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 AT9900136Skin · creasedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CREASE OUT OF LIMITS AT STA 484 RIGHT SIDE L-19-20. ALSO, A COAX CABLE STAND OFF BROKEN AT STA 955 ABOVE L-20R. TRIMMED OUT CREASE, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-30-5, 51-30-2, 53-04 FIG 12B, Feb 1, 1999 · N816AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900083Web · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND LEFT CUSP WEB AT STA 927 CORRODED. REMOVED AND FABRICATED AND INSTALLED CUSP WEB SECTION IAW DC9 SRM 51-10-2, 53-11-3 FIG 11, 51-30-2, AND RES NR 99195.Feb 1, 1999 · N806AT · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9900048Channel · crackedDURING C-CHECK, FOUND THE AFT ENTRY DOOR INTERNAL STIFFENER CRACKED AT UPPER HINGE. REPAIRED DOOR IAW ABX REA D952-26563MR.Feb 1, 1999 · N989AX · Doug DC932 · Passenger/Crew DoorsSDR 9900379603Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK AND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Feb 1, 1999 · N603NW · Doug DC932 · Emergency LightingSDR MWEA99056Slide · detachedFORWARD ENTRANCE DOOR EMERGENCY SLIDE FELL OFF. MTC REINSTALLED SLIDE COVER.Jan 31, 1999 · N502ME · Doug DC932 · Emergency EquipmentSDR MWEA99055Slide · detachedTHE FORWARD ENTRANCE DOOR ESCAPE SLIDE FELL OFF. MTC REINSTALLED SLIDE COVER.Jan 31, 1999 · N212ME · Doug DC932 · Emergency EquipmentSDR GTIA990892Floorbeam · corrodedMHV - AFT CARGO FS 955 RBL 24 EVIDENCE OF MODERATE TO HEAVY LOAL CORROSION ON FLOORBEAM UPPER CAP. REMOVED AND REPLACED UPPER CAP FABRICATED NEW CAP FROM 7075T6511 EXTRUSION S912758T PO NR 81788. INSTALLED FASTENER PER DC9 SRM 51-30-1 FOR TORQUE OF BOLTS DC9Jan 30, 1999 · N13512 · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9900096Connector · dirtyINSPECTION FOUND THE L-1 PORTABLE EMERGENCY LIGHT INOPERATIVE. THE CONNECTOR WAS CLEANED AND SECURED AND OPERATION OF THE LIGHT CHECKED GOOD.Jan 30, 1999 · N14524 · Doug DC932 · Emergency LightingSDR AT9900082Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND NUMEROUS DENTS IN AFT VENTRAL STAIRS LOWER AFT SKIN FROM SPLICE. REMOVED AND REPLACED EXISTING SKIN FROM PREVIOUS SPLICE IAW DC9 SRM 51-10-4, 51-30-2, AND RES NR 99221.Jan 30, 1999 · N816AT · Doug DC932 · Entrance StairsSDR AT9900072Brakes · malfunctionedUPON LANDING EVERYTHING WAS NORMAL, ON TAXI-IN IT FELT LIKE BRAKES WERE APPLIED, IT WOULD TAKE A SECOND OR TWO FOR IT TO RELEASE. AT NO TIME DID THE BRAKES DRAG TO THE EXTEND THAT THEY WERE GOING TO IGNITE. ON ARRIVAL AT THE GATE THE BRAKES WERE SMOKING. TJan 30, 1999 · N810AT · Doug DC932 · Landing Gear Brake SystemSDR TWAA9902004Intercostal · crackedDURING OP 15 MAINT CHECK, FOUND CRACKED INTERCOSTAL AT STA 737, LONGERON 15L. REMOVED AND REPLACED INTERCOSTAL PER STANDARD PROCESSES MANUAL 6-70-01.Jan 29, 1999 · N923L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9902003Membrane · crackedDURING OP 15 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR WITH APPROXIMATELY 12 INCH CRACK, LOCATED AT STA 195, LBL 4 TO 12. REPAIRED PER SRM 53-01, PG 9.Jan 29, 1999 · N923L · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9900907Floor · corrodedMHV - FLOORBOARDS FS 160-200 BL 0 TO LBL 42 CORRODED AND SUPTS CRACKED. FABRICATED A NEW SKIN IAW DC9 SRM 53-21-0, 4B INST HAT SUPPORTS IAW DC9 SRM 53-21-0. ALODINE AND PAINT IAW DC9 SRM. INSTALLED RIVETS IAW SRM DC9. (M)Jan 29, 1999 · N13512 · Doug DC932 · Fuselage Floor PanelSDR GTIA9900901Skin · gougedMHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 130 WATER LINE 0 HAS A COUPLE OF GOUGES. REMOVED DAMAGED AREA (CUT OUT) AND REPAIRED IAW DC9 SRM 53-04 FIG 38 SHT 21, 51-30-2 AND 51-30-5 JOB COMPLETE REPAIRED FRAME AT FS 130 PER BOEING MESSAGE AUQ-MQJ-99-004RJan 29, 1999 · N13512 · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA9900896Stiffener · crackedMHV - LEFT INBOARD FLOOR STATION 484 HAS RIVETS PULLING THROUGH AND BOTH ENDS OF ALL STIFFENERS ARE CRACKED ON 484 AND 520. REMOVED DAMAGED STIFFENERS. FABRICATED NEW STIFFENERS LOCATED AND DRILLED IAW SRM 51-01 TREATED AND PRIMED IAW SRM 51-10-3. INSTALLEDJan 29, 1999 · N13512 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9900093Wire · brokenINSPECTION FOUND THE ESCAPE PATH LIGHT INBOARD OF FORWARD FIRST CLASS COAT CLOSET INOPERATIVE. MAINTENANCE FOUND BROKEN WIRING. THE ESCAPE PATH LIGHT WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-0, PAGE 501.Jan 29, 1999 · N14524 · Doug DC932 · Light System WiringSDR AT9900129Cusp · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND ON CUSP MEMBRANE AT RIGHT OUTBOARD STA 945 AND STA 965 CUSP A7. REMOVED CORROSION AND FABRICATED DOUBLERS AND FILLER IAW DC9 SRM 51-30-2, 51-10-3, 53-20-1. DOUBLER (P/N 1A-42076-1) OFF.Jan 29, 1999 · N816AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900073Lamp · failedFOUND ON THE AFT ACCESSORY COMPARTMENT AFT POSITION TAIL CONE EVACUATION LAMPS LEFT AND RIGHT SIDE INOPERATIVE. REMOVED AND REPLACED LAMPS, SYSTEM CHECKED GOOD IAW MM 33-50.Jan 29, 1999 · N814AT · Doug DC932 · Emergency LightingSDR AT9900067Fuel · ventingFUEL VENTING FROM RIGHT WING FUEL VENT IN FLIGHT. BACK FLUSH FUEL SYSTEM BY TRANSFERRING FUEL BETWEEN ALL THREE TANKS. ALL FILL VALVES AND FUEL SHUT OFF VALVES OPERATE NORMAL. NO LEAKS OR VENTING OF FUEL NOTED, OK FOR SERVICE PER MM 28-20.Jan 29, 1999 · N833AT · Doug DC932 · Aircraft Fuel Distribution SystemSDR TWAA9902605Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION AROUND FASTENER HOLES ON FLOOR TRACK RBL 16, BETWEEN STA 1212 AND 1271. INSTALLED NEW FLOOR TRACK PER STANDARD PROCESSES MANUAL 6-70-01, PAGE 3.Jan 28, 1999 · N941AS · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9902604Intercostal · corrodedDURING OP 16 MAINT CHECK, FOUND INTERCOSTAL BELOW RT FLOOR TRACK AT STA 1308, RBL 16, WAS CORRODED. INSTALLED NEW INTERCOSTAL PER STANDARD PROCESSES MANUAL 6-70-1, PAGE 3.Jan 28, 1999 · N941AS · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9902603Intercostal · corrodedDURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CORRODED BELOW LT FLOOR SUPPORT, BETWEEN STA 1308 AND 1319, LBL 16. INSTALLED NEW INTERCOSTAL PER STANDARD PROCESSES MANAL 6-70-1, PAGE 3.Jan 28, 1999 · N941AS · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9900092Fitting · crackedINSPECTION FOUND AFT CARGO DOOR THIRD BEAM END FITTING CRACKED AT AFT SIDE OF DOOR. THE CRACK WAS .1875 INCH LONG. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2.Jan 28, 1999 · N14524 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9900091Power Supply · inopTHE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE B5-25 POWER SUPPLY AT STA 635 WAS REMOVED AND REPLACED.Jan 28, 1999 · N15525 · Doug DC932 · Emergency LightingSDR AT9900128Longeron · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON LONGERONS AT STA 237 L-30 AND STA 560 TO STA 579 L-30. ALSO, CORRODED RIVETS AT T-CAP AT STA 598 L-24L TO L-24R. REMOVED AND REPLACED FASTENERS ON T-CAP, TREATED CORROSION, CUT OUT DAMAGE LONGERON SEJan 28, 1999 · N816AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900126Doubler · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION BULGED AT STA 937 L-26R. MECHANICALLY REMOVED CORROSION, FASTENERS AND DOUBLER. FABRICATED AND INSTALLED FASTENERS, DOUBLER IAW DC9 SRM 51-30-5, 51-30-2, 51-20-0, AND RES NR 99301.Jan 28, 1999 · N816AT · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9900049Generator · failedEN ROUTE, ALL AIRCRAFT LIGHTING AND RADAR PICTURE INTENSITY STARTED FLUCTUATING. LEFT GENERATOR VOLTS AND FREQS WERE FLUCTUATING, WIND SHEAR ANNUNCIATOR AND WARNING CAME ON. ALL ELECTRICAL POWER FAILED. EMERGENCY POWER REMAINED ON. AC CROSS-TIE ILLUMINATEDJan 28, 1999 · N901AX · Doug DC932 · AC Generator-AlternatorSDR ABXA9900042Angle · corrodedDURING C-CHECK, FOUND INTERCOSTAL ANGLE CORRODED AT STATION 617 LONGERON 17 RIGHT. REPLACED INTERCOSTAL ATTACH ANGLE IAW DC9 SRM 51-30-5.Jan 28, 1999 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9900041Seal · defectiveDURING MAINTENANCE CHECK, WAS UNABLE TO OPEN FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT). REPLACED FIRST OFFICER'S CLEARVIEW WINDOW SEAL.Jan 28, 1999 · N985AX · Doug DC932 · Flight Compartment WindowsSDR MWEA99053Battery Pack · dischargedTHE EMERGENCY PEANUT LIGHTS IN COCKPIT REMAIN ON REGARDLESS OF COCKPIT EMERGENCY LIGHT SWITCH POSITION. MTC REMOVED AND REPLACED EMERGENCY BATTERY PACK.Jan 27, 1999 · N501ME · Doug DC932 · Emergency LightingSDR GTIA9900895Seat Track · corrodedMHV - FORWARD PASS COMPARTMENT FS 220 RBL 21 SEAT TRACK HAS EXFOLIATION CORROSION ON TOP SURFACE. REMOVED SEAT TRACK AND REPLACED NEW SEAT TRACK FOR DC9 SRM 53-05 FIG 4. (M)Jan 27, 1999 · N13512 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA9900894Seat Track · corrodedMHV - FORWARD PASS COMPARTMENT FS 200 TO 230 RBL 42 SEAT TRACK HAS EXFOLIATION CORROSION ON UPPER SURFACE. REMOVED DAMAGED SECTION OF SEAT TRACK CUT NEW SECTION OF SEAT TRACK EXTRUSION 52914913 PO 81257. FABRICATED AND DRILLED IAW SRM 53-05 . TREATED AND PRJan 27, 1999 · N13512 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA9900893Bracket · crackedMHV - R1 DOOR SLIDE SUPPORT BRACKET IS CRACKED FORWARD EDGE. STOP DRILLED CRACK USING .25 INCH DIAMETER DRILL AND BAB DOUBLER IAW DC9 SRM 53-01 FIG 2 DRILLED AND COUNTER SINK RIVET HOLES IAW SRM DC9 51-10-4 AND 51-30-2 ALODINE AND PRIMED IAW DC9 SRM 51-10-3 EJan 27, 1999 · N13512 · Doug DC932 · Emergency EquipmentSDR GTIA9900890Angle · corrodedMHV - FORWARD PASS COMPARTMENT FS 160-220 BL 0 FLOOR SUPPORT ANGLE HAS MILD TO HEAVY CORROSION ENTIRE LENGTH. FLOOR SUPPORT WAS FABRCIATED ALODINED PRIMED AND INSTALLED COMPLETE IAW DC9 SRM 51-10-3, 51-30-5. (M)Jan 27, 1999 · N13512 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9900084Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR BEAM END FITTING AT AFT SIDE OF DOOR. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5, PAGE 4.Jan 27, 1999 · N14524 · Doug DC932 · Cargo/Baggage DoorsSDR AT9900044Power Supply · defectiveOVERHEAD EMERGENCY LIGHTING LIGHTS FROM ROW 1 TO ROW 18 WILL NOT ILLUMINATE, DURING MAINTENANCE TESTING. REMOVED AND REPLACED STATION 628 FORWARD POWER SUPPLY, REFERENCE MM 33-50. OPERATIONAL CHECKED GOOD.Jan 27, 1999 · N839AT · Doug DC932 · Emergency LightingSDR ABXA9900044Longeron · crackedDURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 965. REPLACED SECTION OF LONGERON IAW DC9 SRM 53-02.Jan 27, 1999 · N989AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9900043Longeron · crackedDURING C-CHECK, FOUND LONGERON 16 LEFT CRACKED AT STATION 965. REPLACED SECTION OF LONGERON IAW DC9 SRM 53-02.Jan 27, 1999 · N989AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA9900900Skin · gougedMHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 148 WATER LINE 0 HAS A COUPLE OF GOUGES. CUT OUT AREA DAMAGE, FABRICATE DOUBLER AND FILLER AND INSTALLED DOUBLER AND FILLER IAW DC9 SRM 53-04 FIG 38 PAGE 218 AND IAW DC9 SRM 51-30-02 AND 51-30-05. INSTALLED FAJan 26, 1999 · N13512 · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA9900899Skin · gougedMHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 120 WATER LINE 0 HAS A DENT APPROX 1 INCH BY 1 INCH AND IS GOUGED. CUT OUT AREA DAMAGE, FABRICATED DOUBLER AND FILLER AND INSTALLED DOUBLER AND FILLER IAW DC9 SRM 53-04 FIG 38 218 AND INSTALLED FASTENERS IW SC9Jan 26, 1999 · N13512 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9900082Spar Cap · crackedINSPECTION FOUND A 1.875 INCH CRACK IN RT WING LOWER SPAR CAP, UNDER THE I/B FLAP HINGE FITTING AT STA XRS 164.0. A REPAIR WAS INSTALLED IAW DOUGLAS DRAWING NR 506271.Jan 26, 1999 · N17533 · Doug DC932 · Wing SparSDR CALA9900081Vane · delaminatedINSPECTION FOUND LT WING FLAP I/B FIXED VANE DELAMINATED ON LOWER SURFACE. THE LEFT I/B VANE WAS REMOVED AND REPLACED IAW MM 27-51-3.Jan 26, 1999 · N17533 · Doug DC932 · Trailing Edge FlapsSDR CALA9900080Vane · delaminatedINSPECTION FOUND RT WING FLAP O/B FIXED VANE I/B UPPER END DELAMINATED WITH CORROSION AT TOP AND BOTTOM AREAS. THE RT O/B VANE WAS REMOVED AND REPLACED IAW MM 27-51-3.Jan 26, 1999 · N17533 · Doug DC932 · Trailing Edge FlapsSDR AT9900079Web · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION OUT OF LIMITS AT THE CUSP WEB STA 889 THRU 937 L-18R. FABRICATED NEW CUSP WEB SECTION AND INSTALLED IAW DC9 SRM 51-30-2, AND RES NR 99198.Jan 26, 1999 · N806AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900071Skin · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND ALL DOUBLERS DISBONDED AND CORROSION IN BETWEEN SKIN ON TOP OF LEFT WING TRAILING EDGE FLAP SKIN AT STA 214. REMOVED AND FABRICATED NEW SKIN AND 'T' CAP AND REINSTALLED IAW DC9 SRM 51-30-2, 51-10-4, 51-10-2, 51-10Jan 26, 1999 · N849AT · Doug DC932 · Wing, Plate/SkinSDR ABXA9900046Longeron · crackedDURING C-CHECK, FOUND LONGERON 16 CRACKED AT STATION 256. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2 AND 51-30-5.Jan 26, 1999 · N989AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9900045Longeron · crackedDURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 980. REPLACED LONGERON 17 RIGHT FROM STATION 955 TO 965 IAW DC9 SRM 53-02.Jan 26, 1999 · N989AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA99052Skin · crackedFOUND SMALL FAIRING LIFTING AND RIVETS PULLING THROUGH SKIN ON AFT OUTBOARD CORNER OF RIGHT ELEVATOR. MTC FABRICATED AND INSTALLED NEW DOUBLER AND SKIN.Jan 25, 1999 · N203ME · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR GTIA9900004Light · inoperativeDTW - EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. AFT OF BULKHEAD (TAIL CONE). REMOVED AND REPLACED EMERGENCY BATTERY CHARGER AND OPERATIONAL CHECK GOOD IAW MM 33-50-00. PART TC: 321. (X)Jan 25, 1999 · N12536 · Doug DC932 · Emergency LightingSDR AT9900045Web · corrosionSCHEDULED INSPECTION AT AERO CORP, FL. A CUSP WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF CUSP WEB, FABRICATED A NEW SECTION OF WEB AND TWO SPLICES. INSTALLED REPAIR PARTS IAW DC9 SRM 51-10-2, 53-11-3 AND RES NR 99195 (P/N 1A-41Jan 25, 1999 · N806AT · Doug DC932 · Fuselage Miscellaneous Structure
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