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 MWEA98293Jamb · corrodedVENTRAL STAIR CUTOUT LEFT HAND JAMB HOLE L-ANGLE WAS FOUND CORRODED FROM STA 1038 TO 1086. REMOVED AND REPLACED DAMAGED SECTION OF JAMB.Mar 5, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98292Web · corrodedGALLEY SUBFLOOR WAS FOUND CORRODED IN VARIOUS AREAS. ALSO, A HOLE WAS PUNCHED IN THE FLOOR FROM FS 120 TO FS 160 LBL 8 TO RBL 55. REMOVED AND REPLACED SUBFLOOR.Mar 5, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98291Web · corrodedSUBFLOOR WEB AT FS 160 TO FS 200 LBL 44 TO LBL 55 WAS FOUND CORRODED. REMOVED AND REPLACED SUBFLOOR WEB.Mar 5, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98290Frame · damagedA FRAME AT FS 207 WAS CUT TO FACILITATE OTHER MAINTENANCE. FABRICATED AND INSTALLED REPAIR SPLICES.Mar 5, 1998 · N212ME · Doug DC932 · Fuselage Main, FrameSDR 9803989603Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND CABIN EMERGENCY LIGHTS BETWEEN ROWS 16 THRU 20 INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL.Mar 5, 1998 · N603NW · Doug DC932 · Emergency LightingSDR VJ9800076Floor · corrodedFLOOR PANEL, FS 130, CORRODED BEYOND LIMITS DC9 SRM 53-01, FIG 1. REMOVED CORROSION IAW DC9 SRM 51-10-3. INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-2 AND 51-30-1.Mar 4, 1998 · N905VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800032Link Assy · malfunctionedDURING CLIMB, EXTENDED AND RETRACTED NLG BECAUSE OF NOISE AND VIBRATION. REPLACED LT NLG DOOR LINK ASSEMBLY, PERFORMED GEAR RETRACTION AND OPS CHECKED NORMAL.Mar 4, 1998 · N914VV · Doug DC932 · Landing Gear Door Retract SectionSDR CALA9800388Dnlock Switch · malfunctionedWHEN LANDING GEAR WAS EXTENDED ON APPROACH TO IAH, NO GREEN LIGHTS ILLUMINATED FOR NOSE GEAR. THE UNSAFE GEAR INDICATION CHECKLIST WAS COMPLETED DURING A GO AROUND AND WHEN GEAR WAS LOWERED AGAIN CREW RECEIVED THREE GREEN AND LANDED UNEVENTFULLY. MAINTENANCEMar 4, 1998 · N12508 · Doug DC932 · Landing Gear Position and WarningSDR TWAA9803101Power Supply · inoperativeSTL - FLT 625 - AFT CABIN EGRESS LIGHTS AND TAIL CONE EXIT LIGHTS WERE BLINKING ON AND OFF IN DESCENT. REPLACED POWER SUPPLY FOR AFT CABIN EGRESS LIGHT SYSTEM. CHECK-C 11-15-97 MCI. (X)Mar 3, 1998 · N922L · Doug DC932 · Emergency LightingSDR MWEA98278Slide · defectiveTHE MAIN DOOR SLIDE PRESSURE GAUGE INDICATES IN THE RED. MTC REPLACED SLIDE.Mar 3, 1998 · N301ME · Doug DC932 · Escape SlideSDR VJ9800339Intercoastal · corrodedINTERCOASTAL CORRODED BEYOND LIMITS AT FS 965 BETWEEN LONGERON 27LT AND 29 RT. REPLACED CORRODED INTERCOASTAL AT FS 965, LONGERON 27 LT-29 RT IAW SRM 51-10-2, 51-30-1, 51-30-2.Mar 2, 1998 · N903VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800102Support · corrodedFLOOR SUPPORT UPPER FLANGE FS Y200-220, X15L, CORRODED. FABRICATED, TREATED, AND INSTALLED NEW SUPPORT IAW DC9 SRM 51-10-1, 51-10-3, 51-10-4, AND 51-30-2.Mar 2, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9803306Seat Track · corrodedMCI - DURING MAJOR MAINTENANCE CHECK, NR 4 CABIN CHAIR TRACK CORROSION WAS OUT OF LIMITS AFTER CLEAN UP. REPLACED FLOOR TRACK FROM STATION 200 TO 266 PER SRM 51-01 PAGE 1 ITEM C AND STANDARD PROCEDURES. (M)Mar 2, 1998 · N997Z · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA98277Bulkhead Web · elongated holesTHE AFT PRESSURE BULKHEAD WEB HAS 3 ELONG HOLES ON LT SIDE DOOR JAMB STA Z34 TO 48. MTC FABRICATED REPAIR DOUBLER AND BUSHINGS IAW SVC MSP-0172/PDG ATA 09-053-30-01 DATED 09FEB98.Mar 2, 1998 · N203ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98275Bulkhead Tee · corrosionTHE AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB LOWER RT HORIZONTAL TEE HAS CORROSION. MTC FABRICATED REPLACEMENT TEE.Mar 2, 1998 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98274Bulkhead Clip · corrodedTHE AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB LOWER RT TEE ANGLE ABOVE GUSSETT AND RT TEE CLIP INBOARD OF GUSSET AROUND FASTENERS HAS CORROSION. MTC REMOVED CORROSION.Mar 2, 1998 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98272Frame · corrodedDURING D-CHECK, THE FRAME AT FS 598 HAS CORROSION BETWEEN LONGERON 28L AND 29R. CORROSION BLEND OUTS BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLERS.Mar 2, 1998 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98271Intercostal · corrodedTHE INTERCOSTAL AT LONGERON 29R FROM FS 370 TO 408 WAS FOUND CORRODED. REMOVED AND REPLACED INTERCOSTAL.Mar 2, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98270Frame · corrodedTHE FRAME AT FS 351 WAS FOUND TO HAVE CORROSION BETWEEN LONGERON 28L TO 28R. CORROSION WAS BLENDED BEYOND LIMITS. REMOVED AND REPLACED SECTION OF FRAME.Mar 2, 1998 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98269Jamb · corrodedFORWARD CARGO DOOR JAMB PAN WAS FOUND CORRODED ALONG THE ENTIRE LOWER LENGTH FROM FS 370 TO FS 427. CORROSION BLENDED BEYOND LIMITS. REMOVED AND REPLACED SECTION OF PAN.Mar 2, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98268Intercostal · corrodedINTERCOSTAL BETWEEN FS 484 AND 503 LONGERON 27L AND 28L WAS FOUND CORRODED. REMOVED AND REPLACED INTERCOSTAL.Mar 2, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98267Longeron · corrodedLONGERON 30 WAS FOUND CORRODED FROM FS 415 TO FS 596 WITH EXCESSIVE MATERIAL LOSS AT ALL FRAMES. REMOVED AND REPLACED LONGERON FROM FS 408 TO 596.Mar 2, 1998 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98266Splice · corrodedLONGERON SPLICES AT FRAME STATION 408 AND 427 FOR LONGERON 30 WERE FOUND CORRODED. REMOVED AND REPLACED SPLICES.Mar 2, 1998 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98265Longeron · corrodedLONGERON 29R WAS FOUND CORRODED FROM FS 575 TO FS 605. REMOVED AND REPLACED LONGERON.Mar 2, 1998 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9803759941Skin · corrodedDURING M-CHECK, FOUND CORROSION ON SKIN PANEL AT FS 937 TO 996, LONGERON 21R TO 26R. REPAIRED PER EA 99-154595.Mar 2, 1998 · N3324L · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800075Floorbeam · corrodedFLOOR BEAM AFT LAV FS 965, BL 22R, CORRODED. REMOVED SECTION FLOORBEAM FROM BL 0 TO BL 50R, FABRICATED AND SPLICED NEW SECTION IAW DC9 SRM 53-05, FIG 20A. TREATED AND PRIMED IAW DC9 SRM 51-10-3 AND 51-30-0.Mar 1, 1998 · N905VV · Doug DC932 · Fuselage Main, Floor BeamSDR VJ9800074Floor · corrodedFLOOR PANEL 4410A CORRODED BEYOND LIMITS ON BOTTOM SIDE IAW DC9 SRM 51-10-3 AND SRM 53-01, FIG 1. REMOVED CORROSION AND FABRICATED PANEL IAW DC9 SRM 51-10-2. BONDED NEW PART IAW DC9 SRM 51-70-3.Feb 28, 1998 · N905VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800057Skin · corrodedAFT CARGO FUSELAGE SKIN AND FRAME CORRODED AT FRAME STATION 980 BETWEEN L27R AND L28R ON AFT SIDE. CUT OUT PLATING BETWEEN L27R AND L28R, FABRICATED FILLER USING T2024T3 OF .050 AND .025 THICKNESS, FABRICATED FINGER DOUBLER USING 2024 T3, .025 IAW DC9 SRM 51-Feb 28, 1998 · N909VJ · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800050Skin · corrodedAFT CARGO FUSELAGE SKIN AND FRAME ARE CORRODED HEAVILY ON AFT SIDE AT FRAME STA 980 BETWEEN LONG 28 R AND 27R. CUT OUT AREA OF PLATING BETWEEN L27R AND 28R. FABBED FILLER 2024 T3 .50, FABBED DOUBLER 2024 T3 .025. FABBED FINGER DOUBLER 2024 T3 IAW DC-9 SRM 5Feb 28, 1998 · N909VJ · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800028Battery · dischargedFORWARD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY IAW MM 33-60.Feb 28, 1998 · N919VV · Doug DC932 · Emergency LightingSDR 98ZZZM438Skin · corrodedAFT CARGO FUSELAGE SKIN AND FRAME CORRODED AT FRAME STATION 980 BETWEEN L27R AND L28R ON AFT SIDE. CUT OUT PLATING BETWEEN L27R AND L28R, FABRICATED FILLER USING T2024T3 OF .050 AND .025 THICKNESS, FABRICATED FINGER DOUBLER USING 2024 T3, .025 IAW DC9 SRM 51-Feb 28, 1998 · N909VJ · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800335Angle · corrodedFOUND CORROSION ON BTM (2 EA) CORNERS OF NR 4 AFT AFT GALLEY. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01 PAG 8. REMOVED AND FABRICATED ANGLE FOR BOTTOM OF NR 4 AFT GALLEY FROM S124943T 75 X 1.0 X 11.0 X ANGLE IAW SRM 53-01 FIG 2, 51-10-4, Feb 27, 1998 · N903VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98248Blkhd Stiffener · corrodedTHE STIFFENER ON LONGERON 14R CANTED BULKHEAD 1121 WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98247Blkhd Stiffener · corrodedTHE LONGERON 10R STIFFENER ON THE AFT SIDE OF THE STA 1121 CANTED FRAME WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98246Blkhd Stiffener · corrodedTHE 1121 CANTED BULKHEAD LONGERON 13L STIFFENER WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98245Blkhd Stiffener · corrodedTHE 1121 CANTED BULKHEAD LONGERON 14L STIFFENER WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98244Blkhd Stiffener · corrodedTHE 1121 CANTED BULKHEAD STIFFENER AT LONGERON 12L WAS FOUND EXFOLIATED. REMOVED AND REPLACED STIFFENER.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98243Bulkhead Doubler · corrodedDOUBLER ON CANTED BULKHEAD 1089 LONGERON 11R WAS FOUND CORRODED. REMOVED AND REPLACED DOUBLER.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98242Frame · corrodedTHE STATION 1089 CANTED FRAME FOUND WITH A CORRODED WEB AT LONGERON 12L. BLENDED CORROSION OUT OF LIMITS, FABRICATED REPAIR FILLER AND DOUBLER, INSTALLED REPAIR.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98240Web · corrosionTHE SUBFLOOR WEB AT FS 218 TO FS 237 WAS FOUND CORRODED. REMOVED AND REPLACED DAMAGED SUBFLOOR WEB.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98239Floorbeam · damagedTHE FLOORBEAM AT FS 237 LBL 45 TO 55 HAS AN IMPROPER REPAIR. REMOVED AND REPLACED REPAIR IAW SRM.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA98238Web · corrodedTHE SUBFLOOR WEB IN THE FWD GALLEY AREA FROM FS 160 TO 200. REMOVED AND REPLACED DAMAGED FLOOR WEB.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98237Web · corrodedTHE SUBFLOOR WEB WAS FOUND CORRODED BETWEEN STATION 120 TO 160 LBL 8 TO RBL 148. REMOVED AND REPLACED DAMAGED WEB.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98236Web · corrodedSUBFLOOR WEB AT STA 190 LBL 50 WAS FOUND CORRODED MATERIAL LOSS 10090. REMOVED AND REPLACED SUBFLOOR FROM FS 160 TO 200.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98235Doubler · damagedA PREVIOUSLY BLENDED AREA WAS FOUND ON THE FUEL TANK LOWER ACCESS PLATE MATING SURFACE DOUBLER AT XRS 360.5. REPAIR DOUBLER WAS FABRICATED AND INSTALLED.Feb 27, 1998 · N212ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA98234Rib · gougedTHE NUMBER 6 SLAT TRACK RIB ON THE RIGHT WING WAS FOUND TO BE GOUGED. THE DAMAGED RIB WAS REMOVED AND A NEW ONE FABRICATED AND INSTALLED.Feb 27, 1998 · N212ME · Doug DC932 · Wing, Rib/BulkheadSDR MWEA98233Fitting · crackedKEEL BEAM FITTING AT FS 699 WAS FOUND CRACKED. REMOVED AND REPLACED CRACKED FITTING.Feb 27, 1998 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR CA980402012Oven · malfunctioned(CAN) ELECTRICAL FUMES DETECTED ON CLIMB-OUT. ELECTRICAL FIRE DRILL CARRIED OUT. GALLEY POWER SWITCHED OFF. SMELL DISSIPATED. THE MIDDLE OVEN POSITION NR 16 FOUND TO BE THE CAUSE OF THE PROBLEM AND WAS ISOLATED. OVEN RECEPTACLE CHANGED AND CHECKED SERVICEABFeb 27, 1998 · Doug DC932 · Buffet/GalleysSDR 9803469925Slide · low pressureDURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE, CHECKED OK.Feb 27, 1998 · N925US · Doug DC932 · Escape SlideSDR 9803429604Vent Valve · stuckRIGHT FUEL QUANTITY INDICATOR DROPPED IN EXCESS OF NORMAL FUEL BURN AFTER TAKEOFF. FLIGHT WAS RETURNED TO OKC AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED STICK READINGS WITH FUEL QUANTITY INDICATORS. NO DISCREPANCIES WERE NOTED. IT IS SUSPECTED THAT Feb 27, 1998 · N604NW · Doug DC932 · Fuel Storage
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