Douglas DC-9-31

Service difficulty reports · 7,433

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC931'
  ORDER BY difficulty_date DESC"

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SDR 9516789989Blkhd Web · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND THE AFT PRESSURE BULKHEAD WEB FS 996 TO HAVE LOOSE RIVETS (LONGERON 26R - 27R), CRACKS (AT LONGERON 28R, 29R), AND CORROSION (BL 0). REPAIRED WEB (P/N 5910130-65) PER EA 99-94812.Jul 29, 1995 · N8945E · Doug DC931 · Fuselage Main, BulkheadSDR 9516779989Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT SIDE NOSE LANDING GEAR WHEELWELL SKIN FS 57 - 69. REPAIRED SKIN (P/N 5911400) PER EA 99-94862.Jul 29, 1995 · N8945E · Doug DC931 · Fuselage Main, Plate/SkinSDR 9512579978Web · oil cannedDURING H-CHECK, FOUND OIL CANNING ON THE PYLON BULKHEAD WEB, RIGHT SIDE FS 965. REPAIRED BULKHEAD (P/N 9912243-81) PER EA 99-100832.Jul 28, 1995 · N9342 · Doug DC931 · Nacelle/Pylon, Bulkhead/FirewallSDR 9511789978Fitting · corrodedDURING H-CHECK, FOUND CORROSION IN THE LONGERON 27 END FITTING AT FS 945. REPLACED END FITTING PER SRM 51-30-2.Jul 28, 1995 · N9342 · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950776Eel Batteries · dischargedPIT - FLT 0519 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSTALLED NEW BATTERIES IN THE POWER PACK. (M)Jul 27, 1995 · N969VJ · Doug DC931 · Emergency LightingSDR 9513189929Doubler · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE MAIN CABIN DOOR CUTOUT, LOWER INTERNAL DOUBLER BENEATH THE SEAL DEPRESSOR. REPAIRED PER EA 99-94734.Jul 27, 1995 · N8923E · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950851Angle · crackedPIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN VERTICAL STAB ATTACH ANGLE VERTICAL LEG AFT END LEFT SIDE. INSTALLED DOUBLER REPAIR 14 INCHES IN LENGTH PER SRM 53-05 FIG 23A. (M)Jul 26, 1995 · N933VJ · Doug DC931 · Vertical StabilizerSDR 9511749991Bulkhead · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 69 PRESSURE PANEL TO WHEEL WELL WEB ATTACH FITTING, RIGHT SIDE. REPLACED FITTING PER SRM 51-01.Jul 26, 1995 · N8957E · Doug DC931 · Fuselage Main, BulkheadSDR USAA950772Duct · blownLGA - FLT NR 0329 - DURING CLIMB, FLIGHT EXPERIENCED A RAPID DECOMPRESSION. AN EMERGENCY WAS DECLARED AND A DESCENT WAS MADE TO 10,000 FEET. CABIN PRESSURE DID NOT RAISE ABOVE 14,000 FEET PRE-EMPTING THE OXYGEN MASKS TO DEPLOY. THE FLIGHT DIVERTED TO LGA ANDJul 25, 1995 · N941VJ · Doug DC931 · Cabin Cooling SystemSDR USAA950770Eel Wire · chafingBWI - FLT 0589 - THE EMERGENCY LIGHTS WERE POPPING THE CIRCUIT BREAKER. MAINTENANCE REPAIRED WIRES THAT WERE FOUND TO BE CHAFING IN THE CEILING OF THE AFT LAVATORY AGAINST THE WATER LINE. (M)Jul 25, 1995 · N963VJ · Doug DC931 · Emergency LightingSDR ABXA9500650Frame · damagedDURING C - CHECK INSPECTION, A FUSELAGE FRAME AT STA 897 BETWEEN LONGERONS 30 AND 29 R WAS FOUND WITH IMPROPERLY DRILLED HOLES. REPAIRED IAW ABX REA D953-12219-MR.Jul 25, 1995 · N906AX · Doug DC931 · Fuselage Main, FrameSDR 9513179969Frame · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE OVERWING EMERGENCY EXIT DOOR PAN ADJACENT TO THE NR 14 STOP FITTING. REPAIRED PAN (P/N 5913195-1) PER EA 99-98720.Jul 25, 1995 · N9333 · Doug DC931 · Emergency ExitsSDR ABXA9500648Rib · crackedDURING C - CHECK INSPECTION, SEVERAL RIBS WERE FOUND CRACKED IN THE VERTICAL STABILIZER LEADING EDGE. REPAIRED OR REPLACED RIBS IAW DC-9 SUPP., SRM DRAWING K05159, AND DC-9 SRM 51-30-5, 51-30-2 AND 51-30-3.Jul 24, 1995 · N906AX · Doug DC931 · Vertical Stabilizer, Spar/RibSDR 9511249964Handle · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE HANDLE FROM THE CLIPS. ADJUSTED THE HANDLE PER MAINTENANCE MANUAL 53-50-03.Jul 24, 1995 · N912RW · Doug DC931 · Aerodynamic FairingsSDR 9511149998Radar Tr Unit · malfunctionedWHILE ENROUTE DTW-DFW, RADAR FAILED TO PAINT KNOWN WEATHER. RADAR TEST OK. RADAR WAS OCCASIONALLY SPOKING AND DOES NOT PAINT GROUND RETURN. DIVERTED TO MEM FOR MAINTENANCE, DUE TO THUNDERSTORMS ENROUTE TO DFW. REPLACED THE RADAR TRANSCEIVER. PERFORMED SYSJul 23, 1995 · N8934E · Doug DC931 · Weather Radar SystemSDR 9511129952Alt Indicator · failedDURING CLIMB AT APPROXIMATELY 6,000 FEET, THE NR 1 ALTIMETER AND ALTITUDE ALTERTED OFF FLAGS DISPLAYED. ATTEMPTED RESET OF ALTIMETER, FLAGS RETRACTED THEN RETURNED. FLIGHT RETURNED TO ORIGIN WITHOUT INCIDENT. REPLACED THE NR 1 ALTIMETER INDICATOR, SYSTEM CHJul 23, 1995 · N916RW · Doug DC931 · Altimeter, Barometric/EncoderSDR ABXA9500651Frame · damagedDURING C - CHECK INSPECTION, FOUND THE FUSELAGE FRAME AT STA 1059, LONGERON 5L, GOUGED. REPAIRED IAW ABX REA D953-12144-MR.Jul 19, 1995 · N906AX · Doug DC931 · Fuselage Main, FrameSDR 9511929964Web · oil cannedDURING H-CHECK, FOUND OIL CANNING IN THE PYLON BULKHEAD WEB LEFT AND RIGHT SIDES. REPAIRED WEB (P/N 9912243-81,-4) PER EA 99-100828.Jul 19, 1995 · N912RW · Doug DC931 · Nacelle/Pylon, Bulkhead/FirewallSDR USAA950801Jamb · crackedPIT - DURING RON CHECK MAINTENANCE, FOUND A 1.5 INCH CRACK IN THE TOP LEFT CORNER OF THE VENTRAL DOOR JAM. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 29. (M)Jul 18, 1995 · N987VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950800Frame · crackedPIT - DURING RON CHECK, FOUND A 2 INCH CRACK AT AFT VENTRAL DOOR LEFT SIDE ABOVE TOP LEFT DOOR STOP. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 30. (M)Jul 18, 1995 · N987VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500649Gussett · crackedDURING C - CHECK INSPECTI0N, FOUND A CRACK IN THE GUSSET OF THE VENTRAL DOOR JAMB, RIGHT SIDE, FORWARD EDGE. REPAIRED IAW ABX REA D953-12213-MR.Jul 18, 1995 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500580Eel Battery · dischargedDURING PREDEPARTURE CHECK, FOUND COCKPIT EMERGENCY LIGHTS VERY DIM. REPLACED BATTERIES IAW DC-9 SUPP MM 33-53-0. OPS CHECKED GOOD.Jul 17, 1995 · N907AX · Doug DC931 · Emergency LightingSDR 9511299964Blkhd Fitting · crackedDURING H-CHECK, FOUND A ONE INCH CRACK IN THE PRESSURE BULKHEAD WING SPAR TO T-CAP ATTACH FITTING AT LONGERON 24L. REPLACED FITTING PER SRM 51-30-5.Jul 17, 1995 · N912RW · Doug DC931 · Fuselage Main, BulkheadSDR 9511069907Controller · failedLOSS OF CABIN PRESSURE OCCURRED DURING CRUISE FLIGHT ENROUTE MEM-MIA. CABIN ALTITUDE REACHED 11,000 FEET AND CAPTAIN DECLARED AN EMERGENCY. OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN. PRESSURIZATION WAS REGAINED THROUGH MANUAL CONTROL AND FLIGHT CONTINUED Jul 17, 1995 · N957N · Doug DC931 · Cabin Pressure ControllerSDR 9511909997Longeron · crackedDURING H-CHECK, FOUND 2 INCH CRACK IN LONGERON 29L AT FS 570. REPAIRED LONGERON (P/N 5920319-504), PER EA 99-97107.Jul 15, 1995 · N8933E · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA950769Eel Battery Pack · dischargedCLT -FLT NR 1437 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED GOOD. (M)Jul 13, 1995 · N971VJ · Doug DC931 · Emergency LightingSDR 95ZZZX4155Oleo Seals · stickingSTL - FLT 246 - AFTER TAKEOFF, LANDING GEAR HANDLE WAS LOCKED IN THE DOWN POSITION. FOUND NOSE LANDING GEAR OLEO STICKING IN THE COMPRESSED POSITION. REPLACED NOSE LANDING GEAR SEALS, MFG KIT P/N A03772REVH. NOSE GEAR OPERATION CHECKED NORMAL. CHECK C - 6-Jul 13, 1995 · N977Z · Doug DC931 · Nose/Tail Landing Gear Strut/AxleSDR 9519059946Blkhd Web · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 604 BULKHEAD WEB LOWER AFT EDGE. REPAIRED WEB (P/N 5914865-23), PER EA 99-92255.Jul 13, 1995 · N8926E · Doug DC931 · Fuselage Main, BulkheadSDR 9513169929Skin · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A .25 INCH CRACK IN THE FUSELAGE SKIN FS 197 AT LONGERON 22L. REPAIRED SKIN PER EA 99-94700.Jul 13, 1995 · N8923E · Doug DC931 · Fuselage Main, Plate/SkinSDR 9511049997Frame · corrodedDURING "H" CHECK, FOUND CORROSION ON THE FS 84 FRAME FITTING LOWER RIGHT SIDE. REPLACED FITTING PER SRM 51-30-1 AND 51-30-5.Jul 13, 1995 · N8933E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9511019964Fitting · crackedDURING "H" CHECK, FOUND CORROSION ON THE FORWARD SERVICE DOOR JAMB FITTING LOWER FORWARD CORNER. REPLACED FITTING PER SRM 51-30-5.Jul 13, 1995 · N912RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9510819953Connector · malfunctionedCLIMBING OUT OF MSP, THE NR 1 OIL TEMPERATURE INDICATED 170 DEGREES, THEN BEGAN FLUCTUATING BETWEEN 100 TO 170 DEGREES. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE CANNON PLUG ON THE OIL TEMPERATURE SENSOR, SYSTEM CHECK OK. Jul 13, 1995 · N918RW · Doug DC931 · Engine Oil TemperatureSDR 9510799953Temp Sensor · malfunctionedCLIMBOUT OF MSP, THE NR 1 ENGINE OIL TEMPERATURE WAS FLUCTUATING AND SEEMED TO STABILIZE AT 170 DEGREES. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TEMPERATURE SENSOR, SYSTEM OPERATION APPEARED TO BE NORMAL. AIRCRAFT RJul 13, 1995 · N918RW · Doug DC931 · Engine Oil TemperatureSDR 9510779958Door Switch · out of adjustDURING APPROACH INTO RAP, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. ADJUSTED LEFT MAIN GEAR DOOR SWITCH, OPERATIONAL CJul 13, 1995 · N917RW · Doug DC931 · Landing Gear Position and WarningSDR ABXA9500647Retainer · crackedDURING C - CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03, FOUND THE LEFT OVERHEAD WINDOW OUTER RETAINER CRACKED. REPAIRED IAW EA AD-56-03239-MA.Jul 12, 1995 · N906AX · Doug DC931 · Flight Compartment WindowsSDR 9513159929Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 30 AT FS 813. REPAIRED LONGERON PER EA 99-97390.Jul 12, 1995 · N8923E · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9511279997Jamb · crackedDURING H-CHECK, FOUND A CRACK IN THE GALLEY SERVICE DOOR JAMB PAN, FORWARD UPPER CORNER. REPAIRED PAN (P/N 5921326-501) PER EA 99-100800.Jul 12, 1995 · N8933E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9511009997Fitting · corrodedDURING "H" CHECK, FOUND A ONE INCH CRACK IN THE LONGERON 24R, 25R, AND 26R END FITTINGS AT FS 587. REPLACED FITTINGS PER SRM 51-30-2.Jul 12, 1995 · N8933E · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950893Frame · corrodedPIT - DURING Q-3/CX-2 INSPECTION, FOUND LEVEL 2 CORROSION AT BELTFRAME 20 INCHES BY 2 INCHES BETWEEN LONGERON 27L AND 27R AT STATION 980 (CORROSION TASK REF C51-53300). CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-03 PG 4A FIG 2A. (M)Jul 10, 1995 · N982VJ · Doug DC931 · Fuselage Main, FrameSDR USAA950885Keel Beam · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH CRACK RT SIDE OF KEEL BEAM RIB. INSTALLED ANGLE DOUBLER REPAIRS PER SRM 53-03 FIG 12. (M)Jul 10, 1995 · N982VJ · Doug DC931 · Fuselage Main, KeelSDR USAA950884Clips · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 3 INCH CRACKS IN SKIN CLIPS AT STATION 637 LONGERON 26L AND STATION 658 LONGERON 25L. INSTALLED ANGLE DOUBLERS PER SRM 53-03 PAGE 51. (M)Jul 10, 1995 · N982VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950883Angle · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES LEFT AND RT AT STATION 1076. REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223. (M)Jul 10, 1995 · N982VJ · Doug DC931 · Vertical StabilizerSDR 95ZZZX3419Actuator · failedSTL - FLT 651 - DURING LANDING, SMOKE APPEARED IN COCKPIT. FOUND AUTO GROUND SPOILER ACTUATOR, MFG PN 1040T100-5, HAD OVERHEATED CAUSING SMOKE. REPLACED AUTO GROUND SPOILER ACTUATOR AND OPERATION CHECKED NORMAL. CHECK C - 8-16-94 - STL.Jul 10, 1995 · N982PS · Doug DC931 · Drag Control ActuatorSDR 95ZZZM496Angle · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES LEFT AND RT AT STATION 1076. REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223. REF USAA950883.Jul 10, 1995 · N982VJ · Doug DC931 · Vertical StabilizerSDR 95ZZZM307Actuator · failedSTL - DURING LANDING, SMOKE APPEARED IN COCKPIT. FOUND AUTO GROUND SPOILER ACTUATOR, MFG P/N 1040T100-5, HAD OVERHEATED CAUSING SMOKE. REPLACED AUTO GROUND SPOILER ACTUATOR AND OPERATION CHECKED NORMAL. (M)Jul 10, 1995 · N982PS · Doug DC931 · Drag Control ActuatorSDR 9511269997Skin · crackedDURING H-CHECK, FOUND .1250 INCH AND .0625 INCH CRACKS IN THE FUSELAGE SKIN NEAR THE MAIN CABIN DOOR FS 200, LONGERON 14L. REPAIRED SKIN (P/N 5911406-59) PER EA 99-100799.Jul 10, 1995 · N8933E · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9500834Skin · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 94-03-01, A PREVIOUS REPAIR WAS FOUND CRACKED. REPAIRED IAW ABX REA D953-12134-MR.Jul 7, 1995 · N906AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9500833Skin · damagedDURING C-CHECK INSPECTION, A PREVIOUS REPAIR WAS FOUND TO BE DAMAGED AT THE FORWARD ENTRY DOOR JAMB. REPAIRED IAW ABX REA D953-12135-MR.Jul 7, 1995 · N906AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9500586Doubler · crackedDURING COMPLIANCE OF A.D. 90-18-3; S.B. 56-11, X-RAY INDICATED CRACK IN THE LEFT EYEBROW WINDOW RETAINER. REPLACED DOUBLER IAW DOUGLAS REWORK DRAWING 5952965.Jul 7, 1995 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500585Doubler · crackedDURING COMPLIANCE OF A.D. 90-80-3; S.B. 56-11, X-RAY INDICATED A CRACK IN THE RIGHT EYEBROW WINDOW RETAINER. REPLACED DOUBLER IAW DOUGLAS REWORK DRAWING 5952965.Jul 7, 1995 · N945AX · Doug DC931 · Fuselage Miscellaneous Structure
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