WAS FOUND IN THE I/B FLANGE OF LONGERON 6L AT STA 756. INSTALLED SPLICE FLANGE FASTENERS AND INTERCOSTAL FASTENERS PER SRM 53-02. CHECK-C 2-25-00 STL.Jun 27, 2000 · N931L · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00535Battery Pack · dischargedOMA - BOTH AFT OVERWING EMERGENCY EXIT SIGNS VERY DIM. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN BATTERY PACKS. (X)Jun 26, 2000 · N202ME · Doug DC932 · Emergency LightingSDR ABXA000328Angle · crackedDURING C-CHECK, FOUND INTERCOSTAL TO FLOORBEAM ATTACH ANGLE CRACKED AT STATION 617, LEFT BL 44. REPLACED ANGLE IAW DC9 SRM 51-30-5.Jun 26, 2000 · N982AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA000327Panel · crackedDURING C-CHECK, FOUND RIGHT TRAP PANEL CRACKED AT TOP OUTBOARD FLANGE. REPLACED RIGHT TRAP PANEL IAW DC9 SRM 51-30-5, AND DC9 S/B 53-182.Jun 26, 2000 · N982AX · Doug DC932 · Wing, Plate/SkinSDR AT0000357Skin · crackedFOUND FORWARD CARGO DOOR JAMB, LOWER, HAS CRACKS IN EXTERNAL SKIN. REMOVED EXISTING REPAIR, DOUBLER AND FILLER. CUT OUT CRACKED AREA AND FABRICATED 4 FILLERS, FABRICATED REPAIR DOUBLER AND INSTALLED IAW REO L00223.Jun 25, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/SkinSDR L1GA200000173Uplock Switch · inoperativeRT MLG UNSAFE LIGHT ILLUMINATED UPON GEAR RETRACTION AFTER T/O FROM LAS. CYCLED GEAR INDICATIONS NORMAL. R&R RT MLG UP LIMIT SWITCH, OPS CK GOOD.Jun 25, 2000 · N12508 · Doug DC932 · Landing Gear Position and WarningSDR AT0000344Frame · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND SEVERE EXFOLIATION ON FRAME AT BS 870 LONGERON 23 LEFT. CORRECTIVE ACTION: REMOVED AND REPLACED FRAME ATBS 870 BETWEEN LONGERON Jun 24, 2000 · N823AT · Doug DC932 · Fuselage Main, FrameSDR AT0000463Floorbeam · corrodedAFT LAV FLOORBEAM AT BS 996 LONGERON 18 - 19R CORRODED. REMOVED FLOORBEAM AND CORRODED WEB. INSTALLED NEW WEB AND DOUBLER IAW DC9 SRM 51-05 FIG 72, 51-10-04, 51-10-03, AND 53-05 FIG 2.Jun 24, 2000 · N823AT · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA0010005Longeron · crackedLONGERON 5L WAS CRACKED .5 INCH LONG AT STA 756, UPPER FLANGE FASTENER AREA. REMOVED AND REPLACED DAMAGED LONGERON 5L AT STA 756 PER SRM 53-02, FIG 18, AND 51-30-2 AND 51-30-5. CHECK-C 12-14-99 STL.Jun 24, 2000 · N996Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000345Floor Panel · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEVEL 2 CORROSION ON CABIN FLOOR PANEL #97. CORRECTIVE ACTION: REMOVED AND REPLACED SKIN ON FLOOR PANEL #97 IAW SERVICE ORDER 151063 AND TRAVLER T-5Jun 23, 2000 · N823AT · Doug DC932 · Fuselage Floor PanelSDR AT0000342Spar · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT ELEVATOR SPAR TO HAVE A CRACK AT BS 84.75. CORRECTIVE ACTION: FABRICATED AND INSTALLED REPAIR IAW EO 12-5520-29B1092 REV C.Jun 23, 2000 · N823AT · Doug DC932 · Elevator Control SystemSDR AT0000441Spar Cap · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT OUTBOARD LOWER SPAR CAP CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED ANGLE REPAIR IAW DC9 SRM 57-09 FIG 11 AND 51-10-03.Jun 23, 2000 · N817AT · Doug DC932 · Wing SparSDR AT0000353Spar · corrodedFOUND RIGHT HAND OUTBOARD LOWER SPAR CAP WAS CORRODED. REMOVED CORROSION, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 57-09 FIGURE 11, 51-10-3.Jun 23, 2000 · N817AT · Doug DC932 · Wing SparSDR TWAA0010006Longeron · crackedLONGERON 9L HAD A .5 INCH CRACK AT STA 598, UPPER FLANGE FASTENER AREA. REMOVED AND REPLACED CRACKED LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 12-14-99 STL.Jun 23, 2000 · N996Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00548Structure · corrodedMKE - SUB-FLOOR UNDER GALLEY NR 1 DRAIN PAN CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR. (X)Jun 22, 2000 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000356Skin · bulgedFOUND BULGING SKIN AT BS 917 - 935, L28R - L26. REMOVED AND REPLACED SKIN IAW REO L00232.Jun 22, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000355Skin · corrodedFOUND CORROSION AT BS 973, STRINGER 20 - 24 ON LEFT HAND SIDE. REMOVED CORROSION AND INSTALLED INTERNAL AND EXTERNAL DOUBLER IAW DC9 SRM 51-10-2, 51-30-2 AND REO L00230 REV B.Jun 22, 2000 · N817AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000352Attach Angle · corrodedFOUND AFT CARGO RIGHT HAND AFT BULKHEAD PANEL UPPER ATTACH ANGLE CORRODED. FORMED, FIT, TRIMMED, DRILLED, TREATED, AND PRIMED REPAIR ANGLE. INSTALLED ATTACH ANGLE IAW DCI SRM 51-10-2, 53-21-0 FIGURE 10, 51-10-4, 51-10-3.Jun 22, 2000 · N817AT · Doug DC932 · Fuselage Main, Attach FittingsSDR ABXA000331Intercostal · crackedDURING C-CHECK, FOUND THE FORWARD LOWER CARGO INTERCOSTAL WEB CRACKED. REPLACED FORWARD CARGO DOOR WEB IAW DC9 SRM 51-30-2.Jun 22, 2000 · N982AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA000309Splice · crackedDURING C-CHECK FOUND FLOOR SUPPORT TO INTERCOSTAL STRAP CRACKED AT STATION 737 OUTBOARD OF RIGHT BL 22. INSTALLED SPLICE IAW DC9 SRM 51-30-02.Jun 22, 2000 · N982AX · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0010405Web · corrodedDURING CHECK-C MAINT FOUND IN THE E/E BAY, FLOOR MEMBRANE WAS CORRODED AT STA 152, APPROX RBL 50 INCHES AT GALLEY DRAIN. REMOVED CORROSION PER SPM 6-80-1. INSTALLED DOUBLER PER SRM 53-01, FIG 2. TREATED AND PAINTED PER SRM 53-10-3. --CLOSED---Jun 22, 2000 · N924L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0010404Skin · damagedDURING OP 16 MAINT CHECK FOUND TOP OF LT WING WITH A CRACK APPROX 1 INCH LONG AT INBD FUEL TANK ENTRY MOUNT FLANGE (PLATE LANDING) NUMBER 1307. ACOMP EDDY CURRENT INSP PER NDT 51-00-03 CRACK CONTAINED. INSTALLED REPAIR DOUBLER PER ARA 16921. ---CLOSED---Jun 22, 2000 · N921L · Doug DC932 · Wing, Plate/SkinSDR AT0000343Skin · dentedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND SEVERAL DENTS AT BS 66-110 RIGHT. CORRECTIVE ACTION: COLD WORKED DENTS, FABRICATED AND ISTALLED DOUBLER IAW REO-L00222.Jun 21, 2000 · N823AT · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0010103Door Frame · crackedDURING OP 16 MAINT CHECK, THE FWD CARGO COMPT DOOR JAM LOWER AFT CORNER HAD 1.5 IN LONG CRACK IN FUSELAGE SKIN, AND 2.625 IN LONG CRACK IN DOUBLER. FUSELAGE SKIN AND DOUBLER REPLACED PER ARA 16930.Jun 21, 2000 · N921L · Doug DC932 · Fuselage Main, StructureSDR TWAA0009801Battery Pack · dischargedTHE LEFT OVERWING EMERGENCY LIGHT FAILED TO COME ON DURING TEST. REPLACED THE BATTERY PACK, (P/N MISC0639) AND BATTERY POWER SUPPLY (P/N 60-1177-9LB). CHECK-C 4-29-00 STL.Jun 21, 2000 · N922L · Doug DC932 · Emergency Lighting
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