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 VJ9800283Frame · corrodedCORROSION BEYOND LIMIT AT FS 522, 28L-28R. REMOVED FASTENERS TO ACCESS CORRSION IAW DC9 SRM 51-10-3. TREATED AND PRIMED AREA IAW DC9 SRM 53-01 FIG 1. TREATED AND PRIMED AREA IAW DC9 SRM 51-10-3 AND REPLACED FASTENERS IAW DC9 SRM 51-30-2 AND 51-30-5.Jul 29, 1998 · N902VJ · Doug DC932 · Fuselage Main, FrameSDR TWAA9812514Skin · corrodedDURING OP 16 MAINT CHECK, FOUND FUSELAGE CORROSION CLEAN UP BEYOND MANUAL LIMITS, 30 PERCENT REMOVED, AT FS 993, LONGERON 29L ON FUSELAGE SKIN. REPAIRED DAMAGED AREA BY BLENDING OUT AREA AND INSTALLING A DOUBLER PER SRM 53-04, FIG 38 PAGE 209, CONDITION 3.Jul 29, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9812513Skin · corrodedDURING OP 16 MAINT CHECK, FOUND ON LOWER FUSELAGE CORROSION AND FASTENER HEADS MISSING AT LOWER FWD CORNER OF THE AFT LAV DUMP SERVICE DOOR. CUT OUT CORRODED MATERIAL FOR REPAIR PER ACFT SRM 51-10-03. REPAIRED PER ARA 15367 PAGE 1 OF 1.Jul 29, 1998 · N995Z · Doug DC932 · Service DoorsSDR MWEA98827Splice · crackedFOUND AFT CARGO COMPARTMENT LONGERON SPLICE AT 28L AND FS 837 CORRODED AND CRACKED ON AFT END. MX FABRICATED AND INSTALLED LONGERON SPLICE.Jul 29, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98826Splice · corrodedFOUND CORROSION ON AFT CARGO COMPARTMENT FRAME SPLICE AT FS 908 UNDER NUT PLATE AT LONGERON 28L. MX FABRICATED AND INSTALLED NEW SUPPORT SPLICE.Jul 29, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98825Fitting · crackedFOUND CRACK ON END FITTING AT LONGERON 23L AT STATION 990. MX FABRICATED AND INSTALLED NEW END FITTING.Jul 29, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801368Floorbeam · corrodedINSPECTION FOUND CORROSION AROUND FLOORBEAM NUT PLATES AT RT AFT LAV, STA 980, APPROXIMATELY 18 INCHES FROM RT SIDE OF FUSELAGE. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIGURE 20A.Jul 29, 1998 · N14534 · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9801365Splice · corrodedINSPECTION FOUND FLOOR PANEL SPLICE PLATE IN AFT CARGO PIT AT STA 935 CORRODED. A NEW FLOOR PANEL SPLICE PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.Jul 29, 1998 · N15525 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801364Panel · gougedINSPECTION FOUND RT WING LEADING EDGE PANEL NR 1248 GOUGED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-01, FIGURE 3, 51-10-3, AND 51-30-2.Jul 29, 1998 · N15525 · Doug DC932 · Wing, Plate/SkinSDR CALA9801363Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN ANGLE TO RT WING INBOARD BUTE DOOR STIFFENER ATTACHMENT POINT. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, FIGURE 1.Jul 29, 1998 · N15525 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9801362Floor · crackedINSPECTION FOUND AFT CARGO FLOOR PANEL AT STA 756-935 CRACKED AND WORN IN SEVERAL PLACES. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0.Jul 29, 1998 · N15525 · Doug DC932 · Fuselage Floor PanelSDR ABXA9800736Floorbeam · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON UPPER FLOORBEAM CAP FS 965. FABRICATED REPAIR STRAP AND REPAIR ANGLE IAW ABX REA D 953 24462 MR AND INSTALLED REPAIR IAW ABX REA D 953 24462 MR.Jul 29, 1998 · N983AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9800671Spring · weakDURING PREFLIGHT WAS UNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW. REPLACED AFT LOWER LATCH HOOK RETURN SPRING AND LUBRICATED WINDOW.Jul 29, 1998 · N988AX · Doug DC932 · Flight Compartment WindowsSDR VJ9800375Doubler · corrodedFLOOR SUPPORT DOUBLERS CORRODED UNDER STA 889-908 LONGERON 29L-27L. FABRICATED SUPPORT DOUBLER FROM 7075 T6 .063 3.5 BY 3. INSTALLED REPAIR IAW DC-9 SRM 51-10-3, 53-01 FIG 1 AND 51-30-1.Jul 28, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800374Splice · corrodedLONGERON 30 SPLICE CORRODED OUT OF LIMITS, STA 794-813. REMOVED SPLICE IAW SRM 51-30-2, REMOVED CORROSION IAW SRM 51-10-3, MATERIAL LOSS .030 IAW AERO CORP GAUGE NR A-2039, OUT OF LIMITS IAW SRM 53-01 FIG 1. SPLICE P/N 3914677-501N, DRILLED AND DEBURRED NEWJul 28, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800320Skin · crackedDURING ACCOMPLISHMENT OF AD 88-24-08 INSPECTION PER EO-12-29-B1058I/R, HFEC INDICATES EXTERNAL FUS SKIN CRACK .100 AT COUNTERSUNK FASTENER HOLE COMMON TO FS 617 RT LONG 1 SHEAR TIE. REMOVED FASTENER, VERIFIED CRACK IN SKIN AT COUNTERSUNK, REMOVED FAST, CUT OUJul 28, 1998 · N945VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800273Skin · corrodedINTERNAL SKIN IN FWD PIT CORRODED AT STA 579. REMOVED END CAPS FROM 25L TO 25R, FRAME AND SHEAR TIES AT STA 579 AND CORROSION IAW DC9 SRM 51-10-3. FABRICATED AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW DC9 SRM 53-04, FIG 43, AND RES 981100. REPLACED CRJul 28, 1998 · N902VJ · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800269Longeron · corrodedSPLICE CORRODED BEYOND LIMIT AT STA 794 TO 813, L30. REMOVED SPLICE AND CORROSION IAW DC9 SRM 51-30-2 AND 51-10-3. ORDERED NEW SPLICE, DRILLED, DEBURRED AND INSTALLED SPLICE IAW DC9 SRM 51-10-4, 51-30-5.Jul 28, 1998 · N912VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9812512Intercostal · crackedDURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CRACKED 3 INCHES FWD OF STA 294, AT ZERO BL. FABRICATED NEW INTERCOSTAL FROM 2024-0 ALUM MATERIAL HEAT TREATED TO 2024T3 PER REMOVED INTERCOSTAL. INSTALLED IN ACFT USING HI-LOKS AND MS20470AD RIVETS, PER DOUGLAS PRJul 28, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801360Clip · crackedINSPECTION FOUND A 2 INCH CRACK IN CLIP AT STA 1109, LONGERON 2R. THE CLIP WAS REPLACED IAW SRM 51-60-0.Jul 28, 1998 · N14534 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801351Bulkhead Tee · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT PRESSURE BULKHEAD TEE CAP AT RT LAV BETWEEN LONGERON 15R AND 16R, STA 996. THE TEE CAP WAS REPLACED IAW SRM 53-03, FIGURE 37A.Jul 28, 1998 · N14534 · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9800739Stringer · corrodedDURING C-CHECK, FOUND STRINGER 14 CORRODED. REPAIRED IAW ABX REA D 957 24455 MR.Jul 28, 1998 · N983AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800738Stringer · corrodedDURING C-CHECK, FOUND STRINGER 15 CORRODED. REPAIRED IAW ABX REA D 957 24455 MR.Jul 28, 1998 · N983AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9800735Stringer · corrodedDURING C-CHECK, FOUND STRINGER 16 CORRODED. REPAIRED IAW ABX REA D 957 24455 MR.Jul 28, 1998 · N983AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9809859620Sensor · failedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO OKC. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT TAIL COMPARTMENT TEMPERATURE SENSOR. OPERATIONAL CHECK NORMAL.Jul 28, 1998 · N620NW · Doug DC932 · Overheat DetectionSDR VJ9800280Angle · crackedSPAR CAP XRS AT INBRD FLAP HINGE STUD HOLE HAS A .25 INCH CRACK ON FWD FACE RUNNING VERTICALLY FROM TOP EDGE OF HOLE. FABRICATED ANGLE FROM 2024, 26 1/4 BY 3 INCHES. LOCATED AND DRILLED TWO OTHER ANGLES. INSTALLED REPAIRS IAW DC9 SRM 51-30-5 AND DWG J0602T1Jul 27, 1998 · N912VV · Doug DC932 · Wing Miscellaneous StructureSDR VJ9800240Bungee Cylinder · failedMAIN LANDING GEAR RT UNSAFE LIGHT ON WITH DOOR WARNING LIGHT. AIRCRAFT AIR RETURNED. REMOVED AND REPLACED RT MLG BUNGEE CYLINDER GEAR SWING IAW 32-30-0.Jul 27, 1998 · N947VV · Doug DC932 · Landing Gear Retraction/Extension SystemSDR MWEA98824Longeron · corrodedFOUND CORROSION ON LONGERON 27L AT STATION 218. MTC FABRICATED AND INSTALLED NEW LONGERON SPLICE.Jul 27, 1998 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98823Beam · crackedFOUND CRACK ON AFT END OF PASSENGER DOOR NUMBER ONE BEAM. MTC FABRICATED AND INSTALLED DOUBLER AND REPLACED DOOR STOP ASSEMBLY.Jul 27, 1998 · N209ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA98822Angle · crackedFOUND CRACK ON LEFT PYLON LOWER AFT BOX CORNER ANGLE. MTC FABRICATED AND INSTALLED REPAIR ANGLE.Jul 27, 1998 · N209ME · Doug DC932 · Nacelle/Pylon StructureSDR MWEA98821Pan · crackedFOUND CRACK IN UPPER FORWARD CORNER PASSENGER DOOR PAN. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS.Jul 27, 1998 · N209ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA98820Trap Panel · crackedFOUND CRACK ON LEFT TRAP PANEL UPPER OUTBOARD FLANGE FROM FORWARD EDGE TO JUST PAST THE THIRD BOLT HOLE. MTC TRIMMED TO FOURTH HOLE.Jul 27, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98819Skin · dentedFOUND THREE DENTS ON AFT FUSELAGE SKIN FROM FS 935 TO 965 BETWEEN LONGERON 24R TO 25R. MTC FABRICATED AND INSTALLED DOUBLERS.Jul 27, 1998 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801350Pan · crackedINSPECTION FOUND A .5 INCH CRACK AT UPPER RADIUS OF MAIN CABIN DOOR PAN UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 33.Jul 27, 1998 · N14534 · Doug DC932 · Passenger/Crew DoorsSDR CALA9801349Bulkhead Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN RT LAV ANGLE, LOWER SIDE OF Z-63 FROM END FASTENER AT AFT PRESSURE BULKHEAD. THE ANGLE WAS REPAIRED IAW SRM 51-30-5.Jul 27, 1998 · N14534 · Doug DC932 · Fuselage Main, BulkheadSDR CALA9801348Bulkhead Fitting · crackedINSPECTION FOUND A 3 INCH CRACK IN TIE FITTING ON FORWARD SIDE OF BS 69 BULKHEAD AT TOP OF LT INTERCOSTAL AND A 3 INCH CRACK WAS FOUND IN TIE FITTING ON FORWARD SIDE OF BS 69 BULKHEAD AT TOP OF RT INTERCOSTAL. THE TIE FITTINGS WERE REMOVED AND REPLACED IAW SRJul 27, 1998 · N14534 · Doug DC932 · Fuselage Main, BulkheadSDR CALA9801345Skin · dentedINSPECTION FOUND LT LEADING EDGE SLAT NR 1 SKIN DENTED AT STA XIS 136 AND XIS 132. REPAIRED IAW SRM 57-09, FIGURE 10 AND 10A.Jul 27, 1998 · N18544 · Doug DC932 · Leading Edge DevicesSDR 9809849916Fitting · leakingDURING CRUISE FLIGHT, RIGHT HYDRAULIC SYSTEM QUANTITY DROPPED TO 4 QUARTS. FLIGHT CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FITTING LEAKING AT RIGHT WHEEL WELL PRIORITY VALVE. REPLACEJul 27, 1998 · N949N · Doug DC932 · Hydraulic System, MainSDR VJ980238Cover · looseR1 DOOR EMERGENCY EVACUATION SLIDE CAME LOOSE FROM DOOR. INSTALLED SLIDE COVER LANYARD PINS IAW 25-62-0. NO OTHER DEFECTS NOTED.Jul 26, 1998 · N935VV · Doug DC932 · Emergency EquipmentSDR VJ9800239Sensor · dirtyRIGHT MLG RED UNSAFE LIGHT ALONG WITH DOOR WARNING LIGHT. AIRCRAFT AIR RETURNED. FOUND RT MLG UPLOCK SENSOR DIRTY AND PAINTED OVER. CLEANED SENSOR AND OPS CHECKED GOOD.Jul 26, 1998 · N947VV · Doug DC932 · Landing Gear Position and WarningSDR TWAA9812507Skin · crackedDURING OP 16 MAINT CHECK, FOUND SKIN CRACKED AT STA 192, STR 22L, .1875 IN LONG AT 10 O'CLOCK. REMOVED CRACK PER SRM 53-04, P33 NOTE NR 1. INSTALLED REPAIR PER MO 71N61 PHASE A.Jul 26, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800244Intercoastal · corrodedDURING C CHECK, FOUND INTERCOASTAL CORRODED BETWEEN STA 332 AND 351 LEVEL 2. REMOVED INTERCOASTAL FOUND TO BE OUT OF LIMITS. FABBED AND FORMED NEW INTERCOASTAL 19.5 X 1 X .5 X 27/8 FROM 7075 .050. HEAT TREATED TO 7075-T6 .050. TRIMMED TO FIT, DRILLED, DEBUJul 24, 1998 · N902VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800237Battery · dischargedAFT OVERHEAD CABIN EMERGENCY LIGHTS INOP. REPLACED EMERGENCY POWER SUPPLY BATTERIES PER MM 33-50. OPS CHECK GOOD.Jul 24, 1998 · N967VV · Doug DC932 · Emergency LightingSDR CALA9801344Skin · dentedINSPECTION FOUND A DENT IN LT LOWER WING SKIN AT XRS 530. THE AREA WAS REPAIRED IAW SRM 57-03, PAGE 23.Jul 24, 1998 · N18544 · Doug DC932 · Wing, Plate/SkinSDR CALA9801343Skin · corrodedINSPECTION FOUND LT AND RT WHEEL WELL KEEL SKIN AREA CORRODED AT STA 680 TO 756. THE CORRODED SECTION OF KEEL SKIN WAS REMOVED IAW SRM 53-04, FIGURE 42. A NEW SECTION OF SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 53-04, FIGURE 4Jul 24, 1998 · N18544 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801342Longeron · corrodedINSPECTION FOUND LONGERON 22L CORRODED AT STA 150. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 18 PAGE 48.Jul 24, 1998 · N14534 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801341Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN FUSELAGE CROWN SKIN AT STA 718, LONGERON 1L. THE CRACKED AREA WAS CUT OUT, INTERNAL AND EXTERNAL DOUBLERS WERE INSTALLED IAW ECRA 5330-02688.Jul 24, 1998 · N14534 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801340Skin · corrodedINSPECTION FOUND FUSELAGE BELLY SKIN TORN WITH CORROSION AT STA 794, LONGERON 30. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B PAGE 39.Jul 24, 1998 · N14534 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801332Beltframe · corrodedINSPECTION FOUND BELTFRAME CORRODED AT STA 148, LONGERON 26L. THE CORROSION WAS CUT OUT AND A BELTFRAME REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 2.Jul 24, 1998 · N14534 · Doug DC932 · Fuselage Main, FrameSDR ABXA9800660Stiffener · crackedWHILE COMPLYING WITH C INSPECTION, FOUND STATION 965 LONGERON L17 CRACKED UNDER SPLICE STIFFENER. REPAIRED IAW DC-9 SRM AND DWG K05864.Jul 24, 1998 · N983AX · Doug DC932 · Fuselage Miscellaneous Structure
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