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 VJ9800414Manifold · failedPAX O2 SYSTEM INOP. LEAKING O2 BOTTLE OFF FOR PAX SYSTEM. REMOVED AND REPLACED ROW 23B PSU MANIFOLD. RESTOWED MASK PIN IN AFT F/A MASK.Sep 20, 1998 · N921VV · Doug DC932 · Passenger Oxygen SystemSDR VJ9800413Battery Pack · dischargedF/A REPORTED LOOSE WIRES SHOWING FLOOR LIGHTS. INSTALLED LOOSE WIRES AND REPLACED PATHWAY BATTERY PACK FOR BLOWN FUSE, OPS CHECKED NORMAL.Sep 20, 1998 · N925VV · Doug DC932 · Emergency LightingSDR CA981019030Door · jammed(CAN) AT ARRIVAL GATE, FOUND LEFT MLG DOOR HANGING DOWN. FOUND DOOR JAMMED AND GEAR DOOR FOLLOW-UP EANCO CABLE JAMMING, AND FOLLOW-UP TORQUE TUBE RIVET SHEARED. PARTS REPLACED/REPAIRED. SYSTEM SERVICEABLE.Sep 20, 1998 · Doug DC932 · Landing Gear DoorsSDR CA981001007Actuator · failed(CAN) DURING TAKEOFF WHEN POWER APPLIED PRESSURIZATION CONTROL WAS HUNTING FOR PROPER POSITION. DURING CLIMB-OUT CABIN WAS MAX CLIMB, CABIN ALT SHOWED 2,500 FEET. LEVELLED OFF AT 7,000 FEET BUT NO CONTROL OVER PRESSURIZATION SYSTEM. REPLACED NR 1 CABIN CONTRSep 20, 1998 · Doug DC932 · Pressure Regulator/Outflow ValveSDR 9810079984Sensor · failedDURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW DECLINED A RED EMERGENCY AND CONFIRMED VISUALLY THAT NOSE GEAR WAS DOWN AND LOCKED. MAINTENANCE REPLACED NOSE GEAR DOWNLOCK PROXIMITY SENSOR. OPERATIONAL CHECK NORMAL.Sep 20, 1998 · N984US · Doug DC932 · Landing Gear Position and WarningSDR VJ9800538Fitting · corrodedAFT CABIN FLOORBEAM AT FS 996 RIGHT SIDE FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5, 51-10-4, 51-10-3 AND 53-01 FIG 1.Sep 19, 1998 · N911VV · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801836Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 160, LONGERON 26R. THE DENTED AREA WAS CUT OUT IAW ECRA 5331-01030. DOUBLERS AND FILLER WERE INSTALLED IAW ECRA 5331-01030, SRM 51-10-3 AND 51-30-2.Sep 19, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800432Floor · corrodedCOCKPIT FLOOR PANEL, RT, HAS CORRSION BEYOND LIMIT ON HAT SECTIONS. REMOVED CORRODED SKIN AND HAT SECTIONS. FABRICATED AND INSTALLED NEW FLOOR PANEL SKIN AND HAT SECTIONS IAW DC9 SRM 51-30-2, 51-20-0, 51-10-4, 51-10-3, AND 53-05..Sep 18, 1998 · N936VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800415R1Uplock Latch · lack of lubeLT GEAR UNSAFE LIGHT ILLUMINATED AFTER T/O WITH GEAR HANDLE UP, WHEN GEAR HANDLE PUT BACK DOWN, GEAR DOOR LIGHT ILLUMINATED. INSPECTED AND FOUND DOOR UPLOCK LATCH FROZEN. CLEANED AND LUBRICATED LATCH IAW MM 32-00. OPS CHECKED GOOD WITH GEAR SWING IAW 32-00.Sep 18, 1998 · N918VV · Doug DC932 · Landing Gear Position and WarningSDR VJ9800415Unsafe Light · illuminatedLT GEAR UNSAFE LIGHT ILLUMINATED AFTER T/O WITH GEAR HANDLE UP, WHEN GEAR HANDLE PUT BACK DOWN, GEAR DOOR LIGHT ILLUMINATED.Sep 18, 1998 · N918VV · Doug DC932 · Landing Gear Position and WarningSDR VJ9800589Floor · corrodedAFT PIT RT FLOOR PANEL AT FS 937 - 945 CORRODED BEYOND LIMIT IAW SRM 53-01, FIG 1. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-3, 53-01, FIG 1, 51-10-2, AND 53-21-0, FIG 10.Sep 17, 1998 · N924VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800559Skin · dentedDENTS BETWEEN FS 313 - 362, L23R - L25R, WERE DETERMINED TO BE TOO CLOSE TOGETHER IAW DC9 SRM 53-04, FIG 38, CONDITION 1B, NOTE 3. FABRICATED AND INSTALLED NEW SKIN FROM FS 229 - 389. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 51-30-1, 51-30-9, 51-Sep 17, 1998 · N936VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800547Panel · lightning strikeLIGHTNING STRIKE LT WINDOW PANEL AT 465 TO 484. REMOVED PANEL, CUT OUT SECTION, FABRICATED DOUBLERS AND FILLERS PLUS TWO INTERNAL DOUBLERS. INSTALLED REPAIR PARTS AND WINDOW PANEL IAW DC9 SRM 53-04 FIG 34.Sep 17, 1998 · N911VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800523Skin · crackedHFEC INSPECTION DETECTED A CRACK ON RT SIDE LONGERON AT FS 639 AND AT RT SIDE LONGERON 1 AT FASTENER HOLE. CUT OUT CRACKED AREA, APPROXIMATELY 10 INCHES IN DIAMETER AND CONFIRMED CRACK CONTAINED PER HFEC INSPECTION. CUT OUT CRACK, APPROXIMATELY.875 INCHES. Sep 17, 1998 · N936VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800517Longeron · crackedA CRACK AT FASTENER HOLE FS 617, L1R, DETECTED BY HFEC INSPECTION. CUT OUT CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-0, 51-10-3 AND SR 09530129.Sep 17, 1998 · N936VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800516Support · corrodedFLOORBEAM AT FS 160 TO 200, RBL 45, CORRODED BEYOND LIMIT ON TOP AND AROUND SCREW HOLES. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED NEW SECTION AT FLOOR SUPPORT IAW DC9 SRM 51-10-1, 51-10-3, 51-10-4 AND 51-30-2.Sep 17, 1998 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800512Window Panel · lightning strikeRT WINDOW PANE HAS LIGHTNING STRIKE OUT OF LIMIT AT FS 813 TO 869. REPLACED WINDOW PANEL IAW DC9 SRM 51-30-2, 51-10-4, 51-10-3 AND 53-05, FIG 111.Sep 17, 1998 · N911VV · Doug DC932 · Passenger Compartment WindowsSDR VJ9800479Spar · corrodedRT WING LOWER REAR SPAR XW 530 VERTICAL LEG CORRODED. FABRICATED, INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-1, 51-10-4, 53-22-1, AND AIRTRAN RES 981582.Sep 17, 1998 · N911VV · Doug DC932 · Wing SparSDR VJ9800431Seat Track · corrodedSEAT TRACK FS 965.091, 889, 852, 794 AND 617 HAVE GOUGES AND SEAT TRACK AT FS 965 CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC9 SRM51-10-4, 51-10-3, 51-60-0 AND 53-05, FIG 1.Sep 17, 1998 · N936VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA98966Cover · detachedFORWARD ENTRY DOOR EVACUATION SLIDE COVER PARTIALLY OFF. RESECURED FORWARD ENTRY DOOR EVACUATION SLIDE COVER.Sep 17, 1998 · N95 · Doug DC932 · Emergency EquipmentSDR MWEA98965Battery · dischargedCOCKPIT OVERHEAD PANEL EVACUATION LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY SUPPLY.Sep 17, 1998 · N501ME · Doug DC932 · Emergency LightingSDR MWEA98964Batteries · dischargedFORWARD ATTENDANT PORTABLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERIES.Sep 17, 1998 · N501ME · Doug DC932 · Emergency LightingSDR CALA9801813Skin · lightning strikeINSPECTION FOUND LIGHTNING STRIKE DAMAGE IN LT FUSELAGE SKIN AT STRINGER 25L, STA 246. THE DAMAGED AREA WAS CUT OUT, DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5331-01031.Sep 17, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801812Seat Track · corrodedINSPECTION FOUND FORWARD COCKPIT CO-PILOT'S SEAT TRACK CORRODED AT STA 203.9. THE SEAT TRACK WAS REMOVED AND REPLACED IAW MM 53-40-1.Sep 17, 1998 · N70542 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA9800878Bulkhead · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CANTED BULKHEAD AT FS 699 CORRODED BETWEEN LBL 22 AND LBL 54. FABRICATED NEW PANEL IAW DOUGLAS DRAWING NR 5956065 AND ABX REA D924-24804.Sep 17, 1998 · N903AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9800877Bulkhead · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT CANTED BULKHEAD AT FS 699 CORRODED BETWEEN RBL 22 AND RBL 44. FABRICATED NEW PANEL IAW DOUGLAS DRAWING NR 5956065 AND ABX REA D924-24804.Sep 17, 1998 · N903AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9800870Angle · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT WHEEL WELL SLANT PRESSURE PANEL LOWER ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE IAW DC9 SRM.Sep 17, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800869Angle · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT WHEEL WELL SLANT PRESSURE PANEL LOWER ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE IAW DC9 SRM.Sep 17, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800863Skin · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE UPPER SURFACE OF THE CENTER WING TANK CORRODED AT REAR SPAR AT STATION XCW20. REPAIRED UPPER SKIN SURFACE IAW ABX REA D957-24799MR.Sep 17, 1998 · N903AX · Doug DC932 · Wing, Plate/SkinSDR ABXA9800835Tee · corrodedILN - DUIRNG C-CHECK, FOUND CUSP TEE ANGLES AT LONGERON 18R AND STA 946 - STA 980 CORRODED ON LOWER SIDE. REPAIRED IAW DC9 SRM 53-05. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800834Web · corrodedILN - DURING C-CHECK, FOUND CUSP WEB CORRODED AT STA 965 BETWEEN RBL 44 ND RBL 54.5, IN LIGHTENING HOLE AREA BETWEEN STA 945 - STA 965. REPAIRED CUSP WEB IAW ABX REA D953-24862-MR. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800833Fitting · crackedILN - DURING C-CHECK, FOUND LOWER LEFT VENTRAL DOOR STOP SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND SRM 51-30-5. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Passenger/Crew DoorsSDR ABXA9800832Frame · corrodedILN - DURING C-CHECK, FOUND FUSELAGE FRAME AT STA 180 AND LONGERONS 22R- 27R CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9800831Floorbeam · crackedILN - DURING C-CHECK, FOUND UPPER SURFACE OF FLOORBEAM STA 965 RBL 8.0 TO RBL 21 CORRODED. REPAIRED IAW DC9 SRM 51-10-32 AND DWG K05019. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9800830Frame · crackedILN - DURING C-CHECK, FOUND FUSELAGE FS 980 CRACKED AT LONGERON 17R. REPAIRED FRAME IAW DC9 SRM 53-03. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9800829Skin · crackedILN - DURING C-CHECK, FOUND NR 2 ADF LOOP ANTENNA AREA EXTERIOR FUSELAGE SKIN CRACKED AROUND HOLE FOR ANTENNA LEAD WIRE. REPAIRED SKIN IAW ABX REA D953-24811-MR. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9800828Angle · crackedILN - DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE OUTBOARD INTERIOR ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND SRM 51-30-2. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)Sep 17, 1998 · N939AX · Doug DC932 · Trailing Edge FlapsSDR 9810759926Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.Sep 17, 1998 · N926NW · Doug DC932 · Emergency LightingSDR VJ9800575Seat Track · corrodedFLIGHT ATTENDANT SEAT FLOOR MOUNT AT FS 163, LBL 16, CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW DC9 SRM 53-01 PG 10 AND 6 AND 51-10-3.Sep 16, 1998 · N936VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800574Mount · corrodedFORWARD AIRLOCK ROD MOUNT PAD CORRODED AT FS 160, RBL 10. REMOVED PAD, FABRICATED AND INSTALLED ROD MOUNT PAD IAW DC9 SRM 51-10-3 AND 53-01 FIG 1.Sep 16, 1998 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800548Bulkhead Doubler · corrodedUPPER RT DOUBLER AT BULKHEAD WEB FS 996 CORRODED. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW DC9 SRM 51-10-3, 51-10-2 AND 53-02 FIG 2.Sep 16, 1998 · N911VV · Doug DC932 · Fuselage Main, BulkheadSDR VJ9800545Hinge · corrodedFWD PSGR DOOR UPPER HINGE CORRODED AND COATING MISSING. REPLACED UPPER DOOR HINGE IAW DC9 SRM 51-30-2, OHM 52-11-1 AND MM 52-71-0.Sep 16, 1998 · N936VV · Doug DC932 · Passenger/Crew DoorsSDR VJ9800515Support · corrodedSUB FLOOR AT FS 187, LBL22, CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED NEW SUB FLOOR AND FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-10-4, AND 51-10-3.Sep 16, 1998 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800448Support · corrodedFLOOR SUPPORT UNDER NUT PLATES AT FS 160 - 190, LBL 44, CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-30-2, 51-30-5, 51-10-2, 51-10-4 AND 53-01 FIG 1.Sep 16, 1998 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800862Web · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CUSP WEB CORRODED BETWEEN FS 237 TO FS 313. REPLACED CUSP WEB IAW DC9 SRM CHAPTERS 61-30-1 AND 51-30-5.Sep 16, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800860Web · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CUSP WEB BETWEEN FS 200 AND 218 CORRODED. REPLACED CUSP WEB IAW DC9 SRM CHAPTERS 51-30-2 AND 51-30-5.Sep 16, 1998 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800573Floor · corrodedFLOOR PANEL LOCATED BETWEEN #3 GALLEY AND FORWARD FLIGHT ATTENDAANT SEAT, FS 200.0, CORRODED. REMOVED CORROSION, FABRICATED AAND INSTALLED REPAIR FLOOR PANEL IAW DC9 SRM 51-10-3, 53-21-0, AND 51-30-1.Sep 15, 1998 · N936VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800558Angle · crackedA .75 INCH CRACK FOUND IN STIFFENER AT FS 598 RT SIDE OF FUSELAGE AT FORWARD SECTION OF WING TO FUSELAGE FILLET INTERIOR. REMOVED FILLET AND SKATE ANGLE. FABRICATED AND INSTALLED REPAIR FILLET, INSTALLED NEW SKATE ANGLE IAW DC9 SRM 51-30-2, 51-10-2, 51-10-4,Sep 15, 1998 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800474Support · corrodedFWD PIT FRAME FS 522, L24L-30, CORRODED. FABRICATED REPAIR FLOOR SUPPORT 7075-0, .063, HEAT TREATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-10-4, 51-10-2A, 53-21-0, 51-3-2 AND RES 981418.Sep 15, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800473Doubler · corrodedBULKHEAD SKIN AT STA 600, L28L-28R, CORRODED. FORMED FILLER AND DOUBLERS, TREATED, PRIMED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-3, 51-20, 51-30 AND ROD SKETCH 98-09-04-010.Sep 15, 1998 · N933VV · Doug DC932 · Fuselage Miscellaneous Structure
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