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 VJ9800268Floorbeam · corrodedAFT PIT FLOORBEAM HAS CORROSION BEYOND LIMIT UNDER NUT PLATES AT FS 965, BL17L AND 19L. REMOVED AND REPLACED FLOORBEAM AND 2 Z-ANGLES IAW DC9 SRM 51-10-3, 51-10-4, 51-30-2, 51-30-5 AND 53-11-3. REINSTALLED, RIGGED AND OPS CHECKED STAB TRIM CABLES AND ENGINEJun 12, 1998 · N935VV · Doug DC932 · Fuselage Main, Floor BeamSDR VJ9800193Amplifier · failedEMERGENCY DESCENT PERFORMED BECAUSE AUTO PRESSURIZATION CONTROL INOP, MANUAL WAS OK. PASSENGER OXYGEN MASKS DEPLOYED. REPLACED OUTFLOW ACTUATOR AND RIGGED SUGAR SCOOP AS PRECAUTIONARY MEASURE AND REPLACED PRESSURE AMPLIFIER. PERFORMED TEST FLIGHT AND AUTO PRJun 12, 1998 · N966VV · Doug DC932 · Cabin Pressure Control SystemSDR TWAA9809705Tie · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND STR 30 CORRODED AT TIE CLIP, FS 167. REMOVED CORROSION IN STRINGER PER SRM 51-10-3, PARA 35, PAGE 21. REMOVED STRINGER TIE, DRILLED, DEBURRED, AND INSTALLED NEW TIE PER SRM 51-01, PAGE 1, ITEM C AND SRM 51-30-2, PAJun 12, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9809704Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND 2 EACH CRACKS AT STA 200, LONGERON 4L. REMOVED AND REPLACED 4L LONGERON FROM STA 128 TO STA 229. INSTALLED LONGERON REPAIR SPLICE AT STA 190, L4L, PER SRM 53-02, FIG 18. TOTAL TIME: 77,783 HOURS. TOTAL CYCLES: 8Jun 12, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9809703Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER CRACKED AT STA 180, LONGERON 3R. REPAIRED FORMER RING PER SRM 53-03, CLASS 1, FIG 4, PG 5. TOTAL TIME: 77,783 HOURS. TOTAL CYCLES: 84,471. X)Jun 12, 1998 · N998R · Doug DC932 · Fuselage Main, FrameSDR TWAA9809702Tie · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND STRINGER 29R CORRODED AT TIE CLIP, FS 167. REMOVED CORRODED TIE, ORDERED NEW TIE, DRILLED, DEBURRED, AND INSTALLED NEW TIE PER SRM 51-01, PAGE 1 ITEM C, AND SRM 51-30-2 PAGE 1. TOTAL TIME: 77,783 HOURS. TOTAL CYCLJun 12, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801101Floorpanel · crackedINSPECTION FOUND NR 42 LT CENTER FLOOR PANEL IN FORWARD PIT CRACKED AT FS 579 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 53-05, PAGE 1, AND 51-70-1.Jun 12, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801100Floorpanel · delaminatedINSPECTION FOUND FLOOR PANEL AT BS 365 TO 430 IN FORWARD PIT DELAMINATED. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND ECRA 2551-01010.Jun 12, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801099Floorboard · corrodedINSPECTION FOUND CORROSION ON NR 1 FLOORBOARD IN FORWARD PIT WITH DELAMINATION ON EDGES AT STA 218 TO 284. TWO HAT SECTIONS AND SIX NUT PLATE STRIPS WERE REMOVED. A FLOORBOARD WAS FABRICATED. THE FLOORBOARD, HAT SECTION, AND NUT PLATE STRIPS WERE INSTALLED Jun 12, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801055Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 980, LBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 53-05, FIGURE 20A, AND 51-30-2.Jun 12, 1998 · N12538 · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9801054Floor · crackedINSPECTION FOUND LT FLOOR MEMBRANE DISTORTED AND CRACKED AT STA 627 TO 657. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR WEB WAS FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-10-3, AND 51-30-2.Jun 12, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801053Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 740 TO 755, LONGERON 29L TO 29R. THE CORRODED AREA WAS CUT OUT, A REPAIR SPLICE DOUBLER AND EXTERNAL REPAIR SPLICE WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 53-04, FIGURE 42, AND 51-30-1.Jun 12, 1998 · N12538 · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800190Duct · failedDESENDING THRU FL320, CABIN BEGAN CLIMBING UNCONTROLLABLY. ENACTED EMERGENCY PROCEDURES AND DESCENDED TO FL 100. FOUND RT WATER SEPARATOR INLET DUCT BLOWN. REPLACED DUCT AND CHECKED IAW MM 21-20; NO LEAKS DURING GROUND TEST.Jun 11, 1998 · N946VV · Doug DC932 · Air Distribution SystemSDR TWAA9809419Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RIBS CRACKED, INBD AND OTBD SIDES OF OTBD HINGE CASTING ON RT WING TE FLAP. REPLACED RIBS, INBD AND OTBD OF HINGE CASTING PER SRM 51-01, PAGE 1 ITEM C. (X)Jun 11, 1998 · N995Z · Doug DC932 · Trailing Edge FlapsSDR CALA9801046Floor · crackedINSPECTION FOUND FLOORBOARD NR 82 HAT SECTIONS WORN THROUGH AND CRACKED. A FLOOR PANEL AND HAT SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-10-3, AND 51-30-2.Jun 11, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801045Floorbeam · gougedINSPECTION FOUND FLOORBEAM GOUGED AT STA 968. THE GOUGED SECTION OF FLOORBEAM WAS CUT OUT. AN L-ANGLE DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 20A, 53-05, 51-10-3, 51-30-2, AND 51-20-0.Jun 11, 1998 · N12538 · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9801044Cusp · corrodedINSPECTION FOUND CUSP CORRODED AT STA 980-996, RT SIDE. THE CORRODED SECTION OF CUSP WAS CUT OUT IAW SRM 53-05, FIGURE 25. A REPAIR CUSP WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 25 AND 51-30-2.Jun 11, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801022Web · corrodedINSPECTION FOUND CORROSION AROUND RIVETS IN WEB AT STA 218, STRINGER 18R. THE WEB WAS REMOVED, A REPAIR WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-10-2, 51-10-4, 51-30-2, AND 51-30.Jun 11, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801021Support · crackedINSPECTION FOUND THREE .5 INCH CRACKS IN FORWARD PIT RT FLOOR SUPPORT AT STA 332 ABOVE LONGERON 29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.Jun 11, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801020Floor · corrodedINSPECTION FOUND LT AFT LAV FLOOR WEB CORRODED AT BS 980 TO 996, LBL 18. THE FLOOR WEB WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, 51-10-3, AND 51-30-1.Jun 11, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801019Seat Track · corrodedINSPECTION FOUND RIGHT OUTBOARD SEAT TRACK CORRODED AT STA 908. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.Jun 11, 1998 · N12538 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800189Voltage Reg · failedNR 1 GENERATOR LIGHT OFF, UNABLE TO START APU INFLIGHT. REPLACED VOLTAGE REGULATOR.Jun 10, 1998 · N967VV · Doug DC932 · DC RegulatorSDR MWEA98674Longeron · dentedLONGERON 25L IS DENTED INWARD APPROXIMATELY .125 INCH AT STATION 452. MTC SPLICED IN NEW SECTION OF LONGERON.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98673Skin · dentedFUSELAGE SKIN IS DENTED AT FS 214 ABOVE LONGERON 21L AND AT STATION 218 BETWEEN LONGERON 24 AND 25L. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98672Skin · dentedTHE FUSELAGE SKIN IS DENTED AT FS 296 BETWEEN LONGERON 19 AND 20L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98671Skin · dentedTHE FUSELAGE SKIN IS DENTED AT FS 300 ABOVE AND BELOW LONGERON 23L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98670Skin · dentedFUSELAGE SKIN IS DENTED AT FS 351 AT LONGERON 22L. MTC FABRICATED AND INSTALLED DOUBLER.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98669Skin · dentedFUSELAGE SKIN IS DENTED AT FS 451 BELOW LONGERON 24L. MTC FABRICATED AND INSTALLED DOUBLER.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98668Longeron · crackedLONGERON 24L IS CRACKED AT FS 450. MTC SPLICED IN LONGERON SECTION.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98667Longeron · dentedLONGERON 23L IS DENTED AT FS 300. MTC SPLICED IN NEW LONGERON SECTION.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98666Longeron · dentedLONGERON 22L IS DENTED BETWEEN STATION 427 AND 446. MTC SPLICED IN LONGERON SECTION.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98665Shear Tie · crackedTHE SHEAR TIE CRACKED AT STATION 351 BETWEEN LONGERON 26L AND 27L. MTC SPLICED IN NEW SECTION.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98664Shear Tie · dentedTHE SHEAR TIE IS DENTED INWARD AT STATION 294 BETWEEN L20L AND L19L. MTC SPLICED IN NEW SECTION.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98663Skin · dentedTHE FUSELAGE SKIN IS DENTED AT FS 442 AT LONGERON 22L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98662Skin · dentedTHE FUSELAGE SKIN IS DENTED AT FS 370 ABOVE LONGERON 20L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98661Skin · dentedFUSELAGE SKIN IS DENTED AT FS 351 BELOW LONGERON 26L. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98660Skin · dentedFOUND SLIGHT DENT ON SKIN AT FS 294 BELOW LONGERON 25L. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.Jun 10, 1998 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801018Frame · crackedINSPECTION FOUND A .25 INCH CRACK AT FASTENER IN FRAME AT STA 1104, LONGERON 3R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.Jun 10, 1998 · N12538 · Doug DC932 · Fuselage Main, FrameSDR CALA9801017Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN L-ANGLE ON AFT ENTRY DOOR. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, 51-10-4, AND 51-30-2.Jun 10, 1998 · N12538 · Doug DC932 · Passenger/Crew DoorsSDR CALA9801016Seat Track · corrodedINSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 240. THE SEAT TRACK WAS REMOVED AND A NEW SECTION OF SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, 51-10-3, AND 53-05, FIGURE 4F.Jun 10, 1998 · N12538 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801015Support · crackedINSPECTION FOUND FLOOR SUPPORT CRACKED IN FORWARD PIT AT STA 351 ABOVE LONGERON 26R. THE FLOOR SUPPORT WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263 AND SRM 51-10-3.Jun 10, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9809418Frame · misdrilledMCI - DURING OP 15 MAINTENANCE CHECK, FOUND .3125 INCH HOLE IN TOP OF FORMER 36Z AT STR 29R, RBL 6. HOLE DRILLED FOR RIVNUT NO LONGER NEEDED. DID NDT CHECK FOR CRACKS. PLUGGED AND REPAIRED PER ARA 15285. (X)Jun 9, 1998 · N920L · Doug DC932 · Fuselage Main, FrameSDR TWAA9809417Intercostal · chafedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND INTERCOSTAL FS 980 TO FS 996 BETWEEN S27R AND S28R WITH APPROXIMATELY .25 INCH HOLE WORN INTO LIP. REPLACED AND INSTALLED NEW INTERCOSTAL PER SRM 51-01, PAGE 1 ITEM C. (X)Jun 9, 1998 · N920L · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98656Skin · corrodedRIGHT WING LOWER SKIN PANEL CORROSION AROUND FUEL PANEL NUMBER 1456. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR DOUBLER USING APPROVED DATA.Jun 9, 1998 · N215ME · Doug DC932 · Wing, Plate/SkinSDR MWEA98655Skin · corrosionRIGHT WING LOWER SURFACE FORWARD OF FUEL PANEL NUMBER 1460 HAS NUMEROUS AREAS OF CORROSION AROUND FASTENERS. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR DOUBLER USING APPROVED DATA.Jun 9, 1998 · N215ME · Doug DC932 · Wing, Plate/SkinSDR MWEA98654Doubler · crackedLEFT WING INTERNAL BEADED DOUBLER CRACKED AT STATION XO 198. MAINTENANCE ROUTED OUT CRACK AND INSTALLED REPAIR USING APPROVED DATA.Jun 9, 1998 · N215ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA98653Frame · dentedFRAME AT STA 945 BETWEEN LONGERON 28R AND 29R IS DENTED BEYOND SRM LIMITS. INSTALLED STACKED ANGLE REPAIR.Jun 9, 1998 · N215ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98652Jamb · corrodedTHE AFT CARGO DOOR JAMB PAN WAS FOUND CORRODED. MAINTENANCE REMOVED DAMAGED SECTION INSTALLED REPLACEMENT SECTION OF PAN USING APPROVED DATA.Jun 9, 1998 · N215ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98651Frame · damagedTHE FRAME AT FUSELAGE STATION 897 HAS ELONGATED FASTENER HOLES BETWEEN LONGERON 27L AND 29R. REPAIRED FRAME USING APPROVED DATA.Jun 9, 1998 · N215ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98650Skin · crackedPREVIOUS REPAIR AT STA 962 LONGERON 16R WAS REMOVED AND FOUND TO BE CRACKED. INSTALLED FILLER AND DOUBLER REPAIR OF FUSELAGE SKIN PANEL STA 945-96.Jun 9, 1998 · N215ME · Doug DC932 · Fuselage Main, Plate/Skin
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