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 TWAA0002404Support · crackedDURING OP 16 MAINT CHECK FOUND AFT CABIN PRESSURE BULKHEAD DOOR INTERNAL CENTER SUPPORT WEB CRACKED, LT END WITH END SECTION MISSING. INSTALLED NEW SUPPORT WEB PER PRINT 9915565.Feb 4, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002403Casting · crackedDURING OP 16 MAINT CHECK FOUND AFT CABIN PRESSURE BULKHEAD DOOR INTERNAL LT LOWER TOP CASTING CRACKED AT LOWER LEG. REPLACED WITH NEW CASTING PER SERVICE REWORK DRAWING JO60229.Feb 4, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002402Fastener · looseDURING OP 16 MAINT CHECK FOUND NUMBER 1 PYLON TOP AFT SKIN HAD 4 ROWS OF BLIND FASTENERS LOOSE AND WORKING. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 9957742, 9915500, 9915501, 9915502, AND 9915503.Feb 3, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR TWAA0002316Fastener · misinstalledDURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, TOP OF PYLON SKIN INBD OF AFT ENGINE MOUNT HAD ROW OF SCREWS WITH SKIN WASHERS LOOSE AND IMPROPERLY INSTALLED. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 9957742, 9915500, 9915501, 9915502 AND 9915503.Feb 3, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR AT0000074Door Pan · corrodedFOUND C1 CARGO DOOR CUTOUT PAN HAD SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED CARGO DOOR PAN, FABRICATED AND INSTALLED PAN SPLICES IAW DC9 SRM 53-05 FIGURE 44, 51-30-2, 51-30-5, 51-10-4.Feb 3, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002315Structure · corrodedDURING OP 16 MAINTENANCE CHECK, ON NUMBER 1 PYLON TOP AND BOTTOM OF PYLON FOR ENG MOUNT YOKE STRUCTURE HAD RUSTY SURFACES AT LE ATTACH. CHECKED MATERIAL THICKNESS PER SPM 04-00. REPAIRED PER ARA 16530 AND SRM 54-04 PAGE 77. SHOT PEENED PER DRS 4999.Feb 2, 2000 · N925L · Doug DC932 · Nacelle/Pylon StructureSDR TWAA0002313Skin · damagedDURING OP 16 MAINTENANCE, CHECK NECESSARY TO INSTALL UPPER WINDOW BELT STRIP FROM STA 699 TO 756 ON LT SIDE. REINSTALLED WINDOW BELT DOUBLER PER MO 71K21 AND EMLR 70533 A.Feb 2, 2000 · N925L · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000083Longeron · crackedFOUND LONGERON 25L CORRODED AT ATTACH POINT TO FRAME AT BS 150-170. CUT OUT LONGERON BETWEEN BS 150-170. INSTALLED LINGERON SPLICES IAW DC9 SRM 53-02 FIGURE 18.Feb 2, 2000 · N811AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000076Frame · corrodedFOUND CORROSION ON FORWARD SIDE FRAME AT BS 980, LONGERON 26R -24R. REMOVED CORROSION, BEYOND LIMITS. REMOVED FRAME SECTION AT BS 980, LONGERON 26R - 24R, INSTALLED NEW FRAME AND REPAIR SPLICES IAW DC9 SRM 53-03 FIGURE 2A.Feb 2, 2000 · N803AT · Doug DC932 · Fuselage Main, FrameSDR AT0000070Skin · crackedFOUND CRACK AT FORWARD ENTRY DOOR JAMB, FORWARD UPPER CORNER ON OUTER SKIN. CUT OUT CRACKED SKIN, FABRICATED DOUBLERS, AND INSTALLED IAW SRD 9530252.Feb 2, 2000 · N803AT · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA00038Slide · dislodgedGALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE FELL OFF. MAINTENANCE REINSTALLED SLIDE PACK.Feb 2, 2000 · N501ME · Doug DC932 · Escape SlideSDR TWAA0002002Stringer · crackedDURING OP 16 MAINT CHECK, STRINGER 4L WAS CRACKED AT STA 200. REPLACED STRINGER 4L AT STA 155 TO 229 PER SRM 51-01, PAGE 1. FASTENERS PER SRM 51-30-02 AND 51-30-5.Feb 1, 2000 · N921L · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000073Bulkhead · corrodedFOUND CANTED BULKHEAD AT BS 1143, LEFT HAND UNDER THE END OF LEFT HAND PYLON SKIN WAS CORRODED. REMOVED CORROSION, REPLACED SKIN AND DOUBLERS IAW DC9 SRM 53-01 FIGURE 4, 51-30-2, AND 51-30-3.Feb 1, 2000 · N803AT · Doug DC932 · Fuselage Main, BulkheadSDR AT0000069Skin · crackedFOUND CARGO COMPARTMENT DOOR JAMB FORWARD LOWER CORNER HAS A .375 CRACK ON OUTER SKIN. CUT OUT CRACK, FABRICATED 2 REPAIR DOUBLERS. TREATED PRIMED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 51-10-03 AND EO 95310-29-E1410.Feb 1, 2000 · N803AT · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0002013Finger Doubler · corrodedDURING OP 16 MAINT CHECK, FOUND FUSELAGE CORROSION ON THE LOWER PRESSURE BULKHEAD FINGER DOUBLERS FROM LONGERON 24L TO L24R, STA 604. REPLACED WITH NEW FINGER DOUBLER PER DOUGLAS DRAWING 5914865.Jan 31, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002012Tee · damagedDURING OP 16 MAINT CHECK, THE LOWER FUSELAGE LOWER BULKHEAD TEE AT STA 604 REQUIRED REPLACEMENT. CLEANED LOWER BULKHEAD TEE AREA STA 604. REPLACED WITH NEW TEE CORD PER DRAWING 5914865.Jan 31, 2000 · N925L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0002011Rib · crackedDURING OP 16 MAINT CHECK THE NUMBER 2 ENG PYLON, OTBD SUPPORT RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915502 AND INSTALLED RIB PN 9915501-502.Jan 31, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Longeron/StringerSDR TWAA0002010Web · crackedDURING OP 16 MAINT CHECK, NR 2 PYLON HAD A CRACK IN THE WEB 9.5 INCHES OTBD OF THE FUSELAGE SKIN, TOP OF PYLON AT STA 1038. REPLACED PART PER DAC PRINT INSTALLATION 9915501, INSTALLED RIB 9915501-2.Jan 31, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Main FrameSDR TWAA0002009Rib · crackedDURING OP 16 MAINT CHECK, FOUND NR 2 ENGINE PYLON, INBD RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915503 AND INSTALLED RIB 9915503-502.Jan 31, 2000 · N925L · Doug DC932 · Nacelle/Pylon, Longeron/StringerSDR MWEA00036Heater · malfunctionedFLIGHT CREW NOTICED SMOKE COMING FROM THE LEFT LAVATORY AT THE GATE. EVIDENCE OF ELECTRICAL FIRE. MTC REMOVED AND REPLACED LAV WATER HEATER, FLUSH TIMER, WATER HEATER CIRCUIT BREAKER, AND INSTALLED GROUNDING STRAP.Jan 31, 2000 · N203ME · Doug DC932 · Wash Water SystemSDR CA000215036Tire · failed(CAN) ON WALKAROUND NR 4 WHEEL TIRE CAP FAILED AND DAMAGED RT FIXED HINGE DOOR. WHEEL AND DOOR REPLACED.Jan 30, 2000 · Doug DC932 · TireSDR MWEA00033Slide · dislodgedGALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE CAME LOOSE FROM COVER. MAINTENANCE RE-INSTALLED SLIDE.Jan 30, 2000 · N216ME · Doug DC932 · Emergency EquipmentSDR AT0000087Bulb · failedFOUND AFT EMERGENCY SIGN, NEAR AFT DOOR, HAS BURNT BULBS. RELAMPED, IAW DC9 MM 33-50.Jan 29, 2000 · N846AT · Doug DC932 · Emergency LightingSDR AT0000062Frame · crackedFOUND FRAME CRACKED AT RIGHT HAND SIDE NEAR THE ACTUATOR LOWER MOUNT (AIRSTAIRS) AT BS 1143. CUT OUT CRACKED FRAME SECTION FABRICATED L & Z DOUBLERS, HEAT TREATED AND INSTALLED NEW FRAME SECTION AND L & Z DOUBLERS IAW DC9 SRM 51-30-2, 51-10-3 AND EO L00024.Jan 28, 2000 · N803AT · Doug DC932 · Fuselage Main, FrameSDR ABXA000079Warning System · malfunctionedON DEPARTURE OUT OF DSM, WHEN THE LANDING GEAR WAS RETRACTED, THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. RECYCLED THE GEAR WITH NORMAL OPERATION. ON APPROACH INTO CIA, WHEN THE GEAR WAS LOWERED, THE NOSE LANDING GEAR TOOK LONGER THAN NORMAL TO LOCK DOWN.Jan 28, 2000 · N988AX · Doug DC932 · Landing Gear Position and WarningSDR TWAA0101702Longeron · crackedDURING CHECK-C MAINT LONGERON 4L WAS FOUND CRACKED IN 2 PLACES AT BELT RING, STA 1087. REMOVED AND REPLACED LONGERON PER SRM 53-02, FIG 18.Jan 27, 2000 · N998R · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA0001801Skin · crackedDURING OP 16 MAINT CHECK AT STA 200, THE FIRST FASTENER ABOVE STRINGER 4L HAD CRACK IN FUSELAGE SKIN 0.250 IN LONG. CRACK STOP DRILLED AND CONTAINMENT CONFIRMED BY NDT PER PART 6-51-00-03. SKIN WAS REPAIRED PER SRM 53-04 FIG 38.Jan 27, 2000 · N921L · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000085Light · inoperativeFOUND R1 DOOR OVERHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. RELAMPED, IAW DC9 MM 33-50.Jan 27, 2000 · N823AT · Doug DC932 · Emergency LightingSDR AT0000084Bulb · failedFOUND 1 BULB BURNT ON TAILCONE HANDLE EMERGENCY LIGHT ASSEMBLY. RELAMPED BULB IAW DC9 MM 33-50.Jan 27, 2000 · N823AT · Doug DC932 · Emergency LightingSDR AT0000060Longeron · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LONGERON IN E&E COMPARTMENT BETWEEN BS 200-218 LONGERON 28 CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA AND SPLICED IN NEW REPAIR AT BS 200-218 LONGERON 28 IAW DC9 SRM 53-02 FIG 18, 55-01 FIG 1, 51Jan 27, 2000 · N836AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA00035Oven · smokeRIGHT HAND GALLEY STARTED TO SMOKE DURING FLIGHT. FLIGHT ATTENDANT TURNED OFF OVEN AND SMOKE IMMEDIATELY STOPPED. MTC CHECKED AND RAN OVENS FOR SEVERAL MINUTES, NO SMOKE OR SMELLS OF SMOKE WERE NOTED.Jan 27, 2000 · N206ME · Doug DC932 · Buffet/GalleysSDR TWAA0002008Keel Beam · corrodedDURING OP 16 MAINT CHECK, FOUND FUSELAGE STA 607 TO 667 HAD CORROSION ON THE KEEL BEAM. REMOVED CORROSION PER SRM 6-80-01, PAGE 1.Jan 26, 2000 · N925L · Doug DC932 · Fuselage Main, KeelSDR MWEA00031Unknown · odorAFTER TAKEOFF, NOTICED UNUSUAL ODOR IN COCKPIT. MTC THROUGHLY INSPECTED ALL AREAS AND COMPONENTS WITH NO ODORS OR DEFECT NOTED.Jan 26, 2000 · N502ME · Doug DC932 · Air Distribution SystemSDR AT0000071Skin · corrodedFOUND RIGHT HAND AFT VANITY CLOSE TO ANGLE SKIN WAS CORRODED OUT OF LIMITS. FABRICATED UPPER SKIN, FILLERS, HEAT TREATED AND INSTALLED IAW DC9 SRM 51-30-1, 51-10-3, 53-01 FIGURE 2, 51-7 0-1. DC9 MM 20-20-0, WEBER OVERHAUL MANUAL, 25-42-50, DPS 4901 AND DPS 1Jan 26, 2000 · N803AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000065Frame · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT MAIN FRAME AT BS 699 IN AFT POCKET POINT F TO D, POINT M-B-A, AND POINT G-H CRACKED. REMOVED AND REPLACED RIGHT MAINFRAME AT BS 699 IAW DC9 SRM 51-30-01, 51-30-02, AND 51-30-05.Jan 26, 2000 · N836AT · Doug DC932 · Fuselage Main, FrameSDR AT0000061Door Jamb · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON FORWARD CARGO LOWER DOOR JAMB. REMOVED AND REPLACED LOWER CARGO DOOR JAMB IAW DC9 SRM 51-10-04, 51-10-03, AND 53-05 FIG 4A.Jan 26, 2000 · N836AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0000059Longeron · corrodedFOUND LONGERON 24R HAD CORROSION AT BS 935 FROM END CAP ALONG UPPER CHANNEL TO BS 945. REMOVED LONGERON 24R, END CLIP, END FITTING. INSTALLED NEW SKIN PATCH AT BS 945, LONGERON 24R, END CLIP AND END FITTING IAW DC9 SRM 53-04 FIGURE 38, 52-02 FIGURE 18.Jan 26, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA000090Doubler · corrodedWHILE COMPLYING WITH A C CHECK INSPECTION, FOUND LEFT SIDE STATIC PORT INTERNAL DOUBLER CORRODED. REPLACED INTERNAL DOUBLER IAW DC9 SRM 51-30-2.Jan 26, 2000 · N980AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA000089Column · crackedWHILE COMPLYING WITH A C CHECK INSPECTION, FOUND FIRST OFFICER'S CONTROL COLUMN CRACKED. REPLACED FIRST OFFICER'S CONTROL COLUMN REF DOUGLAS SERVICE BULLETIN.Jan 26, 2000 · N980AX · Doug DC932 · Control Column SectionSDR ABXA000088Fairing · corrodedWHILE COMPLYING WITH A C-CHECK INSPECTION, FOUND LOWER RIGHT SIDE HORSE COLLAR CORRODED. REPLACED LOWER RIGHT SIDE HORSE COLLAR IAW DC9 MM 55-10-0 AND DC9 SRM 51-30-1.Jan 26, 2000 · N980AX · Doug DC932 · Vertical StabilizerSDR 0000529614Hinge · crackedCRACK IN NOSE WHEEL WELL SUPPORT FITTING BS 50 ABOVE FORWARD HINGE OF LEFT FORWARD DOOR 1.5 INCH LONG. CRACKED LOWER SURFACE FRONT END THROUGH FASTENER HOLE. REPAIRED, REMOVED AND REPLACED NOSE GEAR DEFLECTOR STOP PER EA 96-172125 AND SRM 51-30-5 SB 32-124RLJan 25, 2000 · N614NW · Doug DC932 · Fuselage, Door HingeSDR TWAA0002312Fastener · wrong partDURING OP 16 MAINTENANCE CHECK, FOUND SEVERAL CHERRY FASTENERS IN UPSIDE DOWN HAT SECTION FROM STA 606 TO 659 AND BETWEEN KEEL AND STRINGER 29R. RE-INSTALLED MS20470AD6 RIVETS PER DRAWING 5911418. INSTALLED RIVETS PER SRM 51-30-2. SUBSTITUTED HL326-6 FOR NAJan 25, 2000 · N925L · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000057Light · failedFOUND TAIL CONE LEFT STAIR EMERGENCY LIGHT WOULD NOT ILLUMINATE. RELAMPED UNIT IAW DC9 MM 33-50.Jan 25, 2000 · N866AT · Doug DC932 · Emergency LightingSDR AT0000052Frame · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON FRAME AT BS 237 LONGERON 30. AFTER REMOVAL OF CORROSION, FOUND FRAMEOUT OF LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF FRAME AT BS 237 LONGERON 30 IAW DC9 SRM 5 3-01 FIG 1, 53-03 Jan 24, 2000 · N836AT · Doug DC932 · Fuselage Main, FrameSDR ABXA000073Battery · dischargedEMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.Jan 24, 2000 · N982AX · Doug DC932 · Emergency LightingSDR AT0000046Frame · corrodedFOUND AFT PIT LONGERON CORRODED AT BS 832 ALONG FRAME. REMOVED CORROSION, TREATED, ALODINED AND PRIMED IAW DC9 SRM 53-01 FIGURE 1, TABLE 2, 51-10-3.Jan 23, 2000 · N803AT · Doug DC932 · Fuselage Main, FrameSDR AT0000038Strut · dischargedFOUND LANDING GEAR UPLATCH RELEASE OR GROUND SHIFT DID NOT WORK AND WOULD NOT RAISE. ON FINAL AT BUF (BUFFALO). GROUND SHIFT OR THE UPLATCH RELEASE WAS HEARD TO HAVE RELEASED. PERFORMED GEAR SWING. NOSE LANDING GEAR FOUND TO BE UNDER SERVICED WITH FLUID ANJan 23, 2000 · N866AT · Doug DC932 · Nose/Tail Landing Gear Strut/AxleSDR AT0000036Gcu · inoperativeFOUND LEFT GENERATOR FAILED AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED SMELL OF SMOKE IN CABIN AFTER TAKEOFF. REMOVED AND REPLACED GENERATOR CONTROL UNIT. RAN ENGINE PACKS, COULD NOT DUPLICATE SMOKE SMELL..Jan 23, 2000 · N831AT · Doug DC932 · AC Generation SystemSDR MWEA00030Slide · dislodgedGALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE CAME LOOSE. MAINTENANCE REINSTALLED EVACUATION SLIDE.Jan 23, 2000 · N501ME · Doug DC932 · Escape SlideSDR MWEA00026Slide · dislodgedMAIN CABIN DOOR EMERGENCY EVACUATION SLIDE FELL OUT OF COVER. MAINTENANCE REINSTALLED SLIDE PACK INTO COVER.Jan 23, 2000 · N301ME · Doug DC932 · Escape Slide
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