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 9804649983Windshield · failedDURING CLIMB-OUT, AN ELECTRICAL ARC OCCURRED AT FIRST OFFICER'S WINDSHIELD WITH WINDSHIELD HEAT TURNED OFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDHSIELD, HEAT CONTROLLER, AND ASSOCIATED WIRING. OPERATIONAL CHECMar 18, 1998 · N983US · Doug DC932 · Flight Compartment WindowsSDR TWAA9809108Floorbeam · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOORBEAM CAP AT FS 160 TO 196, RBL 44, CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBEAM PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9809106Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK IN FORWARD FUSELAGE INTERCOSTAL TO FS 69.55 FORMER ATTACH 'T' ANGLE AT LBL 13 INCH. REPLACED 'T' ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 17, 1998 · N929L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9809104Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK,F OUND DENT ON LEFT SIDE BELOW AFT CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1 INCH BY .045 INCH DEEP. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 18. (M)Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9809103Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN LEFT SIDE BELOW FORWARD CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1.25 INCH BY .055. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 18. (M)Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9807206Angle · crackedDURING OP 15 MAINTENANCE CHECK, FOUND AT RT STATION 980, FORMER RING TO FUSELAGE ATTACH ANGLE CRACKED AT 2 PLACES JUST BELOW LONGERON 15R. FORMER FOOT FORMED AND HEAT TREATED TO 7075 PER SRM 51-102A. INSTALLED NEW FORMER FOOT SECTION PER SRM 51-01, PAGE 1 ITMar 17, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9807203Skin · dentedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN BEYOND LIMITS AT FS 503 BETWEEN L27 AND L38R, 5.5 INCH BY 2.5 INCH BY .175. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9807104Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON TO CANTED KEEL FORMER TIE CRACKED AT STA 637, APPROX 15 LBL. REPLACED TIE PER SRM 51-01, PAGE 1 ITEM C. SEALED REPAIR PER SRM 51-20-0. (X)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9807103Skin · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND TEMPORARY REPAIR ON OUTER FUSELAGE SKIN AT STA 965, BETWEEN LONGERON 13 AND 14 RT SIDE. REPAIRED PER SRM 53-04, FIG 32, AND TWA STD PRACTICES. (X)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9806912Doubler · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON LONGERON 26L AT STATION 902 'FINGER DOUBLER'. REPLACED FINGER DOUBLER PER SRM 51-01, PAGE 1 ITEM C. REMOVED CORROSION PER SRM 51-10-3. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806910Floor · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED BETWEEN STATION 560 AND 579, APPROX 58 INCH RBL, UNDER AFT END OF FLOOR PANEL 37. REPAIRED PER SRM 53-01, FIG 4. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Floor PanelSDR TWAA9806909Floor · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED BETWEEN STATION 579 AND 598, APPROX 58 INCH RBL, UNDER FWD END OF FLOOR PANEL 43. REPAIRED PER SRM 53-01, FIG 4. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Floor PanelSDR TWAA9806908Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 13R CRACKED AT STATION 1076. REPLACED LONGERON PER SRM 51-03, PAGE 1 ITEM C. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9806907Longeron · crackedDURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 27R CRACKED AT STATION 541. REMOVED AND REPLACED WITH NEW PART PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 17, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98379Girt Bar · lack of lubeTHE RIGHT GALLEY GIRT BAR IS DIFFICULT TO PUT IN THE ARMED POSITION. MTC CLEANED AND LUBED GALLEY DOOR GIRT BAR.Mar 17, 1998 · N207ME · Doug DC932 · Emergency EquipmentSDR MWEA98369Battery Pack · dischargedTHE EMERGENCY LIGHTS AT ROW 15 TO 18 COME ON WHEN POWER IS OFF AND EMERGENCY LIGHT SWITCH IS IN OFF POSITION. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY.Mar 17, 1998 · N207ME · Doug DC932 · Emergency LightingSDR MWEA98368Battery Pack · dischargedFOUND LT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK POWER SUPPLY.Mar 17, 1998 · N207ME · Doug DC932 · Emergency LightingSDR 9804539601Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Mar 17, 1998 · N601NW · Doug DC932 · Emergency LightingSDR MWEA98367Battery Pack · dischargedFOUND 3 AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK POWER SUPPLY.Mar 16, 1998 · N207ME · Doug DC932 · Emergency LightingSDR MWEA98349Slide Cover · fell offTHE GALLEY SERVICE DOOR SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER.Mar 16, 1998 · N502ME · Doug DC932 · Emergency EquipmentSDR 9804499615Connector · damagedLOSS OF CABIN PRESSURE OCCURRED DURING CRUISE FLIGHT AT 31,000 FEET. CABIN PRESSURE WARNING LIGHT ILLUMINATED WITH DROP IN DIFFERENTIAL PRESSURE. CREW INITIATED RAPID DESCENT TO 15,000 FEET AND FLIGHT WAS CONTINUED TO DESTINATION. CABIN RPESSURE STABILIZED Mar 16, 1998 · N615NW · Doug DC932 · Cabin Pressure Control SystemSDR CA980402007Engine · power loss(CAN) ON TAKEOFF POWER LEVERS BROUGHT TO 1.4 EPR FOR RUN-UP, ALL OKAY. AT APPROXIMATELY 85-95 KNOTS, NR 2 ENGINE HAD A POWER LOSS AND THE EGT INITIALLY AT 700C, WENT TO 800 C. ENGINE WAS SHUTDOWN AND FIRE TRUCKS WERE CALLED. THE NR 2 ENGINE WAS REPLACED. RESULMar 15, 1998 · Doug DC932 · Engine (Turbine/Turboprop)SDR VJ9800328Floor · corrodedF/O'S FLOOR PANEL NR 14 CORRODED BEYOND LIMITS IAW SRM 53-01 FIG 1 PG 8. MATERIAL LOSS 100 PERCENT. FORMED NEW FLOOR PANEL FROM 7075 T6 .040 CLAD IAW DC-9 SRM 51-10-2, 51-10-4, TREATED AND PRIMED PANEL IAW SRM 51-10-3.Mar 15, 1998 · N903VJ · Doug DC932 · Fuselage Floor PanelSDR VJ9800048Battery Pack · dischargedEMERGENCY FLOOR PATH LIGHTING, SECTION 3, INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-51, OPS CHECKED NORMAL.Mar 15, 1998 · N939VV · Doug DC932 · Emergency LightingSDR TWAA9803702Radome · puncturedMSY - FLT 8689 - CREW REPORTED LOUD BANG FROM NOSE OF AIRCRAFT, MADE UNSCHEDULED LANDING AT MSY. FOUND BIRD STRIKE TO RADOME AT 9 O'CLOCK POSITION. REPLACED RADOME AND REPAIRED METAL DAMAGE AT THE JOINT BETWEEN RADOME AND FUSELAGE. CHECK-C 2-11-98 STL. (M)Mar 15, 1998 · N923L · Doug DC932 · Aerodynamic FairingsSDR TWA9803704Batteries · dischargedSTL - FLT 218 - DURING PREFLIGHT, ONE SECTION OF OVERHEAD EMERGENCY LIGHTS IN COACH WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER PACK B-2. CHECK-C 8-6-97 MCI. (M)Mar 15, 1998 · N924L · Doug DC932 · Emergency LightingSDR CA990203014Compressor · damaged(CAN) ON TAKEOFF, POWER LEVERS BROUGHT TO 1.4 EPR FOR RUN-UP, ALL OKAY. AT APPROXIMATELY 85-95 KNOTS, THE NR 2 ENGINE HAD A POWER LOSS. EGT INITIALLY AT 700 CELCIUS, ON SHUTDOWN EGT AT 800 CELSIUS. FIRE TRUCKS CALLED. INSPECTION FOUND HEAVY DAMAGE TO THE HMar 15, 1998 · Doug DC932 · Turbine Engine Compressor SectionSDR 9807459941Floorbeam · crackedDURING M CHECK, FOUND CRACK IN FLOORBEAM UPPER FLANGE AT FS 321 JUST OUTBOARD OF CENTERLINE. REPAIRED PER EA 99-154774.Mar 14, 1998 · N3324L · Doug DC932 · Fuselage Main, Floor BeamSDR 9805579920Doubler · crackedDURING L CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD VENTRAL DOOR CUTOUT LEFT -9 DOUBLER. REPAIRED PER EA 99-1562620.Mar 14, 1998 · N942N · Doug DC932 · Fuselage Main, BulkheadSDR 9804349615Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND BOTH FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Mar 14, 1998 · N615NW · Doug DC932 · Emergency LightingSDR 9804329608Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTS BETWEEN ROWS 11 THRU 13 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Mar 14, 1998 · N608NW · Doug DC932 · Emergency LightingSDR VJ9800170Battery Tray · corrodedE/E COMP BATTERY TRAY LT SIDE HAS CORROSION. REMOVED CORROSION IAW DC-9 SRM 51-10-3 MATERIAL LOSS WAS FOUND TO BE 100 PERCENT, OUT OF LIMITS IAW IAW DC-9 SRM 53-01 FIG 1. FABRICATED DOUBLER REPAIR FROM 2004 T3 .875 BY 1.875 X 3.875 IAW DC-9 SRM 53-01 FIG 2. Mar 13, 1998 · N967VV · Doug DC932 · Battery Box StructureSDR VJ9800147Battery Tray · corrodedBATTERY TRAY, LT SIDE, IN E/E COMPARTMENT CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. REMOVED CORROSION IAW DC9 SRM 51-10-3. FABRICATED DOUBLER REPAIR FROM 2024T3, 7/8 BY 13/8 BY 35/8 INCHES, IAW DC9 SRM 53-01, FIG 2. TREATED, PRIMED AND INSTALLED IAW Mar 13, 1998 · N967VV · Doug DC932 · Battery Box StructureSDR VJ9800047Slide · dislodgedMAIN CABIN PASSENGER EMERGENCY DOOR SLIDE DISLODGED. REINSTALLED SLIDE COVER IAW DC9 MM 25-60, ACCOMPLISHED REQUIRED INSPECTIONS.Mar 13, 1998 · N918VV · Doug DC932 · Emergency EquipmentSDR MWEA98348Slide · fell offTHE GALLEY DOOR SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE.Mar 13, 1998 · N209ME · Doug DC932 · Emergency EquipmentSDR MWEA98346Slide · fell offGALLEY SERVICE DOOR EVACUATION SLIDE FELL OFF. REINSTALLED GALLEY SERVICE DOOR EVACUATION SLIDE.Mar 13, 1998 · N209ME · Doug DC932 · Emergency EquipmentSDR 9804389921Slide · low pressureDURNG MAINTENANCE INSPECTION, FOUND TAIL CONE EVACUATION SLIDE BOTTLE LOW ON PRESSURE. REPLACED SLIDE.Mar 13, 1998 · N943N · Doug DC932 · Escape SlideSDR 9804339608Connection · looseDURING PERIODIC CHECK, FOUND EMERGNECY LIGHTS BETWEEN ROWS 11 THRU 13 INOPERATIVE. TIGHTENED CONNECTION UNDER SEATS, OPERATIONAL CHECK NORMAL.Mar 13, 1998 · N608NW · Doug DC932 · Emergency LightingSDR VJ9800045Spar Chord · corrodedVISUAL INSPECTION OF BLEND AREA AT XRS80 PER AIRTRAN WO 30343, CORROSION WAS NOTED IN THE BLEND AREA AND AROUND 1 FASTENER NEXT TO TO THE BLENDED AREA ON THE RIGHT WING REAR SPAR LOWER CHORD. REMOVED CORROSION IAW DC9 SRM 51-10-3, BLENDED AREA TO MINIMUM OF 1Mar 12, 1998 · N909VJ · Doug DC932 · Wing SparSDR TWAA9809405Casting · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND 718 CASTING CRACKED BEYOND PREVIOUS REPAIR ON AFT SIDE OF CASTING, RT SIDE OF ACFT. REMOVED AND REPLACED CASTING PER SRM 51-01, PAGE 1 ITEM C, AND STANDARD MAINT PRACTICES. (X)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9807314Floorbeam · wornMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FLOORBEAM WITH WEAR AREA AT STATION 237, LBL 4 INCHES. REPAIRED FLOORBEAM PER SRM 53-05 FIG 30. (M)Mar 12, 1998 · N929L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9807313Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND BELOW RT AFT LAVATORY FLOOR, ANGLE AT STATION 996 BELOW LONGERON 18R, AT CUST LINE, CRACKED. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 12, 1998 · N929L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806921Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT CUSP ANGLE CRACKED AT STATION 996, 58.5 LBL, APPROX 4 INCH LONG. MANUFACTURED NEW TIE PLATE AND INSTALLED PER SRM 51-01, PAGE 1, AND TWA STANDARD PRACTICE. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806815Bulkhead Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND L ANGLE ON AFT PRESSURE BULKHEAD CRACKED AT S996, BELOW CUSP ANGLE LBL 58.5. REPLACED L ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9806814Former · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FORMER RING AT STATION 1076, LONGERON 15R, CRACKED. REPLACED PER SRM 53-03, FIG 4, AND STD PRACTICES. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806813Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 6L CRACKED AT STATION 639. INSTALLED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9806812Skin · dentedDURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENT AT FS 980, S5R, .75 INCH BY .068. REPAIRED DENT PER SRM 53-04, PAGE 218K, FIG 38. SEALED REPAIR PER SRM 51-20. (M)Mar 12, 1998 · N997Z · Doug DC932 · Fuselage Main, Plate/SkinSDR 9804289611Retract Mech · lack of lubeDURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR AND NOSE GEAR UNSAFE LIGTHS REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR WITH SAME RESULTS. FLIGHT WAS CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATION OF ALL GEARS. Mar 12, 1998 · N611NA · Doug DC932 · Landing Gear Position and WarningSDR VJ9800077Support · corrodedAFT BAGGAGE FLOOR SUPPORT, LT SIDE, BETWEEN LONGERON 28L AND 27L, FS 935, CORRODED. FABRICATED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-4, 51-30-2, AND 53-01, FIG 2. INSTALLED NEW SUPPORT IAW DC9 SRM 51-30-0 AND 51-30-2.Mar 11, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800042Door Linkage · out of adjustAFTER GEAR RETRACTION, EXPERIENCED VIBRATION AND CREW ELECTED AS A PRECAUTIONARY MEASURE TO RETURN TO MAINTENANCE BASE. UPON LANDING DETERMINED THAT LEFT NOSE LANDING GEAR DOOR WAS NOT FULLY CLOSED. ADJUSTED LT NOSE GEAR DOOR LINK ROD ASSEMBLY; OPS CHECKED GMar 11, 1998 · N914VV · Doug DC932 · Landing Gear Door Retract Section
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